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AIRFRAME LOGBOOK

~CIRRUS ~AIRCRAFT

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DOOR KEY CODE: 8AA

FUEL CAP KEY CODE:619 CONTENTS

AIRCRAFT DESCRIPTION .................. ....................... ..... .... ....... .... ..................... ............ PAGE 2

ENGINE INSTALLATIONS ............... .... ........................................................... ......... ..... ... PAGE 3

MAJOR ALTERATIONS ................... .. .. .... .................. .......... ................. .. ................ ... PAGES 4-8

LIFE LIMITED PARTS ..... ..... ... ...... ... .... .. .. ............... ... .. ...... ... ................................... PAGES 9-13

AIRWORTHINESS DIRECTIVES I SERVICE BULLETIN COMPLIANCE .............. PAGES 13-18

ALTIMETER AND STATIC CHECKS ...................................................................... PAGES 19-22

RADIO AND ELECTRONIC CHECKS .. ................. .. ... ............................................. PAGES 23-30

MAINTENANCE RECORDS ......................................... .......................................... PAGES 31-50

INSPECTION RECORDS ................. ....... ........................................ ....................... PAGES 51-66

AIRCRAFT DESCRIPTION

MANUFACTURER:

MODEL:

SERIAL NUMBER:

REGISTRATION NUMBER:

DATE OF MANUFACTURE:

EL T HEX CODE:

EXTERIOR PAINT:

PAINT COLOR 1:

PAINT CODE 1:

PAINT COLOR 2:

PAINT CODE 2 :

PAINT COLOR 3:

PAINT CODE 3:

REGISTERED OWNER 1:

STREET ADDRESS :

CITY, STATE, ZIP:

OPERATOR:

STREET ADDRESS:

CITY, STATE, ZIP:

REGISTERED OWNER 2:

STREET ADDRESS:

CITY, STATE, ZIP:

OPERATOR:

STREET ADDRESS:

CITY, STATE, ZIP:

REGISTERED OWNER 3:

STREET ADDRESS:

CITY, STATE, ZIP:

OPERATOR:

STREET ADDRESS:

CITY, STATE, ZIP:

Cirrus Design Corporation

SF 50

0186

N995LC

27 February 2020

2DC75BCC66FFBFF

Gainsboro

8200705

Snow White

CM0850102

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ENGINE INSTALLATION RECORD AIRFRAME

DATE AIRFRAME DATE TOTAL DATE ENGINE MAKE/MODEL SERIAL NUMBER INSTALLED TOTAL HOURS REMOVED HOURS

Engine Log Book Entry

Date: 22 January 2020

AJC Time: 0.0

Installed Williams International FJ33-5A

S/N: 361095

lAW CDC Drawing Number 26005-003

4

MAJOR ALTERATIONS ·~ DATE

AIRFRAME DESCRIPTION OF ALTERATION TOTAL TIME

.•

- ..

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LIFE LIMIT PARTS I OVERHAUL REQUIREMENTS NAME OF PART SERIAL I INSTALLATION I TIME ON PART I LIFE LIMIT OR I REMOVAL AUTHORIZED SIGNATURE

