AHM560 Data for Check-in & Loadcontrol

Transcription

1 PAGE NO IATA AHM560 DATA LIST OF EFFETIVE PAGES REV 34 Pages/Sheets that are common to all A/ Types. Located in.pdf file "THY-AHM560_FOREWORD" ISSUE DATE REV NO ATION FOR PAGES SHEET NO PAGE DESRIPTION ontents Apr General Info Apr A1,A2 ontact Address Apr B1,B2 Passenger & baggage weights/ crew weights Apr DOW and DOI specifications / Special Information Apr Load&Trim Sheet Information Feb19 34 Updated - List Of Effective Pages / Revision Highlights Nov ,3 Basic and MA formula/ Stabilizer Trim Setting/A/ Registration., Wt Details 16.01A 19Nov Stabilizer Trim Setting table Feb19 34 Updated - A/ Basic Weight & Table 16.02A 28Feb19 34 Updated - Pantry Standard W/I table(atering) Feb19 34 Updated 4 Aircraft Weight Limitations Feb G Limits for Loadsheet Purpose 16.04A 08Feb G Limits for Loadsheet Purpose 16.04B 28Feb19 34 Updated 5 G Limits for Loadsheet Purpose Feb Effect of / APU Taxi Weight 16.05A 28Feb19 34 Updated 6 Effect of / APU Taxi Weight 16.05B 28Feb19 34 Updated 6 Effect of / APU Taxi Weight Feb19 34 Updated 6 Effect of / APU Taxi Weight Feb19 34 Updated 7 rew seats location & distribution Feb19 34 Updated 8 Galley & Pantry Feb19 34 Updated 9 Passenger abin Feb19 34 Updated 9 lass / abin Sections Nov Seating Layout ode Letters Jul Seat Plan Layout T-JYA,B,,D,E,F,G,H,I,J 16.11A 28Feb19 34 Updated 11 Seat Plan Layout T-LYA Feb19 34 Updated 12,13, 14 Details For ompartment Trim & Bay/Section Trim, Ballast Nov D1, D2,D3 Ideal Trim Line, ULD / Special Load May Load&Trim Sheet (T-JYA,B,,D,E,F,G,H,I,J) July Load&Trim Sheet (T-JYL,JYM,JYN,JYO,JYP) Page No:16.00

2 REVISION HIGHLIGHTS REV NO REVISION DESRIPTION 34 T-LYA new aircraft. T-JY,-JYD BW/BI changed due to weighing. Separate fuel tanks added. 33 T-JYB BW/BI changed due to weighing 31 T-JYO BW/BI changed due to weighing 30 T-JYN BW/BI changed due to weighing 29 New cabin location added, T-JYL BW/BI changed due to weighing 28 LM Limits are changed. 27 T-JYJ BW/BI changed due to weighing. Pantry standart weight / index table is revised. 26 T-JYH BW/BI changed due to weighing 25 T-JYI BW/BI changed due to weighing 24 T-JYF,-JYG BW/BI changed due to weighing. 23 T-JYE BW/BI changed due to weighing. 22 T-JYD BW/BI changed due to weighing. 21 T-JY BW/BI changed due to weighing, Alternate Take-off Forward G Limits added. 20 T-JYB BW/BI changed due to weighing. 19 T-JYA BW/BI changed due to weighing. 18 T-JYP entered THY fleet. 17 T-JYN and JYO new aircrafts 16 T-JYM new aircraft 15 T-JYL new aircraft 14 T-JYB seating layout changed due to modification of seat row T-JY seating layout changed due to modification of seat row T-JYA seating layout changed due to modification of seat row T-JYJ new aircraft 10 T-JYI new aircraft 09 T-JYH new aircraft 09 LM values are updated 08 T-JYF & T-JYG new aircraft 07 T-JYE new aircraft 06 T-JYD new aircraft 06 Passenger cabin is divided into 4 sections. 05 T-JY new aircraft 04 All Pantry odes are amended. New design of BW/BI page. ockpit index per kg updated. 03 Pantry standart weight / index table is revised 02 Max. Gross weight of compartment 3 changed to 3382 kg 01 T-JYA & T-JYB new aircraft Page No:16.00

