# |
Title |
Pgs |
Photo |
Type |
| 1 |
Operations/Human Performance 2 - Exhibit No. 2A - Group Chairman Factual Report |
85 |
0 |
Adobe PDF file |
| 2 |
Operations/Human Performance 2 - Exhibit No. 2B - Scheduled and Actual Trip Paring |
3 |
0 |
Adobe PDF file |
| 3 |
Operations/Human Performance 2 - Exhibit No. 2C - Copies of Air Traffic Control Transcripts: Puerto Vallarta, Mexico |
13 |
0 |
Adobe PDF file |
| 4 |
Operations/Human Performance 2 - Exhibit No. 2D - Copies of ATC Flight Progress Strip, Puerto Vallarta, Mexico |
2 |
0 |
Adobe PDF file |
| 5 |
Operations/Human Performance 2 - Exhibit No. 2E - Summary of tape recording between Alaska Airlines flight 261 and SEA Maintenance Control |
3 |
0 |
Adobe PDF file |
| 6 |
Operations/Human Performance 2 - Exhibit No. 2F - Copies of Flight Crewmember Certificates |
5 |
0 |
Adobe PDF file |
| 7 |
Operations/Human Performance 2 - Exhibit No. 2G - Flight Plan, Weight and Balance Documents |
14 |
0 |
Adobe PDF file |
| 8 |
Operations/Human Performance 2 - Exhibit No. 2H - Excerpts from MD-80 Flight Handbook |
13 |
0 |
Adobe PDF file |
| 9 |
Operations/Human Performance 2 - Exhibit No. 2I - Excerpts from MD-80 Flight Operations Manual |
3 |
0 |
Adobe PDF file |
| 10 |
Operations/Human Performance 2 - Exhibit No. 2J - Excerpts from MD-80 Quick Reference Handbook |
4 |
0 |
Adobe PDF file |
| 11 |
Operations/Human Performance 2 - Exhibit No. 2K - FAA briefing papers dated 1/31/00 |
7 |
0 |
Adobe PDF file |
| 12 |
Operations/Human Performance 2 - Exhibit No. 2L - Excerpts from the Evaluation Report of the National Evaluation of the Seattle FSDO |
7 |
0 |
Adobe PDF file |
| 13 |
Operations/Human Performance 2 - Exhibit No. 2M - Special Inspection of Alaska Airlines |
31 |
0 |
Adobe PDF file |
| 14 |
Operations/Human Performance 2 - Exhibit No. 2N - Witness and interview Statements |
16 |
0 |
Adobe PDF file |
| 15 |
Operations/Human Performance 2 - Exhibit No. 2O - Post-Accident Bulletins |
7 |
0 |
Adobe PDF file |
| 16 |
Operations/Human Performance 2 - Exhibit No. 2P - Addendum 1 to the Group Chairman's Factual Report |
4 |
0 |
Adobe PDF file |
| 17 |
Operations/Human Performance 2 - Exhibit No. 2Q - Boeing Airliner Article: "Boeing Introduces a new Grease with Improved Commonality & Performance" January-March 1996 |
49 |
0 |
Adobe PDF file |
| 18 |
Operations/Human Performance 2 - Exhibit No. 2R - Air Transportation Oversight System Briefing Graphics |
4 |
0 |
Adobe PDF file |
| 19 |
Operations/Human Performance 2 - Exhibit No. 2S - First Officer's Military Flying Records |
4 |
0 |
Adobe PDF file |
| 20 |
Operations/Human Performance 2 - Exhibit No. 2T - First Officer's Toxicological Data |
2 |
0 |
Adobe PDF file |
| 21 |
ATC 3 - Exhibit No. 3A - Group Chairman Factual Report |
13 |
0 |
Adobe PDF file |
| 22 |
ATC 3 - Exhibit No. 3B - ASA261-Los Angeles Center Communications Transcripts |
47 |
0 |
Adobe PDF file |
| 23 |
ATC 3 - Exhibit No. 3C - ASA158/ASA261-Puerta Vallarta Approach Communications Transcripts and Controller Statements |
12 |
0 |
Adobe PDF file |
| 24 |
Witness 4 - Exhibit No. 4A - Factual Report of Group Chairman |
6 |
0 |
Adobe PDF file |
| 25 |
Witness 4 - Exhibit No. 4B - Statement of Witness A-D, Gottshall and Location Map |
6 |
0 |
Adobe PDF file |
| 26 |
Witness 4 - Exhibit No. 4C - Statement of Witness B-S, Schoomaker |
3 |
0 |
Adobe PDF file |
| 27 |
Witness 4 - Exhibit No. 4D - Statement of Witness C-M. Blake and Location Map |
4 |
0 |
Adobe PDF file |
| 28 |
Witness 4 - Exhibit 4E - Statement of Witness D-J. Layton and Location Map |
6 |
0 |
Adobe PDF file |
| 29 |
Witness 4 - Exhibit No. 4F - Statement of A. & N. Alfieri |
2 |
0 |
Adobe PDF file |
| 30 |
Witness 4 - Exhibit 4G - Statement of K. tePas |
5 |
0 |
Adobe PDF file |
| 31 |
Witness 4 - Exhibit No. 4H - Statement of 7 Additional Persons |
2 |
0 |
Adobe PDF file |
| 32 |
