B December-2018

Transcription

1 B December2018 IATA AHM560 DATA LIST OF EFFETIVE PAGES REV 24 Pages/Sheets that are common to all A/ Types. Located in.pdf file "THYAHM560_FOREWORD" PAGE NO ATION ISSUE REV SHEET FOR DATE NO NO PAGES PAGE DESRIPTION ontents Apr11 General Info Apr11 A1,A2 ontact Address Apr11 B1,B2 Passenger & baggage weights/ crew weights Apr11 DOW and DOI specifications / Special Information Apr11 Load&Trim Sheet Information Dec18 24 Updated List Of Effective Pages Basic Index and MA formula/ Stabilizer Dec ,3 Trim Setting/A/ Registration., Wt Index Details 04.01A 22Jul10 12 Stabilizer Trim Setting table Dec18 24 Updated A/ Basic Weight & Index Table 04.02A 20Dec18 24 Updated Pantry Standard W/I Table(atering) Oct Aircraft Weight Limitations Jun G Limits for Loadsheet Purpose Dec Effect of Fuel / APU Taxi Fuel Weight Mar rew Seats Location & Distribution Jul Galley & Pantry Jul Passenger abin Jul lass / abin Sections Dec Seating Layout ode Letters July16 11 Seat Plan Layout May ,1 Details For ompartment Trim & 3,14 Bay/Section Trim, Ballast Dec08 01 D1, D2,D3 Ideal Trim Line, ULD / Special Load May12 Load&Trim Sheet (TJKJ,JKK,JKO) Page No:04.00

2 REVISION NOTES: B December2018 REV NO REVISION DESRIPTION 24 TJKO BW/BI values have been updated due to potable water s weight s change and pantry standart weight /ındex table for all Anadolu Jet Flights has been added. 23 TJKO G Limits have been updated. 22 TJKK,JKJ left THY fleet 21 TJKJ,JKK,JKO BW/BI changed due to modification 20 TJKJ,JKK BW/BI changed due to weighing 19 TJKO BW/BI changed due to weighing 19 TJKN left THY fleet 18 LM values are updated Pantry codes amended. Passenger cabin modified by addition of seat row Total index value of 3 cockpit crew amended. Number of cockpit crew seats and average location table amended for JS. Page No:04.00

3 EDPSYSTEM B December2008 Sheet 2 abin onfiguration(s) A / TYPE arrier ALL B TK 2. BASI INDEX AND MA FORMULA 2.1. Examples and definitions Index W (Station Ref.Sta.) K % MA W Station Ref.Station calculated 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 = 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 = 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 04.01A. These are for Flaps 1 & 5 only. EDPSYSTEM Sheet 3 abin onfiguration(s) A / TYPE arrier ALL B TK 3. AIRRAFT REGISTRATIONS, WEIGHT AND INDEX DETAILS DRY OPERATING WEIGHT X BASI WEIGHT X A list of weight and index values for each aircraft registration is given on next page. Page No:04.01

4 B July2010 STABILIZER TRIM SETTING VALUES ENGINE THRUST RATING : LB Page No:04.01A

5 B December2018 A/ BASI & DRY OPERATING WEIGHT & INDEX TABLE Numbe A/c Type MSN A/ Reg. r of Seats Basic*(crew(0/0) How to calculate DOW/DOI? Weight Index B737700W TJKO 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 MTAXI KG TJKO MTOW KG MLDW KG MZFW KG OKPIT REW TOTAL EFFET / ockpit rew No/Locations ockpit rew No/Locations WEIGHT INDEX 2 OKPIT REW (2 FrontSeat) OKPIT REW (2 FrontSeat + 1JumpSeat) 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) PANTRY EFFET / Pantry ode/lass, onfig, App. PANTRY (ATERING) STANDARD W/I TABLE IS ON PAGE 04.02A BW/BI value in the above table already includes potable water with FULL tank (160 kg/ 1.7 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 40 KG / Subtract 0.4 Index Subtract 80 KG / Subract 0.8 Index Subtract 120 KG / 1.3 Subtract Index *Basic Wt/Index 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/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 = 23 KG REW BAGGAGE (in BULK argo ompartment) : For Longhaul 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 DOWDOI_TableB 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. Page No:04.02

6 Pantry ode B December2018 PANTRY STANDART WEIGHT/INDEX TABLE (ATERING) 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. I Valid for all Anadolu Jet Flights Pantry Galley weight TOTAL ode Fwd Aft WEIGHT INDEX Destination / Departure U ,4 DOMESTI FLIGHTS ONE WAY V ,7 DOMESTI FLIGHTS RETURN PANTRY W ,0 ALL INTERNATIONAL FLIGHTS Page No:04.02A

7 EDPSYSTEM B July2016 Sheet 4 abin onfiguration(s) A / TYPE arrier B TK 4. LIMITATIONS 4.1. Aircraft Weight Limitations Maximum weights for: Aircraft Design Takeoff Wet off Dry Landing Design Take Design MSN Ramp/Taxi Zero Fuel Reg. TJKO 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 : 800 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. Page No:04.03

8 EDPSYSTEM B Oct2018 Sheet 5 abin onfiguration(s) A / TYPE arrier B TK G Limits for Loadsheet Purpose FORWARD Special condition if applicable Specify applicability ZERO FUEL HEK Weight(kg) Special condition if applicable TAKEOFF HEK Special condition if applicable LANDING HEK Index Value AFT Special condition if applicable Specify applicability ZERO FUEL HEK Weight(kg) Index Value Special condition if applicable TAKEOFF HEK Special condition if applicable LANDING HEK Page No:04.04

