Aircraft › Grumman American › AA-5 Series › AA-5A
The Grumman American AA-5A Cheetah is a four-seat, low-wing, fixed-tricycle-gear member of the AA-5 series. WBcalc represents the normal-category standard-tank configuration.
Grumman American AA-5A Weight and Balance Calculator →
Grumman American AA-5A specifications
| Manufacturer | Grumman American |
|---|---|
| Model | AA-5A |
| Production years | 1976–1979 |
| Aircraft type | Four-seat piston single |
| Seats | 4 |
| Engine | Lycoming O-320 series |
| Landing gear | Fixed tricycle |
| Certification | FAA A16EA |
Grumman American AA-5A weights and capacities
| Maximum takeoff weight | 2,200 lb |
|---|---|
| Maximum landing weight | 2,200 lb |
| Maximum baggage | 120 lb combined |
Fuel capacity and configuration
| Fuel | Applies to the standard-tank configuration represented by the WBcalc calculator. |
|---|
Grumman American AA-5A history and development
The AA-5A Cheetah is associated with the 1976–1979 production period and is certificated under FAA Type Certificate Data Sheet A16EA.
Within the AA-5 lineage it sits between the earlier Traveler and the higher-powered AA-5B Tiger.
Grumman American AA-5A certification and applicability
| FAA type certificate | A16EA |
|---|---|
| Catalog production period | 1976–1979 |
| Represented fuel configuration | Standard tanks |
Grumman American AA-5A fuel capacity
The standard-tank configuration represented by WBcalc uses 37 U.S. gallons of usable fuel at an arm of 90.9 inches.
Grumman American AA-5A configurations and applicability
Standard-tank configuration
Applicability: AA-5A Cheetah configuration represented by FAA TCDS A16EA and the source-linked operating data.
| Maximum takeoff weight | 2,200 lb |
|---|---|
| Maximum landing weight | 2,200 lb |
| Usable fuel | 37 US gal |
Configuration sources: FAA: Type Certificate Data Sheet A16EA · Grumman American: AA-5A Pilot's Operating Handbook
Grumman American AA-5A model applicability and configuration
The linked calculator is specifically scoped to the AA-5A standard-tank configuration. Fuel-system modifications or other approved changes must be evaluated from the applicable aircraft documentation.
Grumman AA-5A Cheetah vs AA-5B Tiger
| Specification | AA-5A Cheetah | AA-5B Tiger |
|---|---|---|
| Engine family | Lycoming O-320 | Lycoming O-360 |
| Maximum weight represented | 2,200 lb | 2,400 lb |
| Usable fuel represented | 37 US gal | 51 US gal |
Grumman American AA-5A weight and balance
The represented standard-tank AA-5A configuration uses a 2,200 lb maximum takeoff and landing weight, 37 U.S. gallons usable fuel and a 120 lb baggage limit.
Open Grumman American AA-5A Weight and Balance Calculator →
Grumman American AA-5A frequently asked questions
What maximum takeoff weight does the represented AA-5A Cheetah use?
The source-linked standard-tank configuration uses a maximum takeoff weight of 2,200 lb.
How much usable fuel does the represented AA-5A hold?
The standard-tank configuration represented by WBcalc uses 37 U.S. gallons of usable fuel.
What engine family is associated with the AA-5A Cheetah?
FAA records identify the AA-5A with the Lycoming O-320 engine series.
Reference sources
FAA: Type Certificate Data Sheet A16EA
Grumman American: AA-5A Pilot's Operating Handbook
Related AA-5 Series models
- Grumman American AA-5 - 1972–1975
- Grumman American AA-5B - 1975–1979