N528CA, cancelled Jun 26, 2019

Service difficulty reports · 46

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 = 'N528CA' AND deregistration_id = 'N528CA-2019-06-26'
  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 ASOA20161206247Battery Pack · corrodedEMERGENCY LIGHTS OUT IN GALLEY AND MID CABIN. REMOVED AND REPLACED BATTERY PACK ASSY PER AMM 33-51-04. OPS CHECKED GOOD, NO FURTHER DEFECTS NOTED.Dec 6, 2016 · N528CA · Cndair CL6002D24 · Emergency LightingSDR ASOA2014041810381Lamp · burned outFWD ORANGE SEGMENT OF EMERGENCY FLOOR PATH LIGHTS INOPERATIVE. R & R EMERGENCY FLOOR PATH LIGHT FLEXIBLE LAMP NR 1 IAW AMM 33-51-01. OPS CHECK GOOD. SDR CLOSED.Apr 17, 2014 · N528CA · Cndair CL6002B19 · Emergency LightingSDR ASOA2014031010107Light · inoperativeCABIN FLOOR FORWARD MOST EMERGENCY LIGHT STRIP, ORANGE, INOPERATIVE. PERFORMED THE OPS TEST OF THE EMERGENCY FLOOD LIGHTS IAW AMM 33-51-00. OPS CHK GOOD.Mar 6, 2014 · N528CA · Cndair CL6002B19 · Emergency LightingSDR ASOA2013090608962Connector · disconnectedEMERGENCY LIGHT STRIP ABOVE PAX DOOR DOES NOT ILLUMINATE. REINSTALLED CONNECTOR FOR EMERGENCY EXIT SIGN IAW AMM 33-51-01.Sep 3, 2013 · N528CA · Cndair CL6002B19 · Light System WiringSDR ASOA2013050603474Battery Pack · dischargedEMERGENCY LIGHT AT ROW 5 INOPERATIVE. FOUND BATTERY PACK TO BE DISCHARGED. CHARGED BATTERY PACK. OPS CHECKED GOOD IAW AMM 33-51-00.Apr 30, 2013 · N528CA · Cndair CL6002B19 · Emergency LightingSDR ASOA2013050303472Skin · damagedRT OTBD FLAP DAMAGED ON T/E. 41" FROM INBD END, DAMAGE IS APPROX 10" L. COMPLIED WITH MAJOR REPAIR IAW REO 601R-57-53-041, REV A, DATED 2004/05/07. COMPLIED WITH EC/TC EO 600-57-0128 02.Apr 22, 2013 · N528CA · Cndair CL6002B19 · Trailing Edge FlapsSDR ASOA2013050303471Floor Panel · dentedPRESSURE FLOOR SKIN HAS 1 EA DENT MEASURING 4.256" LONG X 1.980" WIDE X .015" DEEP AND HAS 5 EA GOUGES WITH MAX DAMAGE BEING .730" LONG X .062" WIDE X .008" DEEP WITH HIGH METAL AT FS 553 BETWEEN LBL 0 AND LBL 9 AND IS NOT WITHIN REPAIRABLE LIMITS IAW SRM 53-4Apr 8, 2013 · N528CA · Cndair CL6002B19 · Fuselage Floor PanelSDR ASOA2013050303470Bulkhead · damagedAT FS 621.00 BULKHEAD LBL 30 WL 135 THERE IS A DRILL START .150" WIDE .031" DEEP AND .150" FROM CENTER OF FIRE BLOCK HOLE/NUTPLATE AT .1562" TO CENTER OF DRILL START. COMPLIED WITH MAJOR REPAIR IAW REO 601R-53-61-4873, DATED 2013/04/11. COMPLIED WITH EC/TC REApr 8, 2013 · N528CA · Cndair CL6002B19 · Fuselage Main, BulkheadSDR ASOA2013050203469Bushing · damagedLT BUSHINGS AT HORIZONTAL STAB HINGE ARE DAMAGED. REPAIRED IAW REO 