B777F 06-Apr-2018 IATA AHM560 DATA LIST OF EFFECTIVE PAGES REV 02

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1 B777F 06-Apr-2018 IATA AHM560 DATA LIST OF EFFETIVE PAGES REV 02 Pages/Sheets that are common to all A/ Types. Located in.pdf file "THY-AHM560_Pages_ pdf" ATION PAGE ISSUE SHEET REV NO FOR PAGE DESRIPTION NO DATE 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 Apr18 02 hanged - List Of Eff. Pages Dec ,3 Basic Index and MA formula/ Stabilizer Trim Settings/A/ Registration., Wt Index Details Dec A/ Basic & Dry Operating Weight & Index Table Dec Aircraft Weight Limitations Dec G Limits for Loadsheet Purpose 22.04A 01Dec G Limits for Loadsheet Purpose 22.04B 01Dec G Limits for Loadsheet Purpose Dec G Limits for Loadsheet Purpose Dec Effect of Fuel - Fuel Density Dec ockpit Index,abin rew Seats,rew Distr Dec Galley Weight&odes Dec ,10 Passenger Seats Average Station (abin Areas) Dec Seating Layout ode Letters Dec Seat Plan Layout, Facilities & Row index Influence Dec Details For ompartment Trim Dec Details For Bay/Section Trim 22.12a 01Dec Details For Bay/Section Trim 22.12b 01Dec Details For Bay/Section Trim 22.12c 01Dec Details For Bay/Section Trim 22.12d 01Dec Details For Bay/Section Trim 14,D1 BALLAST,G LIMITS / Ideal Trim Line, Unit Load Dec D2,D3 Devices / Special Load Dec Load&Trim Sheet A F (argo) front side 22.14A 01Dec Load&Trim Sheet A F (argo) reverse side Page No:22.00

2 B777F 06-Apr-2018 REVISION NOTES: REV NO REVISION DESRIPTION 02 Ideal G Line has been added.. 01 T-LJM joined to THY Fleet. Page No:22.00

3 EDP-SYSTEM Sheet 2 abin onfiguration(s) A / TYPE arrier 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 = 1258 inch from zero K (onstant) = 50 (onstant) = MA Information Length of MA = inch LEMA at = inch/ from zero 2.4. Stabilizer Trim Setting 777F stabilizer trim settings are based on the sum of the selected derate thrust reduction and percentage of assumed temperature thrust reduction. Since it is not possible to determine the percentage of assumed temperature thrust reduction from the data provided to pilots or dispatchers, the only accurate source for stabilizer trim settings is the FM. MA Range STAB Range EDP-SYSTEM Sheet 3 abin onfiguration(s) A / TYPE arrier 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. Page No:22.01

4 T-LJL B777F 18-Dec-2017 A/ BASI & DRY OPERATING WEIGHT & INDEX TABLE A/ Type MSN A/ Reg. Basic*(crew(0/0) Weight Index B777F T-LJL B777F T-LJM How to calculate DOW/DOI? Basic Weight/Index (Full potable water) + 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 & WV TYPE A/ Limitations (Kg) MTAXI MTOW MLDW MZFW OKPIT REW TOTAL EFFET / ockpit rew No / Locations ockpit rew No/Locations WEIGHT INDEX 2 OKPIT REW OKPIT REW OKPIT REW LOADMASTER TOTAL EFFET / Loadmaster No / Locations WEIGHT INDEX 1 (Loadmaster or Technician) (Loadmaster or Technician) (Loadmaster or Technician) (Loadmaster or Technician) PANTRY EFFET / Pantry ode / lass, onfig, App. WEIGHT INDEX N (International Freighter Flight / Short-Mid Range) Galley@266 (B.Arm) A (ER Freighter Flight / Long Range) INFLUENE OF POTABLE WATER ON DOW/DOI BW/BI value in the above table already includes potable water with FULL tank (156kg / -0.3 Index). If potable water tanks are different, adjust DOW &DOI in proper ratios. %75 POTABLE WATER %50 POTABLE WATER %25 POTABLE WATER Subtract 39 KG / Add 0.1 Index Subtract 78 KG / Add 0.1 Index Subtract 117 KG / Add 0.2 Index *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, Technician KIT, Loadmaster KIT. heck if they are carried, make necessary adjustments. Toolkit box and Technician KIT are loaded in argo comp5. Loadmaster KIT carried in pax.compt.. TOOLKIT BOX = 58,3kg / 0,2iu Technician Kit = 35kg / 0,1 iu Loadmaster KIT = 10kg / 0 iu 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 calculated in consideration of rew Baggage loading position. Spare Wheel&Tire Weight Index Dry Operating Weight/Index does not include nose/main gear spare Nose Gear(NG) (Qty1) in ompt wheel&tire.heck if they are carried in cargo compartment. It should Main Gear(MG) (Qty1) in ompt be shown as Load in compartments (distribution) on loadsheet as TOTAL in Bulk ompt.5 : Equipment in compartment Page No:22.02

