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Operations/Human Performance 2 - Exhibit No. 2A - Group Chairman Factual Report |
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Operations/Human Performance 2 - Exhibit No. 2B - Scheduled and Actual Trip Paring |
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Operations/Human Performance 2 - Exhibit No. 2C - Copies of Air Traffic Control Transcripts: Puerto Vallarta, Mexico |
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Operations/Human Performance 2 - Exhibit No. 2D - Copies of ATC Flight Progress Strip, Puerto Vallarta, Mexico |
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Operations/Human Performance 2 - Exhibit No. 2E - Summary of tape recording between Alaska Airlines flight 261 and SEA Maintenance Control |
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Operations/Human Performance 2 - Exhibit No. 2F - Copies of Flight Crewmember Certificates |
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Operations/Human Performance 2 - Exhibit No. 2G - Flight Plan, Weight and Balance Documents |
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Operations/Human Performance 2 - Exhibit No. 2H - Excerpts from MD-80 Flight Handbook |
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Operations/Human Performance 2 - Exhibit No. 2I - Excerpts from MD-80 Flight Operations Manual |
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Operations/Human Performance 2 - Exhibit No. 2J - Excerpts from MD-80 Quick Reference Handbook |
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Operations/Human Performance 2 - Exhibit No. 2K - FAA briefing papers dated 1/31/00 |
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Operations/Human Performance 2 - Exhibit No. 2L - Excerpts from the Evaluation Report of the National Evaluation of the Seattle FSDO |
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Operations/Human Performance 2 - Exhibit No. 2M - Special Inspection of Alaska Airlines |
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Operations/Human Performance 2 - Exhibit No. 2N - Witness and interview Statements |
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Operations/Human Performance 2 - Exhibit No. 2O - Post-Accident Bulletins |
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Operations/Human Performance 2 - Exhibit No. 2P - Addendum 1 to the Group Chairman's Factual Report |
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Operations/Human Performance 2 - Exhibit No. 2Q - Boeing Airliner Article: "Boeing Introduces a new Grease with Improved Commonality & Performance" January-March 1996 |
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Operations/Human Performance 2 - Exhibit No. 2R - Air Transportation Oversight System Briefing Graphics |
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Operations/Human Performance 2 - Exhibit No. 2S - First Officer's Military Flying Records |
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Operations/Human Performance 2 - Exhibit No. 2T - First Officer's Toxicological Data |
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ATC 3 - Exhibit No. 3A - Group Chairman Factual Report |
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ATC 3 - Exhibit No. 3B - ASA261-Los Angeles Center Communications Transcripts |
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ATC 3 - Exhibit No. 3C - ASA158/ASA261-Puerta Vallarta Approach Communications Transcripts and Controller Statements |
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Witness 4 - Exhibit No. 4A - Factual Report of Group Chairman |
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Witness 4 - Exhibit No. 4B - Statement of Witness A-D, Gottshall and Location Map |
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Witness 4 - Exhibit No. 4C - Statement of Witness B-S, Schoomaker |
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Witness 4 - Exhibit No. 4D - Statement of Witness C-M. Blake and Location Map |
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Witness 4 - Exhibit 4E - Statement of Witness D-J. Layton and Location Map |
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Witness 4 - Exhibit No. 4F - Statement of A. & N. Alfieri |
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Witness 4 - Exhibit 4G - Statement of K. tePas |
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Witness 4 - Exhibit No. 4H - Statement of 7 Additional Persons |
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Witness 4 - Exhibit No. 4I - Statements of Oil Platform and NAS Point Mugu ATC Personnel |
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Survival Factors 6 - Exhibit No. 6A - Group Chairman Factual Report |
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Survival Factors 6 - Appendix A - U.S. Coast Guard Maritime Search and Rescue Areas and Field District Office Locations |
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Survival Factors 6 - Appendix B - Copies of the AFRCC and MSO/Group LA/LB Log Book entries regarding the crash of Alaska Airlines Flight 261 |
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Survival Factors 6 - Appendix C - United States Coast Guard Organizational Chart and the Coast Guard's Incident Command Structure for the Accident. |
