AHM560 Data for Check-in & Loadcontrol ACTION FOR PAGES PAGE NO ISSUE DATE SHEET NO REV NO PAGE DESCRIPTION

Transcription

1 PAGE NO A J 19-Apr-2018 IATA AHM560 DATA LIST OF EFFETIVE PAGES REV 01 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 Apr18 01 hanged - List Of Effective Pages PAGE DESRIPTION Apr A1,A2 ontact & ommunication Addresses Apr B1,B2 Passenger and Baggage Weights / rew Weights Apr B3,1 DOW and DOI specifications / Output on Loadsheet Apr Index and MA formula, Stabilizer Trim Settings Apr18 01 hanged BASI&DRY OPERATING Weight and Index Table Apr Aircraft Weight Limitations Apr18 01 hanged 5 G - Limits for Loadsheet Purpose Apr18 01 hanged 6 Effect of Fuel Apr abin rew Seats, rew Distribution Apr18 0-8,9 Galley & Pantry, Passenger Seats Apr Seating Layout ode Letters Apr Seat Plan Layout, Facilities & Row index influence Apr abin Layout Drawing (LOPA) Apr ,13 Details for compartment trim, max allowable weights Apr argo compartment details chart Apr D1 Ballast, Ideal Trim Line ZFW Apr D2 ULD devices, Special Load Apr Load&Trim Sheet Information Apr Load&Trim Sheet (front left side page) Apr Load&Trim Sheet (reverse right side page) Fuel Index Table Apr TBD --- Load&Trim Sheet Fuel Index Table Apr TBD --- Loading Instruction Report REV NO REVISION DESRIPTION 01 T-ANK re-weighed and G limits changed 00 T-ANK has joined VIP Fleet IMPORTANT: - PLEASE HEK WHETHER ISSUE DATE ON EAH PAGE IN YOUR SET, MATHES WITH THE DATES ON THIS LIST OF EFFETIVE PAGES. IF THERE IS ANY MISMATH, INFORM THESE ADDRESSES: FLIGHT PERFORMANE PLNG.MNG; SITA: ISTOF, PHONE: (90) , FAX: (90) wabe@thy.com PLEASE GIVE A OPY OF THIS DOUMENT TO LOAL HANDLING AGENY - IF HEKIN AND LOADONTROL IS DONE BY OMPUTER (DS), THEN THIS DATA WILL BE INPUT TO DS (DEPARTURE ONTROL SYSTEM) BY THE HANDLING AGENY. - DATA PRINTOUTS AND SAMPLE LOADSHEETS MUST BE SENT TO ABOVE ADDRESS FOR APPROVAL Page No:23.00

2 A J 17-Apr-2018 OMMUNIATION ADRESSES 1. HANDLING AGENTS S ONTAT ADDRESS A Sheet 1 ompleted sheets and changes of basic data and procedure will be forwarded to TURKISH AIRLINES LOAL STATION MANAGER by comail and then it will be handed to Local Handling Agent. 2. ARRIER'S ONTAT ADDRESS Turkish Airlines Inc. Flight Performance and Planning Management THY Genel Yonetim Binası 8.kat Atatürk Airport Yesilkoy Istanbul Turkey Phone: Fax: wabe@thy.com EDP-SYSTEM OMMUNIATION ADRESSES 3. AUTOMATIALLY PRODUED DOUMENTS X NOTO X SEATPLAN X LOADPLAN X PASSANGER INFO LIST X LOADSHEET X LOADING INSTRUTION REPORT 4. MESSAGE REQUIREMENTS LPM Load Planning Message AHM 580 X LDM Load Message AHM 583 ALI Abbreviated Load Information Message AHM 584 X PM ontainer / Pallet Distribution Message AHM 587 UM ULD ontrol Message AHM 388 (dispatch only) X MVT Movement messages AHM 811 and 780 DIV diversion message AHM 781 SOM Seat Occupied Message Recommended Practice 1712 PTM Passenger Transfer Message Recommended Practice 1718 PSM Passenger Service Message recommended Practice 1715 (dispatch only) TPM Teletype Passenger Manifest Recommended Practice 1717 (dispatch only) PFS Passeneger Final Sales Message Recommended Practice 1719 (dispatch only) IDM Industry Discount Message Recommended Practice 1714 RQL Request List Message Recommended Practice 1709 (dispatch only) PNL ADL Passenger Name List and Additions and Deletions List (Recommended Practice 1708 acceptance only) SAL Seats Available List Recommended Practice 1713 (acceptance only) SLS Statistical Load Summary A-M 588 FMM Fuel Monitoring Message A-M 782 RQM Request Information Message AHM 783 UWS ULD Bulk Load Weight Spral AHM 581 (acceptance only) A Sheet 2 REMARKS: ontact Turkish Airlines Local Station Manager for the required messages. 5. MESSAGE ADDRESSES ontact Turkish Airlines Local Station Manager for message Addresses. Page No:23.01

