Blackburn M.1/30 and B-3
For a description of the format and data included in Production Tables, see here.
Contents
Type Description
- M.1/30
- Two seat carrier-based torpedo bomber and reconnaissance to meet the requirements of Specification M.1/30. A single-bay biplane, construction was conventional, with a metal structure and fabric covering to both wings and fuselage. Unusually, the braced tailplane was mounted just above the top decking of the rear fuselage, whilst the wings could be folded to the rear, being hinged around their rear spar attachments. Ailerons were fitted on all four mainplanes. The square shaped tailplane and fin were fitted with horn balanced elevators and rudder. A wide track undercarriage allowed for torpedo carriage beneath the fuselage, whilst bomb racks were provided beneath the wings. Crew comprised of a pilot and observer/ gunner, who were seated in tandem cockpits, with the observer being able to access a prone bomb aiming position below the pilot’s cockpit floor. Armament consisted of a single fixed, forward-firing .303 in Vickers machine gun and one .303 in Lewis Gun in rear cockpit. One 1,900 lb Mk VIII or Mk X torpedo or equivalent (maximum 2,200lb) underwing bomb load. One 825 h.p. Rolls-Royce Buzzard IIIMS V-12 powerplant driving a 15 ft diameter, two blade propeller.
- B-3 'M.1/30A'
- Three seat Private Venture derivative of the original M.1/30, unofficially designated 'M.1/30A'. All metal semi-monocoque fuselage, incorporating sealed compartments to provide buoyancy, and redesigned lower wing of lesser span and chord. The aircraft was also fitted with automatic slats and featured long-span ailerons that could also be lowered symmetrically, to act as camber-changing flaps. A third cockpit was also introduced for a dedicated rear gunner, as well as a sealed structural fuel compartment, which was introduced within the fuselage ahead of the pilot. One 825 h.p. Rolls-Royce Buzzard IIIMS V-12 powerplant.
| Specification | |||||||||
| Span | Length | Height | Wing Area | Empty Wt | Max AUW | Cruise Speed | Maximum Speed | Range | Service Ceiling |
| 49 ft 6 in | 39 ft 10 in | 14 ft 7 in | 651 sq ft | 6138 lb | 10393 lb | 142 mph/ 123 kn | 750 mi | 9150 ft | |
| 15.09 m | 12.14 m | 4.45 m | 60.48 m2 | 2784 kg | 4714 kg | 229 km/h | 1207 km | 2789 m | |
Production Details
| Serial Range | C/n | Type | Batch Qty |
Conv. | Canc'd | Notes |
| 1 aircraft ordered from The Blackburn Aeroplane and Motor Co. Ltd, Brough, Yorkshire, to contract 55826/30. First flew 8 March 1932. | ||||||
| S1640 | 3380/1 | M.1/30 | 1 | |||
| 1 aircraft built by The Blackburn Aeroplane and Motor Co. Ltd, Brough, Yorkshire, as a Private Venture. First flew 24 February 1933; to the Air Ministry under contract 244326/33 on 18 May 1933. | ||||||
| K3591 | 3900/1 | M.1/30A | 1 | Originally flew under Class B conditions as B-3. | ||
| Total Production | 2 | |||||
Production Summary
All Aircraft By Type
| Type | Built New | Conv | Canc'd | Total |
| B-3 | 1 | 1 | ||
| B-3 'M.1/30A' | 1 | 1 | ||
| 2 | (0) | 0 |
Notes
- Blackburn used a series of Works Order Numbers rather than Constructors Numbers to identify individual airframes, but referred to here as C/n's for consistency.
Production References
- Blackburn Aircraft Since 1909, A.J. Jackson (Putnam, 1968 and 1989)
Page Revision History
Revised at Version 2.0.0- Improved Type Description and added Specification details