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0:5419-Mar-2019230AIR COND
1:0419-Mar-201911031406:12ENG 2
1:0419-Mar-201911031406:12ENG 1
1:0419-Mar-201911031406:12AIRCRAFT
Average DailyUtilization
Last ActualDate
Events/LandingsHoursTracking Rate
YR-TRQReg No:
24-Mar-2019 6:11AM
20-Nov-2013
Owner: S.C. TOYO AVIATION S.R.L.
Print Date:
Airworthiness:
Aircraft Serial:
Aircraft Model: 510 - CITATION MUSTANG
Unit:
510-0433
-0433
CESCOM 10 - Aircraft Status Report
(ENG) DUE 2
(ENG) DUE 1
Maintenance Inspections
City Part Serial No
Part Number C/W Time 1
C/W Time 2 + or -
Adj. TBO 1
TBO 2 TSO 2
TSO 1
Remains
RemainsDescription
Drawing # / Task #Position
Item Code
Mod Lvl
MTH 20-Nov-2013 A/R055001 ACCOMPLISH HARD/OVERWEIGHT LANDINGS CHECK
MTH 20-Nov-2013 A/R055002 ACCOMPLISH OVERSPEED CHECK
MTH 20-Nov-2013 A/R055003 ACCOMPLISH DANGEROUS AIR TURBULANCE CHECK
MTH 20-Nov-2013 A/R055004 ACCOMPLISH LIGHTNING STRIKE CHECK
MTH 20-Nov-2013 A/R055005 ACCOMPLISH FOREIGN OBJECT DAMAGE CHECK
MTH 20-Nov-2013 A/R
055006 ACCOMPLISH TOWING WITH FUEL UNBALANCE OR HIGH DRAG/SIDE LOADS CHECK
MTH 20-Nov-2013 A/R
055007 ACCOMPLISH TOWING BEYOND MECHANICAL LIMITS WITH GUST LOCK ENGAGED CHECK
MTH 20-Nov-2013 A/R
055008 ACCOMPLISH TOWING BEYOND MECHANICAL LIMITS WITH GUST LOCK DISENGAGED CHECK
LDG
HRS
MTH
904
1099:24
15-May-2018
450 1549:24 143:12
5-12-01
EDDL
INSPECTION DOCUMENT 01
ACH
LDG
HRS
MTH
155
677
788:24
31-May-2017
900 1688:24 282:12
5-12-02
EDDL
INSPECTION DOCUMENT 02
LDG
HRS
MTH
999
1248:24
26-Sep-2018
1350 2598:24 1192:12
5-12-03
EDDL
INSPECTION DOCUMENT 03
HRS
MTH
0
20-Nov-2013
1800 1800 393:48
5-12-04 INSPECTION DOCUMENT 04
HRS
MTH
0
20-Nov-2013
3150 3150 1743:48
5-12-05 INSPECTION DOCUMENT 05
LDG
HRS
MTH
999
1248:24
26-Sep-2018 12 30-Sep-2019 6 m 6 d5-12-06
EDDL
INSPECTION DOCUMENT 06
LDG
HRS
MTH
999
1248:24
26-Sep-2018 12 30-Sep-2019 6 m 6 d
A256000
EDDL
DETAILED INSPECTION FIRST AID KIT: INSPECTION DOCUMENT 06
LDG
HRS
MTH
999
1248:24
26-Sep-2018 12A-40841253
C352 30-Sep-2019 6 m 6 d
B262100
EDDL
FUNCTIONAL CHECK PORTABLE FIRE EXTINGUISHER (WEIGHT CHECK): INSPECTION DOCUMENT 06
ACH
LDG
HRS
MTH
170
785
935:48
25-Oct-2017 24 31-Oct-2019 7 m 7 d5-12-07
EDDL
INSPECTION DOCUMENT 07
LDG
HRS
MTH
785
935:48
25-Oct-2017 36
5-12-08
EDDL
INSPECTION DOCUMENT 08 (PLEASE REFER TO INDIVIDUAL SUBTASKS FOR DUE TIMES)
MTH 27-Jul-2017 368329
40005369-2 31-Jul-2020 16 m 7 d
B323001
EDDL
RESTORATION LANDING GEAR EMERGENCY PNEUMATIC BOTTLE (HYDROSTATIC TEST): INSPECTION DOCUMENT 08
Page 1 of 50NOTE: Item Codes in italics show pre-migration CESCOM item codes and position (provided for cross-reference). Remains calculated from PrintDate for calendar items.
0:5419-Mar-2019230AIR COND
1:0419-Mar-201911031406:12ENG 2
1:0419-Mar-201911031406:12ENG 1
1:0419-Mar-201911031406:12AIRCRAFT
Average DailyUtilization
Last ActualDate
Events/LandingsHoursTracking Rate
YR-TRQReg No:
24-Mar-2019 6:11AM
20-Nov-2013
Owner: S.C. TOYO AVIATION S.R.L.
Print Date:
Airworthiness:
Aircraft Serial:
Aircraft Model: 510 - CITATION MUSTANG
Unit:
510-0433
-0433
CESCOM 10 - Aircraft Status Report
(ENG) DUE 2
(ENG) DUE 1
Maintenance Inspections
City Part Serial No
Part Number C/W Time 1
C/W Time 2 + or -
Adj. TBO 1
TBO 2 TSO 2
TSO 1
Remains
RemainsDescription
Drawing # / Task #Position
Item Code
Mod Lvl
MTH 27-Jul-2017 366245
40005399-1 31-Jul-2020 16 m 7 d
B324002
EDDL
RESTORATION EMERGENCY BRAKE PNEUMATIC BOTTLE (HYDROSTATIC TEST): INSPECTION DOCUMENT 08
ACH
LDG
HRS
MTH
145
592
687:12
29-Oct-2016 60
5-12-10
EDDL
INSPECTION DOCUMENT 10 (PLEASE REFER TO INDIVIDUAL SUBTASKS FOR DUE TIMES)
MTH 01-Sep-2016 6054968B1
30401102-2 30-Sep-2021 30 m 6 d
B262004
EDDL
RESTORATION FIRE EXTINGUISHER BOTTLE (HYDROSTATIC TEST): INSPECTION DOCUMENT 10
MTH 20-Nov-2013 72 30-Nov-2019 8 m 6 d5-12-11 INSPECTION DOCUMENT 11
MTH 01-Jan-2015 72A-40841253
C352 31-Jan-2021 22 m 7 d
A262100 RESTORATION PORTABLE FIRE EXTINGUISHER (INTERNAL INSPECTION): INSPECTION DOCUMENT 11
MTH 20-Nov-2013 144
5-12-12 INSPECTION DOCUMENT 12 (PLEASE REFER TO INDIVIDUAL SUBTASKS FOR DUE TIMES)
MTH 01-Jan-2015 144A-40841253
C352 31-Jan-2027 94 m 7 d
B262101 RESTORATION PORTABLE FIRE EXTINGUISHER (HYDROSTATIC TEST): INSPECTION DOCUMENT 12
LDG
HRS
MTH
999
1248:24
26-Sep-2018
450
12
1698:24
30-Sep-2019
292:12
6 m 6 d5-12-13
EDDL
INSPECTION DOCUMENT 13
LDG
HRS
MTH
999
1248:24
26-Sep-2018
900
12
2148:24
30-Sep-2019
742:12
6 m 6 d5-12-14
EDDL
INSPECTION DOCUMENT 14
HRS
MTH
1380:06
20-Feb-2019
1350
24
2730:06
28-Feb-2021
1323:54
23 m 4 d5-12-15
UNK
INSPECTION DOCUMENT 15
ACH
LDG
HRS
MTH
145
592
687:12
29-Oct-2016
1350
36
2037:12
31-Oct-2019
631
7 m 7 d5-12-16
EDDL
INSPECTION DOCUMENT 16
ACH
LDG
HRS
MTH
145
592
687:12
29-Oct-2016
1800
36
2487:12
31-Oct-2019
1081
7 m 7 d5-12-17
EDDL
INSPECTION DOCUMENT 17
ACH
LDG
HRS
MTH
145
592
687:12
29-Oct-2016
2250
36
2937:12
31-Oct-2019
1531
7 m 7 d5-12-18
EDDL
INSPECTION DOCUMENT 18
ACH
LDG
HRS
MTH
170
785
935:48
25-Oct-2017
2700
48
3635:48
31-Oct-2021
2229:36
31 m 7 d5-12-20
EDDL
INSPECTION DOCUMENT 20
LDG
HRS
MTH
999
1248:24
26-Sep-2018 12 30-Sep-2019 6 m 6 d5-12-21
EDDL
INSPECTION DOCUMENT 21
LDG
HRS
MTH
785
935:48
25-Oct-2017 24
5-12-22
EDDL
INSPECTION DOCUMENT 22 (PLEASE REFER TO INDIVIDUAL SUBTASKS FOR DUE TIMES)
MTH 24-Oct-2017 24299044A
261440-1143 31-Oct-2019 7 m 7 dAIRSPEED
B341001
EDDL
CALIBRATION TEST INDICATOR 14 CFR PART 91.411: INSPECTION DOCUMENT 22
MTH 24-Oct-2017 241SW005757
011-01110-01 31-Oct-2019 7 m 7 dNO. 1
B341001
EDDL
CALIBRATION TEST GDC 74B AIRDATA SYSTEM 14 CFR PART 91.411: INSPECTION DOCUMENT 22
Page 2 of 50NOTE: Item Codes in italics show pre-migration CESCOM item codes and position (provided for cross-reference). Remains calculated from PrintDate for calendar items.
0:5419-Mar-2019230AIR COND
1:0419-Mar-201911031406:12ENG 2
1:0419-Mar-201911031406:12ENG 1
1:0419-Mar-201911031406:12AIRCRAFT
Average DailyUtilization
Last ActualDate
Events/LandingsHoursTracking Rate
YR-TRQReg No:
24-Mar-2019 6:11AM
20-Nov-2013
Owner: S.C. TOYO AVIATION S.R.L.
Print Date:
Airworthiness:
Aircraft Serial:
Aircraft Model: 510 - CITATION MUSTANG
Unit:
510-0433
-0433
CESCOM 10 - Aircraft Status Report
(ENG) DUE 2
(ENG) DUE 1
Maintenance Inspections
City Part Serial No
Part Number C/W Time 1
C/W Time 2 + or -
Adj. TBO 1
TBO 2 TSO 2
TSO 1
Remains
RemainsDescription
Drawing # / Task #Position
Item Code
Mod Lvl
MTH 24-Oct-2017 241SW005747
011-01110-01 31-Oct-2019 7 m 7 dNO. 2
B341001
EDDL
CALIBRATION TEST GDC 74B AIRDATA SYSTEM 14 CFR PART 91.411: INSPECTION DOCUMENT 22
MTH 24-Oct-2017 24181749C
162350-1161 31-Oct-2019 7 m 7 dSTANDBY
B341001
EDDL
CALIBRATION TEST ALTIMETER 14 CFR PART 91.411: INSPECTION DOCUMENT 22
ACH
LDG
HRS
MTH
170
785
935:48
25-Oct-2017 24 31-Oct-2019 7 m 7 d
B341001
EDDL
FUNCTIONAL CHECK PITOT-STATIC SYSTEM (AIRPLANES WITH AIR DATA COMPUTER P/N 011-01110-00 OR 011-01110-01) : INSPECTION DOCUMENT 22
MTH 24-Oct-2017 24RCE01645
7510700-953 31-Oct-2019 7 m 7 dLEFT
B345000
EDDL
CALIBRATION TEST TRANSPONDER 14 CFR PART 91.413 : INSPECTION DOCUMENT 22
MTH 24-Oct-2017 24RCE01646
7510700-953 31-Oct-2019 7 m 7 dRIGHT
B345000
EDDL
CALIBRATION TEST TRANSPONDER 14 CFR PART 91.413 : INSPECTION DOCUMENT 22
MTH 20-Nov-2013 A/R
5-12-28 INSPECTION DOCUMENT 28 (PLEASE REFER TO INDIVIDUAL SUBTASKS FOR DUE TIMES)
LDG
HRS
MTH
825
973:12
09-Jan-2018 A/R1016
3-1640LEFT
B324000
LOWW
DETAILED INSPECTION MAIN LANDING GEAR WHEEL SPECIAL (NDI): INSPECTION DOCUMENT 28
LDG
HRS
MTH
825
973:12
09-Jan-2018 A/R1012
3-1640RIGHT
B324000
LOWW
DETAILED INSPECTION MAIN LANDING GEAR WHEEL SPECIAL (NDI): INSPECTION DOCUMENT 28
LDG
HRS
MTH
825
973:12
09-Jan-2018 A/R533
3-1642
B324000
LOWW
DETAILED INSPECTION NOSE LANDING GEAR WHEEL SPECIAL (NDI): INSPECTION DOCUMENT 28
ACH
LDG
HRS
MTH
170
785
935:48
25-Oct-2017
1800
48
2735:48
31-Oct-2021
1329:36
31 m 7 d5-12-30
EDDL
INSPECTION DOCUMENT 30
LDG
HRS
MTH
904
1099:24
15-May-2018
450 1549:24 143:12
5-12-31
EDDL
INSPECTION DOCUMENT 31
LDG
MTH
0
20-Nov-2013
1800
72
1800
30-Nov-2019
697
8 m 6 d5-12-32 INSPECTION DOCUMENT 32
HRS
MTH
0
20-Nov-2013
2250
72
2250
30-Nov-2019
843:48
8 m 6 d5-12-33 INSPECTION DOCUMENT 33
HRS
MTH
1380:06
20-Feb-2019
900
125-12-34 INSPECTION DOCUMENT 34
HRS
MTH
1380:06
20-Feb-2019
900
12G03034871
S4324-1
2280:06
29-Feb-2020
873:54
11 m 5 d
B243003
UNK
FUNCTIONAL CHECK MAIN SHIP BATTERY TELEDYNE GILL LEAD-ACID BATTERY (CAPACITY CHECK): INSPECTION DOCUMENT 34
HRS
MTH
1380:06
20-Feb-2019 6 31-Aug-2019 5 m 7 d5-12-35
UNK
INSPECTION DOCUMENT 35
LDG
HRS
MTH
904
1099:24
15-May-2018
500 1599:24 193:12
5-12-MA
EDDL
INSPECTION DOCUMENT MA
ACH
LDG
HRS
MTH
155
677
788:24
31-May-2017
950 1738:24 332:12
5-12-MB
EDDL
INSPECTION DOCUMENT MB
Page 3 of 50NOTE: Item Codes in italics show pre-migration CESCOM item codes and position (provided for cross-reference). Remains calculated from PrintDate for calendar items.
0:5419-Mar-2019230AIR COND
1:0419-Mar-201911031406:12ENG 2
1:0419-Mar-201911031406:12ENG 1
1:0419-Mar-201911031406:12AIRCRAFT
Average DailyUtilization
Last ActualDate
Events/LandingsHoursTracking Rate
YR-TRQReg No:
24-Mar-2019 6:11AM
20-Nov-2013
Owner: S.C. TOYO AVIATION S.R.L.
Print Date:
Airworthiness:
Aircraft Serial:
Aircraft Model: 510 - CITATION MUSTANG
Unit:
510-0433
-0433
CESCOM 10 - Aircraft Status Report
(ENG) DUE 2
(ENG) DUE 1
Maintenance Inspections
City Part Serial No
Part Number C/W Time 1
C/W Time 2 + or -
Adj. TBO 1
TBO 2 TSO 2
TSO 1
Remains
RemainsDescription
Drawing # / Task #Position
Item Code
Mod Lvl
HRS
MTH
0
20-Nov-2013
4000 4000 2593:48
5-12-MC INSPECTION DOCUMENT MC
LDG
HRS
MTH
999
1248:24
26-Sep-2018 12 30-Sep-2019 6 m 6 d5-12-MD
EDDL
INSPECTION DOCUMENT MD
ACH
LDG
HRS
MTH
145
592
687:12
29-Oct-2016
1400
36
2087:12
31-Oct-2019
681
7 m 7 d5-12-ME
EDDL
INSPECTION DOCUMENT ME
HRS
MTH
0
20-Nov-2013
12000 12000 10593:48
5-12-MF INSPECTION DOCUMENT MF
HRS
MTH
0
20-Nov-2013
12000 12000 10593:48
A551001 INSPECT/SURFACE EDDY CURRENT HORIZONTAL STABILIZER FRONT SPAR UPPER FLANGE AND SPLICE STRAPS (BL 0.00 - BL 6.00): INSPECTIONDOCUMENT MF
HRS
MTH
0
20-Nov-2013
5000 5000 3593:48
5-12-MG INSPECTION DOCUMENT MG
HRS
MTH
0
20-Nov-2013
8250 8250 6843:48
5-12-MH INSPECTION DOCUMENT MH
HRS
MTH
0
20-Nov-2013
12000 12000 10593:48
5-12-MI INSPECTION DOCUMENT MI
HRS
MTH
0
20-Nov-2013
10600 10600 9193:48
5-12-MJ INSPECTION DOCUMENT MJ
HRS
MTH
0
20-Nov-2013
10400 10400 8993:48
5-12-MK INSPECTION DOCUMENT MK
LDG
HRS
MTH
785
935:48
27-Oct-2017 A/R080001
EDDL
ACCOMPLISH AIRCRAFT WEIGHT AND BALANCE
ACH
LDG
HRS
MTH
145
592
687:12
29-Oct-2016 372ESD 16G 647-001
13083-5 31-Jul-2022 40 m 7 dLEFT
262003A REPLACE FIRE EXT CARTRIDGE
ACH
LDG
HRS
MTH
145
592
687:12
29-Oct-2016 372ESD 16G 647-001
13083-5 31-Jul-2022 40 m 7 dRIGHT
262003A REPLACE FIRE EXT CARTRIDGE
MTH 01-Jun-2015 60
695979003
4441073-04030-Jun-2020 15 m 6 dB351001
EDDL
RESTORATION OXYGEN BOTTLE HYDROSTATIC TEST
LDG
HRS
MTH
999
1248:24
26-Sep-2018
450
12
(1698:24)1698:24
30-Sep-2019
292:12
6 m 6 dE1
052001
EDDL
ENGINE 450 HOUR/ 12 MONTH INSPECTION
LDG
HRS
MTH
999
1248:24
26-Sep-2018
450
12
(1698:24)1698:24
30-Sep-2019
292:12
6 m 6 dE2
052001
EDDL
ENGINE 450 HOUR/ 12 MONTH INSPECTION
LDG
HRS
MTH
999
1248:24
26-Sep-2018 A/RE1
710010
EDDL
COMPRESSOR WASH
LDG
HRS
MTH
999
1248:24
26-Sep-2018 A/RE2
710010
EDDL
COMPRESSOR WASH
HRS
MTH
0
20-Nov-2013
3500 (3500)3500 2093:48E1
720000 PERFORM ENGINE OVERHAUL
HRS
MTH
0
20-Nov-2013
3500 (3500)3500 2093:48E2
720000 PERFORM ENGINE OVERHAUL
Page 4 of 50NOTE: Item Codes in italics show pre-migration CESCOM item codes and position (provided for cross-reference). Remains calculated from PrintDate for calendar items.
0:5419-Mar-2019230AIR COND
1:0419-Mar-201911031406:12ENG 2
1:0419-Mar-201911031406:12ENG 1
1:0419-Mar-201911031406:12AIRCRAFT
Average DailyUtilization
Last ActualDate
Events/LandingsHoursTracking Rate
YR-TRQReg No:
24-Mar-2019 6:11AM
20-Nov-2013
Owner: S.C. TOYO AVIATION S.R.L.
Print Date:
Airworthiness:
Aircraft Serial:
Aircraft Model: 510 - CITATION MUSTANG
Unit:
510-0433
-0433
CESCOM 10 - Aircraft Status Report
(ENG) DUE 2
(ENG) DUE 1
Maintenance Inspections
City Part Serial No
Part Number C/W Time 1
C/W Time 2 + or -
Adj. TBO 1
TBO 2 TSO 2
TSO 1
Remains
RemainsDescription
Drawing # / Task #Position
Item Code
Mod Lvl
HRS
MTH
0
20-Nov-2013
1750 (1750)1750 343:48E1
720001 PERFORM ENGINE HOT SECTION INSPECTION
HRS
MTH
0
20-Nov-2013
1750 (1750)1750 343:48E2
720001 PERFORM ENGINE HOT SECTION INSPECTION
MTH 20-Nov-2013 144 30-Nov-2025 80 m 6 dE1
720003 INSPECT LOW UTILIZATION ENGINE
MTH 20-Nov-2013 144 30-Nov-2025 80 m 6 dE2
720003 INSPECT LOW UTILIZATION ENGINE
MTH 20-Nov-2013 A/RE1
720020 MONITORING OIL CONSUMPTION TREND
MTH 20-Nov-2013 A/RE2
720020 MONITORING OIL CONSUMPTION TREND
HRS
MTH
1750 (1750)1750 343:48
E1
726040 REPLACE STARTER GENERATOR GEAR-SHAFT SPLINE ADAPTER
HRS
MTH
1750 (1750)1750 343:48
E2
726040 REPLACE STARTER GENERATOR GEAR-SHAFT SPLINE ADAPTER
LDG
HRS
MTH
999
1248:24
26-Sep-2018
900
12
(2148:24)2148:24
30-Sep-2019
742:12
6 m 6 dE1
731020
EDDL
CHECK/REPLACE FUEL FILTER ELEMENT
LDG
HRS
MTH
999
1248:24
26-Sep-2018
900
12
(2148:24)2148:24
30-Sep-2019
742:12
6 m 6 dE2
731020
EDDL
CHECK/REPLACE FUEL FILTER ELEMENT
HRS
MTH
0
20-Nov-2013
1750DE1CAA0391
35C5974-01
(1750)1750 343:48E1
731055 REPLACE FUEL MANIFOLD
HRS
MTH
0
20-Nov-2013
1750DE1CAA0378
35C5974-01
(1750)1750 343:48E2
731055 REPLACE FUEL MANIFOLD
HRS
MTH
0
20-Nov-2013
1750SN-UNKNOWN
PN
(1750)1750 343:48
E1
733020 FUNCTIONAL TEST FUEL FILTER IMPENDING BYPASS SWITCH
HRS
MTH
0
20-Nov-2013
1750SN-UNKNOWN
PN
(1750)1750 343:48
E2
733020 FUNCTIONAL TEST FUEL FILTER IMPENDING BYPASS SWITCH
HRS
MTH
0
20-Nov-2013
1750 (1750)1750 343:48
E1
772001 FUNCTIONAL TEST OF THE T6 THERMOCOUPLE WIRING HARNESS AND ASSEMBLY
HRS
MTH
0
20-Nov-2013
1750 (1750)1750 343:48
E2
772001 FUNCTIONAL TEST OF THE T6 THERMOCOUPLE WIRING HARNESS AND ASSEMBLY
MTH 20-Nov-2013 O/CE1
790010 CHANGE ENGINE OIL/MONITOR /ANALYZE OIL QUALITY
MTH 20-Nov-2013 O/CE2
790010 CHANGE ENGINE OIL/MONITOR /ANALYZE OIL QUALITY
LDG
HRS
MTH
592
687:12
29-Oct-2016
900 (1587:12)1587:12 181E1
790015
EDDL
REPLACE OIL FILTER ELEMENT
LDG
HRS
MTH
592
687:12
29-Oct-2016
900 (1587:12)1587:12 181E2
790015
EDDL
REPLACE OIL FILTER ELEMENT
HRS
MTH
1380:06
20-Feb-2019
100
6SN-UNKNOWN
PN
(1480:06)1480:06
31-Aug-2019
73:54
5 m 7 dE1
793015
UNK
REMOVE CHIP COLLECTOR AND EXAMINE FOR METALLIC DEBRIS
Page 5 of 50NOTE: Item Codes in italics show pre-migration CESCOM item codes and position (provided for cross-reference). Remains calculated from PrintDate for calendar items.
0:5419-Mar-2019230AIR COND
1:0419-Mar-201911031406:12ENG 2
1:0419-Mar-201911031406:12ENG 1
1:0419-Mar-201911031406:12AIRCRAFT
Average DailyUtilization
Last ActualDate
Events/LandingsHoursTracking Rate
YR-TRQReg No:
24-Mar-2019 6:11AM
20-Nov-2013
Owner: S.C. TOYO AVIATION S.R.L.
Print Date:
Airworthiness:
Aircraft Serial:
Aircraft Model: 510 - CITATION MUSTANG
Unit:
510-0433
-0433
CESCOM 10 - Aircraft Status Report
(ENG) DUE 2
(ENG) DUE 1
Maintenance Inspections
City Part Serial No
Part Number C/W Time 1
C/W Time 2 + or -
Adj. TBO 1
TBO 2 TSO 2
TSO 1
Remains
RemainsDescription
Drawing # / Task #Position
Item Code
Mod Lvl
HRS
MTH
1380:06
20-Feb-2019
100
6SN-UNKNOWN
PN
(1480:06)1480:06
31-Aug-2019
73:54
5 m 7 dE2
793015
UNK
REMOVE CHIP COLLECTOR AND EXAMINE FOR METALLIC DEBRIS
Page 6 of 50NOTE: Item Codes in italics show pre-migration CESCOM item codes and position (provided for cross-reference). Remains calculated from PrintDate for calendar items.
0:5419-Mar-2019230AIR COND
1:0419-Mar-201911031406:12ENG 2
1:0419-Mar-201911031406:12ENG 1
1:0419-Mar-201911031406:12AIRCRAFT
Average DailyUtilization
Last ActualDate
Events/LandingsHoursTracking Rate
YR-TRQReg No:
24-Mar-2019 6:11AM
20-Nov-2013
Owner: S.C. TOYO AVIATION S.R.L.
Print Date:
Airworthiness:
Aircraft Serial:
Aircraft Model: 510 - CITATION MUSTANG
Unit:
510-0433
-0433
CESCOM 10 - Aircraft Status Report
(ENG) DUE 2
(ENG) DUE 1
Components
City Part Serial No
Part Number C/W Time 1
C/W Time 2 + or -
Adj. TBO 1
TBO 2 TSO 2
TSO 1
Remains
RemainsDescription
Drawing # / Task #Position
Item Code
Mod Lvl
MTH 20-Nov-2013 0O/C22811601
7011190-1-1100005 WEB BOND ASSY-APB WEB ASSY
MTH 20-Nov-2013 0O/C2110
0113-12212002 UNDER FLOOR BLOWER ASSY.
ACH
LDG
HRS
MTH
172
904
1099:24
15-May-2018 O/C933
52811-102213001
9912661-6 EDDL
KAPS II CONTROLLER
MTH 20-Nov-2013 0O/C1617
9912661-7
NO. 1
213002 KAPS II OUTFLOW VALVE
MTH 20-Nov-2013 0O/C1627
9912661-7
NO. 2
213002 KAPS II OUTFLOW VALVE
MTH 20-Nov-2013 0O/C
535
1133610-4
215001
9912660-14
AIR CONDITIONING COMPRESSOR MODULE
MTH 20-Nov-2013 0O/C646
1134620-5215002
9912660-3
CONDENSOR ASSEMBLY
MTH 20-Nov-2013 0O/C132
1134275-13215003
9912660-18
RECEIVER DRYER ASSY
MTH 20-Nov-2013 0O/C976
1133300-1
NO. 1
215004
9912660-7
(BRUSHLESS) EVAPORATOR
MTH 20-Nov-2013 0O/C989
1133300-1
NO. 2
215004
9912660-7
(BRUSHLESS) EVAPORATOR
MTH 20-Nov-2013 0O/C692
1250435-10215005 VANE AXIAL BLOWER ASSY.
MTH 20-Nov-2013 0O/CSN-UNKNOWN
PN
LH
216000 THERMAL ACTUATOR
HRS
MTH
1380:06
20-Feb-2019
0
0O/CSN-UNKNOWN
74S235H6F255
RH
216000 THERMAL ACTUATOR
LDG
HRS
MTH
326
370
06-Dec-2014
326
370
13O/C66307594
011-00877-00
AILERON
221001
EDDL
GSA 80 TORQUE SERVO
HRS
MTH
1380:06
20-Feb-2019 O/C66301010
011-00877-00
RUDDER
221001
UNK
GSA 80 TORQUE SERVO
LDG
HRS
MTH
326
370
06-Dec-2014
326
370
13O/C71308684
011-00878-10
ELEVATOR
221002
EDDL
GSA 81 TORQUE SERVO
LDG
HRS
MTH
326
370
06-Dec-2014
326
370
13O/C71308625
011-00878-10
ELEVATOR TRIM
221002
EDDL
TAB GSA 81 TORQUE SERVO
LDG
HRS
MTH
326
370
06-Dec-2014
326
370
13O/C10905365
011-01436-A2
AILERON
221003
EDDL
GSM 85A SERVO MOUNT
LDG
HRS
MTH
326
370
06-Dec-2014
326
370
13O/C11205405
011-01436-A0
ELEVATOR
221003
EDDL
GSM 85A SERVO MOUNT
LDG
HRS
MTH
326
370
06-Dec-2014
326
370
13O/C11305397
011-01436-A1
ELEVATOR TRIM
221003
EDDL
GSM 85A SERVO MOUNT
MTH 20-Nov-2013 0O/C11005395
011-01436-A3
RUDDER
221003 GSM 85 SERVO MOUNT
Page 7 of 50NOTE: Item Codes in italics show pre-migration CESCOM item codes and position (provided for cross-reference). Remains calculated from PrintDate for calendar items.
