A May-2018 IATA AHM560 DATA LIST OF EFFECTIVE PAGES REV 57

Transcription

1 A May-2018 IATA AHM560 DATA LIST OF EFFETIVE PAGES REV 57 Pages/Sheets that are common to all A/ Types. Located in.pdf file "THY-AHM560_FOREWORD.pdf" ATION ISSUE REV SHEET PAGE NO FOR PAGE DESRIPTION DATE NO NO PAGES Title Page ontents Jan General Info Jan A1,A2 ontact Address Jan B1,B2 Passenger & baggage weights/ crew weights Jan DOW and DOI specifications / Special Information Jan Load&Trim Sheet Information May18 - Updated - List Of Eff. Pages, Revision Highlights Sep ,3 Basic and MA formula, Stabilizer Trim Settings, A/ Registration., Wt Details May18 - Updated - A/ Basic & Dry Operating Weight & Table 05.02A 28May A/ Basic & Dry Operating Weight & Table Dec Pantry odes 05.03A 04Aug Aircraft Weight Limitations May G Limits for Loadsheet Purpose 05.04A 28May G Limits for Loadsheet Purpose A-B 02Aug Effect of Fuel - Fuel Density Oct ockpit, abin rew Seats,rew Distr May Galley/Pantry Weight&odes May ,10 Passenger Seats Average Station (abin Areas) 05.08A 22 May ,10 Passenger Seats Average Station (abin Areas) Sep Seating Layout ode Letters Jun Seat Plan Layout - T-JNH,IJKLMNOPRSTZ,- JOA,B,,D,E,F,G;H,I, -LN,-LND,-LNE,-LNF 05.10A 22Apr Seat Plan Layout - T-JOM, 05.10B 22 May Seat Plan Layout - T - LOB May Details For ompartment Trim Sep Details For Bay/Section Trim 05.12A 22 May Details For Bay/Section Trim Sep ,D1 BALLAST,G LIMITS / Ideal Trim Line, Unit Load Devices / D2,D3 Special Load Sep Load&Trim Sheet T-JNH,I,J,K,L,M,N,O,P,R 05.14A 11Nov Load&Trim Sheet T-JNS,T,Z,JOA,-B,-,-D,-E,-F,-G,-H,-I,-J,-K,- JOL,-LN,-LND Sep Appendix- Fuel Table per Tank Page No:05.00

2 REV NO REVISION DESRIPTION 57 T-JOJ BW/BI changed due to weighing. 56 T-JNM BW/BI changed due to weighing 55 T-JOF BW/BI changed due to weighing 54 T-JNH,T-JNL BW/BI changed due to weighing 53 T-JNS BW/BI changed due to weighing 52 T-JNI,-JNJ BW/BI changed due to weighing 51 T-JOA BW/BI changed due to weighing 50 T-JNH, -JNI, -JNT BW/BI changed due to weighing. 49 New cabin location added A May-2018 REVISION HIGHLIGHTS 48 T-JOB BW/BI changed due to weighing. 47 LM values are updated. 46 T-LOF and T-LOG certifed limits changed. 45 T-LOB New Aircraft. 44 T-JNZ BW/BI changed due to weighing. 43 T-LOG New Aircraft. 42 T-LOD New Aircraft. 41 T-LO New Aircraft. 40 T-LOA New Aircraft, T-LOE,T-LOF BW/BI changed due to engineering order. 39 T-LOF New Aircraft,T-LOE BW/BI changed due to engineering order. 38 T-LOE New Aircraft joined THY fleet, T-JNH BW/BI changed due to engineering order. 37 T-LNG New Aircraft 36 T-LNF New Aircraft 35 T-LNE New Aircraft. T-JO left THY fleet. 34 T-LND New A/ joined THY fleet. T-LN BW/BI changed due to modification. 33 T-JNO BW/BI changed due to weighing 32 T-JNR BW/BI changed due to weighing 31 T-LN New A/ 30 T-JNP BW/BI changed due to weighing 29 T-JOK New Aircraft 28 T-JOJ and T-JOL New Aircrafts. 27 T-JOI and T-JOM New Aircrafts, Pantry weight s changed 26 T-JOH New Aircraft 25 T-JOG New Aircraft 24 T-JOF new aircraft 23 T-JNL BW/BI changed due to weighing 22 T-JNJ seatplan modified by addition of seat row T-JOE new aircraft 21 T-JNI,JNK,JNM,JNO,JNT seatplan modified by addition of seat row T-JNH,JNI,JNJ,JNK,JNM,JNN BW/BI changed due to weighing or modification 20 T-JNH,JNL,JNN,JNP,JNR,JNS seatplan modified by addition of seat row T-JOD new aircraft 18 T-JO new aircraft 17 T-JOB new aircraft 16 T-JOA new aircraft 15 T-JNH,JNI BW/BI changed due to weighing 14 T-JNZ entered THY fleet. 13 T-JNS,JNT entered THY fleet. 12 LM values are updated 11 Seperate fuel table for influence of trim tank is now available 10 T-JNR entered THY fleet. Page No:05.00

