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ATR42-500
S.NO SHEET # DATE ISSUE #1 LEP 1 22/04/2010 012 A SHEET 1 22/04/2010 013 A SHEET 2 28/03/2007 INITIAL4 B SHEET 1 22/04/2010 015 B SHEET 2 28/03/2007 INITIAL6 B SHEET 3 28/03/2007 INITIAL7 C SHEET 1 28/03/2007 INITIAL8 C SHEET 2 22/04/2010 019 C SHEET 3 28/03/2007 INITIAL10 C SHEET 4 28/03/2007 INITIAL11 C SHEET 4A 28/03/2007 INITIAL12 C SHEET 4B 28/03/2007 INITIAL13 C SHEET 4C 28/03/2007 INITIAL14 C SHEET 4D 28/03/2007 INITIAL15 C SHEET 4E 28/03/2007 INITIAL16 C SHEET 5 28/03/2007 INITIAL17 C SHEET 6 22/04/2010 0118 C SHEET 7 28/03/2007 INITIAL19 C SHEET 8 28/03/2007 INITIAL20 C SHEET 9 28/03/2007 INITIAL21 C SHEET 10 28/03/2007 INITIAL
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ALL (FUEL DENSITY 0.78 Kg / litre)ALL (FUEL DENSITY 0.79 Kg / litre)
ALL (FUEL DENSITY 0.81 Kg / litre)ALL (FUEL DENSITY 0.82 Kg / litre)
ALL (FUEL DENSITY 0.80 Kg / litre)
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LIST OF EFFECTIVE PAGES ISSUE # 02
EFFECTIVITY
ALL (FUEL DENSITY 0.77 Kg / litre)
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EDP EXCHANGE FOR SEMI PERMANENT DATAFOR CHECK IN AND LOAD CONTROL
22 C SHEET 11 22/04/2010 0123 C SHEET 12 22/04/2010 0124 C SHEET 13 22/04/2010 0125 C SHEET 14 22/04/2010 0126 C SHEET 15 28/03/2007 INITIAL27 D SHEET 1 28/03/2007 INITIAL28 D SHEET 2 28/03/2007 INITIAL29 D SHEET 3 28/03/2007 INITIAL
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ALLALL
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LEP 1 Date: 03/07/2018
EDP EXCHANGE FOR SEMI PERMANENT DATA FOR CHECK IN AND LOAD CONTROL
Completed by Operations Engineer MUHAMMAD FARHAN KHAN Issue No: 01
Date: 22/04/2010
OPERATIONS ENGINEERING, TECHNICAL DIVISION, FLIGHT OPERATIONS
EDP-SYSTEM SEMI-PERMANENT DATA
COMMUNICATION ADDRESSES
A SHEET 1
CARRIER PK
1. HANDLING AGENT’S CONTACT ADDRESS Completed sheets and changes of basic data and procedure must be forwarded to:
MAILING ADDRESS:
TELETYPE ADDRESS:
EMAIL ADDRESS:
REMARKS: 2. CARRIER’S CONTACT ADDRESS
MAILING ADDRESS: OPERATIONS ENGINEERING TECHNICAL DIVISION FLIGHT OPERATIONS DEPARTMENT PIA HEAD OFFICE, JINNAH INTERNATIONAL AIRPORT KARACHI, 75200, PAKISTAN. TELETYPE ADDRESS: KHIOLPK KHIOXPK EMAIL ADDRESS: [email protected] REMARKS:
EDP EXCHANGE FOR SEMI PERMANENT DATA FOR CHECK IN AND LOAD CONTROL
Completed by Operations Engineer AMIR MUKHTAR Issue No: INITIAL
Date: 28/03/2007
OPERATIONS ENGINEERING, TECHNICAL DIVISION, FLIGHT OPERATIONS
EDP-SYSTEM SEMI-PERMANENT DATA
COMMUNICATION ADDRESSES
A SHEET 2
CARRIER PK
3. AUTOMATICALLY PRODUCED DOCUMENTS
(Tick as required) NOTAC SEATPLAN LOADPLAN PASSENGER INFO LIST LOAD SHEET LOADING INSTRUCTION/REPORT
4. MESSAGE REQUIREMENTS
(Tick as required)
LPM Load Planning Message AHM 580 LDM Load Message AHM 583 ALI Abbreviated Load Information Message AHM 584 CPM Container/Pallet Distribution Message AHM 587 UCM ULD Control Message AHM 388(Dispatch Only) MVT Movement Messages AHM 011 and 780 DIV Diversion Message AHM 781 SOM Seat Occupied Message RP 1712 PTM Passenger Transfer Message RP1718 PSM Passenger Service Message RP 1715 (Despatch Only) TPM Teletype Passenger Manifest RP 1717 (Despatch only) PFS Passenger Final Sales Message RP 1719 (Despatch) IDM Industry Discount Message RP 1714 RQL Request List Message RP 1709 (despatch) PNL/ADL Passenger Name List, and Additions and Deletions List (RP 1708) (acceptance Only) SAL Seats Available List RP 1713(Acceptance Only) SLS Statistical Load Summary AHM 588 RQM Request Information Message AHM 783 UWS ULD/Bulk Load Weight signal AHM 581 (Acceptance Only)
