| With the B.E.12 established in production in 1916,
based on the B.E.2c airframe with its equi-span two-bay
wing and massive horizontal tail surfaces, a further
marriage was arranged to combine the R. A.F.4a engine
with the newer B.E.2e airframe. This introduced the
single-bay cellule with overhanging upper wing and a
smaller tailplane/elevator combination, together with
the larger, rounded fin of the B.E.12. Designated B.E.12a
in this form, the type was ordered from Coventry Ordnance
Works and Daimler, each of which received
contracts for 50 during 1916 (some of the Daimler batch
being completed as B.E.12s). The B.E.12a's served
briefly with Home Defence units and more extensively
in Palestine, with the Australian-manned No 67 Squadron.
| A three-view drawing (1278 x 894) |
WEIGHTS |
Take-off weight | 1056 kg | 2328 lb |
Empty weight | 730 kg | 1609 lb |
DIMENSIONS |
Wingspan | 12.19 m | 40 ft 0 in |
Length | 8.30 m | 27 ft 3 in |
Height | 3.66 m | 12 ft 0 in |
Wing area | 33.44 m2 | 359.94 sq ft |
PERFORMANCE |
Max. speed | 169 km/h | 105 mph |
beifangren, 20.06.2011 07:02 The B.E.12a's served briefly with Home Defence units and more extensively in Palestine, with the Australian-manned No 67 Squadron. reply |
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