N268CA, cancelled May 11, 2007

Service difficulty reports · 93

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.

Query with SQL
duckdb -csv -c "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"

Prints the whole list as CSV. It reads the release’s Parquet files over HTTPS, so there’s nothing to download first. Install DuckDB to run it.

SDR COMA0210025Circuit BreakerFLIGHT 5061 "TRIM" AURAL WARNING DURING T/O.RESET AURAL WARNING CIRCUIT BREAKER - SYSTEM CHECK NORMAL.Jun 6, 2002 · N268CA · Emb EMB120RT · Central WarningSDR COMA0210021Light · brokenFLIGHT 5063 DURING INSPECTION FOUND EMERGENCY EXIT SIGN AT 5A LOCATION INOPERATIVE.REPLACED THE EMERGENCY LIGHT ASSEMBLY.May 21, 2002 · N268CA · Emb EMB120RT · Emergency LightingSDR COMA0210017EngineFLIGHT 5075 T6 WARNING DURING T/O.COMPLIED WITH COMPRESSOR WASH, ENGINE PERFORMANCE RUNS WERE WITHIN LIMITS.May 3, 2002 · N268CA · Emb EMB120RT · Engine (Turbine/Turboprop)SDR COMA0210006Boot · perforatedFLIGHT 5059 HORZ STAB AND VERT FIN DEICE FAILED.REPLACED THE VERT STABILIZER DEICE BOOT.Feb 16, 2002 · N268CA · Emb EMB120RT · Airfoil Anti/De-ice SystemSDR COMA0110165Roller · wornFLIGHT 5061 - FLAP DISAGREEMENT WARNING WHEN FLAPS SELECTED UP.REPLACED THE R/H OUTBD FLAP SECTION ROLLERS.Dec 21, 2001 · N268CA · Emb EMB120RT · Trailing Edge Flap Control SystemSDR COMA0110147Wire · brokenFLIGHT 5025. OVERHEAD EMERGENCY LIGHT AT ROW 8 IS INOP. REPAIRED BROKEN WIRE AT LIGHT FIXTURE. OPERATIONAL CHECK SATISFACTORY.Sep 30, 2001 · N268CA · Emb EMB120RT · Light System WiringSDR COMA0110151LightFLIGHT #5057. DURING INSPECTION; FOUND THE EMERGENCY EXIT SIGN ON OVERHEAD BIN INOPERATIVE.REPAIRED WIRING AT THE EMERGENCY EXIT SIGN ASSEMBLY.Sep 26, 2001 · N268CA · Emb EMB120RT · Emergency LightingSDR COMA0110149LightFLIGHT #5057. DURING INSPECTION; FOUND THE EMERGENCY EXIT SIGN ON OVERHEAD BIN INOPERATIVE.REPAIRED WIRING AT THE EMERGENCY EXIT SIGN ASSEMBLY.Sep 26, 2001 · N268CA · Emb EMB120RT · Emergency LightingSDR COMA0110033Shear Tie · crackedDURING 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 Feb 4, 2001 · N268CA · Emb EMB120RT · Fuselage Main, StructureSDR COMA0110001Warning System · false activation"BRAKES" MESSAGE ON MAP AFTER T/O. COULD NOT DUPLICATE. INSPECTED ANTI-SKID SYSTEM, FOUND NO DEFECTS.Dec 29, 2000 · N268CA · Emb EMB120RT · Brake Anti-Skid SectionSDR COMA0010436Skin · corrodedUPON 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-3431/00Dec 12, 2000 · N268CA · Emb EMB120RT · Fuselage Main, Plate/SkinSDR COMA0010435Frame · crackedUPON 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.Dec 12, 2000 · N268CA · Emb EMB120RT · Fuselage Main, FrameSDR COMA0010434Pin · corrodedUPON 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.Dec 12, 2000 · N268CA · Emb EMB120RT · Fuselage Miscellaneous StructureSDR COMA0010433Buttstrap · corrodedUPON 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.Dec 12, 2000 · N268CA · Emb EMB120RT · Fuselage Miscellaneous StructureSDR COMA0010432Buttstrap · corrodedUPON 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.Dec 12, 2000 · N268CA · Emb EMB120RT · Fuselage Miscellaneous StructureSDR COMA0010431Buttplate · corrodedUPON 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.Dec 12, 2000 · N268CA · Emb EMB120RT · Fuselage Miscellaneous StructureSDR COMA0010430Sill · corrodedUPON 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.Dec 12, 2000 · N268CA · Emb EMB120RT · Fuselage Miscellaneous StructureSDR COMA0010429Sill · corrodedUPON 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.Dec 12, 2000 · N268CA · Emb EMB120RT · Fuselage Miscellaneous StructureSDR COMA0010428Shear Tie · crackedUPON 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.Dec 12, 2000 · N268CA · Emb EMB120RT · Wing, Rib/BulkheadSDR COMA0010420Crossbeam · corrodedUPON 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.Dec 12, 2000 · N268CA · Emb EMB120RT · Fuselage Miscellaneous StructureSDR COMA0010427Shear Tie · crackedUPON 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.Dec 12, 2000 · N268CA · Emb EMB120RT · Fuselage Main, StructureSDR COMA0010426Floorbeam · crackedUPON 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.Dec 12, 2000 · N268CA · Emb EMB120RT · Fuselage Main, Floor BeamSDR COMA0010425Buttstrap · corrodedUPON 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.Dec 12, 2000 · N268CA · Emb EMB120RT · Fuselage Miscellaneous StructureSDR COMA0010424Buttstrap · corrodedUPON 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.Dec 12, 2000 · N268CA · Emb EMB120RT · Fuselage Miscellaneous StructureSDR COMA0010423Buttstrap · corrodedUPON 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.Dec 12, 2000 · N268CA · Emb EMB120RT · Fuselage Miscellaneous StructureSDR COMA0010422Sill · corrodedUPON 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.Dec 12, 2000 · N268CA · Emb EMB120RT · Fuselage Miscellaneous StructureSDR COMA0010421Crossbeam · corrodedUPON 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.Dec 12, 2000 · N268CA · Emb EMB120RT · Fuselage Main, FrameSDR COMA0010419Shear Tie · crackedUPON 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.Dec 12, 2000 · N268CA · Emb EMB120RT · Fuselage Main, StructureSDR COMA0010418Stringer · corrodedUPON 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.Dec 12, 2000 · N268CA · Emb EMB120RT · Fuselage Main, Longeron/StringerSDR COMA0010412Structure · corrodedUPON 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.Dec 12, 2000 · N268CA · Emb EMB120RT · Fuselage Miscellaneous StructureSDR COMA0010411Buttplate · corrodedUPON 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.`Dec 12, 2000 · N268CA · Emb EMB120RT · Fuselage Miscellaneous StructureSDR COMA0010417Crossbeam · corrodedUPON 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.Dec 12, 2000 · N268CA · Emb EMB120RT · Fuselage Main, FrameSDR COMA0010416Shear Tie · corrodedUPON 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.Dec 12, 2000 · N268CA · Emb EMB120RT · Fuselage Main, StructureSDR COMA0010415Shear Tie · corrodedUPON 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.Dec 12, 2000 · N268CA · Emb EMB120RT · Fuselage Main, FrameSDR COMA0010414Bracket · crackedUPON 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.Dec 12, 2000 · N268CA · Emb EMB120RT · Fuselage Miscellaneous StructureSDR COMA0010413Seat Track · corrodedUPON 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.Dec 12, 2000 · N268CA · Emb EMB120RT · Fuselage, Seat/Cargo Attach FittingsSDR COMA0010410Skin · corrodedUPON 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.Dec 12, 2000 · N268CA · Emb EMB120RT · Passenger/Crew DoorsSDR COMA0010409Fitting · corrodedUPON 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.Dec 12, 2000 · N268CA · Emb EMB120RT · Passenger/Crew DoorsSDR COMA0010406Battery · dischargedEMERGENCY LIGHTS ARE INOPERABLE. REPLACED THE NR 2 EMERGENCY BATTERY.Nov 25, 2000 · N268CA · Emb EMB120RT · Emergency LightingSDR COMA0010405Battery · dischargedEMERGENY LIGHTS ARE INOPERABLE.REPLACED EMERGENCY BATTERY.Nov 22, 2000 · N268CA · Emb EMB120RT · Emergency LightingSDR COMA0010403Light · inoperativeEMERGENCY LIGHTS AT ROW 8 ARE INOPERABLE. COULD NOT DUPLICATE. ALL LIGHTS FUNCTION.Nov 21, 2000 · N268CA · Emb EMB120RT · Emergency LightingSDR COMAWarning Light · illuminatedT6 WARNING DURING T/O. REPLACED THE RIGHT ENGINE.Oct 6, 2000 · N268CA · Emb EMB120RT · Engine Indicating SystemSDR COMA0010326Angle · crackedDURING 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.Aug 31, 2000 · N268CA · Emb EMB120RT · Wing Miscellaneous StructureSDR COMA0010325Angle · crackedDURING 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.Aug 31, 2000 · N268CA · Emb EMB120RT · Wing Miscellaneous StructureSDR COMA0010324Angle · crackedDURING 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.Aug 31, 2000 · N268CA · Emb EMB120RT · Wing Miscellaneous StructureSDR COMA0010317Skin · corrodedON 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 ATAug 11, 2000 · N268CA · Emb EMB120RT · Fuselage Main, Plate/SkinSDR COMA0010160Shutoff Valve · malfunctionedCABIN PRESSURE INCREASES AND DECREASES WITH POWER LEVER MOVEMENT. REPLACED THE PRSOV.Jun 8, 2000 · N268CA · Emb EMB120RT · Cabin Pressure Control SystemSDR COMA0010063Bulb · failedAFT, CEILING EMERGENCY LIGHT IS INOPERABLE. REPLACED LIGHT BULB.May 8, 2000 · N268CA · Emb EMB120RT · Emergency LightingSDR COMA0010057Angle · crackedWHILE 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.Apr 24, 2000 · N268CA · Emb EMB120RT · Fuselage Miscellaneous StructureSDR COMA0010056Angle · corrodedWHILE 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.Apr 24, 2000 · N268CA · Emb EMB120RT · Fuselage Miscellaneous Structure
Back to N268CA, cancelled May 11, 2007