Witness 4 - Exhibit No. 4I - Statements of Oil Platform and NAS Point Mugu ATC Personnel |
2 |
0 |
Adobe PDF file |
| 33 |
Survival Factors 6 - Exhibit No. 6A - Group Chairman Factual Report |
5 |
0 |
Adobe PDF file |
| 34 |
Survival Factors 6 - Appendix A - U.S. Coast Guard Maritime Search and Rescue Areas and Field District Office Locations |
3 |
0 |
Adobe PDF file |
| 35 |
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 |
16 |
0 |
Adobe PDF file |
| 36 |
Survival Factors 6 - Appendix C - United States Coast Guard Organizational Chart and the Coast Guard's Incident Command Structure for the Accident. |
4 |
0 |
Adobe PDF file |
| 37 |
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. |
16 |
0 |
Adobe PDF file |
| 38 |
Structures 7 - Exhibit No. 7A - Group Chairman Factual Report |
55 |
0 |
Adobe PDF file |
| 39 |
Structures 7 - Exhibit No. 7B - Appendix A - Crash Site Map |
2 |
0 |
Adobe PDF file |
| 40 |
Structures 7 - Exhibit No. 7C - Appendix B - Search Area |
2 |
0 |
Adobe PDF file |
| 41 |
Structures 7 - Exhibit No. 7D - Appendix C - Aircraft Dimensions |
3 |
0 |
Adobe PDF file |
| 42 |
Structures 7 - Exhibit No. 7E - Appendix D - Fuselage Compartments |
2 |
0 |
Adobe PDF file |
| 43 |
Structures 7 - Exhibit No. 7F - Appendix E - Fuselage Station Diagram |
2 |
0 |
Adobe PDF file |
| 44 |
Structures 7 - Exhibit No. 7G - Appendix F - Flight Control Surfaces |
2 |
0 |
Adobe PDF file |
| 45 |
Structures 7 - Exhibit No. 7H - Appendix G - Wing - General and Station Diagram |
3 |
0 |
Adobe PDF file |
| 46 |
Structures 7 - Exhibit No. 7I - Appendix H - Stabilizers - General |
2 |
0 |
Adobe PDF file |
| 47 |
Structures 7 - Exhibit No. 7J - Appendix I - Horizontal Stabilizer Stations |
2 |
0 |
Adobe PDF file |
| 48 |
Structures 7 - Exhibit No. 7K - Appendix J - Vertical Stabilizer to Horizontal Stabilizer Fairing |
2 |
0 |
Adobe PDF file |
| 49 |
Structures 7 - Exhibit No. 7L - Appendix K - Vertical Stabilizer Stations |
2 |
0 |
Adobe PDF file |
| 50 |
Structures 7 - Exhibit No. 7M - Appendix L - Landing Gear Figures |
3 |
0 |
Adobe PDF file |
| 51 |
Structures 7 - Exhibit No. 7N - Appendix M - Glossary of Terms Used in the Station Numbering System |
4 |
0 |
Adobe PDF file |
| 52 |
Structures 7 - Exhibit No. 7O - Appendix N - Boeing's Rigid Body Model Clearances for the Horizontal Stabilizer Upward Travel |
4 |
0 |
Adobe PDF file |
| 53 |
Structures 7 - Exhibit No. 7P - Appendix O - Survival Factors Specialist's Report |
5 |
0 |
Adobe PDF file |
| 54 |
Structures 7 - Exhibit No. 7Q - Appendix P - Photographs |
16 |
0 |
Adobe PDF file |
| 55 |
Structures 7 - Exhibit No. 7Q - Appendix P - Photographs (29 Photos) |
1 |
0 |
Adobe PDF file |
| 56 |
Structures 7 - Exhibit No. 7Q - Appendix P - Photo 1. Recovery operation - Horizontal Stabilizer section. The arrow is pointing to the jackscrew (acme screw). |
1 |
0 |
Adobe PDF file |
| 57 |
Structures 7 - Exhibit No. 7Q - Appendix P - Photo 2. Close up of recovered Jackscrew Assembly. |
1 |
0 |
Adobe PDF file |
| 58 |
Structures 7 - Exhibit No. 7Q - Appendix P - Photo 3. On shore rinse operation. |
1 |
0 |
Adobe PDF file |
| 59 |
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. |
1 |
0 |
Adobe PDF file |
| 60 |
Structures 7 - Exhibit No. 7Q - Appendix P - Photo 5. Fuselage - Forward Section (view looking right to left). |
1 |
0 |
Adobe PDF file |
| 61 |
Structures 7 - Exhibit No. 7Q - Appendix P - Photo 6. Fuselage - Mid-Cargo Section (view looking right to left). |
1 |
0 |
Adobe PDF file |
| 62 |
Structures 7 - Exhibit No. 7Q - Appendix P - Photo 7. Fuselage - Aft Cargo Section (right side, view looking aft). |
1 |
0 |
Adobe PDF file |
| 63 |
Structures 7 - Exhibit No. 7Q - Appendix P - Photo 8. Fuselage - Miscellaneous Structure. |
1 |
0 |
Adobe PDF file |
| 64 |
Structures 7 - Exhibit No. 7Q - Appendix P - Photo 9. Left Wing - Inboard Portion |
1 |
0 |
Adobe PDF file |
| 65 |
