SHEET NO Aug15 78 Updated - List Of Effective Pages / Revision Highlights

Transcription

1 PAGE NO A Aug-2015 IATA AHM560 DATA LIST OF EFFETIVE PAGES REV 77 Pages/Sheets that are common to all A/ Types. Located in.pdf file "THY-AHM560_FOREWORD.pdf" ISSUE DATE REV NO ATION FOR PAGES SHEET NO ontents Apr General Info Apr A1,A2 ontact Address. PAGE DESRIPTION Apr B1,B2 Passenger & baggage weights/ crew weights Apr DOW and DOI specifications / Special Information Apr Load&Trim Sheet Information Aug15 78 Updated - List Of Effective Pages / Revision Highlights Mar ,3 Basic Index and MA formula/ Stabilizer Trim Settings/A/ Registration., Wt Index Details Aug15 78 Updated - A/ Basic & Dry Operating Weight & Index Table 08.02B 03Apr Pantry odes Aug Aircraft Weight Limitations Apr G Limits for Loadsheet Purpose JDK, JDM, JDN, JIH, JII 08.04B 18Sep G Limits for Loadsheet Purpose HAJJ onfiguration 08.05,A,B 02Aug Effect of Fuel ( A & 312 ) 08.05,D,E 02Aug Effect of Fuel ( A ) Mar ,8 ockpit Index, abin rew Seats, rew Distr A 07Nov Galley/Pantry Weight&codes Apr Passenger Seats Average Station (abin Areas) 08.07A 20Apr Passenger Seats Average Station (abin Areas) Mar Seating Layout ode Letters 08.08A 20Apr Seat Plan Layout JDK,JDL 08.08B 26Jan Seat Plan Layout JDM,JDN,JIH,JII Apr Seat Plan Layout HAJJ onfiguration Dec Details For ompartment Trim Apr Details For Bay/Section Trim 08.10A 03Apr Details For Bay/Section Trim Mar ,D1 D2,D3 BALLAST,G LIMITS / Ideal Trim Line, Unit Load Devices / Special Load Nov Load&Trim Sheet A ( JDN, JIH, JII ) 270 seat 08.12A 05Nov Load&Trim Sheet A ( JDL, JDM ) 270 seat 08.12B 29May Load&Trim Sheet A ( JDK ) 270 seat Oct Load&Trim Sheet A ( HAJJ onfiguration ) 331 seat 08.12D 10Sep Load&Trim Sheet A ( HAJJ onfiguration ) 331 seat AHM560 Data for heck-in & Loadcontrol Page No:08.00

2 REV NO REVISION DESRIPTION A Aug-2015 REVISION HIGHLIGHTS 78 T-JDM BW/BI changed due to weighing 77 T-JDN seatplan modified by addition of seat row T-JDM,JIH,JII seatplan modified by addition of seat row T-JDJ left THY fleet 75 T-JDN 331 seat configuration is added to AHM560 to be used when instructed 74 T-JIH BW/BI changed due to weighing 73 LM values are updated 72 T-JII BW/BI changed due to weighing 71 Separate fuel table for influence of trim tank is now available 70 T-JDM and T-JDN BW/BI changed due toweighing 69 JDL: onverted from 331 pax to 270 pax 68 JIK: onverted from 342 pax to 278 pax 67 Pantry codes are amended. New design of BW/BI page. New design of Details For Bay/Section Trim page. T-JIJ re-delivered. 66 BW/BI of JII is changed due to weighing 65 JDL: onverted from 270 pax to 331 pax and JIK: onverted from 278 pax to 342 pax 64 JDL: onverted from 331 pax to 270 pax 63 JIJ & JIK: onverted from 342 pax to 278 pax 62 JDL: onverted from 270 pax to 331 pax (Hajj configuration) 61 JIK: onverted from 278 pax to 342 pax (Hajj configuration) 60 JDJ & JDK : BW\ BI changed due to modifications 59 Pantry Standard W/I table (atering) : New stations are added 59 Weight of toolbox and taxi fuel weights are amended 59 T-JDK : BW\ BI changed due to weighing. 58 JIJ: Seat config changed to 342Y seat again to HAJJ/UMRE onfig. Several pages revised accordingly. 57 JIK : Seat onfig changed from 342Y to 278Y(26/252Y) seat again.several pages revised accordingly. 56 T-JDJ : BW\ BI changed due to weighing. 56 JIJ : Seat onfig changed from 342Y to 278Y(26/252Y) seat again.several pages revised accordingly. 56 Pantry Std W/I table : Addition of new stations 55 Pantry Std W/I table : Addition of new stations 54 JIJ & JIK: Seat onfig changed to 342Y seat again to HAJJ/UMRE onfig. Several pages revised accordingly. 53 FWD, MID, AFT average abin rew Seats Locations can be used for simplicity. abin rew Total Effect Index Table is changed on pages & 08.02A 53 Pantry codes are amended. 53 JIJ : Seat onfig changed to 278 seat again from HAJJ onfig. Several pages revised accordingly. 53 Appendix- Fuel Index Table per Tank is added 52 JIK : Seat onfig changed to 278 seat again from HAJJ onfig. Several pages revised accordingly. 51 For JIJ &JIK : Seat onfig changed to 342 seat HAJJ onfig. Several pages revised accordingly. 51 Pantry codes are amended. 51 For JIJ &JIK : Seat onfig changed to 342 seat HAJJ onfig. Several pages revised accordingly. 51 Pantry codes are amended. 50 For JDK : Increase MTWO to 260T, MZFW to 178T and MLW to 188T 49 Seat configuration of T-JIJ &JIK is amended. Row numbers and letters changed only. 49 BW/BI of JDL is amended. AHM560 Data for heck-in & Loadcontrol Page No:08.00

