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| 1 |
Order of Hearing: 1A |
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| 2 |
Notice of Designation of Chairman of Board of Inquiry: 1B |
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| 3 |
Designation of Hearing Officer: 1C |
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| 4 |
Designation of Parties to the Hearing: 1D |
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| 5 |
Notice of Hearing: 1E |
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| 6 |
Hearing Exhibit List: 1F |
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| 7 |
Operations 2 - Factual Report of Group Chairman |
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| 8 |
Operations 2 - Attachments A and B - Interview Summaries |
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| 9 |
Operations 2 - Attachment C - Port Authority Police Reports |
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| 10 |
Operations 2 - Attachment D - Submitted Statements |
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| 11 |
Operations 2 - Attachment E - Airport Diagrams |
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| 12 |
Operations 2 - Attachment F - Kennedy International Airport Departure Information |
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| 13 |
Operations 2 - Attachment G - Airplane Weight and Balance Information |
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| 14 |
Operations 2 - Attachment H - Correspondence from Airplane Manufacturers to American Airlines and Response |
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| 15 |
Operations 2 - Attachment I - Excerpts from the AAMP Flight Training Course Material |
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| 16 |
Operations 2 - Attachment J - FAA Correspondence |
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| 17 |
Operations 2 - Attachment K - Excerpt from Airbus Industrie presentation at 10th Performance and Operations Conference |
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| 18 |
Operations 2 - Attachment L - Excerpts from A300-600 American Airlines Operating Manual - Volume 1 |
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| 19 |
Operations 2 - Attachment M - Flight Operations Technical Informational Bulletin |
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| 20 |
Operations 2 - Attachment N - FCOM Bulletin, Use of Rudder on Transport Category Airplanes |
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| 21 |
Operations 2 - Attachment O - Boeing commercial Airplane Group - Flight Operations Technical Bulletin |
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| 22 |
Operations 2 - Attachment P - Excerpt from T.O. 1C-135(K)-1, Flight - USAF Series KC-135-R/T Aircraft |
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| 23 |
Operations 2 - Attachment Q - Excerpts from the A300-600 American Airlines Operating Manual - Volume 2 |
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| 24 |
Operations 2 - Attachment R - Excerpts from the Airbus A300-600 FCOM - Volume 1 |
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| 25 |
Operations 2 - Attachment S - Excerpts from the Airbus A300-600 FCOM - Volume 2 |
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| 26 |
Operations 2 - Attachment T - Excerpts from the Airbus A300-600 Flight Manual |
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| 27 |
Operations 2 - Attachment U - Excerpts of Airbus Aerodynamic Principles of Large-Airplane Upsets |
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| 28 |
Operations 2 - Attachment V - Excerpts from the Boeing/Airbus Training Aid |
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| 29 |
Operations 2 - Attachment W - Excerpts from the American Airlines Flight Manual - Part 1 |
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| 30 |
Operations 2 - Attachment Z - Excerpts from Pilot Interviews on AA 903 |
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| 31 |
Operations Exhibit No 2-B |
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| 32 |
Operations Exhibit No 2-Q |
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| 33 |
Operations Exhibit No 2-S |
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| 34 |
Operations Exhibit No 2-T |
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| 35 |
Operations Exhibit No 2-U |
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| 36 |
Operations Exhibit No 2-V |
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| 37 |
Operations Exhibit No 2-W |
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| 38 |
Operations Exhibit No 2-X |
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| 39 |
Operations Exhibit No 2-Y |
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| 40 |
Operations Exhibit No 2-Z |
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| 41 |
ATC 3 - Factual Report of Group Chairman |
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| 42 |
ATC 3 - Attachment 1: JFK Daily record of Facility Operations |
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| 43 |
ATC 3 - Attachment 2: JFK Position Logs |
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| 44 |
ATC 3 - Attachment 3: JFK Controller Statements |
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| 45 |
ATC 3 - Attachment 4: JFK Tower Cab Layout |