Structures 7 - Exhibit No. 7Q - Appendix P - Photo 10. Left Wing - Outboard Portion |
1 |
0 |
Adobe PDF file |
| 66 |
Structures 7 - Exhibit No. 7Q - Appendix P - Photo 11. Right wing. - Outboard portion. |
1 |
0 |
Adobe PDF file |
| 67 |
Structures 7 - Exhibit No. 7Q - Appendix P - Photo 12. Right Wing - Trailing Edge. |
1 |
0 |
Adobe PDF file |
| 68 |
Structures 7 - Exhibit No. 7Q - Appendix P - Photo 13. Horizontal Stabilizer (view looking aft). The attached portion of the jackscrew assembly is removed. |
1 |
0 |
Adobe PDF file |
| 69 |
Structures 7 - Exhibit No. 7Q - Appendix P - Photo 14. Horizontal Stabilizer - Close-up of the Center Section. |
1 |
0 |
Adobe PDF file |
| 70 |
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. |
1 |
0 |
Adobe PDF file |
| 71 |
Structures 7 - Exhibit No. 7Q - Appendix P - Photo 16. Horizontal Stabilizer - Right (view looking aft). |
1 |
0 |
Adobe PDF file |
| 72 |
Structures 7 - Exhibit No. 7Q - Appendix P - Photo 17. Horizontal Stabilizer - Right Trailing Edge (view looking right to left). |
1 |
0 |
Adobe PDF file |
| 73 |
Structures 7 - Exhibit No. 7Q - Appendix P - Photo 18. Horizontal Stabilizer - Left (view looking down). |
1 |
0 |
Adobe PDF file |
| 74 |
Structures 7 - Exhibit No. 7Q - Appendix P - Photo 19. Horizontal Stabilizer - Aft Center Section (view looking forward). |
1 |
0 |
Adobe PDF file |
| 75 |
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. |
1 |
0 |
Adobe PDF file |
| 76 |
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. |
1 |
0 |
Adobe PDF file |
| 77 |
Structures 7 - Exhibit No. 7Q - Appendix P - Photo 22. Horizontal Stabilizer Pivot Point. |
1 |
0 |
Adobe PDF file |
| 78 |
Structures 7 - Exhibit No. 7Q - Appendix P - Photo 23. Vertical Structure that holds the Gimbal. |
1 |
0 |
Adobe PDF file |
| 79 |
Structures 7 - Exhibit No. 7Q - Appendix P - Photo 24. Rudder - Upper Aft Section right side). Arrow points to a series of paint abrasions. |
1 |
0 |
Adobe PDF file |
| 80 |
Structures 7 - Exhibit No. 7Q - Appendix P - Photo 25. Vertical Stabilizer Rear Spar Upper Hinge Fitting (view looking down). Arrows point to contact marks. |
1 |
0 |
Adobe PDF file |
| 81 |
Structures 7 - Exhibit No. 7Q - Appendix P - Photo 26. Landing gear - Nose |
1 |
0 |
Adobe PDF file |
| 82 |
Structures 7 - Exhibit No. 7Q - Appendix P - Photo 27. Landing Gear - Right Main Tire and Wheel Assembly. |
1 |
0 |
Adobe PDF file |
| 83 |
Structures 7 - Exhibit No. 7Q - Appendix P - Photo 28. Landing Gear - Right Main Outer Cylinder. |
1 |
0 |
Adobe PDF file |
| 84 |
Structures 7 - Exhibit No. 7Q - Appendix P - Photo 29. Landing Gear - Left Main. |
1 |
0 |
Adobe PDF file |
| 85 |
Structures 7 - Exhibit No. 7S - Appendix R - ASA 261 Horizontal Stabilizer Jackscrew Torque Tube Static Load Test |
72 |
0 |
Adobe PDF file |
| 86 |
Structures 7 - Exhibit No. 7T - Appendix S - Boeing Provided Contact Points for the Upward Rotation of the Horizontal Stabilizer |
31 |
0 |
Adobe PDF file |
| 87 |
Structures 7 - Exhibit No. 7U - Photo No. 1 from NTSB Investigator Michael Stockhill - View of Jackscrew Assembly after recovery from the Pacific Ocean. |
1 |
0 |
Adobe PDF file |
| 88 |
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. |
1 |
0 |
Adobe PDF file |
| 89 |
Structures 7 - Exhibit No. 7U - Witness Statements and Photographs Concerning Jackscrew Observations During Water Recovery (Parts 1 and 2 w/photos) |
9 |
0 |
Adobe PDF file |
| 90 |
Structures 7 - Exhibit No. 7V - Statements from Alaska Airlines Personnel Re: Jackscrew Observation |
4 |
0 |
Adobe PDF file |
| 91 |
Structures 7 - Exhibit No. 7W - ASA 261 Horizontal Stabilizer Jackscrew Torque Tube Static Load Test - Appendix A and Appendix B |
84 |
0 |
Adobe PDF file |
| 92 |
Structures 7 - Exhibit No. 7X - ASA 261 Horizontal Stabilizer Torque Tube Wear Band Strength Analysis |
79 |
0 |
Adobe PDF file |
| 93 |
Structures 7 - Exhibit No. 7Y - ASA 261 Structures Group Chairperson - Addendum to Factual |