PART NUMBER NUMBER DATE/HOURS AT INSTALL T.B.O DATE/HOURS -AND CI;RTIFICATE NUMBE? = ~ Life Limited Parts SF50-0186

--'J PART NAME PART# SERIAL# EXPIRES

C.A.P.S. Motor 36412-002 0·187 Jan 2030

Assembly

CAP.S. 33016-004 0206 Dec 2029

Parachute

C.A.P.S. Release Mechanism

33706-004 0195 Jan 2030

CAP.S. Ejector 33020-005 0186 Jan 2030

Bag

CA P.S. Rocket 38017-003 N/A Jan 2030 1

Warmer l E.LT. Battery Pack 30539-050 LX1101339820 Sep 2026

' I Life Limited Parts SF50-0186 MCY<::--

,...--PART NAME PART# SERIAL# EXPIRES

BASS PRSOV 30062-006 0379 200 HRS

Engine Fire 80469B1 27320-001 Jan 2029

Protection Bottle 80471B1

Engine Fire 1632YH N/A Nov 2029

Protection Squib 1574YH

Oxygen M.D.S. - D1 911 0036 39457-001 Nov 2025

Single D19110037

Oxygen M.D.S. - D1911 0392 39458-001 Nov 2025

Dual D19110638

Oxygen Bottle 32802-001 1-C 19090449 Sep 2034

Assembly, 22 FP ...-. """ I ~L-

~/1..._.1

PART NAME CYCLE CHARGE/TEST

Engine Fire Protection Bottle 5 Years 11-Jan-2019

Oxygen Bottle 5 Years Jun-2019

I I I I

DATE

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AIRWORTHINESS DIRECTIVE I SERVICE BULLETIN COMPLIANCE RECORD

NEXT AIRFRAME DIRECTIVE/ TYPE OFAD DUE

TOTAL BULLETIN DETAILS OF WORK, ITEMS AFFECTED METHOD OF RECURRING DATE/ HRS AUTHORIZED SIGNATURE TIME NUMBER COMPLIANCE AND COMMENTS OR 1 TIME CYCLE CERTI FICATE NUMBER

Searched ADs through bi-weekly issue '

2020-04. All ADs are complied with at this time.

Date: 27 February 2020

NC Time: 4.0 Verified by 1.M.O

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DATE

ALTIMETER & STATIC SYSTEM CHECKS F.A.R. 91.411

I certify that the altimeter, static system, transponder, and altitude reporter test required by FAR's 91.411 , 91.413, & 91 .217 have-+---+------ been performed and found within the limits of FAR 43 appendices E & F and AC 43-60.

Tested to 35,000 feet on 23-Jan-2020 XPDR 1: MFR: Garmin PN: 29034-001

Model: ....,;G'"'"T"'X,....,3""3""D-- SN: 84813567 XPDR 2: MFR: Garmin PN: 36745-001

Model: GTX 345R SN: 3EH026346 ADC 1: MFR: Garmin PN: 39417-002

Model: GDC 728 SN: 4E5000706 ADC2: MFR: Garmin PN: 39417-001

Model: GDC 72 SN: 458002247 STBY ATT: MFR MidContinent PN: 30499-005

Model: MD-302 SN: K19-10006

CDC Quality Assurance on 25-Feb-2020

Cirrus Design Corporation Duluth, MN USA

DATE TOTAL TIME

RADIO AND ELECTRONIC CHECKS EQUIPMENT CHECKED TYPE OF CHECK RESULTS

SWPS Calibration Parameters

AOA Calibration Offset Value: 0.10 Flaps Warning Push

0% 9.0° 13.r 50% 9.0° 14.r

100% a.r 14.5°

Verifiedb~

MAINTENANCE RECORD F.A.R 43.9

OF WORK PERFORMED AND APPROVED DATA USED

MAKE CIRRUS DESIGN CORP MODEL SF50 SIN: 0186

~ ~I}~.~~"~ Cirrus Design Factory Service Center Repair Station No. YD5R855Y 4961 Airport Road

DATE: 315/2020 AIC TSN: 9 9

Landings: REG. NO: N995LC TACH 9 9 WORK ORDER TYS22444-03-2020 Duluth, MN 55811

Phone: 218-788-3049

Airframe Entries (9) Removed ECS ECU PN 30862-008 Cirrus SN 00277 Manufacturer SN 1-C60305-2 Installed PN 30862-008 Cirrus SN 00275

Date:

Aircraft:

Manufacturer SN 1-C60303-2 lAW Cirru F50 AMM 21 -60

I have revrewed the file on thrs arrcraft and the ac o was repaired/inspected rn accordance with curren detarls of thrs work order are on file at thrs Certrfred

DATE: 3/512020 SIGNED

Glenn ~lelson Certified Repair Station No. YD5R855Y

W ork Order: TYS22444-03-2020

Printed by EBis 3 (datcomedia.com)

MAINTENANCE RECORD

Apri l 27, 2020 Page of Pages Reg. No: N995LC

Cirrus SF50 Serial# 0186 Total Time I Flight Time I Hobbs: 48.9 / 48.9/48.9

The below listed items were accomplished in accordance with the Cirrus SF50 Aircraft Maintenance Manual and other approved or acceptable data as applicable.