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Survival Factors 6 - Appendix D - Copies of FAA Order 7110.65, excerpts from LA World Airports Air/Sea Diaster Preparedness Plan and Coast Guard Search & Rescue Standard Operating Procedures. |
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Structures 7 - Exhibit No. 7A - Group Chairman Factual Report |
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Structures 7 - Exhibit No. 7B - Appendix A - Crash Site Map |
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Structures 7 - Exhibit No. 7C - Appendix B - Search Area |
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Structures 7 - Exhibit No. 7D - Appendix C - Aircraft Dimensions |
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Structures 7 - Exhibit No. 7E - Appendix D - Fuselage Compartments |
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Structures 7 - Exhibit No. 7F - Appendix E - Fuselage Station Diagram |
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Structures 7 - Exhibit No. 7G - Appendix F - Flight Control Surfaces |
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Structures 7 - Exhibit No. 7H - Appendix G - Wing - General and Station Diagram |
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Structures 7 - Exhibit No. 7I - Appendix H - Stabilizers - General |
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Structures 7 - Exhibit No. 7J - Appendix I - Horizontal Stabilizer Stations |
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Structures 7 - Exhibit No. 7K - Appendix J - Vertical Stabilizer to Horizontal Stabilizer Fairing |
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Structures 7 - Exhibit No. 7L - Appendix K - Vertical Stabilizer Stations |
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Structures 7 - Exhibit No. 7M - Appendix L - Landing Gear Figures |
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Structures 7 - Exhibit No. 7N - Appendix M - Glossary of Terms Used in the Station Numbering System |
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Structures 7 - Exhibit No. 7O - Appendix N - Boeing's Rigid Body Model Clearances for the Horizontal Stabilizer Upward Travel |
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Structures 7 - Exhibit No. 7P - Appendix O - Survival Factors Specialist's Report |
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Structures 7 - Exhibit No. 7Q - Appendix P - Photographs |
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Structures 7 - Exhibit No. 7Q - Appendix P - Photographs (29 Photos) |
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Structures 7 - Exhibit No. 7Q - Appendix P - Photo 1. Recovery operation - Horizontal Stabilizer section. The arrow is pointing to the jackscrew (acme screw). |
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Structures 7 - Exhibit No. 7Q - Appendix P - Photo 2. Close up of recovered Jackscrew Assembly. |
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Structures 7 - Exhibit No. 7Q - Appendix P - Photo 3. On shore rinse operation. |
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Structures 7 - Exhibit No. 7Q - Appendix P - Photo 4. Fuselage - Nose section (view looking aft). The center windshield, right windshield, right sliding (clearview) window, and the right upper (eyebrow) flight compartment window structure. |
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Structures 7 - Exhibit No. 7Q - Appendix P - Photo 5. Fuselage - Forward Section (view looking right to left). |
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Structures 7 - Exhibit No. 7Q - Appendix P - Photo 6. Fuselage - Mid-Cargo Section (view looking right to left). |
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Structures 7 - Exhibit No. 7Q - Appendix P - Photo 7. Fuselage - Aft Cargo Section (right side, view looking aft). |
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Structures 7 - Exhibit No. 7Q - Appendix P - Photo 8. Fuselage - Miscellaneous Structure. |
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Structures 7 - Exhibit No. 7Q - Appendix P - Photo 9. Left Wing - Inboard Portion |
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Structures 7 - Exhibit No. 7Q - Appendix P - Photo 10. Left Wing - Outboard Portion |
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Structures 7 - Exhibit No. 7Q - Appendix P - Photo 11. Right wing. - Outboard portion. |
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Structures 7 - Exhibit No. 7Q - Appendix P - Photo 12. Right Wing - Trailing Edge. |
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Structures 7 - Exhibit No. 7Q - Appendix P - Photo 13. Horizontal Stabilizer (view looking aft). The attached portion of the jackscrew assembly is removed. |
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Structures 7 - Exhibit No. 7Q - Appendix P - Photo 14. Horizontal Stabilizer - Close-up of the Center Section. |
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Structures 7 - Exhibit No. 7Q - Appendix P - Photo 15. Horizontal Stabilizer - Jackscrew Assembly. Arrows point to the thin, spiral metallic material that was found on the acme screw. |
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Structures 7 - Exhibit No. 7Q - Appendix P - Photo 16. Horizontal Stabilizer - Right (view looking aft). |
