N679SA

Service difficulty reports · 118

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 = 'N679SA' 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 SWIA20250429008Warning Message · false activationGEAR DISAGREE WARNING ON CLIMBOUT. GEAR UP MISTAKENLY DELAYED AND SELECTED UP ONCE AT 250KT. NOSE GEAR WOULDN€™T RETRACT. QRH FIXED ISSUE. (FLIGHT 4807 - FILED CLOSED)GEAR DISAGREE MESSAGE CAUSED BY OVERSPEED CONDITION OF THE GEAR. PERFORMED GEAR OVERSPEED IApr 28, 2025 · N679SA · Cndair CL6002B19 · Landing Gear Retraction/Extension SystemSDR SWIA2025012712Door Sill · corrodedUPON REMOVAL OF SERVICE DOOR SURROUND STRUCTURE LOWER SILL FOUND CORROSION ON LOWER STRUCTURE. (C-CHECK RO 1/26/2025) COMPLIED WITH REO 601R-53-21-3709 FOR REPAIR OF AREA. TASK CARD 51-900-1003-SKY COMPLETEDE, M-337 ATTACHED. CPCP CARD EMAILED MANUALLDec 12, 2024 · N679SA · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA2020127005Door Sill · corrodedWHILE WORKING SERVICE DOOR SURROUND STRUCTURE LWR SILL FOUND SERVICE DOOR AFT LOWER SILL TO BE CORRODED. (C-CHECK RO 1/26/2025) REMOVED AND REPLACED SERVICE DOOR SURROUND STRUCTURE LWR SILL P/N 601R38303-253 IAW CRJ200 SRM 51-42-02. TASK CARD 51-900-10Dec 5, 2024 · N679SA · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA202501270088Web · crackedWEB CRACKED AT THE ACCUMULATOR BRACKET F.S. 200 LBL 40. (C-CHECK RO 1/26/2025) REPAIRED CRACK AT THE ACCUMULATOR BRACKET IAW CRJ 200 SRM REO 601R53-11-081TASK CARD 51-900-1003-SKY COMPLETED. M-337 ATTACHEDNov 19, 2024 · N679SA · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA202501270087Structure · crackedCRACK IN CENTER WING BOX FS 461.5 RBL 4. (C-CHECK RO 1/26/2025) COMPLIED WITH REO 601R-53-41-3272 FOR REPAIR OF AREA.TASK CARD 51-900-1003-SKY COMPLETED. M-337 ATTACHEDNov 19, 2024 · N679SA · Cndair CL6002B19 · Fuselage Main, StructureSDR SWIA20250127114Door Sill · corrodedSERVICE DOOR SURROUND STRUCTURE LWR SILL IS CORRODED. (C-CHECK RO 1/26/2025) REMOVED AND REPLACED SERVICE DOOR SURROUND STRUCTURE LOWER SILL P/N 601R38533-9 IAW CRJ200 SRM 51-42-21 TASK CARD 51-900-1003-SKY COMPLETED. M-337 ATTACHED. CPCP MANUALLY EMANov 14, 2024 · N679SA · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA20250127006Skin · dentedADM# N679SA-8142THERE IS A DENT ABOVE AND AFT OF LOW PRESSURE AIR ACCESS PANEL, BETWEEN APPROXIMATELY FS589-FS605, AND STRINGER 21R-22R. PLEASE PLOT, MAP, AND EVALUATE DAMAGE. IF FOUND WITHIN LIMITS, ELIMINATE ALL EVIDENCE OF DAMAGE USING AIRCRAFT STANDARD PRAOct 6, 2024 · N679SA · Cndair CL6002B19 · Fuselage Main, Plate/SkinSDR SWIA202306196001Unknown · warning messageFLAPS