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Printed page label not indexed. PDF page 39.
tube was pushed towards the locked position, the switch switched off the flight deck warning light, although the ends of the lock pins were still 3 millimetres away from the restraining flanges (fig 3). It should be noted, moreover, thatOpen official document at PDF page 39French Commission of Inquiry final report: Turkish Airlines DC-10 TC-JAV, official UK-hosted English translation
Printed page label not indexed. PDF page 41.
limit warning switch. The incorrect adjustment of this switch caused the flight deck warning light to go out when the door was still unlocked. Because of the insufficient protrusion of the lock pins, the locking handle and vent door couldOpen official document at PDF page 41French Commission of Inquiry final report: Turkish Airlines DC-10 TC-JAV, official UK-hosted English translation
Printed page label not indexed. PDF page 42.
jatches were not fully closed and the latch lock pias were not in place. _ The flight deck warning light had gone out before effective locking had occurred. - The altitude reached by the American Airlines DC-10 was of theOpen official document at PDF page 42French Commission of Inquiry final report: Turkish Airlines DC-10 TC-JAV, official UK-hosted English translation
Printed page label not indexed. PDF page 44.
em 61 [1] Position at which | flight deck visual warning light is witched off FIG.4 Extreme position of lock tube Handle closed Rear face |“ Front face CORRECT ADJUSTMENTS FIG.5 a Lock tube a warning. Lo | switch --Open official document at PDF page 44French Commission of Inquiry final report: Turkish Airlines DC-10 TC-JAV, official UK-hosted English translation
Printed page 47. PDF page 52.
be pulled. down without the use of any. abnormal force and for the flight deck visual warning light to be switched off, when the latches were not fully engaged and the lock pins not in place. The tests and researchOpen official document at PDF page 52French Commission of Inquiry final report: Turkish Airlines DC-10 TC-JAV, official UK-hosted English translation
Printed page 43. PDF page 45.
warning, followed by a characteristic cricket sound and the illumination of the Master Warning light. It is triggered by the FWC when the highest of the valid angle of attack values exceeds 43 F-GZCP - 1st June 2009Open official document at PDF page 45Final Report: Accident on 1st June 2009 to the Airbus A330-203 registered F-GZCP operated by Air France flight AF 447