3 B ER 19-Nov-2011 AIRRAFT DATA Sheet 2 abin onfiguration(s) A / TYPE arrier ALL B ER TK 2.BASI INDEX AND MA FORMULA 2.1. Examples and definitions W (Station Ref.Sta.) K % MA W Station Ref.Station K I MA LEMA ( (I - K) Ref.Sta. LEMA W MA 100 = Weight,actual [kg] = Station, Horizontal distance in inches or meters from station zero = Reference Station/axis. Selected station around which all index values are calculated = onstant used as a plus value to avoid negative index figures = onstant used as a Denominator to convert moment values into index values = value corresponding to respective weight = Length of Mean Aerodynamic hord in inches or meters = Horizontal Distance in inches or meters from the station zero to location of the leading EDGE of the MA formula Ref.Station. at = inches from zero K (onstant) = 45 (onstant) = MA Information Length of MA = inches LEMA at = inches from zero 2.4. Stabilizer Trim Setting Stabilizer Trim Setting tables are on page 16.01A. AIRRAFT DATA Sheet 3 abin onfiguration(s) A / TYPE arrier ALL B ER TK 3. AIRRAFT REGISTRATIONS, WEIGHT AND INDEX DETAILS DRY OPERATING WEIGHT BASI WEIGHT X A list of weight and index values for each aircraft registration is given on next page. X Page No:16.01

4 B ER 19-Nov-2011 STABILIZER TRIM SETTING VALUES 27K FLAPS 1 & 5 FLAPS 10, 15 & 25 Page No:16.01A

5 A/ BASI & DRY OPERATING WEIGHT & INDEX TABLE A/ Number Basic*rew(0/0) How to calculate DOW/DOI? A/ Type MSN Reg. of Seats Weight Basic Weight/ (Full potable water tank) B ER T-JYA ockpit rew Total Weight/ B ER T-JYB B ER T-JY abin rew Total Weight/ B ER T-JYD ,9 + B ER T-JYE Pantry Weight/ B ER T-JYF = Dry Operating Weight/ B ER T-JYG B ER T-JYH If actual is different, then make necessary B ER T-JYI adjustments B ER T-JYJ A/ Reg A/ Limitations B ER T-JYL MTAXI KG T-JYA,,-JYJ, B ER T-JYM MTOW KG T-JYL,-YM,- B ER T-JYN MLDW KG YN,YO,-YP B ER T-JYO MZFW KG B ER T-JYP OKPIT REW TOTAL EFFET / ockpit rew No/Locations ockpit rew No/Locations WEIGHT INDEX 2 OKPIT REW OKPIT REW ABIN REW TOTAL EFFET / abin rew No/Locations abin rew No/Locations WEIGHT INDEX 3 ABIN REW (1 Fwd + 2 Aft) ABIN REW (2 Fwd + 2 Aft) ABIN REW (2 Fwd + 3 Aft) ABIN REW (2 Fwd + 4 Aft) PANTRY EFFET / Pantry ode/lass, onfig, App. PANTRY (ATERING) STANDARD W/I TABLE IS ON PAGE 16.02A BW/BI value in the above table already includes potable water with FULL tank(237 kg/3.6 ).If potable water tanks are different, adjust DOW & DOI in proper ratios. INFLUENE OF POTABLE WATER ON DOW/DOI %75 POTABLE WATER %50 POTABLE WATER %25 POTABLE WATER Subtract 59 KG / Subtract 0.9 Subtract 118 KG / Subract 1.8 Subtract 178 KG / Subtract 2.7 *Basic Wt/ includes: ockpit & A/ Documents, Potable Water Tanks Full, Skylife Magazine, Tare empty Weight of all Trolleys & Galley Equipment (hotcup, hotjug, etc). If some items or Equipment are NOT carried make necessary adjustments. Dry Operating Weight/ does NOT include Toolkit Box. heck if they are carried in cargo compartment. It should be shown as Load in compartments (distribution) on loadsheet as Equipment in compartment. TOOLKIT BOX = 23 KG REW BAGGAGE (in BULK argo ompartment) : For Long-haul flights and for flights that crew stays overnight at destination, additional REW BAGGAGE, standard bag weight of 10 kg per crew member is carried. This load is NOT included in above DOW/DOI, and it should be shown as 'LOAD IN OMPARTMENT - DISTRIBUTION" in Loadsheet. * Refer to DOW-DOI_Table-B file for several possible standard cockpit/cabin crew, pantry codes & potable water tanks fill ratio. DOI calculation remark: During alculations due to DS system rounding (or truncating), approximately +/- 0.3 index difference is acceptable. Page No:16.02