3 A Mar-2008 AIRRAFT DATA Sheet 2 abin onfiguration(s) A / TYPE arrier ALL A TK 2. BASI INDEX AND MA FORMULA 2.1. Examples and definitions Index 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 = Index 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 Index formula Ref.Station. at = meters from zero K (onstant) = 100 (onstant) = MA Information Length of MA = 7.27 meters LEMA at = meters/ from zero 2.4. Stabilizer Trim Setting MA Range STAB Range 18 7 Nose up 22 7 Nose up Linear variation between 22% MA and 38% MA 38 1 Nose up 42 1 Nose up AIRRAFT DATA Sheet 3 abin onfiguration(s) A / TYPE arrier ALL A TK 3. AIRRAFT REGISTRATIONS, WEIGHT AND INDEX DETAILS DRY OPERATING WEIGHT BASI WEIGHT X X A list of weight and index values for each aircraft registration is given on next page. AHM560 Data for heck-in & Loadcontrol Page No:08.01

4 A Aug-2015 A/ BASI & DRY OPERATING WEIGHT & INDEX TABLE A/c Type MSN A/ Number Basic*(crew(0/0) Reg. of Seats Weight Index A T-JDK A T-JDL A T-JDM A T-JDN A T-JIH A T-JII How to calculate DOW/DOI? Basic Weight/Index (Full potable water tank) + ockpit rew Total Weight/Index + abin rew Total Weight/Index + Pantry Weight/Index = Dry Operating Weight/Index If actual is different, then make necessary adjustments A/ Reg A/ Limitations (Kg) MTAXI JDL/JDM MTOW MLDW MZFW MTAXI JDK MTOW MLDW MZFW MTAXI JDN/JIH/JII MTOW MLDW MZFW OKPIT REW TOTAL EFFET / ockpit rew No/Locations ockpit rew No/Locations WEIGHT INDEX 2 OKPIT REW OKPIT REW OKPIT REW ABIN REW TOTAL EFFET / abin rew No/Locations abin rew No/Locations WEIGHT INDEX 8 ABIN REW (2 Fwd +4 Mid +2 Aft) ABIN REW (3 Fwd +4 Mid +2 Aft) ABIN REW (3 Fwd +5 Mid +2 Aft) ABIN REW (3 Fwd +5 Mid +3 Aft) ABIN REW (4 Fwd +5 Mid +3 Aft) ABIN REW (4 Fwd +6 Mid +3 Aft) ABIN REW (4 Fwd +6 Mid +4 Aft) PANTRY EFFET / PANTRY (ATERING) STANDARD W/I TABLE IS ON PAGE 08.02B BW/BI value in the above table already includes potable water with FULL tank (1050 kg/5.6 Index).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 262 KG / Subtract 1.4 Index Subtract 525 KG / Subract 2.8 Index Subtract 787 KG / Subtract 4.2 Index AHM560 Data for heck-in & Loadcontrol Page No:08.02

