N374CA

Service difficulty reports · 193

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 = 'N374CA' 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 SWI2024F01393Stringer · corrodedCORROSION ON STRINGER STGR 23L BETWEEN FS 1015.00 - 1030.00 (C-CHECK RO 12/21/2024) (FILED CLOSED)REMOVED CORROSION ON STRINGER 23L BETWEEN FS 1015.00 - 1030.00 REF CRJ700 SRM 51-21-06-001-001-A01. STRINGER STGR 23L BETWEEN FS 1015.00 - 1030.00 ATTACHED FLANGESep 6, 2024 · N374CA · Cndair CL6002C10 · Fuselage Main, Longeron/StringerSDR SWI2024F01392Frame · corrodedCORROSION ON FRAME FS 1015.00 BETWEEN STGR 24L - 22L(C-CHECK RO 12/21/2024) (FILED CLOSED)COMPLIED WITH EO NO: CL-600-2C10-53-L08265 REV IR REPAIR OF CORROSION ON FRAME FS 1015.00 BETWEEN STGR 24L - 22L LEAK AND OPS CHECK GOODSep 6, 2024 · N374CA · Cndair CL6002C10 · Fuselage Main, FrameSDR SWI2024F01391Stringer · corrodedCORROSION ON STINGER STGR 26L BETWEEN 1088.00 - 1098.00 (C-CHECK RO 12/21/2024) (FILED OPEN)REPAIRED STGR 26L AT FS1088-FS1098 REF CRJ700 SRM 53-00-03-201-001-A01, REO 670-53-61-2377 REV.-- DATED 2024-10-11 AND DWG: MM670-35007 REV W. LEAK CHECK GOOD. COMPLISep 6, 2024 · N374CA · Cndair CL6002C10 · Fuselage Main, Longeron/StringerSDR SWI2024F01390Angle · corrodedPAX DOOR THRESHOLD MIDCAP ANGLE CORRODED AT MULTIPLE SPOTS BETWEEN FS310-FS349 (MARKED) (C-CHECK RO 12/21/2024) (FILED OPEN)REMOVED AND INSTALLED NEW REPLACEMENT MID CAP ANGLE AT PAX DOOR THRESHOLD PER CRJ700 SRM 51-42-06-001-001-A01 & SRM 51-42-21-001-001-A0Sep 6, 2024 · N374CA · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR SWI2024F01389Stringer · corrodedCORROSION NOTED ON STRG 23L BETWEEN FS517.00-FS489.00 (MARKED) (C-CHECK RO 12/21/2024) (FILED OPEN)REPLACED STGR 23L BETWEEN FS517.00-FS489.00 REF CRJ700 SRM 53-00-03-201-001-A01, CRJ700 SRM 51-42-06-001-001-A01, , DWG SH670-30006 REV. A., DWG SH670-33200 REV.Sep 6, 2024 · N374CA · Cndair CL6002C10 · Fuselage Main, Longeron/StringerSDR SWI2024F01388Tie Down · corrodedCORROSION NOTED AT FWD BAG BAY TIE DOWN PLATE BTWN STRG22L-23L AND FS581 (MARKED) (C-CHECK RO 12/21/2024) (FILED OPEN)REMOVED AND INSTALLED NEW BRACKET (TIE DOWN PLATE) P/N: SH670-33390-2 AT FS581 BETWEEN STGR 22L - 23L REF. CRJ700 SRM 51-42-21-001-001-A01 & Sep 6, 2024 · N374CA · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR SWI2024F01387Tie Down · corrodedCORROSION NOTED AT FWD BAG BAY TIE DOWN PLATE BTWN STRG22L-23L AND FS533 (MARKED) (C-CHECK RO 12/21/2024) (FILED OPEN)REMOVED CORROSION FROM TIE DOWN PLATE FOUND OUT OF LIMITS, REMOVED AND REPLACED TIE DOWN PLATE P/N SH670-33390-1 BTWN TSRG22L- STRG23L AND FS5Sep 6, 2024 · N374CA · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR SWI2024F01386Floorbeam · crackedCRACK NOTED AT FLOOR BEAM CLIP ATTACHED TO 280 CROSSBEAM AT RBL 9 (MARKED) (C-CHECK RO 12/21/2024) (FILED OPEN)REMOVED AND REPLACED FLOOR