# Service difficulty reports: N462CA, cancelled Sep 3, 2013 A list on [N462CA, cancelled Sep 3, 2013](https://openairdocs.org/deregistered/N462CA-2013-09-03.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 · 88 reports - [SDR FXGA20101214001](https://openairdocs.org/sdr/FXGA20101214001.md): Skin · chafed · Dec 14, 2010 · N462CA · Emb EMB120QC · Fuselage Main, Plate/Skin > FUSELAGE SKIN CHAFED BY A FLEX DUCT AT FRAME 30(F/S 10172) AND STRINGER L18. REPAIRED IAW SRM 53-00-01. - [SDR COMA0210024](https://openairdocs.org/sdr/COMA0210024.md): Brake Assy · Jun 4, 2002 · N462CA · Emb EMB120RT · Landing Gear Brake System > FLIGHT 5064 DURING LANDING ALL 4 MLG TIRES BLEW OUT. REPLACED 4 MLG BRAKE ASSY, 4 MLG WHEEL AND TIRES. REPLACED BOTH BRAKE CONTROL VALVES FOR PREVENTIVE MAINT. & ANTI SKID CONTROL BOX - CAUSE OF LOCK UP UNDETERMINED. - [SDR COMA0210014](https://openairdocs.org/sdr/COMA0210014.md): Bracket · cracked · Apr 13, 2002 · N462CA · Emb EMB120RT · Wing Miscellaneous Structure > DUIRNG A 2,000 FLIGHT CYCLE INSPECTION, THE FUEL SHUT-OFF SUPPORT BRACKET (P/N 120-24373-002) ON THE RIGHT WING BOX FORWARD SIDE AFT OF FRAME 10 WAS FOUND TO BE CRACKED.THE CRACKED BRACKET (P/N 120-24373-002) WAS REMOVED FROM THE AIRCRAFT, REPAIRED AND RE-INST - [SDR COMA0110161](https://openairdocs.org/sdr/COMA0110161.md): Gauge · malfunctioned · Dec 11, 2001 · N462CA · Emb EMB120RT · Engine BMEP/Torque Indicating > FLIGHT 5070 R/H ENGINE TORQUE GAUGE FAILED DURING T/O.REPLACED THE TORQUE INDICATOR. - [SDR COMA0110132](https://openairdocs.org/sdr/COMA0110132.md): Light · broken · Aug 1, 2001 · N462CA · Emb EMB120RT · Emergency Lighting > EMERGENCY LIGHT AT ROW 5 IS BROKEN.REPLACED LIGHT ASSY. - [SDR COMA0110081](https://openairdocs.org/sdr/COMA0110081.md): Floor Support · cracked · Mar 12, 2001 · N462CA · Emb EMB120RT · Fuselage Miscellaneous Structure > DURING 2C CHECK TASK 121-01Z, THE FUSELAGE LT FLOOR PROP AT FRAME 13 WAS FOUND CRACKED. THE PART WAS REPAIRED IN ACCORDANCE WITH EMB-120 SRM STANDARD PRACTICES AND AERODESIGN REPORT 3647-1, REV IR, 5-3-00. - [SDR COMA0110080](https://openairdocs.org/sdr/COMA0110080.md): Strap · corroded · Mar 12, 2001 · N462CA · Emb EMB120RT · Fuselage Miscellaneous Structure > DURING 2C CHECK TASK 141-01Z, THE FUSELAGE LT FLOORBEAM BUTT STRAP WAS FOUND CORRODED. THE PART WAS REPLACED IN ACCORDANCE WITH EMB-120 SRM STANDARD PRACTICES AND AERODESIGN REPORT 2174-1, REV IR, 1-15-97. - [SDR COMA0110079](https://openairdocs.org/sdr/COMA0110079.md): Crossbeam · corroded · Mar 12, 2001 · N462CA · Emb EMB120RT · Fuselage Miscellaneous Structure > DURING 2C CHECK TASK 131-01Z, THE FUSELAGE LT FLOOR CROSSBEAM AT FRAME 15 WAS FOUND CORRODED. THE PART WAS REPLACED IN ACCORDANCE WITH EMB-120 SRM STANDARD PRACTICES. - [SDR