5 |
0 |
Adobe PDF file |
| 94 |
Structures 7 - AS261 HS Jackscrew Torque Tube Static Load Test (Appendix C) |
30 |
0 |
Adobe PDF file |
| 95 |
Structures 7 - AS261 HS Jackscrew Gimbal Nut Thread Remnant Formation Study |
38 |
0 |
Adobe PDF file |
| 96 |
Structures 7 - Study of the Stress and Deformation in Acme Nut Threads |
21 |
0 |
Adobe PDF file |
| 97 |
Systems/Powerplants 9 - Exhibit No. 9A - Group Chairman Factual Report |
59 |
0 |
Adobe PDF file |
| 98 |
Systems 9 - Addendum 1 |
197 |
0 |
Adobe PDF file |
| 99 |
Systems 9 - Addendum 2 |
7 |
0 |
Adobe PDF file |
| 100 |
Systems 9 - Addendum 3 |
8 |
0 |
Adobe PDF file |
| 101 |
Systems 9 - Statistical End Play Data Study |
29 |
0 |
Adobe PDF file |
| 102 |
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). |
1 |
0 |
Adobe PDF file |
| 103 |
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. |
1 |
0 |
Adobe PDF file |
| 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. |
1 |
0 |
Adobe PDF file |
| 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. |
1 |
0 |
Adobe PDF file |
| 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. |
1 |
0 |
Adobe PDF file |
| 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. |
1 |
0 |
Adobe PDF file |
| 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. |
1 |
0 |
Adobe PDF file |
| 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. |
1 |
0 |
Adobe PDF file |
| 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. |
1 |
0 |
Adobe PDF file |
| 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) |
1 |
0 |
Adobe PDF file |
| 112 |
Systems/Powerplants 9 - Exhibit No. 9B - Photo 11. Circuit breaker panel. Note the three primary longitudinal trim circuit breakers denoted by arrows. |
1 |
0 |
Adobe PDF file |
| 113 |
Systems/Powerplants 9 - Exhibit No. 9B - Photo 12. Circuit breaker panel. Note the G22 and G23 circuit breakers. |
1 |
0 |
Adobe PDF file |
| 114 |
Systems/Powerplants 9 - Exhibit No. 9B - Photo 13. Circuit breaker panel, showing breakers D9, D10, and D11. |
1 |
0 |
Adobe PDF file |
| 115 |
Systems/Powerplants 9 - Exhibit No. 9B - Photo 14. Anti-float and geared tabs from the right half of the elevator. Note attach fittings. |
1 |
0 |
Adobe PDF file |
| 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. |
1 |
0 |
Adobe PDF file |
| 117 |
Systems/Powerplants 9 - Exhibit No. 9B - Photo 16. Right elevator hinge. |
1 |
0 |
Adobe PDF file |
| 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. |
1 |
0 |
Adobe PDF file |
| 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. |
1 |
0 |
Adobe PDF file |
| 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. |
1 |
0 |
Adobe PDF file |
| 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. |
1 |
0 |
Adobe PDF file |
| 122 |
Systems/Powerplants 9 - Exhibit No. 9B - Photo 21. View of the front of the right engine. |
1 |
0 |
Adobe PDF file |
| 123 |
Systems/Powerplants 9 - Exhibit No. 9B - Photo 22. View of the wreckage from the left engine. |
1 |
0 |
Adobe PDF file |
| 124 |
Systems/Powerplants 9 - Exhibit No. 9B - Photo 23. View of the horizontal stabilizer restraining fixture tool used during the endplay demonstration in Tulsa. |
1 |
0 |
Adobe PDF file |
| 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. |
1 |
0 |
Adobe PDF file |
| 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. |
1 |
0 |
Adobe PDF file |
| 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. |
1 |
0 |
Adobe PDF file |
| 128 |
Systems/Powerplants 9 - Exhibit No. 9B - Photo 27. View of the trim system relays and the mechanical linkages that connect to them (arrows). |
1 |
0 |
Adobe PDF file |
| 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. |
1 |
0 |
Adobe PDF file |
| 130 |
Systems/Powerplants 9 - Exhibit No. 9B - Photo 29. Set-up of the dial indicator during the endplay demonstrations at Oakland. |
1 |
0 |
Adobe PDF file |
