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°. Enter exact deadload from the Loading Report (LIR)
°. Enter exact amount of fuel from the fueling order
°. Ensure that the total traffic load does not exceed the allowed traffic load
°. Ensure that the center of gravity will not exceed the operational limits
°. Enter last minute changes and inform the flight crew
°. Sign the loadsheet and give a copy to the crew (or send it by ACARS)
. Check that aircraft documents are on board (Loadsheet, Trim sheet, NOTOC)
. Release the aircraft
. Send the LDM/CPM to the next station (Loadmessage/Cargo Pallet message)
. Store documents in the station‘s flight file
These three functions must be performed by at least two agents to minimize the risk of mistake and ensure a high safety level. The same person can cumulate, as an example, function 1 and function 3.
LOADING LOADING

A. LOADING GENERALITIES

1.2.2. EDP loadsheet
In case of EDP (Electronic Data Processing) loadsheet, the responsibility for correct loadsheet and trim data must be shared and clearly identified due to the various operational possibilities (decentralized input of data, decentralized loadsheet issuance, LMC…).
The above three functions still exist, but can be decentralized. As an example, Load planning and loadsheet can be prepared at the airline‘s base (function 1), whereas loading (function 2) and Load control supervision (function 3) is done at the station.
1.3. Load control qualification
The carrier is responsible for its shipment. In order to achieve an acceptable level of standardization and proficiency, minimum requirements shall be recognized in the training of carriers or handling companies‘ personnel involved in load control functions.
The carrier has the responsibility to: . evaluate and approve the handling company‘s training program or subject the personnel involved to a single or periodical qualification tests . Obtain a list of qualified personnel for a given aircraft type

A. LOADING GENERALITIES

2. AIRCRAFT WEIGHT
2.1. Regulation
The purpose of this chapter is to present what is required by the authorities concerning aircraft weighing. The following part will present how the weighing is performed. For more detailed information on aircraft weighing please report to JAR-OPS 1 Subpart J . Mass and Balance. (Paragraph 1.605 and appendix 1 to JAR-OPS 1.605) or/and to FAA Advisory circular 120-27A.
2.1.1. General information:
In order to elaborate a proper weight and balance document prior to a flight, the weight of the aircraft (as well as its center of gravity) has to be determined. This weight is first determined by the aircraft manufacturer and is found in the Weight and Balance Manual (Chapter 2.00: Weighing Report). It is the Operating Empty Weight in the Airbus weighing report, it may be named Basic Weight in some other weighing reports. From this Operating Empty Weight/Basic Weight the operator can define the aircraft Dry Operating Weight for each aircraft flight.
　
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