0:5419-Mar-2019230AIR COND
1:0419-Mar-201911031406:12ENG 2
1:0419-Mar-201911031406:12ENG 1
1:0419-Mar-201911031406:12AIRCRAFT
Average DailyUtilization
Last ActualDate
Events/LandingsHoursTracking Rate
YR-TRQReg No:
24-Mar-2019 6:11AM
20-Nov-2013
Owner: S.C. TOYO AVIATION S.R.L.
Print Date:
Airworthiness:
Aircraft Serial:
Aircraft Model: 510 - CITATION MUSTANG
Unit:
510-0433
-0433
CESCOM 10 - Aircraft Status Report
(ENG) DUE 2
(ENG) DUE 1
Components
City Part Serial No
Part Number C/W Time 1
C/W Time 2 + or -
Adj. TBO 1
TBO 2 TSO 2
TSO 1
Remains
RemainsDescription
Drawing # / Task #Position
Item Code
Mod Lvl
MTH 20-Nov-2013 0O/C22006493
011-01020-10221004 GMC 710 AFCS CONTROLLER
MTH 20-Nov-2013 0O/C17107223
011-01257-20
NO. 1
231002 GMA 1347D AUDIO PANEL
MTH 20-Nov-2013 0O/C17107226
011-01257-20
NO. 2
231002 GMA 1347D AUDIO PANEL
ACH
LDG
HRS
MTH
117
525
607
25-May-2016
0
0
0O/C2096
VHF10-829
NO. 1
231003
EDDL
VHF COMM ANTENNA
MTH 20-Nov-2013 0O/C1363
VHF10-829
NO. 2
231003 VHF COMM ANTENNA
MTH 20-Nov-2013 0O/C12028
S67-1575-109231011 SAT PHONE ANTENNA
MTH 20-Nov-2013 0O/CP5943
51525-001F
LEFT
243001 DIGITAL GCU
MTH 20-Nov-2013 0O/CP6018
51525-001F
RIGHT
243001 DIGITAL GCU
ACH
LDG
HRS
MTH
117
525
607
25-May-2016 O/C0347
CBS24243002
EDDL
EMER INST BATTERY
HRS
MTH
1380:06
20-Feb-2019
0
0O/CG03034871
S4324-1243007
GILL(7639-30) UNK
MAIN SHIP BATTERY
MTH 20-Nov-2013 0O/CCT-38385
A-931F243015
S3155-1
RELAY DISCONNECT BATTERY
MTH 20-Nov-2013 0O/C
1057
7018920-5LEFT
245002 PCB ASSEMBLY - FUEL CONTROL ASSEMBLY
LDG
HRS
MTH
852
1014:42
13-Feb-2018
0
0
0O/C
1224
7018920-5RIGHT
245002
LGAV
PCB ASSEMBLY - FUEL CONTROL ASSEMBLY
MTH 20-Nov-2013 0O/C603
7018916-9245003 FLAP CONTROL MODULE
MTH 20-Nov-2013 0O/C557
7018917-9
LEFT
245005 ICE PROTECTION CONTROL
MTH 20-Nov-2013 0O/C580
7018918-13
RIGHT
245005 ICE PROTECTION CONTROL
MTH 20-Nov-2013 0O/C
889
7018919-13LEFT
245006 COCKPIT/CABIN ENVIROMENTAL CONTROL
MTH 20-Nov-2013 0O/C
897
7018919-13RIGHT
245006 COCKPIT/CABIN ENVIROMENTAL CONTROL
MTH 20-Nov-2013 0O/C524
7018921-8245008 DOOR MONITOR-
MTH 20-Nov-2013 0O/C538
7018923-12245009 LANDING GEAR MONITOR-
ACH
LDG
HRS
MTH
145
592
687:12
29-Oct-2016
0
0O/C0565
7018924-12
LEFT
245010 EDDLSTART CONTROL
Page 8 of 50NOTE: Item Codes in italics show pre-migration CESCOM item codes and position (provided for cross-reference). Remains calculated from PrintDate for calendar items.
0:5419-Mar-2019230AIR COND
1:0419-Mar-201911031406:12ENG 2
1:0419-Mar-201911031406:12ENG 1
1:0419-Mar-201911031406:12AIRCRAFT
Average DailyUtilization
Last ActualDate
Events/LandingsHoursTracking Rate
YR-TRQReg No:
24-Mar-2019 6:11AM
20-Nov-2013
Owner: S.C. TOYO AVIATION S.R.L.
Print Date:
Airworthiness:
Aircraft Serial:
Aircraft Model: 510 - CITATION MUSTANG
Unit:
510-0433
-0433
CESCOM 10 - Aircraft Status Report
(ENG) DUE 2
(ENG) DUE 1
Components
City Part Serial No
Part Number C/W Time 1
C/W Time 2 + or -
Adj. TBO 1
TBO 2 TSO 2
TSO 1
Remains
RemainsDescription
Drawing # / Task #Position
Item Code
Mod Lvl
ACH
LDG
HRS
MTH
145
592
687:12
29-Oct-2016
0
0O/C0566
7018924-12
RIGHT
245010 EDDLSTART CONTROL
MTH 20-Nov-2013 0O/C571
7018925-11245011 FLAP MONITOR-
MTH 20-Nov-2013 0O/C616
7018927-7245013 DIAGNOSTIC UNIT
MTH 20-Nov-2013 0O/C1112036
85-230-2245014
9912417-3
FUEL FLOW SIGNAL PCB UNIT
MTH 20-Nov-2013 0O/C12068558
10747P03E25245015
UZ100
MASTER INTERIOR SSR UNIT
MTH 20-Nov-2013 0O/C12068545
10747P03E25
RIGHT
245016
UZ102
AVN BUS #1 SENSOR
MTH 20-Nov-2013 0O/C11058294
10747P03E25
LEFT
245017
UZ103
AVN SENSOR
MTH 20-Nov-2013 0O/C11058300
10747P03E25
RIGHT
245018
UZ104
AVN BUS #2 SENSOR
MTH 20-Nov-2013 0O/C12058533
10747P03E10
LEFT
245019
UZ105
IGN #1 SENSOR
MTH 20-Nov-2013 0O/C12058522
10747P03E10
RIGHT
245019
UZ106
IGN #1 SENSOR
MTH 20-Nov-2013 0O/C12058525
10747P03E10
LEFT
245020
UZ107
IGN #2 SENSOR
MTH 20-Nov-2013 0O/C12058521
10747P03E10
RIGHT
245020
UZ108
IGN #2 SENSOR
MTH 20-Nov-2013 0O/C12068553
10747P03E25245021
UZ109
COCKPIT FAN SENSOR
MTH 20-Nov-2013 0O/C11078414
10747P03E25245022
UZ110
CABIN FAN SENSOR
MTH 20-Nov-2013 0O/C11058310
10747P03E25
LEFT
245023
UZ114
LH BOOST PUMP SENSOR
MTH 20-Nov-2013 0O/C12068554
10747P03E25
RIGHT
245023
UZ111
RH BOOST PUMP SENSOR
MTH 20-Nov-2013 0O/C12038466
10747P03E25245024
UZ112
CONDENSER FAN SENSOR
MTH 20-Nov-2013 0O/C12058534
10747P03E10245025
UZ116
DC-DC CONVERTER
MTH 20-Nov-2013 0O/C11068368
10747P03E25245026
UZ200
AVN EMERG SENSOR
MTH 20-Nov-2013 0O/C1167
7018119-1
LEFT
245201 CABIN ALTITUDE MODULE
MTH 20-Nov-2013 0O/C1170
7018119-1
RIGHT
245201 CABIN ALTITUDE MODULE
MTH 20-Nov-2013 0O/CRGA-700815-1
4319027-17251001 GLARESHIELD ASSEMBLY
LDG
HRS
MTH
326
370
04-Dec-2014 25
O/C
12012110840029
P01074-207 01-Nov-2022 43 m 8 dNO. 1
256001 UNK -3LIFE VEST
LDG
HRS
MTH
326
370
04-Dec-2014 21
O/C
12013031990015
P01074-207 01-Mar-2023 47 m 5 dNO. 2
256001 UNK -3LIFE VEST
LDG
HRS
MTH
326
370
04-Dec-2014 25
O/C
12012110840040
P01074-207 01-Nov-2022 43 m 8 dNO. 3
256001 UNK -3LIFE VEST
Page 9 of 50NOTE: Item Codes in italics show pre-migration CESCOM item codes and position (provided for cross-reference). Remains calculated from PrintDate for calendar items.
0:5419-Mar-2019230AIR COND
1:0419-Mar-201911031406:12ENG 2
1:0419-Mar-201911031406:12ENG 1
1:0419-Mar-201911031406:12AIRCRAFT
Average DailyUtilization
Last ActualDate
Events/LandingsHoursTracking Rate
YR-TRQReg No:
24-Mar-2019 6:11AM
20-Nov-2013
Owner: S.C. TOYO AVIATION S.R.L.
Print Date:
Airworthiness:
Aircraft Serial:
Aircraft Model: 510 - CITATION MUSTANG
Unit:
510-0433
-0433
CESCOM 10 - Aircraft Status Report
(ENG) DUE 2
(ENG) DUE 1
Components
City Part Serial No
Part Number C/W Time 1
C/W Time 2 + or -
Adj. TBO 1
TBO 2 TSO 2
TSO 1
Remains
RemainsDescription
Drawing # / Task #Position
Item Code
Mod Lvl
LDG
HRS
MTH
326
370
04-Dec-2014 25
O/C
12012110840022
P01074-207 01-Nov-2022 43 m 8 dNO. 4
256001 UNK -3LIFE VEST
LDG
HRS
MTH
326
370
04-Dec-2014 21
O/C
12013031990023
P01074-207 01-Mar-2023 47 m 5 dNO. 5
256001 UNK -3LIFE VEST
LDG
HRS
MTH
326
370
04-Dec-2014 25
O/C
12012110840023
P01074-207 01-Nov-2022 43 m 8 dNO. 6
256001 UNK -3LIFE VEST
ACH
LDG
HRS
MTH
155
677
788:24
31-May-2017 060372100-020
452-0133 31-May-2022 38 m 7 d256002 EDDLELT BATTERY
MTH 20-Nov-2013 0O/C393149
110-340256004 ELT ANTENNA
MTH 20-Nov-2013 0O/C12625
453-5060256007
C406N
ELT PROCESSOR
ACH
LDG
HRS
MTH
115
471
533:36
23-Nov-2015
0
0O/C214050
3001-212-1004/455-9
NO. 1
261002
9912416-1 EDDL
FIRE -ENGINE LOOP DETECTOR
MTH 20-Nov-2013 0O/C212653
3001-212-1004/455-9
NO. 2
261002
9912416-1
FIRE -ENGINE LOOP DETECTOR
ACH
LDG
HRS
MTH
145
592
687:12
29-Oct-2016
0
0
0O/C54968B1
30401102-2262001
9912048-6 EDDL
FIRE EXTINGUISHER BOTTLE
ACH
LDG
HRS
MTH
145
592
687:12
29-Oct-2016 72ESD 16G 647-001
13083-5 31-Jul-2022 40 m 7 dLEFT
262003
EDDL
FIRE EXT CARTRIDGE
Manufacture Date: 01-Jul-2016
ACH
LDG
HRS
MTH
145
592
687:12
29-Oct-2016 72ESD 16G 647-001
13083-5 31-Jul-2022 40 m 7 dRIGHT
262003
EDDL
FIRE EXT CARTRIDGE
Manufacture Date: 01-Jul-2016
LDG
HRS
MTH
471
533:36
23-Nov-2015
0
0
0O/CA-40841253
C352262004
EDDL
PORTABLE FIRE EXTINGUISHER
MTH 20-Nov-2013 0O/C2029
4319065-3
LEFT
271001 CONTROL WHEEL ASSY
MTH 20-Nov-2013 0O/C2034
4319065-4
RIGHT
271001 CONTROL WHEEL ASSY
MTH 20-Nov-2013 0O/C723
SYLC-53361-1273002
9912639-2
AILERON TRIM ACTUATOR
MTH 20-Nov-2013 0O/C460AC
MP50Y-1275001
9912642-1
FLAP PDU (POWER DRIVE UNIT) UNIT
MTH 20-Nov-2013 0O/C1043
41013930-105
LEFT
275002
9912640-1
FLAP ACTUATOR
MTH 20-Nov-2013 0O/C1054
41013930-106
RIGHT
275002
9912640-2
FLAP ACTUATOR
MTH 20-Nov-2013 0O/C12090447
140527-5900
LEFT
275201
9914344-59
FLAP FLEX SHAFT ASSEMBLY
Page 10 of 50NOTE: Item Codes in italics show pre-migration CESCOM item codes and position (provided for cross-reference). Remains calculated from PrintDate for calendar items.
0:5419-Mar-2019230AIR COND
1:0419-Mar-201911031406:12ENG 2
1:0419-Mar-201911031406:12ENG 1
1:0419-Mar-201911031406:12AIRCRAFT
Average DailyUtilization
Last ActualDate
Events/LandingsHoursTracking Rate
YR-TRQReg No:
24-Mar-2019 6:11AM
20-Nov-2013
Owner: S.C. TOYO AVIATION S.R.L.
Print Date:
Airworthiness:
Aircraft Serial:
Aircraft Model: 510 - CITATION MUSTANG
Unit:
510-0433
-0433
CESCOM 10 - Aircraft Status Report
(ENG) DUE 2
(ENG) DUE 1
Components
City Part Serial No
Part Number C/W Time 1
C/W Time 2 + or -
Adj. TBO 1
TBO 2 TSO 2
TSO 1
Remains
RemainsDescription
Drawing # / Task #Position
Item Code
Mod Lvl
MTH 20-Nov-2013 0O/C12090442
140527-5900
RIGHT
275201
9914344.59
FLAP FLEX SHAFT ASSEMBLY
MTH 20-Nov-2013 0O/C127
2R5211A
LEFT
276001 SPEED BRAKE ACTUATOR
MTH 20-Nov-2013 0O/C37
2R5212A
RIGHT
276001 SPEED BRAKE ACTUATOR
MTH 20-Nov-2013 0O/CC2162
LR45300A
LEFT
282001
9912190-5
PRIMARY EJECTOR
MTH 20-Nov-2013 0O/CC2158
LR45300A
RIGHT
282001
9912190-5
PRIMARY EJECTOR
MTH 20-Nov-2013 0O/C12-0814243
ZSV57282002
9914103-6
TRANSFER VALVE
MTH 20-Nov-2013 0O/C9BH74
1C7-23
LEFT
282003
9912553-1
DC FUEL PUMP
MTH 20-Nov-2013 0O/C9BH73
1C7-23
RIGHT
282003
9912553-1
DC FUEL PUMP
MTH 20-Nov-2013 0O/CC3240
RG45310
L1
282004
9912190-2
SCAVENGE EJECTOR
MTH 20-Nov-2013 0O/CC3187
RG45310
L2
282004
9912190-2
SCAVENGE EJECTOR
MTH 20-Nov-2013 0O/CC3235
RG45310
R1
282004
9912190-2
SCAVENGE EJECTOR
MTH 20-Nov-2013 0O/CCC3241
RG45310
R2
282004
9912190-2
SCAVENGE EJECTOR
MTH 20-Nov-2013 0O/CAA362208
EM9014-3
LEFT
282005
9912014-3
VALVE-FUEL MOTOR
MTH 20-Nov-2013 0O/CAA367068
EM9014-3
RIGHT
282005
9912014-3
VALVE-FUEL MOTOR
MTH 20-Nov-2013 0O/C983
020-251-001
L1
284001
9912664-1
FUEL PROBE
MTH 20-Nov-2013 0O/C962
020-251-002
L2
284001
9912664-2
FUEL PROBE
MTH 20-Nov-2013 0O/C955
020-251-003
L3
284001
9912664-3
FUEL PROBE
MTH 20-Nov-2013 0O/C1072
020-251-004
L4
284001
9912664-4
FUEL PROBE
MTH 20-Nov-2013 0O/C990
020-251-005
L5
284001
9912664-5
FUEL PROBE
MTH 20-Nov-2013 0O/C985
020-251-001
R1
284001
9912664-1
FUEL PROBE
MTH 20-Nov-2013 0O/C1075
020-251-002
R2
284001
9912664-2
FUEL PROBE
MTH 20-Nov-2013 0O/C958
020-251-003
R3
284001
9912664-3
FUEL PROBE
MTH 20-Nov-2013 0O/C1075
020-251-004
R4
284001
9912664-4
FUEL PROBE
MTH 20-Nov-2013 0O/C989
020-251-005
R5
284001
9912664-5
FUEL PROBE
MTH 20-Nov-2013 0O/C1447
367-350-001284002
9912664-6
SIGNAL CONDITIONER
HRS
MTH
0
20-Nov-2013
0
0
7000451B
HM50C-3
7000 5593:48
291001
9912652-2
HYDRAULIC POWER PACK ASSEMBLY
MTH 20-Nov-2013 0O/C39124
19940933-1291003 HYDRAULIC SYS PRESSURE GAUGE
MTH 20-Nov-2013 0O/C
464
80665
291005
9912657-4
HYD POWER PACK PRESSURE SWITCH
Page 11 of 50NOTE: Item Codes in italics show pre-migration CESCOM item codes and position (provided for cross-reference). Remains calculated from PrintDate for calendar items.
0:5419-Mar-2019230AIR COND
1:0419-Mar-201911031406:12ENG 2
1:0419-Mar-201911031406:12ENG 1
1:0419-Mar-201911031406:12AIRCRAFT
Average DailyUtilization
Last ActualDate
Events/LandingsHoursTracking Rate
YR-TRQReg No:
24-Mar-2019 6:11AM
20-Nov-2013
Owner: S.C. TOYO AVIATION S.R.L.
Print Date:
Airworthiness:
Aircraft Serial:
Aircraft Model: 510 - CITATION MUSTANG
Unit:
510-0433
-0433
CESCOM 10 - Aircraft Status Report
(ENG) DUE 2
(ENG) DUE 1
Components
City Part Serial No
Part Number C/W Time 1
C/W Time 2 + or -
Adj. TBO 1
TBO 2 TSO 2
TSO 1
Remains
RemainsDescription
Drawing # / Task #Position
Item Code
Mod Lvl
MTH 20-Nov-2013 0O/C447
8257-3291007
9912657-14
HYDRAULIC MANIFOLD
MTH 20-Nov-2013 0O/C448
2672291008
9912657-2
HYDRAULIC RELIEF VALVE
MTH 20-Nov-2013 0O/C455
80664291009
9912657-3
BRAKE PRESSURE SWITCH
MTH 20-Nov-2013 0O/C445
4251
EXTEND
291010
9912657-5
HYD SOLENOID CONTROL VALVE
MTH 20-Nov-2013 0O/C449
4252
RETRACT
291010
9912657-7
HYD SOLENOID CONTROL VALVE
MTH 20-Nov-2013 0O/C450
9625-1291011
9912657-15
HYDRAULIC DUMP VALVE
MTH 20-Nov-2013 0O/C
1074
7550-2
291013
9912644-2
HYDRAULIC ACCUMULATOR ASSEMBLY
MTH 20-Nov-2013 0O/CNAY7370
P35-4D5317-17
LEFT
301001
9912662-17
WING DE-ICE BOOT
HRS
MTH
1380:06
20-Feb-2019 O/CNEP2970
P35-4D5317-18
RIGHT
301001
9912662-18
UNKWING DE-ICE BOOT
MTH 20-Nov-2013 0O/CNAXX4480
P29S4D5317-05
LEFT
301003
9912662-3
HORIZONTAL STAB DE-ICE BOOT
MTH 20-Nov-2013 0O/CMZCT010
P29S4D5317-06
RIGHT
301003
9912662-4
HORIZONTAL STAB DE-ICE BOOT
MTH 20-Nov-2013 0O/C9575A
1106P55-1
L1
301004 DE-ICE PRESSURE SWITCH
MTH 20-Nov-2013 0O/C9573-A
1106P55-1
L2
301004 DE-ICE PRESSURE SWITCH
MTH 20-Nov-2013 0O/C9567A
1106P55-1
L3
301004 DE-ICE PRESSURE SWITCH
MTH 20-Nov-2013 0O/C9580A
1106P55-1
R1
301004 DE-ICE PRESSURE SWITCH
MTH 20-Nov-2013 0O/C9597A
1106P55-1
R2
301004 DE-ICE PRESSURE SWITCH
MTH 20-Nov-2013 0O/C9579A
1106P55-1
R3
301004 DE-ICE PRESSURE SWITCH
MTH 20-Nov-2013 0O/CNAZ3900
P29S4D5317-13301004
9912662-13
VERT DE-ICE BOOT
MTH 20-Nov-2013 0O/C2850
5285-00-3
LEFT
302001 PRESS REG/SHUTOFF VALVE ASSY
MTH 20-Nov-2013 0O/C2866
5285-00-3
RIGHT
302001 PRESS REG/SHUTOFF VALVE ASSY
MTH 20-Nov-2013 0O/C6708
1173T0759
LEFT
302002 TEMP SWITCH
MTH 20-Nov-2013 0O/C6426
1173T0759
RIGHT
302002 TEMP SWITCH
MTH 20-Nov-2013 0O/CN122336
3D2353-06
L1
304001 DE-ICE VALVE
MTH 20-Nov-2013 0O/CN122662
3D2353-06
L2
304001 DE-ICE VALVE
MTH 20-Nov-2013 0O/C297
7018108-26
LEFT
304002 WINDSHIELD CONTROLLER
MTH 20-Nov-2013 0O/C296
7018108-26
RIGHT
304002 WINDSHIELD CONTROLLER
LDG
MTH
0
20-Nov-2013
0
0
20000433
7041020-5 20000 18897LEFT
321001 MAIN LANDING GEAR TRUNNION ASSEMBLY
Page 12 of 50NOTE: Item Codes in italics show pre-migration CESCOM item codes and position (provided for cross-reference). Remains calculated from PrintDate for calendar items.
0:5419-Mar-2019230AIR COND
1:0419-Mar-201911031406:12ENG 2
1:0419-Mar-201911031406:12ENG 1
1:0419-Mar-201911031406:12AIRCRAFT
Average DailyUtilization
Last ActualDate
Events/LandingsHoursTracking Rate
YR-TRQReg No:
24-Mar-2019 6:11AM
20-Nov-2013
Owner: S.C. TOYO AVIATION S.R.L.
Print Date:
Airworthiness:
Aircraft Serial:
Aircraft Model: 510 - CITATION MUSTANG
Unit:
510-0433
-0433
CESCOM 10 - Aircraft Status Report
(ENG) DUE 2
(ENG) DUE 1
Components
City Part Serial No
Part Number C/W Time 1
C/W Time 2 + or -
Adj. TBO 1
TBO 2 TSO 2
TSO 1
Remains
RemainsDescription
Drawing # / Task #Position
Item Code
Mod Lvl
LDG
MTH
0
20-Nov-2013
0
0
20000431
7041020-6 20000 18897RIGHT
321001 MAIN LANDING GEAR TRUNNION ASSEMBLY
MTH 20-Nov-2013 0O/C415
7042020-1321001 NOSE LANDING GEAR TRUNNION
LDG
MTH
0
20-Nov-2013
0
0
12000197
7041050-5 12000 10897LEFT
321002 MAIN LANDING GEAR OLEO ASSEMBLY
LDG
MTH
0
20-Nov-2013
0
0
12000198
7041050-5 12000 10897RIGHT
321002 MAIN LANDING GEAR OLEO ASSEMBLY
LDG
MTH
0
20-Nov-2013
0
0
2000098
7041030-3 20000 18897LEFT
321003 MAIN LANDING GEAR TRAILING LINK ASSEMBLY
LDG
MTH
0
20-Nov-2013
0
0
2000097
7041030-4 20000 18897RIGHT
321003 MAIN LANDING GEAR TRAILING LINK ASSEMBLY
MTH 20-Nov-2013 0O/C3299
6327504-6
LEFT
322001 MAIN GEAR ACTUATOR UPLOCK
MTH 20-Nov-2013 0O/C3311
6327504-6
RIGHT
322001 MAIN GEAR ACTUATOR UPLOCK
MTH 20-Nov-2013 0O/C
47
7042040-6
322002 NOSE GEAR FORK & PISTON ASSEMBLY
MTH 20-Nov-2013 0O/C1635
6327504-7
NOSE GEAR
322003 UPLOCK ACTUATOR
LDG
MTH
0
20-Nov-2013
0
0
12000416
FA100036-001 12000 10897
322005
9912655-1
NOSE LANDING GEAR DOWNLOCK RELEASE ACTUATOR
LDG
MTH
0
20-Nov-2013
0
0
12000FA100104-1-0431
FA100104-001 12000 10897LEFT
322010
9912653-5
MAIN LANDING GEAR HYDRAULIC ACTUATOR
LDG
MTH
0
20-Nov-2013
0
0
12000FA100105-1-0434
FA100105-001 12000 10897RIGHT
322010
9912653-6
MAIN LANDING GEAR HYDRAULIC ACTUATOR
LDG
MTH
0
20-Nov-2013
0
0
12000442
FA100087-001
12000 10897
322011
9912654-2
NOSE LANDING GEAR ACTUATOR
MTH 20-Nov-2013 0O/CMTM0313
7042030-2322202 SHIMMY DAMPER
LDG
MTH
0
20-Nov-2013
0
0
2000049
7042010-6
20000 18897NOSE
322205 LANDING GEAR STRUT ASSEMBLY
LDG
MTH
0
20-Nov-2013
0
0
20000184
7042120-5
20000 18897NOSE
322206
CHP 4
LANDING GEAR DRAG BRACE ASSY
ACH
LDG
HRS
MTH
170
785
935:48
25-Oct-2017 42288
8329
40005369-230-Apr-2038 229 m 6 d323001
9914678-3 EDDL
LANDING GEAR EMERGENCY PNEUMATIC BOTTLE
Manufacture Date: 28-Apr-2014
ACH
LDG
HRS
MTH
170
785
935:48
25-Oct-2017 113288
6245
40005399-131-May-2032 158 m 7 d323002
9914678-4 EDDL
EMERGENCY BRAKE PNEUMATIC BOTTLE
Manufacture Date: 25-May-2008
MTH 20-Nov-2013 0O/C
39798
19940931-1
323003 EMER BLOW DOWN BTL PRESSURE GAUGE
Page 13 of 50NOTE: Item Codes in italics show pre-migration CESCOM item codes and position (provided for cross-reference). Remains calculated from PrintDate for calendar items.
0:5419-Mar-2019230AIR COND
1:0419-Mar-201911031406:12ENG 2
1:0419-Mar-201911031406:12ENG 1
1:0419-Mar-201911031406:12AIRCRAFT
Average DailyUtilization
Last ActualDate
Events/LandingsHoursTracking Rate
YR-TRQReg No:
24-Mar-2019 6:11AM
20-Nov-2013
Owner: S.C. TOYO AVIATION S.R.L.
Print Date:
Airworthiness:
Aircraft Serial:
Aircraft Model: 510 - CITATION MUSTANG
Unit:
510-0433
-0433
CESCOM 10 - Aircraft Status Report
(ENG) DUE 2
(ENG) DUE 1
Components
City Part Serial No
Part Number C/W Time 1
C/W Time 2 + or -
Adj. TBO 1
TBO 2 TSO 2
TSO 1
Remains
RemainsDescription
Drawing # / Task #Position
Item Code
Mod Lvl
LDG
HRS
MTH
825
973:12
09-Jan-2018
0
0
0O/C6111S00153
021-523-0
LEFT
324001
9912646-1 LOWW
MAIN LANDING GEAR TIRE
LDG
HRS
MTH
825
973:12
09-Jan-2018
0
0
0O/C6147S00368
021-523-0
RIGHT
324001
9912646-1 LOWW
MAIN LANDING GEAR TIRE
LDG
HRS
MTH
825
973:12
09-Jan-2018
0
0
0O/C4269S00234
079-606-0324002
9912649-1 LOWW
NOSE LANDING GEAR TIRE
LDG
HRS
MTH
825
973:12
09-Jan-2018
825
973:12
50O/C1016
3-1640
LEFT
324003
9912645-1
MAIN LANDING GEAR WHEEL
LDG
HRS
MTH
825
973:12
09-Jan-2018
825
973:12
50O/C1012
3-1640
RIGHT
324003
9912645-1 LOWW
MAIN LANDING GEAR WHEEL
LDG
HRS
MTH
825
973:12
09-Jan-2018
825
973:12
50O/C533
3-1642324004
9912648-1 LOWW
NOSE LANDING GEAR WHEEL
ACH
LDG
HRS
MTH
170
785
935:48
25-Oct-2017 O/C064
2-1706-1
LEFT
324005
9912645-3 EDDL
MAIN LANDING GEAR BRAKE ASSY
ACH
LDG
HRS
MTH
170
785
935:48
25-Oct-2017 O/C0763A
2-1706-1
RIGHT
324005
9912645-3 EDDL
MAIN LANDING GEAR BRAKE ASSY
MTH 20-Nov-2013 0O/C898
5145-1
LEFT
324006
9914689-4
SHUTTLE VALVE
MTH 20-Nov-2013 0O/C899
5145-1
RIGHT
324006
9914689-4
SHUTTLE VALVE
MTH 20-Nov-2013 0O/C453
84-75324007
9912650-9
BRAKE METERING VALVE
MTH 20-Nov-2013 0O/C937
466-23-1
LEFT
324101
9912650-5
WHEEL SPEED SENSOR
MTH 20-Nov-2013 0O/C916
466-23-1
RIGHT
324101
9912650-5
WHEEL SPEED SENSOR
MTH 20-Nov-2013 0O/C447
98433-1324101
9912388-10
PARKING BRAKE VALVE
MTH 20-Nov-2013 0O/C302829568
556-3324102
9912650-1
ANTISKID CONTROL UNIT
MTH 20-Nov-2013 0O/C465
211-134-1324103
9912650-6
ANTISKID CONTROL VALVE
MTH 20-Nov-2013 0O/C478
72298324104
9912651-1
EMERGENCY BRAKE VALVE
MTH 20-Nov-2013 0O/C
39799
19940931-1
324105 EMER BRAKE BOTTLE PRESSURE GAUGE
MTH 20-Nov-2013 0O/C982
9912677-3
LEFT
334001 POWER SUPPLY
Page 14 of 50NOTE: Item Codes in italics show pre-migration CESCOM item codes and position (provided for cross-reference). Remains calculated from PrintDate for calendar items.
