Hanriot HD.14
| Hanriot HD.14 | |
|---|---|
 Hanriot HD.14 1921/22 |
|
| Type: | military trainer aircraft |
| Design country: | |
| Manufacturer: |
Appareils d'Aviation Hanriot |
| Production time: |
1922-1928 |
| Number of pieces: |
around 2100 (all versions) |
The Hanriot HD.14 was a French military training aircraft that was built in large numbers. The Aéronautique Militaire alone had 1925 copies. A total of around 2100 machines in eleven different versions were built between 1922 and 1928.
construction
The wings of the double-decker were constructed in a conventional rib-spar design. Teacher and student sat one behind the other. The chassis was designed to be particularly stable for school use. Early versions had four wheels and two runners that were pulled forward to prevent rollover. In 1922 an improved version was worked on, which came out as HD.14 ter . In addition to the license samples in Poland (245 pieces) and Japan (145), the HD.14 was also delivered to other countries.
variants
- HD.14 - First version, also HD.14 EP2 , with Le Rhône - rotary engine with 110 hp
- HD.14 ter - Improved version from 1922, also HD.14 / 23
- HD.14S ( Sanitaire ) - ambulance aircraft
- HD.141 - Reconditioned military aircraft for the French aero clubs
- H.410 - Modified chassis and 5-cylinder Lorraine radial engine
- H.411 - Further developed H-410
- LH.412 - Further developed H-410
- H.28 - Polish license build of the HD.14 / 23
- Ki 1 - Japanese army name for the license version built by Mitsubishi
René Arnoux also built a particularly interesting variant , who converted the machine into a tailless aircraft.
Technical specifications
| Parameter | HD.14 (early version) |
|---|---|
| crew | 2 |
| length | 7.80 m |
| span | 10.87 m |
| height | 3.00 m |
| Wing area | 34.5 m² |
| Empty mass | 555 kg |
| Max. Takeoff mass | 810 kg |
| Top speed | 110 km / h |
| Summit height | 4000 m |
| Range | 120 km |
| Engine | 1 × rotary engine Le Rhône 9 with 80 HP |
operator
literature
- Hanriot HD.14 series. In: World Aircraft Information Files , File 896, Sheet 11
Web links
Individual evidence
- ^ World Aircraft Information Files