3 09 T-JNP entered THY fleet. REV NO REVISION DESRIPTION 08 T-JNO entered THY fleet. 08 All pantry codes are amended. New design of BW/BI page. A May JNI,JNJ,JNK,JNL,JNM,JNN : Basic Weight / amendment due to modifications 07 Pantry Standard W/I table (atering) : New stations are added 07 Weight of toolbox and taxi fuel weights are amended 06 T-JNN entered THY fleet. 05 T-JNL entered THY fleet. 04 T-JNM entered THY fleet. 03 Fuel Table per Tank is added on page FWD, MID, AFT average cabin crew seats locations can be used for simplicity. abin crew total effect index table on page is changed. 02 T-JNK entered THY fleet. 02 T-JNJ entered THY fleet. 01 T-JNI entered THY fleet. Page No:05.00

4 A Sep-2010 Sheet 2 abin onfiguration(s) A / TYPE arrier ALL A TK 2.BASI INDEX AND MA FORMULA 2.1. Examples and definitions % MA W Station Ref.Station K I MA LEMA W (Station Ref.Sta.) K ( (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 = 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 16 7 Nose up 21 7 Nose up Linear variation between 21% MA and 35% MA 35 0 Nose down 41 0 Nose down Sheet 3 abin onfiguration(s) A / TYPE arrier ALL A 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:05.01

5 A A/ BASI & DRY OPERATING WEIGHT & INDEX TABLE 21-May-2018 A/ Type MSN A/ Number Basic*(crew(0/0) How to calculate DOW/DOI? Reg. of Seats Weight Basic Weight/ A T-JNH (Full potable water tank) A T-JNI A T-JNJ ockpit rew Total Weight/ A T-JNK A T-JNL abin rew Total Weight/ A T-JNM A T-JNN Pantry Weight/ A T-JNO = A T-JNP Dry Operating Weight/ A T-JNR If actual is different, then make A T-JNS necessary adjustments A T-JNT A/ Reg. A/ Limitations A T-JNZ MTAXI KG A T-JOA MTOW KG T-JNH,,-JNR A T-JOB MLDW KG A T-JOD MZFW KG A T-JOE MTAXI KG T-JNS,-JNT,-JNZ A T-JOF MTOW KG,-JOA,,,-JOL, A T-JOG MLDW KG A T-JOH MZFW KG A T-JOI A T-JOJ MTAXI KG T-JOM A T-JOK MTOW KG Dynamic A T-JOL MLDW KG Payload A T-JOM MZFW KG 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 + 4 Mid + 3 Aft) ABIN REW (3 Fwd + 4 Mid + 4 Aft) PANTRY EFFET / Pantry ode / lass, onfig, App. (PANTRY (ATERING) STANDARD W/I TABLE IS ON PAGE 05.03) BW/BI value in the above table already includes potable water with FULL tank (700 kg/2.7 ).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 175 KG / Subtract 0.7 Subtract 350 KG / Subract1.3 Subtract 525 KG / Subtract 2.0 TOOLKIT BOX = 58 KG ONTAINERS AND PALLETS (ULD-Unit Load Devices) : - Tare weight of ontainers and Pallets (ULD) should NOT be included in Dry Operating weight/. - 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 Long-haul 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. * 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 alculations due to DS system rounding (or truncating), approximately +/- 0.3 index difference is acceptable Page No:05.02