0:5419-Mar-2019230AIR COND
1:0419-Mar-201911031406:12ENG 2
1:0419-Mar-201911031406:12ENG 1
1:0419-Mar-201911031406:12AIRCRAFT
Average DailyUtilization
Last ActualDate
Events/LandingsHoursTracking Rate
YR-TRQReg No:
24-Mar-2019 6:11AM
20-Nov-2013
Owner: S.C. TOYO AVIATION S.R.L.
Print Date:
Airworthiness:
Aircraft Serial:
Aircraft Model: 510 - CITATION MUSTANG
Unit:
510-0433
-0433
CESCOM 10 - Aircraft Status Report
(ENG) DUE 2
(ENG) DUE 1
Components
City Part Serial No
Part Number C/W Time 1
C/W Time 2 + or -
Adj. TBO 1
TBO 2 TSO 2
TSO 1
Remains
RemainsDescription
Drawing # / Task #Position
Item Code
Mod Lvl
LDG
HRS
MTH
204
255
26-Jun-2014 O/C314
82004-1
RIGHT
334001
9912677-3
EDDLPOWER SUPPLY
MTH 20-Nov-2013 0O/C123
84003-2334002
9912679-3
GROUND RECOGNITION LIGHT
HRS
MTH
0
20-Nov-2013
0
0
8000170
84005-1
8000 6593:48LEFT
334003
9912679-1
ANTI-COLLISION LIGHT
HRS
MTH
0
20-Nov-2013
0
0
8000128
84005-2
8000 6593:48RIGHT
334003
9912679-2
ANTI-COLLISION LIGHT
MTH 20-Nov-2013 0O/C2330
0863B2341001
9912689-1
SWAAT UNIT
MTH 20-Nov-2013 0O/C1SW005757
011-01110-01
NO. 1
341002 GDC 74B AIRDATA SYSTEM
MTH 20-Nov-2013 0O/C1SW005747
011-01110-01
NO. 2
341002 GDC 74B AIRDATA SYSTEM
MTH 20-Nov-2013 0O/C47921150
011-00978-00
NO. 1
341003 GTP 59 OAT PROBE SYSTEM
MTH 20-Nov-2013 0O/C47921151
011-00978-00
NO. 2
341003 GTP 59 OAT PROBE SYSTEM
MTH 20-Nov-2013 0O/C297929
0851LN
LEFT
341004
9912678-1
PITOT PROBE
MTH 20-Nov-2013 0O/C298783
0851LN
RIGHT
341004
9912678-1
PITOT PROBE
MTH 20-Nov-2013 0O/C181749C
162350-1161
STANDBY
342001
S3100-465
ALTIMETER
MTH 20-Nov-2013 0O/C299044A
261440-1143
AIRSPEED
342002 INDICATOR
HRS
MTH
1380:06
20-Feb-2019
1380:06
63O/C46715346
011-00831-00
NO. 1
342003
UNK
GEA 71 ENG/AIRFRAME INTERFACE
HRS
MTH
1380:06
20-Feb-2019
1380:06
63O/C46715406
011-00831-00
NO. 2
342003
UNK
GEA 71 ENG/AIRFRAME INTERFACE
MTH 20-Nov-2013 0O/CNSN
S2800-821342003 MAGNETIC COMPASS
MTH 20-Nov-2013 0O/C86816539
011-00916-10
NO. 1
342004 GDU 1040A DISPLAY
MTH 20-Nov-2013 0O/C86816531
011-00916-10
NO. 2
342004 GDU 1040A DISPLAY
MTH 20-Nov-2013 0O/C42021130
011-00868-10
NO. 1
342005
S3100-483/S3100-517
GRS 77 AHRS UNIT
MTH 20-Nov-2013 0O/C42021145
011-00868-10
NO. 2
342005
S3100-483/S3100-517
GRS 77 AHRS UNIT
ACH
LDG
HRS
MTH
100
424
484:36
06-Aug-2015 1O/C47507864
011-00870-00
NO. 1
342006
LOWW
GMU 44 MAGNETOMETER
LDG
HRS
MTH
978
1220:48
29-Aug-2018 0O/C47521594
011-00870-00
NO. 2
342006
LKPR
GMU 44 MAGNETOMETER
ACH
LDG
HRS
MTH
172
904
1099:24
15-May-2018 O/C43225617
011-01108-10342007 EDDLGDU 1500 MFD UNIT
Page 15 of 50NOTE: Item Codes in italics show pre-migration CESCOM item codes and position (provided for cross-reference). Remains calculated from PrintDate for calendar items.
0:5419-Mar-2019230AIR COND
1:0419-Mar-201911031406:12ENG 2
1:0419-Mar-201911031406:12ENG 1
1:0419-Mar-201911031406:12AIRCRAFT
Average DailyUtilization
Last ActualDate
Events/LandingsHoursTracking Rate
YR-TRQReg No:
24-Mar-2019 6:11AM
20-Nov-2013
Owner: S.C. TOYO AVIATION S.R.L.
Print Date:
Airworthiness:
Aircraft Serial:
Aircraft Model: 510 - CITATION MUSTANG
Unit:
510-0433
-0433
CESCOM 10 - Aircraft Status Report
(ENG) DUE 2
(ENG) DUE 1
Components
City Part Serial No
Part Number C/W Time 1
C/W Time 2 + or -
Adj. TBO 1
TBO 2 TSO 2
TSO 1
Remains
RemainsDescription
Drawing # / Task #Position
Item Code
Mod Lvl
MTH 20-Nov-2013 0O/CJ12-11068
4200-21342008
S3100-513
ATTITUDE INDICATOR
MTH 20-Nov-2013 0O/C4724172
011-00883-20344001 GWX 68 WEATHER RADAR
MTH 20-Nov-2013 0O/C47765997
011-00987-00344002 GDL 69 WEATHER DATA LINK
MTH 20-Nov-2013 0O/C
552-19727
S67-2002-4LEFT
344005 (KRA-405B) RADAR ALTIMETER ANTENNA
MTH 20-Nov-2013 O/C
552-19498
S67-2002-4RIGHT
344005 (KRA-405B) RADAR ALTIMETER ANTENNA
MTH 20-Nov-2013 0O/CKRA405B-14695
066-01153-0202344006 (KRA-405B) RADAR ALTIMETER
MTH 20-Nov-2013 0O/C9983
013-00245-00345001 GPS/WAAS/XM ANTENNA
MTH 20-Nov-2013 0O/CRCE01646
7510700-953
RIGHT
345002 TRANSPONDER
MTH 20-Nov-2013 0O/CRCE01645
7510700-953
LEFT
345003 TRANSPONDER
MTH 20-Nov-2013 0O/C
21805311
011-01054-10
345004 GCU 475 FLIGHT MGMT CONTROL UNIT
MTH 20-Nov-2013 0O/C3283
013-00166-00345005 ADF RECEIVER
MTH 20-Nov-2013 0O/C3812
013-00165-00345006 ADF ANTENNA
MTH 20-Nov-2013 0O/C573
MB10-754-2345007 MARKER BEACON ANTENNA
MTH 20-Nov-2013 0O/C16814
RGS10-48345008 GLIDE SLOPE ANTENNA
MTH 20-Nov-2013 0O/C4789
L10-611-14
LEFT
345009 L-BAND TRANSPONDER ANTENNA
MTH 20-Nov-2013 0O/C4800
L10-611-14
RIGHT
345009 L-BAND TRANSPONDER ANTENNA
MTH 20-Nov-2013 0O/C4750
L10-611-14
UPPER
345009 L-BAND TRANSPONDER ANTENNA
MTH 20-Nov-2013 0O/C4859
L10-611-14
UPPER NO. 2
345009 L-BAND TRANSPONDER ANTENNA
MTH 20-Nov-2013 0O/C2690
VT11-767-3
LEFT
345010 NAV ANTENNA
MTH 20-Nov-2013 0O/C2689
VT11-767-3
RIGHT
345010 NAV ANTENNA
MTH 20-Nov-2013 0O/C35586
066-01070-0001345011 KN63 DME TRANSCEIVER
MTH 20-Nov-2013 0O/C1273
013-00167-00345013 RMI CONVERTER
MTH 20-Nov-2013 0O/C9184
013-00244-00345014 GPS/WAAS/ ANTENNA
MTH 20-Nov-2013 0O/C4760
L10-611-14345015 DME ANTENNA
MTH 20-Nov-2013 O/CTSE01834
9003-500-55905346008 SP-3500 TCAS PROCESSR
MTH 20-Nov-2013 O/CANE36529
7S14081-910346009 TCAS ANTENNA
MTH 20-Nov-2013 0O/C4752
L10-611-14
BOTTOM
346011 TAS ANTENNA
Page 16 of 50NOTE: Item Codes in italics show pre-migration CESCOM item codes and position (provided for cross-reference). Remains calculated from PrintDate for calendar items.
0:5419-Mar-2019230AIR COND
1:0419-Mar-201911031406:12ENG 2
1:0419-Mar-201911031406:12ENG 1
1:0419-Mar-201911031406:12AIRCRAFT
Average DailyUtilization
Last ActualDate
Events/LandingsHoursTracking Rate
YR-TRQReg No:
24-Mar-2019 6:11AM
20-Nov-2013
Owner: S.C. TOYO AVIATION S.R.L.
Print Date:
Airworthiness:
Aircraft Serial:
Aircraft Model: 510 - CITATION MUSTANG
Unit:
510-0433
-0433
CESCOM 10 - Aircraft Status Report
(ENG) DUE 2
(ENG) DUE 1
Components
City Part Serial No
Part Number C/W Time 1
C/W Time 2 + or -
Adj. TBO 1
TBO 2 TSO 2
TSO 1
Remains
RemainsDescription
Drawing # / Task #Position
Item Code
Mod Lvl
MTH 20-Nov-2013 O/C
13622096
7519262-902LEFT
346013 TRANSPONDER CONFIGURATION MODULE
MTH 20-Nov-2013 O/C
136219985
7519262-902RIGHT
346013 TRANSPONDER CONFIGURATION MODULE
ACH
LDG
HRS
MTH
115
471
533:36
19-Nov-2015 1O/C1HQ010337
011-01105-20
NO. 1
346014
DUS
GIA 63W NAV/COMM/LS/GPS UNIT
ACH
LDG
HRS
MTH
172
904
1099:24
15-May-2018 O/C1HQ016602
011-01105-20
NO. 2
346014
EDDL
GIA 63W NAV/COMM/LS/GPS UNIT
ACH
LDG
HRS
MTH
155
677
788:24
31-May-2017 10180695979003
4441073-040 30-Jun-2030 135 m 6 d350001 EDDLOXYGEN BOTTLE
Manufacture Date: 01-Jun-2015
MTH 20-Nov-2013 0O/CF12-10056
MD97-1350002
C668512-0101
OXYGEN PRESSURE GAUGE
LDG
HRS
MTH
904
1099:24
15-May-2018 372116430
MC10-16-101 29-Feb-2024 59 m 5 dLEFT
351001
9914067-41 EDDL
CREW OXYGEN MASK
LDG
HRS
MTH
904
1099:24
15-May-2018 37286373
MC10-16-101 29-Feb-2024 59 m 5 dRIGHT
351001
9914067-41 EDDL
CREW OXYGEN MASK
MTH 20-Nov-2013 0O/CT0883
8315-2
LEFT
361001
9914402-7
PRECOOLER
MTH 20-Nov-2013 0O/CT0882
8315-2
RIGHT
361001
9914402-7
PRECOOLER
MTH 20-Nov-2013 0O/C0879A
2601-34
LEFT
361002 VARIABLE VENTURI VALVE ASSY
LDG
HRS
MTH
999
1248:24
26-Sep-2018
0
0O/C0508A
2601-34
RIGHT
361002
EDDL
VARIABLE VENTURI VALVE ASSY
MTH 20-Nov-2013 0O/C9BH24
1H75-23361003
9912510-2
SERVICE AIR REGULATOR ASSY
MTH 20-Nov-2013 0O/C3365
5253-00-3
LEFT
361004 B/A SHUTOFF VALVE
MTH 20-Nov-2013 0O/C3370
5253-00-3
RIGHT
361004 B/A SHUTOFF VALVE
MTH 20-Nov-2013 0O/CN122340
3D2353-06
R1
361101 DE-ICE VALVE
MTH 20-Nov-2013 0O/CN122657
3D2353-06
R2
361101 DE-ICE VALVE
MTH 20-Nov-2013 0O/C559
S-22560-3522001
9912674-3
CABIN DOOR SEAL
MTH 20-Nov-2013 0O/C607
S-22561522002
9912675-1
ESCAPE HATCH SEAL
LDG
MTH
0
20-Nov-2013
0
0
20000TSW0084
7013022-15 20000 18897LEFT
531001 NOSE LANDING GEAR ATTACH FITTING ASSY
LDG
MTH
0
20-Nov-2013
0
0
20000TSW0082
7013022-16 20000 18897RIGHT
531001 NOSE LANDING GEAR ATTACH FITTING ASSY
Page 17 of 50NOTE: Item Codes in italics show pre-migration CESCOM item codes and position (provided for cross-reference). Remains calculated from PrintDate for calendar items.
0:5419-Mar-2019230AIR COND
1:0419-Mar-201911031406:12ENG 2
1:0419-Mar-201911031406:12ENG 1
1:0419-Mar-201911031406:12AIRCRAFT
Average DailyUtilization
Last ActualDate
Events/LandingsHoursTracking Rate
YR-TRQReg No:
24-Mar-2019 6:11AM
20-Nov-2013
Owner: S.C. TOYO AVIATION S.R.L.
Print Date:
Airworthiness:
Aircraft Serial:
Aircraft Model: 510 - CITATION MUSTANG
Unit:
510-0433
-0433
CESCOM 10 - Aircraft Status Report
(ENG) DUE 2
(ENG) DUE 1
Components
City Part Serial No
Part Number C/W Time 1
C/W Time 2 + or -
Adj. TBO 1
TBO 2 TSO 2
TSO 1
Remains
RemainsDescription
Drawing # / Task #Position
Item Code
Mod Lvl
LDG
MTH
0
20-Nov-2013
0
0
20000TSW0067
7013022-17 20000 18897LEFT
531002
CHP 4
NOSE LANDING GEAR DRAG BRACE FITTING ASSY
LDG
MTH
0
20-Nov-2013
0
0
20000TSW0076
7013022-18 20000 18897RIGHT
531002
CHP 4
NOSE LANDING GEAR DRAG BRACE FITTING ASSY
MTH 20-Nov-2013 0O/C22993117
7012061-3
FWD
534101 ENGINE BEAM
MTH 20-Nov-2013 0O/C23015823
7034001-9
LEFT
552001 ELEVATOR ASSEMBLY
MTH 20-Nov-2013 0O/C23015825
7034001-10
RIGHT
552001 ELEVATOR ASSEMBLY
MTH 20-Nov-2013 0O/C22993847
7031001-1553001 VERTICAL STABILIZER ASSY
MTH 20-Nov-2013 0O/C12151H9187
NP-188601-13
LEFT
561001 WINDSHIELD ASSY, (LH)
MTH 20-Nov-2013 0O/C12111H5280
NP-188601-14
RIGHT
561001 WINDSHIELD ASSY, (LH)
MTH 20-Nov-2013 0O/C2001
93310-1
LEFT
561002
9912746-1
FLIGHT COMPARTMENT SIDE WINDOW
MTH 20-Nov-2013 0O/C1978
93310-2
RIGHT
561002
9912746-2
FLIGHT COMPARTMENT SIDE WINDOW
MTH 20-Nov-2013 0O/C1606
93320-13
L1
562003
9912747-13
CABIN WINDOW
MTH 20-Nov-2013 0O/C1608
93320-13
L2
562003
9912747-13
CABIN WINDOW
MTH 20-Nov-2013 0O/C1639
93320-13
L3
562003
9912747-13
CABIN WINDOW
MTH 20-Nov-2013 0O/C1659
93320-13
R1
562003
9912747-13
CABIN WINDOW
MTH 20-Nov-2013 0O/C1516
93320-13
R2
562003
9912747-13
CABIN (ESCAPE HATCH) WINDOW
MTH 20-Nov-2013 0O/C1592
93320-13
R3
562003
9912747-13
CABIN WINDOW
MTH 20-Nov-2013 0O/C91698
7022022-1
LEFT WING
572001 FWD SPAR
MTH 20-Nov-2013 0O/C90939
7022022-2
RIGHT WING
572001 FWD SPAR
MTH 20-Nov-2013 0O/C92038
7022032-3
LEFT WING
572002 REAR SPAR
MTH 20-Nov-2013 0O/C91113
7022032-4
RIGHT WING
572002 REAR SPAR
MTH 20-Nov-2013 0O/C91025
7022027-1
LEFT WING
572003 MAIN SPAR
MTH 20-Nov-2013 0O/C91716
7022027-2
RIGHT WING
572003 MAIN SPAR
LDG
MTH
0
20-Nov-2013
0
0
20000419
7041165-5
20000 18897LEFT MAIN GEAR
572004 AFT TRUNNION FITTING ASSY
LDG
MTH
0
20-Nov-2013
0
0
20000427
7041165-6
20000 18897RIGHT MAIN GEAR
572004 AFT TRUNNION FITTING ASSY
LDG
MTH
0
20-Nov-2013
0
0
20000429
7041155-9
20000 18897LEFT MAIN GEAR
572005 FWD TRUNNION FITTING ASSY
LDG
MTH
0
20-Nov-2013
0
0
20000413
7041155-10
20000 18897RIGHT MAIN GEAR
572005 FWD TRUNNION FITTING ASSY
LDG
MTH
0
20-Nov-2013
0
0
20000444
7041175-5
20000 18897LEFT MAIN GEAR
572006 SIDE BRACE FITTING ASSY
LDG
MTH
0
20-Nov-2013
0
0
20000441
7041175-6
20000 18897RIGHT MAIN GEAR
572006 SIDE BRACE FITTING ASSY
Page 18 of 50NOTE: Item Codes in italics show pre-migration CESCOM item codes and position (provided for cross-reference). Remains calculated from PrintDate for calendar items.
0:5419-Mar-2019230AIR COND
1:0419-Mar-201911031406:12ENG 2
1:0419-Mar-201911031406:12ENG 1
1:0419-Mar-201911031406:12AIRCRAFT
Average DailyUtilization
Last ActualDate
Events/LandingsHoursTracking Rate
YR-TRQReg No:
24-Mar-2019 6:11AM
20-Nov-2013
Owner: S.C. TOYO AVIATION S.R.L.
Print Date:
Airworthiness:
Aircraft Serial:
Aircraft Model: 510 - CITATION MUSTANG
Unit:
510-0433
-0433
CESCOM 10 - Aircraft Status Report
(ENG) DUE 2
(ENG) DUE 1
Components
City Part Serial No
Part Number C/W Time 1
C/W Time 2 + or -
Adj. TBO 1
TBO 2 TSO 2
TSO 1
Remains
RemainsDescription
Drawing # / Task #Position
Item Code
Mod Lvl
MTH 20-Nov-2013 0O/C445
7051001-1
LEFT
712001
7051001-1
ENG CHANNEL-FWD MOUNT
HRS
MTH
0
20-Nov-2013
0
0
40002078
LM-471-SA11
4000 2593:48LEFT BOTTOM
712001
9912647-1
FWD ENGINE ISOLATOR SYSTEM
HRS
MTH
0
20-Nov-2013
0
0
40002067
LM-471-SA11
4000 2593:48LEFT TOP
712001
9912647-1
FWD ENGINE ISOLATOR SYSTEM
MTH 20-Nov-2013 0O/C399
7051001-2
RIGHT
712001 ENG CHANNEL-FWD MOUNT
HRS
MTH
0
20-Nov-2013
0
0
40002128
LM-471-SA11
4000 2593:48RIGHT BOTTOM
712001
9912647-1
FWD ENGINE ISOLATOR SYSTEM
HRS
MTH
0
20-Nov-2013
0
0
40002120
LM-471-SA11
4000 2593:48RIGHT TOP
712001
9912647-1
FWD ENGINE ISOLATOR SYSTEM
HRS
MTH
0
20-Nov-2013
0
0
8000LK2632
LM-471-SA4
8000 6593:48LEFT
712002
9912647-3
AFT ENGINE ISOLATOR ASSEMBLY
HRS
MTH
0
20-Nov-2013
0
0
8000LK2590
LM-471-SA4
8000 6593:48RIGHT
712002
9912647-3
AFT ENGINE ISOLATOR ASSEMBLY
MTH 20-Nov-2013 0O/C433
7012066-802-1
AFT
712003 ENGINE BEAM
MTH 20-Nov-2013 0O/C454
7051001-3
LEFT
712003 AFT ENGINE MOUNT CHANNEL
MTH 20-Nov-2013 0O/C388
7051001-4
RIGHT
712003 AFT ENGINE MOUNT CHANNEL
E/CLB0887
35C0510-01
NO. 1
71EN1 ENGINE
E/CLB0886
35C0510-01
NO. 2
71EN2 ENGINE
LDG
MTH
0
20-Nov-2013
0
0
10500FRAEPNMP12
35C1940-01
(10500)10500 9397E1
720010 FAN ROTOR
LDG
MTH
0
20-Nov-2013
0
0
10500FRAEPNMP5
35C1940-01
(10500)10500 9397E2
720010 FAN ROTOR
LDG
MTH
0
20-Nov-2013
0
0
5250FRAEPNLB24
35C2311-01
(5250)5250 4147E1
721010 HP TURBINE DISK
LDG
MTH
0
20-Nov-2013
0
0
5250FRAEPNLB25
35C2311-01
(5250)5250 4147E2
721010 HP TURBINE DISK
LDG
MTH
0
20-Nov-2013
0
0
10500FRAEPNHH13
35C2372-01
(10500)10500 9397E1
721020 LP TURBINE DISK
LDG
MTH
0
20-Nov-2013
0
0
10500FRAEPNHH4
35C2372-01
(10500)10500 9397E2
721020 LP TURBINE DISK
LDG
MTH
0
20-Nov-2013
0
0
10500AAPPICTR2021
35C5663-01
(10500)10500 9397E1
723010 IMPELLER AND SHAFT ASSEMBLY
LDG
MTH
0
20-Nov-2013
0
0
10500AAPPIAGV2002
35C5663-01
(10500)10500 9397E2
723010 IMPELLER AND SHAFT ASSEMBLY
LDG
MTH
0
20-Nov-2013
0
0
10500FRAEPNTE24
35C3661-01
(10500)10500 9397E1
725010 HP COMPRESSOR ROTOR
LDG
MTH
0
20-Nov-2013
0
0
10500FRAEPNTE33
35C3661-01
(10500)10500 9397E2
725010 HP COMPRESSOR ROTOR
HRS
MTH
0
20-Nov-2013
0
0
1750SN-UNKNOWN
PN
(1750)1750 343:48E1
726010 AGB STARTER MAGNETIC SEAL
HRS
MTH
0
20-Nov-2013
0
0
1750SN-UNKNOWN
PN
(1750)1750 343:48E2
726010 AGB STARTER MAGNETIC SEAL
MTH 20-Nov-2013 0O/C10072
1103P0448
LEFT
730001
9912033-2
ENGINE FUEL PRESSURE SWITCH
MTH 20-Nov-2013 0O/C10070
1103P0448
RIGHT
730001
9912033-2
ENGINE FUEL PRESSURE SWITCH
MTH 20-Nov-2013 0O/CAAE4676
TFF1573-4
LEFT
733001
9912417-1
FUEL FLOW TRANSMITTER
MTH 20-Nov-2013 0O/CAAE5691
TFF1573-4
RIGHT
733001
9912417-1
FUEL FLOW TRANSMITTER
Page 19 of 50NOTE: Item Codes in italics show pre-migration CESCOM item codes and position (provided for cross-reference). Remains calculated from PrintDate for calendar items.
0:5419-Mar-2019230AIR COND
1:0419-Mar-201911031406:12ENG 2
1:0419-Mar-201911031406:12ENG 1
1:0419-Mar-201911031406:12AIRCRAFT
Average DailyUtilization
Last ActualDate
Events/LandingsHoursTracking Rate
YR-TRQReg No:
24-Mar-2019 6:11AM
20-Nov-2013
Owner: S.C. TOYO AVIATION S.R.L.
Print Date:
Airworthiness:
Aircraft Serial:
Aircraft Model: 510 - CITATION MUSTANG
Unit:
510-0433
-0433
CESCOM 10 - Aircraft Status Report
(ENG) DUE 2
(ENG) DUE 1
Components
City Part Serial No
Part Number C/W Time 1
C/W Time 2 + or -
Adj. TBO 1
TBO 2 TSO 2
TSO 1
Remains
RemainsDescription
Drawing # / Task #Position
Item Code
Mod Lvl
MTH 20-Nov-2013 0O/CDE1CAA0391
35C5974-01
E1
731050 FUEL MANIFOLD
MTH 20-Nov-2013 0O/CDE1CAA0378
35C5974-01
E2
731050 FUEL MANIFOLD
MTH 20-Nov-2013 0O/C17361507
35C0794-05
E1
732101 FUEL METERING UNIT
MTH 20-Nov-2013 0O/C18342291
35C0794-05
E2
732101 FUEL METERING UNIT
MTH 20-Nov-2013 0O/CWDA115791
35C5472-01
E1
741001 IGNITION EXCITER
LDG
HRS
MTH
326
370
06-Dec-2014
0
0
0O/CWDA111456
35C5472-01
E2
741001 EDDLIGNITION EXCITER
MTH 20-Nov-2013 0O/CNSN
35C0844-01
E1 LEFT
741002 IGNITER CABLE
MTH 20-Nov-2013 0O/CNSN
35C0844-01
E2 LEFT
741002 IGNITER CABLE
MTH 20-Nov-2013 0O/CNSN
35C0799-01
E1 RIGHT
741003 IGNITER CABLE
MTH 20-Nov-2013 0O/CNSN
35C0799-01
E2 RIGHT
741003 IGNITER CABLE
MTH 20-Nov-2013 0O/CNSN
35C2353-01
E1 INBOARD
741004 SPARK IGNITER
MTH 20-Nov-2013 0O/CNSN
35C2353-01
E2 INBOARD
741004 SPARK IGNITER
MTH 20-Nov-2013 0O/CNSN
35C2353-01
E1 OUTBOARD
741005 SPARK IGNITER
MTH 20-Nov-2013 0O/CNSN
35C2353-01
E2 OUTBOARD
741005 SPARK IGNITER
MTH 20-Nov-2013 0O/C18231050
35C2851-02
E1
751003 BLEED VALVE ACTUATOR
MTH 20-Nov-2013 0O/C18251392
35C2851-02
E2
751003 BLEED VALVE ACTUATOR
MTH 20-Nov-2013 0O/C12-1072
35C4035-07
E1
761001 FADEC
MTH 20-Nov-2013 0O/C12-1077
35C4035-07
E2
761001 FADEC
MTH 20-Nov-2013 0O/CWA44570
35C3778-04
E1
791001 FUEL TO OIL HEAT EXCHANGER
MTH 20-Nov-2013 0O/CWA44569
35C3778-04
E2
791001 FUEL TO OIL HEAT EXCHANGER
MTH 20-Nov-2013 0O/C8003
102-00083
E1
793001 OIL TEMP SENSOR
MTH 20-Nov-2013 0O/C7998
102-00083
E2
793001 OIL TEMP SENSOR
MTH 20-Nov-2013 0O/C7857-9-382
APTE-304A-250G
E1
793002 OIL PRESSURE TRANSMITER
MTH 20-Nov-2013 0O/C7857-9-397
APTE-304A-250G
E2
793002 OIL PRESSURE TRANSMITER
HRS
MTH
0
20-Nov-2013
0
0
15000985B
MG94E-1
1500 93:48LEFT
801000
9912676-1
STARTER GENERATOR
LDG
HRS
MTH
1039
1303:48
22-Nov-2018
01500916D
MG94E-1
2803:48 1397:36RIGHT
801000
9912676-1 LRBS
STARTER GENERATOR
Page 20 of 50NOTE: Item Codes in italics show pre-migration CESCOM item codes and position (provided for cross-reference). Remains calculated from PrintDate for calendar items.
