# Service difficulty reports: N628AW, cancelled Jan 28, 2014 A list on [N628AW, cancelled Jan 28, 2014](https://openairdocs.org/deregistered/N628AW-2014-01-28.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 6 · 256 reports - [SDR USAA2014F00046](https://openairdocs.org/sdr/USAA2014F00046.md): Bulb · inoperative · Oct 22, 2013 · N628AW · Airbus A320231 · Emergency Lighting > LEFT OVERWING EMERGENCY LIGHTS CONTROL PANEL HAD SEVERAL BULBS OUT. R & R PANEL. - [SDR USAA2013080800015](https://openairdocs.org/sdr/USAA2013080800015.md): Lens · missing · Aug 7, 2013 · N628AW · Airbus A320231 · Emergency Lighting > EMERGENCY LIGHT LENS MISSING ON ROWS 10 & 11. INSTALLED NEW LENS FOR EMERGENCY EXIT LIGHTS ROWS 10 AND 11 LT. - [SDR USAA2013072400007](https://openairdocs.org/sdr/USAA2013072400007.md): Lens · missing · Jul 23, 2013 · N628AW · Airbus A320231 · Emergency Lighting > EMERGENCY LIGHT LENS MISSING AT 17C. REPLACED EMERGENCY LIGHT LENS AT 17C. - [SDR USAA2013070100010](https://openairdocs.org/sdr/USAA2013070100010.md): Lens · missing · Jun 28, 2013 · N628AW · Airbus A320231 · Emergency Lighting > ROW 26, ACFT LT, FLOOR EXIT LIGHT MISSING COVER. REPLACED LENS ON EMERGENCY LIGHT AT 26L. - [SDR USAA2013053000005](https://openairdocs.org/sdr/USAA2013053000005.md): Lens · missing · May 29, 2013 · N628AW · Airbus A320231 · Emergency Lighting > ROW 1, LT MISSING SEAT MOUNTED EMERGENCY LIGHT LENS. REPLACED MISSING LIGHT LENS. - [SDR USAA2013040800017](https://openairdocs.org/sdr/USAA2013040800017.md): Lens · missing · Apr 6, 2013 · N628AW · Airbus A320231 · Emergency Lighting > ROW 26L EMERGENCY LIGHT LENS MISSING. INSTALLED NEW LIGHT LENS AS NEEDED. - [SDR USAA2013040200027](https://openairdocs.org/sdr/USAA2013040200027.md): Lens · missing · Apr 1, 2013 · N628AW · Airbus A320231 · Emergency Lighting > EMERGENCY LIGHT LENS AT ROW 19L IS MISSING. INSTALLED EMERGENCY LIGHT LENS AT ROW 19L. - [SDR USAA2013021100027](https://openairdocs.org/sdr/USAA2013021100027.md): Power Supply · failed · Feb 9, 2013 · N628AW · Airbus A320231 · Emergency Lighting > CABIN FORWARD EMERGENCY POWER SUPPLY UNIT FAILED BITE TEST. REMOVED AND REPLACED CABIN FORWARD EMERGENCY POWER SUPPLY UNIT. - [SDR USAA2013020800019](https://openairdocs.org/sdr/USAA2013020800019.md): Lens · detached · Feb 6, 2013 · N628AW · Airbus A320231 · Emergency Lighting > EMERGENCY EXIT SIGN ON THE LOWER DOOR 2R FELL OFF DURING LANDING. REPLACED EMERGENCY EXIT LENS ON DOOR 2R. - [SDR USAA2013013100016](https://openairdocs.org/sdr/USAA2013013100016.md): Lens · missing · Jan 30, 2013 · N628AW · Airbus A320231 · Emergency Lighting > SEAT MOUNTED EMERGENCY LIGHT AT ROW 9R IS MISSING THE LENS. INSTALLED LENS ON SEAT MOUNTED EMERGENCY LIGHT AT ROW 9R IAW AIRBUS MAINTENANCE MANUAL 33-51-13. - [SDR