# Service difficulty reports: N268CA, cancelled May 11, 2007 A list on [N268CA, cancelled May 11, 2007](https://openairdocs.org/deregistered/N268CA-2007-05-11.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 · 93 reports - [SDR COMA0210025](https://openairdocs.org/sdr/COMA0210025.md): Circuit Breaker · Jun 6, 2002 · N268CA · Emb EMB120RT · Central Warning > FLIGHT 5061 "TRIM" AURAL WARNING DURING T/O.RESET AURAL WARNING CIRCUIT BREAKER - SYSTEM CHECK NORMAL. - [SDR COMA0210021](https://openairdocs.org/sdr/COMA0210021.md): Light · broken · May 21, 2002 · N268CA · Emb EMB120RT · Emergency Lighting > FLIGHT 5063 DURING INSPECTION FOUND EMERGENCY EXIT SIGN AT 5A LOCATION INOPERATIVE.REPLACED THE EMERGENCY LIGHT ASSEMBLY. - [SDR COMA0210017](https://openairdocs.org/sdr/COMA0210017.md): Engine · May 3, 2002 · N268CA · Emb EMB120RT · Engine (Turbine/Turboprop) > FLIGHT 5075 T6 WARNING DURING T/O.COMPLIED WITH COMPRESSOR WASH, ENGINE PERFORMANCE RUNS WERE WITHIN LIMITS. - [SDR COMA0210006](https://openairdocs.org/sdr/COMA0210006.md): Boot · perforated · Feb 16, 2002 · N268CA · Emb EMB120RT · Airfoil Anti/De-ice System > FLIGHT 5059 HORZ STAB AND VERT FIN DEICE FAILED.REPLACED THE VERT STABILIZER DEICE BOOT. - [SDR COMA0110165](https://openairdocs.org/sdr/COMA0110165.md): Roller · worn · Dec 21, 2001 · N268CA · Emb EMB120RT · Trailing Edge Flap Control System > FLIGHT 5061 - FLAP DISAGREEMENT WARNING WHEN FLAPS SELECTED UP.REPLACED THE R/H OUTBD FLAP SECTION ROLLERS. - [SDR COMA0110147](https://openairdocs.org/sdr/COMA0110147.md): Wire · broken · Sep 30, 2001 · N268CA · Emb EMB120RT · Light System Wiring > FLIGHT 5025. OVERHEAD EMERGENCY LIGHT AT ROW 8 IS INOP. REPAIRED BROKEN WIRE AT LIGHT FIXTURE. OPERATIONAL CHECK SATISFACTORY. - [SDR COMA0110151](https://openairdocs.org/sdr/COMA0110151.md): Light · Sep 26, 2001 · N268CA · Emb EMB120RT · Emergency Lighting > FLIGHT #5057. DURING INSPECTION; FOUND THE EMERGENCY EXIT SIGN ON OVERHEAD BIN INOPERATIVE.REPAIRED WIRING AT THE EMERGENCY EXIT SIGN ASSEMBLY. - [SDR COMA0110149](https://openairdocs.org/sdr/COMA0110149.md): Light · Sep 26, 2001 · N268CA · Emb EMB120RT · Emergency Lighting > FLIGHT #5057. DURING INSPECTION; FOUND THE EMERGENCY EXIT SIGN ON OVERHEAD BIN INOPERATIVE.REPAIRED WIRING AT THE EMERGENCY EXIT SIGN ASSEMBLY. - [SDR COMA0110033](https://openairdocs.org/sdr/COMA0110033.md): Shear Tie · cracked · Feb 4, 2001 · N268CA · Emb EMB120RT · Fuselage Main, Structure > DURING 400 FLIGHT CYCLE CHECK, A CRACKED RIVET HEAD WAS DISCOVERED ON THE RIGHT SIDE OF AIRCRAFT FUSELAGE ALONG FRAME 9. UPON FURTHER INVESTIGATION, THE SKIN SUPPORT BRACKET IN WHICH SAID RIVET PASSES THROUGH WAS CRACKED. THE SUPPORT BRACKET WAS REMOVED AND - [SDR COMA0110001](https://openairdocs.org/sdr/COMA0110001.md): Warning System · false activation · Dec 29, 2000 · N268CA · Emb EMB120RT · Brake Anti-Skid Section > "BRAKES" MESSAGE ON MAP AFTER T/O. COULD NOT DUPLICATE. INSPECTED ANTI-SKID SYSTEM, FOUND NO DEFECTS. - [SDR COMA0010436](https://openairdocs.org/sdr/COMA0010436.md): Skin · corroded · Dec 12, 2000 · N268CA · Emb EMB120RT · Fuselage Main, Plate/Skin > UPON COMPLIANCE 2C INSPECTION TASK 191/192 01Z THE LOWER FUSELAGE SKIN WAS FOUND TO BE CORRODED.THE DAMAGED PART WAS REPAIRED I/A/W EMB-120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES AND EMBRAER REPAIR SST-3431/00 - [SDR COMA0010435](https://openairdocs.org/sdr/COMA0010435.md): Frame · cracked · Dec 12, 2000 · N268CA · Emb EMB120RT · Fuselage Main, Frame > UPON COMPLIANCE 2C INSPECTION TASK 163/164 - 01Z THE HALF FRAME 46A WAS FOUND TO BE CRACKED.THE DAMAGED PART WAS REPAIRED I/A/W EMB-120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES AND AERODESIGN REPORT 2400-3. - [SDR COMA0010434](https://openairdocs.org/sdr/COMA0010434.md): Pin · corroded · Dec 12, 2000 · N268CA · Emb EMB120RT · Fuselage Miscellaneous Structure > UPON COMPLIANCE 2C INSPECTION TASK 151-152-01Z THE LOWER ANGLE AND P/N RECEPTACLES AT ROW 8 WAS FOUND TO BE CORRODED.THE DAMAGED PART WAS REPLACED I/A/W EMB-120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES. - [SDR COMA0010433](https://openairdocs.org/sdr/COMA0010433.md): Buttstrap · corroded · Dec 12, 2000 · N268CA · Emb EMB120RT · Fuselage Miscellaneous Structure > UPON COMPLIANCE 2C INSPECTION TASK 131/132 - 01Z THE RH #1 BUTT STRAP WAS FOUND TO BE CORRODED.THE DAMAGED PART WAS REPLACED I/A/W EMB-120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES. - [SDR COMA0010432](https://openairdocs.org/sdr/COMA0010432.md): Buttstrap · corroded · Dec 12, 2000 · N268CA · Emb EMB120RT · Fuselage Miscellaneous Structure > UPON COMPLIANCE 2C INSPECTION TASK 131/132-01Z THE LH #1 BUTTSTRAP WAS FOUND TO BE CORRODED.THE DAMAGED PART WAS REPLACED I/A/W EMB-120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES. - [SDR COMA0010431](https://openairdocs.org/sdr/COMA0010431.md): Buttplate · corroded · Dec 12, 2000 · N268CA · Emb EMB120RT · Fuselage Miscellaneous Structure > UPON COMPLIANCE 2C INSPECTION TASK 131/132-01Z THE CENTER BUTT PLATE WAS FOUND TO BE CORRODED.THE DAMAGED PART WAS REPAIRED I/A/W EMB-120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES AND AERODESIGN REPORT 1671-1. - [SDR COMA0010430](https://openairdocs.org/sdr/COMA0010430.md): Sill · corroded · Dec 12, 2000 · N268CA · Emb EMB120RT · Fuselage Miscellaneous Structure > UPON COMPLIANCE 2C INSPECTION TASK 131/132 - 01Z THE LEFT HAND FORWARD #1 CABIN SILL WAS FOUND TO BE CORRODED.THE DAMAGED PART WAS REPLACED I/A/W EMB-120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES. - [SDR COMA0010429](https://openairdocs.org/sdr/COMA0010429.md): Sill · corroded · Dec 12, 2000 · N268CA · Emb EMB120RT · Fuselage