6 A/ BASI & DRY OPERATING WEIGHT & INDEX TABLE A/ Number Basic*rew(0/0) A/ Type MSN Reg. of Seats Weight B737-9Max T-LYA How to calculate DOW/DOI? Basic Weight/ (Full potable water tank) + ockpit rew Total Weight/ + abin rew Total Weight/ + Pantry Weight/ = Dry Operating Weight/ If actual is different, then make necessary adjustments A/ Reg A/ Limitations MTAXI KG T-LYA MTOW KG MLDW KG MZFW KG OKPIT REW TOTAL EFFET / ockpit rew No/Locations ockpit rew No/Locations WEIGHT INDEX 2 OKPIT REW OKPIT REW ABIN REW TOTAL EFFET / abin rew No/Locations abin rew No/Locations WEIGHT INDEX 3 ABIN REW (1 Fwd + 2 Aft) ABIN REW (2 Fwd + 2 Aft) ABIN REW (2 Fwd + 3 Aft) ABIN REW (2 Fwd + 4 Aft) PANTRY EFFET / Pantry ode/lass, onfig, App. PANTRY (ATERING) STANDARD W/I TABLE IS ON PAGE 16.02A BW/BI value in the above table already includes potable water with FULL tank(237 kg/3.6 ).If potable water tanks are different, adjust DOW & DOI in proper ratios. INFLUENE OF POTABLE WATER ON DOW/DOI %75 POTABLE WATER %50 POTABLE WATER %25 POTABLE WATER Subtract 59 KG / Subtract 0.9 Subtract 118 KG / Subract 1.8 Subtract 178 KG / Subtract 2.7 *Basic Wt/ includes: ockpit & A/ Documents, Potable Water Tanks Full, Skylife Magazine, Tare empty Weight of all Trolleys & Galley Equipment (hotcup, hotjug, etc). If some items or Equipment are NOT carried make necessary adjustments. Dry Operating Weight/ does NOT include Toolkit Box. heck if they are carried in cargo compartment. It should be shown as Load in compartments (distribution) on loadsheet as Equipment in compartment. TOOLKIT BOX = 23 KG REW BAGGAGE (in BULK argo ompartment) : For Long-haul flights and for flights that crew stays overnight at destination, additional REW BAGGAGE, standard bag weight of 10 kg per crew member is carried. This load is NOT included in above DOW/DOI, and it should be shown as 'LOAD IN OMPARTMENT - DISTRIBUTION" in Loadsheet. * Refer to DOW-DOI_Table-B file for several possible standard cockpit/cabin crew, pantry codes & potable water tanks fill ratio. DOI calculation remark: During alculations due to DS system rounding (or truncating), approximately +/- 0.3 index difference is acceptable. Page No:16.02