FAIL CAUTION MESSAGE ON APPROACH AT ATW WHEN SELECTING FLAPS. INDICATED ZERO DEGREES. FOLLOWED QRH. PREFORMED A NO FLAP LANDING AT ORD. (FLT 4742 FILED CLOSED)THIS DISCREPANCY WAS TRANSFERRED TO CAMP ITEM 26767675 WITH THE FOLLOWING CORRECTIVE ACTION: "RJun 16, 2023 · N679SA · Cndair CL6002B19 · Trailing Flap Position Indicating SystemSDR SWIA202301301None · damagedFOUND LH WING WING BOX EXTENSION TRAILING EDGE ASSEMBLY DAMAGED (REF. IPC 57-32-00 ITEM #130) (FILED CLOSED)REMOVED AND REPLACED LH WING BOX EXTENSION TRAILING EDGE ASSEMBLY IN REFERENCE TO DWG. 600-10387 REV. D, SRM 51-21-00, SRM 51-40-11, SRM 51-41-00.ALL WOJan 30, 2023 · N679SA · Cndair CL6002B19 · Wing Main, Frame StructureSDR SWIA2022122967069Bracket · crackedPANEL 326BR FWD NUT PLATE BRACKET CRACKED AT HORIZONTAL STABILIZER. REMOVED ANGLE VISOR SUPPORT IAW SRM 51-42-06. INSTALLED NEW ANGLE VISOR SUPPORT IAW SRM, 51-42-06 AND DWG 600-23060 REV-V.Dec 6, 2022 · N679SA · Cndair CL6002B19 · Horizontal Stabilizer StructureSDR SWIA2022122967068Skin · dentedDENT ON EXTERNAL FUSELAGE SKIN REPAIR DOUBLER BETWEEN FS 589.00 - 605.00, STGR 25R - 26R. PERFORMED REPAIR TO DENT ON EXTERNAL FUSELAGE SKIN REPAIR DOUBLER IAW REO 601R-53-61-7930 REV -.Dec 4, 2022 · N679SA · Cndair CL6002B19 · Fuselage Main, Plate/SkinSDR SWIA2022122967067Skin · dentedDENT ON EXTERNAL FUSELAGE SKIN BETWEEN FS 640.00 - 654.00, STGR 19L - 20L. REPAIRED DENT IN FUSELAGE SKIN IAW REO 601R-53-61-7927 REV -.Dec 4, 2022 · N679SA · Cndair CL6002B19 · Fuselage Main, Plate/SkinSDR SWIA202266451None · crackedCAPTAIN SIDE WINDSHIELD CRACKED DURING CRUISE (FLIGHT #5451 FILED CLOSED) PLEASE REFERENCE AML 992932 FOR NEW REPLACEMENT OF CAPTAINS WIPER ARM. R&R CAPTAINS SIDE WINDSHIELD IN REF TO AMM 56-11-01 AND MIP TASK CARD 56-220-1000-SKY. OPS CHECK AND LEAK CSep 11, 2022 · N679SA · Cndair CL6002B19 · Window/Windshield SystemSDR SWIA202265987None · shutdownR ENG OIL PRESS WARNING MESSAGE NEAR TOP OF CLIMB PASSING THROUGH F300. R ENGINE OIL PRESSURE INDICATION FLUCTUATING INTO LOW RED PRESSURE ZONE. FOLLOWED QRH RETARDED ENGINE TO IDLE AND CONTINUED TO GET MESSAGE. FOLLOWED IN FLIGHT ENGINE SHUTDOWN PROCEDURE. Jul 7, 2022 · N679SA · Cndair CL6002B19 · Engine Oil QuantitySDR SWIA202156964Warning Message · false activationANTI-ICE WARNING MESSAGE IN FLIGHT SHORTLY AFTER TAKE OFF. FLIGHT 5491 NO HISTORY OF ANTI-ICE DUCT OR ANTI-ICE WARNING MSG. INSPECTED RIGHT WING FOR SIGNS OF BLEED LEAK. NO BLEED LEAK NOTED AT THIS TIME. PER FIM 36-20-00 SUSPECT FAULTY RIGHT BLCU. REMOVED AMar 17, 2021 · N679SA · Cndair CL6002B19 · Ice/Rain Protection SystemSDR SWIA202053968Spar · bentREAR SPAR (P/N 601R10851-3 SRM 57-21-07, FIG 4 ITEM 11) LOWER FLANGE BETWEEN WS 371.00-WS 377.00 IS BENT 0.200" UPWARD ALONG 2.20" SPANWISE. CLASSIFIED AS MAJOR REPAIR M-337 INITIATED. FILED CLOSED. REPAIR OF REAR SPAR LOWER FLANGE PERFORMED BY MHIRJ MRT PENov 9, 2020 · N679SA · Cndair CL6002B19 · Wing SparSDR SWIA202053967Skin · bentLOWER SKIN (P/N 601R10871-3 SRM ITEM 8) BETWEEN WS 371.00 WS 377.00 IS BENT 0.250" UPWARD ALONG 3.50" SPANWISE & 1.00? CHORDWISE. CLASSIFIED AS MAJOR REPAIR M-337 INITIATED. FILED CLOSED. REPAIR OF LOWER SKIN PERFORMED BY MHIRJ MRT PERSONNEL, PER REO. COMPNov 9, 2020 · N679SA · Cndair CL6002B19 · Fuselage Main, Plate/SkinSDR SWIA202053966Strap · damagedLOWER STRAP (P/N 601R10871-9 SRM 57-21-31, FIG 3 ITEM 11) WS 371.00-WS 377.00 IS HEAVILY BENT AND SHEARED. CLASSIFIED AS MAJOR REPAIR M-337 INITIATED. FILED CLOSED. NEW LOWER STRAP FABRICATED AND INSTALLED BY MHIRJ MRT PERSONNEL, PER REO, REFERENCE SNIEO FONov 9, 2020 · N679SA · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA202053468Bracket · crackedFWD CARGO DOOR TRACK LOWER BRACKET CRACKED. FILED CLOSED. REPLACED FWD CARGO DOOR TRACK LOWER BRACKET, IN REFERENCE TO CRJ 200 SRM.Oct 19, 2020 · N679SA · Cndair CL6002B19 · Cargo/Baggage DoorsSDR SWIA2019110546713Transmitter · out of toleranceR/H WING FLAP POSITION TRANSMITTER OUT OF SYNC WITH L/H WING FLAP TRANSMITTER. (C-CHECK) RO: 11/04/2019 WORK PERFORMED BY VENDOR AVMAX,Nov 5, 2019 · N679SA · Cndair CL6002B19 · Trailing Flap Position Indicating SystemSDR SWIA2019110546712Panel · damagedPANEL 325AR HAS DAMAGE OUT OF SRM LIMITS. REQUIRES REO FOR RECTIFICATION, (PANEL OPENING LANDING). (C-CHECK) RO: 11/04/2019 WORK PERFORMED BY VENDOR AVMAX.Nov 5, 2019 · N679SA · Cndair CL6002B19 · Vertical Stabilizer, Plate/SkinSDR SWIA2019110546711Panel · damagedPANEL 325BL AND 325CL HAS DAMAGE OUT OF SRM LIMITS. REQUIRES REO FOR RECTIFICATION, (PANEL OPENING LANDING). (C-CHECK) RO: 11/04/2019 WORK PERFORMED BY VENDOR AVMAX. SEE ATTACHED WORK CARD FOR DETAILS.Nov 5, 2019 · N679SA · Cndair CL6002B19 · Vertical Stabilizer, Plate/SkinSDR SWIA2019110546710Control Cable · out of adjustELEVATOR AUTOPILOT CONTROL CABLE OUT OF TENSION LIMITS. (C-CHECK) RO: 11/04/2019 ADJUSTE AUTOPILOT CONTROL CABLES IAW AMM.Nov 5, 2019 · N679SA · Cndair CL6002B19 · Elevator Control SystemSDR SWIA2019110546709Structure · dentedRH FLIGHT SPOILER HAS MANY DENTS AND IS OUT OF LIMITS PER SRM CUSTOMER HAS REQUESTED REMOVAL AND A NEW RH FLIGHT SPOILER INSTALLED. (C-CHECK) RO: 11/04/2019 REPLACED RH FLIGHTS SPOILER ASSY.Nov 5, 2019 · N679SA · Cndair CL6002B19 · SpoilersSDR