5 A Aug-2015 *Basic Wt/Index includes: ockpit & A/ Documents, Potable Water Tanks Full, Skylife Magazine, Tare empty Weight of all Trolleys & Galley Equipments (hotcup, hotjug, etc). If some items or Equipments are NOT carried make necessary adjustments. Dry Operating Weight/Index 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 = 77 KG ONTAINERS AND PALLETS (ULD-Unit Load Devices) :Tare weight of ontainers and Pallets (ULD) should NOT be included in Dry Operating weight/index.tare weight of ULD should be shown within GROSS load in position (added to net cargo/bag weight in ULD position).gross load (sum of Net cargo/bag weight + pallet/container tare weight) should be shown in "LOAD IN OMPARTMENTS" in "DISTRIBUTION" column of LOADSHEET. REW BAGGAGE (in BULK argo ompartment) : For Longhoul flights and for flights that crew stays overnight at destination, additional REW BAGGAGE, standard bag weight of 15 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. AHM560 Data for heck-in & Loadcontrol Page No:08.02

6 Pantry ode A Apr-2012 PANTRY STANDART WEIGHT/INDEX TABLE (ATERING) Galley weight TOTAL FWD MID AFT WEIGHT INDEX Destination / Departure A ER FLIGHTS N INTERNATIONAL FLIGHTS D DOMESTI FLIGHTS ONE WAY G DOMESTI FLIGHTS RETURN PANTRY REMARKS: 1- All weights are in kg. * Refer to DOW-DOI_Table-A file for several possible standard cockpit/cabin crew,pantry codes & potable water tanks fill ratio. DOI calculation Remark : During Index alculations due to DS system rounding (or truncating), approximately +/- 0.3 index difference is acceptable. AHM560 Data for heck-in & Loadcontrol Page No:08.02B

7 A Aug-2012 AIRRAFT DATA Sheet 4 abin onfiguration(s) A / TYPE arrier ALL A TK 4. LIMITATIONS 4.1. Aircraft Weight Limitations Maximum weights for: Aircraft Design Take-off Design Take-off Design MSN Ramp/Taxi Zero Fuel Reg. Wet Dry Landing T-JDK kg N/A kg * kg * kg T-JDL kg N/A kg * kg * kg T-JDM kg N/A kg * kg * kg T-JDN kg N/A kg kg kg T-JIH kg N/A kg kg kg T-JII kg N/A kg kg kg * : PLEASE NOTE THAT MAX DESIGN ZERO FUEL WEIGHT DEREASES LINEARLY TO WHEN AIRRAFT ENTER OF GRAVITY IS LESS THAN %18 MA. * : PLEASE NOTE THAT MAX DESIGN LANDING WEIGHT DEREASES LINEARLY TO WHEN AIRRAFT ENTER OF GRAVITY IS LESS THAN %31 MA 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. A : 1500 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 Index influence should be shown on Load & Trim Sheet in a suitable space under LM title preferably next to LM weight. AHM560 Data for heck-in & Loadcontrol Page No:08.03

8 A Apr-2011 AIRRAFT DATA Sheet 5 abin onfiguration(s) A / TYPE arrier ALL A TK 4.2. G - Limits for Loadsheet Purpose Special condition if applicable Special condition if applicable TAKE-OFF FWD TAKE-OFF AFT Specify applicability Weight Index Index Specify applicability Weight Value Value T-JDL,-JDM T-JDL,-JDM T-JDN,-JIH,-JII T-JDN,-JIH,-JII T-JDK T-JDK Special condition if applicable Special condition if applicable ZERO FUEL FWD ZERO FUEL AFT Specify applicability Weight Index Index Specify applicability Weight Value Value T-JDL,-JDM T-JDL,-JDM T-JDN,-JIH,-JII T-JDN,-JIH,-JII T-JDK T-JDK AHM560 Data for heck-in & Loadcontrol Page No:08.04

