![]() |
If this is your first visit, be sure to check out the FAQ by clicking the link above. You may have to register before you can post: click the register link above to proceed. To start viewing messages, select the forum that you want to visit from the selection below. |
|
|
|
Thread Tools | Display Modes |
|
#1
|
|||
|
|||
![]() The was an incident some years back where a crew lost control of an airliner in turbulence, and pulled forces way outside the design envelope inorder to prevent a dive into the ground. Also lowered landing gear above gear down speed, etc. The aircraft suffered severe damage, but landed OK. Unfortunately, I cannot remember the airline, aircraft type nor location, which makes it a bit hard to find. I believe it was a China Airlines 747, at SFO. I saw the aircraft the next day. Hard to believe it came back. The horizontal stabilizers and elevators were clipped off at about half span. The gear doors came by after the gear was extended. The left aileron had a two foot hole in it where a part came off of the leading edge, and went through the obviously very extended aileron. There were wrinkles everywhere. A commercial pilot in the cabin estimated 6 g's. See: February 19, 1985, China Airlines Flight 006, http://www.rvs.uni-bielefeld.de/publ...r/AAR8603.html) |
#2
|
|||
|
|||
![]() Al Gerharter wrote: The was an incident some years back where a crew lost control of an airliner in turbulence, and pulled forces way outside the design envelope inorder to prevent a dive into the ground. Also lowered landing gear above gear down speed, etc. The aircraft suffered severe damage, but landed OK. Unfortunately, I cannot remember the airline, aircraft type nor location, which makes it a bit hard to find. I believe it was a China Airlines 747, at SFO. I saw the aircraft the next day. Hard to believe it came back. The horizontal stabilizers and elevators were clipped off at about half span. The gear doors came by after the gear was extended. The left aileron had a two foot hole in it where a part came off of the leading edge, and went through the obviously very extended aileron. There were wrinkles everywhere. A commercial pilot in the cabin estimated 6 g's. See: February 19, 1985, China Airlines Flight 006, http://www.rvs.uni-bielefeld.de/publ...r/AAR8603.html) Yes, that looks like the one. Although I cited this as an example where the ability to fly outside the design envelope allowed recovery of an otherwise disasterous situation, it looks to me, on a cursory reading, as if the damaging accelerations occurred during a period when the captain was not trying to recover control because he couldn't tell what the aifcraft was doing anyway. Oh well. I'm amazed that the crew apparently thought it reasonable to resume normal operation after a descent like that. They should surely have realised that an immediate landing was indicated. Sylvia. |
#3
|
|||
|
|||
![]()
I think this was their first opportunity to land. The aircraft was well
outside the envelope when a recovery ensued. I don't know what would have happened to an airbus. This thing had shoe prints on the instrument panel. Al "Sylvia Else" wrote in message u... Al Gerharter wrote: The was an incident some years back where a crew lost control of an airliner in turbulence, and pulled forces way outside the design envelope inorder to prevent a dive into the ground. Also lowered landing gear above gear down speed, etc. The aircraft suffered severe damage, but landed OK. Unfortunately, I cannot remember the airline, aircraft type nor location, which makes it a bit hard to find. I believe it was a China Airlines 747, at SFO. I saw the aircraft the next day. Hard to believe it came back. The horizontal stabilizers and elevators were clipped off at about half span. The gear doors came by after the gear was extended. The left aileron had a two foot hole in it where a part came off of the leading edge, and went through the obviously very extended aileron. There were wrinkles everywhere. A commercial pilot in the cabin estimated 6 g's. See: February 19, 1985, China Airlines Flight 006, http://www.rvs.uni-bielefeld.de/publ...r/AAR8603.html) Yes, that looks like the one. Although I cited this as an example where the ability to fly outside the design envelope allowed recovery of an otherwise disasterous situation, it looks to me, on a cursory reading, as if the damaging accelerations occurred during a period when the captain was not trying to recover control because he couldn't tell what the aifcraft was doing anyway. Oh well. I'm amazed that the crew apparently thought it reasonable to resume normal operation after a descent like that. They should surely have realised that an immediate landing was indicated. Sylvia. |
#4
|
|||
|
|||
![]() Al Gerharter wrote: I think this was their first opportunity to land. The aircraft was well outside the envelope when a recovery ensued. I don't know what would have happened to an airbus. This thing had shoe prints on the instrument panel. Al On the landing question, I was struck by this section, on page 5. "At 1018:42, Flight 006 requested clearance to climb. Oakland ARTCC initially cleared it to climb to FL 200, and, at 1019:17, Flight 006 told the ARTCC that "we can control the aircraft." Oakland ARTCC asked the flight if it wanted to divert to San Francisco, and, at 1019:49, Flight 006 answered "Condition normal now," and that it would continue to Los Angeles." In respect of the evelope issue, my memory said that the upset was caused by turbulence. In this case, it appears to have been crew mishandling. In the circumstances, I have to wonder whether an FBW aircraft would have got into the position of needing an outside the envelope recovery in the first place. Sylvia. |
#5
|
|||
|
|||
