Stingray Don
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Stingray Don
Hope everyone got out okay. Very scary!
Looks like chaos inside the plane
Exactly. Hold up the line so he could take the video. Had I been behind him, I may well have snatched the phone. And thrown it away.Who took the video? Another fool with their cell phone?
Exactly. Hold up the line so he could take the video. Had I been behind him, I may well have snatched the phone. And thrown it away.
By the way, a FedEx DC-10 had it's landing gear collapse and caught fire in Florida today. Also. Not a good day for the big birds.
Concord is a good example of that.Glad it occurred prior to V1. Something burning that strongly might not have made it back.
"Passengers" have no earthly idea of what's going on up front. I bet when the auto brakes on RTO kicked in, it felt like they slammed back to "the tarmac," but I'm doubting this crew rejected the takeoff after V1 and especially after just lifting off.Passengers said...
Who said it happened prior to V1?
"The plane had started to take off around 2:35 p.m. on Runway 28R, according to the FAA. Passengers said the plane was just lifting off when it slammed back to the tarmac."
Concord is a good example of that.
There is some pretty solid evidence that the Air France Concorde could have flown out of its predicament, but the FO shut down an engine. Here is one (abbreviated, but revelatory) write-up on the subject.
http://www.askthepilot.com/untold-concorde-story/
I'm positive there are times that passengers know exactly what's going on with and aircraft. Case in point: The only time l flew Southwest. Descending to land, as flaps were being extended, there became a very noticeable vibration, which, from my vantage point was obviously coming from the right inboard fore flap, outboard carriage attach point. The vibration subsided when the flap handle was returned to a lesser degree detent and we landed that way. In that case, the crew only knew they had a vibration associated with flap position and a passenger was able to pinpoint the exact problem area for them."Passengers" have no earthly idea of what's going on up front.
And, most of the pilots here will think to themselves: "WTF is that."right inboard fore flap, outboard carriage
And, most of the pilots here will think to themselves: "WTF is that."
, as flaps were being extended, there became a very noticeable vibration.
Yeah, that's awful, especially fresh out of heavy check.By the way, a FedEx DC-10 had it's landing gear collapse and caught fire in Florida today. Also.
All of the 727's I've worked on have had the 40° lock. You have to want to go beyond it. And, I don't believe the lock was there for vibration, it's there because of the reduced stall margin at 40 bing dangerous.Simple explanation. FO tried pulling the Johnson bar past the third notch. Happens to the best of us.
I heard a story about 727 pilots using some kind of method having to do with those flaps to be able to go faster in cruise. Cant remember the specifics thoughAll of the 727's I've worked on have had the 40° lock. You have to want to go beyond it. And, I don't believe the lock was there for vibration, it's there because of the reduced stall margin at 40 bing dangerous.
Different issue. The lore is that TWO degrees of flaps would get you better cruise performance but to do this you have to disable the leading edge slats (by pulling the breaker) that also come out with when you did that. This came to a head in the famed Hoot Gibson barrel roll incident on TWA 841. Hoot says it was an uncommanded activation of the slats and ALPA backed him up with similar incidents. The NTSB said no way and blamed the pilots. This was reinforced by the captain mysteriously erasing the CVR after the incident.I heard a story about 727 pilots using some kind of method having to do with those flaps to be able to go faster in cruise. Cant remember the specifics though
Blocking the last flap setting was to meet noise abatement standards. With less landing flaps the engines were at lower power on final and would meet tighter noise standards.All of the 727's I've worked on have had the 40° lock. You have to want to go beyond it. And, I don't believe the lock was there for vibration, it's there because of the reduced stall margin at 40 bing dangerous.
It's only dangerous if you don't tell the FE what you are up to and he resets the CB for the slats after returning from a head call and unaddressed corrosion causes asymmetric slat deployment.....but that was never proven....It proved to be dangerous, extending the flaps slightly, electrically, and pulling the circuit breaker.