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C Sheet 8 details the cabin sections defined by the operator to determine the passenger loading influence per section. C Sheet 9 gives the .index to be used to determine the influence of passenger loading per cabin section. C Sheet 10 gives the .index to be used to determine the influence of passenger loading per seat row. It also enables to indicate the type of seat used in the cabin.
5.4.9. C Sheet 11, 12
C Sheet 11 and 12 gives the .index to be used to determine the influence of any cabin crew, any item in the galleys and any pantry.
5.4.10. C Sheet 13, 14
C Sheet 13 gives the .index to be used to determine the influence of cargo loading per cargo compartment. C Sheet 14 gives the .index to be used to determine the influence of cargo loading per cargo position.
5.4.11. C Sheet 15
C Sheet 15 details the operator‘s procedure for ballast carriage.
5.5. PART D: LOAD PLANNING DATA
This part is composed of sheets to enter general miscellaneous information such as the ideal trim line data in D Sheet 1, details about ULD (containers and pallets) in D Sheet 2, and regulations about special loads transportation in D Sheet 3.
WEIGHT AND
BALANCE

D. LOAD AND TRIM SHEET SOFTWARE

D. LOAD AND TRIM SHEET SOFTWARE

1. INTRODUCTION

The Load and Trim sheet software enables the Airbus operators to produce a load and trim sheet and its associated AHM560, AHM516 and AHM515 documents for any Airbus model: A319, A320, A321, A300, A310, A330 and A340 except for freighter and combi aircraft. These loading and trimming documents are generated from the weight and balance characteristics of the aircraft supplied in a database, from the assumptions set by the user and from the cabin arrangement defined for the aircraft. This software allows the Airbus operators to quickly produce and update these documents following any aircraft modification affecting the certified limits, the passenger distribution, the cargo distribution or the fuel management. The LTS software enables also to produce specific data files that are used by the Weight&Balance module of the Less Paper Cockpit package.
2. OBJECTIVES
The main objectives of this software are the electronic distribution and update of the Weight&Balance data of Airbus aircraft and the calculation and creation of the loading and trimming documents.
. To improve access time to the information. . To ensure technical data accuracy . To propose a user-friendly interface to visualize
and update the Weight & Balance data. . To perform the error calculation required for the operational envelopes determination. . To reduce the production time of the loading and trimming documents.

WEIGHT AND
BALANCE
WEIGHT AND
BALANCE
D. LOAD AND TRIM SHEET SOFTWARE

3. SOFTWARE DESCRIPTION
First of all, the LTS program uses a database containing a complete set of assumptions and data. The program structure relies on a relational database that stores the following pieces of information:
　
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