![]() "Sylvia Else" wrote in message u... Al Gerharter wrote: I think this was their first opportunity to land. The aircraft was well outside the envelope when a recovery ensued. I don't know what would have happened to an airbus. This thing had shoe prints on the instrument panel. Al On the landing question, I was struck by this section, on page 5. "At 1018:42, Flight 006 requested clearance to climb. Oakland ARTCC initially cleared it to climb to FL 200, and, at 1019:17, Flight 006 told the ARTCC that "we can control the aircraft." Oakland ARTCC asked the flight if it wanted to divert to San Francisco, and, at 1019:49, Flight 006 answered "Condition normal now," and that it would continue to Los Angeles." Wow, I hadn't read that. They did indeed declare an emergency, and land in SFO. At least that's where I was when I was looking at it. Yea, big place on the water of the bay, big gold bridge in the background, yep that's it. The guys in the tower said that each time he pitched up a little on final, they got a big roll out of it as well. In respect of the evelope issue, my memory said that the upset was caused by turbulence. In this case, it appears to have been crew mishandling. In the circumstances, I have to wonder whether an FBW aircraft would have got into the position of needing an outside the envelope recovery in the first place. Sylvia. Then there was the Air Transat from Canada to Spain, that developed a fuel leak, and the "automatic" system sent all of the fuel into the leaking tank trying to balance the aircraft. They flamed out, and landed in the Azores dead stick. Al |
#6
|
|||
|
|||
![]()
Al Gerharter wrote:
Then there was the Air Transat from Canada to Spain, that developed a fuel leak, and the "automatic" system sent all of the fuel into the leaking tank trying to balance the aircraft. They flamed out, and landed in the Azores dead stick. Actually, it was the pilots who didn't follow the checklist but rather cross fed the fuel to the leak manually. Legends never die. Eager top hear your next one. Stefan |
#7
|
|||
|
|||
![]()
Al Gerharter wrote:
"Sylvia Else" wrote in message u... Al Gerharter wrote: I think this was their first opportunity to land. The aircraft was well outside the envelope when a recovery ensued. I don't know what would have happened to an airbus. This thing had shoe prints on the instrument panel. Al On the landing question, I was struck by this section, on page 5. "At 1018:42, Flight 006 requested clearance to climb. Oakland ARTCC initially cleared it to climb to FL 200, and, at 1019:17, Flight 006 told the ARTCC that "we can control the aircraft." Oakland ARTCC asked the flight if it wanted to divert to San Francisco, and, at 1019:49, Flight 006 answered "Condition normal now," and that it would continue to Los Angeles." Wow, I hadn't read that. They did indeed declare an emergency, and land in SFO. At least that's where I was when I was looking at it. Yea, big place on the water of the bay, big gold bridge in the background, yep that's it. The guys in the tower said that each time he pitched up a little on final, they got a big roll out of it as well. In respect of the evelope issue, my memory said that the upset was caused by turbulence. In this case, it appears to have been crew mishandling. In the circumstances, I have to wonder whether an FBW aircraft would have got into the position of needing an outside the envelope recovery in the first place. Sylvia. Then there was the Air Transat from Canada to Spain, that developed a fuel leak, and the "automatic" system sent all of the fuel into the leaking tank trying to balance the aircraft. They flamed out, and landed in the Azores dead stick. Al Do you two just pull this stuff out of your asses or what? |
#8
|
|||
|
|||
![]()
Al Gerharter wrote:
Then there was the Air Transat from Canada to Spain, that developed a fuel leak, and the "automatic" system sent all of the fuel into the leaking tank trying to balance the aircraft. It wasn't the automatic system. The pilots made the conscious decision to transfer fuel from the left tank to the right tank, despite transport canada regulation that on etops aircraft, preserving fuel in the wing with the functioning engine was paramount. |
#9
|
|||
|
|||
![]()
Al Gerharter wrote:
I think this was their first opportunity to land. The aircraft was well outside the envelope when a recovery ensued. I don't know what would have happened to an airbus. All modern airplanes, no matter from which manufactorer, are designed to match the legal certification minimas and nothing more. Every little bit of extra strengh is a waste of payload. An engineer who builds too strongly will be fired like one who builds too weakly. Stefan |
#10
|
|||
|
|||
![]()
On Thu, 28 Oct 2004 at 08:50:15 in message
, Sylvia Else wrote: I'm amazed that the crew apparently thought it reasonable to resume normal operation after a descent like that. They should surely have realised that an immediate landing was indicated. They didn't. Their destination was Los Angeles and they diverted to the nearest they could which was San Francisco. The incident took place nearly 300nm off shore when they were NW of San Francisco. Their route would have taken them over San Francisco on the way to Los Angeles (according to my globe anyway!) -- David CL Francis |
|
Thread Tools | |
Display Modes | |
|
|
![]() |
||||
Thread | Thread Starter | Forum | Replies | Last Post |
AOPA Stall/Spin Study -- Stowell's Review (8,000 words) | Rich Stowell | Aerobatics | 28 | January 2nd 09 02:26 PM |
Military: Pilot confusion led to F-16 crash that killed one pilot | Otis Willie | Military Aviation | 0 | September 1st 04 12:30 AM |
P-51C crash kills pilot | Paul Hirose | Military Aviation | 0 | June 30th 04 05:37 AM |
Fatal plane crash kills pilot in Ukiah CA | Randy Wentzel | Piloting | 1 | April 5th 04 05:23 PM |
AmeriFlight Crash | C J Campbell | Piloting | 5 | December 1st 03 02:13 PM |