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JODEL D-150 Mascaret
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D150
| Aircraft | ||||||
|---|---|---|---|---|---|---|
| Name | D-150 Mascaret | |||||
| Manufacturer | JODEL | |||||
| Body | Narrow | |||||
| Wing | Fixed Wing | |||||
| WTC | Light | |||||
| APC | A | |||||
| Type code | L1P | |||||
| Engine | Piston | |||||
| Engine count | Single | |||||
| Mass group | 1 | |||||
|
| ||||||
JODEL D-150 Mascaret
Description
The Jodel D.150 Mascaret is a French two-seat single-engined light aircraft of the 1960s built by Société Aeronautique Normande (SAN) as a replacement for the earlier Jodel D11 trainer/tourer aircraft.
Technical Data
| Wing span | 8.15 m26.739 ft |
|---|---|
| Length | 6.30 m20.669 ft |
| Height | 1.76 m5.774 ft |
| Powerplant | 1 x Rolls-Royce Continental O-200-A air-cooled flat-four, 75 kW (100 hp). |
| Engine model | Continental O-200 |
Performance Data
| Take-Off | Initial Climb (to 5000 ft) |
Initial Climb (to FL150) |
Initial Climb (to FL240) |
MACH Climb | Cruise | Initial Descent (to FL240) |
Descent (to FL100) |
Descent (FL100 & below) |
Approach | ||||||||||
| V2 (IAS) | kts | IAS | kts | IAS | kts | IAS | kts | MACH | TAS | 130 kts | MACH | IAS | kts | IAS | kts | Vapp (IAS) | kts | ||
| Distance | m | ROC | ft/min | ROC | ft/min | ROC | ft/min | ROC | ft/min | MACH | ROD | ft/min | ROD | ft/min | MCS | kts | Distance | m | |
| MTOW | 800800 kg 0.8 tonnes kg |
Ceiling | FL150 | ROD | ft/min | APC | A | ||||||||||||
| WTC | L | Range | NM | ||||||||||||||||
Accidents & Serious Incidents involving D150
- D150 / H500, London UK, 2007 (On 5 October 2007, a loss of separation occurred between a Hughes 369 helicopter and a Jodel D150. The incident occurred outside controlled airspace, in VMC, and the estimated vertical separation as the Jodel took avoiding action by descending, was assessed by both pilots to be less than 50 feet.)
- H500 / D150, en-route, North of London UK, 2007 (On 5 October 2007, a loss of separation occurred between a Hughes 369 helicopter and a Jodel D150. The incident occurred outside controlled airspace, in VMC, and the estimated vertical separation as the Jodel took avoiding action by descending, was assessed by both pilots to be less than 50 feet.)