# Service difficulty reports: N162AA, cancelled Jun 10, 2002 A list on [N162AA, cancelled Jun 10, 2002](https://openairdocs.org/deregistered/N162AA-2002-06-10.md). Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first. Page 1 of 2 · 91 reports - [SDR HALA9900040](https://openairdocs.org/sdr/HALA9900040.md): Wire · chafed · Feb 5, 1999 · N162AA · Doug DC1010 · Fire Detection > LAS - (LOG PAGE NR 4970432). ENGINE NR 3 LOOP B LIGHT FLICKERED ON AND OFF FOR 5 MINUTES DURING CLIMB-OUT. ACCOMPISHED ABNORMAL PROCEDURE CHECK LIST AND SELECTED AND TESTED LOOP A. OPS NORMAL. FOUND CHAFED WIRE. REPAIRED AND REPOSITIONED WIRE, OP CHECKS O - [SDR HALA9900024](https://openairdocs.org/sdr/HALA9900024.md): Dump Valve · malfunctioned · Jan 14, 1999 · N162AA · Doug DC1010 · Fuel Dump System > LAX - FLT 9 - AFTER TAKEOFF AFTER GEAR RETRACTION STRONG VIBRATION FROM NOSE GEAR AREA. EXTENDED GEAR AND DUMPED FUEL. WHEN DUMPING FUEL ONLY RT DUMP VALVE OPENED, CHECKED CBS AND THEY WERE OK. AIRCRAFT RETURNED TO LAX, WHERE AN UNEVENTFUL LANDING WAS MADE. - [SDR HALA9900023](https://openairdocs.org/sdr/HALA9900023.md): Actuator · malfunctioned · Jan 14, 1999 · N162AA · Doug DC1010 · Landing Gear Door Actuator > LAX - FLT 09 - AFTER TAKEOFF AFTER GEAR RETRACTION STRONG VIBRATION FROM NOSE GEAR AREA. EXTENDED GEAR AND DUMPED FUEL. AIRCRAFT RETURNED TO LAX WHERE IT MADE AN UNEVENTFUL LANDING. REMOVED AND REPLACED NOSE GEAR DOOR ACTUATORS, OPS CHECK OK. (M) - [SDR HALA9800023](https://openairdocs.org/sdr/HALA9800023.md): Vertical Gyro · failed · Jan 22, 1998 · N162AA · Doug DC1010 · Attitude Gyro and Indicating System > LOS - FLT 931 - DURING CLIMB PASSING FL 210, WHEN A/P NR 1 INITIATED HDG CHANGE, AIRCRAFT WENT INTO A RAPID RATE OF ROLL. A/P NR 1 DISCONNECTED AUTOMATICALLY. CAPTAINS ADI DISPLAYED ATT FLAG AND SPEED FLAG. WHILE INTERCEPTING LOA HNL, ADI FAILED. REPLACED - [SDR AALA972468](https://openairdocs.org/sdr/AALA972468.md): Stringer · corroded · Dec 17, 1997 · N162AA · Doug DC1010 · Fuselage Main, Longeron/Stringer > TUL - STR 51L IS CORRODED FROM STA 1338 TO STA 1360. REPAIRED DAMAGED AREA PER ESO 7349 DATED 12-10-97. PRIMED AND PAINTED AREA PER SRM 51-21-01. TST: 67,144.30 HOURS. CYCLES: 25,370. (X) - [SDR AALA972473](https://openairdocs.org/sdr/AALA972473.md): Skin · corroded · Dec 15, 1997 · N162AA · Doug DC1010 · Wing, Plate/Skin > TUL - CORROSION ON SKIN AROUND FASTENER HEAD ON LOWER SURFACE OF LEFT WIRE. REPAIR AND BLENDING WERE ACCOMPLISHED PER ESO 7349 DATED 12-11-97. TST: 67,144.30 HOURS. CYCLES: 25,370. (X) - [SDR AALA972472](https://openairdocs.org/sdr/AALA972472.md): Skin · corroded · Dec 15, 1997 · N162AA · Doug DC1010 · Wing, Plate/Skin > TUL - CORROSION AROUND FASTENER HEAD ON LOWER SURFACE OF LEFT WING AT REAR SPAR APPROXIMATELY STA XORS 600. REPAIR AND BLENDING WAS ACCOMPLISHED PER ESO 7349 