3 A J 17-Apr-2018 GENERAL INFORMATION 1. PASSENGER AND BAGGAGE WEIGHTS 1.1. Passenger Weights Male Female All Adult All flight except holiday charters 88 kg 70 kg 84 kg Holiday charters 83 kg 69 kg 76 kg hild (2 years to 12 years) 35 kg 35 kg 35 kg Infant 10 kg 10 kg 10 kg B Sheet 1 REMARKS: Normally Male and Female values should be used. Holiday charters means a charter flights solely intended as an element of a holiday travel package. The holiday charter mass values apply provided that not more than 5% of passenger seats installed in the aeroplane are used for the nonrevenue carriage of certain categories of passengers abin Baggage Weight abin baggage weight is included in the above mentioned passenger weights. X YES NO If no: actual cabin baggage weight must be used hecked Baggage Weight Weight per piece Weight per passenger Actual Actual EDP-SYSTEM 2. REW WEIGHTS GENERAL INFORMATION B Sheet 2 ockpit crew abin crew 85 kg 75 kg rew baggage is included in the above crew weights: X YES NO If NO: Actual crew baggage weight must be used. REMARKS: For Longhoul flights and for the flights that crew stays overnight at destination, additionally Standart baggage weight of 10 Kg per crew member should be added. Page No:23.02

4 A J 17-Apr-2018 GENERAL INFORMATION B Sheet 3 3. DRY OPERATING WEIGHT AND DRY OPERATING INDEX SPEIFIATIONS (Tick as appropriate) DOW DOW Incl Excl Incl Excl REMARKS ITEM BASI WEIGHT REW REW BAGGAGE See Remarks PANTRY ONTAINERS See Remarks PALLETS See Remarks FLY - AWAY KIT See Remarks REMARKS: - Before flight check the Bulk cargo compartment if Nose Gear and Main Gear spare wheel&tire are carried or not. If carried, they should be shown as "LOAD IN OMPARTMENTS", at "DISTRIBUTION" columns on LOADSHEET and specified as EI (Equipment in compartment). - Tare weight of ULD (containers & pallets) should be shown as included in the GROSS load in position. The sum of Net cargo/bag weight + pallet/container tare weight should be shown in LOAD IN OMPARTMENTS" in "DISTRIBUTION" column of LOADSHEET. - REW BAGGAGE on Longhoul flights and for flights that crew stays overnight at destination, is NOT included in DOW/DOI. This additional standard baggage weight of 10 kg per crew member should be shown as 'LOAD IN OMPARTMENT - DISTRIBUTION" in Loadsheet. Use K input in THY DS system. EDP-SYSTEM GENERAL INFORMATION Sheet 1 1. BALANE AND SPEIAL INFORMATION OUTPUT ON LOADSHEET 1.1. Balance Output Requirements are marked in respective box Basic index BI Dry operating Index DOI Deadload index DLI Loaded Index at zero fuel weight LIZFW Loaded Index at take of weight LITOW Loaded Index at landing weight LILAW MA - at zero fuel weight MAZFW MA - at take of weight MATOW MA - at landing weight MALAW Stabilizer trim setting at take off STABTO* REMARKS 1.2. Passenger Trim Output lass Trim abin Area Trim Seat Row Trim REMARKS Page No:23.03

