Hi JB i was reading about the Gimli glider and i would like to get a better understanding of the event.
The wikipedia article is pretty good.
With the fuel load being so much lower than expected , therefore the mass of the plane would be lower than expected. Would the pilots notice any difference in performance on takeoff , and would that be a red flag?
It was roughly 10 tonnes lighter than planned, but honestly that would be barely noticeable when looking at an overall weight of around 120 tonnes. Also, at the time, the 767 was very new, and at all weights it was quite sporty compared to previous aircraft, so the crew would not have had a strong basis for comparison.
When you order fuel , you talk about ordering in tons so who does the conversion to ensure the order is correct ?
Well, I really should be talking tonnes. It's ordered in thousands of kg, down to one decimal place (so, 120.5). These days the aircraft are very smart, and will automatically control the fuel loading, needing only final load, and the specific gravity. The refuellers, deal in litres, but again, the conversion is automated. Loading is checked in many ways, but one is a paper fuel chit, given to us by whomever refuelled the aircraft. We ensure that it matches what he thinks he loaded (and for which the company will be billed).
They were being set up by the mixing of imperial and metric.
From your 767 days would you fly without the fuel gauges working?
No, and neither should this crew have done so. The MELs provide relief for one of the two fuel measuring systems being u/s, but not for two. They should have had two separate checks, which normally would be the two separate FQIS systems, but as one was u/s, should have been the functional one, and the tank stick check. There was no allowance at all for flying with both FQIS systems down.
With the failure of power what inpact would there be on the function of the brakes ,flaps and spoilers in a 767?
The brakes would work off accumulator pressure, so you'd have enough to stop, but would have no anti skid. Don't modulate the pressure, just one mid pressure application, and live with it. Flaps and slats would not work. The RAT only provides pressure to flight controls connected to the centre hydraulic system. Normally multiple systems are powering each part of the controls, so dropping back to just one would make them heavy and sluggish. Partial power to inboard ailerons, elevator and rudder, and about half of the spoiler panels would be powered, for roll control only.
The RAT provides no electrical power.