7 PANTRY STANDART WEIGHT/INDEX TABLE (ATERING) I - Valid for all B Aircrafts (for Turkish Airlines Flights) T-JYA,JYB,JY,JYD,JYE,JYF,JYG,JYH,JYI,JYJ Pantry ode Galley weight TOTAL FWD AFT WEIGHT INDEX Destination / Departure N ALL INTERNATIONAL FLIGHTS D DOMESTI FLIGHTS ONE WAY G DOMESTI FLIGHTS RETURN PANTRY T-JYL,JYM,JYN,JYO,JYP,-LYA Pantry ode Galley weight TOTAL FWD AFT WEIGHT INDEX Destination / Departure N ALL INTERNATIONAL FLIGHTS D DOMESTI FLIGHTS ONE WAY G DOMESTI FLIGHTS RETURN PANTRY REMARKS: 1- All weights are in kg II - Valid for all B Aircrafts (for AnadoluJET Flights) Pantry ode Galley weight TOTAL Fwd Aft WEIGHT INDEX Destination / Departure U AJET-DOMESTI FLIGHTS ONE WAY V AJET-DOMESTI FLIGHTS RETURN PANTRY W AJET-ALL INTERNATIONAL FLIGHTS Page No:16.02A

8 AIRRAFT DATA Sheet 4 abin onfiguration(s): A / TYPE arrier ALL B ER TK 4. LIMITATIONS 4.1. Aircraft Weight Limitations Maximum weights for: Aircraft Design Take-off Design Take-off Design MSN Ramp/Taxi Zero Reg. Wet Dry Landing T-JYA kg kg kg kg T-JYB kg kg kg kg T-JY kg kg kg kg T-JYD kg kg kg kg T-JYE kg kg kg kg T-JYF kg kg kg kg T-JYG kg kg kg kg T-JYH kg kg kg kg T-JYI kg kg kg kg T-JYJ kg kg kg kg T-JYL kg kg kg kg T-JYM kg kg kg kg T-JYN kg kg kg kg T-JYO kg kg kg kg T-JYP kg kg kg kg T-LYA kg kg kg kg LM (Last Minute hanges) Information : Last Minute hanges (LM) to the mass and balance sheet are only permitted when the changes of the load (either minus or plus) in last minutes are within the following limits. B : 500 kg Total Weight (Passengers,argo,Mail or any combination) These changes must be shown as pax, cargo, mail, baggage etc. in the Load & Trim Sheet.The effect of LM in aircraft G must be checked. Aircraft G after LM must not exceed forward and aft operational G Limits. In Addition to LM Weight, LM influence should be shown on Load & Trim Sheet in a suitable space under LM title preferably next to LM weight. Page No:16.03

9 B ER 08-Feb-2016 AIRRAFT DATA Sheet 5 abin onfiguration(s) A / TYPE arrier T-JYA,B,,D,E,F,G,H,I,J B ER TK G - Limits for Loadsheet Purpose T-JYA,JYB,JY,JYD,JYE,JYF,JYG,JYH,JYI,JYJ FORWARD ZERO FUEL HEK Specify applicability FUEL LOADED IN AUX. TANK NO FUEL LOADED IN AUX. TANK AFT ZERO FUEL HEK Weight(kg) Specify applicability Weight(kg) Value Value TAKE-OFF HEK TAKE-OFF HEK NO FUEL LOADED IN AUX. TANK FUEL LOADED IN AUX TANK Alternate Forward Limits-I Take-off heck Alternate Forward Limits-II Take-off heck LANDING HEK LANDING HEK Page No:16.04

10 B ER 08-Feb-2016 AIRRAFT DATA Sheet 5 abin onfiguration(s) A / TYPE arrier T-JYL,JYM,JYN,JYO,JYP B ER TK G - Limits for Loadsheet Purpose FORWARD ZERO FUEL HEK Specify applicability AFT ZERO FUEL HEK Weight(kg) Specify applicability Weight(kg) Value Value TAKE-OFF HEK TAKE-OFF HEK Alternate Forward Limits-I Take-off heck Alternate Forward Limits-II Take-off heck LANDING HEK LANDING HEK Page No:16.04A

