N689CA

Service difficulty reports · 196

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 = 'N689CA' 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 SWIA2020021848511Frame · corroded*EXTERNAL FORWARD FUSELAGE - FS661.00+62.00 (ENCLOSED BY WING-TO-FUSELAGE FAIRINGS) FRAME END CAP HAS MULTABLE AREA'S OF CORROSION. FLAGGED (C-CHECK) RO 2/14/2020 REPLACED THE SPLICE PLATE JOINT (END CAP) WITH A SERVICABLE SPLICE PLATE JOINT REFERENCING BDec 2, 2019 · N689CA · Cndair CL6002D24 · Fuselage Main, FrameSDR SWIA2020021848631Hinge · chafedLH WING INBD FLAP OTBD HINGE BOX HAS CHAFFING AT GUIDE (MARKED) (C-CHECK) RO 2/14/2020 BLENDED LH WING INBD FLAP OTBD HINGE BOX GUIDE OUT OF LIMITS REF CRJ900 SRM. REPLACED GUIDE REF BOMBARDIER DRAWING, CRJ900 SRM, AND CRJ900 SRM. SEE CONTINUE CARD FOR DETNov 27, 2019 · N689CA · Cndair CL6002D24 · Trailing Edge FlapsSDR SWIA2020021848615Web · corroded*PAX DOOR FWD WEB IS CORRODED AT MULTIPLE AREAS. (C-CHECK) RO 2/14/2020 REMOVED CORRODED FWD PAX DOOR WEB AND REPLACED WITH NEW PN #601R317071-12S REFERENCING CRJ 900 SRM.Nov 27, 2019 · N689CA · Cndair CL6002D24 · Passenger/Crew DoorsSDR SWIA2020021848614Skin · corroded*PAX DOOR INNER SKIN IS CORRODED AT MULTIPLE AREAS. (C-CHECK) RO 2/14/2020 REPLACED PASSENGER DOOR INNER SKIN REF BOMBARDIER DRAWING AND CRJ900 SRM.Nov 27, 2019 · N689CA · Cndair CL6002D24 · Passenger/Crew DoorsSDR SWIA2020021848510Former · corroded*PAX DOOR FWD FORMER IS CORRODED ON INNER AND OUTER SURFACES. (C-CHECK) RO 2/14/2020 PAX DOOR FWD FORMER OUT OF LIMITS. REPLACED FORMER REF CRJ900 SRM ,AND BOMBARDIER DRAWING. PRESSURE CHECK NOT REQUIRED DUE TO PASSENGER DOOR REPLACED ON CAMP#20407458.Nov 27, 2019 · N689CA · Cndair CL6002D24 · Passenger/Crew DoorsSDR SWIA2020021848630Panel · chafedCHAFFING ON LEFT HAND WING AILERON PANEL 599CB. (C-CHECK) RO 2/14/2020 REMOVED DAMAGE FROM PANEL 599CB, FOUND TO BE OUT OF LIMITS. LOCATED AND DRILLED NEW REFERENCING CRJ 900 SRM. INSTALLED ON JOB 91513340 OP 7005 CAMP 19937299.Nov 26, 2019 · N689CA · Cndair CL6002D24 · AileronsSDR SWIA2020021848629Panel · chafedCHAFFING ON LEFT HAND WING AILERON PANEL 599BB. (C-CHECK) RO 2/14/2020 REMOVED DAMAGE FROM PANEL 599BB, FOUND TO BE OUT OF LIMITS. LOCATED AND DRILLED NEW REFERENCING CRJ 900 SRM. INSTALLED ON JOB 91513340 OP 7005 CAMP 19937299.Nov 26, 2019 · N689CA · Cndair CL6002D24 · AileronsSDR SWIA2020021848628Panel · chafedCHAFFING ON LEFT HAND WING AILERON PANEL 599AB. (C-CHECK) RO 2/14/2020 REMOVED DAMAGE FROM PANEL 599AB, FOUND TO BE OUT OF LIMITS. LOCATED AND DRILLED NEW REFERENCING CRJ 900 SRM. INSTALLED ON JOB 91513340 OP 7005 CAMP 19937299.Nov 26, 2019 · N689CA · Cndair CL6002D24 · AileronsSDR SWIA2020021848509Door · dentedADM # 6568. L/H ENGINE FWD LOWER FAN COWL DOOR BETWEEN FS 1031.00 AND FS 1047.00 AT THE 4 O'CLOCK POSITION. 