B777RR to GE Take-off differences
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B777RR to GE Take-off differences
Does anyone know any reason why the B777-200RR895 feels much sticker when unsticking at VR compared to the B777-200GE or even the B777-300GE?
I can’t think of any particular reason why this would be the case but it seems to be.
apple
I can’t think of any particular reason why this would be the case but it seems to be.
apple
I don’t know for sure but it could be a problem with the trim calculation. They have been like that since they were introduced - on my first go on an RR variant I thought there was a serious flight control issue when it came to rotate as the forces were so much higher than the GE versions.
For quite a while as SOP we added some back trim to the FMC value to bring it closer to the GE experience but Boeing got wind of that eventually and put the kibosh on it. I joke about having developed a specific set of exercises to do in the gym before a RR flight but it does catch people out who are new to type and haven’t experienced or been briefed about it yet.
I don’t think it’s anything to do with the engines themselves, just (IMO) the trim setting algorithm in the FMC is getting it a bit wrong but the aeroplane flies so no-one can be bothered to fix it. A bit like the blockpoint update which left the plane much worse at holding than before that hasn’t been improved since.
For quite a while as SOP we added some back trim to the FMC value to bring it closer to the GE experience but Boeing got wind of that eventually and put the kibosh on it. I joke about having developed a specific set of exercises to do in the gym before a RR flight but it does catch people out who are new to type and haven’t experienced or been briefed about it yet.
I don’t think it’s anything to do with the engines themselves, just (IMO) the trim setting algorithm in the FMC is getting it a bit wrong but the aeroplane flies so no-one can be bothered to fix it. A bit like the blockpoint update which left the plane much worse at holding than before that hasn’t been improved since.
I do recall the pitch trim setting calculation differing for the RR variant, a procedure which then later disappeared, but I didn't dwell on it. I just looked over the nose of the aircraft and did as was necessary with the elevator to get the required pitch rate, in order to then meet with the flight director pitch bar for the climb away from the ground.
Having flown the 777-200 RR and GE engine variants (and also eventually the 777-300 GE) for around 17 years, I cannot say I ever noticed much of a difference in the elevator feel at rotation and lift-off. 🤷🏼♂️
I certainly had the same impression when I flew it. My impression was solely a difference in force required to initiate the rotation.
My sole uneducated guess was due to the N3 on the RR was higher gyroscopic inertia from the engines resisting the initial rate establishment. Hopefully tdracer or fdr will be alon to tell me if I’m talking rubbish or not!
My sole uneducated guess was due to the N3 on the RR was higher gyroscopic inertia from the engines resisting the initial rate establishment. Hopefully tdracer or fdr will be alon to tell me if I’m talking rubbish or not!