601R-55-00-045 REV B, 2013/04/27. MAJOR REPAIRApr 6, 2013 · N528CA · Cndair CL6002B19 · Horizontal Stabilizer StructureSDR ASOA2013042503445Intercostal · crackedFS 621.00 CRACKED INTERCOSTAL STRINGER 13L,. REMOVED CRACKED INTERCOSTAL IAW SRM 51-42-21. LOCATED & DRILLED NEW INTERCOSTAL IAW SRM 51-40-11. INSTALLED INTERCOSTAL IAW SRM 51-42-21.Apr 5, 2013 · N528CA · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA2013042503444Bulkhead · crackedFOUND REAR PRESSURE BULKHEAD WEB HAS INDICATION NOTED AT LBL 27.50 WL 130 APPROX .2" IN LENGTH 60 PERCENT FSH FAILED NDT INSPECTION. REPAIRED IAW REO 601R-53-61-1541.Apr 4, 2013 · N528CA · Cndair CL6002B19 · Fuselage Main, BulkheadSDR ASOA2013042503443Bulkhead · crackedFOUND FS 559 BULKHEAD WEB RT SIDE HAS INDICATION NOTED APPROX .3" IN LENGTH 50 PERCENT FSH AT WL 59.10 INBD OF RBL 18.0. FAILED NDT INSPECTION. REPAIRED IAW REO 601R-53-41-260 AND REO 601R-53-41-260, REV E, DATED: 08/24/2010, REO 601R-53-41-609, REO 601R-53-Apr 3, 2013 · N528CA · Cndair CL6002B19 · Fuselage Main, BulkheadSDR ASOA2013042503442Post · crackedFOUND FS 409.00+128 VERTICAL POST BL 0.00 RT SIDE HAS INDICATION NOTED AT AFT FLANGE RADIUS WL 69.0 APPROX .2" IN LENGTH 50 PERCENT FSH. FAILED NDT INSPECTION. REPAIRED LT & RT POST BL 0 FS 409+128 IAW SRM 51-42-06 & REO 601R-53-41-889.Apr 3, 2013 · N528CA · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA2013020702965Circuit Card · unserviceableUNCOMMANDED FULL RT RUDDER DEFECTION IN FLT ON A/P, NO EICAS MSG OVER POWERED, DISCONNECTED A/P AND YD, WERE ABLE TO RETRIM (ENROUTE, ACFT DIVERTED TO GSO DUE TO MX) R & R NR 1 AND NR 2 FCC CARDS IAW AMM 22-12-14 , OPS CHECK GOOD IAW AMM 22-12-14 IOC REF 22-Feb 3, 2013 · N528CA · Cndair CL6002B19 · Rudder Control SystemSDR ASOA2012081702076Switch · illuminatedLEFT THRUST REVERSER UNLOCK MESSAGE. EMERGENCY DECLARED. R & R STOW SWITCH IAW AMM 78-37-01. OPS CHECKED GOOD.Aug 13, 2012 · N528CA · Cndair CL6002B19 · Engine Thrust ReverserSDR ASOA201201674Sensing Element · brokenLT 10TH DUCT IN FLIGHT FOLLOWED CHECK LIST IT DID NOT GO OUT. DELCARED EMERGENCY AND RETURNED TO ATC (AFTER T/O ACFT RETURNED TO DEPARTURE AFTER T/O -- EMERGENCY DECLARED AS A PRECAUTION) FOUND SENSING ELEMENT A48WK BROKEN. R & R SENSING ELEMENT A48WK IAW AMay 22, 2012 · N528CA · Cndair CL6002B19 · Overheat DetectionSDR ASOA201201237Fitting · crackedREAR PRESSURE BULKHEAD CRACKED AT MACHINE FITTING (LINTEL FITTING) AT CARGO DOOR CUTOUT. REPAIRED IAW REO 601R-53-61-1230, REV C.Apr 9, 2012 · N528CA · Cndair CL6002B19 · Fuselage Main, Attach FittingsSDR ASOA201201235Pressure