COMA0110078](https://openairdocs.org/sdr/COMA0110078.md): Floorbeam · corroded · Mar 12, 2001 · N462CA · Emb EMB120RT · Fuselage Main, Floor Beam > DURING 2C CHECK TASK 152-01Z, THE FUSELAGE RT FLOOR T-SECTION AT FRAME 36 WAS FOUND CORRODED. THE PART WAS REPLACED IN ACCORDANCE WITH EMB-120 SRM STANDARD PRACTICES. - [SDR COMA0110077](https://openairdocs.org/sdr/COMA0110077.md): Support · cracked · Mar 12, 2001 · N462CA · Emb EMB120RT · Wing Miscellaneous Structure > DURING 2C CHECK TASK 5720-552-01I, THE LT WING UPPER SKIN SUPPORT AT RIB 21, BETWEEN FR ON SPAR AND STRINGERS 2A, WAS FOUND CRACKED. THE PART WAS REPLACED IN ACCORDANCE WITH EMB-120 SRM STANDARD PRACTICES. - [SDR COMA0110076](https://openairdocs.org/sdr/COMA0110076.md): Support · cracked · Mar 12, 2001 · N462CA · Emb EMB120RT · Wing Miscellaneous Structure > DURING 2C CHECK TASK 5720-552-01I, THE LT WING SUPPER SKIN SUPPORT AT RIB 20, BETWEEN STRINGERS 2A AND 3A, WAS FOUND CRACKED. THE PART WAS REPLACED IN ACCORDANCE WITH EMB-120 SRM STANDARD PRACTICES. - [SDR COMA0110075](https://openairdocs.org/sdr/COMA0110075.md): Support · cracked · Mar 12, 2001 · N462CA · Emb EMB120RT · Wing Miscellaneous Structure > DURING 2C CHECK TASK 5720-552-01I, THE LT WING UPPER SUPPORT AT RIB 20, BETWEEN STRINGERS 3A AND 4A, WAS FOUND CRACKED. THE PART WAS REPLACED IN ACCORDANCE WITH EMB-120 SRM STANDARD PRCTICES. - [SDR COMA0110074](https://openairdocs.org/sdr/COMA0110074.md): Support · cracked · Mar 12, 2001 · N462CA · Emb EMB120RT · Fuselage Miscellaneous Structure > DURING 2C CHECK TASK 232-01Z, THE FUSELAGE RT SKIN SUPPORT AT FRAME 13A, STRINGER 14R WAS FOUND CRACKED. THE PART WAS REPAIRED IN ACCORDANCE WITH EMB-120 SRM STANDARD PRACTICES AND AERODESIGN REPORT 3653-2, REV IR, 11-7-00. - [SDR COMA0110073](https://openairdocs.org/sdr/COMA0110073.md): Support · cracked · Mar 12, 2001 · N462CA · Emb EMB120RT · Fuselage Main, Structure > DURING 2C CHECK TASK 5310-221-05I, THE FUSELAGE LT SKIN SUPPORT BEHIND THE CAPTAIN''S DV WINDOW, BETWEEN FRAMES 12A AND 13, WAS FOUND CRCKED. THE PART WAS REPLACED IN ACCORDANCE WITH EMB-120 SRM STANDARD PRACTICES. - [SDR COMA0110072](https://openairdocs.org/sdr/COMA0110072.md): Support · cracked · Mar 12, 2001 · N462CA · Emb EMB120RT · Fuselage Main, Structure > DURING 2C CHECK TASK 5310-221-05I, THE FUSELAGE LT SKIN SUPPORT BEHIND AND ABOVE THE CAPTAIN''S DV WINDOW, BETWEEN FRAMES 12A AND 13, WAS FOUND CRACKED. THE PART WAS REPLACED IN ACCORDANCE WITH EMB-120 SRM STANDARD PRACTICES. - [SDR COMA0110071](https://openairdocs.org/sdr/COMA0110071.md): Support · cracked · Mar 12, 2001 · N462CA · Emb EMB120RT · Fuselage Miscellaneous Structure > DURING 2C CHECK TASK 261-01Z, THE FUSELAGE LT SKIN SUPPORT AT FRAME 40, BETWEEN STRINGERS 3L AND 4L, WAS FOUND CRACKED. THE PART