5. MESSAGE ADDRESSES
Attach a complete address list for all messages mentioned under paragraph 4 above
EDP EXCHANGE FOR SEMI PERMANENT DATA FOR CHECK IN AND LOAD CONTROL
Completed by Operations Engineer MUHAMMAD FARHAN KHA
OPERATIONS ENGINEERING, TECHNICAL DIVISION, FLIGH
EDP-SYSTEM SEMI-PERMANENT DATA
GENERAL INFORMATION
B SHEET 1
CARRIER PK
1. PASSENGER AND BAGGAGE WEIGHTS 1.1 Passenger weights
Adult male 75 KG Adult female 75 KG Child 38 KG Infant 15 KG
Remarks: 1.2 Cabin Baggage Weight
YES NO Cabin weight is included in the above mentioned passenger weights. If NO; Actual cabin baggage weight must be used. Remarks:
1.3 Checked Baggage Weight
Weight per piece ACTUAL Weight per passenger ACTUAL
Enter “actual” if standard weight not permitted. Remarks:
b
N Issue No.: 01 Date: 22/04/2010
T OPERATIONS
EDP EXCHANGE FOR SEMI PERMANENT DATA FOR CHECK IN AND LOAD CONTROL
Completed by Operations Engineer AMIR MUKHTAR
OPERATIONS ENGINEERING, TECHNICAL DIVISION, FLIGHT OPERAT
EDP-SYSTEM SEMI-PERMANENT DATA
AIRCRAFT DATA B SHEET 2
CARRIER PK
ALL WEIGHTS IN KILOGRAMS (KG)
2. CREW AND CREW BAGGAGE WEIGHTS 2.1 Crew Weights
Cockpit crew 81 Cabin crew 75
YES NO Crew baggage is included in the above crew weights:
If NO: Crew baggage weight must be specified in 2.2 Remarks: 2.2 Crew Baggage Weights
For check purposes add list of valid weights and indices.
COCKPIT CABIN SHORTHAUL 30 20 LONGHAUL 30 20 OTHER’S *
* Specify conditions as appropriate Remarks: For International flights include crew baggage.
b
Issue No: INITIAL Date: 28/03/2007
IONS
EDP EXCHANGE FOR SEMI PERMANENT DATA FOR CHECK IN AND LOAD CONTROL
Completed by Operations Engineer AMIR MUKHTAR Issue No: INITIAL Date: 28/03/2007 OPERATIONS ENGINEERING, TECHNICAL DIVISION, FLIGHT OPERATIONS
EDP-SYSTEM SEMI-PERMANENT DATA
GENERAL INFORMATION
B SHEET 3
CARRIER PK
3. DRY OPERATING WEIGHT AND DRY OPERATING INDEX SPECIFICATIONS
(Tick as appropriate)
DOW DOI
Item Incl Excl Incl Excl Remarks
Basic Weight (EMPTY WEIGHT) b
b
Crew Weight b b
Crew Baggage b b
Pantry b b
Containers
Pallets
CONFIG Weight b b
FLIGHT PACK b b
REMARKS:-
EDP EXCHANGE FOR SEMI PERMANENT DATA FOR CHECK IN AND LOAD CONTROL
Completed by Operations Engineer AMIR MUKHTAR Issue No: INITIAL
Date: 28/03/2007
OPERATIONS ENGINEERING, TECHNICAL DIVISION, FLIGHT OPERATIONS
EDP-SYSTEM SEMI-PERMANENT DATA
AIRCRAFT DATA C SHEET 1
A/C TYPE ATR42-500
CARRIER PK
1. BALANCE AND SPECIAL INFORMATION - OUTPUT ON LOADSHEET
1.1 Balance output
Please mark your requirements in respective box. Remarks Basic index BI
b
Dry operating index DOI b
Dead load index DLI Dead load MAC MACDLW Loaded Index at zero fuel weight LIZFW
b
Loaded index at take-off weight LITOW b
Loaded Index at landing weight LILAW MAC – at zero fuel weight MACZFW b MAC - at takeoff weight MACTOW
b
MAC at landing weight MACLAW Stabilizer trim setting at take-off STABTO *
* specify ANU or AND as appropriate. THE FOLLOWING EQUATION IS USED Y = -0.315789 X + 9.2368 Y = STAB TRIM X = C.G IN % MAC
1.2 Passenger trim output
Please mark your requirements in respective box. Remarks Class Trim Cabin Area Trim
b
Seat Row Trim
EDP EXCHANGE FOR SEMI PERMANENT DATA FOR CHECK IN AND LOAD CONTROL
Completed by Operations Engineer MUHAMMAD FARHAN KHAN Issue No: 01
Date: 22/04/2010
OPERATIONS ENGINEERING, TECHNICAL DIVISION, FLIGHT OPERATIONS
EDP-SYSTEM SEMI-PERMANENT DATA
AIRCRAFT DATA C SHEET 2
A/C TYPE ATR42-500
CARRIER PK
ALL WEIGHTS IN KILOGRAMS (KG)
1.3 Seating Conditions
State below how the seating conditions are to be shown on the load sheet in the respective box (give example).