Work Order 062005651 [2700] Removed left pitot tube p/n PH502, s/n N/A and installed new pitot tube p/n PH502, s/n N/A

'sted items have been complet d, and with regard to the above items, that this aircraft has been approved

f------ _1-

MAKE: CIRRUS DESIGN CORP MODEL: SF50

-~ ~' lo~ ~ ~c~ Cirrus Design Factory Service Center DATE. 812712020 AIC TSN: 150 4

Landings: SIN: 0186 REG. NO: N995LC WORK ORDER TYS23263-08-2020

Airframe Entries

Repair Station No. YD5R855Y 4961 Airport Road Duluth. MN 55811 Phone 218-788-3049

(9) Performed Jet Stream Maintenance Vision Check 1100 Hour

TACH: 150.4

(1 0) Checked FADEC system for any outstanding faults or exceedances and downloaded FADEC data via EMT software lAW W illiams International LMM 73-26-01 . Data has been sent to [email protected]. (11) Complied with CMC Download lAW Cirrus Aircraft work instructions. (12) Lubricated flight control hinges lAW SF50AMM 12-20. (15) Adjusted Baggage Door Latch. lAW AMM 52-30 . (1 6) Recharged Air conditioning system lAW Cirrus SFSO AMM 12-10 (1 7) Sealed all quarter-turn receptacles for Engine Cowling in Baggage area lAW AMM 20-10. (18) Cleaned VOR/LOC Antenna Connectors lAW Cirrus SF 50 AMM 34-50 and Standard Practices of the WMM.

I have rev1ewed the file on thts a1rcraft and the acco

DATE: 812712020 W ork Order: TYS23263-08-2020



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DATE OF COMPLETION

AIRCRAFT TIME IN

SERVICE DETAILS OF WORK PERFORMED AND APPROVED DATA USED AUTHORIZED SIGNATURE AND

CERTIFICATE NUMBER

2601 Cessna Lane NW Kennesaw, GA 30144 DK7R795J LOG 10# 22215 09-September-2020 WO# 20493-9 N995LC S/N 0186 CIRRUS SF50 HOBBS 191.7 TACH 159.4

** * AIRFRAME LOG ENTRY ***

**** ITEM# 20493-1 FUEL VALVE #1 FAIL CAS MESSAGE ~*** DISCREPANCY: FUEL VALVE #1 FAIL

Pg 1/1

ACTION: REMOVED FUEL CONTROL VALVE SN 0487 INSTALLED NEW #1 FUEL CONTROL VALVE OJERHAULED BY RAM MANUFACTURING COMPANY WO #181109 DATED 14 MAY 2020 IAW SF560 GROUND RUN FUEL TEST.

PN 26327-009S SN 0263 MM 28-20. PERFORMED

**** ITEM # 20493-2 LEAK CHECK I OPS CHECK DISCREPANCY: LEAK CHECK I OPS CHECK

****

ACTION: LEAK AND OPERATIONAL CHECK GOOD •

MAINTENANCE RELEASE. THIS AIRCRAFT, AIRFRAME, AIRCRAFT ENGINE, OR APPLIANCE IDENTIFIED ABOVE WAS REPAIRED AND INSPECTED IN ACCORDANCE WITH CURRENT REGULATION OF THE FEDERAL AVIATION ADMINISTRATION AND IS APPROVED TO RETURN TO SERVICE. PERTINENT DETAILS OF THE REPAIR ARE ON FILE AT T HIS REPAIR STATION UNDER W0#20493

DATED ~ER 2020.

Signe~95J FOR DLK AVIATION

MAKE CIRR US DESIGN CORP MODEL SF50 SIN 0136 REG NO. N995LC WORK ORDER TKI0633-1 0-2020

Airframe Entries

'Cc,. ~t,R~~~ Cirrus Design Fat~tory Service Center 4961 A1rport Road Duluth MN 55811 Phone 218-788-3049

DATE 1 012012020 AIC TSN 192 2

Land1ngs HOBBS 230 5

(10) Removed and installed new LH Pitch Trim actuator. Rennoved actuator PN : 31235-005 SN: 152. Installed New actuator PN : 31235-005 SN: 239. Inspection and operational check good . All work accomplished lAW SF50 AMM 27·30.

1 have rev1ewed the file on th 1s a1rcraft and the accompan ying d1screpancy forms The a1rcratt. a1rframe a1rcraft eng1ne. propeller or appliance 1dent1f1 ed was repa1red/:nspected 1n 3ccordance w1th current requ irements of tne Federal .'\v1at1on Adm1n1strat10n and IS approved for return to serv1ce Pemnent deta ils of th1s .vork order e~re on file at th1s Cert1f ied Repa1r Stat1on C:R~ ; YDC. 855Y

DATE: 1 0120/2020 SIGNED: /--

Work Order: TKI0633-1 0-2020

Jeffrey Bndges Printed bv£8Js__::Vdmcnmedia com)