1 DENT WITH IN LIMITS DEPTH OF DENT WAS .058 " LENTH WAS 1 INCH WIDTH WAS 18/32 INCH. PLOT, MAP, AND EVALUATE DAMAGE IF WITHIN ACCEPTABLE LIMITS OR REWONov 25, 2019 · N689CA · Cndair CL6002D24 · Nacelle/Pylon, Main FrameSDR SWIA2019021848508Skin · dentedADM #2757. 3 " FORWARD OF FS613.0 AND 6" BELOW WL72.5 (ABOVE AND IN BETWEEN FORWARD AND CENTER BAGGAG BAY DOORS). DENT APPROXIMATELY 1" WIDE AND 0.025" DEEP. PLOT, MAP, AND EVALUATE DAMAGE IF WITHIN ACCEPTABLE LIMITS OR REWORKED, ELIMINATE EVIDENCE USING STANDNov 25, 2019 · N689CA · Cndair CL6002D24 · Fuselage Main, Plate/SkinSDR SWIA201642766Floorbeam · corrodedBS 280 FLOORBEAM CORRODED AT LBL 9. REPLACED THE FLOORBEAM IAW SRM.Oct 8, 2016 · N689CA · Cndair CL6002D24 · Fuselage Main, Floor BeamSDR SWIA201642765Floorbeam · damagedBS 280 FLOORBEAM TITANIUM CAP HAS A SHEARED FASTENER AT LBL 12. REMOVED AND REPLACED TITANIUM CAP IAW SRM.Oct 7, 2016 · N689CA · Cndair CL6002D24 · Fuselage Main, Floor BeamSDR SWIA201642767Stringer · corrodedSTRINGER 25R HAS CORROSION FROM BS 333 - 364. REMOVED AND REPLACED THE STRINGER IAW SRM. LEAK CHECKED GOOD.Oct 6, 2016 · N689CA · Cndair CL6002D24 · Fuselage Main, Longeron/StringerSDR SWIA201642764Stringer Splice · corrodedSTRINGER SPLICE 26R AT BS 333 CORRODED OUT OF LIMITS. REPLACED THE STRINGER SPLICE IAW SRM. PRESSURE CHECKED, GOOD NO LEAKS.Oct 6, 2016 · N689CA · Cndair CL6002D24 · Fuselage Main, Longeron/StringerSDR SWIA201642763Stringer Splice · corrodedSTRINGER SPLICE 25L AT BS 333 CORRODED. REPLACED THE STRINGER SPLICE IAW SRM. PRESSURE CHECKED GOOD, NO LEAKS IAW SRM.Oct 6, 2016 · N689CA · Cndair CL6002D24 · Fuselage Main, Longeron/StringerSDR SWIA201642762Frame · corrodedFRAME AT BS 310 CORRODED. REPLACED THE FRAME IAW REO. PRESSURE CHECKED GOOD, NO LEAKS.Oct 6, 2016 · N689CA · Cndair CL6002D24 · Fuselage Main, FrameSDR SWIA201642761Stringer · corrodedSTRINGER 25L BETWEEN BS 280 - 333 CORRODED. REPLACED THE STRINGER IAW SRM. PRESSURE CHECKED GOOD, NO LEAKS IAW SRM.Oct 6, 2016 · N689CA · Cndair CL6002D24 · Fuselage Main, Longeron/StringerSDR SWIA201642760Angle · corrodedFLOORBEAM ANGLE BS 280 HAS CORROSION. REPLACED THE FLOORBEAM ANGLE IAW SRM.Oct 6, 2016 · N689CA · Cndair CL6002D24 · Fuselage Main, Floor BeamSDR SWIA201642759Butt Joint · corrodedBS 280 BUTT-STRAP HAS CORROSION BETWEEN STRINGERS 25L & 25R. REPAIRED IAW EA.Oct 6, 2016 · N689CA · Cndair CL6002D24 · Fuselage Main, StructureSDR SWIA201642758Doubler · corrodedTCAS ANTENNA DOUBLER CORRODED BETWEEN BS 295 - 310, STRINGERS 26L - 26R. REPLACED THE DOUBLER IAW SRM. PRESSURE CHECKED GOOD ,NO LEAKS IAW SRM.Oct 6, 2016 · N689CA · Cndair CL6002D24 · Fuselage Main, Plate/SkinSDR SWIA201642757Frame · corrodedBS 319 FRAME HAS CORROSION BETWEEN STRINGERS 26L & 26R. REPLACED THE FRAME IAW REO. PRESSURE CHECKED GOOD, NO LEAKS IAW SRM.Oct 6, 2016 · N689CA · Cndair CL6002D24 · Fuselage Main, FrameSDR SWIA201642756Frame · corrodedBS 333 FRAME HAS CORROSION BETWEEN STRINGERS 26L & 26R. REPLACED THE FRAME IAW REO. PRESSURE CHECKED GOOD, NO LEAKS IAW SRM.Oct 6, 2016 · N689CA · Cndair