V-speeds, cruise performance, fuel, and weights, digitized from the POH for planning and study.
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.
Not yet verified against the handbook
| Engine | Continental C-145-2 (145 HP) |
| Propeller | McCauley 1A175/GM8253 |
| Max gross weight | 2200 lb |
| Empty weight (typical) | 1410 lb |
| Useful load (typical) | 790 lb |
| Usable fuel | 37 gal |
| Service ceiling | 15,500 ft |
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.
| Speed | Value | Meaning |
|---|---|---|
| VS0 | 45 kt | Stall, landing configuration |
| VS1 | 50 kt | Stall, clean configuration |
| VX | 66 kt | Best angle of climb |
| VY | 76 kt | Best rate of climb |
| VA | 100 kt | Design maneuvering speed (at max gross) |
| VFE | 87 kt | Max flaps extended |
| VNO | 122 kt | Max structural cruising |
| VNE | 139 kt | Never exceed |
| Best glide | 61 kt | Best glide speed |
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) | RPM | TAS (kt) | Fuel (GPH) |
|---|---|---|---|
| 2000 | 1800 | 88.1 | 7 |
| 2000 | 2100 | 90.6 | 7.8 |
| 2000 | 2300 | 92.3 | 8.3 |
| 4000 | 1800 | 89.2 | 6.9 |
| 4000 | 2100 | 91.8 | 7.6 |
| 4000 | 2300 | 93.4 | 8.2 |
| 6000 | 1800 | 90.4 | 6.8 |
| 6000 | 2100 | 92.9 | 7.5 |
| 6000 | 2300 | 94.5 | 8 |
| 8000 | 1800 | 91.5 | 6.6 |
| 8000 | 2100 | 94 | 7.3 |
| 8000 | 2300 | 95.7 | 7.9 |
Standard-day (ISA) rows shown, sampled across the POH table for readability; the FlightDecide app carries the full digitized table, including non-standard temperatures.
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.
| Figure | Distance |
|---|---|
| Takeoff ground roll | 650 ft |
| Takeoff over a 50 ft obstacle | 1820 ft |
| Landing ground roll | 410 ft |
| Landing over a 50 ft obstacle | 1145 ft |
| Rate of climb | 690 fpm |
See how density altitude stretches these distances on a hot day.
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
| Pressure altitude | 0 °C | 10 °C | 20 °C | 30 °C | 40 °C |
|---|---|---|---|---|---|
| Sea level | 1,652 | 1,760 | 1,864 | 1,966 | 2,075 |
| 1,000 ft | 1,823 | 1,940 | 2,057 | 2,177 | 2,304 |
| 2,000 ft | 1,995 | 2,120 | 2,249 | 2,388 | 2,533 |
| 3,000 ft | 2,191 | 2,325 | 2,465 | 2,620 | 2,788 |
| 4,000 ft | 2,387 | 2,530 | 2,681 | 2,852 | 3,043 |
| 5,000 ft | 2,621 | 2,782 | 2,954 | 3,145 | 3,359 |
| 6,000 ft | 2,855 | 3,035 | 3,227 | 3,437 | 3,674 |
| 7,000 ft | 3,122 | 3,324 | 3,540 | 3,773 | 4,036 |
| 8,000 ft | 3,415 | 3,641 | 3,884 | 4,142 | 4,435 |
| 9,000 ft | 3,734 | 3,988 | 4,261 | 4,547 | 4,873 |
| 10,000 ft | 4,084 | 4,368 | 4,675 | 4,991 | 5,353 |
interpolated extrapolated beyond the handbook
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
| Pressure altitude | 0 °C | 10 °C | 20 °C | 30 °C | 40 °C |
|---|---|---|---|---|---|
| Sea level | 1,094 | 1,128 | 1,159 | 1,190 | 1,222 |
| 1,000 ft | 1,128 | 1,160 | 1,191 | 1,223 | 1,255 |
| 2,000 ft | 1,161 | 1,192 | 1,224 | 1,255 | 1,287 |
| 3,000 ft | 1,194 | 1,226 | 1,259 | 1,290 | 1,322 |
| 4,000 ft | 1,226 | 1,260 | 1,294 | 1,325 | 1,357 |
| 5,000 ft | 1,260 | 1,294 | 1,326 | 1,358 | 1,390 |
| 6,000 ft | 1,294 | 1,328 | 1,359 | 1,390 | 1,422 |
| 7,000 ft | 1,330 | 1,363 | 1,393 | 1,424 | 1,456 |
| 8,000 ft | 1,366 | 1,399 | 1,427 | 1,459 | 1,490 |
| 9,000 ft | 1,403 | 1,436 | 1,463 | 1,494 | 1,525 |
| 10,000 ft | 1,442 | 1,474 | 1,499 | 1,530 | 1,562 |
interpolated extrapolated beyond the handbook
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
| Pressure altitude | -20 °C | 0 °C | 20 °C | 40 °C |
|---|---|---|---|---|
| Sea level | 764 | 725 | 682 | 640 |
| 1,000 ft | 719 | 679 | 637 | 595 |
| 2,000 ft | 675 | 633 | 592 | 550 |
| 3,000 ft | 630 | 588 | 546 | 506 |
| 4,000 ft | 585 | 543 | 500 | 461 |
| 5,000 ft | 540 | 496 | 455 | 413 |
| 6,000 ft | 495 | 450 | 410 | 365 |
| 7,000 ft | 450 | 403 | 365 | 317 |
| 8,000 ft | 405 | 357 | 320 | 269 |
| 9,000 ft | 360 | 310 | 275 | 221 |
| 10,000 ft | 315 | 264 | 230 | 173 |
interpolated extrapolated beyond the handbook
Common QuestionsPer 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.
Check today's wind against your personal crosswind maximum.
See what heat and elevation do to these takeoff and climb numbers.
Fold these numbers into a structured preflight decision.
FlightDecide ships this aircraft as a built-in profile: it computes your fuel, weight and balance, and takeoff/landing performance for the actual conditions, scores 8 risk categories against your personal minimums, and explains the result in plain language.
Get FlightDecide on the App StoreReference 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.