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Empty weight
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The empty weight of plane is based on its weight without any payload (cargo, passengers, usable fuel, etc.).[1][2]
Standards
Many different empty weight definitions exist. Here are some of the more common ones used.
GAMA standardization
In 1975 (or 1976 per FAA-H-8083-1B) [3] the General Aviation Manufacturers Association (GAMA) standardized the definition of empty weight terms for Pilot Operating Handbooks as follows:
Standard Empty Weight | |
+ | Optional Equipment |
| |
Basic Empty Weight |
Standard Empty Weight includes the following:
- Empty weight of the airplane
- Full Hydraulic Fluid
- Unusable Fuel
- Full Oil
Optional Equipment includes the following:
- All equipment installed beyond standard
Non-GAMA usage
Previously (Regarding aircraft certified under CAR Part 3)[4] the following were commonly used to define empty weights:
Empty Weight | |
+ | Unusable Fuel |
| |
Standard Empty Weight |
Standard Empty Weight | |
+ | Optional Equipment |
| |
Licensed Empty Weight |
In this definition Empty Weight includes the following:
- Empty weight of the airplane
- Undrainable Oil
- Full Hydraulic Fluid
Note that weight of oil must be added to Licensed Empty Weight for it to be equivalent to Basic Empty Weight
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See also
References
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