Table of Contents (Partial List of Selected Items) |
|
Document |
Filing Date |
Document Title |
Pages |
Photo |
|
168385 | Oct 03, 2002 | Order of Hearing: 1A |
1 | |
168386 | Oct 03, 2002 | Notice of Designation of Chairman of Board of Inquiry: 1B |
1 | |
168387 | Oct 03, 2002 | Designation of Hearing Officer: 1C |
1 | |
168388 | Oct 03, 2002 | Designation of Parties to the Hearing: 1D |
1 | |
168389 | Oct 03, 2002 | Notice of Hearing: 1E |
1 | |
169692 | Oct 23, 2002 | Hearing Exhibit List: 1F |
4 | |
167209 | Sep 11, 2002 | Operations 2 - Factual Report of Group Chairman |
28 | |
167210 | Sep 11, 2002 | Operations 2 - Attachments A and B - Interview Summaries |
812 | |
167028 | Sep 10, 2002 | Operations 2 - Attachment D - Submitted Statements |
9 | |
167036 | Sep 10, 2002 | Operations 2 - Attachment H - Correspondence from Airplane Manufacturers to American Airlines and Response |
11 | |
167041 | Sep 10, 2002 | Operations 2 - Attachment I - Excerpts from the AAMP Flight Training Course Material |
16 | |
167042* | Sep 10, 2002 | Operations 2 - Attachment J - FAA Correspondence |
23 | |
167043 | Sep 10, 2002 | Operations 2 - Attachment K - Excerpt from Airbus Industrie presentation at 10th Performance and Operations Conference |
7 | |
167044* | Sep 10, 2002 | Operations 2 - Attachment L - Excerpts from A300-600 American Airlines Operating Manual - Volume 1 |
21 | |
167046 | Sep 10, 2002 | Operations 2 - Attachment N - FCOM Bulletin, Use of Rudder on Transport Category Airplanes |
5 | |
167047 | Sep 10, 2002 | Operations 2 - Attachment O - Boeing commercial Airplane Group - Flight Operations Technical Bulletin |
16 | |
167049 | Sep 10, 2002 | Operations 2 - Attachment Q - Excerpts from the A300-600 American Airlines Operating Manual - Volume 2 |
4 | |
167051 | Sep 10, 2002 | Operations 2 - Attachment S - Excerpts from the Airbus A300-600 FCOM - Volume 2 |
7 | |
167189* | Sep 11, 2002 | Operations 2 - Attachment U - Excerpts of Airbus Aerodynamic Principles of Large-Airplane Upsets |
12 | |
167190 | Sep 11, 2002 | Operations 2 - Attachment V - Excerpts from the Boeing/Airbus Training Aid |
11 | |
167193 | Sep 11, 2002 | Operations 2 - Attachment X - Flight Crew Records for Captain States |
10 | |
167194 | Sep 11, 2002 | Operations 2 - Attachment Y - Flight Crew Records for First Officer Molin |
8 | |
166537 | Aug 29, 2002 | ATC 3 - Factual Report of Group Chairman |
8 | |
164340 | Aug 06, 2002 | Witness 4 - Factual Report of Group Chairman |
14 | |
162868 | Jul 15, 2002 | Meteorology 5 - Factual Report of Group Chairman |
32 | |
168195 | Dec 16, 2002 | Structures 7 - Factual Report of Group Chairman (exhibit A) (rev. 16dec2002) |
24 | |
168885 | Oct 11, 2002 | Structures 7 - FAA Loads Exhibits (Exhibit F) |
6 | |
168823 | Oct 10, 2002 | Structures 7 - Airbus Loads - Certification Standards (Exhibit 7-I) |
7 | |
168829 | Oct 10, 2002 | Structures 7 - Airbus A300-600R Vetical Tail Loads Calculation (Exhibit 7-N) |
6 | |
168874 | Oct 11, 2002 | Structures 7 - Airbus AA587 Loads Assesment (Exhibit P) |
11 | |
166317 | Aug 27, 2002 | Powerplants 8 - Factual Report of Group Chairman |