CL6002D24 · Fuselage Main, FrameSDR SWIA201642755Stringer Splice · corrodedSTRINGER SPLICE 25R HAS CORROSION AT BS 333. REPLACED THE STRINGER SPLICE IAW SRM. PRESSURE CHECKED GOOD, NO LEAKS IAW SRM.Oct 6, 2016 · N689CA · Cndair CL6002D24 · Fuselage Main, Longeron/StringerSDR SWIA201642754Stringer · corrodedSTRINGER 26R HAS CORROSION FROM BS 333 - 364. REMOVED AND REPLACED THE STRINGER IAW SRM. LEAK CHECKED GOOD.Oct 6, 2016 · N689CA · Cndair CL6002D24 · Fuselage Main, Longeron/StringerSDR SWIA201642753Striker · corrodedGALLEY SERVICE DOOR LOWER SEAL STRIKER HAS CORROSION AROUND ACCESS HOLES. REPLACED THE SEAL STRIKER IAW SRM. LEAK CHECKED GOOD.Oct 6, 2016 · N689CA · Cndair CL6002D24 · Galley DoorsSDR SWIA201642752Angle · corrodedPAX DOOR KICK ANGLE HAS CORROSION. REMOVED AND REPLACED THE KICK ANGLE IAW SRM. OPS CHECKED GOOD.Oct 6, 2016 · N689CA · Cndair CL6002D24 · Passenger/Crew DoorsSDR SWIA201541007Brake · malfunctionedUPON LANDING, RT BRAKE FAILED TO APPLY PROPERLY, THEN GRABBED UNEXPECTEDLY. CYCLED ANTI-SKID. SYMPTOMS REMAINED FOR TAXI IN. BLED MAIN LANDING GEAR BRAKE ASSEMBLIES 3 AND 4 IN REF AMM.Mar 19, 2015 · N689CA · Cndair CL6002D24 · Landing Gear Brake SystemSDR SWIA201439190Battery Pack · inoperativeFORWARD FLASHLIGHT IS INOPERATIVE. MAINTENANCE R & R THE FLASHLIGHT BATTERY.Aug 19, 2014 · N689CA · Cndair CL6002D24 · Emergency EquipmentSDR SWIA201439051Wire · disconnectedLEFT, FWD, LOWER EMERGENCY EXIT LIGHT INOPERATIVE, OVERWING EXIT ROW 12. FOUND WIRE PULLED FROM SOCKET AT CONNECTOR FOR BATTERY CHARGER NR 4. SEATED WIRING AND PERFORMED SEVERAL OPS CHECKS WITH NO DEFECTS NOTED. ACFT GOOD TO RETURN TO SERVICE.Aug 11, 2014 · N689CA · Cndair CL6002D24 · Light System WiringSDR SWIA201439021Charger · malfunctionedTHREE AFT EMERGENCY LIGHT PODS ARE FLICKERING ON AND OFF. R & R BATTERY CHARGER AND PERFORMED OPS CHECK. OPS CHECKED SATISFACTORY.Aug 10, 2014 · N689CA · Cndair CL6002D24 · Emergency LightingSDR SWIA2014061238146Bulb · burned outEMERGENCY LIGHTS HAVE BULBS BURNED OUT. REPLACED BULBS IAW AMM. OPS CHECKED GOOD.Jun 12, 2014 · N689CA · Cndair CL6002D24 · Emergency LightingSDR SWIA201437377Lamp · burned outRIGHT AFT OVERWING EMERGENCY LIGHT IS BURNED OUT. REPLACED THE LAMP IAW AMM.May 4, 2014 · N689CA · Cndair CL6002D24 · Emergency LightingSDR SWIA201436391Light · inoperativeNR 8 EMERGENCY OVERHEAD LIGHT IS BURNED OUT. FLT 4493 RELAMPED.Feb 15, 2014 · N689CA · Cndair CL6002D24 · Emergency LightingSDR SWIA201436252Light · inoperativeSEVERAL LIGHT BULBS BURNED OUT ON EMERGENCY EXIT ROW SIGNS. FLT 4477 RELAMPED.Feb 6, 2014 · N689CA · Cndair CL6002D24 · Emergency LightingSDR SWIA201333510Power Supply · failed3 EMERGENCY OVERHEAD LIGHTS DO NOT ILLUMINATE. REPLACED NR 5 POSITION BATTERY ASSY POWER SUPPLY IAW AMM, PN: AD-2013-1A, SN ON: 72179, SN OFF: 74729.May 20, 2013 · N689CA · Cndair CL6002D24 · Emergency LightingSDR SWIA201333455Transcowl · chafedOUTBOARD LEADING EDGE OF RIGHT LOWER