Blkhd · crackedREAR PRESSURE BULKHEAD CRACKED AT RBL 36.20. REPAIRED IAW REO 601R-53-61-1285, REV D AND REO 601R-53-61-1285 REV D.Apr 9, 2012 · N528CA · Cndair CL6002B19 · Fuselage Main, BulkheadSDR ASOA201201219Wire · brokenWIRE BROKEN ON EMERGENCY FLOOR TRACK LIGHTING AT FWD END. REPLACED CRIMP CONNECTOR ON RT FWD EMERGENCY LIGHT FLOOR STRIP LIGHTING WIRE IAW ESPM 20-17-00. OPS TESTED IAW AMM 33-51-00-710-801. OPS CHECKED GOOD.Apr 6, 2012 · N528CA · Cndair CL6002B19 · Light System WiringSDR ASOA201101683Connector · damagedEMERGENCY LIGHTS INOPERATIVE, CENTER TWO SECTIONS AND FWD WHITE SECTION AT FLOOR POSITIONS. R & R FWD WHITE EMERG LIGHT SECTION IAW AMM 33-51-01-000-801 AND 33-51-01-400-801. FOUND 2 SETS OF CONNECTORS (MALE/FEMALE) NOT TERMINATED ON LIGHT STRIP INSTALLEDSep 9, 2011 · N528CA · Cndair CL6002B19 · Light System WiringSDR ASOA201101559Attach Fitting · crackedCLIP AT FS 484.00, RBL 27 CRACKED. R & R A NEW CLIP AT FS 484.00, RBL 27 IAW SRM 51-42-21. THIS REPAIR IS CLASSIFIED AS A MINOR REPAIR.Aug 22, 2011 · N528CA · Cndair CL6002B19 · Fuselage Main, Attach FittingsSDR ASOA201101558Beam · crackedFS 280 TRANSVERSE BEAM CRACKED IN WEB OTBD OF RBL 9. THIS DISCREPANCY AND THE AFT J-ANGLES ON JOB 8784121, OP 159 IS BEING REPAIRED AS ONE IAW REO 601R-53-11-926.Aug 22, 2011 · N528CA · Cndair CL6002B19 · Fuselage Main, StructureSDR ASOA201101557Floorbeam · crackedFS 280 TRANVERSE BEAM UPPER AFT J-ANGLE CRACKED OTBD OF LBL 9 AND RBL 9. REPAIRED IAW REO 601R-53-11-926 REV B.Aug 22, 2011 · N528CA · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR ASOA201101556Angle · corrodedPASSENGER DOOR CUTOUT LOWER ANGLE HAS CORROSION AROUND HOLE FOR PROXIMITY SENSOR. REMOVED CORROSION IAW SRM 51-21-06 AND FOUND THE REMOVED MATERIAL (0.003) WITHIN THE LIMIT IAW SRM 53-00-00 AND SRM 53-21-023.Aug 22, 2011 · N528CA · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA201101555Angle · crackedCARGO DOOR FWD TRACK LOWER C-CHANNEL ANGLE CRACKED. R & R DAMAGED C-CHANNEL IAW SRM 51-41-06 & 51-41-04. REPAIR IS CLASSIFIED AS A MINOR REPAIR.Aug 22, 2011 · N528CA · Cndair CL6002B19 · Cargo/Baggage DoorsSDR ASOA201101554Drag Angle · crackedPASSENGER DOOR AFT DRAG ANGLE CRACKED. REPAIRE IAW REO 601R-52-11-513 AND REO NR 610R-52-11-513, REV A.Aug 22, 2011 · N528CA · Cndair CL6002B19 · Passenger/Crew DoorsSDR ASOA201101553Web · crackedPASSENGER DOOR FWD WEB CRACKED AT 4TH RISER. REPAIRED IAW REO 601R-52-11-702.Aug 22, 2011 · N528CA · Cndair CL6002B19 · Passenger/Crew DoorsSDR ASOA201101522Door · noneLEFT EMERGENCY OVERWING EXIT FAILS