| 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. |
1 |
0 |
Adobe PDF file |
| 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. |
1 |
0 |
Adobe PDF file |
| 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. |
1 |
0 |
Adobe PDF file |
| 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. |
1 |
0 |
Adobe PDF file |
| 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 |
1 |
0 |
Adobe PDF file |
| 136 |
Systems/Powerplants 9 - Exhibit No. 9C - Drawings and Diagrams of Pertinent Flight Control System Components |
21 |
0 |
Adobe PDF file |
| 137 |
Systems/Powerplants 9 - Exhibit No. 9D - Horizontal Stabilizer Actuator Travel Data |
5 |
0 |
Adobe PDF file |
| 138 |
Systems/Powerplants 9 - Exhibit No. 9E - Excerpts of the DC-9 Type Certificate Data Sheet |
6 |
0 |
Adobe PDF file |
| 139 |
Systems/Powerplants 9 - Exhibit No. 9F - Civil Air Regulations Part 4b |
40 |
0 |
Adobe PDF file |
| 140 |
Systems/Powerplants 9 - Exhibit No. 9G - Documentation of the Lubrication found on Elevator and Horizontal Stabilizer Fittings of the Accident Airplane |
7 |
0 |
Adobe PDF file |
| 141 |
Systems/Powerplants 9 - Exhibit No. 9H - Flap/Slat Sequence Ground Test Plan & Results |
10 |
0 |
Adobe PDF file |
| 142 |
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 |
7 |
0 |
Adobe PDF file |
| 143 |
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 |
7 |
0 |
Adobe PDF file |
| 144 |
Systems/Powerplants 9 - Exhibit No. 9L - Boeing DC-9 Alert Service Bulletin DC9-27A362, dated Feb. 11, 2000 |
26 |
0 |
Adobe PDF file |
| 145 |
Systems/Powerplants 9 - Exhibit No. 9M - Temporary Revision to MD-80 End Play Check Procedure, dated April 13, 2000 |
4 |
0 |
Adobe PDF file |
| 146 |
Systems/Powerplants 9 - Exhibit No. 9N - Boeing Field Service Messages Addressing DC-9, MD-80/90, B717 Horizontal Stabilizer Issues (Post-Accident) |
10 |
0 |
Adobe PDF file |
| 147 |
Systems/Powerplants 9 - Exhibit No. 9O - Douglas Design Memorandum Addressing Jackscrew Assembly Excessive Wear Rate, dated Feb. 24, 1967 |
4 |
0 |
Adobe PDF file |
| 148 |
Systems/Powerplants 9 - Exhibit No. 9P - Douglas All Operator Letters 9-48 & 9-48A Addressing DC-9 End Play Check Methods, dated 1966-67 |
7 |
0 |
Adobe PDF file |
| 149 |
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 |
3 |
0 |
Adobe PDF file |
| 150 |
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 |
3 |
0 |
Adobe PDF file |
| 151 |
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 |
5 |
0 |
Adobe PDF file |
| 152 |
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 |
25 |
0 |
Adobe PDF file |
| 153 |
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 |
5 |
0 |
Adobe PDF file |
| 154 |
Systems/Powerplants 9 - Exhibit No. 9V - FAA Airworthiness Directive 98-16-01 (MD-11 Horizontal Stabilizer Actuator Assembly Inspection), dated Aug. 14, 1998 |
8 |
0 |
Adobe PDF file |
| 155 |
Systems/Powerplants 9 - Exhibit No. 9W - Excerpts of CAR 4b, Amendment 16, Applicable to DC-9 |
11 |
0 |
Adobe PDF file |
| 156 |
Systems/Powerplants 9 - Exhibit No. 9X - Alaska Airlines Engineering Order No. EO 2740-01036; MD-80 Stabilizer Jackscrew Inspection, dated Feb. 9, 2000 |
8 |
0 |
Adobe PDF file |
| 157 |
Systems/Powerplants 9 - Exhibit No. 9Y - Temporary Revision (27-456) to End-Play Check Procedure; November 20, 2000 |
7 |
0 |
Adobe PDF file |
| 158 |
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) |
13 |
0 |
Adobe PDF file |
| 159 |
Systems 9 - NASA Trip Report |
3 |
0 |
Adobe PDF file |
| 160 |
Systems 9 - NOOK Industry Trip Report |
3 |
0 |
Adobe PDF file |
| 161 |
Systems Photo - Jackscrew |
1 |
0 |
Adobe PDF file |
| 162 |
Systems Photo - Orig. Screw Photo |
1 |
0 |
Adobe PDF file |
| 163 |
Systems Photo - Stab Photo1 |
1 |
0 |
Adobe PDF file |
| 164 |
Systems Photo - Stab Photo2 |
1 |
0 |
Adobe PDF file |
| 165 |
Systems Photo - Stab Photo3 |
1 |
0 |
Adobe PDF file |
| 166 |