BEAM CLIP ATTACHED TO 280 CROSSBEAM AT RBL 9 WITH NEW PN CC670-34144-1 REF CRJ700 SRM 51-42-21-001-001-A01 , DWG CC670-3Sep 6, 2024 · N374CA · Cndair CL6002C10 · Fuselage Main, Floor BeamSDR SWI2024F01385Floorbeam · crackedCRACK NOTED AT FLOOR BEAM CLIP ATTACHED TO 280 CROSSBEAM AT LBL 9 (MARKED) (C-CHECK RO 12/21/2024) (FILED OPEN)REMOVED AND REPLACED FLOOR BEAM CLIP ATTACHED TO 280 CROSSBEAM AT LBL 9 WITH NEW PN CC670-34144-1 REF CRJ700 SRM 51-42-21-001-001-A01 , DWG CC670-3Sep 6, 2024 · N374CA · Cndair CL6002C10 · Fuselage Main, Floor BeamSDR SWI2024F01384Floorbeam · cracked*CRACK FOUND ON FS 280 FLOOR BEAM-VERTICAL WEB AT RBL 9. (C-CHECK RO 12/21/2024) (FILED OPEN)REPLACED FS 280 RH FLOOR BEAM SECTION WITH NEW REF CRJ 700 SRM 53-11-41-201-003-A01 AND REPLACED FS 280 BULKHEAD RH LOWER WEB A REF CRJ700 SRM 53-11-10-201-004-A01 COSep 6, 2024 · N374CA · Cndair CL6002C10 · Fuselage Main, Floor BeamSDR SWI2024F01383Tie Down · corrodedCORROSION NOTED ON FWD BAG BAY TIE DOWN PLATE AT FS581 BTWN STRG26L-27 (MARKED)(C-CHECK RO 12/21/2024) (FILED OPEN)REPLACED FWD BAG BAY TIE DOWN PLATE AT FS581 BETWEEN STGR 26L-27 REF CRJ700 SRM 51-42-21-001-001-A01 AND DWG SH670-33600 REV. AD. LEAK CHECK GOODSep 6, 2024 · N374CA · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR SWI2024F01382Frame · corrodedCORROSION NOTED ON FRAME FLANGE AT FS517.00 BTWN STRG 24L-25L (MARKED) (C-CHECK RO 12/21/2024) (FILED OPEN)REPLACE FRAME SECTOR AT FS517.00 BETWEEN STR 25L-19L REF CRJ700 SRM 51-42-06-001-001-A01, CRJ700 SRM 51-42-20-001-001-A01 AND DWG SH670-33200 REV. G. LEASep 6, 2024 · N374CA · Cndair CL6002C10 · Fuselage Main, FrameSDR SWIA20240906Tie Down · corrodedCORROSION NOTED AT FWD BAG BAY TIE DOWN PLATE BTWN STRG25R-24R BTWN FS549-FS565 (MARKED) (C-CHECK RO 12/21/2024) (FILED OPEN)EVALUATED, REMOVED AND INSTALLED NEW FWD BAG BAY TIE DOWN PLATE FROM INTERCOSTAL SECTION BETWEEN FS549-FS565 BETWEEN APPROX STRG24R -SSep 6, 2024 · N374CA · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR SWIA202501060017Threshold · corrodedSERVICE DOOR LOWER SILL THRESHOLD MOUNT HOLES ON BACK SIDE OF SEAL STRIKER HAVE CORROSION AROUND THEM FROM APROX FS.319.70 TO FS.349.00(MARKED) (C-CHECK RO 12/21/2024) (FILED OPEN)REPLACED SERVICE DOOR LOWER SILL THRESHOLD SEAL STRIKER FROM FS319.70-FS349.00 RSep 5, 2024 · N374CA · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR SWIA202501060016Seal Depressor · gougedPAX DOOR SURROUND LOWER SILL SEAL STRIKER GOUGED IN MULTIPLE SPOTS (MARKED). (C-CHECK RO 12/21/2024) (FILED CLOSED)REPLACED PAX DOOR LOWER SILL SEAL STRIKER REF CRJ700 SRM 51-42-21-001-001-A01, CRJ700 SRM 51-42-06-001-001-A01, DWG SH670-31810 REV. AE. LEAK CHESep 5, 2024 · N374CA · Cndair CL6002C10 · Fuselage Main, StructureSDR SWIA202501060015Floor Support · corrodedCOCKPIT AFT FLOOR BOARD SUPPORT ANGLE AT FS.280.00 CORRODED IN MULTIPLE SPOTS (MARKED).