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Structures 7 - Exhibit No. 7Q - Appendix P - Photo 17. Horizontal Stabilizer - Right Trailing Edge (view looking right to left). |
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Structures 7 - Exhibit No. 7Q - Appendix P - Photo 18. Horizontal Stabilizer - Left (view looking down). |
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Structures 7 - Exhibit No. 7Q - Appendix P - Photo 19. Horizontal Stabilizer - Aft Center Section (view looking forward). |
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Structures 7 - Exhibit No. 7Q - Appendix P - Photo 20. Vertical Stabilizer Tip Fairing - Right Side. Arrow 1 points to wehre the mid and aft section of the recovered fairing is mated. Arrow 2 points to where both fairing skins are factured. |
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Structures 7 - Exhibit No. 7Q - Appendix P - Photo 21. Vertical Stabilizer Tip Fairing - Aft Portion (close-up and cropped). Arrows point to the set of parallel marks that match the size of the elevator control sector. |
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Structures 7 - Exhibit No. 7Q - Appendix P - Photo 22. Horizontal Stabilizer Pivot Point. |
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Structures 7 - Exhibit No. 7Q - Appendix P - Photo 23. Vertical Structure that holds the Gimbal. |
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Structures 7 - Exhibit No. 7Q - Appendix P - Photo 24. Rudder - Upper Aft Section right side). Arrow points to a series of paint abrasions. |
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Structures 7 - Exhibit No. 7Q - Appendix P - Photo 25. Vertical Stabilizer Rear Spar Upper Hinge Fitting (view looking down). Arrows point to contact marks. |
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Structures 7 - Exhibit No. 7Q - Appendix P - Photo 26. Landing gear - Nose |
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Structures 7 - Exhibit No. 7Q - Appendix P - Photo 27. Landing Gear - Right Main Tire and Wheel Assembly. |
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Structures 7 - Exhibit No. 7Q - Appendix P - Photo 28. Landing Gear - Right Main Outer Cylinder. |
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Structures 7 - Exhibit No. 7Q - Appendix P - Photo 29. Landing Gear - Left Main. |
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Structures 7 - Exhibit No. 7S - Appendix R - ASA 261 Horizontal Stabilizer Jackscrew Torque Tube Static Load Test |
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Structures 7 - Exhibit No. 7T - Appendix S - Boeing Provided Contact Points for the Upward Rotation of the Horizontal Stabilizer |
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Structures 7 - Exhibit No. 7U - Photo No. 1 from NTSB Investigator Michael Stockhill - View of Jackscrew Assembly after recovery from the Pacific Ocean. |
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Structures 7 - Exhibit No. 7U - Photo No. 2 from NTSB Investigator Michael Stockhill - View of the Jackscrew Assembly immediately after recovery from the Pacific Ocean. |
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Structures 7 - Exhibit No. 7U - Witness Statements and Photographs Concerning Jackscrew Observations During Water Recovery (Parts 1 and 2 w/photos) |
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Structures 7 - Exhibit No. 7V - Statements from Alaska Airlines Personnel Re: Jackscrew Observation |
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Structures 7 - Exhibit No. 7W - ASA 261 Horizontal Stabilizer Jackscrew Torque Tube Static Load Test - Appendix A and Appendix B |
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Structures 7 - Exhibit No. 7X - ASA 261 Horizontal Stabilizer Torque Tube Wear Band Strength Analysis |
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Structures 7 - Exhibit No. 7Y - ASA 261 Structures Group Chairperson - Addendum to Factual |
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Structures 7 - AS261 HS Jackscrew Torque Tube Static Load Test (Appendix C) |
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95 |
Structures 7 - AS261 HS Jackscrew Gimbal Nut Thread Remnant Formation Study |
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96 |
Structures 7 - Study of the Stress and Deformation in Acme Nut Threads |
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97 |
Systems/Powerplants 9 - Exhibit No. 9A - Group Chairman Factual Report |
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Systems 9 - Addendum 1 |
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Systems 9 - Addendum 2 |
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Systems 9 - Addendum 3 |
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Systems 9 - Statistical End Play Data Study |
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Systems/Powerplants 9 - Exhibit No. 9B - Photo 1. Left side view of horizontal stabilizer structure following recovery. Note that the acme screw remained attached (arrow). |
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Systems/Powerplants 9 - Exhibit No. 9B - Photo 2. Head-on view looking aft of acme screw and support assembly, prior to removal from stabilizer. Note that acme screw is bent toward aircraft left. |