1.4 Special Information Specify the information to be entered in the lower parts of the EDP Load sheet.
1.4.1 Captain’s information/notes, Centre of Gravity limits, ramp weight, etc. (give examples). 1.4.2 Load message before LMC, if required, to be shown.
2. AIRCRAFT REGISTRATIONS, WEIGHT AND INDEX DETAILS
DRY OPERATING WEIGHT BASIC WEIGHT √ (tick as appropriate) For check purpose add list of valid weights and indices.
Standard Fleet Weight: 10824 Standard Fleet Index: 75.0
Registration
Weight Adjustment
Index Adjustment
Registration
Weight Adjustment
Index Adjustment
AP-BHH
00
00
AP-BHN
-34
+0.1
AP-BHI
-20
+1.1
AP-BHO
-22
+1.2
AP-BHJ
-61
+0.4
AP-BHP
-31
-0.1
AP-BHM
-26
-0.8
NOTE: Notification for data changes at short notice may also be made by means of data exchange message (AHM 052). PK does not take Fleet Average Basic Weight; Weight must be taken Tail Wise.
EDP EXCHANGE FOR SEMI PERMANENT DATA FOR CHECK IN AND LOAD CONTROL
Completed by Operations Engineer ALI RAZA Issue No: 02
Date: 03/07/2018
OPERATIONS ENGINEERING, TECHNICAL DIVISION, FLIGHT OPERATIONS
EDP-SYSTEM SEMI-PERMANENT DATA
AIRCRAFT DATA C SHEET 3
A/C TYPE
ATR42-500 CARRIER
PK
3. BASIC INDEX AND MAC FORMULA 3.1 Examples and definitions
Index = W * (Sta - Ref. Sta) + K C
C*(I – K) + Ref.Sta - LEMAC W %MAC = MAC 100 W = Weight Actual Sta. = Station, horizontal distance in inches or metres from station zero to the location Ref. Sta. = Reference station/axis. Selected station around which all index values are calculated K = Constant used as a plus value to avoid negative index figures. C = Constant used as a denominator to convert moment values into index values. I = Index value corresponding to respective weight. MAC = Length of Mean Aerodynamic Chord in inches or meters. LEMAC = Horizontal distance in inches or meters from the station zero to location of the Leading Edge of MAC.
3.2 Index formula Ref. Sta at = 11.996 Meters from zero K (constant) = 50 C (constant) = 100
3.3 MAC Information
Length of MAC = 2.285 Meters LEMAC at = 11.425 Meters from zero
3.4 Stabilizer trim setting
MAC Range Min 15% Max 34% STAB Range Min + 4.5 Max - 1.5 Stabilizer change item per 1% MAC ------------------------------ Y = - 0.315789 X + 9.2368 (attach a table or diagram if item changing at different weights) Y = STAB TRIM , X = C. G in % MAC
EDP EXCHANGE FOR SEMI PERMANENT DATA FOR CHECK IN AND LOAD CONTRO
Completed by Operations Engineer AMIR MUKHTAR Issue No: INITIAL
Date: 28/03/2007
OPERATIONS ENGINEERING, TECHNICAL DIVISION, FLIGHT OPERATIONS
EDP-SYSTEM SEMI-PERMANENT DATA
AIRCRAFT DATA C SHEET 4
A/C TYPE ATR42-500
CARRIER PK
4. EFFECT OF FUEL/INJECTION WATER
Fuel loading Fuel Usage Standard Procedure Non-standard Procedure FUEL DENSITY: 0.77 kg/litre
Index value
Index value Fuel Weight
+/-
100
10
1
Fuel Weight
+/-
100
10
1
1 5 4 0 0 4 6 2 + 0 1 7 7 0 + 0 2
1 2 3 2 + 0 3 1 5 4 0 + 0 4 2 0 0 2 + 0 5 2 3 1 0 + 0 6
2 6 1 8 + 0 7 3 0 8 0 + 0 8 3 3 8 8 + 0 9 3 8 5 0 + 1 0
4 4 1 4 + 1 1
Note 1: Use additional sheets for other fuel densities or state correction factors. Note 2: Specify maximum capacities.
