de Havilland D.H.98 Mosquito B.35 (TT.35) RS712 Specifications

Manufacturer	Airspeed Ltd., Christchurch Aerodrome, Bournemouth Hampshire
Powerplant	Two Rolls Royce Merlin 114A V-12 piston engines
Fuel Total	539 (Imperial) gal.
Oil Total	31 gal.
Fuel Capacity (with drop tanks)	597 gal.
Wingspan	54 ft. 2 in.
Length	40 ft. 6 in.*
Height	12 ft. 6 in.
Wing Area	435 sq. ft.
Aspect Ratio	6.7
Dihedral	1° 34 ft.
Span Loading	7.5 lbs./sq. ft.
Wing Loading	48 lbs./sq. ft.
Undercarriage Track	16 ft. 4 in.
Tare Weight	14,635 lbs.
All-up Weight	23,000 lbs.
Loaded Weight	25,200 lbs. (when carrying 4,000 lb. bomb and two drop tanks)
Landing Weight	20,500 lbs.
Maximum Internal Bomb Load	4,000 lbs.
Underwing Load	1x500 lb. bomb or a 50, 100, or 200 gal. drop tank under each wing
Maximum Speed	415 mph
Maximum Speed Sea Level	326 mph
Maximum Cruising Speed	375 mph TAS at 37,000 ft. (continuous)
Recommended Cruise Speed	300 mph TAS at 25,000 ft.
Dive Speed	400 mph IAS
Initial Rate of Climb	2,500 ft./min. (at sea level, full climb power)
Maximum Range	1,955 miles
Operational Celing	37,000 ft.
Crew	1 pilot, 1 navigator

*Overall length increased to 41 ft. 6 in. when converted to TT.35 and fitted with longer spinners