Beech 77 Skipper

Piston • single engine • Low Wing • Fixed gear

Range Visualization

Origin: · click map to move · nm at current load

Payload vs. Range

Customize assumptions

Avg. pax weight (lbs)

Default: 190 lbs (FAA standard)

Luggage per pax (lbs)

Default: 30 lbs

Passengers

lbs @ lbs / pax

Select payload

0 lbs

Fuel on board

gal

+ Weight

Range

Available Range / nm

Mission capable — Aircraft can handle the current load with full fuel tanks.

Fuel tradeoff required — You'll need to leave gallons of fuel behind ( gal usable for nm range).

Over max gross weight — Reduce payload by lbs to safely operate this aircraft.

Mission Profile

MOSAIC Eligibile Sport Pilot-flyable

105

KTAS

Cruise Speed

Occupants

412

Max Range

400

lbs

Wet Payload

Estimated Ownership Costs

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About the Beech 77 Skipper

The Beechcraft 77 Skipper is a two-seat, low-wing trainer introduced in 1979 to compete with the Cessna 152 and Piper Tomahawk. Distinctive for its T-tail and canopy-style cockpit, it utilized bonded metal construction and a NASA-developed GA(W)-1 airfoil.

Key Features for GA Buyers

Visibility: The bubble canopy provides superior visibility compared to high-wing competitors like the Cessna 150/152.
Cabin Comfort: The cabin is wider than average for its class, offering more shoulder room for students and instructors.
Handling: Known for light control forces and a “big airplane” feel due to its bonded wing construction and tubular spar.

Trade-offs

Performance: With only 115 HP, climb performance (720 fpm ideal, often lower in practice) is considered modest, especially at higher density altitudes.
Production Numbers: Only ~312 units were built before production ceased in 1981, making parts sourcing slightly more challenging than for ubiquitous Cessnas or Pipers.
Spin Recovery: The T-tail blankets the rudder during spins, requiring specific recovery inputs (though it is certified for spins).