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Cessna 175 Skylark

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

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Cessna 175 Skylark preflight numbers at a glance: max gross weight 2350 lb, typical useful load 850 lb, 52 gal usable fuel, cruise up to about 120 KTAS (POH figure at 6000 ft, standard day). All figures below come from the FlightDecide curated aircraft library, digitized from the published POH/AFM. Use them for planning and study, and confirm against the POH for your specific serial number before flight.

Cessna 175 Skylark key numbers

EngineContinental GO-300-E (175 HP)
PropellerMcCauley 7557
Max gross weight2350 lb
Empty weight (typical)1500 lb
Useful load (typical)850 lb
Usable fuel52 gal

Cessna 175 Skylark 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
VS047 ktStall, landing configuration
VS154 ktStall, clean configuration
VX76 ktBest angle of climb
VY88 ktBest rate of climb
VA107 ktDesign maneuvering speed (at max gross)
VFE87 ktMax flaps extended
VNO122 ktMax structural cruising
VNE153 ktNever exceed
Best glide72 ktBest glide speed

Cessna 175 Skylark cruise performance

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

Pressure alt (ft)RPMTAS (kt)Fuel (GPH)
200026001067.7
200029001148.5
200031001189.1
400026001077.5
400029001158.3
400031001198.9
600026001087.4
600029001168.2
600031001208.8
800026001087.2
800029001178.1
800031001208.6

Standard-day (ISA) rows shown, sampled across the POH table for readability; the FlightDecide app carries the full digitized table, including non-standard temperatures.

How much runway does a Cessna 175 Skylark need?

Book figures at 2350 lb, 0 ft pressure altitude, 15 °C. 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.

POH figureDistance
Takeoff ground roll890 ft
Takeoff over a 50 ft obstacle1335 ft
Landing ground roll430 ft
Landing over a 50 ft obstacle730 ft
Rate of climb850 fpm

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

Common Questions

Per the POH cruise table, up to about 120 KTAS at 6000 ft on a standard day, burning roughly 8.8 GPH at that setting. Typical everyday cruise settings run slower and leaner; see the table above.

52 gallons usable. At a high-cruise burn of 8.8 GPH that is roughly 5.9 hours to dry tanks. Plan with reserves, never to zero.

About 850 lb for a typically equipped example (2350 lb max gross minus a typical empty weight of 1500 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 153 kt and VNO (max structural cruising) is 122 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 175 Skylark Owner's Manual, Cessna Aircraft Company Data synced from the FlightDecide aircraft library on 2026-07-17.