5.2. PART A: COMMUNICATION ADDRESSES
This part provides with the handling agents' and the carrier' addresses. It also lists all the documents that need to be produced by the EDP system. The supplemental documents are for instance a Loadsheet, a Loading Instruction/Report, a NOTOC, a LDM, a CPM, …
C. BALANCE CHART DESIGN
5.3. PART B: GENERAL INFORMATION
Part B is a summary of weight data used by the airline : passenger weights (Male / Female / Children / Infants), crew weights and cabin baggage weights, as well as the list of items taken into account for the Dry Operating Weight (DOW) and Dry Operating Index (DOI) calculation.
5.4. PART C: AIRCRAFT DATA
This part contains the aircraft detailed list for which the document is applicable with the aircraft definition in term of weights and index and all the trimming data.
5.4.1. C Sheet 1
C Sheet 1 contains the information the operator needs to be shown on the EDP system Loadsheet output and the way the operator has chosen to determine the passenger loading influence on aircraft CG position.
5.4.2. C Sheet 2
C Sheet 2 contains the aircraft list for which the document is applicable and their definition in term of Dry Operating Weight or Basic Weight.
WEIGHT AND
BALANCE
WEIGHT AND
BALANCE
C. BALANCE CHART DESIGN
5.4.3. C Sheet 3
C Sheet 3 is a reminder of the index formula used for index calculation, with the exact values of
constants and aircraft data that enter in this formula.
At the bottom of this sheet, the stabilizer trim setting is given in function of the MAC value at
takeoff.
5.4.4. C Sheet 4
C Sheet 4 contains the fuel index tables, there may be only one fuel table for the standard fuel density used by the operator of several tables for a range of densities.
Note : for all aircraft equipped with a trim tank it is recommended to issue several tables for different densities.
5.4.5. C Sheet 5
C Sheet 5 gives the .index to be used to determine the influence of items or persons in the cockpit.
5.4.6. C Sheet 6
C Sheet 6 contains the aircraft list for which the document is applicable (same list as in C Sheet 2) and their definition in term of maximum weights.
5.4.7. C Sheet 7
C Sheet 7 contains the operational limits to be used for CG checks in the EDP system. . —takeoff“ operational limit (the limit resulting from the operational margins computation and the selection of the more limiting part between takeoff, landing and in flight operational limits) . zero fuel operational limit.
C. BALANCE CHART DESIGN
5.4.8. C Sheet 8, 9, 10 中國航空網 www.k6050.com 航空翻譯 www.aviation.cn 本文鏈接地址：Getting to Grips with Aircraft Weight and Balance(87)