11 AIRRAFT DATA Sheet 5 abin onfiguration(s) A / TYPE arrier T-LYA B737-9Max TK G - Limits for Loadsheet Purpose FORWARD ZERO FUEL HEK Specify applicability IF LANDING WEIGHT >73345 KG IF LANDING WEIGHT <=73345 KG AFT ZERO FUEL HEK Weight(kg) Specify applicability Weight(kg) Value Value TAKE-OFF HEK LANDING HEK TAKE-OFF HEK LANDING HEK Page No:16.04B

12 B ER 18-Feb-2015 AIRRAFT DATA Sheet 6 abin onfiguration(s) A / TYPE arrier ALL B ER TK 5. EFFET OF FUEL Loading Usage Standard Procedure X Non-standard Procedure MAIN TANK & ENTER TANK FUEL DETAILS FUEL DENSITY: KG/L , , , , , , , , , , , , , , , , , , , , , , , , , , , , , , , , , , , , , , , , , , , , , , , , , , , , , ² -10, , ¹ 9, , , , , , , , , , ,83 ¹ Main tanks are full ² Main tanks and center tank are full REMARKS: FUEL LOADING PROEDURE IS AS FOLLOWS; 1. Load main tanks 1 & 2 equally until they are full. 2. Load additional fuel in the center tank until full. 3. Load additional fuel in the aft auxiliary fuel tank if required. * * Auxiliary fuel tank weight/index table is on page 16.05A. * Auxiliary Tank is installed only on T-JYA,B,,D,E,F,G,H,I,J VOLUMETRI APAITY LITER KG (0.803kg/lt) MAIN TANKS LT 3915 KG MAIN TANKS LT 3915 KG ENTER TANK LT KG TOTAL LT KG VOLUMETRI APAITY LITER KG (0.803kg/lt) AUXILIARY FUEL TANK* LT 2923 KG TOTAL with aux.fuel tank full LT KG Page No:16.05

13 B ER 18-Feb-2015 AIRRAFT DATA Sheet 6 abin onfiguration(s) A / TYPE arrier T-JYA,B,,D,E,F,G,H,I,J B ER TK 5. EFFET OF FUEL Auxiliary Tank is installed only on T-JYA,B,,D,E,F,G,H,I,J If Aft Auxiliary Tank is used, than add fuel index value for the corresponding fuel weight given in the below table, to total index of main tank + center tank. AFT AUXILIARY TANK FUEL DETAILS FUEL DENSITY: KG/L usage procedure; When the aft auxiliary fuel is intended to be used, operate as folows: With normal operation of the Auxiliary System (AFS), auxiliary fuel transfer will start automatically when the enter Tank fuel has decreased to approximately 11100kg, but no sooner than 10 minutes after takeoff rotation. ontinue to use enter Tank fuel until all aft auxiliary fuel has been transferred and the enter Tank is empty. From that point, use fuel feeds from the No.1 and No.2 Main tanks to their respective engines for the remainder of the flight. When aft fuel has not been loaded, follow normal aircraft operating procedures. 5.2 APU / TAXI FUEL WEIGHT Due to local taxiing distances and local needs for APU running, total taxi may be different in your local station. It may be calculated by using the following fuel flow figures; Taxi Flow = 15 kg/minute APU Flow = 105 kg/hour Page No:16.05

14 AIRRAFT DATA Sheet 6 abin onfiguration(s) A / TYPE arrier T-JYA,B,,D,E,F,G,H,I,J B ER TK 5. EFFET OF FUEL Loading Usage Standard Procedure X Non-standard Procedure MAIN TANK 1&2 FUEL DENSITY: KG/L AUXILARY TRIM TANK FUEL DENSITY: KG/L ENTER TANK FUEL DETAILS FUEL DENSITY: KG/L * Auxiliary Tank is installed only on T-JYA,B,,D,E,F,G,H,I,J Page No:16.05A

