Aircraft Weight and Balance HandbookFAA-H-8083-1B
Appendix B
Key Weight and Balance Locations on an Aircraft
2 pagesPages B-1–B-2
- Station 0 Station 50 Station 0 Station 70 10 lb
- MAC
- (+)
- Arm
- (–)
- Arm
- (+)
- Arm
- (+) Arm
- 70"
- TEMAC
- LEMAC
- Aft limit Forward limit Datum
- MAC
- TEM
- LEM
- CG
- CG range
- (–)
- A
- (+)
- A
- Aft lim
- Forward Multiengine aircraft Single-engine aircraft
- Datum
- Datum
- Weight Moment = 700 lb–in