0:5419-Mar-2019230AIR COND
1:0419-Mar-201911031406:12ENG 2
1:0419-Mar-201911031406:12ENG 1
1:0419-Mar-201911031406:12AIRCRAFT
Average DailyUtilization
Last ActualDate
Events/LandingsHoursTracking Rate
YR-TRQReg No:
24-Mar-2019 6:11AM
20-Nov-2013
Owner: S.C. TOYO AVIATION S.R.L.
Print Date:
Airworthiness:
Aircraft Serial:
Aircraft Model: 510 - CITATION MUSTANG
Unit:
510-0433
-0433
CESCOM 10 - Aircraft Status Report
(ENG) DUE 2
(ENG) DUE 1
Service Bulletins
City Part Serial No
Part Number C/W Time 1
C/W Time 2 + or -
Adj. TBO 1
TBO 2 TSO 2
TSO 1
Remains
RemainsDescription
Drawing # / Task #Position
Item Code
Mod Lvl
LDG
HRS
MTH
904
1099:24
15-May-2018 6RECOMMENDED 22-Jun-2019
Complete
2 m 29 d
SL CIL-99-03 R01
EDDL
MISCELLANEOUS - CORROSION PREVENTION AND CONTROL PROGRAM (CPCP)
COMPLIED WITH - PERFORMED CIL-99-03 REV 01 MISCELLANEOUS - CORROSION PREVENTION AND CONTROL PROGRAM(CPCP), SERVICE LETTER. NO FINDINGS
MOC :
-INFORMATIONAL
SL CIL-99-04 MISCELLANEOUS - INCREMENTAL LIBRARY UPDATES FOR CESVIEW
MOC :
-INFORMATIONAL
SL CIL-99-01 REV02
USE OF CORROSION INHIBITING COMPOUNDS
- INFOMOC :
-RECOMMENDED
SL CIL-99-02 MISCELLANEOUS - AVOID OPERATIONS ON RUNWAYS TREATED WITH RUNWAY DE-ICE (RDI) FLUIDS. AIRCRAFT WASHING RECOMMENDED AFTEREXPOSURE TO RDI FLUIDS
- INFOMOC :
-INFORMATIONAL
SB 510-20-02 STANDARD PRACTICES - CESSNA STANDARD PRACTICES MANUAL (SUPERSEDED BY SL510-20-02 R01)
MOC :
-INFORMATIONAL
SL CIL-20-01 REV02
STANDARD PRACTICES - CESSNA CERTIFICATION OF NONDESTRUCTIVE TESTING FACILITIES/PERSONNEL
- INFOMOC :
-INFORMATIONAL
SL 510-20-01 REV01
CESSNA CERTIFICATION OF NONDESTRUCTIVE TESTING FACILITIES/PERSONNEL (SUPERSEDED BY SL510-20-01 REV 02)
- INFOMOC :
A/RINFORMATIONAL
SL 510-20-01 REV02
CESSNA CERTIFICATION OF NONDESTRUCTIVE TESTING FACILITIES/PERSONNEL (SUPERSEDED BY SL510-20-01 REV 03)
- INFOMOC :
A/RINFORMATIONAL
SL 510-20-01 REV03
CESSNA CERTIFICATION OF NONDESTRUCTIVE TESTING FACILITIES/PERSONNEL (SUPERSEDED BY SL510-20-01 REV 04)
- INFOMOC :
A/RINFORMATIONAL
SL 510-20-01 REV04
STANDARD PRACTICES - CESSNA CERTIFICATION OF NONDESTRUCTIVE TESTING FACILITIES/PERSONNEL (SUPERSEDED BY SL510-20-01 REV 05)
- INFOMOC :
-INFORMATIONAL
SL 510-20-01 REV05
CESSNA CERTIFICATION OF NONDESTRUCTIVE TESTING FACILITIES/PERSONNEL (SUPERSEDED BY CIL-20-01 REV 02)
- INFOMOC :
-INFORMATIONAL
SL 510-20-01 CESSNA CERTIFICATION OF NONDESTRUCTIVE TESTING FACILITIES/PERSONNEL (SUPERSEDED BY SL510-20-01 REV 01)
- INFOMOC :
-INFORMATIONAL
SL 510-20-02 R01 STANDARD PRACTICES - CESSNA STANDARD PRACTICES MANUAL
MOC :
A/RINFORMATIONAL Complete
SL 510-23-01 LIGHTNING RELATED ANOMALIES OF THE GARMIN GMA 1347[D] AUDIO PANEL
COMPLIED WITH - INFOMOC :
Page 21 of 50NOTE: Item Codes in italics show pre-migration CESCOM item codes and position (provided for cross-reference). Remains calculated from PrintDate for calendar items.
0:5419-Mar-2019230AIR COND
1:0419-Mar-201911031406:12ENG 2
1:0419-Mar-201911031406:12ENG 1
1:0419-Mar-201911031406:12AIRCRAFT
Average DailyUtilization
Last ActualDate
Events/LandingsHoursTracking Rate
YR-TRQReg No:
24-Mar-2019 6:11AM
20-Nov-2013
Owner: S.C. TOYO AVIATION S.R.L.
Print Date:
Airworthiness:
Aircraft Serial:
Aircraft Model: 510 - CITATION MUSTANG
Unit:
510-0433
-0433
CESCOM 10 - Aircraft Status Report
(ENG) DUE 2
(ENG) DUE 1
Service Bulletins
City Part Serial No
Part Number C/W Time 1
C/W Time 2 + or -
Adj. TBO 1
TBO 2 TSO 2
TSO 1
Remains
RemainsDescription
Drawing # / Task #Position
Item Code
Mod Lvl
ACH
LDG
HRS
DAYS
145
592
687:12
29-Oct-2016 -MANDATORY Complete
SL 510-24-14 REV01 EDDL
ELECTRICAL POWER - PRINTED CIRCUIT BOARD VERIFICATION
COMPLIED WITHMOC :
ACH
LDG
HRS
DAYS
145
592
687:12
29-Oct-2016 -MANDATORY
SL 510-24-14
EDDL
ELECTRICAL POWER - PRINTED CIRCUIT BOARD VERIFICATION (SUPERSEDED BY SL510-24-14 REV 01)
DEFERRED - DEFERRED TO SL510-24-14 REV1MOC :
-OPTIONAL
SB 510-25-04 EQUIPMENT/FURNISHINGS - CABIN COMFORT IMPROVEMENTS
MOC :
A/ROPTIONAL CompleteSB 510-28-02 LOCKING FUEL CAP INSTALLATION
COMPLIED WITH - AT DELIVERYMOC :
HRS
MTH
687:12
29-Oct-2016 -RECOMMENDED
SB 510-30-06 REV01
ICE AND RAIN PROTECTION - WINDSHIELD TEMPERATURE CONTROLLER ENHANCEMENT
DEFERRED - REV 1 POSTPONED TO NEXT MX INPUTMOC :
MTH -RECOMMENDED
SB 510-30-06 ICE AND RAIN PROTECTION - WINDSHIELD TEMPERATURE CONTROLLER ENHANCEMENT (SUPERSEDED BY 510-30-06 REV 01)
MOC :
A/RINFORMATIONAL Complete
SL 510-30-01 REV01
APPROVED DEICING PROGRAM UPDATES (SUPERSEDED BY SL510-30-01 REV 02)
COMPLIED WITH - INFOMOC :
A/RINFORMATIONAL Complete
SL 510-30-01 REV02
APPROVED DEICING PROGRAM UPDATES (SUPERSEDED BY SL510-30-01 REV 03)
COMPLIED WITH - INFOMOC :
A/RINFORMATIONAL Complete
SL 510-30-01 REV03
APPROVED DEICING PROGRAM UPDATES (SUPERSEDED BY (SUPERSEDED BY SL510-30-01 REV 04)
COMPLIED WITH - INFOMOC :
A/RINFORMATIONAL Complete
SL 510-30-01 REV04
ICE AND RAIN PROTECTION - APPROVED DEICING PROGRAM UPDATES (SUPERSEDED BY SL510-30-01 REV 05)
COMPLIED WITH - INFOMOC :
-INFORMATIONAL Complete
SL 510-30-01 REV05
ICE AND RAIN PROTECTION - APPROVED DEICING PROGRAM UPDATES (SUPERSEDED BY SL510-30-01 REV 06)
COMPLIED WITH - INFOMOC :
-INFORMATIONAL Complete
SL 510-30-01 REV06
ICE AND RAIN PROTECTION - APPROVED DEICING PROGRAM UPDATES (SUPERSEDED BY CIL-30-01)
COMPLIED WITH - INFOMOC :
A/RINFORMATIONAL Complete
SL 510-30-01 APPROVED DEICING PROGRAM UPDATES (SUPERSEDED BY SL510-30-01 REV 01)
COMPLIED WITH - INFOMOC :
-INFORMATIONAL
SL CIL-31-01 INDICATING/RECORDING SYSTEMS - CVR, FDR, AND CVDR 90-DAY BATTERY UNDERWATER LOCATOR BEACON (ULB) INSTALLATION
MOC :
-INFORMATIONAL N/A
SL CIL-32-04 WIRELESS TIRE PRESSURE MONITORING SYSTEM INSTALLATION
NOT APPLICABLE - PARTS NOT INSTALLEDMOC :
Page 22 of 50NOTE: Item Codes in italics show pre-migration CESCOM item codes and position (provided for cross-reference). Remains calculated from PrintDate for calendar items.
0:5419-Mar-2019230AIR COND
1:0419-Mar-201911031406:12ENG 2
1:0419-Mar-201911031406:12ENG 1
1:0419-Mar-201911031406:12AIRCRAFT
Average DailyUtilization
Last ActualDate
Events/LandingsHoursTracking Rate
YR-TRQReg No:
24-Mar-2019 6:11AM
20-Nov-2013
Owner: S.C. TOYO AVIATION S.R.L.
Print Date:
Airworthiness:
Aircraft Serial:
Aircraft Model: 510 - CITATION MUSTANG
Unit:
510-0433
-0433
CESCOM 10 - Aircraft Status Report
(ENG) DUE 2
(ENG) DUE 1
Service Bulletins
City Part Serial No
Part Number C/W Time 1
C/W Time 2 + or -
Adj. TBO 1
TBO 2 TSO 2
TSO 1
Remains
RemainsDescription
Drawing # / Task #Position
Item Code
Mod Lvl
ACH
LDG
HRS
DAYS
145
638
738:54
31-Mar-2017 -MANDATORY N/A
SL 510-32-07
LRBS
LANDING GEAR - MAIN LANDING GEAR BRAKE VERIFICATION
NOT APPLICABLE - PARTS NOT INSTALLEDMOC :
ACH
LDG
HRS
DAYS
170
785
935:48
27-Oct-2017 -MANDATORY Complete
SL 510-32-08
EDDL
LANDING GEAR - TRANSMIT GOODRICH SERVICE BULLETIN 2-1706-1-32-1 LANDING GEAR - MAIN BRAKE ASSEMBLY, - INTRODUCTION OF ANINSPECTION PROCEDURE TO MAKE SURE THE WEAR INDICATOR PINS WERE SET CORRECTLY
COMPLIED WITH - NOT APPLICABLE TO RH BRAKE BECAUSE S/N 0763A, LH BRAKE CHECKED IAW SL INSTRUCTION ANDFOUND BOTH WEAR PIN ON BRAKE S/N 0064 WITHIN LIMITS AND MARKED AS REQUESTED BY BF GOODRICH SBNOTE BOTHBRAKES ARE IN OVERHAULED CONDITION AND WERE REPLACED AT THIS TIME
MOC :
-OPTIONAL
SB 510-33-01 LIGHTS - LANDING/TAXI LIGHT IMPROVEMENT
MOC :
A/ROPTIONAL
CompleteSB 510-34-10 GARMIN SYNTHETIC VISION TECHNOLOGY INSTALLATION
COMPLIED WITH - AT DELIVERYMOC :
ACH
LDG
HRS
MTH
145
592
687:12
29-Oct-2016 -MANDATORY
CompleteSB 510-34-16 REV01 EDDL
NAVIGATION - GARMIN GRS-77 AHRS SOFTWARE UPDATE
COMPLIED WITHMOC :
-OPTIONAL N/A
SB 510-34-17 REV01
NAVIGATION - GARMIN G1000 ADS-B OUT INSTALLATION WITH SOFTWARE UPGRADE (SUPERSEDED BY 510-34-17 REV 02)
NOT APPLICABLE - PART NOT INSTALLEDMOC :
-OPTIONAL
SB 510-34-17 REV02
NAVIGATION - GARMIN G1000 ADS-B OUT INSTALLATION WITH SOFTWARE UPGRADE (SUPERSEDED BY SB 510-34-17 REV 03)
MOC :
-OPTIONAL
SB 510-34-17 REV03
NAVIGATION - GARMIN G1000 ADS-B OUT INSTALLATION WITH SOFTWARE UPGRADE
MOC :
MTH -RECOMMENDED New Req
SB 510-34-18 NAVIGATION - GARMIN G1000 ADS-B OUT SOFTWARE UPDATE
MOC :
-INFORMATIONAL
SL CIL-34-07 NAVIGATION - TRANSMITTAL OF GARMIN SERVICE ADVISORY 1604 WORLDWIDE NAVIGATION DATABASE
MOC :
A/RINFORMATIONAL
SL 510-34-01 TRANSMITTAL OF GARMIN SERVICE ALERT 070424-00
- INFOMOC :
A/RINFORMATIONAL
SL 510-34-03 TRANSMITTAL OF GARMIN SERVICE ADVISORY NUMBER 0745 REVISION A, G1000 WAAS GPS CDI SCALING
- INFOMOC :
A/RINFORMATIONAL
SL 510-34-05 GARMIN G1000 TRANSPONDER OPERATION CHANGE
- INFOMOC :
Page 23 of 50NOTE: Item Codes in italics show pre-migration CESCOM item codes and position (provided for cross-reference). Remains calculated from PrintDate for calendar items.
0:5419-Mar-2019230AIR COND
1:0419-Mar-201911031406:12ENG 2
1:0419-Mar-201911031406:12ENG 1
1:0419-Mar-201911031406:12AIRCRAFT
Average DailyUtilization
Last ActualDate
Events/LandingsHoursTracking Rate
YR-TRQReg No:
24-Mar-2019 6:11AM
20-Nov-2013
Owner: S.C. TOYO AVIATION S.R.L.
Print Date:
Airworthiness:
Aircraft Serial:
Aircraft Model: 510 - CITATION MUSTANG
Unit:
510-0433
-0433
CESCOM 10 - Aircraft Status Report
(ENG) DUE 2
(ENG) DUE 1
Service Bulletins
City Part Serial No
Part Number C/W Time 1
C/W Time 2 + or -
Adj. TBO 1
TBO 2 TSO 2
TSO 1
Remains
RemainsDescription
Drawing # / Task #Position
Item Code
Mod Lvl
A/RINFORMATIONAL
SL 510-34-06 TRANSMITTAL OF GARMIN SERVICE ALERT NO. 0811, G1000 SERIES FLIGHT PLAN SEQUENCING ISSUE
- INFOMOC :
A/RINFORMATIONAL
SL 510-34-07 TRANSMITTAL OF GARMIN SERVICE ADVISORY NO.: 0825 LPV AND LNAV/VNAV APPROACHES WITH THREE-CHARACTER AIRPORT IDENTIFIERS
- INFOMOC :
A/RINFORMATIONAL
SL 510-34-08 GPS/WAAS LOSS OF RECEPTION IN ALASKA, NORTHWEST CANADA, AND EASTERN RUSSIA
- INFOMOC :
A/RINFORMATIONAL
SL 510-34-10 TRANSMITTAL OF GARMIN SERVICE ADVISORY NO. 0915 REVISION A, G1000 SERIES NAVIGATION SUSPENDING DURING NON-PRECISIONAPPROACHES
- INFOMOC :
-INFORMATIONAL
SL 510-34-12 NAVIGATION - TRANSMITTAL OF GARMIN SERVICE ADVISORY NO. 0933 REVISION A, SYSTEM MAY SELECT NAV 2 AS A NAVIGATION SOURCE DURINGAPPROACH
- INFOMOC :
A/RINFORMATIONAL
SL 510-34-13 TRANSMITTAL OF GARMIN SERVICE ADVISORY NO. 0922 REVISION A, VOR OR LOC/ILS APPROACHES
- INFOMOC :
ACH
LDG
HRS
MTH
145
592
687:12
29-Oct-2016 -INFORMATIONAL
Complete
SL 510-34-22
EDDL
NAVIGATION - TRANSMITTAL OF GARMIN SERVICE ADVISORY NO 1612 2015 IGRF (INTERNATIONAL GEOMAGNETIC REFERENCE FIELD) MAGNETICFIELD MODEL
COMPLIED WITHMOC :
LDG
HRS
MTH
677
788:12
01-Jun-2017 -RECOMMENDED N/A
SL 510-34-23
BBU
NAVIGATION - GARMIN G1000 DATABASE CARD REPLACEMENT
NOT APPLICABLE - NOT APPLICABLEDUE TO CARD REPLACEMENT NOT REQUIRED DUE TO THE -43 INSTALLEDCARDS.REPLACEMENT TO THE NEW -44 CARDS IS ONLY REQUIRED WITHPREVIOUSLY INSTALLATION OF THE-45 AS POSTEDIN THE SERVICE LETTEREFFECTIVITYTABLE. NO ACTION REQUIRED.
MOC :
-INFORMATIONAL
SL 510-34-24 NAVIGATION - TRANSMITTAL OF GARMIN SERVICE ADVISORY 1729 (REV A) LOCKED WAYPOINTS
MOC :
-INFORMATIONAL
SL 510-34-25 NAVIGATION - TRANSMITTAL OF GARMIN SERVICE ADVISORY 1838 EMERGENCY DESCENT MODE (EDM)
MOC :
-INFORMATIONAL
SL 510-34-26 NAVIGATION - TRANSMITTAL OF GARMIN SERVICE ADVISORY 1802 INCORRECT DIRECT-TO NAVIGATION FOLLOWING INTERCEPT (INTRCPT) LEG
MOC :
LDG
HRS
DAYS
MTH
503
580:06
07-Mar-2016 -MANDATORY N/A
SL CIL-35-05
LRBS
OXYGEN - TRANSMITTAL OF ZODIAC AEROSPACE SB MCF-SBU-35-001
NOT APPLICABLE - PARTS INSTALLED IN THE AIRCRAFT ARE NOT AFFECTED BY THE SERVICE BULLETIN MCF-SBU-35-001.LEFT CREW OXYGEN MASK P/N: MC10-16-101 S/N: SE72089RIGHT CREW OXYGEN MASK P/N: MC10-16-101 S/N: SE72097
MOC :
MTH 20-Nov-2013 -CATEGORY 5 CompleteE1
SB PW600-72-63002
REPLACEMENT OF TURBINE EXHAUST CASE (TEC) COWL BRACKETS
COMPLIED WITH - AT MANUFACTUREMOC :
Page 24 of 50NOTE: Item Codes in italics show pre-migration CESCOM item codes and position (provided for cross-reference). Remains calculated from PrintDate for calendar items.
0:5419-Mar-2019230AIR COND
1:0419-Mar-201911031406:12ENG 2
1:0419-Mar-201911031406:12ENG 1
1:0419-Mar-201911031406:12AIRCRAFT
Average DailyUtilization
Last ActualDate
Events/LandingsHoursTracking Rate
YR-TRQReg No:
24-Mar-2019 6:11AM
20-Nov-2013
Owner: S.C. TOYO AVIATION S.R.L.
Print Date:
Airworthiness:
Aircraft Serial:
Aircraft Model: 510 - CITATION MUSTANG
Unit:
510-0433
-0433
CESCOM 10 - Aircraft Status Report
(ENG) DUE 2
(ENG) DUE 1
Service Bulletins
City Part Serial No
Part Number C/W Time 1
C/W Time 2 + or -
Adj. TBO 1
TBO 2 TSO 2
TSO 1
Remains
RemainsDescription
Drawing # / Task #Position
Item Code
Mod Lvl
MTH 20-Nov-2013 -CATEGORY 5 CompleteE2
SB PW600-72-63002
REPLACEMENT OF TURBINE EXHAUST CASE (TEC) COWL BRACKETS
COMPLIED WITH - AT MANUFACTUREMOC :
MTH 20-Nov-2013 -CATEGORY 9 CompleteE1
SB PW600-72-63003
INTRODUCTION OF ADDITIONAL BALANCING WEIGHTS FOR THE FAN TRIM BALANCE
COMPLIED WITH - AT MANUFACTUREMOC :
MTH 20-Nov-2013 -CATEGORY 9 CompleteE2
SB PW600-72-63003
INTRODUCTION OF ADDITIONAL BALANCING WEIGHTS FOR THE FAN TRIM BALANCE
COMPLIED WITH - AT MANUFACTUREMOC :
MTH 20-Nov-2013 -CATEGORY 5 CompleteE1
SB PW600-72-63005
REPLACEMENT OF BLEED-VALVE-ASSEMBLY BALL BEARING
COMPLIED WITH - AT MANUFACTUREMOC :
MTH 20-Nov-2013 -CATEGORY 5 CompleteE2
SB PW600-72-63005
REPLACEMENT OF BLEED-VALVE-ASSEMBLY BALL BEARING
COMPLIED WITH - AT MANUFACTUREMOC :
MTH 20-Nov-2013 -CATEGORY 9
Complete
E1
SB PW600-72-63006
REPLACEMENT OF SHIPPING CONTAINER HARDWARE
COMPLIED WITH - AT MANUFACTUREMOC :
MTH 20-Nov-2013 -CATEGORY 9
Complete
E2
SB PW600-72-63006
REPLACEMENT OF SHIPPING CONTAINER HARDWARE
COMPLIED WITH - AT MANUFACTUREMOC :
MTH 20-Nov-2013 -CATEGORY 7 CompleteE1
SB PW600-72-63007
REPLACEMENT OF TURBINE EXHAUST CASE COWL ASSEMBLY
COMPLIED WITH - AT MANUFACTUREMOC :
MTH 20-Nov-2013 -CATEGORY 7 CompleteE2
SB PW600-72-63007
REPLACEMENT OF TURBINE EXHAUST CASE COWL ASSEMBLY
COMPLIED WITH - AT MANUFACTUREMOC :
MTH 20-Nov-2013 -CATEGORY 8
Complete
E1
SB PW600-72-63010
REPLACEMENT OF TURBINE EXHAUST CASE ASSEMBLY
COMPLIED WITH - AT MANUFACTUREMOC :
MTH 20-Nov-2013 -CATEGORY 8
Complete
E2
SB PW600-72-63010
REPLACEMENT OF TURBINE EXHAUST CASE ASSEMBLY
COMPLIED WITH - AT MANUFACTUREMOC :
MTH 20-Nov-2013 A/RCATEGORY 7
Complete
E1
SB PW600-72-63012 R01
REPLACEMENT OF COMPRESSOR CASE ASSEMBLY
COMPLIED WITH - AT MANUFACTUREMOC :
MTH 20-Nov-2013 A/RCATEGORY 7
Complete
E2
SB PW600-72-63012 R01
REPLACEMENT OF COMPRESSOR CASE ASSEMBLY
COMPLIED WITH - AT MANUFACTUREMOC :
MTH 20-Nov-2013 -CATEGORY 7 CompleteE1
SB PW600-72-63013
REPLACEMENT OF COMPRESSOR IMPELLER AND SHAFT ASSEMBLY (SUPERSEDED BY PW600-72-63013 R01)
COMPLIED WITH - AT MANUFACTUREMOC :
Page 25 of 50NOTE: Item Codes in italics show pre-migration CESCOM item codes and position (provided for cross-reference). Remains calculated from PrintDate for calendar items.
0:5419-Mar-2019230AIR COND
1:0419-Mar-201911031406:12ENG 2
1:0419-Mar-201911031406:12ENG 1
1:0419-Mar-201911031406:12AIRCRAFT
Average DailyUtilization
Last ActualDate
Events/LandingsHoursTracking Rate
YR-TRQReg No:
24-Mar-2019 6:11AM
20-Nov-2013
Owner: S.C. TOYO AVIATION S.R.L.
Print Date:
Airworthiness:
Aircraft Serial:
Aircraft Model: 510 - CITATION MUSTANG
Unit:
510-0433
-0433
CESCOM 10 - Aircraft Status Report
(ENG) DUE 2
(ENG) DUE 1
Service Bulletins
City Part Serial No
Part Number C/W Time 1
C/W Time 2 + or -
Adj. TBO 1
TBO 2 TSO 2
TSO 1
Remains
RemainsDescription
Drawing # / Task #Position
Item Code
Mod Lvl
MTH 20-Nov-2013 -CATEGORY 7 CompleteE2
SB PW600-72-63013
REPLACEMENT OF COMPRESSOR IMPELLER AND SHAFT ASSEMBLY (SUPERSEDED BY PW600-72-63013 R01)
COMPLIED WITH - AT MANUFACTUREMOC :
MTH 20-Nov-2013 -CATEGORY 7 CompleteE1
SB PW600-72-63016
REPLACEMENT OF COMBUSTION CHAMBER LINER ASSEMBLY
COMPLIED WITH - AT MANUFACTUREMOC :
MTH 20-Nov-2013 -CATEGORY 7 CompleteE2
SB PW600-72-63016
REPLACEMENT OF COMBUSTION CHAMBER LINER ASSEMBLY
COMPLIED WITH - AT MANUFACTUREMOC :
-CATEGORY 7
Complete
E1
SB PW600-72-63017 R01
INTRODUCTION OF CLASSIFIED SPACERS
COMPLIED WITH - AT MANUFACTURERMOC :
-CATEGORY 7
Complete
E2
SB PW600-72-63017 R01
INTRODUCTION OF CLASSIFIED SPACERS
COMPLIED WITH - AT MANUFACTUREMOC :
MTH 20-Nov-2013 -CATEGORY 7 CompleteE1
SB PW600-72-63017
INTRODUCTION OF CLASSIFIED SPACERS (SUPERSEDED BY PW600-72-63017 R01)
COMPLIED WITH - AT MANUFACTUREMOC :
MTH 20-Nov-2013 -CATEGORY 7 CompleteE2
SB PW600-72-63017
INTRODUCTION OF CLASSIFIED SPACERS (SUPERSEDED BY PW600-72-63017 R01)
COMPLIED WITH - AT MANUFACTUREMOC :
-CATEGORY 6
Complete
E1
SB PW600-72-63019 R01
INTRODUCTION OF SHIPPING BRACKET ASSEMBLY
COMPLIED WITH - AT MANUFACTUREMOC :
-CATEGORY 6
Complete
E2
SB PW600-72-63019 R01
INTRODUCTION OF SHIPPING BRACKET ASSEMBLY
COMPLIED WITH - AT MANUFACTURERMOC :
MTH 20-Nov-2013 -CATEGORY 9 CompleteE1
SB PW600-72-63019
INTRODUCTION OF SHIPPING BRACKET ASSEMBLY (SUPERSEDED BY PW600-72-63019 R01)
COMPLIED WITH - AT MANUFACTUREMOC :
MTH 20-Nov-2013 -CATEGORY 9 CompleteE2
SB PW600-72-63019
INTRODUCTION OF SHIPPING BRACKET ASSEMBLY (SUPERSEDED BY PW600-72-63019 R01)
COMPLIED WITH - AT MANUFACTUREMOC :
-CATEGORY 7E1
SB PW600-72-63022 R01
REPLACEMENT OF COMPRESSOR IMPELLER AND SHAFT ASSEMBLY (SUPERSEDED BY PW600-72-63022 R02)
MOC :
-CATEGORY 7E2
SB PW600-72-63022 R01
REPLACEMENT OF COMPRESSOR IMPELLER AND SHAFT ASSEMBLY (SUPERSEDED BY PW600-72-63022 R02)
MOC :
-CATEGORY 7E1
SB PW600-72-63022 R02
REPLACEMENT OF COMPRESSOR IMPELLER AND SHAFT ASSEMBLY
MOC :
Page 26 of 50NOTE: Item Codes in italics show pre-migration CESCOM item codes and position (provided for cross-reference). Remains calculated from PrintDate for calendar items.
0:5419-Mar-2019230AIR COND
1:0419-Mar-201911031406:12ENG 2
1:0419-Mar-201911031406:12ENG 1
1:0419-Mar-201911031406:12AIRCRAFT
Average DailyUtilization
Last ActualDate
Events/LandingsHoursTracking Rate
YR-TRQReg No:
24-Mar-2019 6:11AM
20-Nov-2013
Owner: S.C. TOYO AVIATION S.R.L.