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| 46 |
ATC 3 - Attachment 5: JFK Communications Transcripts |
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| 47 |
ATC 3 - Attachment 6: JFK Airport Diagram |
1 |
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| 48 |
ATC 3 - Attachment 7: AAL587 Flight Strip |
1 |
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| 49 |
ATC 3 - Attachment 8: AAL587 Pre-departure Clearance Data |
1 |
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| 50 |
ATC 3 - Attachment 9: New York TRACON Aircraft Accident Package |
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| 51 |
Witness 4 - Factual Report of Group Chairman |
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| 52 |
Witness 4 - Appendix A: Witness Spreadsheet |
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| 53 |
Witness 4 - Appendix B: Documents Pertaining to Witnesses 1-50 |
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| 54 |
Witness 4 - Appendix C: Documents Pertaining to Witnesses 51-100 |
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| 55 |
Witness 4 - Appendix D: Documents Pertaining to Witnesses 101-150 |
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| 56 |
Witness 4 – Addendum 1 to Appendix D: Documents Pertaining to Witnesses 143 and 144 |
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| 57 |
Witness 4 - Appendix E: Documents Pertaining to Witnesses 151-200 |
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| 58 |
Witness 4 - Appendix F: Documents Pertaining to Witnesses 201-250 |
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| 59 |
Witness 4 - Appendix G: Documents Pertaining to Witnesses 251-300 |
104 |
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| 60 |
Witness 4 - Appendix H: Documents Pertaining to Witnesses 301-354 |
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| 61 |
Systems 9 - ADDENDUM NUMBER 6 TO THE SYSTEMS GROUP CHAIRMAN’S FACTUAL REPORT OF INVESTIGATION – YAW DAMPER EXAMINATION |
56 |
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| 62 |
Systems 9 - Addendum Number 3 to the Systems Group Chairman's Factual Report of Investigation - Flight Control Linkage |
64 |
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| 63 |
Witness 4 - Appendix I: Witness Questionnaires |
4 |
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| 64 |
Systems 9 - Addendum Number 2 to the Systems Group Chairman's Factual Report - Rudder Servo Controls and Linkage - Appendix A |
8 |
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| 65 |
Witness 4 - Appendix J: Additional Information Provided by Local Newspaper |
31 |
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| 66 |
Meteorology 5 - Factual Report of Group Chairman |
32 |
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| 67 |
Flight Data Recorder 10 - Attachment I of Addendum 1 to Factual Report of Ancillary B747 Aircraft |
0 |
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| 68 |
Meteorology 5 - Meteorological Documentation |
7 |
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| 69 |
Flight Data Recorder 10 - Factual Report of Ancillary B747 Aircraft |
6 |
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| 70 |
Flight Data Recorder 10 - Addendum 1 to Factual Report of Ancillary B747 Aircraft |
1 |
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| 71 |
Flight Data Recorder 10 - Attachment 1 Tabular Data of Ancillary B747 Aircraft |
0 |
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| 72 |
Structures 7 - Factual Report of Group Chairman (exhibit A) (rev. 16dec2002) |
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| 73 |
Flight Data Recorder 10 - Flight Recorder System Special Study |
31 |
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| 74 |
Structures 7 - Attachment A (exhibit B) |
51 |
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| 75 |
Structures 7 - Attachment B (exhibit C) |
30 |
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| 76 |
Structures 7 - Attachment C (exhibit D) |
7 |
0 |
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| 77 |
Structures 7 - Addendum 1, Airbus Report "A300B4-605R MSN420 - AAL587 New York Accident - Loads Assessment" |
17 |
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| 78 |
Structures 7 - Addendum 1A, Airbus Report "AAL587 Investigation A300-600R Fin Root CSF diagrams" |
10 |
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| 79 |
Structures 7 - Addendum 1C, Airbus Report "AAL587 Investigation, side-slip computation with integration method" |
21 |
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| 80 |
Structures 7 - Addendum 1D, Airbus Report "HANDLING QUALITIES INVESTIGATIONS" |
24 |
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| 81 |
Structures 7 - Addendum 2, Airbus Report "AAL587 Investigation, Accident Analysis – FEM Global model VTP & Rudder" |
29 |
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| 82 |
Structures 7 - Addendum 3, Airbus Report "AAL587 Airbus Structure Investigation, Accident Analysis – FEM RHS local rear lug model" |
51 |
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| 83 |
Structures 7 - Addendum 4, Airbus Report "AAL587 Airbus Structure Investigation, FEM Global to Local analysis details" |
15 |
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| 84 |
Structures 7 - Addendum 5, Airbus Report "AAL587 Airbus Structure Investigation, LHS Lug sub-component test #1 FEM analysis" |