6 A A/ BASI & DRY OPERATING WEIGHT & INDEX TABLE A/ Type MSN A/ Number Basic*(crew(0/0) Reg. of Seats Weight A T-LN A T-LND A T-LNE A T-LNF A T-LNG May-2017 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 MTOW KG T-LN,-LNG MLDW KG MZFW KG MTAXI KG T-LOA,LOB,-LO, -LOD,T-LOE,- A T-LOA A T-LOB MTOW KG A T-LO LOF,-LOG MLDW KG A T-LOD MZFW KG A T-LOE A T-LOF A T-LOG 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 + 4 Mid + 3 Aft) ABIN REW (3 Fwd + 4 Mid + 4 Aft) BW/BI value in the above table already includes potable water with FULL tank (700 kg/2.7 ).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 175 KG / Subtract 0.7 Subtract 350 KG / Subract1.3 Subtract 525 KG / Subtract 2.0 *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 = 58 KG ONTAINERS AND PALLETS (ULD-Unit Load Devices) : - Tare weight of ontainers and Pallets (ULD) should NOT be included in Dry Operating weight/. - 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 Long-haul 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. * 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 alculations due to DS system rounding (or truncating), approximately +/- 0.3 index difference is acceptable. Page No:05.02A

7 A May-2016 PANTRY STANDART WEIGHT/INDEX TABLE (ATERING) Pantry ode 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. Page No:05.03

8 A Aug2017 Sheet 4 abin onfiguration(s) A / TYPE arrier ALL A TK 4. LIMITATIONS 4.1. Aircraft Weight Limitations Maximum weights for: Aircraft Design Takeoff Wet * Dry Landing Design Take-off Design MSN Ramp/Taxi Reg. Zero Fuel T-JNH T-JNI T-JNJ T-JNK T-JNL T-JNM T-JNN T-JNO T-JNP T-JNR T-JNS T-JNT T-JNZ T-JOA T-JOB T-JO T-JOD T-JOE T-JOF T-JOG T-JOH T-JOI T-JOJ T-JOK T-JOL T-JOM T-LN T-LND T-LNE T-LNF T-LNG T-LOA T-LOB T-LO T-LOD T-LOE T-LOF T-LOG * Valid for Take-off with injection water 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 : 1000 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:05.03A

9 A May-2017 Sheet 5 abin onfiguration(s) A / TYPE arrier ALL A TK 4.2. G - Limits for Loadsheet Purpose Take-off G - Limits T-JNH,-JNI,-JNJ,-JNK,-JNL,- JNM,-JNN,-JNO,-JNP,-JNR TAKE-OFF FWD TAKE-OFF AFT T-JNS,-JNT,-JNZ,-JOA, JOB,-JO,-JOD,-JOE,-JOF, JOG,-JOH,-JOI,-JOJ,-JOK, JOL,-LN,-ND,-NE,-NF,-NG TAKE-OFF FWD TAKE-OFF AFT T-JNH,-JNI,-JNJ,-JNK,-JNL, JNM,-JNN,-JNO,-JNP,-JNR T-JNS,-JNT,-JNZ,-JOA,-JOB,- JO,-JOD,-JOE,-JOF,-JOG,- JOH,-JOI,-JOJ,-JOK,-JOL,- LN,-ND,-NE,-NF,-NG TAKE-OFF FWD TAKE-OFF AFT T-LOA,-LOB,-LO,-LOD ,-LOE,-LOF,-LOG T-LOA,-LOB,-LO,-LOD,-LOE,-LOF,-LOG TAKE-OFF FWD TAKE-OFF AFT T-JOM T-JOM Page No:05.04

10 A Aug2017 Sheet 5 abin onfiguration(s) A / TYPE arrier ALL A TK Zero-Fuel G Limits T-JNH,-JNI,-JNJ,-JNK,-JNL,- JNM,-JNN,-JNO,-JNP,-JNR ZERO FUEL FWD ZERO FUEL AFT T-JNS,-JNT,-JNZ,-JOA, JOB,-JO,-JOD,-JOE,-JOF, JOG,-JOH,-JOI,-JOJ,-JOK, JOL,-LN,-ND,-NE,-NF,-NG ZERO FUEL FWD ZERO FUEL AFT T-JNH,-JNI,-JNJ,-JNK,-JNL, JNM,-JNN,-JNO,-JNP,-JNR T-JNS,-JNT,-JNZ,-JOA,-JOB,- JO,-JOD,-JOE,-JOF,-JOG,- JOH,-JOI,-JOJ,-JOK,-JOL,- LN,-ND,-NE,-NF,-NG ZERO FUEL FWD ZERO FUEL AFT T-LOA,-LOB,-LO,-LOD ,-LOE,-LOF,-LOG T-LOA,-LOB,-LO,-LOD,-LOE,-LOF,-LOG ZERO FUEL FWD ZERO FUEL AFT , , T-JOM ,38 T-JOM , ,32 Trim Sheet in a suitable space under LM title preferably next to LM weight. Page No:05.04A