TRANS COWL UNDER FWD LATCH ASSEMBLY IS CHAFED. (C-CHECK) REPAIRED TRANS COWL LATCH DOUBLER CHAFE IAW REO.May 1, 2013 · N689CA · Cndair CL6002D24 · Engine Thrust ReverserSDR SWIA201333454Doubler · chafedOUTBOARD LEADING EDGE OF UPPER TRANS COWL UNDER FWD LATCH ASSEMBLY IS CHAFED. (C-CHECK) REPAIRED TRANS COWL LATCH DOUBLER CHAFE IAW REO.May 1, 2013 · N689CA · Cndair CL6002D24 · Engine Thrust ReverserSDR SWIA201333453Seat Track · corrodedPOSSIBLE SIGNS OF SURFACE CORROSION ON LEFT SIDE SEAT RAIL SECTION FS 784.00 - FS 855.40. (C-CHECK) BLENDED CORROSION AREA ON LEFT SIDE SEAT RAIL FROM FS 784.00 TO FS 855.40, FOUND TO BE OUT OF LIMITS, FABRICATED NEW FROM SEAT TRACK EXTRUSION PN: N126-2075 May 1, 2013 · N689CA · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach FittingsSDR SWIA201333456Retainer · chafedFORWARD BAGGAGE BAY DOOR HAS TWO CHAFES ON INBOARD SEAL RETAINER. (C-CHECK) COMPLIED WITH FORWARD BAGGAGE BAY DOOR PERMANENT REPAIR IAW REO.Apr 30, 2013 · N689CA · Cndair CL6002D24 · Cargo/Baggage DoorsSDR SWIA201231788Structure · crackedFOUND A CRACK THAT EXTENDS OVER THE ORIGINAL REPAIR CUTOUT AT 1-3 SLAT TRACK. (C-CHECK) REPAIRED LEFT WING LEADING EDGE AT 1-3 SLAT TRACK IAW REO.Sep 6, 2012 · N689CA · Cndair CL6002D24 · Leading Edge DevicesSDR COMA2011070590010Floorbeam · corrodedFS 280 FLOORBEAM UPPER FLANGE CORRODED FROM LBL 9 - RBL 9. REMOVED AND REPLACED FS 280 CROSS BEAM AS PER BOMBARDIER DRAWING CC670-34010 REV J, AND IAW SRM 51-42-06, SRM 51-42-21, SRM 51-42-27 AND REO 690-53-11-032.Jul 4, 2011 · N689CA · Cndair CL6002D24 · Fuselage Main, Floor BeamSDR COMA005BBulkhead · corrodedRT FS 280 BULKHEAD WEB CORRODED JUST ABOVE FLOOR LINE. REMOVED AND REPLACED RT LOWER WEB SECTION IAW SRM 53-11-10-210-003-A01, REPAIR B.Jul 2, 2011 · N689CA · Cndair CL6002D24 · Fuselage Main, BulkheadSDR COMA2011070590008Bulkhead · corrodedLT FS 280 BULKHEAD WEB CORRODED JUST ABOVE FLOOR LINE. REMOVED AND REPLACED LT LOWER WEB SECTION IAW SRM 53-11-10-210-003-A01, REPAIR B.Jul 2, 2011 · N689CA · Cndair CL6002D24 · Fuselage Main, BulkheadSDR COMA2011070190007Drag Angle · crackedPAX DOOR AFT DRAG ANGLE CRACKED ADJACENT TO PULLEY BRACKET. REMOVED AND REPLACED DAMAGED SECTION OF DRAG ANGLE IAW BOMBARDIER REO 670-52-11-072, REV E.Jul 1, 2011 · N689CA · Cndair CL6002D24 · Passenger/Crew DoorsSDR COMA2010121090014Pin · sticksON CLIMBOUT FROM MSP RECEIVED RIGHT ENGINE FAN VIB. EMERGENCY DECLARED, A/C RETURNED TO MSP LANDED SAFELY. REMOVED AND REPLACED RIGHT ENGINE FAN BLADE RETAINING PINS (28EA), VIB CHECK GOOD.Dec 8, 2010 · N689CA · Cndair CL6002D24 · Turbine Engine Compressor SectionSDR COMA0880016Engine · vibrationENROUTE, CREW REPORTS FAN VIBRATION ON RT ENGINE. AC DIVERTED AND LANDED SAFELY. INSPECTED RT ENGINE FAN BLADES NO DEFECTS NOTED. PERFORMED ENGINE RUNS WITH NO DEFECTS NOTED. (K)Sep 4, 2008 · N689CA · Cndair CL6002D24 · Engine (Turbine/Turboprop)
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