33 |
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| 85 |
Structures 7 - Addendum 10, Airbus Report “AAL587 Investigation – Study on potential effect of rudder delamination” |
20 |
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| 86 |
Structures 7 - Addendum 7, Airbus Test Requirement "Test program Rear Main Fitting A300-600R (Lug Test #1)" |
24 |
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| 87 |
Structures 7 - Addendum 8A, NASA Report "NASA Structural Analysis Report for theAmerican Airlines Flight 587 AccidentInvestigation: Part 1 – Summary of Findings" |
15 |
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| 88 |
Structures 7 - Addendum 8A (REV A) NASA Report NASA/TMX—2003–000000 "NASA Structural Analysis Report for theAmerican Airlines Flight 587 AccidentInvestigation: Part 1 – Summary of Findings" |
13 |
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| 89 |
Structures 7 - Addendum 8B, NASA Report NASA/TMX-2003-000000, "Structural Analysis Report on the AmericanAirlines Flight 587 Accident – Part 2 – Global Fin/Rudder StructuralAnalysis and Assessment" |
194 |
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| 90 |
Structures 7 - Addendum 8C, NASA Report NASA/TMX-2003-XXX, “Structural Analysis Report on the American Airlines Flight 587 Accident – Part 3” |
99 |
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| 91 |
Structures 7 - Addendum 8D,NASA Report "NASA Structural Analysis Report on the American Airlines Flight 587 Accident– Part 3- Appendix A" |
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| 92 |
Structures 7 - Addendum 9, Airbus Report "Study of Aeroelastic Scenarios" |
6 |
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| 93 |
Structures 7 - Addendum 6, Airbus Report "AAL587 Airbus Structure Investigation, Lug sub-component test #1 – Results Test/FEA Comparison" |
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| 94 |
Structures 7 - Addendum 6 (REV A) Airbus Report "“AAL587 Airbus Structure Investigation, Lug sub-component test #1 –Results Test/FEA Comparison" Issue 4 |
51 |
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| 95 |
Materials Laboratory 15 - Factual Report 04-065 Appendix F |
22 |
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| 96 |
Materials Laboratory 15 - Factual Report 04-065 Appendix E |
26 |
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| 97 |
Materials Laboratory 15 - Factual Report 04-065 Appendix D |
29 |
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| 98 |
Materials Laboratory 15 - Factual Report 04-065 Appendix C |
17 |
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| 99 |
Materials Laboratory 15 - Factual Report 04-065 Appendix B |
18 |
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| 100 |
Materials Laboratory 15 - Factual Report 04-065 Appendix A |
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| 101 |
Materials Laboratory 15 - Factual Report 04-065 |
7 |
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| 102 |
Structures 7 - Addendum 11, Airbus Report “Engine loads calculation for the A300-600R (flight number 587)” |
10 |
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| 103 |
Structures 7 - Addendum 12, Airbus Report "A300/A310, Rear Fin Box Attachment – Sub-component Test Summary" |
15 |
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| 104 |
Structures 7 - Addendum 13, Airbus Report "A300/A310 Composite Fin Box, Full-Scale Certification Test Summary" |
26 |
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| 105 |
Structures 7 - Addendum 14, Airbus Report "MSN513 LHS and RHS Test Program for Rear Main Fittings Lug Test#2and #3" |
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| 106 |
Structures 7 - Addendum 15, Airbus Report "AAL587 Airbus Structure Investigation, Lug Test#2 – Results Test/FEA Comparison" |
56 |
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| 107 |
Structures 7 - Addendum 16 Airbus Report "AAL587 Airbus Structure Investigation, Lug Test#3 – Results Test/FEA Comparison" |
63 |
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| 108 |
Structures 7 - Addendum 17, Airbus Report "Flight AA587 Structure Accident Investigation, Validation ofSubcomponent Test Principles" |
22 |
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| 109 |
Structures 7 - Addendum 18, Airbus Report "Flight AA587 Accident Investigation Load Summary for Rear Main Lug" |
23 |
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| 110 |
Structures 7 - Addendum 19, Airbus Report “Flight AA587 Accident Investigation, Influence of the VTP Root Bending/Torsion Ratio of Load Case W375 Is 18 and CFD Analyses on the RHS Rear Main Lug Force” |
11 |
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| 111 |
Structures 7 - Addendum 20, Airbus Report "Incoming inspection of the rear lug cut outs LH side shell of the finbox from the aircraft MSN 513 of the American airlines" |
18 |
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| 112 |
Structures 7 - Addendum 21, Airbus Report "Incoming inspection of the rear lug cut outs RH side shell of the finbox from the aircraft MSN 513 of the American airlines” |
17 |
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| 113 |
Structures 7 - Addendum 22 - Russian Requirements Part 25, 25.351 "Yawing Conditions" |
5 |
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| 114 |