Miscellaneous Structure > UPON COMPLIANCE 2C INSPECTION TASK 131/132-01Z THE RH FWD #1 CABIN SILL WAS FOUND TO BE CORRODED.THE DAMAGED PART WAS REPLACED I/A/W EMB-120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES. - [SDR COMA0010428](https://openairdocs.org/sdr/COMA0010428.md): Shear Tie · cracked · Dec 12, 2000 · N268CA · Emb EMB120RT · Wing, Rib/Bulkhead > UPON COMPLIANCE 2C INSPECTION TASK 5720-651-01I THE RIGHT WING SKIN SUPPORT ON RIB 20 WAS FOUND TO BE CRACKED. THE DAMAGED PART WAS REPPLACED I/A/W EMB-120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES. - [SDR COMA0010420](https://openairdocs.org/sdr/COMA0010420.md): Crossbeam · corroded · Dec 12, 2000 · N268CA · Emb EMB120RT · Fuselage Miscellaneous Structure > UPON COMPLIANCE 2C INSPECTION TASK 151/152 - 01Z THE FRAME 36 CROSSBEAM - RT WAS FOUND TO BE CORRODED.THE DAMAGED PART WAS REPLACED I/A/W EMB-120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES. - [SDR COMA0010427](https://openairdocs.org/sdr/COMA0010427.md): Shear Tie · cracked · Dec 12, 2000 · N268CA · Emb EMB120RT · Fuselage Main, Structure > UPON COMPLIANCE 2C INSPECTION TASK 5310-221/222 - 05I THE SKIN SUPPORT BEHIND DU WINDOW - LEFT WAS FOUND TO BE CRACKED.THE DAMAGED PART WAS REPLACED I/A/W EMB-120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES. - [SDR COMA0010426](https://openairdocs.org/sdr/COMA0010426.md): Floorbeam · cracked · Dec 12, 2000 · N268CA · Emb EMB120RT · Fuselage Main, Floor Beam > UPON COMPLIANCE 2C INSPECTION TASK 5310-121/122 - 01I THE LT AND RT FRAME 13 FLOORBEAMS WERE FOUND TO BE CRACKED. THE DAMAGED PART WAS REPAIRED IAW EMB-120 STRUCTURAL RERPAIR MANUAL STANDARD PRACTICES AND 3647-1. - [SDR COMA0010425](https://openairdocs.org/sdr/COMA0010425.md): Buttstrap · corroded · Dec 12, 2000 · N268CA · Emb EMB120RT · Fuselage Miscellaneous Structure > UPON COMPLIANCE 2C INSPECTION TASK 141/142 - 01Z THE LEFT AND RIGHT NR 2 BUTTSTRAPS WERE FOUND TO BE CORRODED. THE DAMAGED PART WAS REPLACED I/A/W EMB-120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES AND AERODESIGN REPORT 2174-1. - [SDR COMA0010424](https://openairdocs.org/sdr/COMA0010424.md): Buttstrap · corroded · Dec 12, 2000 · N268CA · Emb EMB120RT · Fuselage Miscellaneous Structure > UPON COMPLIANCE 2C INSPECTION TASK 141/142 - 01Z THE RT NR 3 BUTTSTRAP WAS FOUND TO BE CORRODED.THE DAMAGED PART WAS REPLACED I/A/W EMB-120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES AND AERODESIGN REPORT 2174-1. - [SDR COMA0010423](https://openairdocs.org/sdr/COMA0010423.md): Buttstrap · corroded · Dec 12, 2000 · N268CA · Emb EMB120RT · Fuselage Miscellaneous Structure > UPON COMPLIANCE 2C INSPECTION TASK 131/132 01Z THE CENTER #1 BUTT STRAP WAS FOUND TO BE CORRODED.THE DAMAGED PART WAS REPLACED I/A/W EMB-120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES. - [SDR