WAS REPLACED IN ACCORDANCE WITH EMB-120 SRM STANDARD PRACTICES. - [SDR COMA0110070](https://openairdocs.org/sdr/COMA0110070.md): Frame · gouged · Mar 12, 2001 · N462CA · Emb EMB120RT · Fuselage Main, Frame > DURING 2C CHECK TASK 163-01Z, THE FUSELAGE FRAME 46A WAS FOUND TO BE GOUGED BY AN INTERIOR LINING SCREW AT FLOOR LEVEL ON THE LEFT SIDE. THE FRAME WAS REPAIRED IN ACCORDANCE WITH EMB-120 SRM STANDARD PRACTICES AND AERODESIGN REPORT 2400=5, REV IR, 3-5-01. - [SDR COMA0110069](https://openairdocs.org/sdr/COMA0110069.md): Strap · corroded · Mar 12, 2001 · N462CA · Emb EMB120RT · Fuselage Miscellaneous Structure > DURING 2C CHECK TASK 162-01Z, THE FORWARD RT FLOORBEAM BUTTSTRAP IN THE CARGO COMPARTMENT, WAS FOUND CORRODED. THE PART WAS REPLACED IN ACCORDANCE WITH EMB-120 SRM STANDARD PRACTICES. - [SDR COMA0110068](https://openairdocs.org/sdr/COMA0110068.md): Stringer · cracked · Mar 12, 2001 · N462CA · Emb EMB120RT · Nacelle/Pylon, Longeron/Stringer > DURING 2C CHECK TASK 5410-432-04I, THE LEFT NACELLE OUTBOARD STRINGER NR 1 WAS FOUND TO BE CRACKED JUST AFT OF NACELLE FRAME 10. THE STRINGER WAS REPLACED IN ACCORDANCE WITH EMB-120 SRM STANDARD PRACTICES. - [SDR COMA0110067](https://openairdocs.org/sdr/COMA0110067.md): Strap · corroded · Mar 12, 2001 · N462CA · Emb EMB120RT · Fuselage Miscellaneous Structure > DURING 2C CHECK TASK 142-01Z, THE RT FLOORBEAM BUTTSTRAP WAS FOUND CORRODED. THE PART WAS REPLACED IN ACCORDANCE WITH EMB-120 SRM STANDARD PRACTICES AND AERODESIGN REPORT 2174-1, REV IR, 1-15-97. - [SDR COMA0110066](https://openairdocs.org/sdr/COMA0110066.md): Floorbeam · corroded · Mar 12, 2001 · N462CA · Emb EMB120RT · Fuselage Main, Floor Beam > DURING 2C CHECK TASK 131-01Z, THE FUSELAGE LT FLOORBEAM T-SECTION AT FRAME 16 WAS FOUND CORRODED. THE PART WAS REPLACED IN ACCORDANCE WITH EMB-120 SRM STANDARD PRACTICES. - [SDR COMA0110065](https://openairdocs.org/sdr/COMA0110065.md): Skin · gouged · Mar 12, 2001 · N462CA · Emb EMB120RT · Fuselage Main, Plate/Skin > DURING 2 YEAR CORROSION CHECK TASK 5310-132-CO1E, THE FUSELAGE LOWER SKIN WAS FOUND TO BE GOUGED JUST BELOW THE LAV DUMP VALVE DOUBLER. THE SKIN WAS REPAIRED IN ACCORDANCE WITH EMB-120 SRM STANDARD PRACTICES AND EMBRAER REPAIR FAX GST-0738/01. - [SDR COMA0110064](https://openairdocs.org/sdr/COMA0110064.md): Support · cracked · Mar 12, 2001 · N462CA · Emb EMB120RT · Wing Miscellaneous Structure > DURING 2C CHECK TASK 5720-561-01I, THE LT WING UPPER SUPPORT AT RIB 23, BETWEEN STRINGERS 2A AND 3A, WAS FOUND CRACKED. THE PART WAS REPLACED IN ACCORDANCE WITH EMB-120 SRM STANDARD PRACTICES. - [SDR COMA0110063](https://openairdocs.org/sdr/COMA0110063.md): Support · cracked · Mar 12, 2001 · N462CA · Emb EMB120RT · Fuselage Miscellaneous Structure > DURING 2C CHECK TASK 5310-221-05I, THE