Print Date:
Airworthiness:
Aircraft Serial:
Aircraft Model: 510 - CITATION MUSTANG
Unit:
510-0433
-0433
CESCOM 10 - Aircraft Status Report
(ENG) DUE 2
(ENG) DUE 1
Service Bulletins
City Part Serial No
Part Number C/W Time 1
C/W Time 2 + or -
Adj. TBO 1
TBO 2 TSO 2
TSO 1
Remains
RemainsDescription
Drawing # / Task #Position
Item Code
Mod Lvl
-CATEGORY 7E2
SB PW600-72-63022 R02
REPLACEMENT OF COMPRESSOR IMPELLER AND SHAFT ASSEMBLY
MOC :
MTH 20-Nov-2013 -CATEGORY 7 CompleteE1
SB PW600-72-63022
REPLACEMENT OF COMPRESSOR IMPELLER AND SHAFT ASSEMBLY (SUPERSEDED BY PW600-72-63022 R01)
COMPLIED WITH - AT MANUFACTUREMOC :
MTH 20-Nov-2013 -CATEGORY 7 CompleteE2
SB PW600-72-63022
REPLACEMENT OF COMPRESSOR IMPELLER AND SHAFT ASSEMBLY (SUPERSEDED BY PW600-72-63022 R01)
COMPLIED WITH - AT MANUFACTUREMOC :
MTH 20-Nov-2013 -CATEGORY 7
Complete
E1
SB PW600-72-63024
REPLACEMENT OF NO. 4 ROLLER BEARING
COMPLIED WITH - AT MANUFACTUREMOC :
MTH 20-Nov-2013 -CATEGORY 7
Complete
E2
SB PW600-72-63024
REPLACEMENT OF NO. 4 ROLLER BEARING
COMPLIED WITH - AT MANUFACTUREMOC :
MTH 20-Nov-2013 -CATEGORY 7 Complete
E1
SB PW600-72-63025
REPLACEMENT OF SEAL RUNNER
COMPLIED WITH - AT MANUFACTUREMOC :
MTH 20-Nov-2013 -CATEGORY 7 Complete
E2
SB PW600-72-63025
REPLACEMENT OF SEAL RUNNER
COMPLIED WITH - AT MANUFACTUREMOC :
MTH 20-Nov-2013 -CATEGORY 9
Complete
E1
SB PW600-72-63026
REPLACEMENT OF SHIPPING CONTAINER ASSEMBLY
COMPLIED WITH - AT MANUFACTUREMOC :
MTH 20-Nov-2013 -CATEGORY 9
Complete
E2
SB PW600-72-63026
REPLACEMENT OF SHIPPING CONTAINER ASSEMBLY
COMPLIED WITH - AT MANUFACTUREMOC :
MTH 20-Nov-2013 -CATEGORY 8 CompleteE1
SB PW600-72-63027 R01
INSPECTION OF NO.1-BEARING AIR-SEAL-RUNNER ASSEMBLY
COMPLIED WITH - AT MANUFACTUREMOC :
MTH 20-Nov-2013 -CATEGORY 8 CompleteE2
SB PW600-72-63027 R01
INSPECTION OF NO.1-BEARING AIR-SEAL-RUNNER ASSEMBLY
COMPLIED WITH - AT MANUFACTUREMOC :
MTH 20-Nov-2013 -CATEGORY 5 CompleteE1
SB PW600-72-63028 R01
REPLACEMENT OF NO.1-BEARING AIR-SEAL-RUNNER ASSEMBLY
COMPLIED WITH - AT MANUFACTUREMOC :
MTH 20-Nov-2013 -CATEGORY 5 CompleteE2
SB PW600-72-63028 R01
REPLACEMENT OF NO.1-BEARING AIR-SEAL-RUNNER ASSEMBLY
COMPLIED WITH - AT MANUFACTUREMOC :
MTH 20-Nov-2013 A/RCATEGORY 7
Complete
E1
SB PW600-72-63031 R01
REPLACEMENT OF IMPELLER HOUSING ASSEMBLY
COMPLIED WITH - AT MANUFACTUREMOC :
Page 27 of 50NOTE: Item Codes in italics show pre-migration CESCOM item codes and position (provided for cross-reference). Remains calculated from PrintDate for calendar items.
0:5419-Mar-2019230AIR COND
1:0419-Mar-201911031406:12ENG 2
1:0419-Mar-201911031406:12ENG 1
1:0419-Mar-201911031406:12AIRCRAFT
Average DailyUtilization
Last ActualDate
Events/LandingsHoursTracking Rate
YR-TRQReg No:
24-Mar-2019 6:11AM
20-Nov-2013
Owner: S.C. TOYO AVIATION S.R.L.
Print Date:
Airworthiness:
Aircraft Serial:
Aircraft Model: 510 - CITATION MUSTANG
Unit:
510-0433
-0433
CESCOM 10 - Aircraft Status Report
(ENG) DUE 2
(ENG) DUE 1
Service Bulletins
City Part Serial No
Part Number C/W Time 1
C/W Time 2 + or -
Adj. TBO 1
TBO 2 TSO 2
TSO 1
Remains
RemainsDescription
Drawing # / Task #Position
Item Code
Mod Lvl
MTH 20-Nov-2013 A/RCATEGORY 7
Complete
E2
SB PW600-72-63031 R01
REPLACEMENT OF IMPELLER HOUSING ASSEMBLY
COMPLIED WITH - AT MANUFACTUREMOC :
MTH 20-Nov-2013 -CATEGORY 7 CompleteE1
SB PW600-72-63032
REPLACEMENT OF HIGH-PRESSURE-COMPRESSOR (HPC) ROTOR BALANCING RING
COMPLIED WITH - AT MANUFACTUREMOC :
MTH 20-Nov-2013 -CATEGORY 7 CompleteE2
SB PW600-72-63032
REPLACEMENT OF HIGH-PRESSURE-COMPRESSOR (HPC) ROTOR BALANCING RING
COMPLIED WITH - AT MANUFACTUREMOC :
MTH 20-Nov-2013 -CATEGORY 8 Complete
E1
SB PW600-72-63034
REPLACEMENT OF OIL PUMP PLATE
COMPLIED WITH - AT MANUFACTUREMOC :
MTH 20-Nov-2013 -CATEGORY 8 Complete
E2
SB PW600-72-63034
REPLACEMENT OF OIL PUMP PLATE
COMPLIED WITH - AT MANUFACTUREMOC :
MTH 20-Nov-2013 -CATEGORY 7
Complete
E1
SB PW600-72-63035
REPLACEMENT OF NO. 1 BEARING SUPPORT ASSEMBLY
COMPLIED WITH - AT MANUFACTUREMOC :
MTH 20-Nov-2013 -CATEGORY 7
Complete
E2
SB PW600-72-63035
REPLACEMENT OF NO. 1 BEARING SUPPORT ASSEMBLY
COMPLIED WITH - AT MANUFACTUREMOC :
MTH 20-Nov-2013 -CATEGORY 7
Complete
E1
SB PW600-72-63037 R01
REPLACEMENT OF ENGINE MOUNT BRACKET ASSEMBLY
COMPLIED WITH - AT MANUFACTUREMOC :
MTH 20-Nov-2013 -CATEGORY 7
Complete
E2
SB PW600-72-63037 R01
REPLACEMENT OF ENGINE MOUNT BRACKET ASSEMBLY
COMPLIED WITH - AT MANUFACTUREMOC :
MTH 20-Nov-2013 -CATEGORY 7
Complete
E1
SB PW600-72-63039
REPLACEMENT OF LPT VANE RING ASSEMBLY
COMPLIED WITH - AT MANUFACTUREMOC :
MTH 20-Nov-2013 -CATEGORY 7
Complete
E2
SB PW600-72-63039
REPLACEMENT OF LPT VANE RING ASSEMBLY
COMPLIED WITH - AT MANUFACTUREMOC :
MTH 20-Nov-2013 -CATEGORY 7 CompleteE1
SB PW600-72-63040
MODIFICATION/REPLACEMENT OF FRONT OUTER BYPASS DUCT ASSEMBLY
COMPLIED WITH - AT MANUFACTUREMOC :
MTH 20-Nov-2013 -CATEGORY 7 CompleteE2
SB PW600-72-63040
MODIFICATION/REPLACEMENT OF FRONT OUTER BYPASS DUCT ASSEMBLY
COMPLIED WITH - AT MANUFACTUREMOC :
MTH 20-Nov-2013 -CATEGORY 7
Complete
E1
SB PW600-72-63041
REPLACEMENT OF TURBINE EXHAUST CASE ASSEMBLY
COMPLIED WITH - AT MANUFACTUREMOC :
Page 28 of 50NOTE: Item Codes in italics show pre-migration CESCOM item codes and position (provided for cross-reference). Remains calculated from PrintDate for calendar items.
0:5419-Mar-2019230AIR COND
1:0419-Mar-201911031406:12ENG 2
1:0419-Mar-201911031406:12ENG 1
1:0419-Mar-201911031406:12AIRCRAFT
Average DailyUtilization
Last ActualDate
Events/LandingsHoursTracking Rate
YR-TRQReg No:
24-Mar-2019 6:11AM
20-Nov-2013
Owner: S.C. TOYO AVIATION S.R.L.
Print Date:
Airworthiness:
Aircraft Serial:
Aircraft Model: 510 - CITATION MUSTANG
Unit:
510-0433
-0433
CESCOM 10 - Aircraft Status Report
(ENG) DUE 2
(ENG) DUE 1
Service Bulletins
City Part Serial No
Part Number C/W Time 1
C/W Time 2 + or -
Adj. TBO 1
TBO 2 TSO 2
TSO 1
Remains
RemainsDescription
Drawing # / Task #Position
Item Code
Mod Lvl
MTH 20-Nov-2013 -CATEGORY 7
Complete
E2
SB PW600-72-63041
REPLACEMENT OF TURBINE EXHAUST CASE ASSEMBLY
COMPLIED WITH - AT MANUFACTUREMOC :
MTH 20-Nov-2013 -CATEGORY 7
Complete
E1
SB PW600-72-63042
REPLACEMENT OF IMPELLER HOUSING ASSEMBLY
COMPLIED WITH - AT MANUFACTUREMOC :
MTH 20-Nov-2013 -CATEGORY 7
Complete
E2
SB PW600-72-63042
REPLACEMENT OF IMPELLER HOUSING ASSEMBLY
COMPLIED WITH - AT MANUFACTUREMOC :
MTH 20-Nov-2013 -CATEGORY 6 CompleteE1
SB PW600-72-63043 R02
REPLACEMENT/MODIFICATION OF FAN CASE ASSEMBLY AND NOSE CONE SHIPPING COVER
COMPLIED WITH - AT MANUFACTUREMOC :
MTH 20-Nov-2013 -CATEGORY 6 CompleteE2
SB PW600-72-63043 R02
REPLACEMENT/MODIFICATION OF FAN CASE ASSEMBLY AND NOSE CONE SHIPPING COVER
COMPLIED WITH - AT MANUFACTUREMOC :
- N/A
E1
SB PW600-72-63045 R01
REPLACEMENT OF OIL NOZZLE HOUSING ASSEMBLY
NOT APPLICABLE - BY ENGINE S/NMOC :
- N/A
E2
SB PW600-72-63045 R01
REPLACEMENT OF OIL NOZZLE HOUSING ASSEMBLY
NOT APPLICABLE - BY ENGINE S/NMOC :
MTH 20-Nov-2013 -CATEGORY 7 CompleteE1
SB PW600-72-63045
REPLACEMENT OF OIL NOZZLE HOUSING ASSEMBLY (SUPERSEDED BY PW600-72-63045 R01)
COMPLIED WITH - AT MANUFACTUREMOC :
MTH 20-Nov-2013 -CATEGORY 7 CompleteE2
SB PW600-72-63045
REPLACEMENT OF OIL NOZZLE HOUSING ASSEMBLY (SUPERSEDED BY PW600-72-63045 R01)
COMPLIED WITH - AT MANUFACTUREMOC :
MTH 20-Nov-2013 -CATEGORY 7 CompleteE1
SB PW600-72-63051 R01
REPLACEMENT OF DIFFUSER CASE ASSEMBLY NO. 4 BEARING OIL PRESSURE AND SCAVENGE TUBE ASSEMBLIES (SUPERSEDED BY PW600-72-63051R02)
COMPLIED WITH - AT MANUFACTUREMOC :
MTH 20-Nov-2013 -CATEGORY 7 CompleteE2
SB PW600-72-63051 R01
REPLACEMENT OF DIFFUSER CASE ASSEMBLY NO. 4 BEARING OIL PRESSURE AND SCAVENGE TUBE ASSEMBLIES (SUPERSEDED BY PW600-72-63051R02)
COMPLIED WITH - AT MANUFACTUREMOC :
-CATEGORY 6E1
SB PW600-72-63051 R03
REPLACEMENT OF DIFFUSER CASE ASSEMBLY, NO. 4 BEARING OIL PRESSURE AND SCAVENGE TUBEASSEMBLIES
MOC :
-CATEGORY 6E2
SB PW600-72-63051 R03
REPLACEMENT OF DIFFUSER CASE ASSEMBLY, NO. 4 BEARING OIL PRESSURE AND SCAVENGE TUBEASSEMBLIES
MOC :
MTH 20-Nov-2013 A/RCATEGORY 7 CompleteE1
SB PW600-72-63052 R01
COMPRESSOR CASE ASSEMBLY AND NO. 1 TO NO. 3 BEARING OIL-PRESSURE TUBE-ASSEMBLY - REPLACEMENT OF
COMPLIED WITH - AT MANUFACTUREMOC :
Page 29 of 50NOTE: Item Codes in italics show pre-migration CESCOM item codes and position (provided for cross-reference). Remains calculated from PrintDate for calendar items.
0:5419-Mar-2019230AIR COND
1:0419-Mar-201911031406:12ENG 2
1:0419-Mar-201911031406:12ENG 1
1:0419-Mar-201911031406:12AIRCRAFT
Average DailyUtilization
Last ActualDate
Events/LandingsHoursTracking Rate
YR-TRQReg No:
24-Mar-2019 6:11AM
20-Nov-2013
Owner: S.C. TOYO AVIATION S.R.L.
Print Date:
Airworthiness:
Aircraft Serial:
Aircraft Model: 510 - CITATION MUSTANG
Unit:
510-0433
-0433
CESCOM 10 - Aircraft Status Report
(ENG) DUE 2
(ENG) DUE 1
Service Bulletins
City Part Serial No
Part Number C/W Time 1
C/W Time 2 + or -
Adj. TBO 1
TBO 2 TSO 2
TSO 1
Remains
RemainsDescription
Drawing # / Task #Position
Item Code
Mod Lvl
MTH 20-Nov-2013 A/RCATEGORY 7 CompleteE2
SB PW600-72-63052 R01
COMPRESSOR CASE ASSEMBLY AND NO. 1 TO NO. 3 BEARING OIL-PRESSURE TUBE-ASSEMBLY - REPLACEMENT OF
COMPLIED WITH - AT MANUFACTUREMOC :
MTH 20-Nov-2013 -CATEGORY 7 CompleteE1
SB PW600-72-63053 R01
REPLACEMENT OF NO.4-BEARING FRONT AND REAR SEAL RUNNERS
COMPLIED WITH - AT MANUFACTUREMOC :
MTH 20-Nov-2013 -CATEGORY 7 CompleteE2
SB PW600-72-63053 R01
REPLACEMENT OF NO.4-BEARING FRONT AND REAR SEAL RUNNERS
COMPLIED WITH - AT MANUFACTUREMOC :
MTH 20-Nov-2013 -CATEGORY 7
Complete
E1
SB PW600-72-63057
REPLACEMENT OF NO. 5 BEARING SEAL RUNNER
COMPLIED WITH - AT MANUFACTUREMOC :
MTH 20-Nov-2013 -CATEGORY 7
Complete
E2
SB PW600-72-63057
REPLACEMENT OF NO. 5 BEARING SEAL RUNNER
COMPLIED WITH - AT MANUFACTUREMOC :
-CATEGORY 9
E1
SB PW600-72-63058
PARTS SUBSTITUTION LIST
MOC :
-CATEGORY 9
E2
SB PW600-72-63058
PARTS SUBSTITUTION LIST
MOC :
- CompleteE1
SB PW600-72-63059 R02
MODIFICATION/REPLACEMENT OF HP DIFFUSER CASE ASSEMBLY
COMPLIED WITH - AT MANUFACTUREMOC :
- CompleteE2
SB PW600-72-63059 R02
MODIFICATION/REPLACEMENT OF HP DIFFUSER CASE ASSEMBLY
COMPLIED WITH - AT MANUFACTUREMOC :
MTH 20-Nov-2013 -CATEGORY 6 CompleteE1
SB PW600-72-63059
MODIFICATION/REPLACEMENT OF HP DIFFUSER CASE ASSEMBLY (SUPERSEDED BY PW600-72-63059 R01)
COMPLIED WITH - AT MANUFACTUREMOC :
MTH 20-Nov-2013 -CATEGORY 6 CompleteE2
SB PW600-72-63059
MODIFICATION/REPLACEMENT OF HP DIFFUSER CASE ASSEMBLY (SUPERSEDED BY PW600-72-63059 R01)
COMPLIED WITH - AT MANUFACTUREMOC :
MTH 20-Nov-2013 A/R CompleteE1
SB PW600-72-63062 R01
REPLACEMENT OF ACCESSORY-GEARBOX (AGB) PLAIN SEAL
COMPLIED WITH - AT MANUFACTUREMOC :
MTH 20-Nov-2013 A/R CompleteE2
SB PW600-72-63062 R01
REPLACEMENT OF ACCESSORY-GEARBOX (AGB) PLAIN SEAL
COMPLIED WITH - AT MANUFACTUREMOC :
MTH 20-Nov-2013 A/RCATEGORY 6 CompleteE1
SB PW600-72-63064 R01
REPLACEMENT/MODIFICATION OF N0. 4 BEARING OIL PRESSURE TUBE ASSEMBLY(SUPERSEDED BY PW600-72-63064 R02)
COMPLIED WITH - AT MANUFACTUREMOC :
Page 30 of 50NOTE: Item Codes in italics show pre-migration CESCOM item codes and position (provided for cross-reference). Remains calculated from PrintDate for calendar items.
0:5419-Mar-2019230AIR COND
1:0419-Mar-201911031406:12ENG 2
1:0419-Mar-201911031406:12ENG 1
1:0419-Mar-201911031406:12AIRCRAFT
Average DailyUtilization
Last ActualDate
Events/LandingsHoursTracking Rate
YR-TRQReg No:
24-Mar-2019 6:11AM
20-Nov-2013
Owner: S.C. TOYO AVIATION S.R.L.
Print Date:
Airworthiness:
Aircraft Serial:
Aircraft Model: 510 - CITATION MUSTANG
Unit:
510-0433
-0433
CESCOM 10 - Aircraft Status Report
(ENG) DUE 2
(ENG) DUE 1
Service Bulletins
City Part Serial No
Part Number C/W Time 1
C/W Time 2 + or -
Adj. TBO 1
TBO 2 TSO 2
TSO 1
Remains
RemainsDescription
Drawing # / Task #Position
Item Code
Mod Lvl
MTH 20-Nov-2013 A/RCATEGORY 6 CompleteE2
SB PW600-72-63064 R01
REPLACEMENT/MODIFICATION OF N0. 4 BEARING OIL PRESSURE TUBE ASSEMBLY(SUPERSEDED BY PW600-72-63064 R02)
COMPLIED WITH - AT MANUFACTUREMOC :
- N/AE1
SB PW600-72-63064 R02
REPLACEMENT/MODIFICATION OF N0. 4 BEARING OIL PRESSURE TUBE ASSEMBLY
NOT APPLICABLE - BY ENGINE S/NMOC :
- N/AE2
SB PW600-72-63064 R02
REPLACEMENT/MODIFICATION OF N0. 4 BEARING OIL PRESSURE TUBE ASSEMBLY
NOT APPLICABLE - BY ENGINE S/NMOC :
MTH 20-Nov-2013 -CATEGORY 7
Complete
E1
SB PW600-72-63065 R01
NO. 5 ANNULAR ROLLER BEARING - REPLACEMENT OF
COMPLIED WITH - AT MANUFACTUREMOC :
MTH 20-Nov-2013 -CATEGORY 7
Complete
E2
SB PW600-72-63065 R01
NO. 5 ANNULAR ROLLER BEARING - REPLACEMENT OF
COMPLIED WITH - AT MANUFACTUREMOC :
MTH 20-Nov-2013 -CATEGORY 7 Complete
E1
SB PW600-72-63066
REPLACEMENT OF IGNITER
COMPLIED WITH - AT MANUFACTUREMOC :
MTH 20-Nov-2013 -CATEGORY 7 Complete
E2
SB PW600-72-63066
REPLACEMENT OF IGNITER
COMPLIED WITH - AT MANUFACTUREMOC :
MTH 20-Nov-2013 A/RCATEGORY 6 CompleteE1
SB PW600-72-63068 R01
REPLACEMENT/MODIFICATION OF OIL FILLER AND INDICATOR ASSEMBLY
COMPLIED WITH - AT MANUFACTUREMOC :
MTH 20-Nov-2013 A/RCATEGORY 6 CompleteE2
SB PW600-72-63068 R01
REPLACEMENT/MODIFICATION OF OIL FILLER AND INDICATOR ASSEMBLY
COMPLIED WITH - AT MANUFACTUREMOC :
MTH 20-Nov-2013 A/RCATEGORY 6
Complete
E1
SB PW600-72-63070
DELETION OF FIRE-INSULATION BLANKET ASSEMBLY
COMPLIED WITH - AT MANUFACTUREMOC :
MTH 20-Nov-2013 A/RCATEGORY 6
Complete
E2
SB PW600-72-63070
DELETION OF FIRE-INSULATION BLANKET ASSEMBLY
COMPLIED WITH - AT MANUFACTUREMOC :
MTH 20-Nov-2013 -CATEGORY 7
Complete
E1
SB PW600-72-63072 R01
REPLACEMENT OF NO. 3 FLANGED BALL BEARING
COMPLIED WITH - AT MANUFACTUREMOC :
MTH 20-Nov-2013 -CATEGORY 7
Complete
E2
SB PW600-72-63072 R01
REPLACEMENT OF NO. 3 FLANGED BALL BEARING
COMPLIED WITH - AT MANUFACTUREMOC :
MTH 20-Nov-2013 A/RCATEGORY 7
Complete
E1
SB PW600-72-63074
REPLACEMENT OF IMPELLER HOUSING ASSEMBLY
COMPLIED WITH - AT MANUFACTUREMOC :
Page 31 of 50NOTE: Item Codes in italics show pre-migration CESCOM item codes and position (provided for cross-reference). Remains calculated from PrintDate for calendar items.
0:5419-Mar-2019230AIR COND
1:0419-Mar-201911031406:12ENG 2
1:0419-Mar-201911031406:12ENG 1
1:0419-Mar-201911031406:12AIRCRAFT
Average DailyUtilization
Last ActualDate
Events/LandingsHoursTracking Rate
YR-TRQReg No:
24-Mar-2019 6:11AM
20-Nov-2013
Owner: S.C. TOYO AVIATION S.R.L.
Print Date:
Airworthiness:
Aircraft Serial:
Aircraft Model: 510 - CITATION MUSTANG
Unit:
510-0433
-0433
CESCOM 10 - Aircraft Status Report
(ENG) DUE 2
(ENG) DUE 1
Service Bulletins
City Part Serial No
Part Number C/W Time 1
C/W Time 2 + or -
Adj. TBO 1
TBO 2 TSO 2
TSO 1
Remains
RemainsDescription
Drawing # / Task #Position
Item Code
Mod Lvl
MTH 20-Nov-2013 A/RCATEGORY 7
Complete
E2
SB PW600-72-63074
REPLACEMENT OF IMPELLER HOUSING ASSEMBLY
COMPLIED WITH - AT MANUFACTUREMOC :
-CATEGORY 7E1
SB PW600-72-63076 R01
REPLACEMENT/MODIFICATION OF OIL FILLER AND INDICATOR ASSEMBLY
MOC :
-CATEGORY 7E2
SB PW600-72-63076 R01
REPLACEMENT/MODIFICATION OF OIL FILLER AND INDICATOR ASSEMBLY
MOC :
MTH 20-Nov-2013 A/RCATEGORY 6 CompleteE1
SB PW600-72-63077 R01
REPLACEMENT OF ACCESSORY DRIVE GEARSHAFT AND SPIRAL BEVEL GEAR (SUPERSEDED BY PW600-72-63077 R02)
COMPLIED WITH - AT MANUFACTUREMOC :
MTH 20-Nov-2013 A/RCATEGORY 6 CompleteE2
SB PW600-72-63077 R01
REPLACEMENT OF ACCESSORY DRIVE GEARSHAFT AND SPIRAL BEVEL GEAR (SUPERSEDED BY PW600-72-63077 R02)
COMPLIED WITH - AT MANUFACTUREMOC :
-CATEGORY 6E1
SB PW600-72-63077 R02
REPLACEMENT OF ACCESSORY DRIVE GEARSHAFT AND SPIRAL BEVEL GEAR
MOC :
-CATEGORY 6E2
SB PW600-72-63077 R02
REPLACEMENT OF ACCESSORY DRIVE GEARSHAFT AND SPIRAL BEVEL GEAR
MOC :
MTH 20-Nov-2013 A/RCATEGORY 7
Complete
E1
SB PW600-72-63078
REPLACEMENT OF HIGH PRESSURE IMPELLER
COMPLIED WITH - AT MANUFACTUREMOC :
MTH 20-Nov-2013 A/RCATEGORY 7
Complete
E2
SB PW600-72-63078
REPLACEMENT OF HIGH PRESSURE IMPELLER
COMPLIED WITH - AT MANUFACTUREMOC :
-CATEGORY 6E1
SB PW600-72-63080 R02
REPLACEMENT / MODIFICATION OF ELECTRICAL WIRING HARNESS (TT0 SENSOR)
MOC :
-CATEGORY 6E2
SB PW600-72-63080 R02
REPLACEMENT / MODIFICATION OF ELECTRICAL WIRING HARNESS (TT0 SENSOR)
MOC :
MTH 20-Nov-2013 A/RCATEGORY 5 CompleteE1
SB PW600-72-63081 R01
REPLACEMENT OF NO.4-BEARING FRONT AND REAR CARBON SEAL
COMPLIED WITH - AT MANUFACTUREMOC :
MTH 20-Nov-2013 A/RCATEGORY 5 CompleteE2
SB PW600-72-63081 R01
REPLACEMENT OF NO.4-BEARING FRONT AND REAR CARBON SEAL
COMPLIED WITH - AT MANUFACTUREMOC :
MTH 20-Nov-2013 -CATEGORY 7 CompleteE1
SB PW600-72-63083 R01
REPLACEMENT OF NO.4-BEARING FRONT AND REAR CARBON SEAL
COMPLIED WITH - AT MANUFACTUREMOC :
Page 32 of 50NOTE: Item Codes in italics show pre-migration CESCOM item codes and position (provided for cross-reference). Remains calculated from PrintDate for calendar items.
0:5419-Mar-2019230AIR COND
1:0419-Mar-201911031406:12ENG 2
1:0419-Mar-201911031406:12ENG 1
1:0419-Mar-201911031406:12AIRCRAFT
Average DailyUtilization
Last ActualDate
Events/LandingsHoursTracking Rate
YR-TRQReg No:
24-Mar-2019 6:11AM
20-Nov-2013
Owner: S.C. TOYO AVIATION S.R.L.
Print Date:
Airworthiness:
Aircraft Serial:
Aircraft Model: 510 - CITATION MUSTANG
Unit:
510-0433
-0433
CESCOM 10 - Aircraft Status Report
(ENG) DUE 2
(ENG) DUE 1
Service Bulletins
City Part Serial No
Part Number C/W Time 1
C/W Time 2 + or -
Adj. TBO 1
TBO 2 TSO 2
TSO 1
Remains
RemainsDescription
Drawing # / Task #Position
Item Code
Mod Lvl
MTH 20-Nov-2013 -CATEGORY 7 CompleteE2
SB PW600-72-63083 R01
REPLACEMENT OF NO.4-BEARING FRONT AND REAR CARBON SEAL
COMPLIED WITH - AT MANUFACTUREMOC :
MTH 20-Nov-2013 A/RCATEGORY 7
Complete
E1
SB PW600-72-63084
REPLACEMENT OF FLANGE DUPLEX BEARING (IC)
COMPLIED WITH - AT MANUFACTUREMOC :
MTH 20-Nov-2013 A/RCATEGORY 7
Complete
E2
SB PW600-72-63084
REPLACEMENT OF FLANGE DUPLEX BEARING (IC)
COMPLIED WITH - AT MANUFACTUREMOC :
MTH 20-Nov-2013 -CATEGORY 7 CompleteE1
SB PW600-72-63085
TURBOFAN ENGINE - COMPRESSOR CASE ASSEMBLY - MODIFICATION/REPLACEMENT OF
COMPLIED WITH - AT MANUFACTUREMOC :
MTH 20-Nov-2013 -CATEGORY 7 CompleteE2
SB PW600-72-63085
TURBOFAN ENGINE - COMPRESSOR CASE ASSEMBLY - MODIFICATION/REPLACEMENT OF
COMPLIED WITH - AT MANUFACTUREMOC :
MTH 20-Nov-2013 A/RCATEGORY 7 CompleteE1
SB PW600-72-63086
REPLACEMENT OF TURBOFAN ENGINE DIFFUSER EXIT DUCT ASSEMBLY
COMPLIED WITH - AT MANUFACTUREMOC :
MTH 20-Nov-2013 A/RCATEGORY 7 CompleteE2
SB PW600-72-63086
REPLACEMENT OF TURBOFAN ENGINE DIFFUSER EXIT DUCT ASSEMBLY
COMPLIED WITH - AT MANUFACTUREMOC :
MTH 20-Nov-2013 -CATEGORY 3 CompleteE1
SB PW600-72-63087 R02
REPLACEMENT/MODIFICATION OF ENGINE ELECTRONIC CONTROL
COMPLIED WITH - AT MANUFACTUREMOC :
MTH 20-Nov-2013 -CATEGORY 3 CompleteE2
SB PW600-72-63087 R02
REPLACEMENT/MODIFICATION OF ENGINE ELECTRONIC CONTROL
COMPLIED WITH - AT MANUFACTUREMOC :
MTH 20-Nov-2013 A/RCATEGORY 7 CompleteE1
SB PW600-72-63088
REPLACEMENT OF ACCESSORY GEARBOX HOUSING ASSEMBLY
COMPLIED WITH - AT MANUFACTUREMOC :
MTH 20-Nov-2013 A/RCATEGORY 7 CompleteE2
SB PW600-72-63088
REPLACEMENT OF ACCESSORY GEARBOX HOUSING ASSEMBLY
COMPLIED WITH - AT MANUFACTUREMOC :
MTH 20-Nov-2013 -CATEGORY 6
Complete
E1
SB PW600-72-63089 R02
FUEL METERING UNIT - REPLACEMENT/MODIFICATION OF
COMPLIED WITH - AT MANUFACTUREMOC :
MTH 20-Nov-2013 -CATEGORY 6
Complete
E2
SB PW600-72-63089 R02
FUEL METERING UNIT - REPLACEMENT/MODIFICATION OF
COMPLIED WITH - AT MANUFACTUREMOC :
MTH 20-Nov-2013 A/RCATEGORY 7 CompleteE1
SB PW600-72-63090
REPLACEMENT/MODIFICATION OF ELECTRONIC ENGINE CONTROL (EEC)
COMPLIED WITH - AT MANUFACTUREMOC :
Page 33 of 50NOTE: Item Codes in italics show pre-migration CESCOM item codes and position (provided for cross-reference). Remains calculated from PrintDate for calendar items.
