Aircraft › Grumman American › AA-5 Series › AA-5
The Grumman American AA-5 Traveler is a four-seat, low-wing, fixed-tricycle-gear piston single in the AA-5 family. The source-linked WBcalc configuration uses a 2,200 lb maximum takeoff and landing weight and 37 U.S. gallons of usable fuel.
Grumman American AA-5 Weight and Balance Calculator →
Grumman American AA-5 specifications
| Manufacturer | Grumman American |
|---|---|
| Model | AA-5 |
| Production years | 1972–1975 |
| Aircraft type | Four-seat piston single |
| Seats | 4 |
| Engine | Lycoming O-320 series |
| Landing gear | Fixed tricycle |
| Certification | FAA A16EA |
Grumman American AA-5 weights and capacities
| Maximum takeoff weight | 2,200 lb |
|---|---|
| Maximum landing weight | 2,200 lb |
| Maximum baggage | 120 lb combined |
Grumman American AA-5 history and development
The AA-5 Traveler is associated with the 1972–1975 production period and is certificated under FAA Type Certificate Data Sheet A16EA.
The Traveler was followed within the AA-5 lineage by the AA-5A Cheetah and higher-powered AA-5B Tiger.
Grumman American AA-5 certification and applicability
| FAA type certificate | A16EA |
|---|---|
| Production period | 1972–1975 |
| Category | Normal |
Grumman American AA-5 fuel capacity
The source-linked AA-5 Traveler configuration represents 37 U.S. gallons of usable fuel at an arm of 90.9 inches.
Fuel quantity is part of the loading calculation, not just a capacity specification. The represented 37 U.S. gallons of usable fuel must be combined with the aircraft's current empty weight, occupants and baggage when evaluating loaded weight and center of gravity.
Grumman American AA-5 model applicability and configuration
The specifications on this page describe the source-linked normal-category AA-5 Traveler configuration. Individual aircraft may differ because of approved modifications and equipment changes.
Grumman AA-5 Traveler vs AA-5A Cheetah
| Specification | AA-5 Traveler | AA-5A Cheetah |
|---|---|---|
| Engine family | Lycoming O-320 | Lycoming O-320 |
| Maximum weight represented | 2,200 lb | 2,200 lb |
| Usable fuel represented | 37 US gal | 37 US gal |
Grumman American AA-5 weight and balance
The source-linked AA-5 calculator represents a maximum takeoff and landing weight of 2,200 lb, 37 U.S. gallons of usable fuel and a 120 lb baggage limit.
The model-level reference identifies a 120 lb maximum combined baggage load. The actual aircraft loading condition must remain within both the represented weight limit and the applicable center-of-gravity envelope.
Open Grumman American AA-5 Weight and Balance Calculator →
Grumman American AA-5 frequently asked questions
What is the maximum takeoff weight of the Grumman AA-5 Traveler?
The source-linked configuration represented by WBcalc uses a maximum takeoff weight of 2,200 lb.
How much usable fuel does the AA-5 Traveler configuration hold?
The represented configuration uses 37 U.S. gallons of usable fuel.
What engine family is associated with the AA-5 Traveler?
FAA records identify the AA-5 with the Lycoming O-320 engine series; exact installed-engine applicability should be verified for the individual aircraft.
Reference sources
FAA: Type Certificate Data Sheet A16EA
WBcalc source-linked calculator dataset: grumman/aa-5-traveler
Related AA-5 Series models
- Grumman American AA-5A - 1976–1979
- Grumman American AA-5B - 1975–1979