9 EDPSYSTEM B Dec2008 Sheet 6 abin onfiguration(s) A / TYPE arrier ALL B TK 5. EFFET OF FUEL Fuel Loading Fuel Usage Standard Procedure X Nonstandard Procedure FUEL DENSITY: 0.79 KG/L FUEL WEIGHT (KG) INDEX VALUE MAIN TANKS =>>> FULL MAIN & ENTER TANKS 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. Fuel usage procedure is just the opposite of loading procedure VOLUMETRI APAITY MAIN TANKS LT MAIN TANKS LT ENTER TANK LT TOTAL LT 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 = 12 kg/minute APU Fuel Flow = 105 kg/hour Page No:04.05

10 EDPSYSTEM B Dec2008 Sheet 7 abin onfiguration(s) A / TYPE arrier ALL B TK 6. REW 6.1. Number of cockpit crew seats and average location Length of arm from reference Index influence station Maximum number of cockpit seats +/ +/ (inch) per 1 kg Number of cabin crew seats and location ABIN rew seats locations Max. Length of arm from Index influence No. of seats reference station +/ +/ (inch) per 1 kg FWD ENTRY DOOR AFT ENTRY DOOR rew Distribution / rew ode rew ode Number of abin rews at ockpit abin rew Location rew Total Total No Location of No FWD AFT rew Baggage 2/ BULK ARGO 2/ OMPT. Page No:04.06

11 EDPSYSTEM B Jul2010 Sheet 8 abin onfiguration(s) A / TYPE arrier ALL B TK 7. GALLEY AND PANTRY Galleys Length of arm from reference Index influence Galley locations station +/ +/ (Inch) per 1 kg G G FWD(G1+G2) G4B AFT(G4B) 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 passenger distribution table if used. Page No:04.07

12 EDPSYSTEM B Jul2010 Sheet 9 abin onfiguration(s) A / TYPE arrier B TK 8. PASSENGER ABIN 8.1 Passenger Seats LASS ODES lass 1: lass 2 : Y lass 3 : Name of cabin section NUMBER OF SEATS lass lass lass Total per cabin section Name of cabin section NUMBER OF SEATS lass lass lass Total per cabin section ABIN ONFIGURATION 124Y ABIN ONFIGURATION 12/112Y OA OA OB OB O O Total per Total per class class Page No:04.08

13 EDPSYSTEM B Jul2010 Sheet 9 abin onfiguration(s) A / TYPE arrier ALL B TK 8.2 lass/abin Sections lass/abin Section Length of arm from reference station Index influence +/ inch +/ per 1 kg OA 308, OB O Page No:04.09

14 EDPSYSTEM 8.3 Seating Layout B Jul2010 Sheet 10 A / TYPE arrier B 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 nonsmoking) 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:04.10

15 EDPSYSTEM B July2016 Sheet 11 abin onfiguration(s) A / TYPE arrier TJKO B TK Seatplan Layout / Facilities and Row Index Influence SETION ROW NO 1 A B Index Influence per Seat Row per1kg ABIN ONFIGURATION 124Y ABIN ONFIGURATION 12/112Y Rows Rows fromtoto: from A B D E F A B D E F 13 NI N Y. Y N NI 13 NI N Y. Y N NI 611 NI N N. N N NI 611 NI N N. N N NI 12 Y NE NE. NE NE Y 12 Y NE NE. NE NE Y 13 NE NE NE. NE NE NE 13 NE NE NE. NE NE NE 1424 NI N N. N N NI 1424 NI N N. N N NI MOVEABLE ERTAIN LASS DIVIDER is shown as: THE AISLE is shown as :. Page No:04.11

16 EDPSYSTEM B Nov2009 Sheet 12 abin onfiguration(s) A / TYPE arrier B TK 9. DETAILS FOR OMPARTMENT TRIM MAXIMUM APAITY INDEX INFLUENE OMPARTMENT DESRIPTION GROSS VOLUME* NUMBER WEIGHT (M 3 ) (kg) +/ 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 EDPSYSTEM Sheet 13 abin onfiguration(s) A / TYPE arrier B TK 10. DETAILS FOR BAY / SETION TRIM MAX. APAITY Index influence BAY / SETION GROSS WEIGHT (kg) VOLUME (M 3 ) +/ per 1 kg NOT APPLIABLE 10.1 Unsymmetrical load limitations: NOT APPLIABLE EDPSYSTEM Sheet 14 abin onfiguration(s) A / TYPE arrier B TK 11. BALLAST FIXED PROVISIONS FOR ARRYING BALLAST? REMARKS : BALLAST IS NOT REQUIRED Page No:04.12

17 B Dec2008 EDPSYSTEM D Sheet 1 A / TYPE arrier B TK 1. G LIMITS 1.1. Planning Limits GLimits 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 EDPSYSTEM D Sheet 2 A / TYPE arrier B TK 2. UNIT LOAD DEVIES DETAILS Maximum apacity Type ode Tare weight Gross Weight VOLUME (m 3 ) Remarks NOT APPLIABLE EDPSYSTEM D Sheet 3 A / TYPE arrier B TK 3. SPEIAL LOAD Apply Turkish Airlines & IATA regulations. When necessary contact Turkish Airlines Station Manager. Page No:04.13