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Cessna 177 Cardinal

V-speeds, cruise performance, fuel, and weights, digitized from the POH for planning and study.

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In the FlightDecide app since 2026-07-16. Reviewed 2026-09-28. 1 of 6 tables from the handbook. Anything marked “Not yet verified against the handbook” comes from FlightDecide's earlier library and hasn't been checked against the printed page.

Cessna 177 Cardinal preflight numbers at a glance: max gross weight 2500 lb, typical useful load 920 lb, 49 gal usable fuel, cruise up to about 130 KTAS (handbook figure at 8000 ft, standard day). 1 of the 6 performance tables below is read from the published POH/AFM and cites its figure and page; treat the ones marked “Not yet verified against the handbook” as estimates. Use them for planning and study, and confirm against the POH for your specific serial number before flight.

Cessna 177 Cardinal specs and key numbers

Not yet verified against the handbook: empty weight and useful load

EngineLycoming Model O-360-A1F6D
PropellerMcCauley B2D34C211/82PCA-6
Max gross weight2500 lb
Empty weight (typical)1580 lb
Useful load (typical)920 lb
Usable fuel49 gal
Service ceiling14,600 ft

Cessna 177 Cardinal V-speeds

Knots indicated (KIAS) unless the POH states otherwise. Speeds vary by model year and serial; the placarded speeds and your POH govern.

SpeedValueMeaning
VS045 ktStall, landing configuration
VS154 ktStall, clean configuration
VX65 ktBest angle of climb
VY79 ktBest rate of climb
VA102 ktDesign maneuvering speed (at max gross)
VFE90 ktMax flaps extended
VNO138 ktMax structural cruising
VNE167 ktNever exceed
Best glide75 ktBest glide speed

Cessna 177 Cardinal cruise performance

Transcribed from the handbook's cruise tables. True airspeed and fuel flow depend on altitude, power setting, temperature and leaning technique.

Source: Pilot's Operating Handbook, Cessna 1977 Cardinal, Cessna Model 177B (code D1084-13), Section 5 Performance, Figure 5-7 Cruise Performance, printed pages 5-17 to 5-22 = PDF pages 43 (right page) to 46 (left page) · Figure 5-7 · Cruise Performance · page 5-17 to 5-20

Cruise performance: 272 published rows
Pressure altitudeRPMMP (inHg)ISA-20 °CISAISA+20 °C
%TASGPH%TASGPH%TASGPH
2,000 ft2,1001847936.545926.344906.2
2,000 ft2,1001951986.949976.747966.6
2,000 ft2,10020551027.3531027.1511016.9
2,000 ft2,10021591067.8571067.5551067.3
2,000 ft2,10022631108.3611108.0591107.8
2,000 ft2,10023671148.8651148.5621138.2
2,000 ft2,10024711179.4681179.0661178.7
2,000 ft2,20021611098.1591097.9571087.6
2,000 ft2,20022661138.7631138.4611128.1
2,000 ft2,20023701169.3671168.9651168.6
2,000 ft2,20024741199.9711199.5691209.2
2,000 ft2,30021641118.4621118.2601117.9
2,000 ft2,30022681159.0661158.7641158.4
2,000 ft2,30023731189.7701189.3681189.0
2,000 ft2,300247712110.3741219.9721229.5
2,000 ft2,40021661138.7641138.4621138.1
2,000 ft2,40022701169.4681179.0661178.7
2,000 ft2,400237511910.0721209.6701209.3
2,000 ft2,400247612310.3741249.9
2,000 ft2,50021681148.9651148.6631148.3
2,000 ft2,50022721179.6701189.2671188.9
2,000 ft2,500237712010.3741219.9711229.5
2,000 ft2,500247812410.57612510.1
4,000 ft2,1001745916.343896.242866.0
4,000 ft2,1001849966.747956.545936.4
4,000 ft2,10019531017.1511016.949996.7
4,000 ft2,10020571067.5551057.3531047.1
4,000 ft2,10021611108.0591107.8571097.5
4,000 ft2,10022651148.6631138.3611138.0
4,000 ft2,10023691179.1671178.8641178.5
4,000 ft2,10024731209.7701219.3681219.0
4,000 ft2,20021641128.4611128.1591127.8
4,000 ft2,20022681169.0651168.6631168.3
4,000 ft2,20023721199.6691209.2671208.9
4,000 ft2,200247612210.2731239.8711239.4
4,000 ft2,30021661158.7641148.4621148.1
4,000 ft2,30022701189.3681189.0661188.7
4,000 ft2,300237512110.0721229.6701229.2
4,000 ft2,300247612510.2741259.8
4,000 ft2,40021681169.0661168.7631168.4
4,000 ft2,40022721209.7701209.3681208.9
4,000 ft2,400237712310.3741239.9721249.6
4,000 ft2,400247912710.67612710.2
4,000 ft2,50020651148.6631148.3611138.0
4,000 ft2,50021701189.2671188.9651188.6
4,000 ft2,50022741219.9721219.5691229.2
4,000 ft2,500237612510.2731259.8
6,000 ft2,1001746946.545926.343906.2
6,000 ft2,10018511006.849996.747976.5
6,000 ft2,10019551057.3531047.1511036.9
6,000 ft2,10020591097.8571097.5551087.3
6,000 ft2,10021631138.3611138.0591137.8
6,000 ft2,10022671178.8651178.5621178.2
6,000 ft2,10023711219.4681219.1661218.7
6,000 ft2,20020611128.1591117.8571117.6
6,000 ft2,20021661168.7631168.3611158.1
6,000 ft2,20022701209.3671208.9651198.6
6,000 ft2,20023741239.9711239.5691239.1
6,000 ft2,30020641148.4611148.1591137.8
6,000 ft2,30021681189.0651188.6631188.4
6,000 ft2,30022721229.6701229.2671228.9
6,000 ft2,300237712510.3741259.9711259.5
6,000 ft2,40020651168.6631168.3611158.1
6,000 ft2,40021701209.3671208.9651208.6
6,000 ft2,400227512310.0721249.6691249.2
6,000 ft2,400237612710.2741279.8
6,000 ft2,50020671178.9651178.5631178.3
6,000 ft2,50021721219.5691219.2671218.8
6,000 ft2,500227612510.3741259.8711259.5
6,000 ft2,500237812810.57512910.1
8,000 ft2,20019591117.8571107.6551097.3
8,000 ft2,20020631158.4611158.1591157.8
8,000 ft2,20021681208.9651198.6631198.3
8,000 ft2,20022721239.6691239.2671238.8
8,000 ft2,30019611138.0591127.8571127.5
8,000 ft2,30020651178.6631178.3611178.0
8,000 ft2,30021701219.3671218.9651218.6
8,000 ft2,30022741259.9721259.5691259.2
8,000 ft2,40019631158.3611148.0581147.7
8,000 ft2,40020671198.9651198.6631198.3
8,000 ft2,40021721239.6691239.2671238.9
8,000 ft2,400227712710.3741279.9711279.5
8,000 ft2,50019641178.5621168.2601167.9
8,000 ft2,50020691219.2671218.8641208.5
8,000 ft2,50021741259.9691259.1
8,000 ft2,500227912810.67612910.1731299.8
8,000 ft2,60019661188.7641188.4621178.1
8,000 ft2,60020711229.4681229.0661228.7
8,000 ft2,600217612610.2731279.7701279.4
8,000 ft2,600227813010.47513010.0
8,000 ft2,70018631158.3611158.0591147.8
8,000 ft2,70019681209.0661208.7631198.4
8,000 ft2,70020731249.7701249.3681249.0
8,000 ft2,700217512810.0721289.6