EDP EXCHANGE FOR SEMI PERMANENT DATA FOR CHECK IN AND LOAD CONTRO
Completed by Operations Engineer AMIR MUKHTAR Issue No: INITIAL
Date: 28/03/2007
OPERATIONS ENGINEERING, TECHNICAL DIVISION, FLIGHT OPERATIONS
EDP-SYSTEM SEMI-PERMANENT DATA
AIRCRAFT DATA C SHEET 4A
A/C TYPE ATR42-500
CARRIER PK
4. EFFECT OF FUEL/INJECTION WATER
Fuel loading Fuel Usage Standard Procedure Non-standard Procedure FUEL DENSITY: 0.78 kg/litre
Index value
Index value Fuel Weight
+/-
100
10
1
Fuel Weight
+/-
100
10
1
1 5 6 0 0 4 6 8 + 0 1 7 8 0 + 0 2
1 2 4 8 + 0 3 1 5 6 0 + 0 4 1 8 7 2 + 0 5 2 3 4 0 + 0 6
2 6 5 2 + 0 7 3 1 2 0 + 0 8 3 4 3 2 + 0 9 3 9 0 0 + 1 0
4 4 7 1 + 1 1
Note 1: Use additional sheets for other fuel densities or state correction factors. Note 2: Specify maximum capacities.
EDP EXCHANGE FOR SEMI PERMANENT DATA FOR CHECK IN AND LOAD CONTRO
Completed by Operations Engineer AMIR MUKHTAR Issue No: INITIAL
Date: 28/03/2007
OPERATIONS ENGINEERING, TECHNICAL DIVISION, FLIGHT OPERATIONS
EDP-SYSTEM SEMI-PERMANENT DATA
AIRCRAFT DATA C SHEET 4B
A/C TYPE ATR42-500
CARRIER PK
4. EFFECT OF FUEL/INJECTION WATER
Fuel loading Fuel Usage Standard Procedure Non-standard Procedure FUEL DENSITY: 0.79 kg/litre
Index value
Index value Fuel Weight
+/-
100
10
1
Fuel Weight
+/-
100
10
1
1 5 8 0 0 4 7 4 + 0 1 7 9 0 + 0 2
1 1 0 6 + 0 3 1 5 8 0 + 0 4 1 8 9 6 + 0 5 2 3 7 0 + 0 6
2 6 8 6 + 0 7 3 0 0 2 + 0 8 3 4 7 6 + 0 9 3 7 9 2 + 1 0
4 5 2 8 + 1 1
Note 1: Use additional sheets for other fuel densities or state correction factors. Note 2: Specify maximum capacities.
EDP EXCHANGE FOR SEMI PERMANENT DATA FOR CHECK IN AND LOAD CONTRO
Completed by Operations Engineer AMIR MUKHTAR Issue No: INITIAL
Date: 28/03/2007
OPERATIONS ENGINEERING, TECHNICAL DIVISION, FLIGHT OPERATIONS
EDP-SYSTEM SEMI-PERMANENT DATA
AIRCRAFT DATA C SHEET 4C
A/C TYPE ATR42-500
CARRIER PK
4. EFFECT OF FUEL/INJECTION WATER
Fuel loading Fuel Usage Standard Procedure Non-standard Procedure FUEL DENSITY: 0.80 kg/litre
Index value
Index value Fuel Weight
+/-
100
10
1
Fuel Weight
+/-
100
10
1
1 6 0 0 0 4 8 0 + 0 1 8 0 0 + 0 2
1 1 2 0 + 0 3 1 6 0 0 + 0 4 1 9 2 0 + 0 5 2 2 4 0 + 0 6
2 7 2 0 + 0 7 3 0 4 0 + 0 8 3 3 6 0 + 0 9 3 8 4 0 + 1 0
4 4 8 0 + 1 1 4 5 8 6 + 1 2
Note 1: Use additional sheets for other fuel densities or state correction factors. Note 2: Specify maximum capacities.
