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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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In the FlightDecide app since 2026-07-16. Reviewed 2026-09-28. 4 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.

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 (reference figure at 8000 ft, standard day). 4 of the 6 performance tables below are read from the published POH/AFM; 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.

Beechcraft Duchess 76 specs and key numbers

Not yet verified against the handbook

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
Service ceiling19,650 ft

Beechcraft Duchess 76 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
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

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)
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?

Not yet verified against the handbook: rate of climb

Figures read off the handbook's charts at 3900 lb, 0 ft pressure altitude, 10 °C. The rate of climb is an estimate, 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 roll930 ft
Takeoff over a 50 ft obstacle1970 ft
Landing ground roll980 ft
Landing over a 50 ft obstacle1860 ft
Rate of climb1250 fpm

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

Takeoff distance

ASSOCIATED CONDITIONS: POWER - TAKE-OFF POWER AT 2700 RPM SET BEFORE BRAKE RELEASE; MIXTURE - FULL RICH (ABOVE 5000 FT LEAN TO 75-100 F ON RICH SIDE OF PEAK EGT); FLAPS - UP; LANDING GEAR - RETRACT AFTER POSITIVE CLIMB ESTABLISHED; RUNWAY - PAVED, LEVEL, DRY SURFACE; COWL FLAPS - OPEN. TAKE-OFF SPEEDS (ALL WEIGHTS): LIFT-OFF 71 KNOTS, 50 FEET 80 KNOTS. Both engines operating (normal take-off sheet, not accelerate-stop or accelerate-go). Read at zero wind component; ground_roll_ft is the value carried straight across the obstacle-height reference line (0 ft), over_50ft_ft follows the obstacle-height guide lines to 50 ft.

Source: Pilot's Operating Handbook and FAA Approved Airplane Flight Manual, BEECHCRAFT Duchess 76 · P/N 105-590000-5 (revision 105-590000-5A7) · Takeoff

Ground roll (bold) and total distance over a 50 ft obstacle at 3,900 lb
Pressure altitude0 °C10 °C20 °C30 °C40 °C
Sea level860 / 1,825930 / 1,9701,010 / 2,1301,105 / 2,3401,215 / 2,585
1,000 ft985 / 2,0801,070 / 2,2551,155 / 2,4501,250 / 2,6601,370 / 2,910
2,000 ft1,110 / 2,3451,205 / 2,5601,300 / 2,7701,400 / 2,9901,520 / 3,245
3,000 ft1,240 / 2,6351,350 / 2,8701,460 / 3,1201,575 / 3,3901,700 / 3,710
4,000 ft1,370 / 2,9201,490 / 3,1851,615 / 3,4951,750 / 3,8201,890 / 4,160
5,000 ft1,530 / 3,2801,665 / 3,6201,810 / 3,9601,960 / 4,3302,120 / 4,760
6,000 ft1,690 / 3,6901,840 / 4,0402,000 / 4,4202,170 / 4,8902,360 / 5,410
7,000 ft1,867 / 4,1512,033 / 4,5092,210 / 4,9332,403 / 5,5222,627 / 6,149
8,000 ft2,062 / 4,6702,247 / 5,0322,442 / 5,5072,660 / 6,2372,925 / 6,988
9,000 ft2,278 / 5,2542,483 / 5,6162,698 / 6,1462,945 / 7,0433,256 / 7,943

read from the handbook's chart   extrapolated beyond the handbook

This handbook publishes performance as charts, not tables. Two people read these figures off its curves, independently, and they are shown only where the readings agreed, so they are close to what the chart shows rather than exact, within about 38 ft. Reading the chart's own worked example back from them comes out 6.1 ft from the answer it prints.

Landing distance

ASSOCIATED CONDITIONS: POWER - RETARD TO MAINTAIN 800 FT/MIN ON FINAL APPROACH; FLAPS - DOWN (DN); LANDING GEAR - DOWN; RUNWAY - PAVED, LEVEL, DRY SURFACE; APPROACH SPEED - 76 KNOTS IAS; BRAKING - MAXIMUM. Heading: APPROACH SPEED 76 KNOTS (ALL WEIGHTS). This sheet has no weight panel at all, so the distances are the same at every weight; they are recorded here at the 3900 lb reference weight. Read at zero wind component; ground_roll_ft is the value at the obstacle-height reference line (0 ft), over_50ft_ft follows the guide lines to 50 ft.

Source: Pilot's Operating Handbook and FAA Approved Airplane Flight Manual, BEECHCRAFT Duchess 76 · P/N 105-590000-5 (revision 105-590000-5A7) · Landing

Ground roll (bold) and total distance over a 50 ft obstacle at 3,900 lb
Pressure altitude0 °C10 °C20 °C30 °C40 °C
Sea level940 / 1,805980 / 1,8601,010 / 1,9101,050 / 1,9651,080 / 2,020
1,000 ft980 / 1,8601,020 / 1,9201,050 / 1,9751,090 / 2,0301,125 / 2,085
2,000 ft1,020 / 1,9201,060 / 1,9801,095 / 2,0401,130 / 2,0951,170 / 2,140
3,000 ft1,060 / 1,9801,100 / 2,0401,135 / 2,1001,170 / 2,1451,210 / 2,190
4,000 ft1,100 / 2,0501,140 / 2,1001,180 / 2,1501,210 / 2,1951,260 / 2,250
5,000 ft1,140 / 2,1101,180 / 2,1551,220 / 2,2001,260 / 2,2501,310 / 2,305
6,000 ft1,180 / 2,1501,220 / 2,2051,265 / 2,2551,310 / 2,3101,360 / 2,365
7,000 ft1,221 / 2,1911,261 / 2,2561,312 / 2,3111,362 / 2,3721,412 / 2,427
8,000 ft1,264 / 2,2321,304 / 2,3091,360 / 2,3691,416 / 2,4351,466 / 2,490
9,000 ft1,309 / 2,2751,348 / 2,3621,410 / 2,4281,472 / 2,5001,522 / 2,555

read from the handbook's chart   extrapolated beyond the handbook

This handbook publishes performance as charts, not tables. Two people read these figures off its curves, independently, and they are shown only where the readings agreed, so they are close to what the chart shows rather than exact, within about 25 ft. Reading the chart's own worked example back from them comes out 13.5 ft from the answer it prints.

Common Questions

Per the library's cruise table, not yet verified against the handbook, 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

Check today's wind against your personal crosswind maximum.

Density Altitude Calculator

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

The Go/No-Go Decision Framework

Fold these numbers into a structured preflight decision.

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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 2026-09-28.