9 A Sep-2014 AIRRAFT DATA Sheet 5 abin onfiguration(s) A / TYPE arrier HAJJ ONFIGURATION A TK 4.2. G - Limits for Loadsheet Purpose HAJJ ONFIGURATION (331Y) Special condition if applicable Special condition if applicable TAKE-OFF FWD TAKE-OFF AFT Specify applicability Index Index Weight Specify applicability Weight Value Value A A Special condition if applicable Special condition if applicable ZERO FUEL FWD ZERO FUEL AFT Specify applicability Weight Index Index Specify applicability Weight Value Value A A HAJJ ONFIGURATION (331Y) Special condition if applicable Special condition if applicable TAKE-OFF FWD TAKE-OFF AFT Specify applicability Index Index Weight Specify applicability Weight Value Value A A Special condition if applicable Special condition if applicable ZERO FUEL FWD ZERO FUEL AFT Specify applicability Weight Index Index Specify applicability Weight Value Value A A AHM560 Data for heck-in & Loadcontrol Page No:08.04B

10 A Aug-2012 AIRRAFT DATA Sheet 6 abin onfiguration(s) A / TYPE arrier A ( T-JDL,-JDM ) A ( T-JDK ) TK 5. EFFET OF FUEL 5.1 EFFET OF FUEL - FUEL LOADING / STANDARD PROEDURE Fuel Wt. kg Fuel Density (Kg/lt) Fuel Fuel Density (Kg/lt) Wt. kg FULL If any non-standard refueling is conducted due to the refueling failures & tank system failures, fuel index values can be calculated manually by using the individual tank fuel index tables (copied from FOM ) on the page AHM A & 08.12B, with the supervision of the responsible technical stuff and commander (flight crew). AHM560 Data for heck-in &Loadcontrol Page No:08.05

11 A Aug-2012 AIRRAFT DATA Sheet 6 abin onfiguration(s) A / TYPE arrier A ( T-JDL,-JDM ) A ( T-JDK ) TK 5.2 EFFET OF FUEL Inner+Outer +enter Tanks & Trim tank seperately If DS database & loadcontroller input command allows loadcontroller to input Inner+Outer+enter Tanks & Trim Tank seperately then the tables below can be used. The amount of fuel in trim tank should be stated as SI message on electronic loadsheet. Fuel Index calculation shall be done as follows: A - Fuel quantity in each individual tank should be recorded. B - Fuel in Inner + Outer + enter tanks should be read and corresponding fuel index should be read from Inner + Outer + enter Tanks Table. - Fuel in Trim tank should be read and corresponding fuel index should be read from Trim Tank Table. D - Fuel Index found from above items B & are summed to get Total Fuel Index. Fuel Wt. Kg Inner + Outer + enter Tanks Table Fuel Density (Kg/lt) Fuel Wt. Fuel Density (Kg/lt) Kg * -59.4* * -61.3* * -62.5* * -64.8* *Max capacity AHM560 Data for heck-in &Loadcontrol Page No:08.05A

12 A Aug-2012 AIRRAFT DATA Sheet 6 abin onfiguration(s) A / TYPE arrier A ( T-JDL,-JDM ) A ( T-JDK ) TK Trim Tank Table Fuel Wt. (Kg) Index Fuel Wt. (Kg) Index * * * * VOLUMETRI APAITY (Inner Tanks + Outer Tanks + enter Tank + Trim Tank) Lt Kg (Density 0.80 Kg/Lt) INNER TANKS LT * 2 = Lt KG OUTER TANKS 3688 LT * 2 = 7376 Lt 5901 KG ENTER TANK Lt kg TRIM TANK 6121 Lt 4897 KG TOTAL Lt KG Example calculation( Density 0.8 Kg / Lt) : Individual Tank Weight Index Inner & Outer Tanks Kg Trim Tank 500 Kg 5.6 Total Fuel Kg ¹ max. fuel capacity for fuel density ² max. fuel capacity for fuel density ³ max. fuel capacity for fuel density max. fuel capacity for fuel density 0.83 AHM560 Data for heck-in & Loadcontrol Page No:08.05B