15 AIRRAFT DATA Sheet 6 abin onfiguration(s) A / TYPE arrier T-JYL,-M,-N,-O,-P B ER TK 5. EFFET OF FUEL Loading Usage Standard Procedure X Non-standard Procedure MAIN TANK 1&2 FUEL DETAILS FUEL DENSITY: KG/L ENTER TANK FUEL DETAILS FUEL DENSITY: KG/L Page No:16.05B

16 AIRRAFT DATA Sheet 6 abin onfiguration(s) A / TYPE arrier T-LYA B ER TK 5. EFFET OF FUEL Loading Usage Standard Procedure X Non-standard Procedure MAIN TANK & ENTER TANK FUEL DETAILS FUEL DENSITY: KG/L Wt. kg ² ¹ ¹ Main tanks 1&2 full at nominal density of kg/l. ² Main tanks 1&2 and enter tank are full at nominal density of kg/l. 3 Main tanks 1&2 and enter tank are full at maximum density of kg/l. REMARKS: FUEL LOADING PROEDURE IS AS FOLLOWS; 1. Load main tanks 1 & 2 equally until they are full. 2. Load additional fuel in the center tank until full. 3. Load additional fuel in the aft auxiliary fuel tank if required. * VOLUMETRI APAITY LITER KG (0.803kg/lt) MAIN TANKS LT 4099 KG MAIN TANKS LT 4099 KG ENTER TANK LT KG TOTAL LT KG Page No:16.05

17 AIRRAFT DATA Sheet 6 abin onfiguration(s) A / TYPE arrier T-LYA B ER TK 5. EFFET OF FUEL Loading Usage Standard Procedure X Non-standard Procedure MAIN TANK 1&2 FUEL DENSITY: KG/L ENTER TANK Page No:16.05

18 B ER 17-Oct-2017 AIRRAFT DATA Sheet 7 abin onfiguration(s) A / TYPE arrier ALL B ER TK 6. REW 6.1. Number of cockpit crew seats and average location Maximum number of Length of arm from reference station influence cockpit seats +/- (inch) +/- per 1 kg Number of cabin crew seats and location ABIN rew seats Max. Length of arm from reference station influence locations No. of seats +/- (inch) +/- per 1 kg FWD AFT rew Distribution / rew ode rew ode ockpit rew Total No abin rew Total No Number of abin rews at Location FWD 2/ / / / / / AFT Location of rew Baggage BULK ARGO OMPT. Page No:16.06

19 AIRRAFT DATA Sheet 8 abin onfiguration(s) A / TYPE arrier ALL B ER TK 7. GALLEY AND PANTRY Galleys Length of arm from Galley Locations Reference Station influence +/- (Inch) +/- per 1 kg G G G FWD(G1+G2+G7) G6A G4B AFT(G6A+G4B) T-LYA Length of arm from Galley Locations Reference Station influence +/- (Inch) +/- per 1 kg G G G FWD(G1+G2+G7) G6A G AFT(G6A+G4) Remarks: FWD, AFT average Galley locations can be used for simplicity 7.2 Pantry Weight / Pantry ode Pantry Weight / Pantry ode table is given on A/ BASI WEIGHT & INDEX TABLE. 7.3 SEATING ONDITIONS LOADSHEET OUTPUT State below how the seating conditions should be shown in the respective loadsheet box.give example.enclose a passanger distribution table if used. Page No:16.07