0:5419-Mar-2019230AIR COND
1:0419-Mar-201911031406:12ENG 2
1:0419-Mar-201911031406:12ENG 1
1:0419-Mar-201911031406:12AIRCRAFT
Average DailyUtilization
Last ActualDate
Events/LandingsHoursTracking Rate
YR-TRQReg No:
24-Mar-2019 6:11AM
20-Nov-2013
Owner: S.C. TOYO AVIATION S.R.L.
Print Date:
Airworthiness:
Aircraft Serial:
Aircraft Model: 510 - CITATION MUSTANG
Unit:
510-0433
-0433
CESCOM 10 - Aircraft Status Report
(ENG) DUE 2
(ENG) DUE 1
Service Bulletins
City Part Serial No
Part Number C/W Time 1
C/W Time 2 + or -
Adj. TBO 1
TBO 2 TSO 2
TSO 1
Remains
RemainsDescription
Drawing # / Task #Position
Item Code
Mod Lvl
MTH 20-Nov-2013 A/RCATEGORY 7 CompleteE2
SB PW600-72-63090
REPLACEMENT/MODIFICATION OF ELECTRONIC ENGINE CONTROL (EEC)
COMPLIED WITH - AT MANUFACTUREMOC :
-CATEGORY 6E1
SB PW600-72-63091 R01
INSPECTION OF PRIMARY AND SECONDARY FUEL FAIRING REDUCERS (SUPERSEDED BY PW600-72-63091 R02)
MOC :
-CATEGORY 6E2
SB PW600-72-63091 R01
INSPECTION OF PRIMARY AND SECONDARY FUEL FAIRING REDUCERS (SUPERSEDED BY PW600-72-63091 R02)
MOC :
-CATEGORY 6E1
SB PW600-72-63091 R02
INSPECTION OF PRIMARY AND SECONDARY FUEL FAIRING REDUCERS
MOC :
-CATEGORY 6E2
SB PW600-72-63091 R02
INSPECTION OF PRIMARY AND SECONDARY FUEL FAIRING REDUCERS
MOC :
MTH 20-Nov-2013 -CATEGORY 6 CompleteE1
SB PW600-72-63091
PRIMARY AND SECONDARY FUEL FAIRING REDUCERS - INSPECTION OF (SUPERSEDED BY PW600-72-63091 R01)
COMPLIED WITH - AT MANUFACTUREMOC :
MTH 20-Nov-2013 -CATEGORY 6 CompleteE2
SB PW600-72-63091
PRIMARY AND SECONDARY FUEL FAIRING REDUCERS - INSPECTION OF (SUPERSEDED BY PW600-72-63091 R01)
COMPLIED WITH - AT MANUFACTUREMOC :
MTH 20-Nov-2013 -CATEGORY 7 CompleteE1
SB PW600-72-63092
REPLACEMENT OF LOW PRESSURE COMPRESSOR SHAFT
COMPLIED WITH - AT MANUFACTUREMOC :
MTH 20-Nov-2013 -CATEGORY 7 CompleteE2
SB PW600-72-63092
REPLACEMENT OF LOW PRESSURE COMPRESSOR SHAFT
COMPLIED WITH - AT MANUFACTUREMOC :
MTH 20-Nov-2013 A/RCATEGORY 6
Complete
E1
SB PW600-72-63093
REPOSITIONING OF OIL FILLER CAP ASSEMBLY BRACKET
COMPLIED WITH - AT MANUFACTUREMOC :
MTH 20-Nov-2013 A/RCATEGORY 6
Complete
E2
SB PW600-72-63093
REPOSITIONING OF OIL FILLER CAP ASSEMBLY BRACKET
COMPLIED WITH - AT MANUFACTUREMOC :
-CATEGORY 7
E1
SB PW600-72-63094 R01
REPLACEMENT OF ELECTRICAL WIRING HARNESS
MOC :
-CATEGORY 7
E2
SB PW600-72-63094 R01
REPLACEMENT OF ELECTRICAL WIRING HARNESS
MOC :
MTH 20-Nov-2013 -CATEGORY 7 CompleteE1
SB PW600-72-63094
REPLACEMENT OF ELECTRICAL WIRING HARNESS (SUPERSEDED BY PW600-72-63094 R01)
COMPLIED WITH - AT MANUFACTUREMOC :
Page 34 of 50NOTE: Item Codes in italics show pre-migration CESCOM item codes and position (provided for cross-reference). Remains calculated from PrintDate for calendar items.
0:5419-Mar-2019230AIR COND
1:0419-Mar-201911031406:12ENG 2
1:0419-Mar-201911031406:12ENG 1
1:0419-Mar-201911031406:12AIRCRAFT
Average DailyUtilization
Last ActualDate
Events/LandingsHoursTracking Rate
YR-TRQReg No:
24-Mar-2019 6:11AM
20-Nov-2013
Owner: S.C. TOYO AVIATION S.R.L.
Print Date:
Airworthiness:
Aircraft Serial:
Aircraft Model: 510 - CITATION MUSTANG
Unit:
510-0433
-0433
CESCOM 10 - Aircraft Status Report
(ENG) DUE 2
(ENG) DUE 1
Service Bulletins
City Part Serial No
Part Number C/W Time 1
C/W Time 2 + or -
Adj. TBO 1
TBO 2 TSO 2
TSO 1
Remains
RemainsDescription
Drawing # / Task #Position
Item Code
Mod Lvl
MTH 20-Nov-2013 -CATEGORY 7 CompleteE2
SB PW600-72-63094
REPLACEMENT OF ELECTRICAL WIRING HARNESS (SUPERSEDED BY PW600-72-63094 R01)
COMPLIED WITH - AT MANUFACTUREMOC :
MTH 20-Nov-2013 -CATEGORY 7 CompleteE1
SB PW600-72-63095
TURBOFAN ENGINE - FUEL MANIFOLD ASSEMBLY - REPLACEMENT OF
COMPLIED WITH - AT MANUFACTUREMOC :
MTH 20-Nov-2013 -CATEGORY 7 CompleteE2
SB PW600-72-63095
TURBOFAN ENGINE - FUEL MANIFOLD ASSEMBLY - REPLACEMENT OF
COMPLIED WITH - AT MANUFACTUREMOC :
MTH 20-Nov-2013 -CATEGORY 7
Complete
E1
SB PW600-72-63096
REPLACEMENT OF OIL NOZZLE ASSEMBLY
COMPLIED WITH - AT MANUFACTUREMOC :
MTH 20-Nov-2013 -CATEGORY 7
Complete
E2
SB PW600-72-63096
REPLACEMENT OF OIL NOZZLE ASSEMBLY
COMPLIED WITH - AT MANUFACTUREMOC :
-E1
SB PW600-72-63097 R01
REPLACEMENT/MODIFICATION OF ELECTRONIC ENGINE CONTROL (EEC)
- OPENMOC :
-E2
SB PW600-72-63097 R01
REPLACEMENT/MODIFICATION OF ELECTRONIC ENGINE CONTROL (EEC)
- OPENMOC :
MTH 20-Nov-2013 -CATEGORY 7
Complete
E1
SB PW600-72-63099
REPLACEMENT OF BLEED VALVE ACTUATOR BRACKET
COMPLIED WITH - AT MANUFACTUREMOC :
MTH 20-Nov-2013 -CATEGORY 7
Complete
E2
SB PW600-72-63099
REPLACEMENT OF BLEED VALVE ACTUATOR BRACKET
COMPLIED WITH - AT MANUFACTUREMOC :
-
E1
SB PW600-72-63100
REPLACEMENT/MODIFICATION OF FUEL METERING UNIT
- OPENMOC :
-
E2
SB PW600-72-63100
REPLACEMENT/MODIFICATION OF FUEL METERING UNIT
- OPENMOC :
-CATEGORY 7
E1
SB PW600-72-63104
REPLACEMENT/MODIFICATION OF FAN CASE
MOC :
-CATEGORY 7
E2
SB PW600-72-63104
REPLACEMENT/MODIFICATION OF FAN CASE
MOC :
-CATEGORY 7
E1
SB PW600-72-63105 R01
REPLACEMENT OF FUEL OIL HEAT EXCHANGER (FOHE)
MOC :
Page 35 of 50NOTE: Item Codes in italics show pre-migration CESCOM item codes and position (provided for cross-reference). Remains calculated from PrintDate for calendar items.
0:5419-Mar-2019230AIR COND
1:0419-Mar-201911031406:12ENG 2
1:0419-Mar-201911031406:12ENG 1
1:0419-Mar-201911031406:12AIRCRAFT
Average DailyUtilization
Last ActualDate
Events/LandingsHoursTracking Rate
YR-TRQReg No:
24-Mar-2019 6:11AM
20-Nov-2013
Owner: S.C. TOYO AVIATION S.R.L.
Print Date:
Airworthiness:
Aircraft Serial:
Aircraft Model: 510 - CITATION MUSTANG
Unit:
510-0433
-0433
CESCOM 10 - Aircraft Status Report
(ENG) DUE 2
(ENG) DUE 1
Service Bulletins
City Part Serial No
Part Number C/W Time 1
C/W Time 2 + or -
Adj. TBO 1
TBO 2 TSO 2
TSO 1
Remains
RemainsDescription
Drawing # / Task #Position
Item Code
Mod Lvl
-CATEGORY 7
E2
SB PW600-72-63105 R01
REPLACEMENT OF FUEL OIL HEAT EXCHANGER (FOHE)
MOC :
-CATEGORY 7E1
SB PW600-72-63105
REPLACEMENT OF FUEL OIL HEAT EXCHANGER (FOHE) (SUPERSEDED BY PW600-72-63105 R01)
MOC :
-CATEGORY 7E2
SB PW600-72-63105
REPLACEMENT OF FUEL OIL HEAT EXCHANGER (FOHE) (SUPERSEDED BY PW600-72-63105 R01)
MOC :
-CATEGORY 5
E1
SB PW600-72-63106 R01
RE-IDENTIFICATION OF AGB HOUSING AND COVER
MOC :
-CATEGORY 5
E2
SB PW600-72-63106 R01
RE-IDENTIFICATION OF AGB HOUSING AND COVER
MOC :
-CATEGORY 5E1
SB PW600-72-63106
RE-IDENTIFICATION OF AGB HOUSING AND COVER (SUPERSEDED BY PW600-72-63106 R01)
MOC :
-CATEGORY 5E2
SB PW600-72-63106
RE-IDENTIFICATION OF AGB HOUSING AND COVER (SUPERSEDED BY PW600-72-63106 R01)
MOC :
-CATEGORY 7
E1
SB PW600-72-63107
REPLACEMENT OF TURBINE EXHAUST CASE
MOC :
-CATEGORY 7
E2
SB PW600-72-63107
REPLACEMENT OF TURBINE EXHAUST CASE
MOC :
-CATEGORY 5E1
SB PW600-72-63109
REPLACEMENT OF NO. 4 BEARING CARBON SEALS AND IMPELLER BAFFLE
MOC :
-CATEGORY 5E2
SB PW600-72-63109
REPLACEMENT OF NO. 4 BEARING CARBON SEALS AND IMPELLER BAFFLE
MOC :
-CATEGORY 5
E1
SB PW600-72-63110
VALIDATION OF NO. 3 BEARING ASSEMBLY PROCEDURE
MOC :
-CATEGORY 5
E2
SB PW600-72-63110
VALIDATION OF NO. 3 BEARING ASSEMBLY PROCEDURE
MOC :
HRS
MTH
600
12CATEGORY 3
(1900:12)1900:12
20-Nov-2019
494
7 m 27 dE1
SB PW600-72-63111
INSPECTION OF FUEL OIL HEAT EXCHANGER (FOHE) FUEL FILTER BYPASS VALVE PACKING
MOC :
Page 36 of 50NOTE: Item Codes in italics show pre-migration CESCOM item codes and position (provided for cross-reference). Remains calculated from PrintDate for calendar items.
0:5419-Mar-2019230AIR COND
1:0419-Mar-201911031406:12ENG 2
1:0419-Mar-201911031406:12ENG 1
1:0419-Mar-201911031406:12AIRCRAFT
Average DailyUtilization
Last ActualDate
Events/LandingsHoursTracking Rate
YR-TRQReg No:
24-Mar-2019 6:11AM
20-Nov-2013
Owner: S.C. TOYO AVIATION S.R.L.
Print Date:
Airworthiness:
Aircraft Serial:
Aircraft Model: 510 - CITATION MUSTANG
Unit:
510-0433
-0433
CESCOM 10 - Aircraft Status Report
(ENG) DUE 2
(ENG) DUE 1
Service Bulletins
City Part Serial No
Part Number C/W Time 1
C/W Time 2 + or -
Adj. TBO 1
TBO 2 TSO 2
TSO 1
Remains
RemainsDescription
Drawing # / Task #Position
Item Code
Mod Lvl
HRS
MTH
600
12CATEGORY 3
(1900:12)1900:12
20-Nov-2019
494
7 m 27 dE2
SB PW600-72-63111
INSPECTION OF FUEL OIL HEAT EXCHANGER (FOHE) FUEL FILTER BYPASS VALVE PACKING
MOC :
MTH 20-Nov-2013 A/RCATEGORY 3 CompleteE1
ASB PW600-72-A63071 R01
REPLACEMENT OF FUEL OIL HEAT EXCHANGER (FOHE) FUEL-FILTER BYPASS VALVE (SUPERSEDED BY PW600-72-A63071 R02)
COMPLIED WITH - AT MANUFACTUREMOC :
MTH 20-Nov-2013 A/RCATEGORY 3 CompleteE2
ASB PW600-72-A63071 R01
REPLACEMENT OF FUEL OIL HEAT EXCHANGER (FOHE) FUEL-FILTER BYPASS VALVE (SUPERSEDED BY PW600-72-A63071 R02)
COMPLIED WITH - AT MANUFACTUREMOC :
MTH 20-Nov-2013 A/RCATEGORY 7 CompleteE1
SB PW600-73-63030 R01
MODIFICATION/REPLACEMENT OF ELECTRICAL WIRING HARNESS
COMPLIED WITH - AT MANUFACTUREMOC :
MTH 20-Nov-2013 A/RCATEGORY 7 CompleteE2
SB PW600-73-63030 R01
MODIFICATION/REPLACEMENT OF ELECTRICAL WIRING HARNESS
COMPLIED WITH - AT MANUFACTUREMOC :
A/RMANDATORY Complete
LEFT
ASL 510-73-01 TRANSMITTAL OF PRATT AND WHITNEY CANADA ALERT SERVICE BULLETIN A63069 TITLED, TURBOFAN ENGINE FUEL OIL HEAT EXCHANGER (FOHE)FUEL-FILTER BYPASS VALVE
COMPLIED WITH - AT MANUFACTURERMOC :
MTH 20-Nov-2013 -CATEGORY 8
Complete
E1
SB PW600-1007-63009
REPLACEMENT OF FUEL SHUT-OFF CABLE ASSEMBLY
COMPLIED WITH - AT MANUFACTUREMOC :
MTH 20-Nov-2013 -CATEGORY 8
Complete
E2
SB PW600-1007-63009
REPLACEMENT OF FUEL SHUT-OFF CABLE ASSEMBLY
COMPLIED WITH - AT MANUFACTUREMOC :
MTH 20-Nov-2013 -CATEGORY 7 CompleteE1
SB PW600-72-63067
REPLACEMENT OF BYPASS-DUCT FUEL FAIRING ASSEMBLY
COMPLIED WITH - AT MANUFACTUREMOC :
MTH 20-Nov-2013 -CATEGORY 7 CompleteE2
SB PW600-72-63067
REPLACEMENT OF BYPASS-DUCT FUEL FAIRING ASSEMBLY
COMPLIED WITH - AT MANUFACTUREMOC :
MTH 20-Nov-2013 A/RCATEGORY 6 CompleteE1
SB PW600-72-63073
REPLACEMENT OF THE FUEL-SHUT-OFF-LEVER COTTER PIN BY A SAFETY WIRE
COMPLIED WITH - AT MANUFACTUREMOC :
MTH 20-Nov-2013 A/RCATEGORY 6 CompleteE2
SB PW600-72-63073
REPLACEMENT OF THE FUEL-SHUT-OFF-LEVER COTTER PIN BY A SAFETY WIRE
COMPLIED WITH - AT MANUFACTUREMOC :
MTH 20-Nov-2013 A/RCATEGORY 7 CompleteE1
SB PW600-72-63075
REPLACEMENT/MODIFICATION OF FUEL OIL/HEATER EXCHANGER (FOHE)
COMPLIED WITH - AT MANUFACTUREMOC :
MTH 20-Nov-2013 A/RCATEGORY 7 CompleteE2
SB PW600-72-63075
REPLACEMENT/MODIFICATION OF FUEL OIL/HEATER EXCHANGER (FOHE)
COMPLIED WITH - AT MANUFACTUREMOC :
Page 37 of 50NOTE: Item Codes in italics show pre-migration CESCOM item codes and position (provided for cross-reference). Remains calculated from PrintDate for calendar items.
0:5419-Mar-2019230AIR COND
1:0419-Mar-201911031406:12ENG 2
1:0419-Mar-201911031406:12ENG 1
1:0419-Mar-201911031406:12AIRCRAFT
Average DailyUtilization
Last ActualDate
Events/LandingsHoursTracking Rate
YR-TRQReg No:
24-Mar-2019 6:11AM
20-Nov-2013
Owner: S.C. TOYO AVIATION S.R.L.
Print Date:
Airworthiness:
Aircraft Serial:
Aircraft Model: 510 - CITATION MUSTANG
Unit:
510-0433
-0433
CESCOM 10 - Aircraft Status Report
(ENG) DUE 2
(ENG) DUE 1
Service Bulletins
City Part Serial No
Part Number C/W Time 1
C/W Time 2 + or -
Adj. TBO 1
TBO 2 TSO 2
TSO 1
Remains
RemainsDescription
Drawing # / Task #Position
Item Code
Mod Lvl
MTH 20-Nov-2013 A/RCATEGORY 7
Complete
E1
SB PW600-72-63079
REPLACEMENT OF FUEL SHUT-OFF CABLE ASSEMBLY
COMPLIED WITH - AT MANUFACTUREMOC :
MTH 20-Nov-2013 A/RCATEGORY 7
Complete
E2
SB PW600-72-63079
REPLACEMENT OF FUEL SHUT-OFF CABLE ASSEMBLY
COMPLIED WITH - AT MANUFACTUREMOC :
MTH 20-Nov-2013 A/RCATEGORY 6 CompleteE1
SB PW600-72-63080 R01
MODIFICATION/REPLACEMENT OF ELECTRICAL WIRING HARNESS (TT0 SENSOR) (SUPERSEDED BY PW600-72-63080 R02)
COMPLIED WITH - AT MANUFACTUREMOC :
MTH 20-Nov-2013 A/RCATEGORY 6 CompleteE2
SB PW600-72-63080 R01
MODIFICATION/REPLACEMENT OF ELECTRICAL WIRING HARNESS (TT0 SENSOR) (SUPERSEDED BY PW600-72-63080 R02)
COMPLIED WITH - AT MANUFACTUREMOC :
MTH 20-Nov-2013 A/RCATEGORY 3 CompleteE1
ASB PW600-72-A63061 R02
REPLACEMENT/MODIFICATION OF ELECTRONIC ENGINE CONTROL (EEC)
COMPLIED WITH - AT MANUFACTUREMOC :
MTH 20-Nov-2013 A/RCATEGORY 3 CompleteE2
ASB PW600-72-A63061 R02
REPLACEMENT/MODIFICATION OF ELECTRONIC ENGINE CONTROL (EEC)
COMPLIED WITH - AT MANUFACTUREMOC :
MTH 20-Nov-2013 -CATEGORY 7
Complete
E1
SB PW600-73-63004
REPLACEMENT OF FUEL-SHUT-OFF-VALVE PIN
COMPLIED WITH - AT MANUFACTUREMOC :
MTH 20-Nov-2013 -CATEGORY 7
Complete
E2
SB PW600-73-63004
REPLACEMENT OF FUEL-SHUT-OFF-VALVE PIN
COMPLIED WITH - AT MANUFACTUREMOC :
MTH 20-Nov-2013 -CATEGORY 8 CompleteE1
SB PW600-73-63011 R01
REPROGRAMMING/ REPLACEMENT OF ELECTRONIC ENGINE CONTROL (EEC)
COMPLIED WITH - AT MANUFACTUREMOC :
MTH 20-Nov-2013 -CATEGORY 8 CompleteE2
SB PW600-73-63011 R01
REPROGRAMMING/ REPLACEMENT OF ELECTRONIC ENGINE CONTROL (EEC)
COMPLIED WITH - AT MANUFACTUREMOC :
MTH 20-Nov-2013 -CATEGORY 7
Complete
E1
SB PW600-73-63014
REPLACEMENT OF FUEL MANIFOLD ASSEMBLY
COMPLIED WITH - AT MANUFACTUREMOC :
MTH 20-Nov-2013 -CATEGORY 7
Complete
E2
SB PW600-73-63014
REPLACEMENT OF FUEL MANIFOLD ASSEMBLY
COMPLIED WITH - AT MANUFACTUREMOC :
MTH 20-Nov-2013 -CATEGORY 8
Complete
E1
SB PW600-73-63020
REPLACEMENT/MODIFICATION OF FUEL METERING UNIT
COMPLIED WITH - AT MANUFACTUREMOC :
MTH 20-Nov-2013 -CATEGORY 8
Complete
E2
SB PW600-73-63020
REPLACEMENT/MODIFICATION OF FUEL METERING UNIT
COMPLIED WITH - AT MANUFACTUREMOC :
Page 38 of 50NOTE: Item Codes in italics show pre-migration CESCOM item codes and position (provided for cross-reference). Remains calculated from PrintDate for calendar items.
0:5419-Mar-2019230AIR COND
1:0419-Mar-201911031406:12ENG 2
1:0419-Mar-201911031406:12ENG 1
1:0419-Mar-201911031406:12AIRCRAFT
Average DailyUtilization
Last ActualDate
Events/LandingsHoursTracking Rate
YR-TRQReg No:
24-Mar-2019 6:11AM
20-Nov-2013
Owner: S.C. TOYO AVIATION S.R.L.
Print Date:
Airworthiness:
Aircraft Serial:
Aircraft Model: 510 - CITATION MUSTANG
Unit:
510-0433
-0433
CESCOM 10 - Aircraft Status Report
(ENG) DUE 2
(ENG) DUE 1
Service Bulletins
City Part Serial No
Part Number C/W Time 1
C/W Time 2 + or -
Adj. TBO 1
TBO 2 TSO 2
TSO 1
Remains
RemainsDescription
Drawing # / Task #Position
Item Code
Mod Lvl
MTH 20-Nov-2013 -CATEGORY 7
Complete
E1
SB PW600-73-63023
REPLACEMENT OF FUEL SHUT-OFF CABLE ASSEMBLY
COMPLIED WITH - AT MANUFACTUREMOC :
MTH 20-Nov-2013 -CATEGORY 7
Complete
E2
SB PW600-73-63023
REPLACEMENT OF FUEL SHUT-OFF CABLE ASSEMBLY
COMPLIED WITH - AT MANUFACTUREMOC :
MTH 20-Nov-2013 -CATEGORY 7
Complete
E1
SB PW600-73-63029
REPLACEMENT OF FUEL MANIFOLD ASSEMBLY
COMPLIED WITH - AT MANUFACTUREMOC :
MTH 20-Nov-2013 -CATEGORY 7
Complete
E2
SB PW600-73-63029
REPLACEMENT OF FUEL MANIFOLD ASSEMBLY
COMPLIED WITH - AT MANUFACTUREMOC :
MTH 20-Nov-2013 -CATEGORY 7
Complete
E1
SB PW600-73-63036
REPLACEMENT OF FUEL DRAIN VALVE ADAPTER
COMPLIED WITH - AT MANUFACTUREMOC :
MTH 20-Nov-2013 -CATEGORY 7
Complete
E2
SB PW600-73-63036
REPLACEMENT OF FUEL DRAIN VALVE ADAPTER
COMPLIED WITH - AT MANUFACTUREMOC :
MTH 20-Nov-2013 -CATEGORY 7
Complete
E1
SB PW600-73-63038
REPLACEMENT OF FUEL OIL HEAT EXCHANGER (FOHE)
COMPLIED WITH - AT MANUFACTUREMOC :
MTH 20-Nov-2013 -CATEGORY 7
Complete
E2
SB PW600-73-63038
REPLACEMENT OF FUEL OIL HEAT EXCHANGER (FOHE)
COMPLIED WITH - AT MANUFACTUREMOC :
MTH 20-Nov-2013 -CATEGORY 7
Complete
E1
SB PW600-73-63048
REPLACEMENT/MODIFICATION OF FUEL METERING UNIT
COMPLIED WITH - AT MANUFACTUREMOC :
MTH 20-Nov-2013 -CATEGORY 7
Complete
E2
SB PW600-73-63048
REPLACEMENT/MODIFICATION OF FUEL METERING UNIT
COMPLIED WITH - AT MANUFACTUREMOC :
MTH 20-Nov-2013 -CATEGORY 7
Complete
E1
SB PW600-73-63049
REPLACEMENT OF FUEL-SHUT-OFF LEVER SUPPORT
COMPLIED WITH - AT MANUFACTUREMOC :
MTH 20-Nov-2013 -CATEGORY 7
Complete
E2
SB PW600-73-63049
REPLACEMENT OF FUEL-SHUT-OFF LEVER SUPPORT
COMPLIED WITH - AT MANUFACTUREMOC :
MTH 20-Nov-2013 -CATEGORY 7 Complete
E1
SB PW600-74-63056
REPLACEMENT OF IGNITION EXCITER
COMPLIED WITH - AT MANUFACTUREMOC :
MTH 20-Nov-2013 -CATEGORY 7 Complete
E2
SB PW600-74-63056
REPLACEMENT OF IGNITION EXCITER
COMPLIED WITH - AT MANUFACTUREMOC :
Page 39 of 50NOTE: Item Codes in italics show pre-migration CESCOM item codes and position (provided for cross-reference). Remains calculated from PrintDate for calendar items.
0:5419-Mar-2019230AIR COND
1:0419-Mar-201911031406:12ENG 2
1:0419-Mar-201911031406:12ENG 1
1:0419-Mar-201911031406:12AIRCRAFT
Average DailyUtilization
Last ActualDate
Events/LandingsHoursTracking Rate
YR-TRQReg No:
24-Mar-2019 6:11AM
20-Nov-2013
Owner: S.C. TOYO AVIATION S.R.L.
