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| Description | Part Number | Price | Buy |
|---|---|---|---|
| Durand Mark V Tail Surfaces Hardware Kit Group 1 Click Here for Kit Components | 01-01623 | $130.42 | |
| Durand Mark V Wings Hardware Kit Group 2 Click Here for Kit Components | 01-01624 | $302.65 | |
| Durand Mark V Control Systems Materials Kit Group 3 Click Here for Kit Components | 01-01625 | $1466.69 | |
| Durand Mark V Fuselage Tail Cone & Interior Sect Group 4-A Click Here for Kit Components | 01-01626 | $69.04 | |
| Durand Mark V Basic Forward Fuselage Structure Group 4-B Click Here for Kit Components | 01-01627 | $401.13 | |
| Durand Mark V Ngn-Structural Fuselage Parts Group 4-C Click Here for Kit Components | 01-01628 | $24.16 | |
| Durand Mark V Landing Gear Group 5 Click Here for Kit Components | 01-01630 | $3693.90 | |
| Durand Mark V Final Assembly Group 6 Click Here for Kit Components | 01-01631 | $130.92 |
Overview
| The Durand Mk V was a two-seat sports biplane aircraft developed in the United States in the 1970s and marketed for home building. The design was distinctive due to a large negative stagger on the wings, but was otherwise conventional. The single-bay wings were braced with I-struts, and while both upper and lower wings were equipped with full-span flaps, lateral control was by spoilers on the lower wing rather than ailerons. Flight testing revealed that the aircraft was impossible to stall. The pilot and single passenger sat side by side beneath an expansive canopy, and the undercarriage was of fixed, tricycle type. |
 |
WARNING: Cancer and Reproductive Harm - www.P65Warnings.ca.gov. |
Specifications
- Crew: One pilot
- Capacity: 1 passenger
- Length: 6.17 m (20 ft 3 in)
- Wingspan: 7.47 m (24 ft 6 in)
- Height: 2.03 m (6 ft 8 in)
- Wing area: 13.3 m2 (144 ft2)
- Empty weight: 549 kg (1,210 lb)
- Gross weight: 834 kg (1,840 lb)
- Powerplant: 1 × Lycoming O-320, 112 kW (150 hp) each
- Cruising Speed: 217 km/h (135 mph)
- Range: 644 km (400 miles)
- Service ceiling: 4,575 m (15,000 ft)
- Rate of climb: 6.1 m/s (1,200 ft/min)
Documents
Durand Mark V Story (PDF)
Q&A
Please note, Aircraft Spruce's personnel are not certified aircraft mechanics and can only provide general support and ideas, which should not be relied upon or implemented in lieu of consulting an A&P or other qualified technician. Aircraft Spruce assumes no responsibility or liability for any issue or problem which may arise from any repair, modification or other work done from this knowledge base. Any product eligibility information provided here is based on general application guides and we recommend always referring to your specific aircraft parts manual, the parts manufacturer or consulting with a qualified mechanic.