SWIA2019110546708Pump · leakingFUEL SEEPING OUT OF 5 EA. SCREW HOLES ON L/H ELECTRICAL BOOST PUMP. (C-CHECK) RO: 11/04/2019 RE-SEALED DOME NUTS. LEAK CHECKS GOOD.Nov 5, 2019 · N679SA · Cndair CL6002B19 · Fuel Boost PumpSDR SWIA2019110546707Throttle · out of adjustLH THROTTLE OUT OF LIMITS AND HAS HIGH RESISTANCE WHEN MOVING. (C-CHECK) RO: 11/04/2019 PERFORMED ADJUSTMENT AND RIGGING CHECKS OF THROTTLES. OPS CHECKS GOOD.Nov 5, 2019 · N679SA · Cndair CL6002B19 · Power LeverSDR SWIA2019110546706Potentiometer · out of tolerancePOTENTIOMETER 5,6,7 AND 8 OUT OF TOLERANCE (READING .011) ON FECU. (C-CHECK) RO: 11/04/2019 WORK PERFORMED BY VENDOR AVMAX.Nov 5, 2019 · N679SA · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR SWIA2019110546705Flap · out of toleranceRH O/B FLAP POP MARKS OUT OF TOLERANCE. (C-CHECK) RO: 11/04/2019 WORK PERFORMED BY VENDOR AVMAX,Nov 5, 2019 · N679SA · Cndair CL6002B19 · Trailing Edge FlapsSDR SWIA2019110546704Potentiometer · out of toleranceRH BPSU POTENTIOMETER OUT OF TOLERANCE. (C-CHECK) RO: 11/04/2019 WORK PERFORMED BY VENDOR AVMAX,Nov 5, 2019 · N679SA · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR SWIA2019110546703Potentiometer · out of toleranceLH BPSU POTENTIOMETER OUT OF TOLERAANCE. (C-CHECK) RO: 11/04/2019 WORK PERFORMED BY VENDOR AVMAX.Nov 5, 2019 · N679SA · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR SWIA2019110546702Support Beam · corrodedFLOOR SUPPORT BEAM AT FS 409+70, ON LBL 9 INBVOARD FLANGE AT FLOOR BOARD NUT PLATE HOLE HAS CORROSION. (C-CHECK) RO: 11/04/2019 PERFORMED REPAIR TO FLOOR SUPPORT BEAM AT FS 409+70 LBL 9. COMPLIED WITH FORM M-337.Nov 5, 2019 · N679SA · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA2019110546701Fitting · corrodedO/B LUG ON O/B PCU FITTING ON RH AILERON HAS CORROSION. (C-CHECK) RO: 11/04/2019 REMOVED CORROSION BY OVERSIZING RH AILERON, OUTBOARD PCU LUG. COMPLIED WITH M-337.Nov 5, 2019 · N679SA · Cndair CL6002B19 · AileronsSDR SWIA2019110546700Fitting · crackedRH WINDOW SIDE POST - LOWER AFT FITTING (CLIP) CRACKED. (C-CHECK) RO: 11/04/2019 REPLACED RH WINDOW SIDE POST LOWER AFT FITTING. COMPLIED WITH M-337.Nov 5, 2019 · N679SA · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA2019110546699Fitting · crackedLH WINDOW SIDE POST - LOWER AFT FITTING (CLIP) CRACKED. (C-CHECK) RO: 11/04/2019 REPLACE LH WINDOW SIDE POST, LOWER AFT FITTING. COMPLIED WITH M-337.Nov 5, 2019 · N679SA · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA2019110546698Support Beam · corrodedVERTICAL FLOOR SUPPORT BEAM AT RBL27 FS 409+128 IS CRACKED AT LOWER INBOARD AFT CORNER. (C-CHECK) RO: 11/04/2019 PERFORMED