13 A Aug-2012 AIRRAFT DATA Sheet 6 abin onfiguration(s) A / TYPE arrier A ( T-JDN,-JIH,-JII ) TK 5.3 EFFET OF FUEL - FUEL LOADING / STANDARD PROEDURE Fuel Fuel Density (Kg/lt) Fuel Wt. Fuel Density (Kg/lt) Wt. kg kg FULL If any non-standard refueling is conducted due to the refueling failures & tank system failures, fuel index values can be calculated manually by using the individual tank fuel index tables (copied from FOM ) on the page AHM A & 08.12B, with the supervision of the responsible technical stuff and commander (flight crew). AHM560 Data for heck-in & Loadcontrol Page No:08.05

14 A Aug-2012 AIRRAFT DATA Sheet 6 abin onfiguration(s) A / TYPE arrier A ( T-JDN,-JIH,-JII ) TK 5.4 EFFET OF FUEL Inner+Outer +enter Tanks & Trim tank seperately If DS database & loadcontroller input command allows loadcontroller to input Inner+Outer+enter Tanks & Trim Tank seperately then the tables below can be used. The amount of fuel in trim tank should be stated as SI message on electronic loadsheet. Fuel Index calculation shall be done as follows: A - Fuel quantity in each individual tank should be recorded. B - Fuel in Inner + Outer + enter tanks should be read and corresponding fuel index should be read from Inner + Outer + enter Tanks Table. - Fuel in Trim tank should be read and corresponding fuel index should be read from Trim Tank Table. D - Fuel Index found from above items B & are summed to get Total Fuel Index. Inner + Outer + enter Tanks Table Fuel Fuel Density (Kg/lt) Fuel Wt. Fuel Density (Kg/lt) Wt. Kg Kg * -59.4* * -61.4* * -62.6* * -64.9* *Max capacity AHM560 Data for heck-in &Loadcontrol Page No:08.05D

15 A Aug-2012 AIRRAFT DATA Sheet 6 abin onfiguration(s) A / TYPE arrier A ( T-JDN,-JIH,-JII ) TK Trim Tank Table Fuel Wt. (Kg) Index Fuel Wt. (Kg) Index * * * * VOLUMETRI APAITY (Inner Tanks + Outer Tanks + enter Tank + Trim Tank) Lt Kg (Density 0.80 Kg/Lt) INNER TANKS LT * 2 = Lt KG OUTER TANKS 3650 LT * 2 = 7300 Lt 5840 KG ENTER TANK Lt kg TRIM TANK 6231 Lt 4985 KG TOTAL Lt KG Example calculation( Density 0.8 Kg / Lt) : Individual Tank Weight Index Inner & Outer Tanks Kg Trim Tank 500 Kg 5.6 Total Fuel Kg ¹ max. fuel capacity for fuel density ² max. fuel capacity for fuel density ³ max. fuel capacity for fuel density max. fuel capacity for fuel density APU / TAXI FUEL WEIGHT Due to local taxiing distances and local needs for APU running, total taxi Fuel may be different in your local station. It may be calculated by using the following fuel flow figures; Taxi Fuel Flow = 25 kg/minute APU Fuel Flow = 215 kg/hour AHM560 Data for heck-in & Loadcontrol Page No:08.05E

16 A Mar-2012 AIRRAFT DATA Sheet 7 abin onfiguration(s) A / TYPE arrier ALL A TK 6. REW 6.1. Number of cockpit crew seats and average location Length of arm from reference Maximum number of cockpit Index influence station seats +/- meter(s) +/- per 1 kg Number of cabin crew seats and location ABIN rew seats locations Max. No. of seats Length of arm from reference station Index influence +/- meter(s) +/- per 1 kg FWD MID AFT Remarks: FWD, MID, AFT average abin rew Seats Locations can be used for simplicity rew Distribution / rew ode rew ode ockpit rew Total No abin rew Total No Number of abin rews at Location FWD MID AFT 4/ / / / / / / Location of rew Baggage BULK ARGO OMPT. 5 AHM560 Data for heck-in & Loadcontrol Page No:08.06

17 A Nov-2008 AIRRAFT DATA Sheet 8 abin onfiguration(s) A / TYPE arrier A TK 7. GALLEY AND PANTRY 7.1. Galleys For T- JDK,-JDL,-JDM,-JDN,-JIH,-JII Length of arm from reference Galley locations station Index influence +/- meter(s) +/- per 1 kg G G BAR UNIT G FWD (G1+G1+BAR UNIT+G2) G G3R G3L G MID (G3+G3R+G3L+G4) G G G AFT (G5+G6+G7) Pantry Weight / Pantry ode Pantry Weight / Pantry ode is given on A/ BASI & DRY OPERATING WEIGHT & INDEX TABLE. AHM560 Data for heck-in & Loadcontrol Page No:08.06A