Systems Photo - Aft Bulk Door |
1 |
0 |
Adobe PDF file |
| 167 |
Systems Photo - HS Piece |
1 |
0 |
Adobe PDF file |
| 168 |
Systems Photo - HS Structure |
1 |
0 |
Adobe PDF file |
| 169 |
Systems Photo - HS Hinges |
1 |
0 |
Adobe PDF file |
| 170 |
Systems Photo - HS Hinges2 |
1 |
0 |
Adobe PDF file |
| 171 |
Systems Photo - Slinky Closeup |
1 |
0 |
Adobe PDF file |
| 172 |
Systems Photo - Gearbox Closeup |
1 |
0 |
Adobe PDF file |
| 173 |
Systems Photo - Upper Stop |
1 |
0 |
Adobe PDF file |
| 174 |
Systems Photo - Upper Stop Closeup |
1 |
0 |
Adobe PDF file |
| 175 |
Systems Photo - Upper Stop Fracture1 |
1 |
0 |
Adobe PDF file |
| 176 |
Systems Photo - Upper Stop Fracture2 |
1 |
0 |
Adobe PDF file |
| 177 |
Systems Photo - Upper Stop Fracture3 |
1 |
0 |
Adobe PDF file |
| 178 |
Flight Data Recorder 10 - Exhibit No. 10A - Group Chairman Factual Report |
7 |
0 |
Adobe PDF file |
| 179 |
Flight Data Recorder 10 - Exhibit No. 10B - Digital Flight Data Recorder Plots |
9 |
0 |
Adobe PDF file |
| 180 |
Flight Data Recorder 10 - Exhibit No. 10C - Digital Flight Data Recorder Tabular Data |
72 |
0 |
Adobe PDF file |
| 181 |
Maintenance Records 11 - Exhibit No. 11A - Group Chairman Factual Report |
71 |
0 |
Adobe PDF file |
| 182 |
Maintenance Records 11 - Exhibit No. 11B - Operations Specifications Management Personnel |
2 |
0 |
Adobe PDF file |
| 183 |
Maintenance Records 11 - Exhibit No. 11C - Mechanical Reliability Reports |
3 |
0 |
Adobe PDF file |
| 184 |
Maintenance Records 11 - Exhibit No. 11D - MD-80 On Aircraft Maintenance Planning (OAMP):MSG-2 |
3 |
0 |
Adobe PDF file |
| 185 |
Maintenance Records 11 - Exhibit No. 11E - MD-80 On Aircraft Maintenance Planning (OAMP):MSG-3 |
2 |
0 |
Adobe PDF file |
| 186 |
Maintenance Records 11 - Exhibit No. 11F - Boeing Message Concerning Tooling |
3 |
0 |
Adobe PDF file |
| 187 |
Maintenance Records 11 - Exhibit No. 11G - ME-01 Technical Change Request |
2 |
0 |
Adobe PDF file |
| 188 |
Maintenance Records 11 - Exhibit No. 11H - Boeing Message Concerning Lubrication Change |
3 |
0 |
Adobe PDF file |
| 189 |
Maintenance Records 11 - Exhibit No. 11I - Monthly Task Card Changes Sent to FAA in December 1997 |
7 |
0 |
Adobe PDF file |
| 190 |
Maintenance Records 11 - Exhibit No. 11J - Boeing Message Concerning Acceptability of Grease |
2 |
0 |
Adobe PDF file |
| 191 |
Maintenance Records 11 - Exhibit No. 11K - Boeing Message Concerning Aeroshell Grease 33 Lubrication |
3 |
0 |
Adobe PDF file |
| 192 |
Maintenance Records 11 - Exhibit No. 11L - Acme Screw and Nut Endplay Check |
4 |
0 |
Adobe PDF file |
| 193 |
Maintenance Records 11 - Exhibit No. 11M - MIG-4 Non-Routine Work Card |
2 |
0 |
Adobe PDF file |
| 194 |
Maintenance Records 11 - Exhibit No. 11N - Elevator/Stabilizer Lubrication Task Card |
4 |
0 |
Adobe PDF file |
| 195 |
Maintenance Records 11 - Exhibit No. 11O - Alaska Airlines Action Plan |
76 |
0 |
Adobe PDF file |
| 196 |
Maintenance Records 11 - Exhibit No. 11P - Safety Assessment for Alaska Airlines issued June 19, 2000 |
75 |
0 |
Adobe PDF file |
| 197 |
Maintenance Records 11 - Exhibit No. 11Q - Telex Message Between Alaska Airlines and Boeing Regarding Elevator Events and Grease Compatibility; Feb. 2, 2000 |
4 |
0 |
Adobe PDF file |
| 198 |
Maintenance Records 11 - Exhibit No. 11R - Boeing Airliner Magazine Article Re: Aeroshell 33 Grease |
8 |
0 |
Adobe PDF file |
| 199 |
Maintenance Records 11 - Exhibit No. 11S - Letter and Statements Regarding Mr. Falla |
16 |
0 |
Adobe PDF file |
| 200 |
Maintenance Records 11 - Exhibit No. 11T - DoD Survey of Alaska Airlines of 1998 |
30 |
0 |
Adobe PDF file |
| 201 |
Maintenance Records 11 - Exhibit No. 11U - CSET Evaluation Memorandums re: September 18-22, 2000 Inspection |
16 |
0 |
Adobe PDF file |
| 202 |
Maintenance Records 11 - Exhibit No. 11V - Alaska Airlines End Play Check Presentation Slides |
6 |
0 |
Adobe PDF file |
| 203 |
