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ATR72-500

S.NO SHEET # DATE ISSUE #1 LEP 1 23/04/2018 INITIAL2 A SHEET 1 23/04/2018 INITIAL3 A SHEET 2 23/04/2018 INITIAL4 B SHEET 1 23/04/2018 INITIAL5 B SHEET 2 23/04/2018 INITIAL6 B SHEET 3 23/04/2018 INITIAL7 C SHEET 1 23/04/2018 INITIAL8 C SHEET 2 23/04/2018 INITIAL9 C SHEET 3 23/04/2018 INITIAL

10 C SHEET 4 23/04/2018 INITIAL11 C SHEET 4A 23/04/2018 INITIAL12 C SHEET 4B 23/04/2018 INITIAL13 C SHEET 4C 23/04/2018 INITIAL14 C SHEET 4D 23/04/2018 INITIAL15 C SHEET 4E 23/04/2018 INITIAL16 C SHEET 5 23/04/2018 INITIAL17 C SHEET 6 23/04/2018 INITIAL18 C SHEET 7 23/04/2018 INITIAL19 C SHEET 8 23/04/2018 INITIAL20 C SHEET 8A 23/04/2018 INITIAL21 C SHEET 9 23/04/2018 INITIAL22 C SHEET 10 23/04/2018 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)

LIST OF EFFECTIVE PAGES ISSUE # 00

EFFECTIVITY

ALL (FUEL DENSITY 0.77 Kg / litre)

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EDP EXCHANGE FOR SEMI PERMANENT DATAFOR CHECK IN AND LOAD CONTROL

LEP 1 Date: 23/04/2018

21 C SHEET 9 23/04/2018 INITIAL22 C SHEET 10 23/04/2018 INITIAL23 C SHEET 11 23/04/2018 INITIAL24 C SHEET 12 23/04/2018 INITIAL25 C SHEET 13 23/04/2018 INITIAL26 C SHEET 14 23/04/2018 INITIAL27 C SHEET 15 23/04/2018 INITIAL28 D SHEET 1 23/04/2018 INITIAL29 D SHEET 2 23/04/2018 INITIAL

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LEP 1 Date: 23/04/2018

EDP EXCHANGE FOR SEMI PERMANENT DATA FOR CHECK IN AND LOAD CONTROL

Completed by Operations Engineer ALI RAZA Issue No: INITIAL

Date: 23/04/2018

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:

mailto:[email protected]



Date: 23/04/2018



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


Completed by Operations Engineer ALI RAZA Issue No.: INITIAL

Date: 23/04/2018



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:


Completed by Operations Engineer ALI RAZA Issue No: INITIAL Date: 20/04/2018 OPERATIONS ENGINEERING, TECHNICAL DIVISION, FLIGHT OPERATIONS


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.


Completed by Operations Engineer ALI RAZA Issue No: INITIAL Date: 23/04/2018 OPERATIONS ENGINEERING, TECHNICAL DIVISION, FLIGHT OPERATIONS


GENERAL INFORMATION

B SHEET 3

CARRIER PK

3. DRY OPERATING WEIGHT AND DRY OPERATING INDEX SPECIFICATIONS

(Tick as appropriate)

DOW DOI Remarks

Item Incl Excl Incl Excl

Basic Weight (EMPTY WEIGHT) Crew Weight Crew Baggage Pantry Containers

Pallets

CONFIG Weight

FLIGHT PACK

REMARKS:-



Date: 23/04/2018



AIRCRAFT DATA C SHEET 1

A/C TYPE ATR72-500

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 Dry operating index DOI Dead load index DLI Dead load MAC MACDLW Loaded Index at zero fuel weight LIZFW Loaded index at take-off weight LITOW Loaded Index at landing weight LILAW MAC – at zero fuel weight MACZFW MAC - at takeoff weight MACTOW MAC at landing weight MACLAW Stabilizer trim setting at take-off STABTO *

* specify ANU or AND as appropriate. Passenger trim output

Please mark your requirements in respective box. Remarks Class Trim Cabin Area Trim Seat Row Trim



Date: 23/04/2018




A/C TYPE ATR72-500

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: 13224 Standard Fleet Index: 46.2

Registration

Weight Adjustment

Index Adjustment

Registration

Weight Adjustment

Index Adjustment

AP-BKZ

-165

4.6

AP-BKY

15

-1.0

AP-BKV

-33

-1.6

AP-BKW

104

0.2

AP-BKX

79

-2.0

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.