FUNCTION TEST, FORCE TO OPERATE HANDLE EXCEEDS 40 LBS. PERFORMED FUNCT TEST OF THE LT EMERGENCY EXIT IAW AMM 52-21-00-720-801. FUNCTION TEST GOOD AT 35LBS.Aug 17, 2011 · N528CA · Cndair CL6002B19 · Emergency ExitsSDR ASOA201101072Attach Fitting · crackedFS 625, OBLIQUE CLIP IS CRACKED. REMOVED CLIP IAW SRM 51-42-20. COMPLIED WITH EDDY CURENT INSP IAW NDTM 51-20-06, PART 1 53-00-096, PART 6 AND COMFIRMED CRACK. INSTALLED NEW CLIP IAW REO 601R-53-61-100 AND REO 601R-53-61-422.May 27, 2011 · N528CA · Cndair CL6002B19 · Fuselage Main, Attach FittingsSDR ASOA201101071Doubler · crackedLT SIDE FS 640.00 DOUBLER CRACKED AT CUTOUT RADIUS FOR ENGINE SUPPORT BEAM ATTACH POINT. REPAIRED.May 27, 2011 · N528CA · Cndair CL6002B19 · Fuselage Main, StructureSDR REXA201100128Warning System · activatedGEAR DISAGREE NOSE DOOR WARNING NOSE GEAR NEVER CAME UP DEFERRED PER MEL 32-30-01.Feb 16, 2011 · N528CA · Cndair CL6002B19 · Landing Gear Position and WarningSDR REXA201000234Connector · dirtyDURING CLIMB, PASSING 27000FT CARGO BOTTLE LOW CAUTION MESSAGE CAUTION MESSAGE EXTINGUISHED DESCENDING THROUGH 11000FT. REMOVED, CLEANED, RESECURED CONNECTOR ON CARGO BOTTLES, TEST GOOD PER CRJ AMM 26-20-00.Oct 24, 2010 · N528CA · Cndair CL6002B19 · Fire Protection System WiringSDR REXA201000136Unknown · odorFUMES IN COCKPIT/CABIN LED TO DIVERSION. APU OFF/BLEEDS ON ENGINES/SMELLED LIKE CIGARETTE BURNING/NO VISIBLE SMOKE. PERFORMED GROUND RUNS WITH BLEEDS ON ENGINES AND APU NO FUMES OR SMOKE NOTED. PER 71-00-00 OPS CHECKED 1 AND 2 PACKS PER 21-50-00 OPS GOOD.Sep 10, 2010 · N528CA · Cndair CL6002B19 · Air Distribution SystemSDR REXA201000092Selector Valve · malfunctionedUPON CLIMBOUT AFTER THE CLIMB CHECK, HAD A GEAR DISAGREE MSTR WARNING. THE NOSE GEAR WAS THE ONE IN DISAGREEMENT. THE F/O START THE QRH, THE WARNING WENT AWAY. A/C RETURNED TO DTW AND MAINTENANCE REMOVED AND REPLACED THE NLG SELECTOR VALVE IAW AMM 32-20-00.Jun 7, 2010 · N528CA · Cndair CL6002B19 · Landing Gear Retraction/Extension SystemSDR COMA0760474Ecu · faultyFLIGHT 5011 - FLAP FAIL CAUTION RECEIVED ON TAXI OUT. RETURNED TO GATE. REPLACED FECU. NO FURTHER DEFECTS.Jul 11, 2007 · N528CA · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR COMA0760261Windshield · crackedCAPTAIN'S WINDSHIELD INNER PANEL SHATTERED. PROCEEDED TO CVG WITHOUT INCIDENT. REPLACED CAPTAIN'S WINDSHIELD.Mar 15, 2007 · N528CA · Cndair CL6002B19 · Flight Compartment WindowsSDR COMA0760150Flap System · malfunctionedFLIGHT 5115 - DURING YUL APPROACH RECEIVED A FLAP FAIL CAUTION MESSAGE. COMPLIED WITH AD 2006-12-21 FLAP