MAKE: CIRRUS DESIGN CORP MODEL SF50

~ CIRRUS Cirrus Design Factory Service Center DATE 1111312020 'R '> " p (' p " ~ T A/C TSN: 210.5

SIN: 0186 Land ings: REG NO N995LC

Repair Station No. YD5R855Y 4961 Atrport Road FLIGHTIIME 2105

WORK ORDER TYS23671-11 -2020 Duluth, MN 55811 Phone 218-788-3049

Airframe Entries (5) Performed Jet Stream Maintenance Vision Check II 200 Hour (6) Checked FADEC system for any outstanding faults or exceedances and downloaded FADEC data via EMT software lAW Williams International LMM 73-26-01 . Data has been sent to [email protected]_ (11) Swapped GIA#1 P/N 011-03711-00 S/N 4SK008924 with GIA#2 P/N 011-03711-00 S/N 4SK0089431AW Garmin Line Maintenance Manual and Cirrus SF50 AMM 31-40. (12) Installed new thumb wheel checklist switch assembly P/N 39591-002 lAW Cirrus SF50 AMM 31-60. (13) Completed Safe Return Autoland Enabling lAW SB5X-90-10R1. (14) Downloaded _C4 Software lAW Garmin LMM. Ops Check Good. (17) Complied with CMC Download lAW Cirrus Aircraft work instructions. (18) Lubricated flight control hinges lAW SF50AMM 12-20. (1 9) Completed visual inspection of engine compartment for defects, leaks and airworthy condition lAW SF50 AMM 5-20. (20) Completed visual inspection of landing gear, wheels and brakes for defects and airworthy condition lAW SF50 AMM 32-42 , 12-20 & 5-20. (21) Performed Inspection/Check on Battery 1 and Battery 21AW SFSOAMM 24-30. (22) Performed Functional Check on IPS PRSOV lAW SF50 AMM 30-20. (23) Performed Functional Check on BASS PRSOV lAW SF50 AMM 36-10.

I have reviewed the file on this atrcraft and the accompany! g discrepancy forms. The aircraft, airframe, aircraft engine, propeller or appliance identified was repaired/inspected in accordance with current requir ents of the Federal Aviation Administratio nd"is-approved for retu rn to service. Pertinent detarls of this work order are on file at this Certified Rep Station CRS YD5R855Y.

DATE: 11 /13/2020 SIGNED: Work Order: TYS23671-11-2020

Philip Fellman Printed by EBis 3 (datcomedia.com) Certilied Repair Station No. YD5R855Y


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MAKE: CIRRUS DESIGN CORP MODEL SF50

R ~ lo~ ~ ~c~ Cirrus Design Factory Service Center Repan Station No YD5R855Y 4961 .<ltrport !load

D.A. TE. 12/4/2020 A/C TSN 221 1

Landmgs.

rHORIZED SIGNATURE AND CERTIFICATE NUMBER

SIN 0186 FUGHTIIME 221 1

Duluth MN 558 11 ?hone 218-788-3049

REG NO N995LC WORK ORDER TYS23812-12-2020

Airframe Entries (9) Removed and replaced sceet dueling from FCVoutlet to muffle~ PiN: 50730-150 lAW Cirrus SF50AMM 21 -40. Installed new bass valve PN 30062-006 SN:0496 lAW Cirrus SF 50 AMM 36-10. OPS CHECK GOOD (1 0) Complied with CMC Download lAW Cirrus Aircraft work mstruct1ons. (12) Adjusted exterior door handle lAW C1rrus SF 50 AMM 52-20

d re anc forrns The a1rcraft airframe a1rcraft eng1ne. propeller or appliance 1dent1fied I have reviewed the fi le on thiS atrcraft and the accompanymg ~sc f ~e F~deral Aviation Adm,lnJStratlon. and IS approved for return to service. Pertinent w as repa1red/inspected m accordance w1th current requ1rem en s o • · detailS of this work order are on file at thiS Certified Repalf Station CRS YD5R855Y

./A' ___..-- Work Order: TYS2381 2-12-2020 DATE: 1214/2020 SIGNED.:_~-------------~~=::::::.~:_=-:=-~~---:-

Ph111p Fellman Printed by EBis 3 (datcomedia.com) Certified Repatr Stat1on No YD5R855Y

2601 Cessna Lane NW Kennesaw, GA 30144 DK7R795J LOG ID# 22570 15-December-2020 WO# 20671-0 N995LC SIN 0186 CIRRUS SF50 Pg 111

*** AI RFRAME LOG ENTRY ***

DISCREPANCY: IPS INLET OVERHEAT ACTION: REMOVED PRSOV IPS VALVE P/N 30064-004 S/N 0084. INSTALLED NEW PRSOVE IPS VALVE P/N 30064- 004 S/ N 1323 IAW CIRRUS 30- 20. FUNCTIONAL, LEAK, AND OPERATIONAL TESTS OK.