Date: 23/04/2018




A/C TYPE ATR72-500

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 = 14.180 Meters from zero K (constant) = 50 C (constant) = 150

3.3 MAC Information

Length of MAC = 2.303 Meters LEMAC at = 13.604 Meters from zero

3.4 Stabilizer trim setting

MAC Range Min 14% Max 37% STAB Range Min 2.5 Max 0



Date: 23/04/2018




A/C TYPE ATR72-500

CARRIER PK

4. EFFECT OF FUEL/INJECTION WATER

Fuel loading � Fuel Usage � Standard Procedure � Non-standard Procedure � FUEL DENSITY: 0.77 kg/litre

Fuel Weight Index value


+/-

100

10

1

+/-

100

10

1

1 8 9 0 0 7 4 9 + 0 1 1 3 2 9 + 0 2 1 8 9 9 + 0 3 2 4 5 8 + 0 4 3 0 2 8 + 0 5 3 5 9 7 + 0 6 4 2 4 1 + 0 7 4 9 0 5 + 0 8

Note 1: Use additional sheets for other fuel densities or state correction factors. Note 2: Specify maximum capacities.



Date: 23/04/2018



AIRCRAFT DATA C SHEET 4A

A/C TYPE ATR72-500

CARRIER PK





+/-

100

10

1

+/-

100

10

1

1 8 8 0 0 7 4 8 + 0 1 1 3 2 7 + 0 2 1 8 9 8 + 0 3 2 4 5 6 + 0 4 3 0 2 8 + 0 5 3 5 9 3 + 0 6 4 2 2 7 + 0 7 4 9 6 9 + 0 8




Date: 23/04/2018 OPERATIONS ENGINEERING, TECHNICAL DIVISION, FLIGHT OPERATIONS


AIRCRAFT DATA C SHEET 4B

A/C TYPE ATR72-500

CARRIER PK


Fuel loading Fuel Usage Standard Procedure Non-standard Procedure FUEL DENSITY: 0.79 kg/litre



+/-

100

10

1

+/-

100

10

1

1 8 7 0 0 7 4 6 + 0 1 1 3 2 6 + 0 2 1 8 9 7 + 0 3 2 4 5 4 + 0 4 3 0 2 8 + 0 5 3 5 8 8 + 0 6 4 2 1 3 + 0 7 5 0 3 2 + 0 8




Date: 23/04/2018



AIRCRAFT DATA C SHEET 4C

A/C TYPE ATR72-500

CARRIER PK





+/-

100

10

1

+/-

100

10

1

1 8 6 0 0 7 4 4 + 0 1 1 3 2 4 + 0 2 1 8 9 6 + 0 3 2 4 5 2 + 0 4 3 0 2 8 + 0 5 3 5 9 2 + 0 6 4 2 0 0 + 0 7 5 0 9 6 + 0 8




Date: 23/04/2018



AIRCRAFT DATA C SHEET 4D

A/C TYPE ATR72-500

CARRIER PK





+/-

100

10

1

+/-

100

10

1

1 8 6 0 0 7 4 3 + 0 1 1 3 2 2 + 0 2 1 8 9 5 + 0 3 2 4 5 0 + 0 4 3 0 2 8 + 0 5 3 5 9 2 + 0 6 4 1 8 8 + 0 7 5 0 0 6 + 0 8






AIRCRAFT DATA C SHEET 4E

A/C TYPE ATR72-500

CARRIER PK


Fuel loading Fuel Usage Standard Procedure Non-standard Procedure FUEL DENSITY: 0.82 kg/litre



+/-

100

10

1

+/-

100

10

1

1 8 5 0 0 7 4 1 + 0 1 1 3 2 1 + 0 2 1 8 9 4 + 0 3 2 4 4 9 + 0 4 3 0 2 8 + 0 5 3 5 9 1 + 0 6 4 1 7 6 + 0 7 4 9 5 1 + 0 8 5 2 2 3 + 0 9