42 | |
168123 | Sep 30, 2002 | Systems 9 - Factual Report of Group Chairman |
25 | |
168467 | Oct 04, 2002 | Systems 9 - A300-600 Yaw Damper System Overview (Exhibit No. 9-B) |
5 | |
168468 | Oct 04, 2002 | Systems 9 - A300-600 Yaw Autopilot System Overview (Exhibit No. 9-C) |
6 | |
168469 | Oct 04, 2002 | Systems 9 - A300-600 Rudder Travel Limitation System (Exhibit No. 9-D) |
7 | |
168592 | Oct 07, 2002 | Systems 9 - A300-600 Rudder Servo Controls Overview (Exhibit No. 9-E) |
5 | |
168199 | Sep 30, 2002 | Flight Data Recorder 10 - Flight Data Recorder Group Chairman's Solid State Flight Data Recorder Factual Report |
12 | |
168794 | Oct 10, 2002 | Maintenance Records 11 - Factual Report of Group Chairman |
35 | |
168249 | Oct 02, 2002 | Cockpit Voice Recorder 12 - Factual Report of Group Chairman |
35 | |
168250 | Oct 02, 2002 | Cockpit Voice Recorder 12B - Specialist's Sound Spectrum Study, Cockpit Voice Recorder |
15 | |
168982* | Oct 15, 2002 | Aircraft Performance 13 - Factual Report of Group Chairman |
176 | |
174831 | Jan 30, 2003 | Aircraft Performance 13 - Factual Report Errata #1 |
4 | |
198619 | Oct 16, 2003 | Aircraft Performance 13 - Factual Report of Group Chairman - Addendum 1 |
44 | |
217763 | Aug 25, 2004 | Aircraft Performance 13 - Factual Report of Group Chairman - Addendum 2 (Revised 13Oct2004) |
50 | |
168575 | Oct 07, 2002 | Human Performance 14 - Factual Report of Group Chairman |
33 | |
168576 | Oct 07, 2002 | Human Performance 14 - Study Report, Vertical Motion Simulator Activities, Phase I: Backdrive of Accident Flight |
21 | |
288388 | Dec 24, 2003 | Human Performance 14 - Hess Report |
22 | |
158773 | May 17, 2002 | Materials Laboratory 15 - Factual Report 02-046 |
3 | |
164273* | Aug 06, 2002 | Materials Laboratory 15 - Factual Report 02-076 |
5 | |
168606 | Oct 07, 2002 | Materials Laboratory 15 - Factual Report 02-077 |
63 | |
168619* | Oct 07, 2002 | Materials Laboratory 15 - Factual Report 02-078 with Appendix A |
26 | |
168624* | Oct 07, 2002 | Materials Laboratory 15 - Factual Report 02-078 Appendix B |
52 | |
169028* | Oct 16, 2002 | Materials Laboratory 15 - Factual Report 02-083 |
51 | |
168880 | Oct 11, 2002 | Materials Laboratory 15 - Factual Report 02-091 |
7 | |
168584 | Oct 07, 2002 | Materials Laboratory 15 - Exhibit 15A Selected Photographs and Drawings of the Damage Areas on the Fin and Rudder |
13 | |
168947* | Oct 15, 2002 | Materials Laboratory 15 - Exhibit 15B - Selected Results of the Nondestructive Examination of the Vertical Stabilizer and Rudder |
29 | |
168653 | Oct 08, 2002 | Materials Laboratory 15 - Exhibit 15C Selected Photographs of the Fractographic Examination of the Vertical Stabilizer and Rudder |
28 | |
168806 | Oct 10, 2002 | Materials Laboratory 15 - Exhibit 15D Airbus Submission - Thermal Analysis by DMA and MDSC |
20 | |
168983 | Oct 15, 2002 | Specialist's Report of Investigation - Video Study (Exhibit 17A) |
25 | |
290584 | Jan 29, 2004 | BEA comments on the report entitled "An Inquiry into Whether a Pilot-Induced oscillation was a factor in the crash of American Airlines Flight 587." |
5 | |