11 A May-2017 Sheet 5 abin onfiguration(s) A / TYPE arrier ALL A TK Landing G - Limits Landing G FWD Landing G AFT T-JNH,-JNI,-JNJ,-JNK,-JNL,- JNM,-JNN,-JNO,-JNP,-JNR T-JNH,-JNI,-JNJ,-JNK,-JNL,- JNM,-JNN,-JNO,-JNP,-JNR T-JNS,-JNT,-JNZ,-JOA,-JOB,- JO,-JOD,-JOE,-JOF,-JOG,- JOH,-JOI,-JOJ,-JOK,-JOL,- LN,-ND,-NE,-NF,-NG Landing G FWD Landing G AFT T-JNS,-JNT,-JNZ,-JOA, JOB,-JO,-JOD,-JOE,-JOF, JOG,-JOH,-JOI,-JOJ,-JOK,- JOL,-LN,-ND,-NE,-NF,-NG Landing G FWD Landing G AFT T-LOA,-LOB,-LO,-LOD ,-LOE,-LOF,-LOG T-LOA,-LOB,-LO,-LOD,-LOE,-LOF,-LOG Landing G FWD Landing G AFT T-JOM T-JOM Page No:05.04B

12 A Aug-2012 Sheet 6 abin onfiguration(s) A / TYPE arrier ALL A TK 5. EFFET OF FUEL -FUEL LOADING STANDARD PROEDURE 5.1 EFFET OF FUEL Fuel Wt. kg INNER TANKS + OUTER TANKS + TRIM TANK Fuel Density (Kg/lt) Fuel Wt. Fuel Density (Kg/lt) kg Page No:05.05

13 Fuel Wt. kg A Aug-2012 Fuel Density (Kg/lt) Fuel Wt. Fuel Density (Kg/lt) kg FULL 40.7 **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 , with the supervision of the responsible technical stuff and commander (flight crew). 5.2 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 Page No:05.05

14 A Aug-2012 Sheet 5 abin onfiguration(s) A / TYPE arrier A TK 5.3 EFFET OF FUEL Inner+Outer Tanks & Trim tank seperately If DS database & loadcontroller input command allows loadcontroller to input inner+outer tanks 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 calculation shall be done as follows: A - Fuel quantity in each individual tank should be recorded. B - Fuel in Inner + Outer tanks should be read and corresponding fuel index should be read from Inner + Outer Tanks Table. - Fuel in Trim tank should be read and corresponding fuel index should be read from Trim Tank Table. D - Fuel found from above items B & are summed to get Total Fuel. -Note that there is NO ENTER TANK. Fuel Wt. Kg Inner + Outer Tanks Table Fuel Density (Kg/lt) Fuel Wt. Fuel Density (Kg/lt) Kg Page No:05.05A

15 A Aug-2012 Sheet 5 abin onfiguration(s) A / TYPE arrier A TK 5.3 EFFET OF FUEL Inner+Outer Tanks & Trim tank seperately Trim Tank Table Fuel Wt. (Kg) Fuel Wt. (Kg) ¹ ² ³ VOLUMETRI APAITY (Inner Tanks + Outer Tanks + Trim Tank) Lt Kg (Density 0.80 Kg/Lt) INNER TANKS LT * 2 = Lt KG OUTER TANKS 3650 LT * 2 = 7300 Lt 5840 KG TRIM TANK 6230 Lt 4984 KG TOTAL Lt KG Example calculation (Density 0.8 Kg / Lt) : Individual Tank Weight 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 Page No:05.05B