MAINTENANCE RELEASE. . THIS AIRCRAFT, AIRFRAME, AIRCRAFT ENGINE, OR APPLIANCE IDENTIFIED ABOVE WAS REPAIRED AND INSPECTED I N ACCORDANCE WIT ~RRENT REGULATION OF THE FEDERAL AVIATION ADMINISTRATION AND IS APPROVED TO RETURN TO SERV . PERTINENT DETAILS OF THE REPAIR ARE ON FILE AT THIS REPAIR STATION UNDER W0#20671 DATED 15 DECE ER 2 0 .

FOR DLK AVIATION

2601 Cessna Lane NW Kennesaw, GA 30144 DK7R795J LOG ID# 22609 21-January-2021 WO# 20649-0 N995LC SIN 0186 CIRRUS SF50 HOBBS 273.4 TACH 226.2

Pg 111

*** AIRFRAME LOG ENTRY ***

DI SCREPANCY: R/R FS510 DATA CARD ACTI ON: REPLACED GARMIN FLIGHTSTREAM 510 WIFI DATA CARD P/N 011-03595- 05 IN ACCORDANCE WI TH · CIRRUS SF50 GARMIN PERSPECTIVE+ LMM 190-02093-03 REVI SION l. ALL OPERATIONS ARE SATISFACTORY AT THIS TIME.

MAINTENANCE RELEASE. THIS AI RCRAFT , AIRFRAME, AIRCRAFT ENGINE, OR APPLIANCE I DENTI FI ED ABOVE WAS REPAIRED AND I NSPECTED I N ACCORDANC WITH CURRENT REGULATION OF THE FEDERAL AVIATION ADMINISTRATION AND IS APPROVED TO RETURN TO S ICE. PERTINENT DETAILS OF THE REPAIR ARE ON FILE AT THIS REPAIR STATION UNDER W0#20649 DATED. 21 J ARY ::1~

DLK AVIATION

AIRCRAFT DATE OF TIME IN

COMPLETION SERVICE

''D

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MAKE: CIRRUS DESIGN CORP iiJ. ~. ~o~ ~ ~<~ Cirrus Design Factory Service Center MODEL: SF50 SIN: 0186 Repair Station No YD5R855Y REG. NO: N995LC 4961 Airport Road WORK ORDER: TYS241 01-02-2021 Duluth, MN 55811

Phone 218-788-3049

Airframe Entries

DATE: 2/1612021 AIC TSN: 270.9

Landings FLIGHTIIME 270.9

(6) Performed an annual inspection of this aircraft in accordance with the Cirrus Aircraft SF-50 AMM Chapter 05-20 inspection checklist . (7) Performed Jet Stream Maintenance Vision Check II. (8) Performed Jet Stream Maintenance Vision Check Ill. (1 0) Completed Operational test of the BASS Pressure Regulating Shut-Off Valve (PRSOV) lAW SF 50 AMM 36-10. Operational Checked Satisfactory. (13) Performed research of the aircraft logbooks for applicable Airworthiness Directives through bi-weekly 2021-03. (14) Performed research of the aircraft records for any mandatory service bulletins that are due. No MSBs are due at this time. (19) Inspected Fire Extinguisher, H3R Model A344, Manufacture date 2019, gauge pressure is in the operable (green) range (20) Complied with inspection of the ELT in accordance with 91 .207(d). Battery due date : 09/2026. (22) continued (23) continued. (24) continued. (25) continued. (26) Secured bolster switch panel overlay placard lAW SF50 AMM 11-30. (27) Installed correct fi les onto supplemental database card and flightstream card lAW garmin perspective touch plus pilot's guide. (28) Replaced U H And R/H brake pads PN# 3451 3-304 lAW SF50AMM 32-42. (29) Installed new LH main tire PIN 27664-003 lAW SF50 AMM 32-41 and Beringer MM-ETS0-004. (30) Installed new RH main tire P/N 27664-003 lAW SF50 AMM 32-41 and Beringer MM-ETS0-004. (31 ) Removed rocket warmer assy P/N 3801 7-003 Installed new rocket warmer assy PIN 38017-003. lAW SF50 CMM 90-00. (32) Serviced Oxygen system lAW SF50AMM 12-10. (33) Replaced RH main Gear courtesy Light PN# 35403-002 and repaired ground strap lAW SF50 WM 20-00. (34) Installed new Relief disk indicator P/N 171-10 lAW Cirrus SF50 AMM 35-00. (35) Resealed Wing access panel W 2R lAW SF50 AMM 57-30 . (36) Complied with SB5X-27-07 RH Side Stick Inspection.