DATED 12-11-97. TST: 67,144.30 HOURS. CYCLES: 25,370. (X) - [SDR AALA972469](https://openairdocs.org/sdr/AALA972469.md): Stringer · corroded · Dec 15, 1997 · N162AA · Doug DC1010 · Fuselage Main, Longeron/Stringer > TUL - CORROSION ON STR 48R FROM STA 1257 TO STA 1360. REPAIRED DAMAGED AREA IAW ESO-7349. ALODINED, PRIMED AND PAINTED AREA IAW SRM 51-21-01. TST: 67,144.30 HOURS. CYCLES: 25,370. (X) - [SDR AALA972476](https://openairdocs.org/sdr/AALA972476.md): Trap Panel · corroded · Dec 13, 1997 · N162AA · Doug DC1010 · Wing Miscellaneous Structure > TUL - THE INBOARD BARREL NUT HALF IN THE TRAPEZOIDAL PANEL FOR THE SIDE BRACE TO TRAPEZOIDAL PANEL ATTACHMENT IS CORRODED. FABRICATED AND INSTALLED BUSHING PER SRM 57-20-00. HOLES WERE REWORKED PER ESO 7349 DATED 12-11-97 PER ENGINEERING. TST: 67,144.30 HO - [SDR AALA972467](https://openairdocs.org/sdr/AALA972467.md): Shear Tie · corroded · Dec 13, 1997 · N162AA · Doug DC1010 · Fuselage Miscellaneous Structure > TUL - CORROSION ON FORWARD AND AFT SIDE OF SHEAR TIE AT STA 1216 FROM STR 40R TO STR 46R. INSTALLED NEW SHEAR TIE PER AARD 51-01-00-05. TST: 67,144.30 HOURS. CYCLES: 25,370. (X) - [SDR AALA972429](https://openairdocs.org/sdr/AALA972429.md): Support · corroded · Dec 13, 1997 · N162AA · Doug DC1010 · Fuselage Miscellaneous Structure > TUL - CORROSION ON SLANT PANEL AND FLOORBOARD SUPPORT. REPLACED SUPPORT WITH NEW PER SRM 51-01-00-05. TST: 67,144.30 HOURS. CYCLES: 25,370. (X) - [SDR AALA972428](https://openairdocs.org/sdr/AALA972428.md): Support · corroded · Dec 13, 1997 · N162AA · Doug DC1010 · Fuselage Miscellaneous Structure > TUL - FOUND CORROSION ON SLANT PANEL AND FLOORBOARD SUPPORT BETWEEN BS 1781-1964. REPLACED SUPPORT WITH NEW PER SRM 51-01-00-05. (M) - [SDR ALA972437](https://openairdocs.org/sdr/ALA972437.md): Roller Tray · corroded · Dec 12, 1997 · N162AA · Doug DC1010 · Fuselage Miscellaneous Structure > TUL- CORROSION FOUND ON ROLLER TRAY IN CENTER CARGO COMPARTMENT. REPLACED ROLLER TRAY PER SRM 51-01-00-05. TST: 67,144.30 HOURS. CYCLES: 25,370. (X) - [SDR AALA972475](https://openairdocs.org/sdr/AALA972475.md): Trap Panel · corroded · Dec 12, 1997 · N162AA · Doug DC1010 · Wing Miscellaneous Structure > TUL - INBOARD BOLT HOLE FOR THE SIDE BRACE ATTACHMENT TO THE TRAPEZOIDAL PANEL CORRODED. FABRICATED AND INSTALLED BUSHING PER 57-20-00. REWORKED 4 EACH HOLES PER ESO 7349 DATED 12-11-97. TST: 67,144.30 HOURS. CYCLES: 25,370. (X) - [SDR AALA972474](https://openairdocs.org/sdr/AALA972474.md): Skin · corroded · Dec 12, 1997 · N162AA · Doug DC1010 · Wing, Plate/Skin > TUL - CORROSION ON UPPER LEFT WING SKIN FROM STR 7 TO STR 5 BETWEEN STA XORS-402 AND XORS-489. REPAIRED UPPER WING SKIN AND PROTECTED AS OUTLINED IN ESO 7349 DATED 12-11-97. TST: 67,144.30 HOURS. CYCLES: 25,370. (X) - [SDR AALA972471](https://openairdocs.org/sdr/AALA972471.md): Skin · corroded · Dec 12, 1997 · N162AA · Doug DC1010 · Wing, Plate/Skin > TUL - CORROSION ON UPPER WING SKIN FROM STA XORS-216 TO XORS-235 BETWEEN STR 10 AND STR 11. REPAIRED UPPER WING SKIN AND PROTECTED AS OUTLINED IN ESO 7349 - 12-11-97. TST: 67,144.30 HOURS. CYCLES: 25,370. (X) - [SDR AALA972470](https://openairdocs.org/sdr/AALA972470.md): Skin · corroded · Dec 12, 1997 · N162AA · Doug DC1010 · Fuselage Main, Plate/Skin > TUL - CORROSION ON SKIN AT BS 1175-1179. REPAIRED PER SRM 53-00-01 WITH DOUBLER. TST: 67,144.30 HOURS. CYCLES: 25,370. (X) - [SDR AALA972439](https://openairdocs.org/sdr/AALA972439.md): Longeron · corroded · Dec 12, 1997 · N162AA · Doug DC1010 · Fuselage Main, Longeron/Stringer > TUL - STR 48R IS CORRODED FROM STA 1156 TO STA 1257. REPLACED DAMAGED AREA IAW ESO 7349 DATED 12-10-97. TST: 67,144.30 HOURS. CYCLES: 25,370. (X) - [SDR AALA972438](https://openairdocs.org/sdr/AALA972438.md): Longeron · corroded · Dec 12, 1997 · N162AA · Doug DC1010 · Fuselage Main, Longeron/Stringer > TUL - CORROSION FOUND ON LONGERON 46L. REWORK AND OK FOR CONTINUED SERVICE PER ESO 7349 DATED 12-10-97. TST: 67,144.30 HOURS. CYCLES: 25,370. (X) - [SDR AALA972431](https://openairdocs.org/sdr/AALA972431.md): Skin · corroded · Dec 12, 1997 · N162AA · Doug DC1010 · Wing, Plate/Skin > TUL - LOCAL CORROSION AT LOWER WING SKIN JUST INBOARD (2 FASTENERS) AND OUTBOARD (3 FASTENERS) OF JACK PAD. REMOVED FASTENERS AND BLENDED AND REPAIRED AREA, THEN, RE-INSTALLED FASTENERS PER ESO 7349 DATED 12-11-97. TST: 67,144.30 HOURS. CYCLES: 25,370. ( - [SDR AALA972430](https://openairdocs.org/sdr/AALA972430.md): Skin · corroded · Dec 12, 1997 · N162AA · Doug DC1010 · Wing, Plate/Skin > TUL - CORROSION ON UPPER WING SKIN FROM STR 7 TO STR 5 AND BETWEEN STA XORS 506 AND STA XORS 545. REPAIRED PER ESO 7349 PAGE 1. REMOVED CORROSION AND FLAPPER PEEN. REWORKED SURFACES AND TREATED METAL. TST: 67,144.30 HOURS. CYCLES: 25,370. (X) - [SDR AALA972427](https://openairdocs.org/sdr/AALA972427.md): Stringer · corroded · Dec 12, 1997 · N162AA · Doug DC1010 · Fuselage Main, Longeron/Stringer > CORROSION ON STRINGER 47L AT STATION 1216. ALODINED AND PRIMED, REINSTALLED FASTENERS, OK FOR SERVICE PER ESO 7349 DATED 12-10-93. (M) - [SDR AALA972426](https://openairdocs.org/sdr/AALA972426.md): Shear Tie · corroded · Dec 12, 1997 · N162AA · Doug DC1010 · Fuselage Miscellaneous Structure > TUL - FOUND CORROSION FOUND ON SHEAR TIE AT BS 1236. INSTALLED NEW SHEAR TIE PER AARD 51-01-00-05. (M) - [SDR AALA972425](https://openairdocs.org/sdr/AALA972425.md): Stringer · corroded · Dec 12, 1997 · N162AA · Doug DC1010 · Fuselage Main, Longeron/Stringer > TUL - FOUND CORROSION ON STRINGER 48L AT STATION 1216. ALODINED AND PRIMED AND REINSTALLED FASTENERS OK FOR SERVICE PER ESO7349 DATED 12-10-97. (M) - [SDR