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104 |
Systems/Powerplants 9 - Exhibit No. 9B - Photo 3. Left side view of acme screw and support assembly prior to removal from stabilizer. Note that it is bent aft. Also note that primary and alternate motors had separated. |
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105 |
Systems/Powerplants 9 - Exhibit No. 9B - Photo 4. Close-up view of middle-portion of acme screw. Note brass-colored thread remnants coiled around the acme screw. Also note rust deposits and lack of grease in this area. |
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106 |
Systems/Powerplants 9 - Exhibit No. 9B - Photo 5. View of the lower end of the acme screw near the location of the torque tube fracture laid next to the lower stop (left side of photo). The lower stop was recovered separately. |
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107 |
Systems/Powerplants 9 - Exhibit No. 9B - Photo 6. Close-up view of lower stop immediately after it was recovered and brought to shore. Note damage to its upper surface (arrow) and the intact stop contact surface. |
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108 |
Systems/Powerplants 9 - Exhibit No. 9B - Photo 7. View of vertical stabilizer structure that was recovered separately from the horizontal stabilizer structure. Note that acme nut and gimbal supports are attached. |
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109 |
Systems/Powerplants 9 - Exhibit No. 9B - Photo 8. Close-up view acme nut and gimbal supports. Note that acme nut threads are stripped out. Also note globules of shiny red grease. |
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110 |
Systems/Powerplants 9 - Exhibit No. 9B - Photo 9. Portion of the slat drive bull wheel. Note cable mark-up impressions in the grooves. Also note stretched and separated slat drive cables. |
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111 |
Systems/Powerplants 9 - Exhibit No. 9B - Photo 10. Frontal view of cockpit pedestal wreckage. Note the two throttles and the alternate trim switches (two yellow knobs in lower center portion of photo) |
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112 |
Systems/Powerplants 9 - Exhibit No. 9B - Photo 11. Circuit breaker panel. Note the three primary longitudinal trim circuit breakers denoted by arrows. |
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113 |
Systems/Powerplants 9 - Exhibit No. 9B - Photo 12. Circuit breaker panel. Note the G22 and G23 circuit breakers. |
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114 |
Systems/Powerplants 9 - Exhibit No. 9B - Photo 13. Circuit breaker panel, showing breakers D9, D10, and D11. |
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115 |
Systems/Powerplants 9 - Exhibit No. 9B - Photo 14. Anti-float and geared tabs from the right half of the elevator. Note attach fittings. |
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116 |
Systems/Powerplants 9 - Exhibit No. 9B - Photo 15. Close-up view of an attach fittings for anti-float and geared tabs from the right half of the elevator. Note the characteristics of lubrication on attach fittings. |
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117 |
Systems/Powerplants 9 - Exhibit No. 9B - Photo 16. Right elevator hinge. |
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118 |
Systems/Powerplants 9 - Exhibit No. 9B - Photo 17. Close-up view of right elevator hinge shown in Photo No. 16. Note the characteristics of lubrication on attach fittings. |
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119 |
Systems/Powerplants 9 - Exhibit No. 9B - Photo 18. Another elevator/aileron attach fitting that is more closely surrounded by structure. Note the characteristics of lubrication fittings. |
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120 |
Systems/Powerplants 9 - Exhibit No. 9B - Photo 19. One of the trim relays found in the wreckage. Note lack of any thermal damage on the relay body and the relay contacts. |
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121 |
Systems/Powerplants 9 - Exhibit No. 9B - Photo 20. Primary trim motor from accident airplane, after outer housing had been removed by the System Group. |
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122 |
Systems/Powerplants 9 - Exhibit No. 9B - Photo 21. View of the front of the right engine. |
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123 |
Systems/Powerplants 9 - Exhibit No. 9B - Photo 22. View of the wreckage from the left engine. |
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124 |
Systems/Powerplants 9 - Exhibit No. 9B - Photo 23. View of the horizontal stabilizer restraining fixture tool used during the endplay demonstration in Tulsa. |
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125 |
Systems/Powerplants 9 - Exhibit No. 9B - Photo 24. View of the endplay check set-up in Tulsa. Note dial indicator (above) and the C-clamp on the lower retaining nut. |
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126 |
Systems/Powerplants 9 - Exhibit No. 9B - Photo 25. View of the MD-80 cockpit during ground testing in Tulsa. This photo was taken after the stabilizer had been moved to the full nose down trim position (electric stop). Note trim indicator position. |
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127 |