CAUTION MESSAGE -FIRST EVENT- MAINTENANCE ACTION, PARAGRAPH (G) 1, 2, 3, (A, B, C). FLAP SYSTEM WAS RESET WITH NO FURTHER FLAP CAUTION MESSAGES.Feb 6, 2007 · N528CA · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR COMA0760080Shaft · damagedFLIGHT 5510 - FLAP FAIL MESSAGE AT 8 DEGREES. LANDED WITHOUT INCIDENT. PERFORMED EO 27-046 AD INCLUDING FLAP SHAFT REJUVENATION. NO FURTHER DEFECTS.Jan 26, 2007 · N528CA · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR COMA0660501Skin Panel · crackedPAX DOOR SECOND STEP DOWN FORWARD AND AFT SKINS CRACKED UNDER BRACKETS WHERE HAND RAILS STOW WHEN DOWN. AFT SKIN ALSO CRACKED THIRD STEP DOWN IN RADIUS OF TREAD/RISER. REMOVED DAMAGED AREAS OF PAX DOOR FORWARD AND AFT SKINS SECOND STEP, AND THIRD STEP AFT SKAug 18, 2006 · N528CA · Cndair CL6002B19 · Passenger/Crew DoorsSDR COMA0660103Generator · faultyFLIGHT 5104 - CLIMBING OUT OF AUS DURING GEAR RETRACTION, THE AIR DRIVE GENERATOR DEPLOYED, FLIGHT RETURNED TO THE FIELD. REPLACED THE ADG AUTO DEPLOY CONTROL PANEL.Jan 28, 2006 · N528CA · Cndair CL6002B19 · AC Generation SystemSDR COMA0560199Window · crackedFLIGHT 5380 PILOTS SIDE WINDOW CRACKED. REPLACED PILOTS SIDE WINDOW.Mar 21, 2005 · N528CA · Cndair CL6002B19 · Flight Compartment WindowsSDR COMA0560072Hydraulic System · lowFLIGHT 5045 - DURING APPROACH TO BOS, RECEIVED A GEAR DISAGREE FOLLOWED BY A HYDRAULIC NR 3 LOW PRESSURE CAUTION, CREW DECLARED AN EMERGENCY, FOLLOWED QRH AND LANDED WITHOUT INCIDENT. SERVICED THE NR 3 HYDRAULIC SYSTEM.Jan 22, 2005 · N528CA · Cndair CL6002B19 · Hydraulic System, MainSDR COMA0460288Pitot Line · contaminatedFLIGHT 5208 ABORTED TAKEOFF AT 75 KTS DUE TO INOPERATIVE STANDBY AIRSPEED INDICATION. PURGED WATER FROM THE STANDBY PITOT SYSTEM LINE.Apr 23, 2004 · N528CA · Cndair CL6002B19 · Pitot/Static SystemSDR COMA0460058Control Unit · malfunctionedFLIGHT 5710 STAB TRIM AND MACH TRIM DISENGAGED DURING T/O. REPLACED THE HSTCU.Jan 14, 2004 · N528CA · Cndair CL6002B19 · Stabilizer Control SystemSDR COMA0460009Engine · fluctuatesFLIGHT 5732 N1 AND N2 AND F/F FLUCTUATING. COULD NOT DUPLCIATE. GROUND RUNS WERE NORMAL AND SATISFACTORY.Dec 30, 2003 · N528CA · Cndair CL6002B19 · Engine (Turbine/Turboprop)SDR COMA0360420Warning Light · illuminatedDURING DECENT INTO DTW RECEIVED A FLAP FAIL CAUTION MESSAGE AT 20 DEGREE FLAP POSITION. COMPLIED WITH AD 98-20-01 FLAP CAUTION MESSAGE (FIRST EVENT) FLAP SYSTEM WAS RESET WITH NO FURHTER FLAP CAUTION MESSAGES.Sep 21, 2003 · N528CA · Cndair CL6002B19 · Trailing Edge Flap Control System
Back to N528CA, cancelled Jun 26, 2019