Search report text, read a short matching passage, then open the source page.
Exact phrases match first; otherwise all words must occur close together. Six excerpts maximum. Text extraction cannot search image-only charts. Warsaw uses a report transcription with missing figures and appendices.
7 matching PDF pages. Showing 6 short source excerpts. Open the document for full context.
Printed page 3. PDF page 9.
to manipulate the flight controls. The check airman attempted to use engine power to control pitch and roll. He said that the airplane had a continuous tendency to turn right, making it diffi<;ult to maintain a stable pitch attitude. HeOpen official document at PDF page 9United Airlines Flight 232, McDonnell Douglas DC-10-10, Sioux Gateway Airport, Sioux City, Iowa, July 19, 1989
Printed page 118. PDF page 124.
pitch the nose up and a decrease In thrust wlll pitch the nose down. Consequently, to control pitch osclllatlons with wing engine thrust changes, It Is necessary to apply power Just as the nose Is coming down, and to retardOpen official document at PDF page 124United Airlines Flight 232, McDonnell Douglas DC-10-10, Sioux Gateway Airport, Sioux City, Iowa, July 19, 1989
Printed page 119. PDF page 125.
lower altitudes. Jam accelerations followed by rapid throttle chops may be necessary to control pitch without generating additional pitch oscillations as a sustained thrust input would do. If asymmetric thrust is required to keep the wings level, a rolling tendencyOpen official document at PDF page 125United Airlines Flight 232, McDonnell Douglas DC-10-10, Sioux Gateway Airport, Sioux City, Iowa, July 19, 1989
Printed page 121. PDF page 127.
and roll axis. (If the ailerons were not trtrrimed and the $tablllzer was not used to control pitch, the con- dition would be Identical to the Sioux City aircraft.) It Is this control that will be dis- cussed below: 2.1Open official document at PDF page 127United Airlines Flight 232, McDonnell Douglas DC-10-10, Sioux Gateway Airport, Sioux City, Iowa, July 19, 1989
Printed page 122. PDF page 128.
pitch-control. As In the case with no hydraulics, the throttles are used in the same manner to control pitch (that Is an aggressive advance just as the nose is coming down, or a rapid retard just as the nose beginsOpen official document at PDF page 128United Airlines Flight 232, McDonnell Douglas DC-10-10, Sioux Gateway Airport, Sioux City, Iowa, July 19, 1989
Printed page 120. PDF page 126.
advancing the power and allowing the aircraft to pitch up. Remember that the power Is not controlling speed, so only enough thrust should be used to Initiate a climb at moderate pitch attitude. Too much pitch could cause the stickOpen official document at PDF page 126United Airlines Flight 232, McDonnell Douglas DC-10-10, Sioux Gateway Airport, Sioux City, Iowa, July 19, 1989