Systems/Powerplants 9 - Exhibit No. 9B - Photo 26. View of the stabilizer position sensor after the position cable loop had been manually moved beyond its normal position towards aircraft nose down during the Tulsa tests. |
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128 |
Systems/Powerplants 9 - Exhibit No. 9B - Photo 27. View of the trim system relays and the mechanical linkages that connect to them (arrows). |
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129 |
Systems/Powerplants 9 - Exhibit No. 9B - Photo 28. View of the torque-ing of an Alaska Airlines restraining fixture during the endplay check demonstration in Oakland. |
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130 |
Systems/Powerplants 9 - Exhibit No. 9B - Photo 29. Set-up of the dial indicator during the endplay demonstrations at Oakland. |
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131 |
Systems/Powerplants 9 - Exhibit No. 9B - Photo 30. Interior view of the vertical stabilizer of an Alaska Airlines MD-80 used during the Oakland visit. Note size of the access panel normally used to lubricate acme screw and nut assembly. |
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132 |
Systems/Powerplants 9 - Exhibit No. 9B - Photo 31. Exterior view (left side of airplane) of the vertical stabilizer of an Alaska Airlines MD-80 used during the Oakland visit. Note size of the access panel used to lubiricate acme screw and nut assembly. |
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133 |
Systems/Powerplants 9 - Exhibit No. 9B - Photo 32. View of the acme screw and nut assembly after removal (and prior to cleaning) from the Oakland airplane. Note endplay bench check set-up as performed at Trig Aerospace. |
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134 |
Systems/Powerplants 9 - Exhibit No. 9B - Photo 33. View of the acme screw nd nut assembly after removal (and prior to cleaning) from the Oakland airplane. Note endplay test fixure check set-up as performed at Trig Aerospace at direction of System Group. |
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135 |
Systems/Powerplants 9 - Exhibit No. 9B - Photo 34. Acme screw & nut assembly after removal from Oakland airplane. Note endplay bench check set-up as at Trig Aerospace, after the acme nut was removed, the assembly steam-cleaned & re-assembled for the check |
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136 |
Systems/Powerplants 9 - Exhibit No. 9C - Drawings and Diagrams of Pertinent Flight Control System Components |
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137 |
Systems/Powerplants 9 - Exhibit No. 9D - Horizontal Stabilizer Actuator Travel Data |
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138 |
Systems/Powerplants 9 - Exhibit No. 9E - Excerpts of the DC-9 Type Certificate Data Sheet |
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139 |
Systems/Powerplants 9 - Exhibit No. 9F - Civil Air Regulations Part 4b |
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140 |
Systems/Powerplants 9 - Exhibit No. 9G - Documentation of the Lubrication found on Elevator and Horizontal Stabilizer Fittings of the Accident Airplane |
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141 |
Systems/Powerplants 9 - Exhibit No. 9H - Flap/Slat Sequence Ground Test Plan & Results |
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Systems/Powerplants 9 - Exhibit No. 9J - FAA Airworthiness Directive 2000-03-51 (DC-9/MD-80/90, B-717 Horizontal Stabilizer Actuator Assembly Inspection), issued February 11, 2000 |
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Systems/Powerplants 9 - Exhibit No. 9K - FAA Airworthiness Directive 2000-15-15 (Revised DC-9/MD-80/90, B-717 Horizontal Stabilizer Actuator Assembly Inspection), effective Aug. 23, 2000 |
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Systems/Powerplants 9 - Exhibit No. 9L - Boeing DC-9 Alert Service Bulletin DC9-27A362, dated Feb. 11, 2000 |
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Systems/Powerplants 9 - Exhibit No. 9M - Temporary Revision to MD-80 End Play Check Procedure, dated April 13, 2000 |
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Systems/Powerplants 9 - Exhibit No. 9N - Boeing Field Service Messages Addressing DC-9, MD-80/90, B717 Horizontal Stabilizer Issues (Post-Accident) |
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Systems/Powerplants 9 - Exhibit No. 9O - Douglas Design Memorandum Addressing Jackscrew Assembly Excessive Wear Rate, dated Feb. 24, 1967 |
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Systems/Powerplants 9 - Exhibit No. 9P - Douglas All Operator Letters 9-48 & 9-48A Addressing DC-9 End Play Check Methods, dated 1966-67 |
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Systems/Powerplants 9 - Exhibit No. 9Q - Douglas All Operator Letter 9-1526 Addressing DC-9/MD-80 Horizontal Stabilizer Actuator Assembly Lubrication Requirements, dated May 29, 1984 |
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Systems/Powerplants 9 - Exhibit No. 9R - Internal Douglas & Airline Correspondence Supporting All Operator Letter 9-1526 Addressing DC-9/MD 80 Horizontal Stabilizer Actuator Assembly Lubrication Requirements, dated May 29, 19 |