Structures 7 - A310, A300-600 & A300-600R Airworthiness Requirements (Exhibit E) |
51 |
0 |
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| 115 |
Structures 7 - FAA Loads Exhibits (Exhibit F) |
6 |
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| 116 |
Structures 7 - Airworthiness Directives 2001-23-51, 2002-06-09, 2001-09-03 & 2002-03-11 (Exhibit G) |
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| 117 |
Structures 7 - Airbus Loads Overview (Exhibit 7-H) |
21 |
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| 118 |
Structures 7 - Airbus Loads - Certification Standards (Exhibit 7-I) |
7 |
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| 119 |
Structures 7 - Airbus Loads Models (Exhibit J) |
4 |
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| 120 |
Structures 7 - Airbus Loads Methods (Exhibit K) |
3 |
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| 121 |
Structures 7 - Airbus Flexibilty Description (Exhibit L) |
5 |
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| 122 |
Structures 7 - Airbus Gust Requirements - Historical Overview (Exhibit M) |
19 |
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| 123 |
Structures 7 - Airbus A300-600R Vetical Tail Loads Calculation (Exhibit 7-N) |
6 |
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| 124 |
Structures 7 - Airbus Loads Process & Methods for In Service Events (Exhibit O) |
4 |
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| 125 |
Structures 7 - Airbus AA587 Loads Assesment (Exhibit P) |
11 |
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| 126 |
Structures 7 - Airbus Vertical Tail High Loads in Service Events (Exhibit 7-Q) |
6 |
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| 127 |
Structures 7 - Summary of Airbus Loads Analysis for AA903 (Exhibit R) |
12 |
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| 128 |
Structures 7 - Airbus Comparison of AA587 & AA903 Events (Exhibit S) |
2 |
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| 129 |
Structures 7 - Airbus FE Model Loading - Nodal Loads Process (Exhibit 7-T) |
11 |
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| 130 |
Structures 7 - Airbus Report "AAL587 Crash: Study of Aeroelastic Scenarios" (Exhibit U) |
7 |
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| 131 |
Structures 7 - Airbus Report "AAL587 Crash: Study on Potential effect of Rudder Delamination" (Exhibit V) |
6 |
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| 132 |
Human Performance 14 - Study Report, American Airlines Simulator Exercise |
13 |
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| 133 |
Structures 7 - FAA Composite Exhibit (Exhibit W) |
2 |
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| 134 |
Structures 7 - Airbus Structures Overview (Exhibit X) |
29 |
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| 135 |
Structures 7 - Static and Fatigue/Damage Tolerance Demonstration (Exhibit Y) |
2 |
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| 136 |
Structures 7 - Compliance with FAR/JAR 25.571 (Exhibit Z) |
6 |
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| 137 |
Structures 7 - Stabilizer Attach Point Design Conditions (Exhibit AA) |
3 |
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| 138 |
Materials Laboratory 15 - Factual Report 03-033, CT Scanning |
22 |
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| 139 |
Materials Laboratory 15 - Factual Report 03-018, Porosity |
6 |
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| 140 |
Materials Laboratory 15 - Factual Report 02-082, Material Testing |
43 |
0 |
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| 141 |
Structures 7 - Airbus FEM Calculation of Rear Main Lug (Exhibit BB) |
13 |
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| 142 |
Structures 7 - Airbus Report Part 1 Calculation of the load Levels experienced by the VTP & rudder during the accident (Exhibit CC) |
18 |
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| 143 |
Structures 7 - Airbus Report Part 2 Analysis of the rupture sequence of the VTP during the accident Exhibit DD) |
16 |
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| 144 |
Structures 7 - Airbus Report Veryical Stabilizer attachment loads experienced during the flight AA093 incident and NDI finding assessment (Exhibit EE) |
15 |
1 |
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| 145 |
Structures 7 - Static Test on rudder fittings (BR3) A300-600 (Exhibit FF) |
18 |
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| 146 |
Structures 7 - A300-600R Vertical Stabilizer StructureDesign & Certification (Exhibit GG) |
30 |
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| 147 |
Structures 7 - NASA Support Overview (Exhibit HH) |
13 |
0 |
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| 148 |
Structures 7 - NASA Local Lug Analysis (Exhibit JJ) |
8 |
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| 149 |
Structures 7 - Airbus Report Part 3 Analysis of the rupture sequence of the rudder following the accident (Exhibit KK) |
24 |
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| 150 |
Structures 7 - Various Airbus Correspondence referencing American Airlines Flight 903 (Exhibit 7-LL ) |
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| 151 |
Powerplants 8 - Factual Report of Group Chairman |
42 |
36 |
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| 152 |
