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Beechcraft Bonanza A36

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

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Beechcraft Bonanza A36 preflight numbers at a glance: max gross weight 3600 lb, typical useful load 1236 lb, 74 gal usable fuel, cruise up to about 182 KTAS (POH figure at 10,000 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.

Beechcraft Bonanza A36 key numbers

EngineContinental IO-550-B (300 HP)
PropellerHartzell PHC-C3YF-2UF
Max gross weight3600 lb
Empty weight (typical)2364 lb
Useful load (typical)1236 lb
Usable fuel74 gal

Beechcraft Bonanza A36 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
VS059 ktStall, landing configuration
VS168 ktStall, clean configuration
VX84 ktBest angle of climb
VY100 ktBest rate of climb
VA141 ktDesign maneuvering speed (at max gross)
VFE124 ktMax flaps extended
VNO167 ktMax structural cruising
VNE205 ktNever exceed
Best glide110 ktBest glide speed

Beechcraft Bonanza A36 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)PowerMixtureTAS (kt)Fuel (GPH)
200021/2100best_power14811.5
200023/2300best_power15813.2
200025/2500best_power16615.2
400021/2100best_power15211.2
400023/2300best_power16212.9
400025/2500best_power17014.8
600021/2100best_power15610.9
600023/2300best_power16814
600025/2500best_power17616
800021/2100best_power16010.6
800023/2300best_power17213.2
800025/2500best_power18015.2
10,00021/2100best_power16310.3
10,00023/2300best_power17412.8
10,00025/2500best_power18214.7

How much runway does a Beechcraft Bonanza A36 need?

Book figures at 3600 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 roll1000 ft
Takeoff over a 50 ft obstacle1750 ft
Landing ground roll600 ft
Landing over a 50 ft obstacle1450 ft
Rate of climb1030 fpm

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

Common Questions

Per the POH cruise table, up to about 182 KTAS at 10,000 ft on a standard day, burning roughly 14.7 GPH at that setting. Typical everyday cruise settings run slower and leaner; see the table above.

74 gallons usable. At a high-cruise burn of 14.7 GPH that is roughly 5.0 hours to dry tanks. Plan with reserves, never to zero.

About 1236 lb for a typically equipped example (3600 lb max gross minus a typical empty weight of 2364 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 205 kt and VNO (max structural cruising) is 167 kt. Full V-speed table above; verify against the POH for your serial.

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Crosswind Calculator

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Density Altitude Calculator

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

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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: Beechcraft Bonanza A36 POH, Beechcraft/Textron Aviation. FD-125 audit (ADR-006, 2026-06-01): cruise rows tagged mixture_mode=best_power — current rows match the POH Section V Cruise Power Settings, Best Power Mixture sub-table; Best Economy Mixture sub-table digitization queued under constraint #5. Data synced from the FlightDecide aircraft library on 2026-07-17.