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Systems/Powerplants 9 - Exhibit No. 9S - Douglas All Operator Letters 9-2120 & 2120A Addressing DC-9 / MD-80 Horizontal Stabilizer Jackscrew Wear Rates, dated Dec. 6,1990 |
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Systems/Powerplants 9 - Exhibit No. 9T - McDonnell Douglas Service Bulletin No. MD11-27-067 Addressing MD-11 Horizontal Stabilizer Actuator Assemblies, dated Feb. 24, 1998 |
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Systems/Powerplants 9 - Exhibit No. 9U - Excerpts of McDonnell Douglas Alert Service Bulletin No. MD11-27A067 Addressing MD-11 Horizontal Stabilizer Actuator Assemblies, dated Nov. 19, 1999 |
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Systems/Powerplants 9 - Exhibit No. 9V - FAA Airworthiness Directive 98-16-01 (MD-11 Horizontal Stabilizer Actuator Assembly Inspection), dated Aug. 14, 1998 |
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Systems/Powerplants 9 - Exhibit No. 9W - Excerpts of CAR 4b, Amendment 16, Applicable to DC-9 |
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Systems/Powerplants 9 - Exhibit No. 9X - Alaska Airlines Engineering Order No. EO 2740-01036; MD-80 Stabilizer Jackscrew Inspection, dated Feb. 9, 2000 |
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Systems/Powerplants 9 - Exhibit No. 9Y - Temporary Revision (27-456) to End-Play Check Procedure; November 20, 2000 |
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Systems/Powerplants 9 - Exhibit No. 9Z - Excerpts of FAA Advisory Circular 121-1AA; "Standard Operations Specifications - Aircraft Maintenance Handbook", dated June 26, 1973 (April 1980 Revision) |
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Systems 9 - NASA Trip Report |
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Systems 9 - NOOK Industry Trip Report |
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Systems Photo - Jackscrew |
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Systems Photo - Orig. Screw Photo |
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Systems Photo - Stab Photo1 |
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Systems Photo - Stab Photo2 |
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Systems Photo - Stab Photo3 |
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Systems Photo - Aft Bulk Door |
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Systems Photo - HS Piece |
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Systems Photo - HS Structure |
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Systems Photo - HS Hinges |
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Systems Photo - HS Hinges2 |
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Systems Photo - Slinky Closeup |
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Systems Photo - Gearbox Closeup |
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Systems Photo - Upper Stop |
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Systems Photo - Upper Stop Closeup |
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Systems Photo - Upper Stop Fracture1 |
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Systems Photo - Upper Stop Fracture2 |
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Systems Photo - Upper Stop Fracture3 |
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Flight Data Recorder 10 - Exhibit No. 10A - Group Chairman Factual Report |
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Flight Data Recorder 10 - Exhibit No. 10B - Digital Flight Data Recorder Plots |
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Flight Data Recorder 10 - Exhibit No. 10C - Digital Flight Data Recorder Tabular Data |
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Maintenance Records 11 - Exhibit No. 11A - Group Chairman Factual Report |
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Maintenance Records 11 - Exhibit No. 11B - Operations Specifications Management Personnel |
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Maintenance Records 11 - Exhibit No. 11C - Mechanical Reliability Reports |
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Maintenance Records 11 - Exhibit No. 11D - MD-80 On Aircraft Maintenance Planning (OAMP):MSG-2 |
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Maintenance Records 11 - Exhibit No. 11E - MD-80 On Aircraft Maintenance Planning (OAMP):MSG-3 |
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Maintenance Records 11 - Exhibit No. 11F - Boeing Message Concerning Tooling |
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Maintenance Records 11 - Exhibit No. 11G - ME-01 Technical Change Request |
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Maintenance Records 11 - Exhibit No. 11H - Boeing Message Concerning Lubrication Change |
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Maintenance Records 11 - Exhibit No. 11I - Monthly Task Card Changes Sent to FAA in December 1997 |
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Maintenance Records 11 - Exhibit No. 11J - Boeing Message Concerning Acceptability of Grease |
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Maintenance Records 11 - Exhibit No. 11K - Boeing Message Concerning Aeroshell Grease 33 Lubrication |
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Maintenance Records 11 - Exhibit No. 11L - Acme Screw and Nut Endplay Check |