Print Date:
Airworthiness:
Aircraft Serial:
Aircraft Model: 510 - CITATION MUSTANG
Unit:
510-0433
-0433
CESCOM 10 - Aircraft Status Report
(ENG) DUE 2
(ENG) DUE 1
Service Bulletins
City Part Serial No
Part Number C/W Time 1
C/W Time 2 + or -
Adj. TBO 1
TBO 2 TSO 2
TSO 1
Remains
RemainsDescription
Drawing # / Task #Position
Item Code
Mod Lvl
MTH 20-Nov-2013 -CATEGORY 6 CompleteE1
SB PW600-72-63060
REPLACEMENT OF BLEED-VALVE-ACTUATOR (BVA) BRACKET BOLTS
COMPLIED WITH - AT MANUFACTUREMOC :
MTH 20-Nov-2013 -CATEGORY 6 CompleteE2
SB PW600-72-63060
REPLACEMENT OF BLEED-VALVE-ACTUATOR (BVA) BRACKET BOLTS
COMPLIED WITH - AT MANUFACTUREMOC :
MTH 20-Nov-2013 -CATEGORY 7
Complete
E1
SB PW600-75-63054 R01
REPLACEMENT OF BLEED VALVE ACTUATOR (BVA)
COMPLIED WITH - AT MANUFACTUREMOC :
MTH 20-Nov-2013 -CATEGORY 7
Complete
E2
SB PW600-75-63054 R01
REPLACEMENT OF BLEED VALVE ACTUATOR (BVA)
COMPLIED WITH - AT MANUFACTUREMOC :
MTH 20-Nov-2013 -MANDATORY Complete
SB 510-76-01 REV02
TRANSMITTAL OF PRATT AND WHITNEY CANADA SERVICE BULLETN PW600-72-63087
COMPLIED WITH - AT MANUFACTUREMOC :
MTH 20-Nov-2013 -CATEGORY 8 CompleteE1
SB PW600-77-63033
REPLACEMENT OF T6 THERMOCOUPLE WIRING HARNESS
COMPLIED WITH - AT MANUFACTUREMOC :
MTH 20-Nov-2013 -CATEGORY 8 CompleteE2
SB PW600-77-63033
REPLACEMENT OF T6 THERMOCOUPLE WIRING HARNESS
COMPLIED WITH - AT MANUFACTUREMOC :
-OPTIONAL
SB 510-79-03 OIL - OIL PRESSURE TRANSDUCER REPLACEMENT
MOC :
MTH 20-Nov-2013 -CATEGORY 7 CompleteE1
SB PW600-72-63055
REPLACEMENT/MODIFICATION OF AIR COOLED OIL COOLER
COMPLIED WITH - AT MANUFACTUREMOC :
MTH 20-Nov-2013 -CATEGORY 7 CompleteE2
SB PW600-72-63055
REPLACEMENT/MODIFICATION OF AIR COOLED OIL COOLER
COMPLIED WITH - AT MANUFACTUREMOC :
MTH 20-Nov-2013 A/RCATEGORY 7 CompleteE1
SB PW600-72-63076
REPLACEMENT/MODIFICATION OF OIL FILLER AND INDICATOR ASSEMBLY (SUPERSEDED BY PW600-72-63076 R01)
COMPLIED WITH - AT MANUFACTUREMOC :
MTH 20-Nov-2013 A/RCATEGORY 7 CompleteE2
SB PW600-72-63076
REPLACEMENT/MODIFICATION OF OIL FILLER AND INDICATOR ASSEMBLY (SUPERSEDED BY PW600-72-63076 R01)
COMPLIED WITH - AT MANUFACTUREMOC :
MTH 20-Nov-2013 -CATEGORY 5 CompleteE1
SB PW600-79-63008 R02
REPLACEMENT OF OIL PUMP HOUSING AND SPUR GEARS
COMPLIED WITH - AT MANUFACTUREMOC :
MTH 20-Nov-2013 -CATEGORY 5 CompleteE2
SB PW600-79-63008 R02
REPLACEMENT OF OIL PUMP HOUSING AND SPUR GEARS
COMPLIED WITH - AT MANUFACTUREMOC :
Page 40 of 50NOTE: Item Codes in italics show pre-migration CESCOM item codes and position (provided for cross-reference). Remains calculated from PrintDate for calendar items.
0:5419-Mar-2019230AIR COND
1:0419-Mar-201911031406:12ENG 2
1:0419-Mar-201911031406:12ENG 1
1:0419-Mar-201911031406:12AIRCRAFT
Average DailyUtilization
Last ActualDate
Events/LandingsHoursTracking Rate
YR-TRQReg No:
24-Mar-2019 6:11AM
20-Nov-2013
Owner: S.C. TOYO AVIATION S.R.L.
Print Date:
Airworthiness:
Aircraft Serial:
Aircraft Model: 510 - CITATION MUSTANG
Unit:
510-0433
-0433
CESCOM 10 - Aircraft Status Report
(ENG) DUE 2
(ENG) DUE 1
Service Bulletins
City Part Serial No
Part Number C/W Time 1
C/W Time 2 + or -
Adj. TBO 1
TBO 2 TSO 2
TSO 1
Remains
RemainsDescription
Drawing # / Task #Position
Item Code
Mod Lvl
MTH 20-Nov-2013 -CATEGORY 7 CompleteE1
SB PW600-79-63015
REPLACEMENT/MODIFICATION OF AIR COOLED OIL COOLER
COMPLIED WITH - AT MANUFACTUREMOC :
MTH 20-Nov-2013 -CATEGORY 7 CompleteE2
SB PW600-79-63015
REPLACEMENT/MODIFICATION OF AIR COOLED OIL COOLER
COMPLIED WITH - AT MANUFACTUREMOC :
MTH 20-Nov-2013 -CATEGORY 7 CompleteE1
SB PW600-79-63046
REPLACEMENT OF OIL FILTER IMPENDING BYPASS SWITCH
COMPLIED WITH - AT MANUFACTUREMOC :
MTH 20-Nov-2013 -CATEGORY 7 CompleteE2
SB PW600-79-63046
REPLACEMENT OF OIL FILTER IMPENDING BYPASS SWITCH
COMPLIED WITH - AT MANUFACTUREMOC :
MTH 20-Nov-2013 -CATEGORY 3 CompleteE1
SB PW600-79-63047 R02
REPLACEMENT OF AIR-COOLED OIL-COOLER PRESSURE-OIL-TUBE BOLTS (SUPERSEDED BY PW600-79-63047 R03)
COMPLIED WITH - AT MANUFACTUREMOC :
MTH 20-Nov-2013 -CATEGORY 3 CompleteE2
SB PW600-79-63047 R02
REPLACEMENT OF AIR-COOLED OIL-COOLER PRESSURE-OIL-TUBE BOLTS (SUPERSEDED BY PW600-79-63047 R03)
COMPLIED WITH - AT MANUFACTUREMOC :
-INFORMATIONAL CompleteSL 510-80-01 ENGINE STARTING
COMPLIED WITH - INFOMOC :
MTH -RECOMMENDED New Req
SL 510-80-02 STARTING - STARTER/GENERATOR REPLACEMENT PROGRAM
MOC :
Page 41 of 50NOTE: Item Codes in italics show pre-migration CESCOM item codes and position (provided for cross-reference). Remains calculated from PrintDate for calendar items.
0:5419-Mar-2019230AIR COND
1:0419-Mar-201911031406:12ENG 2
1:0419-Mar-201911031406:12ENG 1
1:0419-Mar-201911031406:12AIRCRAFT
Average DailyUtilization
Last ActualDate
Events/LandingsHoursTracking Rate
YR-TRQReg No:
24-Mar-2019 6:11AM
20-Nov-2013
Owner: S.C. TOYO AVIATION S.R.L.
Print Date:
Airworthiness:
Aircraft Serial:
Aircraft Model: 510 - CITATION MUSTANG
Unit:
510-0433
-0433
CESCOM 10 - Aircraft Status Report
(ENG) DUE 2
(ENG) DUE 1
Airworthiness Directives
City Part Serial No
Part Number C/W Time 1
C/W Time 2 + or -
Adj. TBO 1
TBO 2 TSO 2
TSO 1
Remains
RemainsDescription
Drawing # / Task #Position
Item Code
Mod Lvl
-MANDATORY N/A
EASA 2014-0088PARA (1)
REMOVE THE TEAM CVR P/N AP71232101 OR P/N AP71231101, AS APPLICABLE, FROM THE AIRCRAFT AND, DEPENDING ON OPERATIONALREGULATIONS, INSTALL A SERVICEABLE CVR IN ACCORDANCE WITH APPROVED AIRCRAFT MODIFICATION INSTRUCTIONS
NOT APPLICABLEMOC :
-MANDATORY
Complete
EASA 2014-0088PARA (2)
DO NOT INSTALL ON ANY AIRCRAFT A TEAM CVR P/N AP71232101 OR P/N AP71231101, AS REQUIRED BY PARAGRAPH (2.1) OR (2.2) OF THIS AD, ASAPPLICABLE
COMPLIED WITHMOC :
-MANDATORY N/A
EASA 2014-0088 APPLIANCE AD - COMMUNICATIONS - COCKPIT VOICE RECORDER - REPLACEMENT
NOT APPLICABLEMOC :
MTH 22-Apr-2014 -MANDATORY N/A
EASA 2013-0020R03 (1)
INSPECT THE MARKINGS OF SAFETY BELTS AND/OR TORSO RESTRAINT SYSTEMS, TO DETERMINE IF THEY HAVE BEEN MAINTAINED OR REPAIREDBY ORGANISATIONS OTHER THAN THE DESIGN APPROVAL HOLDER
NOT APPLICABLE - PARTS INSTALLED NEW ON A/CMOC :
MTH 22-Apr-2014 -MANDATORY N/A
EASA 2013-0020R03 (2)
VERIFY IF THE ORGANISATION IS LISTED AMONG THE AUTHORIZED MAINTENANCE OR REPAIR ORGANISATION REFERENCE DOCUMENTS QUOTEDIN THE REF. PUBLICATIONS SECTION OF THIS AD
NOT APPLICABLE - PARTS INTALLED ARE NEWMOC :
MTH 22-Apr-2014 -MANDATORY N/A
EASA 2013-0020R03 (3)
REMOVE AND REPLACE BELTS NOT MEETING THE CERTIFICATION REQUIREMENTS OR MAKE RELEVANT SEAT INOPERATIVE
NOT APPLICABLE - PARTS INSTALLED ARE NEWMOC :
MTH 22-Apr-2014 -MANDATORY Complete
EASA 2013-0020R03 (4)
AFTER 14 FEBRUARY 2013 [THE EFFECTIVE DATE OF THE ORIGINAL ISSUE OF THIS AD], DO NOT INSTALL SAFETY BELTS OR TORSO RESTRAINTSYSTEMS ON ANY AIRCRAFT, UNLESS INSPECTED AND CORRECTED IN COMPLIANCE WITH THE REQUIREMENTS OF THIS AD
COMPLIED WITHMOC :
LDG
HRS
MTH
130
176:29
22-Apr-2014 -MANDATORY
Complete
EASA 2013-0020R03
APPLIANCE AD - EQUIPMENT & FURNISHINGS - SAFETY BELTS / TORSO RESTRAINTSYSTEMS - INSPECTION / REPLACEMENT (SUPERSEDED BY 2013-0020 R04)
COMPLIED WITH - PARTS INSTALLED NEW ON A/CMOC :
MTH 24-Jul-2014
DUE
DUEMANDATORY N/A
EASA 2013-0020R04 (1)
INSPECT THE MARKINGS OF SAFETY BELTS AND/OR TORSO RESTRAINT SYSTEMS, TO DETERMINE IF THEY HAVE BEEN MAINTAINED OR REPAIREDBY ORGANISATIONS OTHER THAN THE DESIGN APPROVAL HOLDER
NOT APPLICABLE - PARTS INSTALLED NEW ON A/CMOC :
MTH 24-Jul-2014 1MANDATORY N/A
EASA 2013-0020R04 (2)
VERIFY IF THE ORGANISATION IS LISTED AMONG THE AUTHORIZED MAINTENANCE OR REPAIR ORGANISATION REFERENCE DOCUMENTS QUOTED INTHE REF. PUBLICATIONS SECTION OF THIS AD
NOT APPLICABLE - PARTS INSTALLED NEW ON A/CMOC :
MTH 24-Jul-2014 18MANDATORY N/A
EASA 2013-0020R04 (3)
REMOVE AND REPLACE BELTS NOT MEETING THE CERTIFICATION REQUIREMENTS OR MAKE RELEVANT SEAT INOPERATIVE
NOT APPLICABLE - PARTS INSTALLED NEW ON A/CMOC :
MTH 24-Jul-2014 -MANDATORY Complete
EASA 2013-0020R04 (4)
AFTER 14 FEBRUARY 2013 [THE EFFECTIVE DATE OF THE ORIGINAL ISSUE OF THIS AD], DO NOT INSTALL SAFETY BELTS OR TORSO RESTRAINTSYSTEMS ON ANY AIRCRAFT, UNLESS INSPECTED AND CORRECTED IN COMPLIANCE WITH THE REQUIREMENTS OF THIS AD
COMPLIED WITH - PARTS INSTALLED NEW ON A/CMOC :
MTH 24-Jul-2014 -MANDATORY Complete
EASA 2013-0020R04
APPLIANCE AD - EQUIPMENT & FURNISHINGS - SAFETY BELTS / TORSO RESTRAINT SYSTEMS - INSPECTION / REPLACEMENT
COMPLIED WITH - PARTS INSTALLED NEW ON A/CMOC :
Page 42 of 50NOTE: Item Codes in italics show pre-migration CESCOM item codes and position (provided for cross-reference). Remains calculated from PrintDate for calendar items.
0:5419-Mar-2019230AIR COND
1:0419-Mar-201911031406:12ENG 2
1:0419-Mar-201911031406:12ENG 1
1:0419-Mar-201911031406:12AIRCRAFT
Average DailyUtilization
Last ActualDate
Events/LandingsHoursTracking Rate
YR-TRQReg No:
24-Mar-2019 6:11AM
20-Nov-2013
Owner: S.C. TOYO AVIATION S.R.L.
Print Date:
Airworthiness:
Aircraft Serial:
Aircraft Model: 510 - CITATION MUSTANG
Unit:
510-0433
-0433
CESCOM 10 - Aircraft Status Report
(ENG) DUE 2
(ENG) DUE 1
Airworthiness Directives
City Part Serial No
Part Number C/W Time 1
C/W Time 2 + or -
Adj. TBO 1
TBO 2 TSO 2
TSO 1
Remains
RemainsDescription
Drawing # / Task #Position
Item Code
Mod Lvl
LDG
HRS
DAYS
127
169:32
11-Apr-2014 -MANDATORY
N/AEASA 2014-0019PARA (1)
AMEND THE AFM OF THE AFFECTED AIRCRAFT
NOT APPLICABLEMOC :
LDG
HRS
MTH
127
169:32
11-Apr-2014 -MANDATORY N/A
EASA 2014-0019PARA (2)
REPLACE THE SYSTEM INTERFACE UNIT P/N 503-24-() OR 503-42-()
NOT APPLICABLEMOC :
LDG
HRS
MTH
127
169:32
11-Apr-2014 -MANDATORY N/A
EASA 2014-0019PARA (3)
DO NOT INSTALL A HR SMITH (TECHNICAL DEVELOPMENTS) CPI SYSTEM SERIES 15-503-134 OR 15-503-134-1 EQUIPPED WITH CONTROL PANEL P/N503-22-(), BEACON RELEASE UNIT P/N 503-21 AND SYSTEM INTERFACE UNIT P/N 503-24-() OR P/N 503-42-(), EXCLUDING SYSTEM INTERFACE UNIT P/N503-24-A, OR 503-24-()-A, OR 503-24-G, OR 503-24-()-G, OR 503-42-A OR 503-42-()-A OR 503-42-G OR 503-42-()-G, ON AN AIRCRAFT, UNLESS INCOMPLIANCE WITH THE REQUIREMENTS OF THIS AD
NOT APPLICABLEMOC :
LDG
HRS
MTH
127
169:32
11-Apr-2014 -MANDATORY N/A
EASA 2014-0019PARA (4)
REMOVE AFM AMENDMENT AND PLACARD AS REQUIRED BY PARAGRAPH (1) OF THIS AD
NOT APPLICABLEMOC :
LDG
HRS
MTH
127
169:32
11-Apr-2014 -MANDATORY
N/A
EASA 2014-0019 APPLIANCE AD - EQUIPMENT / FURNISHINGS - CRASH POSITION INDICATOR - MODIFICATION AIRCRAFT FLIGHT MANUAL - AMENDMENT(SUPERSEDED BY EASA 2014-0095)
NOT APPLICABLEMOC :
MTH 24-Jun-2014 -MANDATORY N/A
EASA 2014-0095R01 (1)
INSTALL EQUIPMENT / FURNISHINGS - CRASH POSITION INDICATOR - MODIFICATION AIRCRAFT FLIGHT MANUAL - AMENDMENT A PLACARD "DO NOTUSE TRANSMIT OVER WATER" NEXT TO THE CPI CONTROL PANEL/AMEND THE AFM OF THE AIRCRAFT
NOT APPLICABLE - PART NOT INSTALLEDMOC :
MTH 24-Jun-2014 -MANDATORY N/A
EASA 2014-0095R01 (2)
INCORPORATION EQUIPMENT / FURNISHINGS - CRASH POSITION INDICATOR - MODIFICATION AIRCRAFT FLIGHT MANUAL - AMENDMENT OFAPPENDIX A OF THIS AD INTO THE EMERGENCY PROCEDURES SECTION OF THE AFM OF THE AIRCRAFT IS AN ACCEPTABLE METHOD TO COMPLYWITH THE REQUIREMENT OF PARAGRAPH (1.2) OF THIS AD
NOT APPLICABLE - PART NOT INSTALLEDMOC :
MTH 24-Jun-2014 -MANDATORY N/A
EASA 2014-0095R01 (3)
REPLACE EQUIPMENT / FURNISHINGS - CRASH POSITION INDICATOR - MODIFICATION AIRCRAFT FLIGHT MANUAL - AMENDMENT THE SYSTEMINTERFACE UNIT P/N 503-24-() (INCLUDING 503-24) OR P/N 503-42-() (INCLUDING 503-42) WITH AN IMPROVED PART P/N 503-24-A, OR P/N 503-24-()-A, ORP/N 503-24-G, OR P/N 503-24-()-G, OR P/N 503-42-A OR P/N 503-42-()-A OR P/N 503-42-G OR P/N 503-42-()-G (THAT INCORPORATES AUTOMATIC CPIDEPLOYMENT AFTER MANUAL ACTIVATION) IN ACCORDANCE WITH AN APPROVED AIRCRAFT MAINTENANCE INSTRUCTION
NOT APPLICABLE - PART NOT INSTALLEDMOC :
MTH 24-Jul-2014 -MANDATORY N/A
EASA 2014-0095R01 (4)
DO NOT INSTALL EQUIPMENT / FURNISHINGS - CRASH POSITION INDICATOR - MODIFICATION AIRCRAFT FLIGHT MANUAL - AMENDMENT A HR SMITH(TECHNICAL DEVELOPMENTS) CPI SYSTEM SERIES 15-503-134 OR 15-503-134-1 EQUIPPED WITH CONTROL PANEL P/N 503-22-(), BEACON RELEASEUNIT P/N 503-21 AND SYSTEM INTERFACE UNIT P/N 503-24-() (INCLUDING 503-24) OR P/N 503-42-() (INCLUDING 503-42) EXCLUDING SYSTEMINTERFACE UNIT P/N 503-24-A OR P/N 503-24-()-A OR P/N 503-24-G OR P/N 503-24-()-G OR P/N 503-42-A OR P/N 503-42-()-A OR P/N 503-42-G OR P/N 503-42-()-G ON AN AIRCRAFT UNLESS IN COMPLIANCE WITH THE REQUIREMENTS OF THIS AD
NOT APPLICABLE - PART NOT INSTALLEDMOC :
Page 43 of 50NOTE: Item Codes in italics show pre-migration CESCOM item codes and position (provided for cross-reference). Remains calculated from PrintDate for calendar items.
0:5419-Mar-2019230AIR COND
1:0419-Mar-201911031406:12ENG 2
1:0419-Mar-201911031406:12ENG 1
1:0419-Mar-201911031406:12AIRCRAFT
Average DailyUtilization
Last ActualDate
Events/LandingsHoursTracking Rate
YR-TRQReg No:
24-Mar-2019 6:11AM
20-Nov-2013
Owner: S.C. TOYO AVIATION S.R.L.
Print Date:
Airworthiness:
Aircraft Serial:
Aircraft Model: 510 - CITATION MUSTANG
Unit:
510-0433
-0433
CESCOM 10 - Aircraft Status Report
(ENG) DUE 2
(ENG) DUE 1
Airworthiness Directives
City Part Serial No
Part Number C/W Time 1
C/W Time 2 + or -
Adj. TBO 1
TBO 2 TSO 2
TSO 1
Remains
RemainsDescription
Drawing # / Task #Position
Item Code
Mod Lvl
MTH 24-Jun-2014 -MANDATORY N/A
EASA 2014-0095R01
APPLIANCE AD - EQUIPMENT / FURNISHINGS - CRASH POSITION INDICATOR - MODIFICATION AIRCRAFT FLIGHT MANUAL - AMENDMENT
NOT APPLICABLE - PART NOT INSTALLEDMOC :
-MANDATORY N/A
EASA 2014-0125PARA (1)
AMEND THE AFM OF AFFECTED AIRCRAFT TO INCORPORATE TEMPORARY CPI SIU OPERATING PROCEDURES BY INSERTING A COPY OF APPENDIX 1OF THIS AD (OR ITS TEXT) INTO THE APPLICABLE NORMAL PROCEDURES SECTION OF THE AFM
NOT APPLICABLE - PARTS NOT INSTALLEDMOC :
-MANDATORY N/A
EASA 2014-0125PARA (2)
ACCOMPLISH THE COMPLETE START-UP PROCEDURE/APPLICABLE START-UP PROCEDURE/SHUTDOWN PROCEDURE
NOT APPLICABLE - PARTS NOT INSTALLEDMOC :
-MANDATORY N/A
EASA 2014-0125PARA (3)
COMPLIANCE WITH THE REQUIREMENTS OF PARAGRAPH (2) OF THIS AD
NOT APPLICABLE - PARTS NOT INSTALLEDMOC :
-MANDATORY N/A
EASA 2014-0125PARA (4)
REPLACE THE CPI SIU HAVING P/N 503-24 OR P/N 503-24-2 OR P/N 503-24-6 WITH AN IMPROVED UNIT P/N 503-24G OR P/N 503-24-2G OR P/N 503-24-6GIN ACCORDANCE WITH THE APPLICABLE AIRCRAFT DESIGN APPROVAL HOLDER SERVICE INSTRUCTIONS AND, CONCURRENTLY, REMOVE THETEMPORARY AFM PROCEDURE AS REQUIRED BY PARAGRAPH (2) OF THIS AD
NOT APPLICABLE - PARTS NOT INSTALLEDMOC :
-MANDATORY N/A
EASA 2014-0125PARA (5)
MODIFICATION OF AN AIRCRAFT AS REQUIRED BY PARAGRAPH (4) OF THIS AD CONSTITUTES TERMINATING ACTION FOR ACCOMPLISHMENT OF THEPROCEDURES AS REQUIRED BY PARAGRAPH (2) OF THIS AD
NOT APPLICABLE - PARTS NOT INSTALLEDMOC :
-MANDATORY N/A
EASA 2014-0125PARA (6)
FROM THE EFFECTIVE DATE OF THIS AD, INSTALLATION ON AN AIRCRAFT OF AN HR SMITH (TECHNICAL DEVELOPMENTS) CPI SYSTEM SERIES 15-503-134-1 EQUIPPED WITH BRU P/N 503-21-1 AND SIU P/N 503-24 OR P/N 503-24-2 OR P/N 503-24-6 IS ALLOWED, PROVIDED THE AIRCRAFT IS OPERATEDIN COMPLIANCE WITH THE PROCEDURES AS REQUIRED BY THIS AD
NOT APPLICABLE - PARTS NOT INSTALLEDMOC :
-MANDATORY N/A
EASA 2014-0125PARA (7)
AFTER REPLACEMENT OF THE CPI SIU ON AN AIRCRAFT AS REQUIRED BY PARAGRAPH (4) OF THIS AD, DO NOT INSTALL AN SIU P/N 503-24 OR P/N503-24-2 OR P/N 503-24-6 ON THE CPI SYSTEM OF THAT AIRCRAFT
NOT APPLICABLE - PARTS NOT INSTALLEDMOC :
MTH -MANDATORY N/A
EASA 2014-0125 APPLIANCE AD - EQUIPMENT / FURNISHINGS - CRASH POSITION INDICATOR SYSTEM - REPLACEMENT; AIRCRAFT FLIGHT MANUAL - AMENDMENT
NOT APPLICABLE - PART NOT INSTALLEDMOC :
-MANDATORY
N/AEASA 2014-0187PARA (1)
INSPECT THE SAFETY BELT ATTACHMENT BOLTS
NOT APPLICABLE - PARTS NOT INSTALLEDMOC :
-MANDATORY N/A
EASA 2014-0187PARA (2)
IF, DURING THE INSPECTION AS REQUIRED BY PARAGRAPH (1) OF THIS AD, DETACHED OR LOOSENED SAFETY BELT ATTACHMENT BOLTS AREFOUND, BEFORE NEXT FLIGHT, RE-TORQUE THE AFFECTED BOLTS TO THE VALUE AS DEFINED IN, AND IN ACCORDANCE WITH THE INSTRUCTIONSOF, GEVEN SB NO. D103-25-004 REVISION 2.
NOT APPLICABLE - PARTS NOT INSTALLEDMOC :
-MANDATORY N/A
EASA 2014-0187PARA (3)
FOR SPECIFIC D1-03 SEAT ASSEMBLIES (P/N AS IDENTIFIED IN TABLE 1.1.1 OF GEVEN SB NO. D103-25-004 REVISION 2, EFF CODE FROM AAA TO AUC),WITHIN 6 MONTHS AFTER THE EFFECTIVE DATE OF THIS AD, MODIFY THE SEAT BELT ATTACHMENT ASSEMBLY ON THE AISLE SIDE SPREADER OFSTANDARD AND LAST ROW SEATS IN ACCORDANCE WITH THE INSTRUCTIONS OF GEVEN SB NO. D103-25-004 REVISION 2.
NOT APPLICABLE - PARTS NOT INSTALLEDMOC :
-MANDATORY N/A
EASA 2014-0187PARA (4)
AS AN ALTERNATIVE TO THE CORRECTIVE ACTIONS AS REQUIRED BY PARAGRAPH (1) OR (2) OF THIS AD, AS APPLICABLE, BEFORE NEXT FLIGHT,BLOCK EACH AFFECTED SEAT FOR OCCUPANCY, PENDING ACCOMPLISHMENT OF THE APPLICABLE CORRECTIVE ACTION(S).
NOT APPLICABLE - PARTS NOT INSTALLEDMOC :
Page 44 of 50NOTE: Item Codes in italics show pre-migration CESCOM item codes and position (provided for cross-reference). Remains calculated from PrintDate for calendar items.
0:5419-Mar-2019230AIR COND
1:0419-Mar-201911031406:12ENG 2
1:0419-Mar-201911031406:12ENG 1
1:0419-Mar-201911031406:12AIRCRAFT
Average DailyUtilization
Last ActualDate
Events/LandingsHoursTracking Rate
YR-TRQReg No:
24-Mar-2019 6:11AM
20-Nov-2013
Owner: S.C. TOYO AVIATION S.R.L.