Date: 23/04/2018




A/C TYPE ATR72-500

CARRIER PK

5. COCKPIT 5.1 Number of seats and average station

Maximum number of cockpit seats

Length of arm from reference station Index influence

± Inch / metre ± per 1 kg

CAPT -

4.540 -

0 . 0 6 4 2 7

F/O

-

4.540 -

0 . 0 6 4 2 7

OBSERVER

-

5.500 - 0 . 0 5 7 8 7

Remarks:


Completed by Operations Engineer ALI RAZA Issue No: INITIAL Date: 23/04/2018




A/C TYPE ATR72-500

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-BKZ

AP-BKV

AP-BKW

AP-BKY

AP-BKY

22970

22970

22970

22970

22970

N O T

A P P L I C A B L E

22800

22800

22800

22800

22800

20800

20800

20800

20800

20800

22350

22350

22350

22350

22350

*Valid for take-off with water- injection






A/C TYPE ATR72-500

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 3 0 0 0 + 3 2 0 0 ZFW 1 3 0 0 0 + 5 9 0 0 1 4 7 0 0 + 3 6 0 0 2 0 8 0 0 + 7 6 0 0 1 8 0 0 0 + 2 8 0 0 2 0 8 0 0 + 3 6 0 0

TOGW 1 3 0 0 0 + 3 2 0 0 TOGW 1 3 0 0 0 + 5 9 0 0 1 4 7 0 0 + 3 6 0 0 2 2 8 0 0 + 8 1 0 0 1 8 0 0 0 + 2 8 0 0

2 2 8 0 0 + 4 4 0 0

*Zero Fuel, Taxi, Take-off, In-flight, Landing NOTE: Attach a balance chart for check purposes. Remarks :




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.

Name of cabin section

Number of seats Total per cabin section Class 1

Class 2

Class 3

Class 4

Class 5

ZONE A 12 8Y

ZONE B - 32

ZONE C - 18

12 58

Remarks



Cabin-Configuration (s) 12YP/58Y

A/C TYPE ATR72-500 .

CARRIER PK

Sub total Total per Class




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.

Name of cabin section

Number of seats Total per cabin section Class 1

Class 2

Class 3

Class 4

Class 5

ZONE A - 20

ZONE B - 32

ZONE C - 18

- 70

Remarks


AIRCRAFT DATA C SHEET 8 A

Cabin-Configuration (s) 70Y

A/C TYPE ATR72-500 .

CARRIER PK

Sub total Total per Class



Date: 23/04/2018




Cabin-Configuration(s) 12YP/58Y OR 70Y

A/C TYPE ATR72-500

CARRIER PK

8. Average Station 8.1 Class / Cabin Sections

Class / Cabin section Length of arm from

reference station Index influence

± Inch / metre ± per 1 kg ZONE A - 4.161 - . 0 2 7 7 4 ZONE B + 0.792 + . 0 0 5 2 8 ZONE C + 5.576 + . 0 3 7 1 7

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.


Completed by Operations Engineer ALI RAZA Issue No:

INITIAL

Date: 23/04/2018



CABIN CONFIGURATION(S) 12YP/58Y OR 70Y

A/C TYPE ATR72-500

CARRIER PK

8.2.1 Seat plan Layout / Facilities and Row Index Influence.

SEC

TIO

N

RO

W N

O

ROW LETTER Index influence per seat row ± per 1 kg

A B C D

A A A A A B B B B B B B B C C C C C

1 X X X X - . 0 2 7 7 42 X X X X - . 0 2 7 7 43 X X X X - . 0 2 7 7 44 X X X X + . 0 2 7 7 4

5 X X X X + . 0 2 7 7 46 X X X X + . 0 0 5 2 87 X X X X + . 0 0 5 2 88 X X X X + . 0 0 5 2 89 X X X X + . 0 0 5 2 810 X X X X + . 0 0 5 2 811 X X X X + . 0 0 5 2 812 X X X X + . 0 0 5 2 813 X X X X + . 0 0 5 2 814 X X X X + . 0 3 7 1 715 X X X X + . 0 3 7 1 716 X X X X + . 0 3 7 1 717 X X X X + . 0 3 7 1 718 X X + . 0 3 7 1 7






Cabin-configuration(s) 12YP/58Y OR 70Y

A/C TYPE ATR72-500

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 + 7.75 - . 0 4 2 8 7AFT 1 + 22.34 + . 0 5 4 4 1