EDP EXCHANGE FOR SEMI PERMANENT DATA FOR CHECK IN AND LOAD CONTRO
Completed by Operations Engineer AMIR MUKHTAR Issue No: INITIAL
Date: 28/03/2007
OPERATIONS ENGINEERING, TECHNICAL DIVISION, FLIGHT OPERATIONS
EDP-SYSTEM SEMI-PERMANENT DATA
AIRCRAFT DATA C SHEET 4D
A/C TYPE ATR42-500
CARRIER PK
4. EFFECT OF FUEL/INJECTION WATER
Fuel loading Fuel Usage Standard Procedure Non-standard Procedure FUEL DENSITY: 0.81 kg/litre
Index value
Index value Fuel Weight
+/-
100
10
1
Fuel Weight
+/-
100
10
1
1 6 2 0 0 4 8 6 + 0 1 8 1 0 + 0 2
1 1 3 4 + 0 3 1 6 2 0 + 0 4 1 9 4 4 + 0 5 2 2 6 8 + 0 6
2 5 9 2 + 0 7 3 0 7 8 + 0 8 3 4 0 2 + 0 9 3 8 8 8 + 1 0
4 3 7 4 + 1 1 4 6 4 3 + 1 2
Note 1: Use additional sheets for other fuel densities or state correction factors. Note 2: Specify maximum capacities.
EDP EXCHANGE FOR SEMI PERMANENT DATA FOR CHECK IN AND LOAD CONTRO
Completed by Operations Engineer AMIR MUKHTAR Issue No: INITIAL
Date: 28/03/2007
OPERATIONS ENGINEERING, TECHNICAL DIVISION, FLIGHT OPERATIONS
EDP-SYSTEM SEMI-PERMANENT DATA
AIRCRAFT DATA C SHEET 4E
A/C TYPE ATR42-500
CARRIER PK
4. EFFECT OF FUEL/INJECTION WATER
Fuel loading Fuel Usage Standard Procedure Non-standard Procedure FUEL DENSITY: 0.82 kg/litre
Index value
Index value Fuel Weight
+/-
100
10
1
Fuel Weight
+/-
100
10
1
1 6 4 0 0 3 2 8 + 0 1 8 2 0 + 0 2
1 1 4 8 + 0 3 1 6 4 0 + 0 4 1 9 6 8 + 0 5 2 2 9 6 + 0 6
2 6 2 4 + 0 7 2 9 5 2 + 0 8 3 4 4 4 + 0 9 3 7 7 2 + 1 0
4 4 2 8 + 1 1 4 7 0 0 + 1 2
Note 1: Use additional sheets for other fuel densities or state correction factors. Note 2: Specify maximum capacities.
EDP EXCHANGE FOR SEMI PERMANENT DATA FOR CHECK IN AND LOAD CONTROL
Completed by Operations Engineer AMIR MUKHTAR Issue No: INITIAL
28/03/2007
OPERATIONS ENGINEERING, TECHNICAL DIVISION, FLIGHT OPERATIONS
Date:
EDP-SYSTEM SEMI-PERMANENT DATA
AIRCRAFT DATA C SHEET 5
A/C TYPE ATR42-500
CARRIER PK
5. COCKPIT 5.1 Number of seats and average station
Length of arm from reference station Index influence Maximum number of
cockpit seats ± Inch / metre ± per 1 kg
CAPT
-
7.456 -
0 . 0 7 4 5 6
F/O
-
7.456 -
0 . 0 7 4 5 6
OBSERVER
-
6.496 - 0 . 0 6 4 9 6
Remarks:
EDP EXCHANGE FOR SEMI PERMANENT DATA FOR CHECK IN AND LOAD CONTROL
Completed by Operations Engineer MUHAMMAD FARHAN KHAN Issue No: 01
Date: 22/04/2010
OPERATIONS ENGINEERING, TECHNICAL DIVISION, FLIGHT OPERATIONS
EDP-SYSTEM SEMI-PERMANENT DATA
AIRCRAFT DATA C SHEET 6
A/C TYPE ATR42-500
CARRIER PK
6. LIMITATIONS 6.1 Aircraft Weight Limitations Maximum weight for:
Aircraft Reg.