USAA2013011400020](https://openairdocs.org/sdr/USAA2013011400020.md): Power Supply · inoperative · Jan 12, 2013 · N628AW · Airbus A320231 · Emergency Lighting > EMERGENCY LIGHT POWER SUPPLY UNIT 10WL INOPERATIVE. REMOVED AND REPLACED EPSU IAW MM 33-51-38. - [SDR USAA2013010300018](https://openairdocs.org/sdr/USAA2013010300018.md): Power Supply · inoperative · Dec 31, 2012 · N628AW · Airbus A320231 · Emergency Lighting > EMERGENCY LIGHTS DO NOT TEST CORRECTLY L1 AND R1 DOOR. REMOVED AND REPLACED POWER SUPPLY PER AMM 33-51-38 - OPS CHECKED GOOD. - [SDR USAA2013010300017](https://openairdocs.org/sdr/USAA2013010300017.md): Power Supply · inoperative · Dec 31, 2012 · N628AW · Airbus A320231 · Emergency Lighting > EMERGENCY LIGHTS DO NOT TEST CORRECTLY L1 & R1 DOOR. REMOVED AND REPLACED POWER SUPPLY 10WL PER 33-51-38-000-001. SYSTEM OPS CHECKED GOOD. - [SDR USAA2012110200025](https://openairdocs.org/sdr/USAA2012110200025.md): Sign · cracked · Nov 1, 2012 · N628AW · Airbus A320231 · Emergency Lighting > THE 2L EXIT SIGN CRACKED. REMOVED & REPLACED 2L EXIT SIGN. - [SDR USAA2012100500037](https://openairdocs.org/sdr/USAA2012100500037.md): Lens · detached · Oct 4, 2012 · N628AW · Airbus A320231 · Emergency Lighting > EXIT PATH LIGHTING LENS COVER OFF LEFT SIDE LAST ROW. REPLACED EMERGENCY LIGHT LENS ROW 26 LEFT. - [SDR USAA2012100500032](https://openairdocs.org/sdr/USAA2012100500032.md): Lens · missing · Oct 2, 2012 · N628AW · Airbus A320231 · Emergency Lighting > EMERGENCY LIGHT LENS MISSING NEAR ROW 25ABC FLOORING. INSTALLED LENS AT ROW 25ABC. - [SDR USAA2012071600004](https://openairdocs.org/sdr/USAA2012071600004.md): Wire · broken · Jul 12, 2012 · N628AW · Airbus A320231 · Light System Wiring > BC1 CHECK - FORWARD LEFT WINDSCREEN EMERGENCY LIGHT WIRES BROKEN. REPAIRED FORWARD LEFT WINDSCREEN EMERGENCY LIGHT WIRES IAW A320 ESPM 20-48-25. OPS CHECK GOOD IAW A320 AMM 33-51-00-710-001A. - [SDR USAA2012071600003](https://openairdocs.org/sdr/USAA2012071600003.md): Wire · broken · Jul 12, 2012 · N628AW · Airbus A320231 · Light System Wiring > BC1 CHECK - NR 1 LEFT AND NR 3 LEFT EMERGENCY LIGHT WIRES BROKEN. REPAIRED NR 1 LEFT AND NR 3 LEFT EMERGENCY LIGHT WIRES IAW A320 AMM 33-51-19-0401 AND AIRBUS ESPM 20-43-13. OPS CHECK GOOD IAW A320 AMM 33-51-00-710-001A. - [SDR USAA2012071600012](https://openairdocs.org/sdr/USAA2012071600012.md): Skin · saturated · Jul 4, 2012 · N628AW · Airbus A320231 · Elevator, Plate/Skin > BC1 CHECK - WATER INGRESS ON UPPER SURFACE OF LEFT ELEVATOR AT ZONE 1 AND ZONE 3. REPAIRED UPPER SURFACE OF LEFT ELEVATOR AT ZONE 1 AND ZONE 3 IAW A320 SRM 55-21-11 AND 55-20-00. - [SDR USAA2012071600015](https://openairdocs.org/sdr/USAA2012071600015.md): Skin · saturated · Jul 3, 2012 · N628AW · Airbus A320231 · Elevator, Plate/Skin > BC1 CHECK - WATER INGRESS ON UPPER SURFACE OF RIGHT ELEVATOR AT ZONE 1 AND ZONE 5. REPAIRED UPPER SURFACE OF RIGHT ELEVATOR AT ZONE 1 AND ZONE 5 IAW A320 SRM 55-21-11, PARAGRAPH D & E. - [SDR USAA2012031200025](https://openairdocs.org/sdr/USAA2012031200025.md): Bracket · broken · Mar 11, 2012 · N628AW · Airbus A320231 · Emergency Equipment > SLIDE BUSTLE DOOR 2R NEEDS TO BE REFITTED. FOUND LATCHING BRACKET BROKEN. REPAIRED SLIDE COVER DOOR R2 IAW STRUCTURAL REPAIR MANUAL 51-42-11. - [SDR USAA2012030800016](https://openairdocs.org/sdr/USAA2012030800016.md): Battery · discharged · Mar 2, 2012 · N628AW · Airbus A320231 · Emergency Equipment > AFT FLIGHT ATTENDANT SWIVEL SEAT FLASHLIGHT INOPERATIVE. REMOVED AND REPLACED FLASHLIGHT BATTERY AFT SWIVEL JUMPSEAT. OPS CHECKED GOOD. - [SDR USAA2012021300020](https://openairdocs.org/sdr/USAA2012021300020.md): Lens · missing · Feb 11, 2012 · N628AW · Airbus A320231 · Emergency Lighting > LENS MISSING FROM EMERGENCY SEAT MOUNTED LIGHT ROW 11L. INSTALLED LENS ON SEAT MOUNTED EMERGENCY LIGHT ROW 11L. - [SDR USAA2012012600005](https://openairdocs.org/sdr/USAA2012012600005.md): Light · broken · Jan 25, 2012 · N628AW · Airbus A320231 · Emergency Lighting > SMALL EMERGENCY LIGHT AT EDGE OF FORWARD BULKHEAD BROKEN. REPLACED FORWARD WINDSCREEN EMERGENCY LIGHT ASSEMBLY. - [SDR USAA2012010400021](https://openairdocs.org/sdr/USAA2012010400021.md): Transducer · failed · Jan 1, 2012 · N628AW · Airbus A320231 · Compressor Bleed Control > AFTER TAKEOFF PRIOR TO 1000', ENGINE NR 1 SURGED TWICE AND SELF-RECOVERED WITH NORMAL INDICATIONS. ON LANDING ROLLOUT, RECEIVED ECAM MESSAGES FOR ENG 1 COMPRESSOR VANE AND FADEC MX. TWO SUBSEQUENT EVENTS FOR NR 1 ENGINE SURGE ON TAKEOFF ON 1/3/12 AND 1/4/12. - [SDR USAA2011101000008](https://openairdocs.org/sdr/USAA2011101000008.md): Connector · defective · Oct 8, 2011 · N628AW · Airbus A320231 · Light System Wiring > RIGHT SIDE OVERWING EMERGENCY EXIT LIGHT INOPERATIVE. MAINTENANCE REMOVED AND RE-INSTALLED BAYONET CONNECTOR - OPERATIONAL CHECK NORMAL IAW AIRBUS MAINTENANCE MANUAL 33-51-16. - [SDR USAA2011100400017](https://openairdocs.org/sdr/USAA2011100400017.md): Spring · broken · Oct 3, 2011 · N628AW · Airbus A320231 · Emergency Equipment > CABIN DOOR 2L ARMED INDICATION INTERMITTENT. MAINTENANCE REPLACED BROKEN SPRING IN AFT GIRT BAR FLOOR FITTING. - [SDR USAA2011092900013](https://openairdocs.org/sdr/USAA2011092900013.md): Wire · loose · Sep 28, 2011 · N628AW · Airbus A320231 · Light System Wiring > EMERGENCY LIGHT WIRING IS HANGING LOOSE UNDER SEAT ROW 11L. MAINTENANCE SECURED LIGHT WIRING FOR SEAT 11L - OPERATIONAL CHECK NORMAL. - [SDR USAA2011091200016](https://openairdocs.org/sdr/USAA2011091200016.md): Container · broken · Sep 9, 2011 · N628AW · Airbus A320231 · Passenger Oxygen System > SEAT ROW 12L PASSENGER EMERGENCY O2 PANEL WILL NOT LATCH - SEAT ROW 18R PASSENGER EMERGENCY O2 PANEL TEST BUTTON IS BROKEN. MAINTENANCE REPLACED PASSENGER EMERGENCY O2 CONTAINERS AT SEAT ROWS 12L & 18R IAW AIRBUS MAINTENANCE MANUAL 35-21-41-401. - [SDR USAA2011061400004](https://openairdocs.org/sdr/USAA2011061400004.md): Control Unit · malfunctioned · Jun 13, 2011 · N628AW · Airbus A320231 · Emergency Lighting > LAS - EEL - EMERGENCY EXIT LIGHT TEST FAULTS 'AFT L'. RESET 'AFT L' POWER CONTROL UNIT, OPERATIONAL CHECK GOOD. - [SDR USAA2010121793113](https://openairdocs.org/sdr/USAA2010121793113.md): Profile · cracked · Dec 17, 2010 · N628AW · Airbus A320231 · Emergency Exits > SAL - S5 - MAJOR REPAIR - CRACKS ON LOWER FLANGE OF RIGHT LOAD TRANSMITTING PROFILE OF THE LEFT AFT EMERGENCY EXIT (834) AT CENTRAL FUSELAGE. REPLACED LOWER FLANGE OF RIGHT LOAD TRANSMITTING PROFILE OF THE LEFT AFT EMERGENCY EXIT (834) AT CENTRAL FUSELAGE IAW - [SDR USAA2010121793112](https://openairdocs.org/sdr/USAA2010121793112.md): Profile · cracked · Dec 17, 2010 · N628AW · Airbus A320231 · Emergency Exits > SAL - S5 - MAJOR REPAIR - CRACKS ON LOWER FLANGE OF RIGHT LOAD TRANSMITTING PROFILE OF THE FORWARD LEFT EMERGENCY EXIT (833) AT CENTRAL FUSELAGE. REPLACED LOWER FLANGE OF RIGHT LOAD TRANSMITTING PROFILE OF THE FORWARD RIGHT EMERGENCY EXIT (833) AT CENTRAL FUS - [SDR USAA2010121793111](https://openairdocs.org/sdr/USAA2010121793111.md): Profile · cracked · Dec 17, 2010 · N628AW · Airbus A320231 · Emergency Exits > SAL - S5 - MAJOR REPAIR - CRACKS ON LOWER FLANGE OF RIGHT LOAD TRANSMITTIG PROFILE OF THE FORWARD RIGHT EMERGENCY EXIT (843) AT CENTRAL FUSELAGE. REPLACED LOWER FLANGE OF RIGHT LOAD TRANSMITTING PROFILE OF THE FORWARD RIGHT EMERGENCY EXIT (843) AT CENTRAL FUS - [SDR USAA2010121793125](https://openairdocs.org/sdr/USAA2010121793125.md): Sill · corroded · Dec 16, 2010 · N628AW · Airbus A320231 · Fuselage Miscellaneous Structure > SAL - MAJOR REPAIR - S5 CHECK - CORROSION ON LOWER SILL AROUND GIRT BAR FITTING AT FR 66, S23L. REPAIRED LOWER SILL AROUND GIRT BAR FITTING AT FR 66, S23L IAW EA 133170. - [SDR USAA2010121793124](https://openairdocs.org/sdr/USAA2010121793124.md): Sill · corroded · Dec 16, 2010 · N628AW · Airbus A320231 · Fuselage Miscellaneous Structure > SAL - MAJOR REPAIR - S5 CHECK - CORROSION ON LOWER SILL AROUND GIRT BAR FITTING AT FR 68, S23R. REPAIRED LOWER SILL AROUND GIRT BAR FITTING AT FR 68, S23R IAW EA 133170. - [SDR USAA2010121793118](https://openairdocs.org/sdr/USAA2010121793118.md): Floorbeam · cracked · Dec 16, 2010 · N628AW · Airbus A320231 · Fuselage Main, Floor Beam > SAL - S5 - MAJOR REPAIR - CRACK ON FLOORBEAM BETWEEN FR46 TO FR47, -Y254. REPAIRED FLOORBEAM BETWEEN FR46 TO FR47, -Y254 IAW EA 133198. - [SDR