Powerplants 8 - Appendix 1 - Left and right engine's engine condition monitoring data. |
2 |
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| 153 |
Powerplants 8 - Appendix 2 - Left and right engine's takeoff performance data. |
2 |
0 |
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| 154 |
Powerplants 8 - Appendix 3 - Port Authority of NY and NJ Police report on obtaining the fuel samples and transferring them to Nobil Petro Testing |
1 |
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| 155 |
Powerplants 8 - Appendix 4 - Nobil Petro Testing reports on 8-point tests accomplished on fuel samples. |
3 |
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| 156 |
Powerplants 8 - Appendix 5 - Nobil Petro Testing laboratory worksheet for sample from tank No. 314 and corrected laboratory analysis report showing correct 90 percent recovered. |
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| 157 |
Powerplants 8 - Appendix 6 - Nobil Petro Testing reports on the full tests accomplished on the fuel samples. |
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| 158 |
Systems 9 - Factual Report of Group Chairman |
25 |
5 |
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| 159 |
Systems 9 - A300-600 Yaw Damper System Overview (Exhibit No. 9-B) |
5 |
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| 160 |
Systems 9 - A300-600 Yaw Autopilot System Overview (Exhibit No. 9-C) |
6 |
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| 161 |
Systems 9 - A300-600 Rudder Travel Limitation System (Exhibit No. 9-D) |
7 |
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| 162 |
Systems 9 - A300-600 Rudder Servo Controls Overview (Exhibit No. 9-E) |
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| 163 |
Systems 9 - Addendum 1 to the Systems Group Chairmann's Factual Report of Investigation Concerning the Artificial Feel and Trim System (Exhibit 9-F) |
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| 164 |
Flight Data Recorder 10 - Flight Data Recorder Group Chairman's Solid State Flight Data Recorder Factual Report |
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| 165 |
Flight Data Recorder 10 - Flight Data Recorder Factual Report Attachment I (FDR Parameter Listing Sorted By Word Location) |
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| 166 |
Flight Data Recorder 10 - Flight Data Recorder Factual Report Attachment II (Selected FDR Data Plotted - 8 Plots Total) |
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| 167 |
Maintenance Records 11 - Factual Report of Group Chairman |
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| 168 |
Maintenance Records 11 - Factual Report, Att. B: References Between MRB and ESM |
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| 169 |
Maintenance Records 11 - Factual Report, Att. C: Delivery Papers of N14053 |
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| 170 |
Maintenance Records 11 - Factual Report, Att. D: Concession Documents |
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Maintenance Records 11 - Factual Report, Att. E: Inspection Card 3204 |
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Maintenance Records 11 - Factual Report, Att. F: Non-Routine Card 2462733 |
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Maintenance Records 11 - Factual Report, Att. G: Corrective Action of Non-Routine Card |
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| 174 |
Maintenance Records 11 - Factual Report, Att. H: Examples from the Illustrated Parts Catalog |
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| 175 |
Maintenance Records 11 - Factual Report, Att. I: 1994 Turbulence Event |
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Maintenance Records 11 - Factual Report, Att. J: Mechanic Interviews |
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Maintenance Records 11 - Factual Report, Att. K: E58 Repair Form |
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| 178 |
Maintenance Records 11 - Factual Report, Att. L: Parts List Documentation |
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| 179 |
Cockpit Voice Recorder 12 - Factual Report of Group Chairman |
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| 180 |
Cockpit Voice Recorder 12B - Specialist's Sound Spectrum Study, Cockpit Voice Recorder |
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| 181 |
Aircraft Performance 13 - Factual Report of Group Chairman |
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| 182 |
Aircraft Performance 13 - Errata Sheet #1 to Aircraft Performance Study |
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| 183 |
Aircraft Performance 13 - Exhibit 13B Aircraft Performance Factual Report for American Airlines Flight 903 |
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| 184 |
Aircraft Performance 13 - Addendum 1 |
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| 185 |
Aircraft Performance 13 - Addendum 2 (Revised 13Oct2004) |
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| 186 |
Human Performance 14 - Factual Report of Group Chairman |
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| 187 |
Human Performance 14 - Study Report, Vertical Motion Simulator Activities, Phase I: Backdrive of Accident Flight |
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| 188 |
Human Performance Exhibit No 14-C |
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| 189 |
