V-speeds, cruise performance, fuel, and weights, digitized from the POH for planning and study.
Cessna 152 preflight numbers at a glance: max gross weight 1670 lb, typical useful load 590 lb, 24.5 gal usable fuel, cruise up to about 107 KTAS (POH figure at 8000 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.
| Engine | Lycoming O-235-L2C |
| Propeller | Sensenich 69EM6-0-56 |
| Max gross weight | 1670 lb |
| Empty weight (typical) | 1080 lb |
| Useful load (typical) | 590 lb |
| Usable fuel | 24.5 gal |
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 | 43 kt | Stall, landing configuration |
| VS1 | 48 kt | Stall, clean configuration |
| VX | 55 kt | Best angle of climb |
| VY | 67 kt | Best rate of climb |
| VA | 104 kt | Design maneuvering speed (at max gross) |
| VFE | 85 kt | Max flaps extended |
| VNO | 111 kt | Max structural cruising |
| VNE | 149 kt | Never exceed |
| Best glide | 60 kt | Best glide speed |
Transcribed from the POH cruise tables. True airspeed and fuel flow depend on altitude, power setting, temperature, and leaning technique.
| Pressure alt (ft) | RPM | % power | TAS (kt) | Fuel (GPH) |
|---|---|---|---|---|
| 2000 | 2000 | 47 | 80 | 3.9 |
| 2000 | 2200 | 59 | 91 | 4.8 |
| 2000 | 2400 | 75 | 101 | 6.1 |
| 4000 | 2000 | 46 | 80 | 3.8 |
| 4000 | 2300 | 63 | 95 | 5.1 |
| 4000 | 2450 | 75 | 103 | 6.1 |
| 6000 | 2000 | 45 | 79 | 3.7 |
| 6000 | 2300 | 60 | 95 | 4.9 |
| 6000 | 2500 | 75 | 105 | 6.1 |
| 8000 | 2100 | 48 | 83 | 3.9 |
| 8000 | 2400 | 64 | 99 | 5.2 |
| 8000 | 2550 | 75 | 107 | 6.1 |
| 10,000 | 2100 | 46 | 82 | 3.9 |
| 10,000 | 2300 | 56 | 93 | 4.5 |
| 10,000 | 2500 | 68 | 103 | 5.5 |
| 12,000 | 2100 | 45 | 81 | 3.8 |
| 12,000 | 2300 | 54 | 92 | 4.4 |
| 12,000 | 2450 | 62 | 100 | 5 |
Standard-day (ISA) rows shown, sampled across the POH table for readability; the FlightDecide app carries the full digitized table, including non-standard temperatures.
Book figures at 1670 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 figure | Distance |
|---|---|
| Takeoff ground roll | 746 ft |
| Takeoff over a 50 ft obstacle | 1297 ft |
| Landing ground roll | 371 ft |
| Landing over a 50 ft obstacle | 917 ft |
| Rate of climb | 681 fpm |
See how density altitude stretches these distances on a hot day.
Common QuestionsPer the POH cruise table, up to about 107 KTAS at 8000 ft on a standard day, burning roughly 6.1 GPH at that setting. Typical everyday cruise settings run slower and leaner; see the table above.
24.5 gallons usable. At a high-cruise burn of 6.1 GPH that is roughly 4.0 hours to dry tanks. Plan with reserves, never to zero.
About 590 lb for a typically equipped example (1670 lb max gross minus a typical empty weight of 1080 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 149 kt and VNO (max structural cruising) is 111 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 Model 152 Pilot's Operating Handbook, Cessna Aircraft Company (1978 issue). Cruise performance rows transcribed verbatim from Section 5 Performance, Figure 5-7 Cruise Performance, page 5-13. Conditions: 1670 lb, Recommended Lean Mixture at all altitudes. Engine red line (Lycoming O-235-L2C): 2550 RPM, Section 2 Limitations page 2-5. Data synced from the FlightDecide aircraft library on 2026-07-17.