Range Map

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1

Tank-dry, where fuel runs out at catalogue's stored cruise burn.

Excludes reserves: range beyond the dashed circle requires a leaner cruise than what we store. Great-circle, still air, book cruise. Estimates only: always verify against the POH.

Payload vs. Range

Occupants:

Fuel on board

Cargo

nm

Range

Cargo is additional payload after occupants and baggage.
full tanks
Available Range / nm
Mission capable. This load flies with full fuel.
Fuel reduced by . left aboard for nm range.
Over max payload by . At this load it cannot lift a single occupant.

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Mission Profile

MOSAIC Eligible
Used market Only available used
121
KTAS
Cruise Speed
430
nm
Max Range
12,650
ft
Service Ceiling
4
Occupants
485
lbs
Wet Payload
Grumman AA-5 Traveler (D-EAXA) at Uetersen. Photo: Frank Schwichtenberg, CC BY-SA 3.0.
Grumman AA-5 Traveler (D-EAXA) at Uetersen. Photo: Frank Schwichtenberg, CC BY-SA 3.0.

Estimated Ownership Costs

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About the Grumman American AA5

Type certificated 1971 Source: FAA Type Certificate Data Sheet

Overview

The Grumman American AA-5 Traveler is a four-seat, fixed-gear, low-wing single built from 1972 to 1975, the first four-place development of the two-seat AA-1 Yankee. It carried the line’s signature engineering up to family size: a bonded aluminum-honeycomb structure with almost no rivets, a tubular-spar wing, and a sliding canopy. American Aviation launched it, and Grumman American continued it after the 1972 merger; more than 800 were built before the refined Cheetah took its place.

The Traveler is the entry point to four-seat Grumman ownership. It runs the same 150 hp Lycoming O-320 as the Cheetah but sells for less and gives up only a few knots, so it cross-shops against the high-wing Cessna 172 and the Piper Cherokee of the same years, trading their strut-braced familiarity for sharper controls, a lower stance, and far better visibility under the canopy. A buyer who wants Grumman handling on the smallest budget, and can live with the early small-elevator pitch sensitivity and the shorter standard-tank range, will find this the cheapest way into the airframe; pilots who fly longer legs or want crisper manners in the flare usually move up to the Cheetah or Tiger.

Key Features for GA Buyers

  • Sports-car handling for the class. Light, responsive controls and a high roll rate give the Traveler a livelier feel than its high-wing contemporaries.
  • Bonded, rivet-free airframe. The metal-bonded wing and honeycomb fuselage produce a clean, low-drag surface that is easy to inspect and wash, and contribute to the type’s speed-per-horsepower.
  • Visibility and access. The sliding canopy offers a near-360-degree view and can be cracked open for ground taxi, something neither a Cessna nor a Piper cabin can match.
  • Fold-flat cargo. The rear seats fold to open a large flat cargo bay behind the cabin.

Trade-offs

  • Pitch sensitivity. The Traveler’s smaller elevator makes it more sensitive in pitch during the landing flare than the later Cheetah and Tiger, which received a larger surface. Transition training matters.
  • Standard tanks limit range. With 37 gallons (36 usable) in standard tanks, the Traveler has shorter legs than the Cheetah on long-range tanks or the Tiger. Plan fuel stops accordingly.
  • Density-altitude performance. 150 hp moving a true four-seat cabin means climb and takeoff suffer on hot, high days, especially near gross.

See Also

Technical Specifications

Dimensions & Weights

Wingspan 31 ft
Height
8 ft
Length
22 ft
Parking area (ft²2)
1,118 ft²
Max Takeoff Weight
Source: FAA Type Certificate Data Sheet 2,200 lbs
Max Landing Weight
2,200 lbs
Useful Load
707 lbs
Fuel Capacity
Source: FAA Type Certificate Data Sheet 37 gal

Performance

Cruise Speed
121 KTAS
Never-Exceed (VNE)
Source: FAA Type Certificate Data Sheet 165 KIAS
Max Structural Cruise (VNO)
Source: FAA Type Certificate Data Sheet 130 KIAS
Approach Speed
70 KIAS
Stall, Clean (VS1)
Source: manufacturer figure 54 KIAS
Range
430 NM
Service Ceiling
12,650 ft
Rate of Climb
660 fpm
Takeoff over 50 ft obstacle
1,600 ft
Landing over 50 ft obstacle
1,100 ft

Engine

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Sources

Where the figures on this page come from. Grumman American AA5 specifications are traced to published references; estimated values are flagged inline next to the figure.

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