LT FUSELAGE SKIN SUPPORT AT FRAME 9, WAS FOUND CRACKED. THE PART WAS REPLACED IN ACCORDANCE WITH EMB-120 SRM STANDARD PRACTICES AND AERODESIGN REPORT 660-1, REV IR, 2-16-93. - [SDR COMA0110062](https://openairdocs.org/sdr/COMA0110062.md): Stiffener · cracked · Mar 12, 2001 · N462CA · Emb EMB120RT · Nacelle/Pylon, Main Frame > DURING 2C CHECK TASK 5410-442-04I, THE RT NACELLE FRAME 10 STIFFENER ANGLE, WAS FOUND CRACKED. THE PART WAS REPLACED IN ACCORDANCE WITH EMB-120 SRM STANDARD PRACTICES. - [SDR COMA0110061](https://openairdocs.org/sdr/COMA0110061.md): Shear Tie · cracked · Mar 12, 2001 · N462CA · Emb EMB120RT · Fuselage Main, Structure > DURING 2C CHECK TASK 5310-222-05I, THE RT FUSELAGE SKIN SUPPORT AT FRAME 9, WAS FOUND CRACKED. THE PART WAS REPLACED IN ACCORDANCE WITH EMB-120 SRM STANDARD PRACTICES AND AERODESIGN REPORT 660-1, REV IR, 2-16-93. - [SDR COMA0110060](https://openairdocs.org/sdr/COMA0110060.md): Support · cracked · Mar 12, 2001 · N462CA · Emb EMB120RT · Wing Miscellaneous Structure > DURING 2C CHECK TASK 5720-561-01I, THE LT WING UPPER SKIN SUPPORT AT RIB 23, BETWEEN STRINGERS 3A AND 4A, WAS FOUND CRACKED. THE PART WAS REPLACED IN ACCORDANCE WITH EMB-120 SRM STANDARD PRACTICES. - [SDR COMA0110059](https://openairdocs.org/sdr/COMA0110059.md): Floor Support · cracked · Mar 12, 2001 · N462CA · Emb EMB120RT · Fuselage Miscellaneous Structure > DURING 2C CHECK TASK 122-01Z, THE FUSELAGE RT FLOOR PROP AT FRAME 13 WAS FOUND CRACKED. THE PART WAS REPAIRED IN ACCORDANCE WITH EMB-120 SRM STANDARD PRACTICES AND AERODESIGN REPORT NR 3647-1, REV IR, 5-3-00. - [SDR COMA0110058](https://openairdocs.org/sdr/COMA0110058.md): Support · cracked · Mar 12, 2001 · N462CA · Emb EMB120RT · Wing Miscellaneous Structure > DURING 2C CHECK TASK 5720-561-01I, THE LT WING UPPER SKIN SUPPORT AT RIB 23, BETWEEN STRINGER 5A AND REAR SPAR, WAS FOUND CRACKED. THE PART WAS REPLACED IN ACCORDANCE WITH EMB-120 SRM STANDARD PRACTICES. - [SDR COMA0110057](https://openairdocs.org/sdr/COMA0110057.md): Support · cracked · Mar 12, 2001 · N462CA · Emb EMB120RT · Wing Miscellaneous Structure > DURING 2C CHECK TASK 5720-522-011, THE LT WING LOWER SKIN SUPPORT AT RIB 8, AND STRINGER 10, WAS FOUND CRACKED. THE PART WAS REPLACED IN ACCORDANCE WITH EMB-120 SRM STANDARD PRACTICES AND AERODESIGN REPORT 3813-1, REV IR, 11-5-00. - [SDR COMA0110056](https://openairdocs.org/sdr/COMA0110056.md): Crossbeam · corroded · Mar 12, 2001 · N462CA · Emb EMB120RT · Fuselage Miscellaneous Structure > DURING 2C CHECK TASK 132-01Z, THE FUSELAGE RT FLOOR CROSSBEAM AT FRAME 16 WAS FOUND CORRODED. THE PART WAS REPLACED IN ACCORDANCE WITH EMB-120 SRM STANDARD PRACTICES. - [SDR COMA0110055](https://openairdocs.org/sdr/COMA0110055.md): Beam · cracked · Mar 12, 2001 · N462CA · Emb