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.
Not yet verified against the handbook
| Engine | 2x Lycoming O-360-A1G6D (180 HP each) |
| Propeller | Hartzell HC-C2YR-2/C8475-0 (2x) |
| Max gross weight | 3900 lb |
| Empty weight (typical) | 2530 lb |
| Useful load (typical) | 1370 lb |
| Usable fuel | 100 gal |
| Service ceiling | 19,650 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 | 60 kt | Stall, landing configuration |
| VS1 | 70 kt | Stall, clean configuration |
| VX | 71 kt | Best angle of climb |
| VY | 85 kt | Best rate of climb |
| VXSE | 85 kt | Best angle of climb, single engine |
| VYSE | 85 kt | Best rate of climb, single engine |
| VA | 132 kt | Design maneuvering speed (at max gross) |
| VFE | 110 kt | Max flaps extended |
| VNO | 154 kt | Max structural cruising |
| VNE | 194 kt | Never exceed |
| VMC | 65 kt | Min control, one engine inoperative |
| Best glide | 95 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 | 2200 | 146.5 | 16.5 |
| 2000 | 2500 | 151 | 18 |
| 2000 | 2700 | 154 | 19 |
| 4000 | 2200 | 148 | 16.4 |
| 4000 | 2500 | 152.5 | 17.9 |
| 4000 | 2700 | 155.5 | 18.9 |
| 6000 | 2200 | 149.5 | 16.2 |
| 6000 | 2500 | 154 | 17.7 |
| 6000 | 2700 | 157 | 18.7 |
| 8000 | 2200 | 151 | 16.1 |
| 8000 | 2500 | 155.5 | 17.6 |
| 8000 | 2700 | 158.5 | 18.6 |
Standard-day (ISA) rows shown, sampled across the POH table for readability; the FlightDecide app carries the full digitized table, including non-standard temperatures.
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.
| Figure | Distance |
|---|---|
| Takeoff ground roll | 930 ft |
| Takeoff over a 50 ft obstacle | 1970 ft |
| Landing ground roll | 980 ft |
| Landing over a 50 ft obstacle | 1860 ft |
| Rate of climb | 1250 fpm |
See how density altitude stretches these distances on a hot day.
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
| Pressure altitude | 0 °C | 10 °C | 20 °C | 30 °C | 40 °C |
|---|---|---|---|---|---|
| Sea level | 860 / 1,825 | 930 / 1,970 | 1,010 / 2,130 | 1,105 / 2,340 | 1,215 / 2,585 |
| 1,000 ft | 985 / 2,080 | 1,070 / 2,255 | 1,155 / 2,450 | 1,250 / 2,660 | 1,370 / 2,910 |
| 2,000 ft | 1,110 / 2,345 | 1,205 / 2,560 | 1,300 / 2,770 | 1,400 / 2,990 | 1,520 / 3,245 |
| 3,000 ft | 1,240 / 2,635 | 1,350 / 2,870 | 1,460 / 3,120 | 1,575 / 3,390 | 1,700 / 3,710 |
| 4,000 ft | 1,370 / 2,920 | 1,490 / 3,185 | 1,615 / 3,495 | 1,750 / 3,820 | 1,890 / 4,160 |
| 5,000 ft | 1,530 / 3,280 | 1,665 / 3,620 | 1,810 / 3,960 | 1,960 / 4,330 | 2,120 / 4,760 |
| 6,000 ft | 1,690 / 3,690 | 1,840 / 4,040 | 2,000 / 4,420 | 2,170 / 4,890 | 2,360 / 5,410 |
| 7,000 ft | 1,867 / 4,151 | 2,033 / 4,509 | 2,210 / 4,933 | 2,403 / 5,522 | 2,627 / 6,149 |
| 8,000 ft | 2,062 / 4,670 | 2,247 / 5,032 | 2,442 / 5,507 | 2,660 / 6,237 | 2,925 / 6,988 |
| 9,000 ft | 2,278 / 5,254 | 2,483 / 5,616 | 2,698 / 6,146 | 2,945 / 7,043 | 3,256 / 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.
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
| Pressure altitude | 0 °C | 10 °C | 20 °C | 30 °C | 40 °C |
|---|---|---|---|---|---|
| Sea level | 940 / 1,805 | 980 / 1,860 | 1,010 / 1,910 | 1,050 / 1,965 | 1,080 / 2,020 |
| 1,000 ft | 980 / 1,860 | 1,020 / 1,920 | 1,050 / 1,975 | 1,090 / 2,030 | 1,125 / 2,085 |
| 2,000 ft | 1,020 / 1,920 | 1,060 / 1,980 | 1,095 / 2,040 | 1,130 / 2,095 | 1,170 / 2,140 |
| 3,000 ft | 1,060 / 1,980 | 1,100 / 2,040 | 1,135 / 2,100 | 1,170 / 2,145 | 1,210 / 2,190 |
| 4,000 ft | 1,100 / 2,050 | 1,140 / 2,100 | 1,180 / 2,150 | 1,210 / 2,195 | 1,260 / 2,250 |
| 5,000 ft | 1,140 / 2,110 | 1,180 / 2,155 | 1,220 / 2,200 | 1,260 / 2,250 | 1,310 / 2,305 |
| 6,000 ft | 1,180 / 2,150 | 1,220 / 2,205 | 1,265 / 2,255 | 1,310 / 2,310 | 1,360 / 2,365 |
| 7,000 ft | 1,221 / 2,191 | 1,261 / 2,256 | 1,312 / 2,311 | 1,362 / 2,372 | 1,412 / 2,427 |
| 8,000 ft | 1,264 / 2,232 | 1,304 / 2,309 | 1,360 / 2,369 | 1,416 / 2,435 | 1,466 / 2,490 |
| 9,000 ft | 1,309 / 2,275 | 1,348 / 2,362 | 1,410 / 2,428 | 1,472 / 2,500 | 1,522 / 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 QuestionsPer 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.
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: Beechcraft Duchess 76 Pilot's Operating Handbook, Beechcraft Corporation Data synced from the FlightDecide aircraft library on 2026-09-28.