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. . 102 5. APPENDIXES Appendix A--Investigation and Hearing ....................... 111 Appendix B--Personnel Information . . . . . .. .. . . .. .. . .. . . .. . .. . 112 Appendix C--Horizontal Stabilizer Damage Diagram............Open official document at PDF page 5United Airlines Flight 232, McDonnell Douglas DC-10-10, Sioux Gateway Airport, Sioux City, Iowa, July 19, 1989
Printed page 5. PDF page 11.
longitude. 1.2 Injuries to Persons In1uries Crew passengers Others Total Fatal 1 110 0 111 Serious 6 41* 0 47 Minor 4 121 0 125 None _Q 13 Q _n Total 11 285 0 296 *One passenger died 31 daysOpen official document at PDF page 11United Airlines Flight 232, McDonnell Douglas DC-10-10, Sioux Gateway Airport, Sioux City, Iowa, July 19, 1989
Printed page 18. PDF page 24.
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Printed page 24. PDF page 30.
24 The data revealed no evidence of RPM that exceeded the maximum allowable limit of 111 percent Ni for flights prior to the accident flight. However, the data did reveal cyclic excursions in Ni within allowable values on allOpen official document at PDF page 30United Airlines Flight 232, McDonnell Douglas DC-10-10, Sioux Gateway Airport, Sioux City, Iowa, July 19, 1989
Printed page 26. PDF page 32.
1:1::1 - Prime Search Area : 12 1 E9 9 I : .. E LK ~--+--+----:f.~ l!·~ 13'136 111 ...~--~---~---~-~---~--~---~---~-~..+.--l---~c29>-1-~--1-- ;: . 17 ,-=·:~···· . M31 SCOTT TOWNSHIP I 3 I I f BOpen official document at PDF page 32United Airlines Flight 232, McDonnell Douglas DC-10-10, Sioux Gateway Airport, Sioux City, Iowa, July 19, 1989
Printed page 65. PDF page 71.
manufacture the bi 11 et used for disk S/N MPO 00385 and the Category I disks. Category 111.--(total 213) Fan disks were inspected by either contact or immersion-ultrasonic inspect ion methods by February 4, 1990. Contact-ultrasonic inspection on installed enginesOpen official document at PDF page 71United Airlines Flight 232, McDonnell Douglas DC-10-10, Sioux Gateway Airport, Sioux City, Iowa, July 19, 1989