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Cover Sheet for FOI99MA178, FOI99MA178X and FOI99MA178XX (Freedom of Information Data) |
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Supplement A |
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Supplement B |
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Operations 2 - Group Chairman Factual Report |
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ATC 3 - ATC Information |
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Meteorology 5 - Group Chairman Factual Report |
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Meteorology 5 - Attachment 1 |
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Meteorology 5 - Attachment 1 - Chart 1A |
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Meteorology 5 - Attachment 1 - Chart 2A |
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Meteorology 5 - Attachment 1 - Chart 3A |
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Meteorology 5 - Attachment 1 - Chart 4A |
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Meteorology 5 - Attachment 1 - Chart 5A |
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Meteorology 5 - Attachment 1 - Chart 6A |
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Meteorology 5 - Attachment 1 - Chart 7A |
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Meteorology 5 - Attachment 1 - (continued) |
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Meteorology 5 - Attachment 1 - Chart (page24) |
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Meteorology 5 - Attachment 1 - Chart (page 25) |
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Meteorology 5 - Attachment 1 (continued) |
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Meteorology 5 - Attachment 1 - Chart (page 28) |
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Meteorology 5 - Attachment 1 - Chart (page 29) |
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Meteorology 5 - Attachment 1 - (continued) |
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Meteorology 5 - Attachment 1 - Chart (page 37) |
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Meteorology 5 - Attachment 1 - (continued) |
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Meteorology 5 - Attachment 1 - Chart (page 42) |
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Meteorology 5 - Attachment 1 - Chart (page 43) |
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Meteorology 5 - Attachment 1 - Chart (page 44) |
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Meteorology 5 - Attachment 1 - (continued) |
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Meteorology 5 - Attachment 1 - Chart (page 50) |
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Meteorology 5 - Attachment 1 - Chart (page 51) |
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Meteorology 5 - Attachment 1 - Chart (page 52) |
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Meteorology 5 - Attachment 1 - Chart (page 53) |
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Meteorology 5 - Attachment 1 - Chart (page 54) |
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Meteorology 5 - Attachment 1 - Chart (page 55) |
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Meteorology 5 - Attachment 1 - Chart (page 56) |
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Meteorology 5 - Attachment 1 - Chart (page 57) |
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Meteorology 5 - Attachment 1 - Chart (page 58) |
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Meteorology 5 - Attachment 1 - Chart (page 59) |
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Meteorology 5 - Attachment 1 - Chart (page 60) |
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Meteorology 5 - Attachment 1 - Chart (page 61) |
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Meteorology 5 - Attachment 1 - Chart (page 62) |
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Meteorology 5 - Attachment 1 - Chart (page 63) |
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Meteorology 5 - Attachment 1 - Chart (page 64) |
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Meteorology 5 - Attachment 1 - (continued) |
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Meteorology 5 - Attachment 1 - Chart (page 74) |
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Meteorology 5 - Attachment 1 - (continued) |
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Meteorology 5 - Attachment 1 - (continued) |
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Powerplants 8 - Group Chairman Factual Report |
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Aircraft Performance 13 - Attachment 1 - Tabular Radar Data & Radar Data Plots |
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Aircraft Performance 13 - Attachment 1 - Chart 1 - Flight Path of N9253N based on New York Center ARSR data. |
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Aircraft Perfromance 13 - Attachment 1 - Chart 2 - Radar Data from Several sources |
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Aircraft Performance 13 - Attachment 1 - Chart 3 - Selected Final Radar Returns for N9253N |
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Aircraft Performance 13 - Attachment 1 - Chart 4 - Radar Data from Several Sources |
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Aircraft Performance 13 - Attachment 1 - Chart 5 - Westchester County Airport ASR Data Ground Track of AA 1484 and N9253N |
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Aircraft Performance 13 - Attachment 1 - Chart 6 - Westchester County Airport ASR Data |
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Aircraft Performance 13 - Attachment 2 - Wind Data |
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Aircraft Performance 13 - Attachment 3 - Chart 1 - Input to Simulation 7/16/99 |
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Aircraft Performance 13 - Attachment 3 - Chart 2 - Radar Data from several sources compared with Simulation Results |
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Aircraft Performance 13 - Attachment 3 - Chart 3 - Comparison of Simulattion Altitude with Radar Altitude |
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Aircraft Performance 13 - Attachment 3 - Chart 4 - Simulation Results 7/16/99 |
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Aircraft Performance 13 - Attachment 3 - Chart 5 - Simulation Results 7/16/99 |
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Aircraft Performance 13 - Attachment 3 - Chart 6 - View from South East, Looking North West |
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Aircraft Performance 13 - Attachment 3 - Chart 7 - View from East of Wreckage Site, Looking West |
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Aircraft Performance 13 - Attachment 3 - Chart 8 - View from South of Wreckage site, Looking North |
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Airworthiness - Group Chairman Factual Report |
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Airworthiness - Appendix A - Photographs (28) |
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Airworthiness - Photo 1. View of the cockpit and cabin area. (NTSB-B2) |
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Airworthiness - Photo 2. Close-up view of the instrument panel. Note that the attitude indicator (denoted by arrow) is captured in nose-down, steep right bank attitude. (NTSB-E21) |
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Airworhtiness - Photo 3. View of right wing damage (view from forward looking aft). Note that the entire length of the wing spar was recovered. (NTSB-C2) |