20 abin onfiguration(s) ALL 8. PASSENGER ABIN 8.1 Passenger Seats Passenger Seats (T-JYA,...,JYJ) LASS ODES lass 1 : lass 2 : Y lass 3 : Name of abin Section NUMBER OF SEATS lass 1 lass 2 lass 3 Total per cabin section AIRRAFT DATA Sheet 9 A / TYPE arrier B ER TK Name of abin Section NUMBER OF SEATS lass 1 lass 2 lass 3 Total per cabin section ABIN ONFIGURATION 16 / 135Y ABIN ONFIGURATION 151Y OA OA OB OB O O OD OD Total per Total per class class Passenger Seats (T-JYL,JYM,JYN,JYO,JYP) LASS ODES lass 1 : lass 2 : Y lass 3 : Name of abin Section NUMBER OF SEATS lass 1 lass 2 lass 3 Total per cabin section Name of abin Section NUMBER OF SEATS lass 1 lass 2 lass 3 Total per cabin section ABIN ONFIGURATION 16 / 153Y ABIN ONFIGURATION 169Y OA OA OB OB O O OD OD Total per Total per class class Passenger Seats (T-LYA) LASS ODES lass 1 : lass 2 : Y lass 3 : Name of abin Section NUMBER OF SEATS lass 1 lass 2 lass 3 Total per cabin section ABIN ONFIGURATION 16 / 153Y OA OB O OD Total per class Page No:16.08

21 AIRRAFT DATA Sheet 9 abin onfiguration(s) A / TYPE arrier ALL B ER TK 8.2 lass/abin Sections T-JYA,...,JYJ lass/abin Section Length of arm from Reference station influence +/- inch +/- per 1 kg OA OB O OD T-JYL,JYM,JYN,JYO,JYP T-LYA lass/abin Section Length of arm from Reference station influence +/- inch +/- per 1 kg OA OB O OD lass/abin Section Length of arm from Reference station influence +/- inch +/- per 1 kg OA OB O OD Page No:16.09

22 8.3 Seating Layout B ER 19-Nov-2011 AIRRAFT DATA Sheet 10 A / TYPE arrier B ER TK 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 description codes listed below : B = Bassinet position = rew seat E = Emergency exit G = Groups H = Incapacitated passenger I = Infant preference rows/seats J = Rear facing seats K = Near galley L = Leg space seat M = Wheel chair N = No Smoking O = Over wing seat P = Stretcher location Q = Quiet zone S = Smoking T = Near toilet U = Unaccompanied minor V = Seat left vacant/offered last W = No Movie X = No facility seat (e.g. no distinction between smoking and non-smoking) Y = Not fitted Z = Buffer zone. = Aisle Alfa/haracters - A, D, F, R, Blank not used Note : Seat designators to be in accordance with Recommended Pratice Page No:16.10

23 SETION ROW NO abin onfiguration(s) T-JYA,B,,D,E,F,G,H,I,J Seatplan Layout / Facilities and Row Influence A B D Influence per Seat- Row per1kg Rows from-to: B ER 07-Jul-2014 AIRRAFT DATA Sheet 11 A / TYPE arrier B ER TK ABIN ONFIGURATION 151Y A B D E F Rows from-to: A B D E F ABIN ONFIGURATION 16 / 135Y NBI N Y. Y N NBI 1 NBI N Y. Y N NBI NI N Y. Y N NI 2-4 NI N Y. Y N NI NBI N N. N N NBI 5 NBI N N. N N NBI NI N N. N N NI 6-10 NI N N. N N NI NE NE NE. NE NE NE NE NE NE. NE NE NE NI N N. N N NI NI N N. N N NI Y Y Y. N N NI 27 Y Y Y. N N NI FIXED ERTAIN LASS DIVIDER is shown as : THE AISLE is shown as :. Page No:16.11

24 SETION ROW NO abin onfiguration(s) T-JYL,JYM,JYN,JYO,JYP Seatplan Layout / Facilities and Row Influence A B D Influence per Seat- Row per1kg Rows from-to: B ER 10-July-2015 AIRRAFT DATA Sheet 11 A / TYPE arrier B ER TK ABIN ONFIGURATION 169Y A B D E F Rows from-to: A B D E F ABIN ONFIGURATION 16 / 153Y N NBI Y. Y NBI N 1 N NBI Y. Y NBI N NI N Y. Y N NI 2-4 NI N Y. Y N NI N NBI N. N NBI N 5 N NBI N. N NBI N NI N N. N N NI 6-12 NI N N. N N NI NE NE NE. NE NE NE NE NE NE. NE NE NE NI N N. N N NI NI N N. N N NI Y Y Y. N N NI 30 Y Y Y. N N NI FIXED ERTAIN LASS DIVIDER is shown as : THE AISLE is shown as :. FIXED ERTAIN LASS DIVIDER is shown as : THE AISLE is shown as :. Page No:16.11A

