This section discusses general guidelines and procedures for weighing large fixed-wing aircraft exceeding a takeoff weight of 12,500 pounds. Several examples of center of gravity (CG) determination for various operational aspects of these aircraft are also included. Persons seeking approval for a weight and balance control program for aircraft operated under Title 14 of the Code of Federal Regulations (14 CFR) part 91, subpart K, 121, 125, or 135 should consult with the Flight Standards District Office (FSDO) or Certificate Management Office (CMO) that has jurisdiction in their area. Additional information on weight and balance for large aircraft can be found in Federal Aviation Administration (FAA) Advisory Circular (AC) 120-27, Aircraft Weight and Balance Control, FAA Type Certificate Data Sheets (TCDS), and the aircraft flight and maintenance manuals for specific aircraft.
Contents
- Establishing the Initial Weight of an Aircraft
- Determining the Empty Weight and Empty Weight CG (EWCG)
- Documenting Changes to an Aircraft’s Weight and Balance
- Airplane in Percent MAC
- Operational Empty Weight (OEW)
- Determining CG Changes Caused by Modifying the Cargo (Part 1)
- Determining CG Changes Caused by Modifying the Cargo (Part 2)
- Determining CG Changes Caused by Modifying the Cargo (Part 3)