5 B777F 18-Dec-2017 Sheet 4 abin onfiguration(s) A / TYPE arrier 4. LIMITATIONS 4.1. Aircraft Weight Limitations Maximum weights for: Aircraft Design Takeoff Wet * Dry Landing Design Take-off Design MSN Ramp/Taxi Zero Fuel Reg. T-LJL T-LJM 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. 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. Page No:22.03

6 EDP-SYSTEM Sheet 5 abin onfiguration(s) A / TYPE arrier - B777F TK 4.2. G - Limits for Loadsheet Purpose Special condition if applicable Specify applicability All TAKE-OFF FWD Weight Index Value Special condition if applicable Specify applicability All ZERO FUEL FWD Weight Index Value Special condition if applicable Specify applicability All TAKE-OFF AFT Weight Special condition if applicable Specify applicability All ZERO FUEL AFT Weight Index Value Index Value Page No:22.04

2 APU / TAXI FUEL WEIGHT Due to local taxiing distances and local needs for APU running, total taxi

7 EDP-SYSTEM Sheet 6 abin onfiguration(s) A / TYPE arrier B777F TK 5. EFFET OF FUEL 5.1 EFFET OF FUEL (FUEL DENSITY : 0.80 KG/L) 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 = 200 kg/hour Page No:22.05

8 Sheet 7 abin onfiguration(s) A/ TYPE arrier 6. REW 6.1. Number of cockpit crew seats and average location Maximum number of cockpit seats Length of arm from reference station Index influence +/- Inch (s) +/- per 1 kg 1.& 2. Seats seats seats Number of cabin crew seats and location Max. Length of arm from Loadmaster seat locations No. of reference station Index influence seats +/- Inch (s) +/- per 1 kg FWD of Safety Barrier Wall rew Distribution / rew ode Number of abin rew at Location rew ockpit rew abin rew ode Total No Total No FWD MID AFT 2/ / / / / / Location of rew Baggage BULK ARGO OMPT. Page No:22.06

9 abin onfiguration(s) ALL 7. GALLEY AND PANTRY 7.1. Galleys Sheet 8 A / TYPE arrier B777F TK Length of arm from reference Galley locations station Index influence +/- Inch (s) +/- per 1 kg G Pantry Weight / Pantry ode Pantry Weight / Pantry ode is given on A/ BASI & DRY OPERATING WEIGHT & INDEX TABLE. 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. Page No:22.07

10 abin onfiguration(s) ALL 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 A / TYPE B777F Sheet 9 arrier TK 8.2 lass/abin Sections lass/abin Section Length of arm from reference Index influence station +/- meter(s) +/- per 1 kg Page No:22.08

11 Sheet 10 A / TYPE arrier B777F 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 Pratice Page No:22.09

12 SETION ROW NO EDP-SYSTEM Sheet 11 abin onfiguration(s) A / TYPE arrier B777F TK Seatplan Layout / Facilities and Row Index Influence abin onfig. A B D E F G J K Length of arm from reference station INDEX INFLUENE per SEAT- ROW per1kg Page No:22.10

13 Sheet 12 abin onfiguration(s) A / TYPE arrier 9. DETAILS FOR OMPARTMENT TRIM OMPARTMENT MAXIMUM APAITY Length of Index influence NUMBE GROSS WEIGHT Arm from DESRIPTION Max.Weight R (kg) Ref.Sta. +/- 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 Page No:22.11