16 A Oct-2017 Sheet 7 abin onfiguration(s) A / TYPE arrier ALL A 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 +/- meter(s) +/- per 1 kg Number of cabin crew seats and location Length of arm from ABIN rew seats Max. influence reference station locations No. of seats +/- meter(s) +/- per 1 kg FWD MID AFT ABIN rew seats locations Max. Length of arm from influence No. of seats reference station SEATS +/- meter(s) +/- per 1 kg FWD* 3-24,125-0,00965 MID* 4-3,475-0,00139 AFT* , ,00908 *Its valid only for T-LOA,-LOB,-LO,-LOD,-LOE,-LOF,-LOG 6.3. rew Distribution / rew ode rew ode ockpit rew Total No abin rew Total No Number of abin rews at Location FWD MID AFT 2/ / / / / / / / / / / / / / / / / / / Location of rew Baggage BULK ARGO OMPT. 51 Page No:05.06

17 7. GALLEY AND PANTRY 7.1. Galleys For JNH JOK,-JOL,-LN,-LND,-LNE,-LNF,-LNG For JOM A May-2017 Sheet 8 A / TYPE arrier A TK Galley locations Length of arm from reference station influence +/- meter(s) +/- per 1 kg FWD MID AFT Galley locations Length of arm from reference station influence +/- meter(s) +/- per 1 kg FWD MID AFT For T- LOE,- LOA,-LO,-LOD, LOF,-LOG,-LOB Galley locations Length of arm from reference station influence +/- meter(s) +/- per 1 kg FWD MID AFT Pantry Weight / Pantry ode Pantry Weight / Pantry ode is given on A/ BASI & DRY OPERATING WEIGHT & INDEX TABLE. Page No:05.07

18 A May-2017 Sheet 9 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 ODES lass 1 : lass 2 : Y lass 3 : - Sheet 10 A / TYPE arrier A TK T-JNH,-I,-J,-K,-L,-M,-N,-O,-P,-R,-S,-T,-JNZ,-JOA,-B,-,-D,-E,-F,-G,-H,-I,-J,-K,-L,-LN,-ND,-NE,-NF,-NG NUMBER OF SEATS Total NUMBER OF SEATS Total Name of Name of per per cabin lass lass lass cabin lass lass lass cabin cabin section section section section ABIN ONFIGURATION 289Y ABIN ONFIGURATION 28/261Y OA OA OB OB O O Total per Total per 289 class class T-JOM Name of cabin section NUMBER OF SEATS lass 1 lass 2 lass 3 Total per cabin section Name of cabin section NUMBER OF SEATS lass 1 lass 2 lass 3 Total per cabin section ABIN ONFIGURATION 291Y ABIN ONFIGURATION 28/263Y OA OA OB OB O O Total per Total per 291 class class T-LOA,-LOB,-LO,-LOD,-LOE, -LOF, -LOG NUMBER OF SEATS Total Name of per cabin lass lass lass cabin section section Name of cabin section NUMBER OF SEATS lass 1 lass 2 lass 3 Total per cabin section ABIN ONFIGURATION 305Y ABIN ONFIGURATION 40/265Y OA OA OB OB O O Total per Total per 305 class class Page No:05.08

19 A May-2017 Sheet 10 A / TYPE arrier A TK 8. PASSENGER ABIN 8.2 lass/abin Sections T-JNH,-I,-J,-K,-L,-M,-N,-O,-P,-R,-S,-T,-JNZ,-JOA,-B,-,-D,-E,-F,-G,-H,-I,-J,-K,-L,-LN-ND,-NE,-NF,-NG lass/abin Section Length of arm from H.Arm reference station influence +/- meter(s) meter(s) +/- per 1 kg OA OB O T-JOM +/- meter(s) meter(s) +/- per 1 kg OA OB O T-LOA,-LOB,-LO,-LOD,-LOE, -LOF, -LOG +/- meter(s) meter(s) +/- per 1 kg OA OB O Page No:05.08A

20 A Sep-2010 Sheet 11 A / TYPE arrier A TK 8.3 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 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 Practice Page No:05.09