Or Subtype Nr. Ramp/Taxi Design take-off wet*
Design take-off dry Zero fuel Design landing
AP-BHH
AP-BHI
AP-BHJ
AP-BHM
AP-BHN
AP-BHO
AP-BHP
18770
18770
18770
18770
18770
18770
18770
N O T
A P P L I C A B L E
18600
18600
18600
18600
18600
18600
18600
16700
16700
16700
16700
16700
16700
16700
18300
18300
18300
18300
18300
18300
18300
*Valid for take-off with water- injection
EDP EXCHANGE FOR SEMI PERMANENT DATA FOR CHECK IN AND LOAD CONTROL
Completed by Operations Engineer ALI RAZA Issue No: 02
Date: 03/07/2018
OPERATIONS ENGINEERING, TECHNICAL DIVISION, FLIGHT OPERATIONS
EDP-SYSTEM SEMI-PERMANENT DATA
AIRCRAFT DATA C SHEET 7
A/C TYPE
ATR42-500 CARRIER
PK
6.2. CG – Limits for Loadsheet
Purposes
Enter the forward and the aft balance limits in the boxes commencing at the lowest weight and terminating at the highest weight to be checked. IMPORTANT – If limits are affected and / or determined by passenger / fuel / version / or other conditions specify each set of limits on a separate sheet entering the special condition(s) in the box.
FORWARD AFT
Special condition if applicable
Special condition if applicable
Specify Applicability *
Weight
Index value Specify
Applicability * Weight
Index value
± 10
0
10
1 0.1
0.01
± 10
0
10
1 0.1
0.01
ZFW 1 1 0 0 0 + 2 9 8 7 ZFW 1 1 0 0 0 + 5 7 8 1 1 1 5 0 0 + 3 1 8 3 1 6 7 0 0 + 7 5 5 4 1 5 8 0 0 + 1 8 8 7 1 6 7 0 0 + 2 5 2 8
TOGW 1 1 0 0 0 + 2 9 8 7 TOGW 1 1 0 0 0 + 5 7 8 1 1 1 5 0 0 + 3 1 8 3 1 8 6 0 0 + 7 6 7 8 1 5 8 0 0 + 1 8 8 7
1 8 6 0 0 + 4 0 7 0
*Zero Fuel, Taxi, Take-off, In-flight, Landing NOTE: Attach a balance chart for check purposes. Remarks :
EDP EXCHANGE FOR SEMI PERMANENT DATA FOR CHECK IN AND LOAD CONTROL
Com
OPE
EDP-SYSTEM SEMI-PERMANENT DATA
AIRCRAFT DATA C SHEET 8
Cabin-Configuration (s) 10YP/38Y
A/C TYPE ATR42-500 .
CARRIER PK
7. PASSENGER SEATS
Class codes :
(e.g. F, Y, C, M etc.) Class 1 YP Class 4
Class 2 Y Class 5
Class 3
NOTE: Fill in one table for each cabin configuration code. Number of seats Name of cabin
section Class 1
Class 2
Class 3
Class 4
Class 5
Total per cabin section
ZONE A 10 -
ZONE B - 24
ZONE C - 14
10 38
Sub total Total per Class
pleted by Operations Engineer AMIR MUKHTAR Issue No: INITIAL
Date: 28/03/2007
RATIONS ENGINEERING, TECHNICAL DIVISION, FLIGHT OPERATIONS
Remarks
EDP EXCHANGE FOR SEMI PERMANENT DATA FOR CHECK IN AND LOAD CONTROL
Completed by Operations Engineer AMIR MUKHTAR Issue No: INITIAL
Date: 28/03/2007
OPERATIONS ENGINEERING, TECHNICAL DIVISION, FLIGHT OPERATIONS
EDP-SYSTEM SEMI-PERMANENT DATA
AIRCRAFT DATA C SHEET 9
Cabin-Configuration(s) 10YP/38Y
A/C TYPE ATR42-500
CARRIER PK
8. Average Station 8.1 Class / Cabin Sections
Length of arm from reference station Index influence Class / Cabin section
± Inch / metre ± per 1 kg ZONE A - 3.669 - . 0 3 6 6 9ZONE B + 0.051 + . 0 0 0 5 1ZONE C + 3.861 + . 0 3 8 6 1
8.2 Seating Layout
Show the passenger seating layout for the configurations given in the box at the top by inserting the seat row numbers and letters in the following table. For special seats use the facility codes listed below. B = Bassinet position P = Stretcher location C = Crew seat Q = Quiet zone E = Emergency exit S = Smoking G = Groups T = Near toilet H = Incapacitated passenger U = Unaccompanied minor I = Infant preference rows / seats V = Seat left vacant / offered last J = Rear facing seats W = No movie K = Near galley X = No facility seat, e.g. no distinction L = Leg space seat between smoking and non – smoking M = Wheel chair Y = Not fitted N = No smoking Z = Buffer zone O = Over wing seat A = Aisle Alpha / Characters --- D, F, R, Blank, not used.