5 A J 17-Apr-2018 A / TYPE A J Sheet 3 2. BASI INDEX AND MA FORMULA 2.1. Examples and definitions Index % 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 = 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) = 50 (onstant) = MA Information Length of MA = meters LEMA at = meters/ from zero 2.4. Stabilizer Trim Setting MA Range STAB Range Nose up Nose down Linear variation between 15% MA and 35% MA Page No:23.04

6 A J 19-Apr-2018 A / TYPE A J BASI & DRY OPERATING WEIGHT & INDEX TABLE WEIGHT UNIT: KG INDEX UNIT: KG.M MAX TAXI WEIGHT BASI WEIGHT INLUDES ALSO FOLLOWINGS ONBOARD IN EVERY FLIGHT;IF NOT ADJUST WT&INDX: HEK&OBSERVE THE ARGO OMPT MAX LIMITS MAX TAKE-OFF WT MAX LANDING WT MAX ZERO FUEL WT Max FUEL ap (d=0.785kg/lt) + FWD GALLEY G1[STD UNIT(Qty11)+DRYSTORE] Total 145kg / -1.5 index INTRODUTION REF T-ANK A/ Name / Total No. of Pax Seats 2+17 Date last weighed / modif. 23JUN16/ Manufacturer s serial number msn4042 WEIGHT INDEX BASI WEIGHT/ INDEX REF Pilots (2 ockpit rew) 170-3,9 2 abin rew (2fwd) 150-2,7 SUB TOTAL 2 / 2 REW Additional ockpit rew (FWD) 85-1,8 SUB TOTAL 3 / 2 REW Additional ockpit rew (FWD) SUB TOTAL 4 / 2 REW DRY OPERATING WT/INDX REF REW 2/4+PANTRY ODE A 1+A REW 2/4+PANTRY ODE B 1+B REW 2/4+PANTRY ODE 1+ REW 3/5+PANTRY ODE A 3+A + Plate+Glass in Doghouse; total 20kg / 0.2index + AFT GALLEY G4[DRYSTORE+PORSELEN MATERIALS] + STD UNIT (Qty13) Total 320,3kg / +3.9 index + ockpit Docs in radenza; Total 48kg / 0.3index + PILLOW(Qty60) + BLANKETS(Qty17) + SHAM(Qty25) + TABLE headbins. Total 45kg / 0.05 index + SUITS(Qty3) + LEANING SUPPLIES + HANGER(Qty30)+ Pillow and lankets; Total 40kg / +0.2 index + TEH.EQUIPMENTS in ompt 5 [SPARE PARTS BOX(Hyd+Oil=61kg,box Mech=59kg,4EA Rafts=38kg)158kg TOWBAR 57.5kg, JAK UNIT 90kg, TOOL BOX 18.5kg, SMALL SPAREPARTS BOX 38.5kg, LADDER 12.5kg, FLYAWAYKIT BOX 11.5kg, SPAREWHEEL&TIRE ASSBLY 1NG+1MG 185kg] Total 571.5kg / +4.8 index OVERALL TOTAL = kg / 6.9 index DRY OPERATING WT/INDX for Typical rew and Pantry combinations are given above. For other crew and Pantry combinations use crew SUB TOTALS given above and Pantry Weights/odes below. PANTRY TOTAL FWD AFT PANTRY WEIGHT & ODES APPLIABLE ODES WEIGHT INDEX G1 G4 FLIGHTS, ONDITIONS PANTRY ODE A Hours Flights PANTRY ODE B 300 1, Hours Flights PANTRY ODE hours Flights * STANDARD PANTRY WEIGHT/INDEX for several Flight onditions is given in above table. * Select the appropriate Pantry ode and Adjust Dry Operating Weight/Index. * Tare weight of all trolleys and Galley Equipments such as hot-cups, S/U s (Galley Standard Units) are included in Basic Weight/Index. If some of these equipments are not carried, make necessary adjustments. OKPIT REW TOTAL EFFET / ockpit rew No/Locations ockpit rew No/Locations WEIGHT INDEX 2 OKPIT REW (2 FrontSeat) 170-3,9 3 OKPIT REW (2 FrontSeat +1 JumpSeat) 255-5,7 4 OKPIT REW (2 FrontSeat +2 JumpSeat) 340-7,5 ABIN REW TOTAL EFFET / abin rew No/Locations abin rew No/Locations WEIGHT INDEX 2 ABIN REW (2 Fwd) 150-2,7 Page No:23.05