18 A Apr-2012 AIRRAFT DATA Sheet 8 abin onfiguration(s) A / TYPE arrier ALL A TK 7.3 SEATING ONDITIONS LOADSHEET OUTPUT STATE BELOW HOW THE SEATING ONDITIONS SHOULD BE SHOWN IN THE RESPETIVE LOADSHEET BOX. GIVE EXAMPLE. ENLOSE A PASSENGER DISTRIBUTION TABLE IF USED. A PERMANENT PASSENGER DISTRIBUTION TABLE IS NOT USED. 8. PASSENGER ABIN 8.1 Passenger Seats lass 1 : LASS ODES lass 2 : Y lass 3 : NUMBER OF SEATS Name of cabin section lass 1 lass 2 lass 3 Total per cabin section AIRRAFT DATA Sheet 9 A / TYPE arrier A TK Name of cabin section NUMBER OF SEATS lass 1 lass 2 lass 3 Total per cabin section T-JDK,-JDL,-JDM,-JDN,-JIH,-JII (270 SEATS) (331 SEATS) ABIN ONFIGURATION 34/236Y HAJJ ONFIGURATION OA OA OB OB O O Total per Total per class class AHM560 Data for heck-in & Loadcontrol Page No:08.07

19 A Apr-2012 AIRRAFT DATA Sheet 9 abin onfiguration(s) A / TYPE arrier A TK 8.2 lass/abin Sections T-JDK,-JDL,-JDM,-JDN,-JIH,-JII (270 SEATS) lass/abin Section Length of arm from reference station Index influence +/- meter(s) +/- per 1 kg OA OB O HAJJ ONFIGURATION (331 SEATS) lass/abin Section Length of arm from reference station Index influence +/- meter(s) +/- per 1 kg OA OB O AHM560 Data for heck-in & Loadcontrol Page No:08.07A

20 8.3 Seating Layout A Mar-2008 AIRRAFT DATA Sheet 10 A / TYPE arrier A 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 AHM560 Data for heck-in & Loadcontrol Page No:08.08

21 SETION ROW NO A Apr-2011 AIRRAFT DATA Sheet 11 abin onfiguration(s) A / TYPE arrier T-JDK,-JDL A TK Seatplan Layout / Facilities and Row Index Influence abin onfig. 34/236Y A B D E F G J K Length of arm from reference station INDEX INFLUENE per SEAT- ROW per1kg A B 1 NBI N. N N I. N NBI NI N. N N. N NI NI N. N I N I. N NI NI N. N I N I. N NI NI N. N I N I. N NI NI N.. N NI NBI N. N NBI NBI N. N NBI NI NM. NM NI NI NM. NM NI NI NM. NM NI NI NM. NM NI NI NM. NM N NI NM. NM NI NI NM. NM NI N NM. NM NI NI NM. NM N NI NM. NM NI NI NM. NM NI N NM. NM NI NI NM. NM N NI NM. NM NI NI NM. NM NI N NM. NM NI NI NM. NM N NI NM. NM NI NI NM. NM NI N NM. NM NI NI NM. NM N NI NM. NM NI NI NM. NM NI N NM. NM NI NI NM. NM N NI NM. NM NI NI NM. NM NI N NM. NM NI NEL NEL. N NBI NBI N. NEL NEL NI NM. NM NI N NM. NM NI NI NM. NM N NI NM. NM NI NI NM. NM NI N NM. NM NI NI NM. NM N NI NM. NM NI NI NM. NM NI N NM. NM NI NI NM. NM N NI NM. NM NI NI NM. NM NI N NM. NM NI NI NM. NM N NI NM. NM NI NI NM. NM NI N NM. NM NI NI NM. NM N NI NM. NM NI NI NM. NM NI N. NM NI NI NM. NM N N. NM NI NI NM. NM N N. NM NI NI NM. NM N N. NM NI FIXED ERTAIN LASS DIVIDER is shown as : THE AISLE is shown as :. AHM560 Data for heck-in & Loadcontrol Page No:08.08A