14 Sheet 13 abin onfiguration(s) A / TYPE arrier 10. DETAILS FOR BAY / SETION TRIM Bulk BAY / SETION DESRIPTION GROSS WEIGHT Index influence B.Arm (kg) +/- per 1 kg section1 Bulk section2 Bulk REMARKS: -PAG and PM pallet index influences are equalized by averaging original influences. This allowed to minimize the number of Hold versions. I. ONTAINER Lower Deck Maximum capacity Bay/Section Gross Weight Volume * Index value per 1 kg ontainers Page No:22.12

15 Sheet 13 abin onfiguration(s) A / TYPE arrier II. PALLET 88 x125 III. PALLET 96 x125 Lower Deck Maximum capacity Bay/Section Gross Weight Volume * Index value per 1 kg PALLET 96 x125 11P P P P P P P P P P Page No:22.12a

16 Sheet 13 abin onfiguration(s) A / TYPE arrier 10. DETAILS FOR BAY / SETION TRIM Main Deck Bay/Section 96 x 196 Single Row Gross Weight Maximum capacity B.Arm entroid Index value per 1 kg A AB B D D DE EF FG G GH HJ JK K L LM MP P * Volume information required for bulk compartments only. Page No:22.12b

17 Sheet 13 abin onfiguration(s) A / TYPE arrier 10. DETAILS FOR BAY / SETION TRIM Main Deck Bay/Section 125 x 96 Side By side Gross Weight Maximum capacity B.Arm entroid Index value per 1 kg A 8150* B 8150* * D 8150* E 8150* F 13606** G 13606** H 13606** J 8150* K 8150* L 8150* M 8150* P 8150* R (single) * When load more than 4075kg for each positon, please check unsymmetrical load limits table. ** 6803kg is max limit for each position for side-by side loading. Bay/Section G Longitudinal Gross Weight (kg) B.Arm entroid Index value per 1 kg AB 15550* D 15550* EF 15550* GH JK 15550* MP 15550* * When load more than 7775kg for each positon, please check unsymmetrical load limits table. Bay/Section R Longitudinal Gross Weight B.Arm entroid Index value per 1 kg AB 12778* D 12778* EF 12778* GH JK 12778* MP 12778* * When load more than 6389kg for each positon, please check unsymmetrical load limits table. Page No:22.12c

18 Sheet 13 abin onfiguration(s) A / TYPE arrier 10. DETAILS FOR BAY/SETION TRIM 16ft Pallets & 20ft. Pallets Main Deck Bay/Section 16ft & 20ft. PALLETS Maximum capacity Gross Weight Volume * Index value per 1 kg EF GH JK * Volume information required for bulk compartments only. Note 1: Attach a plan for each compartment configuration. Note 2: Use additional sheets as required. Main Deck Bay/Section 125 x 96 enteroid Gross Weight Maximum capacity B.Arm entroid Index value per 1 kg A B D E F G H J K L M P Page No:22.12d

19 11. BALLAST FIXED PROVISIONS FOR ARRYING BALLAST? REMARKS : BALLAST IS NOT REQUIRED EDP-SYSTEM B777F 6-Apr-2018 Sheet 14 A / TYPE arrier B777F TK A / TYPE B777F 1. G LIMITS 1.1. Planning Limits G-Limits for loadplanning purpose shall be agreed between carrier and system operator. D Sheet 1 arrier TK 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 EDP-SYSTEM 2. UNIT LOAD DEVIES DETAILS A / TYPE B777F 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 D Sheet 2 arrier TK 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. EDP-SYSTEM A / TYPE B777F 3. SPEIAL LOAD Turkish Airlines & IATA regulations apply. When necessary contact Turkish Airlines Station Manager. D Sheet 3 arrier TK Page No:22.13

A F 19-Dec-2017 IATA AHM560 DATA LIST OF EFFECTIVE PAGES REV 13

A F 19-Dec-2017 IATA AHM560 DATA LIST OF EFFECTIVE PAGES REV 13 A330-243F 19-Dec-2017 IATA AHM560 DATA LIST OF EFFETIVE PAGES REV 13 Pages/Sheets that are common to all A/ Types. Located in.pdf file "THY-AHM560_Pages_00.00-02.04.pdf" ATION PAGE ISSUE SHEET REV NO FOR