7 A J 19-Apr-2018 A / TYPE A J ADDITIONAL ABIN STOWAGE OMPARTMENTS: These stowage ompts contains those included in BW/BI. If more other things are carried, adjust DOW/DOI NOTES: LOATION REF no Maxap Index S S S S Washroom S S S VIP Private Area Executive Lounge Entourage Area Stowage Stowage Stowage S S S S S S S S S S S S S S S S S S S 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 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. Flyaway-Kit Equipment in Bulk ompt.5 weight index NOSE GEAR WHEEL & TIRE (Qty1) & MAIN Nose Gear(NG) Spare Wheel & Tire (Qty 1) GEAR WHEEL & TIRE (Qty1) ARE ALWAYS Main Gear(MG) Spare Wheel & Tire (Qty 1) ARRIED. TOTAL SO, on the contrary to other fleets, for this Dry Oper.Wt/Index INLUDES Spare wheel & tire aircraft, THEY ARE INLUDED IN BASI WEIGHT & BASI INDEX. Page No:23.05

8 4. LIMITATIONS 4.1. Aircraft Weight Limitations Maximum weights for: (KG) A J 17-Apr-2018 A / TYPE A J Sheet 4 Aircraft Design Take-off Design Take-off Design MSN Ramp/Taxi Zero Fuel Reg. Wet Dry Landing T-ANK N/A 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. Page No:23.06

9 4.2. G - Limits for Loadsheet Purpose FORWARD Special condition if applicable Specify applicability TAKE-OFF FWD A J 19-Apr-2018 A / TYPE A J AFT Special condition if applicable TAKE-OFF AFT Sheet 5 Weight(kg) Index Index Specify applicability Weight(kg) Value Value Special condition if applicable Specify applicability ZERO FUEL FWD Special condition if applicable ZERO FUEL AFT Weight(kg) Index Index Specify applicability Weight(kg) Value Value Page No:23.07

10 5. EFFET OF FUEL Fuel Loading Fuel Usage Standard Procedure X X A J 19-Apr-2018 A / TYPE A J Sheet 6 Non-standard Weight (kg) Index REMARK: FUEL TANKS' TOTAL VOLUMETRI APAITY IS LT 5.1 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 = 10 kg/minute APU Fuel Flow = 130 kg/hour Page No:23.08

11 A J 19-Apr-2018 Left Outer Tank Kg Index Right Outer Tank Kg Index Left InnerTank Kg Index Right InnerTank Kg Index enter Tank Kg Index enter Tank Kg Index Page No:23.08

12 A J 17-Apr-2018 EDP-SYSTEM Sheet 7 abin onfiguration(s) A / TYPE ALL A REW 6.1. Number of cockpit crew seats and average location Maximum H.Arm Length of arm from reference number of cockpit Location (Balance Arm) station Index influence seats meters +/- meter(s) +/- per 1 kg aptain st Officer st Observer nd Observer Average OKPIT REW TOTAL EFFET / ockpit rew No/Locations ockpit rew No/Locations WEIGHT INDEX 2 OKPIT REW (2 FrontSeat) 170-3,9 3 OKPIT REW (2 FrontSeat +1 JumpSeat) OKPIT REW (2 FrontSeat +2 JumpSeat) Number of cabin crew seats and location ABIN rew seats locations Max. No. of seats H.Arm Balance Arm (m) Length of arm from reference station Index influence +/- meter(s) +/- per 1 kg REAR WALL OF FWD TOILET La FWD ABIN REW TOTAL EFFET / abin rew No/Locations abin rew No/Locations WEIGHT INDEX 2 ABIN REW (2 Fwd) 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. 5 Page No:23.09