22 SETION ROW NO A Jan-2015 AIRRAFT DATA Sheet 11 abin onfiguration(s) A / TYPE arrier T-JDM,-JDN,-JIH,-JII A TK Seatplan Layout / Facilities and Row Index Influence abin onfig. 34/236Y A B D E F G J K Length of arm from reference station INDEX INFLUENE per SEAT- ROW per1kg A B 1 NBI N. N N I. N NBI NI N. N N. N NI NI N. N I N I. N NI NI N. N I N I. N NI NI N. N I N I. N NI NI N.. N NI NBI N. N NBI NBI N. N NBI NI NM. NM NI NI NM. NM NI NI NM. NM NI NI NM. NM NI NI NM. NM N NI NM. NM NI NI NM. NM NI N NM. NM NI NI NM. NM N NI NM. NM NI NI NM. NM NI N NM. NM NI NI NM. NM N NI NM. NM NI NI NM. NM NI N NM. NM NI NI NM. NM N NI NM. NM NI NI NM. NM NI N NM. NM NI NI NM. NM N NI NM. NM NI NI NM. NM NI N NM. NM NI NI NM. NM N NI NM. NM NI NI NM. NM NI N NM. NM NI NEL NEL. N NBI NBI N. NEL NEL NI NM. NM NI N NM. NM NI NI NM. NM N NI NM. NM NI NI NM. NM NI N NM. NM NI NI NM. NM N NI NM. NM NI NI NM. NM NI N NM. NM NI NI NM. NM N NI NM. NM NI NI NM. NM NI N NM. NM NI NI NM. NM N NI NM. NM NI NI NM. NM NI N NM. NM NI NI NM. NM N NI NM. NM NI NI NM. NM NI N. NM NI NI NM. NM N N. NM NI NI NM. NM N N. NM NI NI NM. NM N N. NM NI FIXED ERTAIN LASS DIVIDER is shown as : THE AISLE is shown as :. AHM560 Data for heck-in & Loadcontrol Page No:08.08B

23 SETION ROW NO A Apr-2012 AIRRAFT DATA Sheet 11 abin onfiguration(s) A / TYPE arrier HAJJ ONFIGURATION A TK Seatplan Layout / Facilities and Row Index Influence A B abin onfig. 331Y A B D E F G J K Length of arm from reference station INDEX INFLUENE per SEAT- ROW per1kg 1. N N N N N. N N N N. N N N N. N N N N. N N N N. N N N N. N N N N. N N N N. N N N N. N N N N. N N N N. N N N N. N N N N. N N N N. N N N N. N N N N. N N N N. N N N N. N N N N.. N N N N. N N N N. N N N N. N N N N. N N N N. N N N N. N N N N. N N N N. N N N N. N N N N. N N N N. N N N N. N N N N. N N N N. N N N N. N N N N. N N N N. N N N N. N N N N. N N N N. N N N N. N N N N. N N N N. N N N N. N N N N. N N N N. N N N N. N N N N. N N N N. N N N N. N N N N. N N N N. N N NE NE. N N N N. NE NE N N. N N N N. N N N N. N N N N. N N N N. N N N N. N N N N. N N N N. N N N N. N N N N. N N N N. N N N N. N N N N. N N N N. N N N N. N N N N. N N N N. N N N N. N N N N. N N N N. N N N N. N N N N. N N N N. N N N. N N N N. N N N. N N N N. N N N. N N N N. N N N. N N THE AISLE is shown as :. AHM560 Data for heck-in & Loadcontrol Page No:08.08

24 A Dec-2009 AIRRAFT DATA Sheet 12 abin onfiguration(s) A / TYPE arrier ALL A TK 9. DETAILS FOR OMPARTMENT TRIM For T-JDK,-JDL,-JDM,-JDN,-JIH,-JII OMPARTMENT MAXIMUM APAITY Index influence NUMBER DESRIPTION GROSS WEIGHT VOLUME* (kg) (m 3 +/- ) per 1 kg 1 FWD ARGO HOLD 1+2 MAX.UM FWD ARGO HOLD AFT ARGO HOLD 3+4 MAX.UM AFT ARGO HOLD REAR / BULK argohold Remarks: * : Volume information is given only for Bulk compartments. 9.1 ombined Load Limitations : N/A For T- JDK,-JDL,-JDM,-JDN,-JIH,-JII OMPARTMENT 1 + OMPARTMENT 2 OMPARTMENT 3 + OMPARTMENT 4 MAX UMULATIVE = KG MAX UMULATIVE = KG AHM560 Data for heck-in & Loadcontrol Page No:08.09

