Mitsubishi MU-2
Target for the Mitsubishi MU-2
60 to 120fpm
Full marks for descent rate up to 120 fpm; under 60 fpm the coach says the touchdown was softer than this aircraft is normally flown.
- Vref reference
- 100ktat 4,516 kg
- Tail-strike limit
- 9°the category's
- Ideal touchdown zone
- 120 to 380mpast the threshold
- G-force
- 1.10Gfull marks, the category's curve
Japanese high-wing twin-turboprop business aircraft with Garrett TPE331 engines, using spoilers instead of ailerons for roll control, first flown in 1963.
Roundout scores this aircraft with the Twin-Engine Turboprop category's curves and touchdown-zone window. The figures it uses are below.
How its touchdown is scored.
The score at each point of its curves. Between the points, scores fall in a straight line; the full method is in the scoring methodology.
No shared landings or board for this aircraft yet. Its figures appear once pilots with a public profile have shared 5 graded landings in it, and a board once at least 5 opted-in pilots have flown it 10 or more times each. See the boards there are.
For reference.
Aircraft data
- Manufacturer
- Mitsubishi
- Model
- MU-2
- Variant
- MU-2B-25/-26 (short body, TPE331-6-251M)
- FAA approach category
- B
- MTOW
- 4,749 kg (10,470 lbs)
- Vref in flight
- Adjusted to the weight you land at
- MSFS source
- Default Aviator
- Category
- Twin-Engine Turboprop
Roundout recognizes it in a title that contains
Mitsubishi MU-2MU-2
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Every landing in the Mitsubishi MU-2, graded against these numbers. Every update included, and tax or VAT in most countries.