AALA972424](https://openairdocs.org/sdr/AALA972424.md): Shear Tie · corroded · Dec 12, 1997 · N162AA · Doug DC1010 · Fuselage Miscellaneous Structure > FOUND CORROSION FOUND ON SHEAR TIE AT BS 1195. REPLACED SHEAR TIE WITH NEW ONE PER AARD 51-01-00-05. (M) - [SDR AALA972423](https://openairdocs.org/sdr/AALA972423.md): Shear Tie · corroded · Dec 12, 1997 · N162AA · Doug DC1010 · Fuselage Miscellaneous Structure > TUL -SHEAR TIE CORRODED. REPLACED WITH NEW SHEAR TIE PER SRM AARD 51-01-00-05. TST: 67,144.30 HOURS. CYCLES: 25,370. (X) - [SDR AALA972433](https://openairdocs.org/sdr/AALA972433.md): Skin · corroded · Dec 11, 1997 · N162AA · Doug DC1010 · Wing, Plate/Skin > TUL - LOWER WING SKIN CORRODED TWO PLACES NEAR FASTENERS 2 FEET INBOARD OF JACK PAD. ACCOMPLISHED REPAIR PER ESO 7349 DATED 12-11-97. TST: 67,144.30 HOURS. CYCLES: 25,370. (X) - [SDR AALA972432](https://openairdocs.org/sdr/AALA972432.md): Skin · corroded · Dec 11, 1997 · N162AA · Doug DC1010 · Wing, Plate/Skin > TUL - LOWER WING SKIN CORRODED SEVERAL AREAS OUTBOARD OF JACK PAD. REPAIR OF WING LOWER SKIN ACCOMPLISHED PER ESO 7349 DATED 12-11-97. TST: 67,144.30 HOURS. CYCLES: 25,370. (X) - [SDR AALA972401](https://openairdocs.org/sdr/AALA972401.md): Angle · corroded · Dec 11, 1997 · N162AA · Doug DC1010 · Fuselage Miscellaneous Structure > TUL - TEE CAP ANGLE CORRODED OUTBOARD OF LONGERON 48L AT STA 595. REPLACED EXISTING LOWER EXTERNAL DOUBLER WITH ENLARGED DOUBLER. INSTALLED IAW GENERAL NOTES PER ESO 7349 DATED 12-10-97. TST: 67,144.30 HOURS. CYCLES: 25,370. (X) - [SDR AALA972400](https://openairdocs.org/sdr/AALA972400.md): Bracket · corroded · Dec 11, 1997 · N162AA · Doug DC1010 · Fuselage Miscellaneous Structure > TUL - AFT WALL LOWER ATTACH BRACKET IS CORRODED. REMOVED AND REPLACED BRACKET PER AARD 51-01-00-05. TST: 67,144.30 HOURS. CYCLES: 25,370. (X) - [SDR AALA972399](https://openairdocs.org/sdr/AALA972399.md): Shear Tie · corroded · Dec 11, 1997 · N162AA · Doug DC1010 · Fuselage Miscellaneous Structure > TUL - LOWER LEG OF SHEAR TIE IS CORRODED. REMOVED AND REPLACED SHEAR TIE PER SRM 53-30-00 FIG 10. INSTALLED INTERCOSTAL PER AARD 51-01-00-5. TST: 67,144.30 HOURS. CYCLES: 25,370. (X) - [SDR AALA972398](https://openairdocs.org/sdr/AALA972398.md): Stringer · corroded · Dec 11, 1997 · N162AA · Doug DC1010 · Fuselage Main, Longeron/Stringer > TUL - CORROSION ON STR 48L FROM STA 535 TO STA 595. REPLACED CORRODED SECTION OF STR 48L BETWEEN STA 535 AND STA 595 PER ESO 7349 DATED 12-10-97. TST: 67,144.30 HOURS. CYCLES: 25,370. (X) - [SDR AALA972397](https://openairdocs.org/sdr/AALA972397.md): Frame · corroded · Dec 11, 1997 · N162AA · Doug DC1010 · Fuselage Main, Frame > TUL - CORROSION ON FRAME NEAR LONGERON 48L. INSTALLED DOUBLER ON FRAME AND REINSTALLED FRAME PER ESO 7349 DATED 12-10-97. TST: 67,144.30 HOURS. CYCLES: 25,370. (X) - [SDR