25 A Apr-2012 AIRRAFT DATA Sheet 13 abin onfiguration(s) A / TYPE arrier ALL A TK 10. DETAILS FOR BAY / SETION TRIM BAY / SETION DESRIPTION GROSS WEIGHT VOLUME Index influence (kg) (M 3 ) +/- per 1 kg 11 R or L AVE, AKE R or L AVE, AKE R or L AVE, AKE PLA, P9A PLA, P9A PLA, P9A P PAG P PAG P PM (96x125 inch) P PM (96x125 inch) R or L AVE, AKE R or L AVE, AKE R or L AVE, AKE R or L AVE, AKE R or L AVE, AKE R or L AVE, AKE PLA, P9A PLA, P9A PLA, P9A PLA, P9A PLA, P9A PLA, P9A P PAG (88x125 inch) P PAG (88x125 inch) P PAG (88x125 inch) P PAG (88x125 inch) P PM (96x125 inch) P PM (96x125 inch) P PM (96x125 inch) P PM (96x125 inch) AHM560 Data for heck-in & Loadcontrol Page No:08.10

26 A Apr-2012 AIRRAFT DATA Sheet 13 abin onfiguration(s) A / TYPE arrier ALL A TK 10. DETAILS FOR BAY / SETION TRIM BAY / SETION DESRIPTION GROSS WEIGHT VOLUME Index influence (kg) (M 3 ) +/- per 1 kg 31 R or L JDK/L/M/N/JIH/II Occupied by Mobile rew Rest ontainer in every flight 32 R or L AVE, AKE R or L AVE, AKE R or L AVE, AKE JDK/L/M/N/JIH/II Occupied by Mobile rew Rest ontainer in every flight 32 PLA, P9A PLA, P9A PLA, P9A P JDK/L/M/N/JIH/II Occupied by Mobile rew Rest ontainer in every flight 32P PAG P PAG P PM (96x125 in) L or R AVE, AKE L or R AVE, AKE L or R AVE, AKE PLA, P9A PLA, P9A PLA, P9A P PAG (88x125 in) P PAG(88x125 in) P PM (96x125 in) P PM (96x125 in) JDK/L/M/N/JIH/II bulk loading JDK/L/M/N/JIH/II bulk loading JDK/L/M/N/JIH/II bulk loading AHM560 Data for heck-in & Loadcontrol Page No:08.10A

27 11. BALLAST FIXED PROVISIONS FOR ARRYING BALLAST? REMARKS : BALLAST IS NOT REQUIRED A Mar-2008 AIRRAFT DATA Sheet 14 A / TYPE arrier A TK D AIRRAFT DATA Sheet 1 A / TYPE arrier A 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 Fuel 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 D AIRRAFT DATA Sheet 2 A / TYPE arrier A TK Maximum apacity Type Tare Gross VOLUME ode weight Weight (M 3 ) Remarks AVE x61.5 in.half-size container V3(LD3) AKE x61.5 in. half-size container V3(LD3) PLA x125 inch size pallet (W2) P9A x125 inch size pallet (W2) PAG x125 inch size pallet (A2) PM x125 inch size pallet (Q2) NOTES : - GROSS WEIGHT includes tare weight of pallets, containers, nets and igloo - GROSS WEIGHT is valid for only the aircraft type A UNIT LOAD DEVIES NOTES In ULD compartments (compartments other than bulk ompartment) cargo and bags should be loaded only in ULD.Do not load anything at the empty spaces around ULDs and between ULDs. D AIRRAFT DATA Sheet 3 A / TYPE arrier A TK 3. SPEIAL LOAD Turkish Airlines & IATA regulations apply. When necessary contact Turkish Airlines Station Manager. AHM560 Data for heck-in & Loadcontrol Page No:08.11