(C-CHECK RO 12/21/2024) (FILED CLOSED)REMOVED AND REPLACED THE FS. 280 COCKPIT FWD FLOOR SUPPORT ANGLE P/N CC670-33292-13 REF. CRJ 700 SRM 51-42-06-001-001-A01, DWG CC670-3Sep 5, 2024 · N374CA · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR SWIA20250106905Intercostal · corrodedINTERCOSTAL AT STR.20R BETWEEN FS.310.00 AND FS.319.70 HAS SPOTS OF CORROSION (MARKED). (C-CHECK RO 12/21/2024) (FILED CLOSED)REMOVED AND INSTALLED NEW INTERCOSTAL PN SH670-32047-1 AT STGR 20R BETWEEN FS310.00 - FS319.70 REF DWG SH670-31950 REV Y, CRJ700 SRM 5Sep 5, 2024 · N374CA · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR SWI2024F01396Striker · gougedPAX DOOR SURROUND LOWER SILL SEAL STRIKER GOUGED IN MULTIPLE SPOTS (MARKED). (C-CHECK RO 12/21/2024) (FILED OPEN)REPLACED PAX DOOR LOWER SILL SEAL STRIKER REF CRJ700 SRM 51-42-21-001-001-A01, CRJ700 SRM 51-42-06-001-001-A01, DWG SH670-31810 REV. AE. LEAK CHECKSep 5, 2024 · N374CA · Cndair CL6002C10 · Fuselage Main, StructureSDR SWI2024F01395Floor Support · corrodedCOCKPIT AFT FLOOR BOARD SUPPORT ANGLE AT FS.280.00 CORRODED IN MULTIPLE SPOTS (MARKED).(C-CHECK RO 12/21/2024) (FILED OPEN)REMOVED AND REPLACED THE FS. 280 COCKPIT FWD FLOOR SUPPORT ANGLE P/N CC670-33292-13 REF. CRJ 700 SRM 51-42-06-001-001-A01, DWG CC670-330Sep 5, 2024 · N374CA · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR SWI2024F01394Intercostal · corrodedINTERCOSTAL AT STR.20R BETWEEN FS.310.00 AND FS.319.70 HAS SPOTS OF CORROSION (MARKED). (C-CHECK RO 12/21/2024) (FILED OPEN)REMOVED AND INSTALLED NEW INTERCOSTAL PN SH670-32047-1 AT STGR 20R BETWEEN FS310.00 - FS319.70 REF DWG SH670-31950 REV Y, CRJ700 SRM 51-Sep 5, 2024 · N374CA · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR SWIA20250106903Seat Track · damagedREPLACE PILOT INBOARD AND OUTBOARD SEAT TRACKS (C-CHECK RO 12/21/2024) (FILED CLOSED)REMOVED AND INSTALLED NEW PILOT SIDE INBOARD AND OUTBOARD SEAT TRACKS. REF CRJ700 SRM 51-42-21-001-001-A01 & CC670-40010 REV B. COMPLIED WITH SKYWEST TASK CARD 51-900-1002-SKYSep 3, 2024 · N374CA · Cndair CL6002C10 · Fuselage, Powerplant Attach FittingsSDR SWIA202412240903Seat Track · damagedREPLACE PILOT INBOARD AND OUTBOARD SEAT TRACKS (C-CHECK RO 12/21/2024) (FILED OPEN)REMOVED AND INSTALLED NEW PILOT SIDE INBOARD AND OUTBOARD SEAT TRACKS. REF CRJ700 SRM 51-42-21-001-001-A01 & CC670-40010 REV B. COMPLIED WITH SKYWEST TASK CARD 51-900-1002-SKY.Sep 3, 2024 · N374CA · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR SWIA20240901Hinge · nickedPASSENGER DOOR PIANO HINGE, DOOR SIDE HAS VARIOUS SCUFFS AND NICKS, (MARKED) HN00184680 (C-CHECK RO 12/21/2024) (FILED OPEN)REMOVED DAMAGE FROM HINGE AT MARKED LOCATIONS. REF: CRJ-700 S.R.M. 51-12-00-001-001-A01. EVALUATED PASSENGER DOOR PIANO HINGE ON DOORSep 1, 2024 · N374CA · Cndair CL6002C10 · Fuselage, Door HingeSDR SWIA20250106830Fairing · wornRIGHT WING, INBOARD FLAP, INBOARD AND OUTBOARD FAIRINGS HAVE WORN THROUGH THE PAINT OF THE FLAP LOWER SKIN, HN00184284 (C-CHECK RO 12/21/2024) (FILED CLOSED)R/H WING, I/B FLAP LWR SKIN HAS BEEN REPAIRED REF CRJ 700 SRM 57-52-01-201-005-A01, FIG. 57-52-01-9Aug 30, 2024 · N374CA · Cndair CL6002C10 · Wing Main, Frame StructureSDR SWIA202412240830Fairing · wornRIGHT WING, INBOARD FLAP, INBOARD AND OUTBOARD FAIRINGS HAVE WORN THROUGH THE PAINT OF THE FLAP LOWER SKIN, HN00184284 (C-CHECK RO 12/21/2024) (FILED OPEN)R/H WING, I/B FLAP LWR SKIN HAS BEEN REPAIRED REF CRJ 700 SRM 57-52-01-201-005-A01, FIG. 57-52-01-995Aug 30, 2024 · N374CA · Cndair CL6002C10 · Trailing Edge FlapsSDR SWIA202412240827Drag Fitting · crackedSUSPECTED CRACK ON THE RIGHT SIDE FWD DRAG FITTING. (C-CHECK RO 12/21/2024) (FILED CLOSED)PERFORMED REPAIR OF RH FWD DRAG ANGLE FITTING REF BOMBARDIER R.E.O. 670-55-31-018 REV. -A DATED 2016-11-18. COMPLIED WITH 51-900-1002-SKYAug 27, 2024 · N374CA · Cndair CL6002C10 · Nacelle/Pylon, Main FrameSDR SWIA202501060825Skin · dentedLH WING OTBD FLAP HAS A DENT ON LOWER INBOARD EXTERNAL SKIN, MARKED (C-CHECK RO 12/21/2024) (FILED CLOSED)L/H WING O/B FLAP, AFT I/B LWR SKIN HAS BEEN REPAIRED REF CRJ 700 SRM 57-53-01-201-001-A01, TYPE 3 REPAIR. COMPLIED FULLY W/SKYCARD 51-900-1002-SKY. SEE CAug 25, 2024 · N374CA · Cndair CL6002C10 · Aileron TabsSDR SWIA202412240825Skin · dentedLH WING OTBD FLAP HAS A DENT ON LOWER INBOARD EXTERNAL SKIN, MARKED (C-CHECK RO 12/21/2024) (FILED OPEN)L/H WING O/B FLAP, AFT I/B LWR SKIN HAS BEEN REPAIRED REF CRJ 700 SRM 57-53-01-201-001-A01, TYPE 3 REPAIR. COMPLIED FULLY W/SKYCARD 51-900-1002-SKY. SEE CONAug 25, 2024 · N374CA · Cndair CL6002C10 · Trailing Edge FlapsSDR SWIA20250106014Hinge · nickedPASSENGER DOOR PIANO HINGE, UPPER AFT AIRCRAFT SIDE, NICKED, HN00182891 (C-CHECK RO 12/21/2024) (FILED CLOSED)REPLACED PASSENGER DOOR PIANO HINGE(FUSELAGE SIDE) REF DWG SH670-31810 REV. AE, CRJ700 SRM 53-21-23-201-007-A01. LEAK CHECK GOOD. COMPLIED WITHAug 24, 2024 · N374CA · Cndair CL6002C10 · Fuselage, Door HingeSDR SWI2024F01397Hinge · nickedPASSENGER DOOR PIANO HINGE, UPPER AFT AIRCRAFT SIDE, NICKED, HN00182891 (C-CHECK RO 12/21/2024) (FILED OPEN)REPLACED PASSENGER DOOR PIANO HINGE(FUSELAGE SIDE) REF DWG SH670-31810 REV. AE, CRJ700 SRM 53-21-23-201-007-A01. LEAK CHECK GOOD. COMPLIED WITH SAug 24, 2024 · N374CA · Cndair CL6002C10 · Fuselage, Door HingeSDR SWIA20240824Tail Cone · crackedSUSPECTED CRACK ON THE TAILCONE RIGHT SIDE AFT DRAG. (C-CHECK RO 12/21/2024) (FILED OPEN)COMPLIED WITH BOMBARDIER R.E.O. 670-55-31-018 REV. A IN REPAIR TO V/STAB TO FUSE ATTACHMENT R/H AFT DRAG ANGLE. COMPLIED WITH 51-900-1002-SKYAug 24, 2024 · N374CA · Cndair CL6002C10 · Aerodynamic FairingsSDR SWIA20250106816Skin · dentedADM# N374CA-7225 - LH FUSELAGE SKIN AT FS 220.00, BETWEEN STR20L AND STR21L. ONE