Grumman American AA-5A Cheetah Weight and Balance Calculator
This calculator represents the AA-5A Cheetah normal-category configuration with standard tanks. Enter the current basic empty weight and arm from the certified weight and balance record for the individual aircraft.
Maximum takeoff weight: 2,200 lbs. Usable fuel represented: 37 US gal. Fuel arm: 90.9 in.
Data source: FAA TCDS A16EA and AA-5A Pilot's Operating Handbook. How WBcalc sources aircraft data
Enter the aircraft loading and fuel plan to check takeoff and expected landing conditions. After calculating, you can print or save the completed weight and balance worksheet as a PDF.
Grumman American AA-5A Cheetah (standard tanks) specifications
| Specification | Value |
|---|---|
| Maximum takeoff weight | 2,200 lbs |
| Maximum landing weight | 2,200 lbs |
| Forward CG at 1,780 lbs or less | 81 in |
| Forward CG at 2,200 lbs | 85.6 in |
| Aft CG limit | 92.5 in |
| Usable fuel | 37 US gal |
| Fuel arm | 90.9 in |
Source: FAA TCDS A16EA and AA-5A Pilot's Operating Handbook.
Grumman American AA-5A Cheetah (standard tanks) CG limits
| Aircraft weight | Forward CG limit | Aft CG limit |
|---|---|---|
| 1,780 lbs | 81 in | 92.5 in |
| 2,200 lbs | 85.6 in | 92.5 in |
The calculator uses the published CG envelope points and linear interpolation between forward-limit breakpoints where applicable.
Grumman American AA-5A Cheetah (standard tanks) loading stations
| Station | Arm | Limit |
|---|---|---|
| Front seats | 90.6 in | |
| Rear seats | 126 in | |
| Baggage | 148 in | 120 lbs |
Grumman American AA-5A Cheetah (standard tanks) fuel capacity
This calculator uses 37 US gallons of usable fuel at an arm of 90.9 inches.
Grumman American AA-5A Cheetah (standard tanks) baggage limits
Baggage is limited to 120 lbs
Normal category limits
The CG envelope on this page is for the normal category.
About this Grumman American AA-5A Cheetah (standard tanks) configuration
This page represents the normal-category Grumman American AA-5A Cheetah (standard tanks) configuration identified in FAA TCDS A16EA and AA-5A Pilot's Operating Handbook. The calculator uses a maximum takeoff weight of 2,200 lb and 37 US gal of usable fuel.
The reference datum for the loading arms on this page is Datum defined by FAA TCDS A16EA.
Need help with the terminology? Read the aircraft weight and balance guide or the CG envelope guide.
Related aircraft
Grumman American AA-5B Tiger, American General AG-5B Tiger, Grumman American AA-5 Traveler
Grumman American AA-5A Cheetah (standard tanks) FAQ
What maximum takeoff weight does this Grumman American AA-5A Cheetah (standard tanks) calculator use?
This calculator uses a maximum takeoff weight of 2,200 lb for the configuration identified on this page.
How much usable fuel is represented for the Grumman American AA-5A Cheetah (standard tanks)?
This page uses up to 37 US gal of usable fuel at an arm of 90.9 in.
What baggage limit is represented for the Grumman American AA-5A Cheetah (standard tanks)?
Baggage is limited to 120 lb on this page.
Source and applicability
Source: FAA TCDS A16EA and AA-5A Pilot's Operating Handbook. Check the current POH or AFM, aircraft weight and balance record, equipment list and applicable supplements for the individual aircraft.
WBcalc is a planning aid. Check the current POH or AFM, aircraft weight and balance record, equipment list and applicable supplements before flight.
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