USAA2010121793117](https://openairdocs.org/sdr/USAA2010121793117.md): Profile · cracked · Dec 16, 2010 · N628AW · Airbus A320231 · Emergency Exits > SAL - S5 - MAJOR REPAIR - CRACKS ON LOWER FLANGE OF LEFT LOAD TRANSMITTING PROFILE OF THE LEFT AFT EMERGENCY EXIT (834) AT CENTER FUSELAGE. REPLACED LOWER FLANGE OF LEFT LOAD TRANSMITTING PROFILE OF THE LEFT AFT EMERGENCY EXIT (834) AT CENTER FUSELAGE IAW EA - [SDR USAA2010121793116](https://openairdocs.org/sdr/USAA2010121793116.md): Profile · cracked · Dec 16, 2010 · N628AW · Airbus A320231 · Emergency Exits > SAL - S5 - MAJOR REPAIR - CRACKS ON LOWER FLANGE OF RIGHT LOAD TRANSMITTING PROFILE OF THE RIGHT AFT EMERGENCY EXIT (844) AT CENTRAL FUSELAGE. REPLACED LOWER FLANGE OF RIGHT LOAD TRANSMITTING PROFILE OF THE RIGHT AFT EMERGENCY EXIT (844) AT CENTRAL FUSELAGE I - [SDR USAA2010121793115](https://openairdocs.org/sdr/USAA2010121793115.md): Profile · cracked · Dec 16, 2010 · N628AW · Airbus A320231 · Emergency Exits > SAL - S5 - MAJOR REPAIR - CRACKS ON LOWER FLANGE OF LEFT LOAD TRANSMITTING PROFILE OF THE FORWARD LEFT EMERGENCY EXIT (833) AT CENTRAL FUSELAGE. REPLACED LOWER FLANGE OF LEFT LOAD TRANSMITTING PROFILE OF THE FORWARD LEFT EMERGENCY EXIT (833) AT CENTRAL FUSELA - [SDR USAA2010121793114](https://openairdocs.org/sdr/USAA2010121793114.md): Profile · cracked · Dec 16, 2010 · N628AW · Airbus A320231 · Emergency Exits > SAL - S5 - MAJOR REPAIR - CRACKS ON LOWER FLANGE OF LEFT LOAD TRANSMITTING PROFILE OF THE FORWARD RIGHT EMERGENCY EXIT (843) AT CENTRAL FUSELAGE. REPLACED LOWER FLANGE OF LEFT LOAD TRANSMITTING PROFILE OF THE FORWARD RIGHT EMERGENCY EXIT (843) AT CENTRAL FUSE - [SDR USAA2010121793123](https://openairdocs.org/sdr/USAA2010121793123.md): Skin · corroded · Dec 14, 2010 · N628AW · Airbus A320231 · Fuselage Main, Plate/Skin > SAL - S5 - MAJOR REPAIR - CORROSION ON INTERNAL SKIN AT FR58 + 15 INCHES BETWEEN S43R & S44R AFT CARGO COMPARTMENT. REPAIRED INTERNAL SKIN AT FR58 + 15 INCHES BETWEEN S43R & S44R IAW EA 133191. - [SDR USAA2010121793122](https://openairdocs.org/sdr/USAA2010121793122.md): Frame · cracked · Dec 13, 2010 · N628AW · Airbus A320231 · Fuselage Main, Frame > SAL - S5 - MAJOR REPAIR - CRACK ON UPPER FLANGE OF FRAME 25 AT LEVEL S31L FWD C.C. REPAIRED UPPER FRAME FLANGE AT FR25, S31L IAW A320 SRM 53-00-12. - [SDR USAA2010121793120](https://openairdocs.org/sdr/USAA2010121793120.md): Angle · corroded · Dec 13, 2010 · N628AW · Airbus A320231 · Fuselage Miscellaneous Structure > SAL - S5 - MAJOR REPAIR - CORROSION ON ANGLE AT FR71 CUTOUT ACCESS DOOR 312AR BETWEEN S27R TO S30R TAIL SECTION AFT FUSELAGE. REPLACED ANGLE AT FR71 CUTOUT ACCESS DOOR 312AR BETWEEN S27R TO S30R IAW A320 SRM 51-72-11 & AIRBUS DRAWING D53571500. - [SDR USAA2010121793142](https://openairdocs.org/sdr/USAA2010121793142.md): Slide