DENT MEASURING 3.25" DIAMETER X .025" MAX DEPTH. AFTER DRESSBACK, NEW DENT DIMENSIONS ARE 2.3"L BY 1.7"W BY .010" DEEP. PLOT, MAP, AND EVALUATE DAMAGE IF WITHIN ACCEPTABLE LIMITAug 16, 2024 · N374CA · Cndair CL6002C10 · Fuselage Main, Plate/SkinSDR SWIA202412240816Skin · dentedLH FUSELAGE SKIN AT FS 220.00, BETWEEN STR20L AND STR21L. ONE DENT MEASURING 3.25" DIAMETER X .025" MAX DEPTH. AFTER DRESSBACK, NEW DENT DIMENSIONS ARE 2.3"L BY 1.7"W BY .010" DEEP. PLOT, MAP, AND EVALUATE DAMAGE IF WITHIN ACCEPTABLE LIMITS OR REWORKED, ELIMAug 16, 2024 · N374CA · Cndair CL6002C10 · Fuselage Main, Plate/SkinSDR SWIA2021110662753Windshield · delaminatedAT CRUISE (FL360) THE FIRST OFFICER NOTICED WHAT SEEMED TO BE DELAMINATION AROUND THE EDGES OF HIS WINDSHIELD AND ALSO NOTICED HIS WINDSHIELD WAS ICE COLD BUT WE HAD NO WINDSHIELD HEAT CAUTION MESSAGE. THE FLIGHT WAS AT NIGHT SO WE TOOK A FLASHLIGHT OUT TO INSNov 24, 2021 · N374CA · Cndair CL6002C10 · Flight Compartment WindowsSDR SWIA202157470Windshield · crackedON CLIMB OUT THROUGH 25,000 FO NOTICE CONSTANT FLASHES LIKE SPARKS AT BASE OF THE RIGHT WINDSHIELD. THE FLASHES PICKED UP INTENSITY TO THE POINT THAT I COULD SEE IT FROM THE CAPTAIN SIDE. I TURNED OFF THE WINDSHIELD HEAT AND IT SEEMED TO STOP. UPON LANDING WE Apr 11, 2021 · N374CA · Cndair CL6002C10 · Flight Compartment WindowsSDR SWIA202156968Skin · dentedFOUND DENT IN SKIN AT FS193 AND STR23R. FILED CLOSED REPAIRED FUSELAGE SKIN BETWEEN FS 185 AND FS 202.75 AT STR 23R IAW REO 670-53-11-1649 REV -- DATED 3/12/21 & REO 670-51-00-085 REV A DATED 8/23/17. C/W TASK CARD 51-900-1002-SKY AND M-337.Feb 9, 2021 · N374CA · Cndair CL6002C10 · Fuselage Main, Plate/SkinSDR V0XD201909090005Drag Angle · crackedVERTICAL STAB LT DRAG ANGLE CRACKED. CORRECTIVE ACTION: REPAIRED VERT STAB DRAG ANDLGE IAW REO670-55-31-018 REVA, 2016-11-10 BY COMPLYING WITH EO-C700-55MR-001-0.Aug 31, 2019 · N374CA · Cndair CL6002C10 · Vertical Stabilizer Miscellaneous StructureSDR V0XD201909090004Door Sill · damagedLT FLOOR SILL FS 280 TO 318 HAVE 2 OBLONGED HOLES. CORRECTIVE ACTION: REMOVED AND REPLACED LT FLOOR SILL AT FS 280 TO 318 IAW SRM 51-42-11 AND 51-42-06.Aug 31, 2019 · N374CA · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR V0XD201909090003Rib · crackedRT WING LEADING EDGE RIB AT SS 58.41 IS CRACKED. CORRECTIVE ACTION: REMOVED AND REPLACED RT WING LEADING EDGE RIB AT SS 58.41 IAW SRM 51-42-13, 51-42-06, 51-42-21.Aug 29, 2019 · N374CA · Cndair CL6002C10 · Wing, Rib/BulkheadSDR V0XD2019091200001Floorbeam · crackedLT FLOOR STRUCTURE CROSSBEAM FS280.00 CRACKED. CORRECTIVE ACTION: ACCOMPLISHED SPLICE REPAIR OF THE FLOOR STRUCTURE, CROSSBEAM FS280.00 IAW ENGINEERING ORDER#: C700-55MR-011, DATED 01/07/2019.Aug 26, 2019 · N374CA · Cndair CL6002C10 · Fuselage Main, Floor BeamSDR V0XD201909090002Door Sill · corrodedRT FLOOR SILL FS280 TO 318 