13 A J 18-Apr-2018 A / TYPE A J Sheet 8 7. GALLEY AND PANTRY 7.1. Galleys Galley locations Length of arm from reference station Index influence +/- meter(s) +/- per 1 kg G1 FWD GALLEY G5 AFT GALLEY Pantry Weight / Pantry ode Pantry Weight / Pantry ode table is given on page 14.02A 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. EDP-SYSTEM 8.1 PASSENGER SEATS A / TYPE A J Sheet 9 LASS ODES => lass 1: onference Area lass 2: Private Office lass 3: Guest/Staff NAME OF ABIN SETION NUMBER OF SEATS lass 1 lass 2 lass 3 TOTAL Per ABIN SETION ABIN ONFIGURATION 132Y 0A 2 2 0B Total per class lass/abin Sections abin Section H.Arm Balance Arm (meters) Length of arm from Index influence reference station +/- meter(s) +/- per 1 kg Page No:23.10

14 8.3 Seating Layout A J 17-Apr-2018 Sheet 10 A / TYPE A 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:23.11

15 A J 17-Apr-2018 A / TYPE A J Sheet Seatplan Layout / Facilities and Row Index Influence A B E F Index influence per seat row Section Location Definition Row +/- per 1 kg Entourage 1 X - 0,01467 A Seat Area 2 X - 0,01101 Section Location Definition Row A B E F B Executive Lounge Index influence per seat row +/- per 1 kg X X X Seat 3-3 Not allowed for takeoff and landing Seat 4 X X X Seat 5 X X - 0,00219 Seat 6 X X + 0,00196 Seat 7 X X + 0,00456 Seat 8 X + 0,00464 Seat 9 X + 0,00629 Section Location Definition Row A B E F REMARKS: Private Office Seat Index influence per seat row +/- per 1 kg X X A Not allowed for takeoff and landing 11 X X X ode letter "X" means facility of this seat not described or not known (e.g. No distinction between smoking or non-smoking) 2. Seat Rows marked as "Not allowed for takeoff and landing" are in locations "Bed (onvertible Divan)", "ommunication enter" & "rew Rest ompartment". They are given for information purposes only. They are not included in cabin area and they should not be used for weight and balance purposes. They should not be seated during takeoff and landing. 3. Seats..,.. are prefered seats for Technicians. Page No:23.12

16 A J 17-Apr-2018 abin Layout Drawing (LOPA) Page No:23.13

17 9. DETAILS FOR OMPARTMENT TRIM NO OMPARTMENT DESRIPTION A J 17-Apr-2018 A / TYPE A J MAXIMUM APAITY GROSS WT (kg) VOLUME* (m 3 ) Average H.Arm Balance Arm (m) Sheet 12 Index influence +/- per 1 kg 1 FWD ompartment Bulk Loading AFT ompartment Bulk Loading REMARKS: Other compartments are occupied by Additional enter Fuel Tank (AT) Only Bulk loading is allowed. ULD (containerized/palletized) loading (LS loading) is NOT possible. 9.1 ombined Load Limitations: N/A EDP-SYSTEM 10. DETAILS FOR BAY / SETION TRIM A / TYPE A J Sheet 13 MAX. APAITY Posi.Avrg. H.Arm Index influence BAY / SETION GROSS WEIGHT (kg) VOLUME (M 3 ) Balance Arm (m) +/- per 1 kg 11 BULK BULK BULK BULK BULK REMARKS: Other sections are occupied by Additional enter Fuel Tank (AT) Page No:23.14