How much runway does a Cessna 177 Cardinal need?

Not yet verified against the handbook

Estimated figures at 2500 lb, 0 ft pressure altitude, 15 °C. These have not yet been re-checked against the handbook. Real-world technique, wind, surface, and density altitude move these substantially, so apply your own margin (many pilots use 1.5× the book number) and run the numbers for the actual conditions.

Estimated figureDistance
Takeoff ground roll890 ft
Takeoff over a 50 ft obstacle1335 ft
Landing ground roll440 ft
Landing over a 50 ft obstacle750 ft
Rate of climb840 fpm

See how density altitude stretches these distances on a hot day.

Common Questions

Per the POH cruise table, up to about 130 KTAS at 8000 ft on a standard day, burning roughly 10.4 GPH at that setting. Typical everyday cruise settings run slower and leaner; see the table above.

49 gallons usable. At a high-cruise burn of 10.4 GPH that is roughly 4.7 hours to dry tanks. Plan with reserves, never to zero.

About 920 lb for a typically equipped example (2500 lb max gross minus a typical empty weight of 1580 lb). Your aircraft's actual empty weight and CG come from its own weight-and-balance records. Always use those, not type averages.

VNE (never exceed) is 167 kt and VNO (max structural cruising) is 138 kt. Full V-speed table above; verify against the POH for your serial.

Plan a flight in this aircraft

Crosswind Calculator

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Density Altitude Calculator

See what heat and elevation do to these takeoff and climb numbers.

The Go/No-Go Decision Framework

Fold these numbers into a structured preflight decision.

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Reference data for planning and study: approximate, and not a substitute for the FAA-approved AFM/POH for your specific aircraft, an official weather briefing, or your judgment as pilot in command (14 CFR 91.3). Source: Cessna Model 177 and Cardinal Owner's Manual, Cessna Aircraft Company (1968 issue). Cruise performance rows transcribed verbatim from Section V Operational Data, Figure 5-4 Cruise & Range Performance, page 5-4. Conditions: 2350 Pounds Gross Weight, Standard Conditions, Zero Wind, Lean Mixture, 48 Gallons of Fuel (No Reserve). Engine red line (Lycoming O-320-E2D 150 HP): 2700 RPM, per POH Section III Operating Limitations. Data synced from the FlightDecide aircraft library on 2026-09-28.