HAVE SIGNS OF CORROSION. CORRECTIVE ACTION: REMOVED AND REPLACED RT FLOOR SILL FROM FS280 TO 318 IAW SRM 51-43-13, 51-42-06 AND 51-42-21, REO 670-53-00-390.Aug 22, 2019 · N374CA · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR V0XD2019090900000Seat Track · corrodedLT SIDE SEAT RAILS FROM FS669 TO FS989 HAVE SIVE SIGNS OF CORROSION. CORRECTIVE ACTION: EVALUATED LT SIDE SEAT RAILS AND REPLACED SEAT RAILS THAT WERE OUT OF LIMITS AT FS669 TO 713 AND 828 TO 959 IAW SRM 53-41-49, 51-26-00, 51-41-02, AMM 20-21-00.Aug 22, 2019 · N374CA · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR V0XD201908626001Strap · crackedAFT WING TO FUSELAGE FAIRING PANEL 195DL ATTACHMENT POINT STRAP CRACKED. REMOVED AND INSTALLED STRAP ON PANEL 195DL IAW SRM 51-42-13, 53-00-01, AND 51-40-11.Aug 18, 2019 · N374CA · Cndair CL6002C10 · Aerodynamic FairingsSDR V0XD201908290001Seat Track · corrodedRH SIDE SEAT RAILS FROM FS 669 TO FS 989 HAVE SIGNS OF CORROSION. CORRECTIVE ACTION: EVALUATED RH SIDE SEAT RAILS AND REPLACED SEAT RAILS THAT WERE OUT OF LIMITS AT FS 669-712, FS785-853, AND FS 867-960 IAW CRJ 700 SRM 53-41-49, 51-26-00, 51-41-02,AMM 20-21-00Aug 15, 2019 · N374CA · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR N6WA2019072401Status Message · false activationPROXIMITY SYS FAULT 1 STATUS MESSAGE. DEACTIVATED GROUND VALVE AVIONICS COOLING IAW AMM 21-24-18. INSPECTED PASSENGER DOOR AND ENSURED GREEN MARKS ALIGNED. EVALUATED AND INSPECTED AIRCRAFT AND FOUND TO BE IN SAFE CONDITION FOR ONE TIME FERRY FLIGHT MHT TO DTW.Jul 24, 2019 · N374CA · Cndair CL6002C10 · Door Warning SystemSDR N6WA2019010701Computer · malfunctionedHEADING DISPLAY BETWEEN MFD 1 AND 2 DISAGREE BY 20 DEGREES. R/R AHC NR 1 IAW AMM 34-21-01 PN ON/OFF 622-9336-400 SN OFF 1729 SN ON 3749 PERFORMED OPS CHECK OPS CHECK GOOD.Jan 7, 2019 · N374CA · Cndair CL6002C10 · Attitude and Direction Data SystemSDR N6WA2017081001Bulb · inoperativeEXIT ROW BY C & D HAS TWO BULBS OUT IN EMERGENCY LIGHT. R & R THE BULBS, OPS CHECKED GOOD IAW AMM 33-51-09.Aug 10, 2017 · N374CA · Cndair CL6002C10 · Emergency LightingSDR V0XD2017041320Seat Track · corrodedRT SIDE SEAT RAIL CORRODED BETWEEN FS 724.08 AND FS 761.85. REMOVED AND REPLACED RT SEAT RAIL BETWEEN FS 724.08 AND 761.85 IAW SRM 51-42-02 AND AMM 53-00-49.Apr 12, 2017 · N374CA · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR V0XD20170413019Seat Track · corrodedLT SIDE SEAT RAIL CORRODED BETWEEN FS 677.00 AND FS 708.00. REMOVED AND REPLACED LT SIDE SEAT RAIL BETWEEN FS 677.00 AND FS 708.00 IAW AMM 53-00-49 AND SRM 51-41-02.Apr 12, 2017 · N374CA · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR V0XD20170410018Tripler · gougedSKIN TRIPLER AT BS 977 HAS A GOUGE. REPAIRED IAW REO 670-53-61-727.Apr 10, 2017 · N374CA · Cndair CL6002C10 · Fuselage Main, Plate/Skin
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