Remarks: 8.4 Galleys

Galley locations Length of arm from

reference station

Index influence

± Inch / metre ± per 1 kg FWD + 21.47 + . 0 4 8 6 1 AFT + 23.09 + . 0 5 9 4 3

Remarks:



Date: 23/04/2018





A/C TYPE ATR72-500

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

467 KG

364 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







A/C TYPE ATR72-500

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 480

3 - . 0 4 9 8 9

LH FWD COMPT BULK 448

2.8 - . 0 4 9 8 9

FWD PART AFT COMPT BULK 195

1.23 + . 0 6 0 4 4

AFT PART AFT COMPT BULK 442 2.75 + . 0 6 7 5 3

* Volume information required for bulk compartments only.

Remarks: IN CASE OF CATERING IS LOADED IN REAR CARGO GALLEY, ONLY AFT PART OF THE AFT HOLD WILL BE USED FOR BULK BAGGAGE AND CARGO LOADING AND FWD PART OF AFT HOLD WILL REMAIN EMPTY DUE TO CATERING LOADING AND UNLOADING IN THE REAR CARGO COMPARTMENT GALLEY. 9.1 Combined Load Limitations. Attach relevant company regulations.




10. DETAILS FOR BAY / SECTION TRIM

Bay / Section Maximum Capacity Index value

± per 1 kg

Gross Weight (kg)

Volume * (m3)

FWD HOLD FWD RH COMPT 480 3 - . 0 4 9 8 9 FWD LH COMPT 448 2.8 - . 0 4 9 8 9

AFT HOLD

AFT PART AFT COMPT 442 2.75 + 0 6 7 5 3

* 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.



Cabin-Configuration(s) 12YP/58Y OR 70Y (WITH PANTRY LOADED IN REAR CARGO GALLEY)

A/C TYPE ATR72-500

CARRIER PK



Date: 23/04/2018




A/C TYPE ATR72-500

CARRIER PK

11. BALLAST

FIXED PROVISIONS FOR CARRYING BALLAST.

Specify or attach a table.

Remarks:





LOADPLANNING-DATA D SHEET 1

A/C TYPE ATR72-500

CARRIER PK

1. 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.



Date: 28/04/2018



LOADPLANNING-DATA D SHEET 2

A/C TYPE ATR72-500

CARRIER PK

2. 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.

LEP AHM50 ISSUE 00.xlssheet a 1ASHEET 1

COMMUNICATIONADDRESSESPK

sheet a 2ASHEET 2

COMMUNICATIONADDRESSESPK

sheet b 1BSHEET 1PK

GENERAL INFORMATION

sheet b 2BSHEET 2

AIRCRAFT DATAPK

sheet b 3BSHEET 3

GENERAL INFORMATIONPK

sheet c 1CSHEET 1

AIRCRAFT DATAPKATR72-500

sheet c 2CSHEET 2


sheet c 3CSHEET 3


sheet c 4CSHEET 4


sheet c 4aCSHEET 4A


sheet c 4bsheet c 4cCSHEET 4C


sheet c 4dCSHEET 4D


sheet c 4esheet c 5CSHEET 5

AIRCRAFT DATAATR72-500PK

sheet c 6CSHEET 6

AIRCRAFT DATAPKN

ATR72-500

sheet c 7sheet c 8CSHEET 8ATR72-500PK

AIRCRAFT DATAClass codes :(e.g. F, Y, C, M etc.) Class 1 YP Class 4Class 2 Y Class 5Class 3Remarks

sheet c 8asheet c 9CSHEET 912YP/58Y OR 70Y

ATR72-500PK

AIRCRAFT DATA

sheet c 10sheet c 11sheet c 12sheet c 13CSHEET 1312YP/58Y OR 70Y


sheet c 14sheet c 15CSHEET 15

AIRCRAFT DATAFIXED PROVISIONS FOR CARRYING BALLAST.Specify or attach a table.Remarks:

sheet d 1DSHEET 1

LOADPLANNING-DATAPKATR72-500

sheet d 2DSHEET 2

LOADPLANNING-DATAAttach relevant company regulations for special load (AVI, Dangerous Goods, etc.).

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