Correspondence - From A300-600 Pilots |
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| 190 |
Human Performance 14 - Phase II Report |
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| 191 |
Materials Laboratory 15 - Factual Report 02-046 |
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| 192 |
Human Performance 14 - Addendum 1 |
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| 193 |
Materials Laboratory 15 - Factual Report 02-076 |
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| 194 |
Materials Laboratory 15 - Factual Report 02-077 |
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| 195 |
Materials Laboratory 15 - Factual Report 02-078 with Appendix A |
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| 196 |
Materials Laboratory 15 - Factual Report 02-078 Appendix B |
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| 197 |
Materials Laboratory 15 - Factual Report 02-078 Appendix C |
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| 198 |
Materials Laboratory 15 - Factual Report 02-083 |
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| 199 |
Materials Laboratory 15 - Factual Report 02-091 |
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| 200 |
Materials Laboratory 15 - Exhibit 15A Selected Photographs and Drawings of the Damage Areas on the Fin and Rudder |
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| 201 |
Materials Laboratory 15 - Exhibit 15B - Selected Results of the Nondestructive Examination of the Vertical Stabilizer and Rudder |
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| 202 |
Materials Laboratory 15 - Exhibit 15C Selected Photographs of the Fractographic Examination of the Vertical Stabilizer and Rudder |
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| 203 |
Materials Laboratory 15 - Exhibit 15D Airbus Submission - Thermal Analysis by DMA and MDSC |
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| 204 |
Specialist's Report of Investigation - Video Study (Exhibit 17A) |
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| 205 |
Specialist's Report of Investigation - Video Study(Exhibit 17A) - Addendum |
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| 206 |
Specialist's Report of Investigation - Video Study (Exhibit 17A) - Addendum - Available Videos |
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| 207 |
Actual Flight Videos and Reconstruction Animation |
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| 208 |
Investigator-In-Charge Opening Statement at the Public Hearing |
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| 209 |
Transcript - Public Hearing Day 1 (10/29/2002) |
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| 210 |
Transcript - Public Hearing Day 2 (10/30/2002) |
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| 211 |
Transcript - Public Hearing Day 3 (10/31/2002) |
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| 212 |
Transcript - Public Hearing Day 4 (11/01/2002) |
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| 213 |
Systems 9 - Addendum Number 2 to the Systems Group Chairman's Factual Report - Rudder Servo Controls and Linkage - Appendix B |
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| 214 |
Systems 9 - Addendum Number 2 to the Systems Group Chairman's Factual Report - Rudder Servo Controls and Linkage - Appendix C |
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| 215 |
Systems 9 - Addendum Number 2 to the Systems Group Chairman's Factual Report - Rudder Servo Controls and Linkage - Appendix D |
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| 216 |
Systems 9 - Addendum Number 2 to the Systems Group Chairman's Factual Report - Rudder Servo Controls and Linkage - Appendix E |
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| 217 |
Systems 9 - Addendum Number 2 to the Systems Group Chairman's Factual Report - Rudder Servo Controls and Linkage - Appendix G |
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| 218 |
Systems 9 - Addendum Number 2 to the Systems Group Chairman's Factual Report - Rudder Servo Controls and Linkage - Appendix H |
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| 219 |
Systems 9 - Addendum Number 2 to the Systems Group Chairman's Factual Report - Rudder Servo Controls and Linkage - Appendix I |
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| 220 |
Systems 9 - Addendum Number 2 to the Systems Group Chairman's Factual Report - Rudder Servo Controls and Linkage - Appendix J |
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| 221 |
Systems 9 - Addendum Number 2 to the Systems Group Chairman's Factual Report - Rudder Servo Controls and Linkage - Appendix K |
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| 222 |
Systems 9 - Addendum Number 2 to the Systems Group Chairman's Factual Report - Rudder Servo Controls and Linkage |
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| 223 |
Systems 9 - Addendum Number 2 to the Systems Group Chairman's Factual Report - Rudder Servo Controls and Linkage - Appendix F |
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| 224 |
Correspondence Concering American Airlines Flight 903 |
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| 225 |
Flight Data Recorder 10 - Addendum 1 (7 plots total) |
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| 226 |
Flight Data Recorder 10 - Addendum 2 SDAC Bench Test |
