Cessna 177 Cardinal

Piston • single engine • High Wing • Fixed gear

Range Visualization

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Payload vs. Range

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Default: 190 lbs (FAA standard)

Default: 30 lbs

Passengers
lbs @ lbs / pax
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
124
KTAS
Cruise Speed
4
Occupants
604
nm
Max Range
715
lbs
Wet Payload

Estimated Ownership Costs

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About the Cessna 177 Cardinal

Overview

The Cessna 177 Cardinal was designed in the mid-1960s as Cessna’s intended successor to the Skyhawk: a cleaner-looking, more modern four-seat single with a cantilever wing and forward-positioned cabin. The 1968 debut at 150 hp was widely judged underpowered, which damaged the type’s reputation early and is part of why the Cardinal never displaced the 172 in the role it was built for. The 1970 177B revision, which standardized the 180 hp Lycoming O-360, fixed the original criticism and is the variant whose specifications the catalogue reflects.

What remains is a four-seat single with a distinctive cabin proposition. The strutless high wing and the pilot’s seating position forward of the wing’s leading edge produce visibility unusual for a high-wing GA aircraft. The 90-degree doors and low cabin floor make entry and exit notably easier than in a Skyhawk. Production ended in 1978 with the C-model. Used-market liquidity is meaningfully thinner than the 172’s, but the type retains a committed owner community and a deep type-specific support base.

Key Features for GA Buyers

  • Visibility. Without wing struts and with the pilot sitting forward of the wing’s leading edge, the Cardinal offers a panoramic view that no other production high-wing single matches.
  • Cabin Access. The 90-degree doors and the absence of a wing strut to step over make boarding meaningfully easier than in any other Cessna single in the same class.
  • Cabin Dimensions. The cabin is wider than a Skyhawk’s and the floor is flat, which materially affects long-flight comfort for pilots and passengers.
  • Type-Specific Owner Support. The Cessna Cardinal Flyers Association is one of the deeper single-type owner communities in GA, which is consequential for SID inspection guidance, PIO training resources, and parts-sourcing knowledge.

Trade-offs

  • Pitch Sensitivity. The all-moving stabilator is more responsive than a conventional elevator and is the source of the Cardinal’s reputation for pilot-induced oscillations in the flare. Type-specific landing training meaningfully reduces this; without it, the issue is real.
  • Payload vs. Range. With 50-gallon standard or 61-gallon optional tanks, filling to the brim leaves limited margin for passengers and bags. Full-fuel, four-adult flights are rarely feasible.
  • SID Inspection Burden. The strutless cantilever-wing design requires the Cessna SID wing-carry-through corrosion inspection, which is more involved than the structural checks on strut-braced Cessnas. Pre-purchase scope and ongoing inspection cost both reflect this.
  • Used-Market Depth. Production ended in 1978, the fleet is finite, and 150 hp versus 180 hp variants do not trade interchangeably. Buyers should price the variant, not the model line.

See Also

  • Cessna 177RG Cardinal RG – the retractable evolution: 200 hp fuel-injected, roughly 24 KTAS faster, complex/high-performance training required. Compare
  • Cessna Skyhawk 172/Cutlass – the Skyhawk the Cardinal was designed to succeed: less distinctive, more numerous, deeper parts and training infrastructure. Compare
  • Cessna Skylane 182 – the in-line step-up: 230 hp, higher useful load, higher ceiling, materially more capable cross-country platform. Compare
  • Piper Cherokee Warrior II – the low-wing fixed-gear class competitor: similar power and mission, opposite handling and visibility character. Compare
  • Grumman American AA5B Tiger – the fixed-gear low-wing alternative with notably strong cruise for its power: a different design philosophy reaching a similar mission profile. Compare

Featured in our buying guides

Technical Specifications

Dimensions

Wingspan
35.5 ft
Length
27.67 ft
Height
8.58 ft
Parking area (ft2)
1486.49 ft2

Weights

Max Takeoff Weight
2,500 lbs
Max Landing Weight
2,500 lbs
Useful Load
1,015 lbs
Fuel Capacity
50 gal

Performance

Cruise Speed
124 KTAS
Never-Exceed (Vne)
164 KIAS
Max Structural Cruise (Vno)
124 KIAS
Approach Speed
70 KIAS
Stall, Clean (Vs1)
55 KIAS
Range
604 NM
Service Ceiling
14,600 ft
Rate of Climb
670 - 840 fpm
Takeoff over 50 ft obstacle
1,400 ft
Landing ground roll
1,220 ft

Engine

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