21 SETION ROW NO A June-2016 Sheet 11 abin onfiguration(s) A / TYPE arrier T-JNH,I,J,K,L,M,N,O,P,R,S,T,Z, -JOA,B,,D,E,F,G,-H,-I,-J,-K,-L,-LN- LND,-LNE,-LNF,-LNG A TK Seatplan Layout / Facilities and Row Influence abin onfig. 28/261Y A B D E F G J K Length of arm from reference station Influence per Seat-Row per1kg 1 NBI NI. NI N. NI NBI NI N. NI N. N NI A 3 NI N. NI N. N NI NI N. NI N. N NI NI N.. N NI NI NBI. N NBI NBI N. NBI NI NI N. N N NI N. N NI NI N. N N NI N. N NI NI N. N N NI N. N NI NI N. N N NI N. N NI NI N. N N NI N. N NI NI N. N N NI N. N NI NI N. N N NI N. N NI B 14 NI N. N N NI N. N NI NI N. N N NI N. N NI NI N. N N NI N. N NI NI N. N N NI N. N NI NI N. N N NI N. N NI NI N. N N NI N. N NI NI N. N N NI N. N NI NI N. N N NI N. N NI NI N. N N NI N. N NI N NI NE NE. N NBI NBI N. NE NE NI N. N N NI N. N NI NI N. N N NI N. N NI NI N. N N NI N. N NI NI N. N N NI N. N NI NI N. N N NI N. N NI NI N. N N NI N. N NI NI N. N N NI N. N NI NI N. N N NI N. N NI NI N. N N NI N. N NI NI N. N N NI N. N NI NI N. N NI N N. N NI NI N. N NI N. N NI NI N. N NI N. N NI NI N. N NI N. N NI N NI N N NI N FIXED ERTAIN LASS DIVIDER is shown as : THE AISLE is shown as : Page No:05.10

22 SETION ROW NO A Apr-2015 Sheet 11 abin onfiguration(s) A / TYPE arrier T-JOM A TK Seatplan Layout / Facilities and Row Influence abin onfig. 28/263Y A B D E F G J K Length of arm from reference station Influence per Seat-Row per1kg 1 NBI NI. NI N. NI NBI NI N. NI N. N NI A 3 NI N. NI N. N NI NI N. NI N. N NI NI N.. N NI NBI NI. N N N N. NI NBI NI N. N N NI N. N NI NI N. N N NI N. N NI NI N. N N NI N. N NI NI N. N N NI N. N NI NI N. N N NI N. N NI NI N. N N NI N. N NI NI N. N N NI N. N NI B 19 NI N. N N NI N. N NI NI N. N N NI N. N NI NI N. N N NI N. N NI NI N. N N NI N. N NI NI N. N N NI N. N NI NI N. N N NI N. N NI NI N. N N NI N. N NI NI N. N N NI N. N NI NI N. N N NI N. N NI N N NI N N NBI NBI N NE NE. N N NI N. NE NE NI N. N N NI N. N NI NI N. N N NI N. N NI NI N. N N NI N. N NI NI N. N N NI N. N NI NI N. N N NI N. N NI NI N. N N NI N. N NI NI N. N N NI N. N NI NI N. N N NI N. N NI NI N. N N NI N. N NI NI N. N NI N N. N NI NI N. N NI N. N NI NI N. N NI N. N NI NI N. N NI N. N NI NI N. N NI N. NI N N NI N FIXED ERTAIN LASS DIVIDER is shown as Page No:05.10A

23 SETION ROW NO A May-2017 Sheet 11 abin onfiguration(s) A / TYPE arrier T-LOA,-LOB-LO,-LOD,-LOE,-LOF,-LOG A TK Seatplan Layout / Facilities and Row Influence abin onfig. 40/265Y A B D E F G J K Length of arm from reference station Influence per Seat-Row per1kg 1 NBI NI. NI N. NI NBI NI N. NI N. N NI NI N. NI N. N NI A 4 NI N. NI N. N NI NI N. NI N. N NI NI N. NI N. N NI NI N. NI N NI NI. NI NI NI NI. NI NI NI N. N N NI N. N NI NI N. N N NI N. N NI NI N. N N NI N. N NI NI N. N N NI N. N NI NI N. N N NI N. N NI NI N. N N NI N. N NI NI N. N N NI N. N NI NI N. N N NI N. N NI B 17 NI N. N N NI N. N NI NI N. N N NI N. N NI NI N. N N NI N. N NI NI N. N N NI N. N NI NI N. N N NI N. N NI NI N. N N NI N. N NI NI N. N N NI N. N NI NI N. N N NI N. N NI NI N.. N NI NI N N NI NI NBI NBI NI NIE NE. N N NI N. NE NIE NI N. N N NI N. N NI NI N. N N NI N. N NI NI N. N N NI N. N NI NI N. N N NI N. N NI NI N. N N NI N. N NI NI N. N N NI N. N NI NI N. N N NI N. N NI NI N. N N NI N. N NI NI N. N N NI N. N NI NI N. N NI N N. N NI NI N. N NI N. N NI NI N. N NI N. N NI NI N. N NI N. N NI N NI N. NI N N NI N FIXED ERTAIN LASS DIVIDER is shown as THE AISLE is shown as : Page No:05.10B

