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Beechcraft Duchess 76

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

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Beechcraft Duchess 76 preflight numbers at a glance: max gross weight 3900 lb, typical useful load 1370 lb, 100 gal usable fuel, cruise up to about 158.5 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.

Beechcraft Duchess 76 key numbers

Engine2x Lycoming O-360-A1G6D (180 HP each)
PropellerHartzell HC-C2YR-2/C8475-0 (2x)
Max gross weight3900 lb
Empty weight (typical)2530 lb
Useful load (typical)1370 lb
Usable fuel100 gal

Beechcraft Duchess 76 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
VS060 ktStall, landing configuration
VS170 ktStall, clean configuration
VX71 ktBest angle of climb
VY85 ktBest rate of climb
VXSE85 ktBest angle of climb, single engine
VYSE85 ktBest rate of climb, single engine
VA132 ktDesign maneuvering speed (at max gross)
VFE110 ktMax flaps extended
VNO154 ktMax structural cruising
VNE194 ktNever exceed
VMC65 ktMin control, one engine inoperative
Best glide95 ktBest glide speed

Beechcraft Duchess 76 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)
20002200146.516.5
2000250015118
2000270015419
4000220014816.4
40002500152.517.9
40002700155.518.9
60002200149.516.2
6000250015417.7
6000270015718.7
8000220015116.1
80002500155.517.6
80002700158.518.6

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 Beechcraft Duchess 76 need?

Book figures at 3900 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 roll1280 ft
Takeoff over a 50 ft obstacle1855 ft
Landing ground roll590 ft
Landing over a 50 ft obstacle1005 ft
Rate of climb1250 fpm

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

Common Questions

Per the POH cruise table, up to about 158.5 KTAS at 8000 ft on a standard day, burning roughly 18.6 GPH at that setting. Typical everyday cruise settings run slower and leaner; see the table above.

100 gallons usable. At a high-cruise burn of 18.6 GPH that is roughly 5.4 hours to dry tanks. Plan with reserves, never to zero.

About 1370 lb for a typically equipped example (3900 lb max gross minus a typical empty weight of 2530 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 194 kt and VNO (max structural cruising) is 154 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

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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 Duchess 76 Pilot's Operating Handbook, Beechcraft Corporation Data synced from the FlightDecide aircraft library on 2026-07-17.