Bloch MB.220
The Bloch MB.220 was a French twin-engine passenger transport airplane built by Société des Avions Marcel Bloch during the 1930s.
Design and development
The M.B.220 was an all-metal low-wing cantilever monoplane. It was powered by two Gnome-Rhône 14N radial engines and had a retractable landing gear. Normal crew was four, with room for 16 passengers, with eight seats each side of a central aisle. The prototype first flew in December 1935, and was followed by 16 production aircraft. At least five examples survived the war and were modified as the M.B.221 with Wright R-1820-97 Cyclone engines.
Service
By the middle of 1938, the type was being utilised by Air France on European routes. The first service of the type (between Paris and London) was flown on 27 March 1938 with a scheduled time of 1 hour 15 minutes. During World War II, most MB.220s were taken over as military transports, including service with German, Free French and Vichy French air forces. Air France continued to fly the aircraft (as MB.221s) after the war on short-range European routes. It sold four aircraft in 1949 but within a year all had been withdrawn from service.
Variants
- MB.220
- One Prototype and 16 production aircraft with Gnome-Rhône 14N-16 and Gnome-Rhône 14N-17 engines (opposite rotation).
- MB.221
- At least 5 survivors re-engined with the Wright R-1820-97 Cyclone.
Operators
- Air France
- Free French Air Force
- Vichy French Air Force
- Societé Auxiliaire de Navigation Aérienne
Accidents and incidents
- On March 3, 1940, an Air France MB.220, registration F-AOHA, crashed into a mountain near Orange, France in poor weather, killing all three crew on board.
- On September 1, 1941, an Air France MB.220, registration F-AQNL, crashed into a lake on takeoff from Marseille due to engine failure, killing 15 of 17 on board.
Specifications (M.B.220)
General characteristics
- Crew: 4
- Length: 19.25 m (63 ft 1¾ in)
- Wingspan: 22.82 m (74 ft 10½ in)
- Height: ()
- Wing area: 75 m² (807.32 ft²)
- Empty weight: 6,807 kg (15,007 lb)
- Max. takeoff weight: 9,500 kg (20,944 lb)
- Powerplant: 2 × Gnome-Rhône 14N-16/-17 (opposite rotation) radial engine, 735 kw (985 hp) each
Performance
- Maximum speed: 330 km/h (205 mph)
- Range: 1,400 km (870 mi)
- Service ceiling: 7,000 m (22,965 ft)
See also
- Related development
- Aircraft of comparable role, configuration and era
References
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Wikimedia Commons has media related to Bloch MB.220. |
- The Illustrated Encyclopedia of Aircraft (Part Work 1982-1985). Orbis Publishing.
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