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Maintenance Records 11 - Exhibit No. 11M - MIG-4 Non-Routine Work Card |
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Maintenance Records 11 - Exhibit No. 11N - Elevator/Stabilizer Lubrication Task Card |
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Maintenance Records 11 - Exhibit No. 11O - Alaska Airlines Action Plan |
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Maintenance Records 11 - Exhibit No. 11P - Safety Assessment for Alaska Airlines issued June 19, 2000 |
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Maintenance Records 11 - Exhibit No. 11Q - Telex Message Between Alaska Airlines and Boeing Regarding Elevator Events and Grease Compatibility; Feb. 2, 2000 |
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Maintenance Records 11 - Exhibit No. 11R - Boeing Airliner Magazine Article Re: Aeroshell 33 Grease |
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Maintenance Records 11 - Exhibit No. 11S - Letter and Statements Regarding Mr. Falla |
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Maintenance Records 11 - Exhibit No. 11T - DoD Survey of Alaska Airlines of 1998 |
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Maintenance Records 11 - Exhibit No. 11U - CSET Evaluation Memorandums re: September 18-22, 2000 Inspection |
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Maintenance Records 11 - Exhibit No. 11V - Alaska Airlines End Play Check Presentation Slides |
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Maintenance Records 11 - Exhibit No. 11W - Excerpts of Boeing Airline Maintenance Inspection Interval Listing; January 2000 |
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Cockpit Voice Recorder 12 - Exhibit No. 12A - Group Chairman Factual Report |
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Cockpit Voice Recorder 12 - Exhibit No. 12B - Timing and Correlation Study Cockpit Voice Recorder |
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Cockpit Voice Recorder 12 - Exhibit No. 12C - Group Chairman's Report of Investigation Sound Spectrum Study |
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Aircraft Performance 13 - Exhibit No. 13A - Aircraft Performance Study |
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Aircraft Performance 13 - Exhibit No. 13B - Aircraft Performance Study - Radar Data |
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Aircraft Performance 13 - Exhibit No. 13C - Aircraft Performance Study - Data Plots |
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Aircraft Performance 13 - Exhibit No. 13D - Supplement 1 to Group Chairman Performance Study |
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Aircraft Performance 13 - Exhibit No. 13E - Supplement 2 to Group Chairman Performance Study |
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Materials Laboratory 15 - Factual Report of Group Chairman - Report 00-145 |
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Materials Laboratory 15 - Factual Report 00-145 Errata Sheet |
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Materials Laboratory 15 - Factual Report 00-045 |
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Materials Laboratory 15 - Factual Report 00-068 |
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Materials Laboratory 15 - Factual Report 00-074 |
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Materials Laboratory 15 - Factual Report 00-146 |
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Materials Laboratory 15 - Errata/Addendum Report - Report No. 00-148 - November 9, 2000 |
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Materials Laboratory 15 - Factual Report 01-082 HWI |
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Materials Laboratory 15 - Factual Report 01-120 Fractography |
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Materials Laboratory 15 - Factual Report 01-118 Restraining Tools |
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Materials Laboratory 15 - Factual Report 01-150 Corrosion Test Specimens |
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Grease Reports 17 - Exhibit No. 17A - Results of Testing of Grease Samples Interim Report |
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Grease Reports 17 - Exhibit No. 17A - Appendix A - Materials Engineering Analysis Report - Submitted by Materials Engineering Laboratory NADEP - Cherry Point, Code 4.3.4 |
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Grease Reports 17 - Exhibit No. 17A - Appendix B - Materials Engineering Investigation Report - Submitted by Materials Engineering Laboratory NADEP - Jacksonville, Code 4.3.4 |
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Grease Reports 17 - Exhibit No. 17A - Appendix C - Analytical Laboratory Report - Submitted by Analytical Laboratory NAWCAD - Patuxent River, Code 4.3.4 |
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Grease Reports 17 - Exhibit No. 17B - Report of Corrosion Testing of Greases |
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Grease Reports 17 - Exhibit No. 17C - Visual Aid (Cover Sheet) |
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Grease Reports 17 - Exhibit No. 17C - Visual Aid (Greases used to lubricate jackscrew) |
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Grease Reports 17 - Exhibit No. 17D - Boeing Service Letter dated August 12, 1993 |
