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Cessna 170B

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. 3 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 170B preflight numbers at a glance: max gross weight 2200 lb, typical useful load 790 lb, 37 gal usable fuel, cruise up to about 95.7 KTAS (reference figure at 8000 ft, standard day). 3 of the 6 performance tables below are read from the published POH/AFM and cite their 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 170B specs and key numbers

Not yet verified against the handbook

EngineContinental C-145-2 (145 HP)
PropellerMcCauley 1A175/GM8253
Max gross weight2200 lb
Empty weight (typical)1410 lb
Useful load (typical)790 lb
Usable fuel37 gal
Service ceiling15,500 ft

Cessna 170B V-speeds

Not yet verified against the handbook

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
VS150 ktStall, clean configuration
VX66 ktBest angle of climb
VY76 ktBest rate of climb
VA100 ktDesign maneuvering speed (at max gross)
VFE87 ktMax flaps extended
VNO122 ktMax structural cruising
VNE139 ktNever exceed
Best glide61 ktBest glide speed

Cessna 170B cruise performance

Not yet verified against the handbook

Source not verified: the library's record cites no handbook page for these rows. True airspeed and fuel flow depend on altitude, power setting, temperature, and leaning technique.

Pressure alt (ft)RPMTAS (kt)Fuel (GPH)
2000180088.17
2000210090.67.8
2000230092.38.3
4000180089.26.9
4000210091.87.6
4000230093.48.2
6000180090.46.8
6000210092.97.5
6000230094.58
8000180091.56.6
80002100947.3
8000230095.77.9

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 170B need?

Not yet verified against the handbook: takeoff ground roll and landing ground roll

Handbook figures at 2200 lb, 0 ft pressure altitude, 15.6 °C. The takeoff ground roll and landing ground roll are estimates, at 15 °C, not yet 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.

FigureDistance
Takeoff ground roll650 ft
Takeoff over a 50 ft obstacle1820 ft
Landing ground roll410 ft
Landing over a 50 ft obstacle1145 ft
Rate of climb690 fpm

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

Takeoff distance

Flaps up, full throttle, to clear a 50 ft. obstacle at 76 MPH TIAS, gross weight 2200 lb, zero wind, hard surface level runway. The handbook prints only the total distance over the 50 ft obstacle; it gives the ground run as a rule rather than a column ("Ground run approx. 40% distance shown"), so no ground-roll value is carried. Distances are reduced approximately 10% for each 6 m.p.h. of wind.

Source: Cessna 170 Owner's Manual, "52, 53, 54 and 55 Models" (form P213-13-RPC-200-3/79). Section V - Operational Data, Performance Information - Landplane, printed page 37 (PDF page 43) · Performance Information - Landplane: Take-off Distance (Ft.), Flaps Up · page 37

Total distance over a 50 ft obstacle at 2,200 lb
Pressure altitude0 °C10 °C20 °C30 °C40 °C
Sea level1,6521,7601,8641,9662,075
1,000 ft1,8231,9402,0572,1772,304
2,000 ft1,9952,1202,2492,3882,533
3,000 ft2,1912,3252,4652,6202,788
4,000 ft2,3872,5302,6812,8523,043
5,000 ft2,6212,7822,9543,1453,359
6,000 ft2,8553,0353,2273,4373,674
7,000 ft3,1223,3243,5403,7734,036
8,000 ft3,4153,6413,8844,1424,435
9,000 ft3,7343,9884,2614,5474,873
10,000 ft4,0844,3684,6754,9915,353

interpolated   extrapolated beyond the handbook

Landing distance

Flaps 40 deg, to land over a 50 ft. obstacle at 67 MPH TIAS approach, gross weight 2200 lb, zero wind, hard surface level runway. The handbook prints only the total distance over the 50 ft obstacle; it gives the ground roll as a rule rather than a column ("Roll 40% distance shown"), so no ground-roll value is carried. Distances are reduced approximately 10% for each 6 m.p.h. of wind.

Source: Cessna 170 Owner's Manual, "52, 53, 54 and 55 Models" (form P213-13-RPC-200-3/79). Section V - Operational Data, Performance Information - Landplane, printed page 37 (PDF page 43) · Performance Information - Landplane: Landing Distance (Ft.), Flaps 40 deg · page 37

Total distance over a 50 ft obstacle at 2,200 lb
Pressure altitude0 °C10 °C20 °C30 °C40 °C
Sea level1,0941,1281,1591,1901,222
1,000 ft1,1281,1601,1911,2231,255
2,000 ft1,1611,1921,2241,2551,287
3,000 ft1,1941,2261,2591,2901,322
4,000 ft1,2261,2601,2941,3251,357
5,000 ft1,2601,2941,3261,3581,390
6,000 ft1,2941,3281,3591,3901,422
7,000 ft1,3301,3631,3931,4241,456
8,000 ft1,3661,3991,4271,4591,490
9,000 ft1,4031,4361,4631,4941,525
10,000 ft1,4421,4741,4991,5301,562

interpolated   extrapolated beyond the handbook

Rate of climb

Flaps up, full throttle, gross weight 2200 lb, McCauley propeller. Best climb speed TIAS is printed beside the rows and is not carried as a field because it sits LEFT of the altitude column, outside the window the shared extractor reads: 89 MPH at sea level, 86 at 2000 ft, 84 at 4000 ft, 81 at 6000 ft, 79 at 7000 ft.

Source: Cessna 170 Owner's Manual, "52, 53, 54 and 55 Models" (form P213-13-RPC-200-3/79). Section V - Operational Data, Performance Information - Landplane, printed page 37 (PDF page 43) · Performance Information - Landplane: Normal Rate of Climb, Feet per min., Flaps Up · page 37

Rate of climb in feet per minute at 2,200 lb
Pressure altitude-20 °C0 °C20 °C40 °C
Sea level764725682640
1,000 ft719679637595
2,000 ft675633592550
3,000 ft630588546506
4,000 ft585543500461
5,000 ft540496455413
6,000 ft495450410365
7,000 ft450403365317
8,000 ft405357320269
9,000 ft360310275221
10,000 ft315264230173

interpolated   extrapolated beyond the handbook

Common Questions

Per the library's cruise table, not yet verified against the handbook, up to about 95.7 KTAS at 8000 ft on a standard day, burning roughly 7.9 GPH at that setting. Typical everyday cruise settings run slower and leaner; see the table above.

37 gallons usable. At a high-cruise burn of 7.9 GPH that is roughly 4.7 hours to dry tanks. Plan with reserves, never to zero.

About 790 lb for a typically equipped example (2200 lb max gross minus a typical empty weight of 1410 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 139 kt and VNO (max structural cruising) is 122 kt. Full V-speed table above; verify against the POH for your serial.

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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 170B Owner's Manual, Cessna Aircraft Company Data synced from the FlightDecide aircraft library on 2026-09-28.