EDP EXCHANGE FOR SEMI PERMANENT DATA FOR CHECK IN AND LOAD CONTROL
Completed by Operations Engineer AMIR MUKHTAR Issue No: INITIAL
Date: 28/03/2007
OPERATIONS ENGINEERING, TECHNICAL DIVISION, FLIGHT OPERATIONS
EDP-SYSTEM SEMI-PERMANENT DATA
AIRCRAFT DATA C SHEET 10
CABIN CONFIGURATION(S) 10YP/38Y
A/C TYPE ATR42-500
CARRIER PK
8.2.1 Seat plan Layout / Facilities and Row Index Influence.
ROW LETTER
SEC
TIO
N
RO
W N
O
A C J L
Index influence per seat row ± per 1 kg
1 X X - . 0 3 6 6 92 X X X X - . 0 3 6 6 93 X X X X - . 0 3 6 6 9
21 X X X X + . 0 0 0 5 122 X X X X + . 0 0 0 5 123 X X X X + . 0 0 0 5 124 X X X X + . 0 0 0 5 125 X X X X + . 0 0 0 5 126 X X X X + . 0 0 0 5 127 X X X X + . 0 3 8 6 128 X X X X + . 0 3 8 6 129 X X X X + . 0 3 8 6 130 X X + . 0 3 8 6 1
A A A B B B B B B C C C C
EDP EXCHANGE FOR SEMI PERMANENT DATA FOR CHECK IN AND LOAD CONTROL
Completed by Operations Engineer MUHAMMAD FARHAN KHAN Issue No: 01 Date: 22/04/2010
OPERATIONS ENGINEERING, TECHNICAL DIVISION, FLIGHT OPERATIONS
EDP-SYSTEM SEMI-PERMANENT DATA
AIRCRAFT DATA C SHEET 11
Cabin-configuration(s) 10YP/38Y
A/C TYPE ATR42-500
CARRIER PK
8.3 Cabin Crew Seats
Crew seats location Max. No. of seats
Length of arm from reference station Index influence
± Inch / metre ± per 1 kg FWD 1 - 4.251 - . 0 4 2 5 1AFT 1 + 5.849 + . 0 5 8 4 9
Remarks: 8.4 Galley
Galley location Length of arm from
reference station
Index influence
± Inch / metre ± per 1 kg REAR CABIN RIGHT + 4.978 + . 0 4 9 7 8
Remarks:
EDP EXCHANGE FOR SEMI PERMANENT DATA FOR CHECK IN AND LOAD CONTROL
Completed by Operations Engineer MUHAMMAD FARHAN KHAN Issue No: 01
Date: 22/04/2010
OPERATIONS ENGINEERING, TECHNICAL DIVISION, FLIGHT OPERATIONS
EDP-SYSTEM SEMI-PERMANENT DATA
AIRCRAFT DATA C SHEET 12
Cabin-Configuration(s) 10YP/38Y
A/C TYPE ATR42-500
CARRIER PK
8.5 Pantry Weight / Pantry Code (normally used for above mentioned cabin configurations). NOTE: The columns “Pantry Weight” and “Location” must be filled in only if Basic Weight is specified under paragraph 2.
Pantry Code Pantry Weight Location *
International
Domestic
Test & Training
190 KG
160 KG
45 KG
* Use the locations as under paragraph 8.4. REMARKS:
8.6 Crew Distribution / Crew Code (normally used for above mentioned cabin configurations). NOTE: The column “Location” is to be filled in only if Basic Weight is specified under paragraph 2.
Crew Code Cockpit Crew Cabin Crew Location * Location of Crew
Baggage
REFER ENCLOSED PAGE FOR CREW
IN RH FWD HOLD
* Use the location as under paragraph 8.3.
Total
EDP EXCHANGE FOR SEMI PERMANENT DATA FOR CHECK IN AND LOAD CONTROL
Completed by Operations Engineer ALI RAZA Issue No: 02
Date: 03/07/2018
OPERATIONS ENGINEERING, TECHNICAL DIVISION, FLIGHT OPERATIONS
EDP-SYSTEM SEMI-PERMANENT DATA
AIRCRAFT DATA C SHEET 13
Cabin-Configuration(s) 10YP/38Y
A/C TYPE
ATR42-500 CARRIER
PK
9. DETAILS FOR COMPARTMENT TRIM
Compartment Number
Description
Maximum Capacity
Index value ± per 1 kg
Gross Weight (kg)
Volume * (m3)
RH FWD COMPT
BULK 288
1.8 - . 0 5 7 5 7
LH FWD COMPT
BULK 448
2.8 - . 0 5 2 9 9
FWD PART AFT COMPT
BULK 304
1.9 + . 0 6 7 5
4
AFT PART AFT COMPT
BULK 440 2.75 + . 0 7 8 1 8
* Volume information required for bulk compartments only.