Raft · faulty · Dec 4, 2010 · N628AW · Airbus A320231 · Escape Slide > SAL - EES - S5 CHECK - PASSENGER CREW DOOR 842 SLIDE RAFT WAS OVER INFLATED. REPLACED SLIDE RAFT AT PASSENGER CREW DOOR 842 IAW TASK CARD 26C84252006. - [SDR USAA2010121793141](https://openairdocs.org/sdr/USAA2010121793141.md): Slide Raft · faulty · Dec 4, 2010 · N628AW · Airbus A320231 · Escape Slide > SAL - EES - S5 CHECK - PASSENGER CREW DOOR 832 SLIDE RAFT WAS OVER INFLATED. REPLACED SLIDE RAFT AT PASSENGER CREW DOOR 832 IAW TASK CARD 26C83252008. - [SDR USAA2010121793140](https://openairdocs.org/sdr/USAA2010121793140.md): Slide Raft · faulty · Dec 4, 2010 · N628AW · Airbus A320231 · Escape Slide > SAL - EES - S5 CHECK - PASSENGER CREW DOOR 841 SLIDE RAFT WAS OVER INFLATED. REPLACED SLIDE RAFT AT PASSENGER CREW DOOR 841 IAW TASK CARD 26C84152006. - [SDR USAA2010120792901](https://openairdocs.org/sdr/USAA2010120792901.md): Fitting · corroded · Dec 4, 2010 · N628AW · Airbus A320231 · Fuselage Miscellaneous Structure > SAL - S5 - MAJOR REPAIR - LEVEL 2 GALVANIC CORROSION ON CLEAT AT FR30 BETWEEN S39L TO S40L. REPLACED CLEAT AT FR30 BETWEEN S39L TO S40L IAW A320 SRM 51-72-11 & AIRBUS DRAWING D53231212. - [SDR USAA2010121793119](https://openairdocs.org/sdr/USAA2010121793119.md): Stiffener · cracked · Dec 3, 2010 · N628AW · Airbus A320231 · Horizontal Stabilizer, Spar/Rib > SAL - S5 - MAJOR REPAIR - CRACKS FRONT SPAR OF LEADING EDGE OF LEFT HORIZONTAL STABILIZER INTERNAL AREA OF ACCESS PANEL 331AB. REPAIRED STIFFENER BETWEEN RIB 4 TO RIB 5 OF LEADING EDGE OF LEFT HORIZONTAL STABILIZER INTERNAL AREA IAW EA 133177 & A320 SRM 51-77 - [SDR USAA2010120892925](https://openairdocs.org/sdr/USAA2010120892925.md): Shear Pin · corroded · Dec 3, 2010 · N628AW · Airbus A320231 · Engine Mount Section > SAL - MAJOR REPAIR - S5 - CORROSION WAS FOUND BETWEEN RIB 4 AND RIB 5 ON INNER PIN, LOCATED AT LEFT UPPER FROM LINK PIN ASSY OF AFT ENGINE MOUNT (ENGINE NR 1). REPLACED INNER PIN BETWEEN RIB 4 AND RIB 5 LOCATED AT LEFT UPPER FROM LINK PIN ASSY OF AFT ENGINE M - [SDR USAA2010120892924](https://openairdocs.org/sdr/USAA2010120892924.md): Shear Pin · corroded · Dec 3, 2010 · N628AW · Airbus A320231 · Engine Mount Section > SAL - MAJOR REPAIR - S5 - CORROSION WAS FOUND BETWEEN RIB 4 AND RIB 5 ON INNER PIN, LOCATED AT LEFT MIDDLE FROM LINK PIN ASSY OF AFT ENGINE MOUNT (ENGINE NR 1). REPLACED INNER PIN BETWEEN RIB 4 AND RIB 5 LOCATED AT LEFT MIDDLE FROM LINK PIN ASSY OF AFT ENGINE Next page: https://openairdocs.org/deregistered/N628AW-2014-01-28/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 = 'N628AW' AND deregistration_id = 'N628AW-2014-01-28' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/deregistered/N628AW-2014-01-28/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.