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| 227 |
Flight Data Recorder 10 - Addendum 3 Rudder Pedal Ground Tests Study |
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| 228 |
Flight Data Recorder 10 - Addendum 4 FDR Time Latency |
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| 229 |
Flight Data Recorder 10 - Addendum 5, Rudder Pedal Ground Test Feb. 1, 2002 Study |
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| 230 |
Additional Correspondence from American Airlines |
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| 231 |
ULD Report - Attachment One |
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| 232 |
ULD Report - Attachment Two |
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| 233 |
ULD report - Attachment Three |
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| 234 |
ULD Report - Attachment Four |
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| 235 |
ULD Report - Attachment Five |
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| 236 |
ULD Report - Attachment Six |
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| 237 |
ULD Report - Attachment Seven |
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| 238 |
ULD Report - Attachment Eight |
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| 239 |
ULD Report - Attachment Nine |
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| 240 |
ULD Group Chairman - Factual Report |
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| 241 |
Human Performance 14 - Study Report, Airbus A300-600 Ground Test |
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| 242 |
Human Performance 14 - Study Report, Airbus A300-600 Ground Test Attachment I |
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| 243 |
Human Performance 14 - Study Report, Airbus A300-600 Ground Test Attachment II |
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| 244 |
Human Performance 14 - Study Report, Airbus A300-600 Ground Test Attachment III |
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| 245 |
Human Performance 14 - Study Report, Airbus A300-600 Ground Test Attachment IV |
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| 246 |
Human Performance 14 - Study Report, Airbus A300-600 Ground Test Attachment V |
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| 247 |
Cockpit Voice Recorder 12B - Addendum 1 to Specialist's Sound Spectrum Study, Cockpit Voice Recorder |
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| 248 |
Human Performance 14 - Hess Report |
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| 249 |
Human Performance 14 - Speech Study Report |
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| 250 |
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." |
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| 251 |
Systems 9 - ADDENDUM NUMBER 5 TO THE SYSTEMS GROUP CHAIRMAN’S FACTUAL REPORT OF INVESTIGATION– AUTOPILOT SERVOMOTOR EXAMINATION |
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| 252 |
Submission of American Airlines, Inc. - Accident involving American Airlines Flight 587 at Belle Harbor, New York - November 12, 2001 |
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| 253 |
Submission of the Allied Pilots Association regarding the accident of American Airlines Flight 587 at Belle Harbor, New York - November 12,2001 |
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| 254 |
AIRBUS submission for the American Airlines Flight 587 - Belle Harbor, New York - November 12,2001 |
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| 255 |
Systems 9 - ADDENDUM NUMBER 4 TO THE SYSTEMS GROUP CHAIRMAN’S FACTUAL REPORT OF INVESTIGATION - A300-600 GROUND TEST |
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| 256 |
Systems 9 - APPENDIX A TO ADDENDUM NUMBER 4 |
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| 257 |
Systems 9 - APPENDIX B TO ADDENDUM NUMBER 4 |
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Systems 9 - APPENDIX C TO ADDENDUM NUMBER 4 |
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Systems 9 - APPENDIX D TO ADDENDUM NUMBER 4 |
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| 260 |
Systems 9 - APPENDIX E TO ADDENDUM NUMBER 4 |
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| 261 |
Systems 9 - APPENDIX F TO ADDENDUM NUMBER 4 |
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| 262 |
Systems 9 - APPENDIX G TO ADDENDUM NUMBER 4 |
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| 263 |
Systems 9 - APPENDIX H TO ADDENDUM NUMBER 4 |
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| 264 |
Systems 9 - APPENDIX I TO ADDENDUM NUMBER 4 |
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| 265 |
Meteorology and Wake Vortex Influence on American Airlines FL-587 Accident |
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| 266 |
American Airlines Submission Addendum 1 |
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| 267 |
Human Performance 14 - Addendum 3 |
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| 268 |
Miscellaneous - AA903 Merged Timeline of Events |
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| 269 |
Miscellaneous - December 2006 Letter From AAL To IIC |
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| 270 |
Specialist's Report of Investigation - Video Study (Exhibit 17A) - Addendum 2 - Available Videos (DVD AVI Format) |
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