N582CA

Service difficulty reports · 174

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 = 'N582CA' AND registry_match = 'registration'
  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 ASOA2014050110447Seat Track · corrodedLT SIDE SEAT TRACK AT FS 785.15 CORRODED. BLENDED CORROSION AND FOUND TO BE OUT OF LIMITS IAW REO 670-53-00-013 AND SRM 51-21-06. REMOVED AND INSTALLED NEW SEAT TRACK FROM BS 784 - 847 IAW AMM 53-00-49-000-801-A07 AND 53-00-49-400-801-A07.Apr 8, 2014 · N582CA · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA2014050110446Seat Track · corrodedRT SIDE SEAT TRACK CORRODED AT FS 785.15. REMOVED SEAT TRACK FROM BS 784 - 847 IAW AMM 53-00-49-000-801-A07. INSTALLED SEAT TRACK IAW AMM 53-00-49-400-801.Apr 8, 2014 · N582CA · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA2014050110445Seat Track · corrodedRT SIDE SEAT TRACK CORRODED AT BS 761.85. R & R SEAT TRACK IAW AMM 53-00-49-400-801 AND REO 670-53-00-013.Apr 8, 2014 · N582CA · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA2014050110444Seat Track · corrodedRT SIDE SEAT TRACK CORRODED AT BS 720.85. R & R SEAT TRACK IAW AMM 53-00-49-000-801 AND 53-00-49-400-801 AND REO 670-53-00-013.Apr 8, 2014 · N582CA · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA2014050110443Seat Track · corrodedLT SIDE SEAT TRACK CORRODED AT BS 720.85. R & R SEAT TRACK IAW AMM 53-00-49-000-801 & 53-00-49-400-801 AND REO 670-53-00-013.Apr 8, 2014 · N582CA · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA2014050110442Skin · gougedSKIN DAMAGED AT BS 942. COMPLIED WITH REO 670-53-00-290 AND EC/TC REO 670-53-00-290. MAJOR REPAIR.Apr 7, 2014 · N582CA · Cndair CL6002D24 · Fuselage Main, Plate/SkinSDR ASOA2014050110441Web · crackedFLOOR WEB CRACKED AT ADG STOW PUMP. COMPLIED WITH REO 670-53-11-509.Apr 5, 2014 · N582CA · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR ASOA2014050110440Fairing · damagedTHRUST REVERSER UPPER HINGE LINE FAIRING 443BT, RT ENGINE, HAS A GOUGE AND IS CRACKED. REMOVED UPPER THRUST REVERSER HINGE LINE FAIRING 443BT ON RT ENGINE IAW AMM 54-12-01-000-802-A02. THIS REPAIR IS CLASSIFIED AS A REPAIR IAW SOP 5702. CRACK AND GOUGE IS OUApr 5, 2014 · N582CA · Cndair CL6002D24 · Engine Thrust ReverserSDR ASOA2013091108983Light · inoperativePAX DOOR EMERGENCY LIGHT AT FWD SIDE OF ENTRANCE HAS SEVERAL LIGHTS OUT. REPAIRED.Sep 7, 2013 · N582CA · Cndair CL6002D24 · Emergency LightingSDR ASOA2013091008980Lamp · inoperativePAX DOOR EMERGENCY LIGHT AT FWD SIDE OF ENTRANCE HAS SEVERAL LIGHTS OUT. REPLACED LAMPS IAW GMM 3-8-9. OPS CHECKED IAW 33-51-00-710-802. OPS NORMAL.Sep 6, 2013 · N582CA · Cndair CL6002D24 · Emergency LightingSDR ASOA2013071708689Skin · damagedLEFT SLAT T/E DAMAGED SS 142.25. REPAIRED IAW REO 670-57-41-254. MAJOR REPAIR IAW GMM 5-3.Jul 13, 2013 · N582CA · Cndair CL6002D24 · Leading Edge DevicesSDR ASOA2013071608685Skin · damagedLEFT SLAT AND L/E DAMAGED AT SS 142.25 AND WS144.95. REPAIRED IAW SRM 51-13-01 AND REO 670-57-41-109. MAJOR REPAIR IAW GMM 5-3.Jul 12, 2013 · N582CA · Cndair CL6002D24 · Leading Edge DevicesSDR ASOA2013032903272Light · damagedEMERGENCY LIGHT AT SEAT 13B IS DAMAGED. SECURED EMERGENCY LIGHT AT 13B IAW AMM 33-51-01. NO FURTHER DEFECTS NOTED. ACFT OK FOR SERVICE.Mar 25, 2013 · N582CA · Cndair CL6002D24 · Emergency LightingSDR COMA2012091890020Slat System · malfunctionedON APPROACH INTO MSP RECEIVED SLAT FAIL CAUTION MSG. EMERGENCY DECLARED, A/C LANDED SAFELY. RESET SLAT CONTROL SYSTEM AND CLEARED INHIBITS IN MDC. PERFORMED OPS CHECK OF SLATS, OPS CHECK GOOD.Sep 18, 2012 · N582CA · Cndair CL6002D24 · Leading Edge Slat Control SystemSDR COMA2012062790012Skin · dentedFUSELAGE SKIN DENTED AND PUNCTURED ABOVE AND AFT OF AFT LAV SERVICE PANEL. CUT OUT DAMAGED SKIN AND INSTALLED A DOUBLER IAW BOMBARDIER REO 690-53-61-269.Jun 20, 2012 · N582CA · Cndair CL6002D24 · Fuselage Main, Plate/SkinSDR COMA2012042390008Warning System · false activationON APPROACH INTO MSP RECEIVED SLAT FAIL MSG, PREFORMED QRH. EMERGENCY DECLARED, A/C LANDED SAFELY. INSPECTED SLATS, NO DEFECTS FOUND. PERFORMED ELECTRICAL RIGGING OF SLAT SYSTEM, CLEARED INHIBITS OF BOTH CHANNELS, PERFORMED SFECU SELF TEST, NO DEFECTS. OPSApr 21, 2012 · N582CA · Cndair CL6002D24 · Leading Edge Slat Position Indicating SystemSDR COMA2012031290006Warning System · false activationON DESCENT INTO BHM RECEIVED SLAT FAIL CAUTION MSG. EMERGENCY DECLARED, A/C LANDED SAFELY IN BHM. CLEARED INHIBITS FOR SLAT CH 1 AND CH 2. OPS CHECK GOOD.Mar 9, 2012 · N582CA · Cndair CL6002D24 · Leading Edge Slat Position Indicating SystemSDR COMA2012022790005Skin · dentedFUSELAGE SKIN DENTED ABOVE FWD LAV SERVICE DOOR. CUT OUT DAMAGED SKIN AND INSTALLED A DOUBLER IAW BOMBARDIER REO 690-53-21-338.Feb 25, 2012 · N582CA · Cndair CL6002D24 · Fuselage Main, Plate/SkinSDR COMA2012022390004Sill · corrodedRIGHT SIDE FLOOR SILL, FS 280.00 TO 319.70 CORRODED BEYOND ALLOWABLE LIMITS. INSTALLED NEW SILL IAW SRM 51-42-06, 51-42-13,51-42-20.Feb 22, 2012 · N582CA · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR COMA2010073090007Controller · intermittentON CLIMBOUT FROM DTW RECEIVED BLEED AIR DUCT WARNING MSG. EMERGENCY DECLARED, A/C RETURNED TO DTW LANDED SAFELY. REMOVED AND REPLACED ANTI-ICE LEAK CONTROLLER.Jul 29, 2010 · N582CA · Cndair CL6002D24 · Pneumatic Distribution SystemSDR COMA2010051790002Engine · vibrationON CLIMBOUT FROM RDU LEFT ENGINE FAN VIB AT 2.6. EMERGENCY DECLARED, A/C DIVERTED TO GSO LANDED SAFELY. TRANSFERRED TO DEFERRED LIST PER MEL GMM 5-2 CAT 1.May 14, 2010 · N582CA · Cndair CL6002D24 · Engine (Turbine/Turboprop)SDR COMA2010020150029Bulkhead · crackedAFT PRESSURE BULKHEAD CRACKED AT FS 621.00 LBL 27.50 ABOVE CARGO DOOR TRACK. REPAIRED AFT PRESSURE BULKHEAD FS 621.00 LBL 27.50 IAW REO 601R-53-61-1541.Jan 30, 2010 · N582CA · Cndair CL6002B19 · Fuselage Main, BulkheadSDR COMA2009011190004Slat System · malfunctionedON APPROACH, RECEIVED SLAT FAIL CAUTION MSG. QRH PROCEDURES ACCOMPLISHED, EMERGENCY DECLARED. FLAPS EXTENDED ACFT LANDED SAFELY. RESET SSCU AND SLAT SYS, OPS CHECK GOOD. NO DEFECTS NOTED.Jan 11, 2009 · N582CA · Cndair CL6002D24 · Leading Edge Slat Control SystemSDR COMA2009010590003Computer · malfunctionedON APPROACH, RECEIVED SLATS FAIL CAUTION MSG AP ON CONFIGURING THE ACFT FOR LANDING. FOLLOWED QRH, EMERGENCY DECLARED. ACFT LANDED SAFELY WITH FUNCTIONAL FLAPS. CLEARED SLAT FAULTS FROM MDC, PERFORMED OPS CHECK OF SLAT SYSTEM, NO DEFECTS NOTED.Jan 3, 2009 · N582CA · Cndair CL6002D24 · Leading Edge Slat Control System
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