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(37) Completed Sealing of Pitch Trim Pushrods lAW SB5X-27-08R1 (38) Complied with SB5X-35-02 Passenger Oxygen System Inspection. (39) Verified SB5X-36-02 PRSOV Adhered Nutplate Backing Plate Sealing has been previously complied with. (40) Complied with SB5X-53-13R1 W ing Attach Bulkhead Core Seal . (41 ) Completed SB5X-57-08 Wing Skin Bond inspection and repair (42) Not due. Customer has been provided with a duplicate log entry for replacement on 12-4-21 at 221 .1 (43) Repaired #5 pitch and roll push rods lAW with FRA00016181 (44) Adjusted Yaw Servo Bridal Cable Tension lAW SF50 Amm 22-10. ( 45) Connected oil chip detectors lAW Cirrus SFSO AMM 71-50. (46) Performed 200 hour Fire Bottle inspection/check lAW SF-50 AMM chapter 26-20. (47) Performed 200 hour Fuel Control Switch Dormant Failure Inspection lAW SF-50AMM chapter 28-20. (48) Performed 200 hour Primary FCV Check Valve Dormant Failure Inspection lAW SF-50 AMM chapter 28-20. (49) Performed 200 hour Fuel Shutoff Valve Dormant Failure Inspection lAW SF-50AMM chapter 28-20. (50) Performed 200 hour Special Inspection/Check-Battery 2 Charging lAW SF-50 AMM chapter 24-30. (51) Performed 200 hour Special Inspection/Check-Battery 1 Charging lAW SF-50 AMM chapter 24-30. (52) Performed 200 hour passenger oxygen mask dormant failure inspection lAW Cirrus SF-50 AMM 35-20. (53) Performed 200 hour Crew Oxygen Mask dormant failure inspection lAW Cirrus SF-50 AMM 35-10. (54) Performed 200 hour Alternate gear extension system dormant failure inspection lAW Cirrus SF-50 AMM chapter 32-30. (55) Performed 200 hour Engine Inlet Pressure Regulating Shut off Valve (PRSOV) lAW SF50 AMM 30-20. (56) Performed 200 hour windshield/radome sprayer function test lAW SF50 AMM 30-40. (59) I certify that this aircraft has been inspected in accordance with an annual inspection and was determined to be in an airworthy condition.

I have revtewed the file on this atrcraft and the accompanymg discrepancy forms The a1rcraft, atrframe , atrcraft eng me propelle r or appl1ance ;de nttfied was repatred/inspected in accordance w 1th current requirements of the Federal Avtat1on Administration a nd IS approved for return to servtce Pertinent details of thls work order are on file at this Cert1f1ed Repa1r Station CRS YD5R855Y A, DATE 2/16/2021 SIGNED: ·-'/~ ~ h/ ~/ -=- W ork Order: TYS24101-02-2021

Hayden Settl: 4!n' V c'L/ Certified Repa St 10n No. YD5R855Y


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INSPECTION RECORD F.A.R43.11-91.409

AIRCRAFT . DATE OF TIME IN AUTHORIZED SIGNATURE

INSPECTION SERVICE DETAILS OF IN~~ IIUN STATUS. RESULTS AND RETURN TO SERVICE NOTES CI::K IIFICATE NUMBER

~~- ~ l . ')~.l() 4·D Production Flight Test accomplished in accordance with Cirrus Procedure #90506

Name: Mark Matthys Date :Z,.\ hb W Z...O

s;gnaMe' ~~ Title' Pmd"ct;on FlightTest P:

~7-feb·lo'Jo ~.o (find that the aircraft meets the requirements for the ""\

certification requested and have issued an U.S. Standard Airworthiness Certificate dated _fl_; feb IJ.Qia_. The next inspection is due 2.l__j !fJJM~._I ~.

.1~£ ttJ,h '

Troy E. Nickila ODA(AIR)-834662-CE

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~ CIRRUS ~AIRCRAFT

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