Print Date:
Airworthiness:
Aircraft Serial:
Aircraft Model: 510 - CITATION MUSTANG
Unit:
510-0433
-0433
CESCOM 10 - Aircraft Status Report
(ENG) DUE 2
(ENG) DUE 1
Airworthiness Directives
City Part Serial No
Part Number C/W Time 1
C/W Time 2 + or -
Adj. TBO 1
TBO 2 TSO 2
TSO 1
Remains
RemainsDescription
Drawing # / Task #Position
Item Code
Mod Lvl
-MANDATORY N/A
EASA 2014-0187 APPLIANCE AD - EQUIPMENT & FURNISHINGS – SAFETY BELT ATTACHMENT BOLTS – INSPECTION / REPLACEMENT
NOT APPLICABLE - PARTS NOT INSTALLEDMOC :
-MANDATORY N/A
EASA 2014-0279PARA (1)
INSPECT THE LABEL OF THE ROTARY BUCKLE SUB-ASSEMBLY TO DETERMINE ITS PART NUMBER (P/N) AND SERIAL NUMBER (S/N)
NOT APPLICABLE - PART NOT INSTALLEDMOC :
-MANDATORY N/A
EASA 2014-0279PARA (1.1)
REPLACE THE ROTARY BUCKLE SUB-ASSEMBLY WITH A SERVICEABLE PART
NOT APPLICABLE - PART NOT INSTALLEDMOC :
-MANDATORY N/A
EASA 2014-0279PARA (1.2)
MARK THE SEAT AS “INOPERATIVE” UNTIL REPLACEMENT OF THE ROTARY BUCKLE SUB-ASSEMBLY AS REQUIRED BY PARAGRAPH (2) OF THIS AD
NOT APPLICABLE - PART NOT INSTALLEDMOC :
-MANDATORY
N/A
EASA 2014-0279PARA (2)
REPLACE EACH ROTARY BUCKLE SUB-ASSEMBLY HAVING A P/N AND S/N AS SPECIFIED IN ROMTEX ANJOU AERONAUTIQUE SB 358SB-14-101 WITH ASERVICEABLE PART
NOT APPLICABLE - PART NOT INSTALLEDMOC :
-MANDATORY N/A
EASA 2014-0279PARA (3)
DO NOT INSTALL:- ON ANY RESTRAINT SYSTEM A SPARE ROTARY BUCKLE SUB-ASSEMBLY, OR- ON ANY AIRCRAFT A RESTRAINT SYSTEM EQUIPPEDWITH A ROTARY BUCKLESUB-ASSEMBLY HAVING A P/N AND A S/N LISTED IN ROMTEX ANJOU AERONAUTIQUE SB 358SB-14-101, UNLESS THE SUB-ASSEMBLY HAS BEEN REPAIRED,
NOT APPLICABLE - PART NOT INSTALLEDMOC :
MTH -MANDATORY N/A
EASA 2014-0279 APPLIANCE AD - EQUIPMENT / FURNISHING - RESTRAINT SYSTEM ROTARY BUCKLE SUBASSEMBLY - IDENTIFICATION / REPLACEMENT
NOT APPLICABLE - PART NOT INSTALLEDMOC :
ACH
LDG
HRS
MTH
170
808
949:54
13-Dec-2017 - N/A
FAA 2017-16-01PARA (G)
LRBS
PERFORM GENERAL VISUAL INSPECTIONS OF THE ELT FOR DISCREPANCIES; CHECKS , TESTS AND VERIFICATIONS AS APPLICABLE, TO ENSURETHE ELT IS FUNCTIONING, AND ALL APPLICABLE CORRECTIVE ACTIONS
NOT APPLICABLE - PART NOT INSTALLEDMOC :
ACH
LDG
HRS
MTH
170
808
949:54
13-Dec-2017 -MANDATORY N/A
FAA 2017-16-01PARA (J) LRBS
OPTIONAL TERMINATING ACTION: REPLACE ELT WITH A SERVICEABLE FAA-APPROVED ELT
NOT APPLICABLE - PART NOT INSTALLEDMOC :
ACH
LDG
HRS
MTH
170
808
949:54
13-Dec-2017 -MANDATORY N/A
FAA 2017-16-01
LRBS
EQUIPMENT / FURNISHINGS - AMERI-KING CORPORATION MODEL AK-450() AND AK-451() SERIES EMERGENCY LOCATOR TRANSMITTERS -REPETATIVE INSPECTIONS, CHECKS, TESTS AND VERIFICATIONS
NOT APPLICABLE - PART NOT INSTALLEDMOC :
LDG
HRS
MTH
503
580:06
07-Mar-2016 -MANDATORY N/A
EASA 2016-0024PARA (1) LRBS
INSPECT EACH SIEMENS SMOKE DETECTOR TO DETERMINE WHETHER IT IS AN AFFECTED PART
NOT APPLICABLE - NOT APPLICABLE, PART NOT INSTALLED IN AIRCRAFTMOC :
Page 45 of 50NOTE: Item Codes in italics show pre-migration CESCOM item codes and position (provided for cross-reference). Remains calculated from PrintDate for calendar items.
0:5419-Mar-2019230AIR COND
1:0419-Mar-201911031406:12ENG 2
1:0419-Mar-201911031406:12ENG 1
1:0419-Mar-201911031406:12AIRCRAFT
Average DailyUtilization
Last ActualDate
Events/LandingsHoursTracking Rate
YR-TRQReg No:
24-Mar-2019 6:11AM
20-Nov-2013
Owner: S.C. TOYO AVIATION S.R.L.
Print Date:
Airworthiness:
Aircraft Serial:
Aircraft Model: 510 - CITATION MUSTANG
Unit:
510-0433
-0433
CESCOM 10 - Aircraft Status Report
(ENG) DUE 2
(ENG) DUE 1
Airworthiness Directives
City Part Serial No
Part Number C/W Time 1
C/W Time 2 + or -
Adj. TBO 1
TBO 2 TSO 2
TSO 1
Remains
RemainsDescription
Drawing # / Task #Position
Item Code
Mod Lvl
LDG
HRS
MTH
503
580:06
07-Mar-2016 -MANDATORY N/A
EASA 2016-0024PARA (2.1) LRBS
REPLACE CARGO COMPARTMENT SMOKE DETECTORS, IDENTIFIED IN PARAGRAPH (1), IN ACCORDANCE WITH TABLE 1 OR TABLE 2
NOT APPLICABLE - NOT APPLICABLE, PART NOT INSTALLED IN AIRCRAFTMOC :
LDG
HRS
MTH
503
580:06
07-Mar-2016 -MANDATORY N/A
EASA 2016-0024PARA (2.2)
LRBS
REPLACE PASSENGER, CABIN OR ANY OTHER ON BOARD LOCATION SMOKE DETECTORS, IDENTIFIED IN PARAGRAPH (1), IN ACCORDANCE WITHTABLE 3
NOT APPLICABLE - NOT APPLICABLE, PART NOT INSTALLED IN AIRCRAFTMOC :
LDG
HRS
MTH
503
580:06
07-Mar-2016 -MANDATORY N/A
EASA 2016-0024PARA (2.3) LRBS
REPLACE REPAIRED SMOKE DETECTOR IDENTIFIED IN APPENDIX 1
NOT APPLICABLE - NOT APPLICABLE, PART NOT INSTALLED IN AIRCRAFTMOC :
LDG
HRS
MTH
503
580:06
07-Mar-2016 -MANDATORY N/A
EASA 2016-0024PARA (3)
LRBS
FROM THE EFFECTIVE DATE OF THIS AD, DO NOT INSTALL ON ANY AEROPLANE AN AFFECTED P/N SMOKE DETECTOR UNLESS THE UNIT (GMC ONLY)IS MARKED 'SIL PMC-26-002'
NOT APPLICABLE - NOT APPLICABLE, PART NOT INSTALLED IN AIRCRAFTMOC :
LDG
HRS
MTH
503
580:06
07-Mar-2016 -MANDATORY N/A
EASA 2016-0024
LRBS
FIRE PROTECTION - OPTICAL AND AMBIENT SMOKE DETECTORS - IDENTIFICATION / REPLACEMENT
NOT APPLICABLE - NOT APPLICABLE, PART NOT INSTALLED IN AIRCRAFTMOC :
MTH -MANDATORY N/A
EASA 2016-0044PARA (1)
INSPECT EACH FIRE EXTINGUISHER, EXCEPT THOSE HAVING P/N 57333 SERIES, INSTALLED ON BAE146 AND RJ AEROPLANES, AND THOSE HAVINGP/N57183 SERIES, INSTALLED ON ATP AEROPLANES, AND DEPENDING ON FINDINGS, ACCOMPLISH CORRECTIVE ACTIONS IN ACCORDANCE WITHTHE INSTRUCTIONS OF KG SB 26-080 REVISION 1
NOT APPLICABLE - PART NOT INSTALLEDMOC :
-MANDATORY N/A
EASA 2016-0044PARA (2)
ACCOMPLISHMENT OF AN OVERHAUL (SEE NOTE 2 OF THIS AD) OF A FIRE EXTINGUISHER BY KIDDE GRAVINER OR HUGEN, OR IN ACCORDANCEWITH THE INSTRUCTIONS OF KG SIL 01-10 OR IN ACCORDANCE WITH KG CMM 26-21-40 REVISION 14 OR LATER OR KG CMM 26-21-52 REVISION 13 ORLATER (AS APPLICABLE TO FIRE EXTINGUISHER P/N) IS ACCEPTABLE TO COMPLY WITH THE REQUIREMENT OF PARAGRAPH (1).
NOT APPLICABLE - PART NOT INSTALLEDMOC :
-MANDATORY Complete
EASA 2016-0044PARA (3)
FROM THE EFFECTIVE DATE OF THIS AD DO NOT INSTALL ON ANY AIRCRAFT AN AFFECTED FIRE EXTINGUISHER, UNLESS IT IS NEW, OR HAS PASSEDAN INSPECTION IN ACCORDANCE WITH THE INSTRUCTIONS OF KG SB 26-080 REVISION 1, OR IT HAS BEEN OVERHAULED (SEE NOTE 2) BY KG, OR BYHUGEN OR IN ACCORDANCE WITH THE INSTRUCTIONS OF KG SIL 01-10 OR IN ACCORDANCE WITH THE INSTRUCTIONS OF KG CMM 26-21-40REVISION 14, OR OF KG CMM 26-21-52 REVISION 13, AS APPLICABLE TO FIRE EXTINGUISHER P/N
COMPLIED WITHMOC :
MTH -MANDATORY N/A
EASA 2016-0044 APPLIANCE AD - ATA 26 - FIRE PROTECTION - ENGINE AND AUXILIARY POWER UNIT AUTOMATIC FIRE EXTINGUISHERS - INSPECTION/OVERHAUL
NOT APPLICABLE - PART NOT INSTALLEDMOC :
Page 46 of 50NOTE: Item Codes in italics show pre-migration CESCOM item codes and position (provided for cross-reference). Remains calculated from PrintDate for calendar items.
0:5419-Mar-2019230AIR COND
1:0419-Mar-201911031406:12ENG 2
1:0419-Mar-201911031406:12ENG 1
1:0419-Mar-201911031406:12AIRCRAFT
Average DailyUtilization
Last ActualDate
Events/LandingsHoursTracking Rate
YR-TRQReg No:
24-Mar-2019 6:11AM
20-Nov-2013
Owner: S.C. TOYO AVIATION S.R.L.
Print Date:
Airworthiness:
Aircraft Serial:
Aircraft Model: 510 - CITATION MUSTANG
Unit:
510-0433
-0433
CESCOM 10 - Aircraft Status Report
(ENG) DUE 2
(ENG) DUE 1
Airworthiness Directives
City Part Serial No
Part Number C/W Time 1
C/W Time 2 + or -
Adj. TBO 1
TBO 2 TSO 2
TSO 1
Remains
RemainsDescription
Drawing # / Task #Position
Item Code
Mod Lvl
LDG
HRS
DAYS
887
1067:42
23-Apr-2018 -MANDATORY Complete
FAA 2018-07-13
LRBS
LANDING GEAR - INSPECTION OF THE BRAKE PAD WEAR INDICATOR PINS AND REPLACEMENT OF THE BRAKE ASSEMBLY IF ANY PIN IS FOUND TOHAVE AN INCORRECT LENGTH
COMPLIED WITH - PARTS CHECKED I.A.W SL510-32-08MOC :
MTH -MANDATORY N/A
EASA 2010-0003R02 (1)
VERIFY AIRCRAFT TYPE MODE STRAPPING CODE S SET TO ¿0¿ (ZERO) OR ¿1¿, AS DEFINED IN ROCKWELL-COLLINS SERVICE LETTER TDR-94( ) SIL07-2.
NOT APPLICABLE - PART NOT INSTALLEDMOC :
-MANDATORY
N/AEASA 2010-0003R02 (2)
EXEMPTIONS: DASSAULT AEROPLANES
NOT APPLICABLE - PART NOT INSTALLEDMOC :
-MANDATORY
N/AEASA 2010-0003R02 (3)
EXEMPTIONS: ATR 42 AND ATR 72 AEROPLANES
NOT APPLICABLE - PART NOT INSTALLEDMOC :
-MANDATORY
N/AEASA 2010-0003R02 (4)
EXEMPTIONS: SAAB 2000 AEROPLANES
NOT APPLICABLE - PART NOT INSTALLEDMOC :
-MANDATORY N/A
EASA 2010-0003R02 (5)
EXEMPTIONS: BOMBARDIER AEROSPACE (CANADAIR) AEROPLANES: CL-600-2B16 (604 VARIANT) AND CL-600-2B19 (RJ100 AND RJ200)
NOT APPLICABLE - PART NOT INSTALLEDMOC :
-MANDATORY N/A
EASA 2010-0003R02 (6)
EXEMPTIONS: CESSNA AIRCRAFT COMPANY AEROPLANES: CESSNA MODEL 525, 525A, 525B; AND CESSNA MODEL 525, 525A, 525B, 560; 560XL
NOT APPLICABLE - PART NOT INSTALLEDMOC :
-MANDATORY N/A
EASA 2010-0003R02 (7)
EXEMPTIONS: PIAGGIO AERO INDUSTRIES AEROPLANES: P.180 (AVANTI) AND P.180 (AVANTI II)
NOT APPLICABLE - PART NOT INSTALLEDMOC :
-MANDATORY N/A
EASA 2010-0003R02
APPLIANCE AD - NAVIGATION - MODE S TRANSPONDER AIRCRAFT TYPE MODE STRAPPING - CHECK / MODIFICATION
NOT APPLICABLE - PART NOT INSTALLEDMOC :
-MANDATORY N/A
EASA 2015-0093PARA (1)
AMEND THE AFM OF THE AIRCRAFT BY INSERTING A TEMPORARY REVISION (TR) TO THE AFM (SUPPLEMENT)
NOT APPLICABLE - PART NOT INSTALLEDMOC :
-MANDATORY N/A
EASA 2015-0093PARA (2)
MODIFY THE AIRCRAFT BY REPLACING EACH AHRS UNIT HAVING A P/N SPECIFIED AS ‘OLD’ IN TABLE 2 OF THIS AD WITH A MODIFIED UNIT, HAVING AP/N SPECIFIED AS ‘NEW’ IN TABLE 2 OF THIS AD
NOT APPLICABLE - PART NOT INSTALLEDMOC :
-MANDATORY N/A
EASA 2015-0093PARA (3)
CONCURRENT WITH MODIFICATION OF AN AIRCRAFT AS REQUIRED BY PARAGRAPH (2) OF THIS AD, THE AFM CHANGE, IF REQUIRED BY PARAGRAPH(1) OF THIS AD (SEE NOTE 1 OF THIS AD), CAN BE REMOVED FROM THAT AIRCRAFT
NOT APPLICABLE - PART NOT INSTALLEDMOC :
-MANDATORY N/A
EASA 2015-0093PARA (4)
DO NOT INSTALL ON ANY AIRCRAFT A LCR-100 AHRS UNIT, HAVING A P/N SPECIFIED AS ‘OLD’ IN TABLE 1 OF THIS AD
NOT APPLICABLE - PART NOT INSTALLEDMOC :
MTH -MANDATORY N/A
EASA 2015-0093 APPLIANCE AD - NAVIGATION ¿ ATTITUDE HEADING REFERENCE SYSTEM ¿ MODIFICATION / REPLACEMENT
NOT APPLICABLE - PART NOT INSTALLEDMOC :
-MANDATORY N/A
FAA 2014-18-01 APPLIANCE AD - NAVIGATION - ROCKWELL COLLINS, INC. MODE S TRANSPONDERS - INSPECTION / MODIFICATION
NOT APPLICABLE - PARTS NOT INSTALLEDMOC :
Page 47 of 50NOTE: Item Codes in italics show pre-migration CESCOM item codes and position (provided for cross-reference). Remains calculated from PrintDate for calendar items.
0:5419-Mar-2019230AIR COND
1:0419-Mar-201911031406:12ENG 2
1:0419-Mar-201911031406:12ENG 1
1:0419-Mar-201911031406:12AIRCRAFT
Average DailyUtilization
Last ActualDate
Events/LandingsHoursTracking Rate
YR-TRQReg No:
24-Mar-2019 6:11AM
20-Nov-2013
Owner: S.C. TOYO AVIATION S.R.L.
Print Date:
Airworthiness:
Aircraft Serial:
Aircraft Model: 510 - CITATION MUSTANG
Unit:
510-0433
-0433
CESCOM 10 - Aircraft Status Report
(ENG) DUE 2
(ENG) DUE 1
Airworthiness Directives
City Part Serial No
Part Number C/W Time 1
C/W Time 2 + or -
Adj. TBO 1
TBO 2 TSO 2
TSO 1
Remains
RemainsDescription
Drawing # / Task #Position
Item Code
Mod Lvl
MTH -MANDATORY
N/A
FAA 2015-10-51-E APPLIANCE AD - AVIDYNE INTEGRATED FLIGHT DISPLAY (IFD)- INCORPORATE OPERATIONAL LIMITATIONS INTO LIMITATIONS SECTION OF THE AFMOR AFMS.
NOT APPLICABLE - PART NOT INSTALLEDMOC :
-MANDATORY
N/A
FAA 2015-10-51 APPLIANCE AD - AVIDYNE INTEGRATED FLIGHT DISPLAY (IFD)- INCORPORATE OPERATIONAL LIMITATIONS INTO LIMITATIONS SECTION OF THE AFMOR AFMS
NOT APPLICABLE - PART NOT INSTALLEDMOC :
MTH 26-Jun-2014 -MANDATORY N/A
EASA 2014-0142PARA (1)
ACCOMPLISH ACCOMPLISH THE ACTIONS AS SPECIFIED IN PARAGRAPHS (1.1) AND (1.2) OF THIS AD - DETERMINE THE DATE OF MANUFACTURING /REPLACE THE HARNESS INFLATION HOSE P/N 445952 WITH A SERVICEABLE PART, OR REMOVE THE INFLATABLE HARNESS FROM THE MASKREGULATOR AND REPLACE IT WITH A SERVICEABLE HARNESS
NOT APPLICABLE - DUE TO INSTALLED PARTSMOC :
MTH 26-Jun-2014 -MANDATORY N/A
EASA 2014-0142PARA (2)
ACCOMPLISH AN OXYGEN MASK REGULATOR EQUIPPED WITH A P/N MXH21-1 INFLATABLE HARNESS HAVING A DMF CODE OF NOVEMBER 2008 (0845-S OR 08/45-S) OR EARLIER, AND THOSE WITH A DMF OF JANUARY 2011 (1101-S OR 11/01-S) OR LATER, IS EXCLUDED FROM THE INSPECTION ANDREPLACEMENT REQUIREMENTS OF PARAGRAPH (1) OF THIS AD
NOT APPLICABLE - DUE TO INSTALLED PARTSMOC :
MTH 26-Jun-2014 -MANDATORY N/A
EASA 2014-0142PARA (3)
ACCOMPLISH IT IS ALLOWED TO INSTALL ON AN AEROPLANE A FLIGHT CREW OXYGEN MASK REGULATOR, HAVING A P/N AS IDENTIFIED IN SECTION1.A.(1) OF ZODIAC AEROTECHNICS SB MC10-35-274, PROVIDED IT HAS BEEN DETERMINED THAT A P/N MXH21-31 INFLATABLE HARNESS IS INSTALLED,OR THAT THE P/N MXH21-1 INFLATABLE HARNESS INSTALLED ON THAT FLIGHT CREW OXYGEN MASK REGULATOR HAS BEEN CORRECTED, ASREQUIRED BY THIS AD.
NOT APPLICABLEMOC :
LDG
HRS
MTH
204
255
26-Jun-2014 -MANDATORY N/A
EASA 2014-0142R01 (1)
EDDL
ACCOMPLISH ACCOMPLISH THE ACTIONS AS SPECIFIED IN PARAGRAPHS (1.1) AND (1.2) OF THIS AD - DETERMINE THE DATE OF MANUFACTURING /REPLACE THE HARNESS INFLATION HOSE P/N 445186 OR P/N 445952, AS APPLICABLE, WITH A SERVICEABLE PART, OR REMOVE THE INFLATABLEHARNESS FROM THE MASK REGULATOR AND REPLACE IT WITH A SERVICEABLE HARNESS
NOT APPLICABLE - PILOT AND COPILOT OXYGEN MASKS NOT AFFECTEDMOC :
LDG
HRS
MTH
204
255
26-Jun-2014 -MANDATORY N/A
EASA 2014-0142R01 (2)
EDDL
ACCOMPLISH AN OXYGEN MASK REGULATOR EQUIPPED WITH A P/N MXH20-1 OR P/N MXH21-1 INFLATABLE HARNESS HAVING A DMF CODE OFNOVEMBER 2008 (0845-S OR 08/45-S) OR EARLIER, AND THOSE WITH A DMF OF JANUARY 2011 (1101-S OR 11/01-S) OR LATER, IS EXCLUDED FROMTHE INSPECTION AND REPLACEMENT REQUIREMENTS OF PARAGRAPH (1) OF THIS AD
NOT APPLICABLE - PILOT AND COPILOT OXYGEN MASKS NOT AFFECTEDMOC :
LDG
HRS
MTH
204
255
26-Jun-2014 -MANDATORY N/A
EASA 2014-0142R01 (3)
EDDL
ACCOMPLISH IT IS ALLOWED TO INSTALL ON AN AEROPLANE A FLIGHT CREW OXYGEN MASK REGULATOR, HAVING A P/N AS IDENTIFIED IN SECTION1.A.(1) OF ZODIAC AEROTECHNICS SB MC10-35-274, PROVIDED IT HAS BEEN DETERMINED THAT A P/N MXH21-31 INFLATABLE HARNESS IS INSTALLED,OR THAT THE P/N MXH20-1 OR P/N MXH21-1 INFLATABLE HARNESS INSTALLED ON THAT FLIGHT CREW OXYGEN MASK REGULATOR HAS BEENCORRECTED, AS REQUIRED BY THIS AD
NOT APPLICABLE - PILOT AND COPILOT OXYGEN MASKS NOT AFFECTEDMOC :
LDG
HRS
MTH
204
255
26-Jun-2014 -MANDATORY N/A
EASA 2014-0142R01 EDDL
APPLIANCE AD - OXYGEN ¿ OXYGEN MASK REGULATOR INFLATABLE HARNESS / INFLATION HOSE ¿ IDENTIFICATION / REPLACEMENT
NOT APPLICABLE - PILOT AND COPILOT OXYGEN MASKS NOT AFFECTEDMOC :
Page 48 of 50NOTE: Item Codes in italics show pre-migration CESCOM item codes and position (provided for cross-reference). Remains calculated from PrintDate for calendar items.
0:5419-Mar-2019230AIR COND
1:0419-Mar-201911031406:12ENG 2
1:0419-Mar-201911031406:12ENG 1
1:0419-Mar-201911031406:12AIRCRAFT
Average DailyUtilization
Last ActualDate
Events/LandingsHoursTracking Rate
YR-TRQReg No:
24-Mar-2019 6:11AM
20-Nov-2013
Owner: S.C. TOYO AVIATION S.R.L.
Print Date:
Airworthiness:
Aircraft Serial:
Aircraft Model: 510 - CITATION MUSTANG
Unit:
510-0433
-0433
CESCOM 10 - Aircraft Status Report
(ENG) DUE 2
(ENG) DUE 1
Airworthiness Directives
City Part Serial No
Part Number C/W Time 1
C/W Time 2 + or -
Adj. TBO 1
TBO 2 TSO 2
TSO 1
Remains
RemainsDescription
Drawing # / Task #Position
Item Code
Mod Lvl
MTH 26-Jun-2014 -MANDATORY
N/A
EASA 2014-0142 APPLIANCE AD - OXYGEN - OXYGEN MASK REGULATOR INFLATABLE HARNESS / INFLATION HOSE - IDENTIFICATION / REPLACEMENT (SUPERSEDEDBY 2014-0142 R01)
NOT APPLICABLE - DUE TO INSTALLED PARTSMOC :
LDG
HRS
MTH
887
1067:42
19-Apr-2018 -MANDATORY N/A
FAA 2016-11-20PARA (G)
LRBS
PHYSICALLY INSPECT THE PBE POUCH TO DETERMINE IF IT HAS AN INTACT VACUUM SEAL IN ACCORDANCE WITH B/E AEROSPACE SERVICEBULLETIN NO. 119003-35-011, REV .000, DATED FEBRUARY 4, 2015, PARA III.A.1 SUPERSEDED BY FAA AD 2017-18-12
NOT APPLICABLE - PART NOT INSTALLEDMOC :
LDG
HRS
MTH
887
1067:42
19-Apr-2018 -MANDATORY N/A
FAA 2016-11-20PARA (H.1)
LRBS
REPLACEMENT OF A PBE POUCH, FOUND DURING THE INSPECTION IN PARAGRAPH (G) OF THIS AD, THAT DOES NOT HAVE AN INTACT VACUUMSEAL. SUPERSEDED BY FAA AD 2017-18-12
NOT APPLICABLE - PART NOT INSTALLEDMOC :
LDG
HRS
MTH
887
1067:42
19-Apr-2018 -MANDATORY
N/A
FAA 2016-11-20PARA (H.2)
LRBS
REPLACEMENT OF A PBE POUCH, FOUND DURING THE INSPECTION IN PARAGRAPH (G) OF THIS AD, WHERE THE VACUUM SEAL IS INTACT.SUPERSEDED BY FAA AD 2017-18-12
NOT APPLICABLE - PART NOT INSTALLEDMOC :
LDG
HRS
MTH
887
1067:42
19-Apr-2018 -MANDATORY N/A
FAA 2016-11-20
LRBS
APPLIANCE AD - OXYGEN - INSPECTION AND REPLACEMENT OF B/E AEROSPACE PROTECTIVE BREATHING EQUIPMENT (PBE), PART NUMBER 119003-11 THAT ARE INSTALLED ON AIRPLANES. SUPERSEDED BY FAA AD 2017-18-12
NOT APPLICABLE - PART NOT INSTALLEDMOC :
LDG
HRS
MTH
887
1067:42
23-Apr-2018 -MANDATORY N/A
FAA 2017-18-12PARA (G) LRBS
INSPECTION RETAINED FROM AD 2016-11-20 FOR AIRPLANES WITH PBE, P/N 119003-11, INSTALLED
NOT APPLICABLE - PART NOT INSTALLEDMOC :
LDG
HRS
MTH
887
1067:42
23-Apr-2018 -MANDATORY N/A
FAA 2017-18-12PARA (H) LRBS
REPLACEMENT RETAINED FROM AD 2016-11-20 FOR AIRPLANES WITH PBE, P/N 119003-11, INSTALLED
NOT APPLICABLE - PART NOT INSTALLEDMOC :
LDG
HRS
MTH
887
1067:42
23-Apr-2018 -MANDATORY N/A
FAA 2017-18-12PARA (I) & (J)
LRBS
INSPECT TO DETERMINE IF THE S/N OF THE INSTALLED PBE, P/N 119003-21, IS WITHIN THE RANGE OF 004-14768M THROUGH 004-21093M OR 004-02393M THROUGH 004-03033M AND IF FOUND WITHIN THE S/N RANGE REPLACE IT.
NOT APPLICABLE - PART NOT INSTALLEDMOC :
LDG
HRS
MTH
887
1067:42
23-Apr-2018 -MANDATORY N/A
FAA 2017-18-12
LRBS
OXYGEN - INSPECTION AND REPLACEMENT OF B/E AEROSPACE PROTECTIVE BREATHING EQUIPMENT (PBE), PART NUMBER 119003-11 AND 119003-21THAT ARE INSTALLED ON AIRPLANES
NOT APPLICABLE - PART NOT INSTALLEDMOC :
Page 49 of 50NOTE: Item Codes in italics show pre-migration CESCOM item codes and position (provided for cross-reference). Remains calculated from PrintDate for calendar items.
0:5419-Mar-2019230AIR COND
1:0419-Mar-201911031406:12ENG 2
1:0419-Mar-201911031406:12ENG 1
1:0419-Mar-201911031406:12AIRCRAFT
Average DailyUtilization
Last ActualDate
Events/LandingsHoursTracking Rate
YR-TRQReg No:
24-Mar-2019 6:11AM
20-Nov-2013
Owner: S.C. TOYO AVIATION S.R.L.
Print Date:
Airworthiness:
Aircraft Serial:
Aircraft Model: 510 - CITATION MUSTANG
Unit:
510-0433
-0433
CESCOM 10 - Aircraft Status Report
(ENG) DUE 2
(ENG) DUE 1
Airworthiness Directives
City Part Serial No
Part Number C/W Time 1
C/W Time 2 + or -
Adj. TBO 1
TBO 2 TSO 2
TSO 1
Remains
RemainsDescription
Drawing # / Task #Position
Item Code
Mod Lvl
MTH 06-Nov-2012 -MANDATORY N/AE1
TCCA CF-2010-03 FUEL OIL HEAT EXCHANGER (FOHE) FUEL FILTER BYPASS VALVE WEAR
NOT APPLICABLE - DUE TO THE PART NUMBER OF THE FUEL OIL HEAT EXCHANGER INSTALLED AT MANUFACTUREMOC :
MTH 17-Oct-2012 -MANDATORY N/AE2
TCCA CF-2010-03 FUEL OIL HEAT EXCHANGER (FOHE) FUEL FILTER BYPASS VALVE WEAR
NOT APPLICABLE - DUE TO THE PART NUMBER OF THE FUEL OIL HEAT EXCHANGER INSTALLED AT MANUFACTUREMOC :
MTH 06-Nov-2012 -MANDATORY N/AE1
FAA 2010-17-06 REPLACEMENT OF FUEL OIL HEAT EXCHANGER (FOHE) FUEL-FILTER BYPASS VALVE
NOT APPLICABLE - DUE TO THE PART NUMBER OF THE FUEL OIL HEAT EXCHANGER INSTALLED AT MANUFACTUREMOC :
MTH 17-Oct-2012 -MANDATORY N/AE2
FAA 2010-17-06 REPLACEMENT OF FUEL OIL HEAT EXCHANGER (FOHE) FUEL-FILTER BYPASS VALVE
NOT APPLICABLE - DUE TO THE PART NUMBER OF THE FUEL OIL HEAT EXCHANGER INSTALLED AT MANUFACTUREMOC :
Page 50 of 50NOTE: Item Codes in italics show pre-migration CESCOM item codes and position (provided for cross-reference). Remains calculated from PrintDate for calendar items.