EMB120RT · Passenger/Crew Doors > DURING 2C CHECK TASK 811-02Z, THE PAX DOOR AFT LATERAL BEAM WAS FOUND CRACKED. THE PART WAS REPAIRED IN ACCORDANCE WITH EMB-120 SRM 52-10-02, FIGURE 201. - [SDR COMA0110054](https://openairdocs.org/sdr/COMA0110054.md): Floorbeam · corroded · Mar 12, 2001 · N462CA · Emb EMB120RT · Fuselage Main, Floor Beam > DURING 2C CHECK TASK 131/132-01Z, THE FUSELAGE CENTER FORWARD FLOOR OMEGA BEAM WAS FOUND CORRODED. THE PART WAS REPAIRED IN ACCORDANCE WITH EMB-120 STANDARD PRACTICES AND AERODESIGN REPORT 2181-12, REV IR, 3-4-01. - [SDR COMA0110053](https://openairdocs.org/sdr/COMA0110053.md): Strap · corroded · Mar 12, 2001 · N462CA · Emb EMB120RT · Fuselage Miscellaneous Structure > DURING 2C CHECK TASK 132-01Z, THE FUSELAGE RT FORWARD FLOOR BEAM BUTTSTRAP WAS FOUND CORRODED. THE PART WAS REPLACED IN ACCORDANCE WITH EMB-120 SRM STANDARD PRACTICES. - [SDR COMA0110052](https://openairdocs.org/sdr/COMA0110052.md): Sill · corroded · Mar 12, 2001 · N462CA · Emb EMB120RT · Fuselage Miscellaneous Structure > DURING 2C CHECK TASK 131-01Z, THE FUSELAGE LT FORWARD FLOOR BEAM SILL WAS FOUND CORRODED. THE PART WAS REPLACED IN ACCORDANCE WITH EMB-120 SRM STANDARD PRACTICES. - [SDR COMA0110051](https://openairdocs.org/sdr/COMA0110051.md): Sill · corroded · Mar 12, 2001 · N462CA · Emb EMB120RT · Fuselage Miscellaneous Structure > DURING 2C CHECK TASK 132-01Z, THE FUSELAGE RT FORWARD FLOORBEAM SILL WAS FOUND CORRODED. THE PART WAS REPLACED IN ACCORDANCE WITH EMB-120 SRM STANDARD PRACTICES. - [SDR COMA0110050](https://openairdocs.org/sdr/COMA0110050.md): Strap · corroded · Mar 12, 2001 · N462CA · Emb EMB120RT · Fuselage Miscellaneous Structure > DURING 2C CHECK TASK 131/132-01Z, THE FUSELAGE CENTER FORWARD FLOORBEAM BUTTSTRAP WAS FOUND CORRODED. THE PART WAS REPLACED IN ACCORDANCE WITH EMB-120 SRM STANDARD PRACTICES. - [SDR COMA0110048](https://openairdocs.org/sdr/COMA0110048.md): Strap · corroded · Mar 12, 2001 · N462CA · Emb EMB120RT · Fuselage Miscellaneous Structure > DURING 2C CHECK TASK 131-01Z, THE FUSELAGE LT FORWARD FLOORBEAM BUTTSTRAP WAS FOUND CORRODED. THE PART WAS REPLACED IN ACCORDANCE WITH EMB-120 SRM STANDARD PRACTICES. - [SDR COMA0110047](https://openairdocs.org/sdr/COMA0110047.md): Strap · corroded · Mar 12, 2001 · N462CA · Emb EMB120RT · Fuselage Miscellaneous Structure > DURING 2C CHECK TASK 131/132-01Z, THE FUSELAGE CENTER FORWARD FLOORBEAM BUTTSTRAP WAS FOUND CORRODED. THE PART WAS REPLACED IN ACCORDANCE WITH EMB-120 SRM STANDARD PRACTICES AND AERODESIGN REPORT 1671-1, REV A, 1-28-97. - [SDR COMA0110046](https://openairdocs.org/sdr/COMA0110046.md): Channel · cracked · Mar 12, 2001 · N462CA · Emb EMB120RT · Passenger/Crew Doors > DURING 2C CHECK TASK 811-02Z, THE PAX DOOR 3RD U-CHANNEL WAS FOUND CRACKED. THE