UAL 787 early- mid 2012
#32
Gets Weekends Off
Joined APC: Mar 2008
Posts: 1,083
Today the B767-300 and 400 are the queens and again (tail strike less than 9 degrees body angle), never hit a one.
I agree with your view that this is a technique issue, but you've got to know it's an issue to emphasize it. Until I flew with an FO who had one, I didn't know we had any tail strikes on the -900ER and assumed if the pitch at touchdown was under eight, you were OK... not so.
For you and all the CAL guys and gals out there the 80 knot "thrust set" call is because the A/T system goes to hold and an abort above this activates RTO and the spoilers. So why 100knots?
#33
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X:
The majority of the tailstrikes on the B767 are also on landing. Anything above 8.5 DGNU is questionable and flaps less than 30 will highly increase the likely hood. It was the same with the 727 and if you look back I tried to emphasize landing technique is the issue.
I flew the B737-200,300 for thousands of hours in both seats and because of the length of the fuselage tail strike were only for the severely slow and high pitched on landing. The problem is/was if one gets used to "flaring" the airplane on to get a "smooth" landing and then changes to a -900, well let's say old habits are hard to break.
As far as all the auto stuff goes the reason UAL originally chose 80 knots was because it all starts to happen near there. Originally we had pilots calling 90 or 100 knots and some even had the 3000' acceleration check of 90 knots (727) to make sure the airplane was really acceleration normally. So for standardization and letting the designed auto stuff do what it is supposed to 80 knots was chosen as the standard.
Let's say you notice a generator light come on at 85 knots or prior to your 100 knot call and by the time you react and reduce thrust the airplane is over 90 knots, won't the RTO engage with full brakes? The MEL, at least on 757/767, says if rejected takeoff engages RTO the airplane must return and have maintenance inspection.
I think I like the earlier 80 knot call better, but if the "experts" change the SOP I will follow.
The majority of the tailstrikes on the B767 are also on landing. Anything above 8.5 DGNU is questionable and flaps less than 30 will highly increase the likely hood. It was the same with the 727 and if you look back I tried to emphasize landing technique is the issue.
I flew the B737-200,300 for thousands of hours in both seats and because of the length of the fuselage tail strike were only for the severely slow and high pitched on landing. The problem is/was if one gets used to "flaring" the airplane on to get a "smooth" landing and then changes to a -900, well let's say old habits are hard to break.
As far as all the auto stuff goes the reason UAL originally chose 80 knots was because it all starts to happen near there. Originally we had pilots calling 90 or 100 knots and some even had the 3000' acceleration check of 90 knots (727) to make sure the airplane was really acceleration normally. So for standardization and letting the designed auto stuff do what it is supposed to 80 knots was chosen as the standard.
Let's say you notice a generator light come on at 85 knots or prior to your 100 knot call and by the time you react and reduce thrust the airplane is over 90 knots, won't the RTO engage with full brakes? The MEL, at least on 757/767, says if rejected takeoff engages RTO the airplane must return and have maintenance inspection.
I think I like the earlier 80 knot call better, but if the "experts" change the SOP I will follow.
#34
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I think I like the earlier 80 knot call better, but if the "experts" change the SOP I will follow.
#35
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Joined APC: Dec 2007
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At UA, we do not.
#36
Keep Calm Chive ON
Joined APC: Feb 2008
Position: Boeing's Plastic Jet Button Pusher - 787
Posts: 2,086
Just what a B756 Ck Airman shared on the line last week.....stay tuned.
#37
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Joined APC: Dec 2007
Position: Fero's
Posts: 472
Like you said, stay tuned. Lot's of change is a 'comin...
#38
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Posts: 1,083
I'd heard the same thing and that we'd also go to an 80 KIAS call. We'll see.
#39
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I don't know... what's the likely greater danger... a fire light or an abort just below V1? That's not rhetorical, I really wonder. We've got fire bottles and you can get an airplane back on the ground within 10 minutes IMC, about half that VMC. How many fire lights are false indications? I'm not wedded to any particular course of action, I just hope what the Star Chamber comes up with is based on logic. Like the rest of us, I'll try to do what they tell me to do.
#40
Take a look at the Concorde accident, if they had the opportunity to abort they no doubt would have and the outcome may have been different. The Quantas A380 is another example. It didn't happen on the ground, but an uncontained engine failure nearly brought the plane down. I forget the number, I think something like 56, ECAM messages that they had to deal with. If it's possible to stay on the ground safely, I'm staying on the ground.
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