De Havilland Canada CL-415
Target for the De Havilland Canada CL-415
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
- 88ktat 16,783 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
Amphibious firefighting aircraft with two Pratt & Whitney Canada PW123AF turboprops, first flown by Canadair in 1993 and nicknamed the Super Scooper.
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
- De Havilland Canada
- Model
- CL-415
- Variant
- CL-415 (CL-215-6B11), firefighting
- FAA approach category
- A
- MTOW
- 19,890 kg (43,850 lbs)
- Vref in flight
- Adjusted to the weight you land at
- MSFS source
- Default Std
- Category
- Twin-Engine Turboprop
Roundout recognizes it in a title that contains
De Havilland Canada CL-415CL-415
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Every landing in the De Havilland Canada CL-415, graded against these numbers. Every update included, and tax or VAT in most countries.