Maintenance Records 11 - Exhibit No. 11W - Excerpts of Boeing Airline Maintenance Inspection Interval Listing; January 2000 |
36 |
0 |
Adobe PDF file |
| 204 |
Cockpit Voice Recorder 12 - Exhibit No. 12A - Group Chairman Factual Report |
54 |
0 |
Adobe PDF file |
| 205 |
Cockpit Voice Recorder 12 - Exhibit No. 12B - Timing and Correlation Study Cockpit Voice Recorder |
14 |
0 |
Adobe PDF file |
| 206 |
Cockpit Voice Recorder 12 - Exhibit No. 12C - Group Chairman's Report of Investigation Sound Spectrum Study |
13 |
0 |
Adobe PDF file |
| 207 |
Aircraft Performance 13 - Exhibit No. 13A - Aircraft Performance Study |
19 |
0 |
Adobe PDF file |
| 208 |
Aircraft Performance 13 - Exhibit No. 13B - Aircraft Performance Study - Radar Data |
47 |
0 |
Adobe PDF file |
| 209 |
Aircraft Performance 13 - Exhibit No. 13C - Aircraft Performance Study - Data Plots |
15 |
0 |
Adobe PDF file |
| 210 |
Aircraft Performance 13 - Exhibit No. 13D - Supplement 1 to Group Chairman Performance Study |
17 |
0 |
Adobe PDF file |
| 211 |
Aircraft Performance 13 - Exhibit No. 13E - Supplement 2 to Group Chairman Performance Study |
11 |
0 |
Adobe PDF file |
| 212 |
Materials Laboratory 15 - Factual Report of Group Chairman - Report 00-145 |
90 |
0 |
Adobe PDF file |
| 213 |
Materials Laboratory 15 - Factual Report 00-145 Errata Sheet |
1 |
0 |
Adobe PDF file |
| 214 |
Materials Laboratory 15 - Factual Report 00-045 |
19 |
0 |
Adobe PDF file |
| 215 |
Materials Laboratory 15 - Factual Report 00-068 |
21 |
0 |
Adobe PDF file |
| 216 |
Materials Laboratory 15 - Factual Report 00-074 |
12 |
0 |
Adobe PDF file |
| 217 |
Materials Laboratory 15 - Factual Report 00-146 |
35 |
0 |
Adobe PDF file |
| 218 |
Materials Laboratory 15 - Errata/Addendum Report - Report No. 00-148 - November 9, 2000 |
5 |
0 |
Adobe PDF file |
| 219 |
Materials Laboratory 15 - Factual Report 01-082 HWI |
40 |
0 |
Adobe PDF file |
| 220 |
Materials Laboratory 15 - Factual Report 01-120 Fractography |
25 |
0 |
Adobe PDF file |
| 221 |
Materials Laboratory 15 - Factual Report 01-118 Restraining Tools |
14 |
0 |
Adobe PDF file |
| 222 |
Materials Laboratory 15 - Factual Report 01-150 Corrosion Test Specimens |
34 |
0 |
Adobe PDF file |
| 223 |
Grease Reports 17 - Exhibit No. 17A - Results of Testing of Grease Samples Interim Report |
21 |
0 |
Adobe PDF file |
| 224 |
Grease Reports 17 - Exhibit No. 17A - Appendix A - Materials Engineering Analysis Report - Submitted by Materials Engineering Laboratory NADEP - Cherry Point, Code 4.3.4 |
3 |
0 |
Adobe PDF file |
| 225 |
Grease Reports 17 - Exhibit No. 17A - Appendix B - Materials Engineering Investigation Report - Submitted by Materials Engineering Laboratory NADEP - Jacksonville, Code 4.3.4 |
10 |
0 |
Adobe PDF file |
| 226 |
Grease Reports 17 - Exhibit No. 17A - Appendix C - Analytical Laboratory Report - Submitted by Analytical Laboratory NAWCAD - Patuxent River, Code 4.3.4 |
5 |
0 |
Adobe PDF file |
| 227 |
Grease Reports 17 - Exhibit No. 17B - Report of Corrosion Testing of Greases |
2 |
0 |
Adobe PDF file |
| 228 |
Grease Reports 17 - Exhibit No. 17C - Visual Aid (Cover Sheet) |
1 |
0 |
Adobe PDF file |
| 229 |
Grease Reports 17 - Exhibit No. 17C - Visual Aid (Greases used to lubricate jackscrew) |
1 |
0 |
Adobe PDF file |
| 230 |
Grease Reports 17 - Exhibit No. 17D - Boeing Service Letter dated August 12, 1993 |
12 |
0 |
Adobe PDF file |
| 231 |
Grease Reports 17 - Exhibit No. 17E - Boeing Service Letter dated December 21, 1995 |
5 |
0 |
Adobe PDF file |
| 232 |
Grease Reports 17 - Exhibit No. 17F - Boeing Service Letter dated June 30, 1997 |
13 |
0 |
Adobe PDF file |
| 233 |
Grease Reports 17 - Exhibit No. 17G - Excerpts from BCAG Twin Jet Technical Focus Report |
3 |
0 |
Adobe PDF file |
| 234 |
Grease Reports 17 - Exhibit No. 17H - Excerpts from BCAG Maintenance Manual |
4 |
0 |
Adobe PDF file |
| 235 |