Remarks: 9.1 Combined Load Limitations. Attach relevant company regulations.
EDP EXCHANGE FOR SEMI PERMANENT DATA FOR CHECK IN AND LOAD CONTROL
Completed by Operations Engineer ALI RAZA Issue No: 02
Date: 03/07/2018
OPERATIONS ENGINEERING, TECHNICAL DIVISION, FLIGHT OPERATIONS
10. DETAILS FOR BAY / SECTION TRIM
* Volume information required for bulk compartments only. NOTE 1: Attach a plan for each compartment configuration. NOTE 2: Use additional sheets as required.
10.1 Unsymmetrical Load Limitations.
Attach relevant company regulations.
EDP-SYSTEM SEMI-PERMANENT DATA
AIRCRAFT DATA C SHEET 14
Cabin-Configuration(s) 10YP/38Y
A/C TYPE
ATR42-500 CARRIER
PK
Bay / Section Description
Maximum Capacity
Index value ± per 1 kg
Gross Weight (kg)
Volume * (m3)
RH FWD COMPT
BULK 288
1.8 - . 0 5 7 5 7
LH FWD COMPT
BULK 448
2.8 - . 0 5 2 9 9
FWD PART AFT COMPT
BULK 304
1.9 + . 0 6 7 5
4
AFT PART AFT COMPT
BULK 440 2.75 + . 0 7 8 1 8
EDP EXCHANGE FOR SEMI PERMANENT DATA FOR CHECK IN AND LOAD CONTROL
Completed by Operations Engineer AMIR MUKHTAR Issue No: INITIAL
Date: 28/03/2007
OPERATIONS ENGINEERING, TECHNICAL DIVISION, FLIGHT OPERATIONS
EDP-SYSTEM SEMI-PERMANENT DATA
AIRCRAFT DATA C SHEET 15
A/C TYPE ATR42-500
CARRIER PK
11. BALLAST
FIXED PROVISIONS FOR CARRYING BALLAST.
Specify or attach a table.
Remarks:
EDP EXCHANGE FOR SEMI PERMANENT DATA FOR CHECK IN AND LOAD CONTROL
Completed by Operations Engineer AMIR MUKHTAR Issue No: INITIAL
Date: 28/03/2007
OPERATIONS ENGINEERING, TECHNICAL DIVISION, FLIGHT OPERATIONS
EDP-SYSTEM SEMI-PERMANENT DATA
LOADPLANNING-DATA D SHEET 1
A/C TYPE ATR42-500
CARRIER PK
EDP EXCHANGE FOR SEMI PERMANENT DATA FOR CHECK IN AND LOAD CONTRO
Completed by Operations Engineer AMIR MUKHTAR Issue No: INITIAL
Date: 28/03/2007
OPERATIONS ENGINEERING, TECHNICAL DIVISION, FLIGHT OPERATIONS
EDP-SYSTEM SEMI-PERMANENT DATA
LOADPLANNING-DATA D SHEET 2
A/C TYPE ATR42-500
CARRIER PK
2. UNIT LOAD DEVICES DETAILS
MAXIMUM CAPACITY TYPE CODE TARE WEIGHT GROSS WEIGHT VOLUME * REMARKS
------------- NOT -------------------- APPLICABLE --------------------
* Containers / lgloos only Note: For pallets, specify Lower Deck or Main Deck.
EDP EXCHANGE FOR SEMI PERMANENT DATA FOR CHECK IN AND LOAD CONTROL
Completed by Operations Engineer AMIR MUKHTAR Issue No: INITIAL
Date: 28/03/2007
OPERATIONS ENGINEERING, TECHNICAL DIVISION, FLIGHT OPERATIONS
EDP-SYSTEM SEMI-PERMANENT DATA
LOADPLANNING-DATA D SHEET 3
A/C TYPE ATR42-500
CARRIER PK
3. SPECIAL LOAD
Attach relevant company regulations for special load (AVI, Dangerous Goods, etc.). PLEASE REFER TO PIA WEIGHT AND BALANCE MANUAL AND CARGO HANDLING MANUAL.