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Diamond DA42 Twin Star

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

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Diamond DA42 Twin Star preflight numbers at a glance: max gross weight 3935 lb, typical useful load 1279 lb, 50 gal usable fuel, cruise up to about 190 KTAS (POH figure at 16,000 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 DA42 Twin Star key numbers

Engine2x Austro AE300 (168 HP diesel each)
PropellerMT-Propeller MTV-6-A/187-129 (2x)
Max gross weight3935 lb
Empty weight (typical)2656 lb
Useful load (typical)1279 lb
Usable fuel50 gal

Diamond DA42 Twin Star 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
VS062 ktStall, landing configuration
VS168 ktStall, clean configuration
VX80 ktBest angle of climb
VY89 ktBest rate of climb
VXSE80 ktBest angle of climb, single engine
VYSE85 ktBest rate of climb, single engine
VFE113 ktMax flaps extended
VNO151 ktMax structural cruising
VNE188 ktNever exceed
VMC68 ktMin control, one engine inoperative
Best glide90 ktBest glide speed

Diamond DA42 Twin Star 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)% powerTAS (kt)Fuel (GPH)
20006013910.3
20007515313.2
20009216616.6
40006014210.3
40007515613.2
40009216916.6
60006014410.3
60007515913.2
60009217316.6
80006014710.3
80007516213.2
80009217616.6
10,0006015010.3
10,0007516513.2
10,0009217916.6
12,0006015210.3
12,0007516813.2
12,0009218316.6
16,0006015710.3
16,0007517513.2
16,0009219016.8

How much runway does a Diamond DA42 Twin Star need?

Book figures at 3935 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 roll1480 ft
Takeoff over a 50 ft obstacle2145 ft
Landing ground roll560 ft
Landing over a 50 ft obstacle950 ft
Rate of climb1280 fpm

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

Common Questions

Per the POH cruise table, up to about 190 KTAS at 16,000 ft on a standard day, burning roughly 16.8 GPH at that setting. Typical everyday cruise settings run slower and leaner; see the table above.

50 gallons usable. At a high-cruise burn of 16.8 GPH that is roughly 3.0 hours to dry tanks. Plan with reserves, never to zero.

About 1279 lb for a typically equipped example (3935 lb max gross minus a typical empty weight of 2656 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 188 kt and VNO (max structural cruising) is 151 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

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 DA42 Twin Star Pilot's Operating Handbook, Diamond Aircraft Industries | FD-215: cruise re-digitized on POH axis (recommended_lean, high conf), fuel total both-engines for twins. Data synced from the FlightDecide aircraft library on 2026-07-17.