COMA0010422](https://openairdocs.org/sdr/COMA0010422.md): Sill · corroded · Dec 12, 2000 · N268CA · Emb EMB120RT · Fuselage Miscellaneous Structure > UPON COMPLIANCE 2C INSPECTION TASK 161/162 - 01Z THE CARGO BAY FWD SILL WAS FOUND TO BE CORRODED.THE DAMAGED PART WAS REPLACED I/A/W EMB-120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES. - [SDR COMA0010421](https://openairdocs.org/sdr/COMA0010421.md): Crossbeam · corroded · Dec 12, 2000 · N268CA · Emb EMB120RT · Fuselage Main, Frame > UPON COMPLIANCE 2C INSPECTION TASK 151/152 - 01Z THE FRAME 33 RH CROSSBEAM WAS FOUND TO BE CORRODED.THE DAMAGED PART WAS REPLACED I/A/W EMB-120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES. - [SDR COMA0010419](https://openairdocs.org/sdr/COMA0010419.md): Shear Tie · cracked · Dec 12, 2000 · N268CA · Emb EMB120RT · Fuselage Main, Structure > UPON COMPLIANCE 2C INSPECTION TASK 231/232 - 01Z THE FRAME 13A SKIN SUPPORT WAS FOUND TO BE CRACKED. THE DAMAGED PART WAS REPAIRED I/A/W EMB-120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES AND AERODESIGN REPORT 3653-2. - [SDR COMA0010418](https://openairdocs.org/sdr/COMA0010418.md): Stringer · corroded · Dec 12, 2000 · N268CA · Emb EMB120RT · Fuselage Main, Longeron/Stringer > UPON COMPLIANCE 2C INSPECTION TASK 5310-131/132 - CO1I (2 YR CORROSION SK) THE STRINGERS 18L AND 19L WAS FOUND TO BE CORRODED. THE DAMAGED PART WAS REPAIRED I/A/W EMB-120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES AND AERODESIGN REPORT 3841-1. - [SDR COMA0010412](https://openairdocs.org/sdr/COMA0010412.md): Structure · corroded · Dec 12, 2000 · N268CA · Emb EMB120RT · Fuselage Miscellaneous Structure > UPON COMPLIANCE 2C INSPECTION TASK 131/132-01Z THE FRAME 13 Z SECTION WAS FOUND TO BE CORRODED.THE DAMAGED PART WAS REPLACED I/A/W EMB-120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES. - [SDR COMA0010411](https://openairdocs.org/sdr/COMA0010411.md): Buttplate · corroded · Dec 12, 2000 · N268CA · Emb EMB120RT · Fuselage Miscellaneous Structure > UPON COMPLIANCE 2C INSPECTION TASK 131/132-01Z THE LEFT FORWARD BUTTPLATE WAS FOUND TO BE CORRODED.THE DAMAGED PART WAS REPLACED I/A/W EMB-120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES AND AERODESIGN REPORT 1671-2.` - [SDR COMA0010417](https://openairdocs.org/sdr/COMA0010417.md): Crossbeam · corroded · Dec 12, 2000 · N268CA · Emb EMB120RT · Fuselage Main, Frame > UPON COMPLIANCE 2C INSPECTION TASK 141/142 - 01Z THE FRAME 23 RT CROSSBEAM WAS FOUND TO BE CORRODED.THE DAMAGED PART WAS REPLACED I/A/W EMB-120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES. - [SDR COMA0010416](https://openairdocs.org/sdr/COMA0010416.md): Shear Tie · corroded · Dec 12, 2000 · N268CA · Emb EMB120RT · Fuselage Main, Structure > UPON COMPLIANCE 2C INSPECTION TASK 141/142 - 01Z THE FRAME 23 SKIN SUPPORT WAS FOUND TO BE CORRODED.THE