24 A May-2017 Sheet 12 abin onfiguration(s) A / TYPE arrier ALL A TK 9. DETAILS FOR OMPARTMENT TRIM OMPARTMENT MAXIMUM APAITY 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 argo Hold T-LOA,-LOB,-LO,-LOD,-LOE, -LOF, -LOG OMPARTMENT MAXIMUM APAITY 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 argo Hold Remarks: * : Volume information is given only for Bulk compartments. 9.1 ombined Load Limitations: N/A OMPARTMENT 1 + OMPARTMENT 2 OMPARTMENT 3 + OMPARTMENT 4 MAX UMULATIVE = KG MAX UMULATIVE = KG Page No:05.11

25 A Sep-2010 Sheet 13 abin onfiguration(s) A / TYPE arrier ALL A TK 10. DETAILS FOR BAY / SETION TRIM BAY / SETION DESRIPTION GROSS WEIGHT(kg) VOLUME (M 3 ) H.Arm influence (mt) +/- per 1 kg 11 L or R AVE, AKE L or R AVE, AKE L or R AVE, AKE PLA, P9A PLA, P9A PLA, P9A P PAG P PAG P PM P PM L or R AVE, AKE L or R AVE, AKE L or R AVE, AKE L or R AVE, AKE L or R AVE, AKE L or R AVE, AKE PLA, P9A PLA, P9A PLA, P9A PLA, P9A PLA, P9A PLA, P9A P PAG P PAG P PAG P PAG P PM P PM P PM P PM REMARKS: -PAG and PM pallet index influences are equalized by averaging original influences. This allowed to minimize the number of Hold versions. Page No:05.12

26 JOM LOE-LOF- LOA LO,LOD,- LOG- LOB A May-2017 Sheet 13 abin onfiguration(s) A / TYPE arrier ALL A TK 10. DETAILS FOR BAY / SETION TRIM BAY / SETION DESRIPTION GROSS WEIGHT(kg) VOLUME (m 3 ) H.Arm influence (mt) +/- per 1 kg 31 L or R. AVE, AKE PLA, P9A P PAG , P PM L or R AVE, AKE L or R AVE, AKE L or R AVE, AKE PLA, P9A PLA, P9A PLA, P9A P PAG P PAG P PM P * PM L or R AVE, AKE L or R AVE, AKE L or R AVE, AKE PLA, P9A PLA, P9A PLA, P9A P PAG P PAG P PM P PM REMARKS: * With 96 X 125 in (PM) ULD loaded on position 33P, positions 32P and 41P have to remain unoccupied or loaded with 88 X 125 in ULDs. * * Positions 31R, 31L, 31, 31P are occupied by Lower Deck Mobile rew rest (LDMR) container in every flight. So these positions are not available for loading and they are not given in above table. (valid for only T-JNH,I,J,K,L,M,N,O,P,R,S,T,Z,-JOA,B,,D,E,F,G,-H,-I,-J,-K,-L) - PAG and PM pallet index influences are equalized by averaging original influences. This allowed to minimize the number of hold versions. 10. UNSYMMETRIAL LOAD LIMITATIONS N/A Page No:05.12A

27 11. BALLAST FIXED PROVISIONS FOR ARRYING BALLAST? REMARKS: BALLAST IS NOT REQUIRED A Sep-2010 Sheet 14 A / TYPE arrier A TK D 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 A/ TYPE 2. UNIT LOAD DEVIES DETAILS D Sheet 2 arrier A TK Maximum apacity Type Tare Gross VOLUME ode weight Weight (M 3 ) Remarks AVE x61.5in.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 Sheet 3 A / TYPE arrier A TK 3. SPEIAL LOAD Turkish Airlines & IATA regulations apply. When necessary contact Turkish Airlines Station Manager. Page No:05.13