Wed Sep 29, 2021 3:28 pm
#1873380
The Beech 18 vid showed very little rudder use, presumably on the brakes and overdid it?
I had the fortunate experience of flying a UK based NA B25 for a number of years.
The WWII Pilots Notes for the weights flown then, approx 34,000 lbs was “ EFATO land straight ahead” So no SE performance there.
At the weights we flew for demos etc., approx 24000lbs perhaps, the SE performance was predicted to be somewhat better.
Other than simulated failure in training, I luckily never had the chance to try the real thing.
The all engine performance was quite sprightly, and although of course with higher control forces and speeds, the SE performance would not be much different to an Aztec/ Navajo, Cessna twin, all with marginal SE performance at MTOW.
Airborne at 105 mph, the aircraft speedily attained the approx 165 mph SE safety speed in a shallow climb as the gear retracted. No flaps were used during T/O.
As a rule of thumb for an EFATO, I planned for up to 1000ft definitely land ahead. 1000-1500ft with the gear retracted, evaluate the performance and perhaps again land head. Above 1500ft with no obstacles in the vicinity, (Climbing at 170 mph at hopefully 200fpm covered a lot of countryside) some very gentle turns to land back on the departure runway. Keeping in mind the possibility of having perhaps to reduce power on the good engine, to control the yaw.
Early in my B25 experience, we flew to an ex Swiss Air force airfield, 3000ft amsl. Situated in a narrow valley surrounded by 4/9000ft terrain, it did though, give one food for thought in the event of a failure.
At least the previous Mirage/ Hunter airbase occupants had the option to eject!
In normal operations though the B25 was a sprightly performer for its bulk, great experience, and a privilege to be let loose in.
Last edited by Oldfart on Wed Sep 29, 2021 10:38 pm, edited 1 time in total.