DAMAGED PART WAS REPLACED I/A/W EMB-120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES. - [SDR COMA0010415](https://openairdocs.org/sdr/COMA0010415.md): Shear Tie · corroded · Dec 12, 2000 · N268CA · Emb EMB120RT · Fuselage Main, Frame > UPON COMPLIANCE 2C INSPECTION TASK 5310-131/132 - CO1I (2 YR CORROSION TASK) THE SKIN SUPPORT FRAME 19 WAS FOUND TO BE CORRODED. THE DAMAGED PART WAS REPLACED I/A/W EMB-120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES. - [SDR COMA0010414](https://openairdocs.org/sdr/COMA0010414.md): Bracket · cracked · Dec 12, 2000 · N268CA · Emb EMB120RT · Fuselage Miscellaneous Structure > UPON COMPLIANCE 2C INSPECTION TASK 261/262 - 01Z THE CARGO DOOR TRACK BRACKET WAS FOUND TO BE CRACKED.THE DAMAGED PART WAS REPLACED I/A/W EMB-120 STRUCTURAL REAPIR MANUAL STANDARD PRACTICES. - [SDR COMA0010413](https://openairdocs.org/sdr/COMA0010413.md): Seat Track · corroded · Dec 12, 2000 · N268CA · Emb EMB120RT · Fuselage, Seat/Cargo Attach Fittings > UPON COMPLIANCE 2C INSPECTION TASK ZONE 200 THE SEAT TRACKS - ALL WAS FOUND TO BE CORRODED.THE DAMAGED PART WAS REPLACED I/A/W EMB-120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES AND AERODESIGN REPORT 2141. - [SDR COMA0010410](https://openairdocs.org/sdr/COMA0010410.md): Skin · corroded · Dec 12, 2000 · N268CA · Emb EMB120RT · Passenger/Crew Doors > UPON COMPLIANCE 2C INSPECTION TASK 811-02Z THE PAX DOOR INNER SKIN WAS FOUND TO BE CORRODED. THE DAMAGED PART WAS REPAIRED I/A/W EMB-120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES AND AERODESIGN REPORT 3840-1. - [SDR COMA0010409](https://openairdocs.org/sdr/COMA0010409.md): Fitting · corroded · Dec 12, 2000 · N268CA · Emb EMB120RT · Passenger/Crew Doors > UPON COMPLIANCE 2C INSPECTION TASK 811-02Z THE PAX DOOR BOTTOM CHANNEL AND END FITTING WAS FOUND TO BE CORRODED. THE DAMAGED PART WAS REPLACED I/A/W EMB-120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES. - [SDR COMA0010406](https://openairdocs.org/sdr/COMA0010406.md): Battery · discharged · Nov 25, 2000 · N268CA · Emb EMB120RT · Emergency Lighting > EMERGENCY LIGHTS ARE INOPERABLE. REPLACED THE NR 2 EMERGENCY BATTERY. - [SDR COMA0010405](https://openairdocs.org/sdr/COMA0010405.md): Battery · discharged · Nov 22, 2000 · N268CA · Emb EMB120RT · Emergency Lighting > EMERGENY LIGHTS ARE INOPERABLE.REPLACED EMERGENCY BATTERY. - [SDR COMA0010403](https://openairdocs.org/sdr/COMA0010403.md): Light · inoperative · Nov 21, 2000 · N268CA · Emb EMB120RT · Emergency Lighting > EMERGENCY LIGHTS AT ROW 8 ARE INOPERABLE. COULD NOT DUPLICATE. ALL LIGHTS FUNCTION. - [SDR COMA](https://openairdocs.org/sdr/COMA.md): Warning Light · illuminated · Oct 6, 2000 · N268CA · Emb EMB120RT · Engine Indicating System > T6 WARNING DURING T/O. REPLACED THE RIGHT ENGINE. - [SDR COMA0010326](https://openairdocs.org/sdr/COMA0010326.md): Angle · cracked · Aug 31, 2000 · N268CA · Emb EMB120RT · Wing Miscellaneous Structure > DURING A 1C INSPECTION TASK 193-01Z, THE WING TO FUSELAGE FAIRING (193) LOWER ATTACH ANGLE WAS FOUND TO BE CRACKED. THE ANGLE WAS REPLACED WITH A SERVICEABLE ANGLE IAW AERODESIGN REPORT 1226-9. - [SDR COMA0010325](https://openairdocs.org/sdr/COMA0010325.md): Angle · cracked · Aug 31, 2000 · N268CA · Emb EMB120RT · Wing Miscellaneous Structure > DURING A 1C INSPECTION TASK 194-01Z, THE WING TO FUSELAGE FAIRING (194) LOWER ATTACH ANGLE WAS FOUND TO BE CRACKED. THE ANGLE WAS REPLACED WITH A SERVICEABLE ANGLE IAW AERODESIGN REPORT 1226-9. - [SDR COMA0010324](https://openairdocs.org/sdr/COMA0010324.md): Angle · cracked · Aug 31, 2000 · N268CA · Emb EMB120RT · Wing Miscellaneous Structure > DURING A 1C INSPECTION TASK 194-01Z, THE WING TO FUSELAGE FAIRING (194) LOWER ATTCH ANGLE WAS FOUND TO BE CRACKED. THE ANGLE WAS REPLACED WITH A SERVICEABLE ANGLE IAW AERODESIGN REPORT 1226-9. - [SDR COMA0010317](https://openairdocs.org/sdr/COMA0010317.md): Skin · corroded · Aug 11, 2000 · N268CA · Emb EMB120RT · Fuselage Main, Plate/Skin > ON AN OVERNIGHT, MECHANIC NOTICED A BULGE ON EXTERNAL SKIN AT FRAME 21 LOWER RIGHT SIDE. UPON FURTHER INSPECTION, FOUND STRINGER 21R HAD CORROSION BETWEEN FRAME 21 AND FRAME 22 UNDER TCAS ANTENNA INTERNAL DOUBLER. CUT OUT CORRODED SECTION OF FUSELAGE SKIN AT - [SDR COMA0010160](https://openairdocs.org/sdr/COMA0010160.md): Shutoff Valve · malfunctioned · Jun 8, 2000 · N268CA · Emb EMB120RT · Cabin Pressure Control System > CABIN PRESSURE INCREASES AND DECREASES WITH POWER LEVER MOVEMENT. REPLACED THE PRSOV. - [SDR COMA0010063](https://openairdocs.org/sdr/COMA0010063.md): Bulb · failed · May 8, 2000 · N268CA · Emb EMB120RT · Emergency Lighting > AFT, CEILING EMERGENCY LIGHT IS INOPERABLE. REPLACED LIGHT BULB. - [SDR COMA0010057](https://openairdocs.org/sdr/COMA0010057.md): Angle · cracked · Apr 24, 2000 · N268CA · Emb EMB120RT · Fuselage Miscellaneous Structure > WHILE PERFORMING OTHER MAINTENANCE TO THE PASSENGER DOOR, THE FUSELAGE ENTRY WAY DOOR SILL ANGLE WAS FOUND CRACKED. THE ANGLE WAS REPLACED PER EMB 120 SRM STANDARD PRACTICES. - [SDR COMA0010056](https://openairdocs.org/sdr/COMA0010056.md): Angle · corroded · Apr 24, 2000 · N268CA · Emb EMB120RT · Fuselage Miscellaneous Structure > WHILE REPLACING THE FUSELAGE PASSENGER DOOR ENTRYWAY LOWER SILL ANGLE, THE SUPPORT ANGLE UNDERNEATH WAS FOUND SEVERELY CORRODED. THE ANGLE WAS REPLACED PER EMB120 SRM STANDARD PRACTICES. Next page: https://openairdocs.org/deregistered/N268CA-2007-05-11/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 = 'N268CA' AND deregistration_id = 'N268CA-2007-05-11' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/deregistered/N268CA-2007-05-11/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.