Grease Reports 17 - Exhibit No. 17I - Exposure Tests of Aluminum Bronze to Lubricating Greases and Fluid Contaminants |
13 |
0 |
Adobe PDF file |
| 236 |
Grease Reports 17 - Exhibit No. 17I - Appendix A - Photographs of exposed test coupons |
17 |
0 |
Adobe PDF file |
| 237 |
Grease Reports 17 - Exhibit No. 17I - Appendix B - Photographs of grease mixtures following the tests. |
8 |
0 |
Adobe PDF file |
| 238 |
Grease Reports 17 - Exhibit No. 17J - Examination of Grease Samples Taken from Jackscrew Assemblies of In-service Aircraft |
10 |
0 |
Adobe PDF file |
| 239 |
Table of Samples from Examination of Grease Samples Taken from Jackscrew Assemblies of In-service Aircraft |
10 |
0 |
Adobe PDF file |
| 240 |
Appendix A-Photographs of Extraction Samples; Examination of Grease Samples Taken from Jackscrew Assemblies of In-service Aircraft |
9 |
0 |
Adobe PDF file |
| 241 |
Grease Reports 17 - Exhibit No. 17K - Surface Chemistry Analysis of Discolorations on Aluminum Bronze Specimens |
6 |
0 |
Adobe PDF file |
| 242 |
Grease Reports 17 - Exhibit No. 17L - Investigation of the Wear Rate of Grease-lubricated C95500 Bronze (Executive Report) |
7 |
0 |
Adobe PDF file |
| 243 |
Grease Reports 17 - Investigation of the Wear Rate of Grease-Lubricated C95500 Aluminum Bronze (Full Report) |
66 |
0 |
Adobe PDF file |
| 244 |
Grease Report 17 - Microstructural Analysis Laboratory Report MA-1044 NTSB Grease-Particulate Analysis |
26 |
0 |
Adobe PDF file |
| 245 |
Grease Report 17 - Materials Engineering Analysis Report - Naval Aviation Depot-Cherry Point, North Carolina |
3 |
0 |
Adobe PDF file |
| 246 |
Consultant's Review of Chemical Analyses of Residues From Aircraft Jackscrews in Support of Alaska Air Flight 261 ACCIDENT INVESTIGATION |
7 |
0 |
Adobe PDF file |
| 247 |
NAVAIR-Aerospace Materials Division Report: Grease Evaluation by Fourier Transform Infrared Spectrometry |
19 |
0 |
Adobe PDF file |
| 248 |
NAVAIR Aerospace Division: Materials Engineering Investigation-NTSB Grease Evaluation |
13 |
0 |
Adobe PDF file |
| 249 |
Interview Transcript (August 7) |
251 |
0 |
Adobe PDF file |
| 250 |
Interview Transcript (August 8) |
288 |
0 |
Adobe PDF file |
| 251 |
Interview Transcript (August 9) |
269 |
0 |
Adobe PDF file |
| 252 |
Interview Transcript (August 10) |
119 |
0 |
Adobe PDF file |
| 253 |
Interview Transcript (August 15) |
264 |
0 |
Adobe PDF file |
| 254 |
Interview Transcript - Federal Labor Relations Authority |
68 |
0 |
Adobe PDF file |
| 255 |
Interview Transcript of Azbell |
20 |
0 |
Adobe PDF file |
| 256 |
Interview Transcript of Bautista |
22 |
0 |
Adobe PDF file |
| 257 |
Interview Transcript of Afman |
45 |
0 |
Adobe PDF file |
| 258 |
Interview Transcript of Siotkas |
9 |
0 |
Adobe PDF file |
| 259 |
Public Hearing Testimony Transcript Review - Alaska Airlines MD-83 N963AS |
5 |
0 |
Adobe PDF file |
| 260 |
Transcript - Public Hearing Day 1 (12/13/2000) |
346 |
0 |
Adobe PDF file |
| 261 |
Transcript - Public Hearing Day 2 (12/14/2000) |
275 |
0 |
Adobe PDF file |
| 262 |
Transcript - Public Hearing Day 3 (12/15/2000) |
358 |
0 |
Adobe PDF file |
| 263 |
Transcript - Public Hearing Day 4 (12/16/2000) |
330 |
0 |
Adobe PDF file |
| 264 |
ALPA Submission Correspondence dated August 23, 2002 |
11 |
0 |
Adobe PDF file |
| 265 |
ALPA Submission |
58 |
0 |
Adobe PDF file |
| 266 |
Boeing Submission |
26 |
0 |
Adobe PDF file |
| 267 |
Aircraft Mechanics Fraternal Association Submission |
34 |
0 |
Adobe PDF file |
| 268 |
Alaska Airlines Submission |
32 |
0 |
Adobe PDF file |
| 269 |
Alaska Airlines Submission - Attachment 1 - Deposition of Michael Minnette |
74 |
0 |
Adobe PDF file |
| 270 |
Alaska Airlines Submission - Attachment 2 - |
116 |
0 |
Adobe PDF file |
| 271 |
Alaska Airlines Submission - Attachment 3 - Falex Report |
318 |
0 |
Adobe PDF file |
| 272 |
Transcript-Board Meeting 12/10 |
292 |
0 |
Adobe PDF file |
| 273 |
VHS Animation Tape |
1 |
0 |
Adobe PDF file |