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Airworthiness - Photo 4. Close-up view of the outboard portion of the right wing (view from forward looking aft). Note aftward accordion crush damage of the leading edge skin. (NTSB-C13) |
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Airworthiness - Photo 5. View of the inboard section of the right wing (view from aft looking forward). Note damage to main spar (background). Also note entire left flap (foreground) and lack of bulging or bowing deformation |
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Airworthiness - Photo 6. View off the inboard section of the right wing (view from forward looking aft). Note damage to main spar and the 90-degree forward bend (foreground) (NTSB-C14) |
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Airworthiness - Photo 7. Close-up view of the right wing spar area near 90-degree forward bend. Right main landing gear trunion (shown in foreground) is normally installed in this area. Note damage to the spar web in this ar |
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Airworthiness - Photo 8. View of right wing damage (view from froward looking aft). Note that the entire length of the wing spar was recovered. (NTSB-C3) |
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Airworthiness - Photo 9. Close-up view of the leading edge skin of the left wing (view from forward looking aft). Note hydrodynamic deformation in aft direction. (NTSB-I12) |
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Airworthiness - Photo 10. View of inboard section of left wing spar. Note spar web damage and the diverging spar caps. Right main landing gear is normally stowed directly behind this area. (NTSB-I6) |
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Airworthiness - Photo 11. Close-up view of the upper spar cap fitting of the wing carry-through section where it mates with the left wing spar. Note rearward direction of fractures. (NTSB-I12) |
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Airworhtiness - Photo 12. View of the left side of the aft cabin and tail section. Note the bowing deformation of the separated rudder (denoted by arrow) and the twisting of the vertical stabilizer toward the right side of t |
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Airworthiness - Photo 13. Close-up view of the vertical stabilizer (view from right side view). Note that the upper half of the stabilizer is bent over toward the right side of the airplane. (NTSB-C22) |
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Airworthiness - Photo 14. View of stabilator damage and upper structure of mating tail cone (denoted by arrow). Note bowing deformation of the tail cone and the rudder adjacent to it, and impact damage of the left stabilator. |
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Airworthiness - Photo 15. View of the damage to the bottom structure of the aft-facing passenger seats in row 2. |
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Airworthiness - Photo 16. View of the seat back structure of the aft-facing passenger seats in row 2. Note that the structure is bulged outward (forward relative to their normal installation in airplane). (NTSB-A2) |
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Airworthiness - Photo 17. Close-up view of left main landing gear actuator. Note that the end of the actuator (denoted by arrow) is in the retracted position. (NTSB-E2) |
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Airworthiness - Photo 18. Close-up view of the exposed portion of the stabilator trim jackscrew. (NTSB-T18) |
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Airworthiness - Photo 19. Microscopic view of the airspeed indicator face. Note needle slap mark (denoted by arrow) beyond the 210-knot marking. This slap mark corresponds to the designed maximum needle travel. (NTSB-Lab Po |
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Airworthiness - Photo 20. Microscopic view of the vertical speed indicator face. Note needle slap mark is near the maximum indication of 2,000 feet per minute descent. (NTSB-Lab Polaroid) |
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Airworthiness - Photo 21. Close-up view of the engine tachometer after removal from wreckage. Note that needle is captured at the 2,750 rpm indications, and the tachometer time reads 663.5 hours. (NTSB-T1) |
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Airworthiness - Photo 22. View of primary (engine-driven) vacuum pump, after diassembly. The shear shaft was found intact. Note lack of vane damage or deformation. Also note lack of any pre-impact mechanical damage. (NTSB-S |
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Airworthiness - Photo 23. View of propeller assembly, prior to disassembly by investigators. Note "S" bending, chordwise scratching, and leading edge gouging. (NTSB-BB) |
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Airworthiness - Photo 24. View of all three propeller blades after removal from hub by investigators. Note "S" bending, chordwise scratching, and leading edge gouging. Also note two impressions in leading edge of blade no. 1 |
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Airworthiness - Photo 25. Close-up view of leading edge damage of propeller blade no. 1. (NTSB-CC) |
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Airworthiness - Photo 26. Overall view of engine prior to disassembly and inspection. Note that propeller had separated from the engine. Also note damage to the top of the no. 2 cylinder head section. (NTSB-AA) |
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Airworthiness - Photo 27. Close-up view of the top of the no. 1 cylinder head section (view looking outboard) with propeller blade no. 1 resting next to it. Note consistent locations of blade damage with the cylinder damage. |
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Airworthiness - Photo 28. Close-up view of the top of the no. 1 cylinder head section (view looking inboard) with propeller blade no. 1 resting next to it. Note consistent locations of blade damage with the cylinder damage. |
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Airworthiness - Appendix B - Drawings of Structural Damage |
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Airworthiness - Appendix C - Autopilot & GPS Information |
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Airworthiness - Appendix D - Maintenance Record Excerpts |
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Release of Aircraft Wreckage, NTSB Form 6120.15 |
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Photo 1. Photograph of the accident airplane taken within three months of the accident. (Photograph provided by previous owner of accident airplane) |
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Photo 2. Photograph of the cockpit and instrument panel layout of the accident airplane taken within three months of the accident. (Photograph provided by previous owner of accident airplane) |
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Photo 3. Photograph showing the interior cabin of the accident taken within three months of the accident. Second row of seats were aft-facing. (Photograph provided by previous owner of accident airplane) |
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Photo 4. Overall view of wreckage (with right wing in the foreground) after it was laid out in a two-dimensional reconstruction. (NTSB-B2) |
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Statement of Party Representatives to NTSB Investigation |
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Toxicological Report |
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