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

Used market Only available used
117
KTAS
Cruise Speed
424
nm
Max Range
11,250
ft
Service Ceiling
2
Occupants
306
lbs
Wet Payload
Grumman American AA-1 (D-EBYU). Photo: Frank Schwichtenberg, CC BY 3.0.
Grumman American AA-1 (D-EBYU). Photo: Frank Schwichtenberg, CC BY 3.0.

Estimated Ownership Costs

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About the Grumman American AA1

Type certificated 1967 Source: FAA Type Certificate Data Sheet

Overview

The Grumman American AA-1 Yankee is a two-seat, fixed-gear, low-wing single produced from 1968 to 1978, the airplane that launched the bonded-aluminum Grumman light-aircraft line. Designed by Jim Bede as the BD-1 and certified by American Aviation, it pairs a rivet-free metal-bonded structure and a sliding canopy with a 108 hp Lycoming O-235, and earned a reputation as the sports car of two-seaters, faster and far more responsive than the Cessna and Piper trainers it competed with. The family runs from the original AA-1 Yankee through the AA-1A and AA-1B Trainer and TR-2 to the final AA-1C T-Cat and Lynx, the last of which moved to the 115 hp O-235-L2C.

The Yankee suits a pilot who already understands its tradeoffs and wants the speed and the sliding canopy anyway. It is not a primary trainer and it is not a four-seater: a Cessna 150 is friendlier for learning, and the Grumman Cheetah adds two seats and real range for not much more money. Its slick wing also carries a higher stall and steeper sink than those trainers, which is why it demands speed discipline on final and sits just outside sport-pilot eligibility. Bought clear-eyed as a low-cost sport two-seater, though, few airplanes return more fun per dollar.

Key Features for GA Buyers

  • Speed and responsiveness. Noticeably faster than a Cessna 150 or 152 on comparable power, with a high roll rate and light, sporty controls that owners prize.
  • Bubble canopy. The sliding canopy gives near-360-degree visibility and slides open on the ground for hot-day taxi.
  • Low-drag bonded airframe. The rivet-free metal-bonded structure is clean, simple, and easy to keep.
  • Low cost of ownership. A small O-235, simple systems, and an active owner community keep direct operating costs at the lower end of certificated two-seat singles.

Trade-offs

  • A demanding wing. The AA-1’s airfoil stalls higher and sinks faster than a typical trainer’s; let speed decay on final and it comes down quickly. Transition training is essential, and this is not a forgiving first airplane.
  • Not sport-pilot eligible. Clean stall at the certification-basis forward CG is about 60 KCAS, just above the 59 KCAS MOSAIC limit. Unlike the four-seat AA-5 siblings, the Yankee cannot be flown on a sport-pilot certificate.
  • Two people, short legs. With about 22 gallons usable and a modest useful load, it is strictly a two-person airplane with limited baggage and roughly 2.5 to 3 hours of endurance.
  • Free-castering nosewheel. Ground steering is by differential braking, a learning curve for pilots used to a steerable nosewheel.

See Also

Featured in our buying guides

Technical Specifications

Dimensions & Weights

Wingspan 24 ft
Height
7 ft
Length
19 ft
Parking area (ft²2)
835 ft²
Max Takeoff Weight
Source: FAA Type Certificate Data Sheet 1,500 lbs
Max Landing Weight
1,500 lbs
Useful Load
450 lbs
Fuel Capacity
Source: FAA Type Certificate Data Sheet 24 gal

Performance

Cruise Speed
117 KTAS
Never-Exceed (VNE)
Source: FAA Type Certificate Data Sheet 169 KIAS
Max Structural Cruise (VNO)
Source: FAA Type Certificate Data Sheet 125 KIAS
Approach Speed
74 KIAS
Stall, Clean (VS1)
Source: manufacturer figure 60 KIAS
Range
424 NM
Service Ceiling
11,250 ft
Rate of Climb
810 fpm
Takeoff over 50 ft obstacle
1,615 ft
Landing over 50 ft obstacle
1,240 ft

Engine

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Sources

Where the figures on this page come from. Grumman American AA1 specifications are traced to published references; estimated values are flagged inline next to the figure.

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