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Diamond DA62

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

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Diamond DA62 preflight numbers at a glance: max gross weight 5071 lb, typical useful load 1940 lb, 79 gal usable fuel, cruise up to about 179.2 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.

Diamond DA62 key numbers

Engine2x Austro AE330 (180 HP diesel each)
PropellerMT-Propeller MTV-6-A/187-129 (2x)
Max gross weight5071 lb
Empty weight (typical)3131 lb
Useful load (typical)1940 lb
Usable fuel79 gal

Diamond DA62 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
VS069 ktStall, landing configuration
VS173 ktStall, clean configuration
VX86 ktBest angle of climb
VY89 ktBest rate of climb
VXSE85 ktBest angle of climb, single engine
VYSE96 ktBest rate of climb, single engine
VFE119 ktMax flaps extended
VNO162 ktMax structural cruising
VNE205 ktNever exceed
VMC72 ktMin control, one engine inoperative
Best glide95 ktBest glide speed

Diamond DA62 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)
40001800166.716
40002100171.518
40002300174.719.4
60001800168.215.8
6000210017317.8
60002300176.219.2
80001800169.715.4
80002100174.517.6
80002300177.718.8
10,0001800171.215.2
10,000210017617.2
10,0002300179.218.6

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 Diamond DA62 need?

Book figures at 5071 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 roll1750 ft
Takeoff over a 50 ft obstacle2540 ft
Landing ground roll640 ft
Landing over a 50 ft obstacle1090 ft
Rate of climb1200 fpm

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

Common Questions

Per the POH cruise table, up to about 179.2 KTAS at 10,000 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.

79 gallons usable. At a high-cruise burn of 18.6 GPH that is roughly 4.2 hours to dry tanks. Plan with reserves, never to zero.

About 1940 lb for a typically equipped example (5071 lb max gross minus a typical empty weight of 3131 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 162 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: Diamond DA62 Pilot's Operating Handbook, Diamond Aircraft Industries Data synced from the FlightDecide aircraft library on 2026-07-17.