PART WAS REPLACED IN ACCORDANCE WITH EMB-120 SRM STANDARD PRACTICES. - [SDR COMA0110045](https://openairdocs.org/sdr/COMA0110045.md): Channel · cracked · Mar 12, 2001 · N462CA · Emb EMB120RT · Passenger/Crew Doors > DURING 2C CHECK TASK 811-02Z, THE PAX DOOR AFT U-CHANNEL WAS FOUND CRACKED. THE PART WAS REPLACED IN ACCORDANCE WITH EMB-120 SRM STANDARD PRACTICES. - [SDR COMA0110044](https://openairdocs.org/sdr/COMA0110044.md): Channel · cracked · Mar 12, 2001 · N462CA · Emb EMB120RT · Passenger/Crew Doors > DURING 2C CHECK TASK 811-02Z, THE PAX DOOR 1ST U-CHANNEL WAS FOUND CRACKED. THE PART WAS REPLACED IN ACCORDANCE WITH EMB-120 SRM STANDARD PRACTICES. - [SDR COMA0110003](https://openairdocs.org/sdr/COMA0110003.md): Relay · malfunctioned · Dec 31, 2000 · N462CA · Emb EMB120RT · Landing Gear Retraction/Extension System > LANDING GEAR WILL NOT RETRACT. REPLACED THE LANDING GEAR RELAY BOX. - [SDR COMA0010005](https://openairdocs.org/sdr/COMA0010005.md): Relay · inoperative · Jan 7, 2000 · N462CA · Emb EMB120RT · Emergency Lighting > EMERGENCY LIGHTS WILL NOT ARM. REPLACED RELAY KO201. - [SDR COMA9910100](https://openairdocs.org/sdr/COMA9910100.md): Sign · missing · Jun 24, 1999 · N462CA · Emb EMB120RT · Emergency Lighting > EMERGENCY EXIT SIGN ON BULKHEAD AT CABIN DOOR WAS MISSING. REPLACED EXIT SIGN ASSY. - [SDR COMA9910057](https://openairdocs.org/sdr/COMA9910057.md): Windshield · shattered · Apr 6, 1999 · N462CA · Emb EMB120RT · Flight Compartment Windows > PILOTS WINDSHIELD SHATTERED. REPLACED WINDSHIELD. - [SDR COMA9810181](https://openairdocs.org/sdr/COMA9810181.md): Fuel Line · cracked · Aug 27, 1998 · N462CA · Emb EMB120RT · Aircraft Fuel Distribution System > WHILE REPLACING LEAKING RIVET IN RIGHT OUTBOARD WING, FOUND RE-FUEL LINE (P/N 120-08728-009) CRACKED AT BEND RADIUS. REPLACED CRACKED FUEL LINE. - [SDR COMA0810177](https://openairdocs.org/sdr/COMA0810177.md): Battery · discharged · Aug 15, 1998 · N462CA · Emb EMB120RT · Emergency Lighting > EMERGENCY LIGHTS INOPERABLE. REPLACED BATTERY. - [SDR COMA9810154](https://openairdocs.org/sdr/COMA9810154.md): Lamp · failed · Jul 12, 1998 · N462CA · Emb EMB120RT · Emergency Lighting > THREE EMERGENCY LIGHTS ARE INOP ROW 6 AND 7. REPLACED INOP LAMPS. - [SDR COMA9810135](https://openairdocs.org/sdr/COMA9810135.md): Battery · discharged · Jun 8, 1998 · N462CA · Emb EMB120RT · Emergency Lighting > EMERGENCY LIGHTS AFT OF ROW 6 ARE INOPERABLE. REPLACED EMERGENCY LIGHTS BATTERY. Next page: https://openairdocs.org/deregistered/N462CA-2013-09-03/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 = 'N462CA' AND deregistration_id = 'N462CA-2013-09-03' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/deregistered/N462CA-2013-09-03/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.