18 A J 17-Apr-2018 ARGO HOLD LAYOUT LEFT BLANK INTENTIONALLY Page No:13.15

19 A J 17-Apr-2018 EDP-SYSTEM 11. BALLAST FIXED PROVISIONS FOR ARRYING BALLAST REMARKS : BALLAST IS NOT REQUIRED A / TYPE A J Sheet 14 EDP-SYSTEM A / TYPE A J D Sheet 1 1. G LIMITS 1.1. Planning Limits G-Limits for load planning 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 load planning 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 Important note: The Ideal trim line given on the table is for Zero Fuel Weight onditions. Page No:23.16

20 A J 17-Apr-2018 EDP-SYSTEM 2. UNIT LOAD DEVIES DETAILS Not Applicable A / TYPE A J D Sheet 2 EDP-SYSTEM 2. SPEIAL LOAD A / TYPE A J D Sheet 3 Turkish Airlines & IATA regulations apply. When necessary contact Turkish Station Manager Page No:23.17

21 A J 17-Apr-2018 Description of the Sheet. Formun Açıklaması: 1. FLIGHT NO:Flight Number / Uçuş numarası 2. FROM / TO: Depart./Arrival Airport Nereden / nereye 3. A / REG: Aircraft Registration / Uçak kanat adı 4. DATE: Date of Departure / Tarih 5. REGULATORY TOW/LDW: Max allowed take-off & landing wt for that Runway./Mevcut şartlara göre uçağın Max kalkış/iniş ağırlığı. 6. TOTAL (RAMP) FUEL: Eğer yakıt alınmışsa göstergelerde okunan yakıt değeri. (örnek: 14560kg.)Yakıt alınmamışsa Dispach ile mutabık kalınan yakıt. 7. TRIP FUEL: Uçuş planındaki trip yakıtı. 8. TAXI FUEL: Uçuş Planındaki taxi yakıtı. 9. FLIGHT TIME: Uçuş Planındaki "Trip Time" 10. REW (ockpit/abin): Son durumu yansıtan değerler (Eğer uçakta görevli teknisyen varsa REW olarak değerlendirilmeyecektir. 11. EI (Equipment in ompartment): Equipments such as Spare Wheel&Tire, Toolbox, Engine Oil boxes. This box should be filled in by The Load ontroller. "Flyaway Kit"i (Yedek lastikler+ alet çantası v.b.) kapsamaktadır.bu bölüm Load ontroller (Koordinatör) tarafından doldurulacaktır. 12. APU : If APU is removed due to technical maintenance reasons, APU status should be recorded as removed/installed for weight& balance purposses. Bir teknik arıza nedeniyle APU'nun uçaktan sökülmesi halinde,uçağın gerçek ağırlığını Load and Trim Sheet'e yansıtabilmek amacıyla doldurulacaktır.load ontroller (Koordinatör) tarafından doldurulur.ancak bir yanlışlığa meydan vermemek için "Maintenance Log Book" ta "Hold Items" bölümüne bakılarak kontrol edilmesi gereklidir. 13. FORWARD AIRSTAIR: To be filled in for the similar purposses as in item maddedeki konular bu madde için de geçerlidir. Remarks: A similar sheet as described in this page should be used in your station. Please produce and develope a similar sheet adopted to your local needs. For each flight just after landing and after doors opened, this form should be brought to cockpit. Necessary spaces should be filled in by the loadcontroller and the cockpit crew. Information exchange between loadcontroller and the cockpit crew will be maintained by this form to produce loadsheet with the correct data. / Yukarıda tanımlanan form, bulundugunuz istasyon icerisinde de kullanılmalıdır. Lutfen,bu formun benzerinden kendi istasyonunuzun ihtiyacini karsilayacak şekilde birkopya olusturunuz. Bu form, her uçuşta inisten hemen sonra ve kapılar açılınca kokpite getirilmelidir. Gerekli olan boşluklar, loadcontroller ve Kokpit personeli tarafından doldurulmalıdır. Loadcontroller ve Kokpit personeli arasındaki bilgi akışı, bu formun doğru bilgilerle Loadsheet üretilmesine imkan verecektir. Page No:23.18

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