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Printed page Unnumbered appendix sheet. PDF page 189.
Without the use of horizontal stabilizer trim, this would require control column forces greater than 50 pounds and large control column inputs; if those forces were relaxed, the airplane would have initiated a return to a nose- up attitude dueOpen official document at PDF page 189Aircraft Accident Report: SilkAir Flight MI 185, Boeing B737-300, 9V-TRF
Printed page Unnumbered appendix sheet. PDF page 226.
the last ATC radar points, this would and large control require control column forces greater than 50 pounds column inputs. However, the simulations indicated that if the control column input forces had been relaxed, the aircraft would have initiated aOpen official document at PDF page 226Aircraft Accident Report: SilkAir Flight MI 185, Boeing B737-300, 9V-TRF
Printed page 3. PDF page 6.
Without the use of horizontal stabilizer trim, this would require control column forces greater than 50 pounds and large control column inputs; if those forces were relaxed, the airplane would have initiated a return to a nose-up attitude due toOpen official document at PDF page 6NTSB comments on the draft final report of the SilkAir MI 185 accident
Printed page 37. PDF page 40.
similar to that of the last ATC radar points, this would require control column forces greater than 50 pounds and large control column inputs. However, the simulations indicated that if the control column input forces had been relaxed, the aircraftOpen official document at PDF page 40NTSB comments on the draft final report of the SilkAir MI 185 accident