AALA972396](https://openairdocs.org/sdr/AALA972396.md): Frame · corroded · Dec 11, 1997 · N162AA · Doug DC1010 · Fuselage Main, Frame > TUL - CORROSION ON FRAME NEAR LONGERON 48L. INSTALLED DOUBLER AND REINSTALLED FRAME PER ESO 7349 DATED 12-10-97. TST: 67,144.30 HOURS. CYCLES: 25,370. (X) - [SDR AALA972395](https://openairdocs.org/sdr/AALA972395.md): Frame · corroded · Dec 11, 1997 · N162AA · Doug DC1010 · Fuselage Main, Frame > TUL - CORROSION ON FRAME AT STA 542, 5 INCHES INBOARD OF NOSE GEAR BULKHEAD. INSTALLED DOUBLER ON FRAME AND REINSTALLED PER ESO 7349 DATED 12-10-97. TST: 67,144.30 HOURS. CYCLES: 25,370. (X) - [SDR AALA972394](https://openairdocs.org/sdr/AALA972394.md): Frame · corroded · Dec 11, 1997 · N162AA · Doug DC1010 · Fuselage Main, Frame > TUL - CORROSION ON FRAME NEAR LONGERON 48L. INSTALLED DOUBLER ON FRAME. ACCOMPLISHED PER ESO 7349 DATED 12-10-97. TST: 67,144.30 HOURS. CYCLES: 25,370. (X) - [SDR AALA972523](https://openairdocs.org/sdr/AALA972523.md): Roller Tray · corroded · Dec 9, 1997 · N162AA · Doug DC1010 · Fuselage Miscellaneous Structure > TUL - CORROSION ON NR 2 ROLLER TRAY. REPLACED NR 2 ROLLER TRAY FROM STA 1521 TO STA 1701 IAW AARD 51-01-00-05. TST: 67,144.30 HOURS. CYCLES: 25,370. (X) - [SDR AALA972436](https://openairdocs.org/sdr/AALA972436.md): Guide Rail · corroded · Dec 9, 1997 · N162AA · Doug DC1010 · Fuselage Miscellaneous Structure > TUL - CORROSION FOUND ON LT GUIDE RAIL IN CENTER CARGO COMPARTMENT. REPLACED GUIDE RAIL PER AARD 51-01-00-05. TST: 67,144.30 HOURS. CYCLES: 25,370. (X) - [SDR AALA972364](https://openairdocs.org/sdr/AALA972364.md): Roller Tray · corroded · Dec 9, 1997 · N162AA · Doug DC1010 · Fuselage Miscellaneous Structure > TUL - FOUND CORROSION. REPLACED ROLLER TRAY NR 3 FROM 1521 TO 1701 PER SRM 51-01-00-05. (M) - [SDR AALA972363](https://openairdocs.org/sdr/AALA972363.md): Frame · corroded · Dec 9, 1997 · N162AA · Doug DC1010 · Fuselage Main, Frame > TUL - FOUND CORROSION. SPLICED IN NEW SECTION OF BELL FRAME FROM LONGERON 48L TO 48R PER SRM 53-30-00. (M) - [SDR AALA972362](https://openairdocs.org/sdr/AALA972362.md): Bulkhead Tee · cracked · Dec 9, 1997 · N162AA · Doug DC1010 · Fuselage Main, Bulkhead > TUL - HFEC INDICATES CRACK AT 1 FASTENER HOLE IN BULKHEAD TEE CAP LEG, RT SIDE. INSTALLED ARROWHEAD DOUBLER AND STRAP PER ESO 7349, DATED 11/20/97. (M) - [SDR AALA972435](https://openairdocs.org/sdr/AALA972435.md): Skin · corroded · Dec 8, 1997 · N162AA · Doug DC1010 · Fuselage Main, Plate/Skin > TUL - CORROSION FOUND ON SKIN AT BS 1721-1741. REPAIRED BY ENGINEERS ESO 7349 DATED 12-4-97. SPLICED LONGERONS AND INSTALLED SKIN DOUBLERS. TST: 67,144.30 HOURS. CYCLES, 25,370. (X) - [SDR AALA972331](https://openairdocs.org/sdr/AALA972331.md): Splice Plate · corroded · Dec 8, 1997 · N162AA · Doug DC1010 · Fuselage Miscellaneous Structure > TUL - FOUND CORROSION ON SPLICE PLATE, LONGERON AND HAT CHANNEL. ENGINEERS ESO 7349 DATED 12-2-97, COVERS THE REWORK OF THE AREA. (M) - [SDR AALA972333](https://openairdocs.org/sdr/AALA972333.md): Frame · corroded · Dec 5, 1997 · N162AA · Doug DC1010 · Fuselage Main, Frame > TUL - THE BELLFRAME FLANGE UPPER SURFACE FROM 50L TO 50R LONGERON HAS CORROSION. INSTALLED CHANNEL REPAIR AS PER SRM 53-30-00 PAGE 31. (M) - [SDR AALA972332](https://openairdocs.org/sdr/AALA972332.md): Longeron · corroded · Dec 5, 1997 · N162AA · Doug DC1010 · Fuselage Main, Longeron/Stringer > TUL - LONGERON HAS CORROSION IN AND OUTSIDE. REMOVED CORRODED SECTION OF LONGERON AND INSTALLED NEW SECTION WITH SPLICE REPAIR IAW 53-10-00 OF SRM VOL I. (M) - [SDR AALA972335](https://openairdocs.org/sdr/AALA972335.md): Splice · corroded · Dec 4, 1997 · N162AA · Doug DC1010 · Fuselage Miscellaneous Structure > FOUND CORROSION ON LONG 52 SPLICE. REMOVED OLD LONG SPLICE AND INSTALLED NEW SPLICE IAW 51-01-01-05 SRM. (M) - [SDR AALA972334](https://openairdocs.org/sdr/AALA972334.md): Longeron · corroded · Dec 4, 1997 · N162AA · Doug DC1010 · Fuselage Main, Longeron/Stringer > TUL - FOUND CORROSION IN LONG 51 LEFT FROM STATION 1721 TO STATION 1766. REMOVED CORROSION IN LONG AND INSTALLED NEW SECTION ALONG WITH SPLICE REPAIRS IAW 53-10-00 OF SRM VOL I AARD. (M) - [SDR AALA972318](https://openairdocs.org/sdr/AALA972318.md): Doubler · corroded · Dec 4, 1997 · N162AA · Doug DC1010 · Fuselage Miscellaneous Structure > TUL - FOUND CORROSION AROUND NUTPLATES ON ANTENNA DOUBLER AT STATION 1226 BETWEEN STRINGER 49L AND 50L. REMOVED AND REPLACED ANTENNA DOUBLER AND NUTPLATES PER AARD 51-01-00. (M) - [SDR AALA972317](https://openairdocs.org/sdr/AALA972317.md): Doubler · corroded · Dec 4, 1997 · N162AA · Doug DC1010 · Fuselage Miscellaneous Structure > TUL - FOUND CORROSION ON ANTENNA DOUBLER AT STATION 1185 BETWEEN STRINGER 49L AND 50L AROUND NUTPLATES. REMOVED AND REPLACED ANTENNA DOUBLER AND NOT PLATES PER 51-01-00 OF AARD. (M) - [SDR AALA972316](https://openairdocs.org/sdr/AALA972316.md): Angle · corroded · Dec 4, 1997 · N162AA · Doug DC1010 · Fuselage Miscellaneous Structure > TUL - FOUND ANGLE CORRODED NEAR FASTENERS. REPLACE ANGLE AND FASTENERS PER SRM 51-10-00-1. (M) Next page: https://openairdocs.org/deregistered/N162AA-2002-06-10/reports.md?page=2 ## The whole list in SQL Runs in DuckDB 1.2 or later on the release's Parquet files over HTTPS: ```sql SELECT sdr_id, difficulty_date, n_number, aircraft_make, aircraft_model, part_name, part_condition, jasc_code, discrepancy FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet' WHERE n_number = 'N162AA' AND deregistration_id = 'N162AA-2002-06-10' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/deregistered/N162AA-2002-06-10/reports --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.