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IIRC, the Bleinheim bomb load was 1000lb so using it with a 1600lb torpedo might be problematic.
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The MK V finally getting clamshell landing gear doors that not only fully enclosed the wheels but didn't add sq ft of extra drag when the landing gear was down like the "apron" style doors did, see engine out scenario.
There were medium supercharged Mercury engines, giving 830hp for take off and 890 hp at 6000ft on 87 octane fuel. Running the fully supercharged engines on 100 octane boosted take-off/low altitude performance without sacrificing higher altitude performance (in this case higher altitude being around 9000ft and up.
Blenheinm I carried 1000 lbs of bombs, along with 2000 lbs (278 imp gals) of fuel. The Mk.IV upped the fuel to 3355 lbs ( 466 gals), while still retaining the high-altitude Mercury VIII engine (840 HP at 14000 ft).
Mk.V ('Bisley') received the low-altitude Mercury XV (955 HP at 8500 ft), carrying same bomb load and fuel as the Mk.IV; some sources give also that engine, but with 905 HP (on 87 oct fuel?) for the Mk.IV .
Max take off weight went from 12500 lbs for the Mk.I, to 15800 for Mk.IV, and finally 17040 for Mk.V. Tare weight (ie. no fuel, bombs, ammo) went from 8077 lbs -> 9790 -> 10775 for the Mk.V.
So my idea is to trade the increase of fuel (and respective fuel tanks) and nose turret for torpedo load, obviously installing the low-level rated engine for better take of performance.
edit: Hmmm, the Mercury XV was geared same as the VIII, the result of using greater boost via 100 oct fuel was increase of power down low.