25 SETION ROW NO abin onfiguration(s) T-LYA Seatplan Layout / Facilities and Row Influence A B D Influence per Seat- Row per1kg Rows from-to: ABIN ONFIGURATION 16 / 153Y A B D E F NBI N Y. Y N NBI NI N Y. Y N NI N NBI N. N NBI N NI N N. N N NI NE NE NE. NE NE NE NI N N. N N NI N N NI AIRRAFT DATA Sheet 11 A / TYPE arrier B ER TK FIXED ERTAIN LASS DIVIDER is shown as : THE AISLE is shown as :. Page No:16.11B

26 AIRRAFT DATA Sheet 12 abin onfiguration(s) A / TYPE arrier ALL B ER TK 9. DETAILS FOR OMPARTMENT TRIM T-JYA,...,JYJ OMPARTMENT NUMBER DESRIPTION MAXIMUM APAITY GROSS VOLUME* WEIGHT (M 3 ) (kg) INDEX INFLUENE +/- per 1 kg 1 FWD HOLD FWD HOLD AFT HOLD AFT HOLD T-JYL,JYM,JYN,JYO,JYP OMPARTMENT NUMBER T-LYA DESRIPTION MAXIMUM APAITY GROSS VOLUME* WEIGHT (M 3 ) (kg) INDEX INFLUENE +/- per 1 kg 1 FWD HOLD FWD HOLD AFT HOLD AFT HOLD OMPARTMENT NUMBER DESRIPTION MAXIMUM APAITY GROSS VOLUME* WEIGHT (M 3 ) (kg) INDEX INFLUENE +/- per 1 kg 1 FWD HOLD FWD HOLD AFT HOLD AFT HOLD Volume information required for bulk compartments only. 9.1 ombined Load Limitations : None 9.2 umulative Load Limitations : None AIRRAFT DATA Sheet 13 abin onfiguration(s) A / TYPE arrier ALL B ER TK 10. DETAILS FOR BAY / SETION TRIM MAX. APAITY influence BAY / SETION GROSS WEIGHT (kg) VOLUME (M 3 ) +/- per 1 kg NOT APPLIABLE 10.1 Unsymmetrical load limitations: NOT APPLIABLE AIRRAFT DATA Sheet 14 abin onfiguration(s) A / TYPE arrier ALL B ER TK 11. BALLAST FIXED PROVISIONS FOR ARRYING BALLAST? REMARKS : BALLAST IS NOT REQUIRED Page No:16.12

27 B ER 19-Nov-2011 D AIRRAFT DATA Sheet 1 A / TYPE arrier B ER TK 1. G LIMITS 1.1. Planning Limits G-Limits for loadplanning purpose shall be agreed between carrier and system operator. 1.2 Ideal Trim Line at ZFW for Saving Purposes The IDEAL TRIM LINE shown in the balance graph below is a loadplanning limit only. In the interest of fuel economy the load in the compartments shall whenever possible. be distributed in such a way that the LIZFW is aft of this line. The respective breakpoints (weight / index) of the ideal trim line shall be entered in the table below. WEIGHT INDEX VALUE UNIT LOAD DEVIES DETAILS Type ode Tare weight Maximum apacity Gross VOLUME Weight (m 3 ) AIRRAFT DATA A / TYPE B ER Remarks D Sheet 2 arrier TK NOT APPLIABLE AIRRAFT DATA A / TYPE B ER 3. SPEIAL LOAD Apply Turkish Airlines & IATA regulations. When necessary contact Turkish Airlines Station Manager. D Sheet 3 arrier TK Page No:16.13