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Printed page 30. PDF page 43.
results suggested that a separation had taken place at a low altitude near or below 12,000 ft., while the aircraft was flying at a high Mach number. 2.3.2 Results of Flutter Studies Flutter studies undertaken suggested that the applied staticOpen official document at PDF page 43Aircraft Accident Report: SilkAir Flight MI 185, Boeing B737-300, 9V-TRF
Printed page 31. PDF page 44.
separation of the empennage parts could have had occurred at an altitude near or below 12,000 ft, due to an unstable flutter as the aircraft exceeded 1.2 Vd� 2.4 Power Control Units and Actuators 2.4.1 Main Rudder PCU As statedOpen official document at PDF page 44Aircraft Accident Report: SilkAir Flight MI 185, Boeing B737-300, 9V-TRF
Printed page Unnumbered appendix sheet. PDF page 219.
separation of the empennage parts could have had occurred at an altitude near or below 12,000 ft, due to an unstable .flutter as the aircraft exceeded 1.2 Vd. N-37Open official document at PDF page 219Aircraft Accident Report: SilkAir Flight MI 185, Boeing B737-300, 9V-TRF
Printed page 30. PDF page 33.
separation of the empennage parts could have had occurred at an altitude near or below 12,000 ft, due to an unstable flutter as the aircraft exceeded 1. 2 Vd. These two sentences may be misleading. To provide clarification, the NTSCOpen official document at PDF page 33NTSB comments on the draft final report of the SilkAir MI 185 accident
Printed page 21. PDF page 34.
separation of the remaining components took place at a lower altitude near or below 12,000 feet. 1.16.5 Flutter Studies The NTSB-Boeing Report [Reference 14] showed the following: � During cruise at 35,000 feet at 0.74 Mach The applied static loadsOpen official document at PDF page 34Aircraft Accident Report: SilkAir Flight MI 185, Boeing B737-300, 9V-TRF