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Grease Reports 17 - Exhibit No. 17E - Boeing Service Letter dated December 21, 1995 |
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Grease Reports 17 - Exhibit No. 17F - Boeing Service Letter dated June 30, 1997 |
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Grease Reports 17 - Exhibit No. 17G - Excerpts from BCAG Twin Jet Technical Focus Report |
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Grease Reports 17 - Exhibit No. 17H - Excerpts from BCAG Maintenance Manual |
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Grease Reports 17 - Exhibit No. 17I - Exposure Tests of Aluminum Bronze to Lubricating Greases and Fluid Contaminants |
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Grease Reports 17 - Exhibit No. 17I - Appendix A - Photographs of exposed test coupons |
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Grease Reports 17 - Exhibit No. 17I - Appendix B - Photographs of grease mixtures following the tests. |
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Grease Reports 17 - Exhibit No. 17J - Examination of Grease Samples Taken from Jackscrew Assemblies of In-service Aircraft |
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Table of Samples from Examination of Grease Samples Taken from Jackscrew Assemblies of In-service Aircraft |
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Appendix A-Photographs of Extraction Samples; Examination of Grease Samples Taken from Jackscrew Assemblies of In-service Aircraft |
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Grease Reports 17 - Exhibit No. 17K - Surface Chemistry Analysis of Discolorations on Aluminum Bronze Specimens |
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Grease Reports 17 - Exhibit No. 17L - Investigation of the Wear Rate of Grease-lubricated C95500 Bronze (Executive Report) |
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Grease Reports 17 - Investigation of the Wear Rate of Grease-Lubricated C95500 Aluminum Bronze (Full Report) |
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Grease Report 17 - Microstructural Analysis Laboratory Report MA-1044 NTSB Grease-Particulate Analysis |
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Grease Report 17 - Materials Engineering Analysis Report - Naval Aviation Depot-Cherry Point, North Carolina |
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Consultant's Review of Chemical Analyses of Residues From Aircraft Jackscrews in Support of Alaska Air Flight 261 ACCIDENT INVESTIGATION |
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NAVAIR-Aerospace Materials Division Report: Grease Evaluation by Fourier Transform Infrared Spectrometry |
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NAVAIR Aerospace Division: Materials Engineering Investigation-NTSB Grease Evaluation |
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Interview Transcript (August 7) |
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Interview Transcript (August 8) |
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Interview Transcript (August 9) |
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Interview Transcript (August 10) |
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Interview Transcript (August 15) |
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Interview Transcript - Federal Labor Relations Authority |
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Interview Transcript of Azbell |
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Interview Transcript of Bautista |
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Interview Transcript of Afman |
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Interview Transcript of Siotkas |
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Public Hearing Testimony Transcript Review - Alaska Airlines MD-83 N963AS |
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Transcript - Public Hearing Day 1 (12/13/2000) |
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Transcript - Public Hearing Day 2 (12/14/2000) |
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Transcript - Public Hearing Day 3 (12/15/2000) |
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Transcript - Public Hearing Day 4 (12/16/2000) |
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ALPA Submission Correspondence dated August 23, 2002 |
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ALPA Submission |
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Boeing Submission |
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Aircraft Mechanics Fraternal Association Submission |
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Alaska Airlines Submission |
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Alaska Airlines Submission - Attachment 1 - Deposition of Michael Minnette |
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Alaska Airlines Submission - Attachment 2 - |
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Alaska Airlines Submission - Attachment 3 - Falex Report |
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Transcript-Board Meeting 12/10 |
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VHS Animation Tape |
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