CUTOUT REPAIR TO VERTICAL FLOOR SUPPORT BEAM AT RBL 27 FS 409+128. COMPLIED WITH M-337.Nov 5, 2019 · N679SA · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA2019110546697Support Beam · crackedVERTICAL FLOOR SUPPORT BEAM AT LBL27 FS 409 +128 IS CRACKED AT LOWER INBOARD AFT CORNER. (C-CHECK) RO: 11/04/2019 PERFORMED REPAIR TO FLOOR SUPPORT BEAM LBL 27 FS 409+128. COMPLIED WITH M-337.Nov 5, 2019 · N679SA · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA2019110546696Structure · crackedFLOOR FRAME AT FS280 IS CRACKED IN 2 SPOTS RBL9 AND LBL12. (C-CHECK) RO: 11/04/2019 WORK PERFORMED BY VENDOR AVMAX. COMPLIED WITH M-337.Nov 5, 2019 · N679SA · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA2019110546689Doubler · corrodedCABIN - PRESS FLOOR DOUBLER AND WEB CORROSION FS424 - 439 RBL38 - 42. (C-CHECK) RO: 11/04/2019 BLENDED OUT CORROSION TO PRESSURE FLOOR PANEL. COMPLIED WITH M-337.Nov 5, 2019 · N679SA · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA2019110546679Floor Panel · corrodedCABIN - PRESSURE FLOOR CORROSION. FS424 - 439, LBL38-42. (C-CHECK) RO: 11/04/2019 BLENDED OUT CORROSION TO PRESSURE FLOOR PANEL. COMPLIED WITH M-337.Nov 5, 2019 · N679SA · Cndair CL6002B19 · Fuselage Floor PanelSDR SWIA2019110546677Door Sill · corrodedCABIN - PRESSURE FLOOR - WEB & DOUBLER CORRODED FS439-449 RBL38-42. (C-CHECK) RO: 11/04/2019 BLENDED OUT CORROSION ON PRESSURE FLOOR SILL PANEL AND ANGLE. BLENDS WITHIN LIMITS. COMPLIED WITH M-337.Nov 5, 2019 · N679SA · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA2019110546676Frame · chafedCHAFE DAMAGE AT AFT EDGE OF RH FRAME AT FS559+48 BETWEEN STR2R AND STR3R. (C-CHECK) RO: 11/04/2019 PERFORMED REPAIR TO FRAME DAMAGE AT FS 559+48 BETWEEN STR 2R AND 3R. COMPLIED WITH M-337.Nov 5, 2019 · N679SA · Cndair CL6002B19 · Fuselage Main, FrameSDR SWIA2019110546675Door Sill · corrodedCORROSION ON RH OTBD FLOOR SILL BETWEEN FS559 AND FS559+32. (C-CHECK) RO: 11/04/2019 REPLACED FLOOR SILL AT FS 559-559+16 TO 559+32. COMPLIED WITH M-337.Nov 5, 2019 · N679SA · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA2019110546674Support Fitting · damagedMECHANICAL DAMAGE ON THE INTERNAL FACE OF THE BACKUP FITTING FOR THE I/B HINGE FITTING ES14.47 FOR THE L/H ELEVATOR. (C-CHECK) RO: 11/04/2019 REPLACED SUPPORT FITTING AT ES 14.47. COMPLIED WITH M-337.Nov 5, 2019 · N679SA · Cndair CL6002B19 · Elevator Miscellaneous StructureSDR SWIA2019110546673Attach Fitting · corrodedCORROSION IN THE BORE AND BADLY WORN BUSHING AT THE OTBD LUG OF THE LH AILERON INBD PCU ATTACH FITTING. RADIAL CHAFE ON THE OTBD FACE. (C-CHECK) RO: 11/04/2019 REMOVED CORROSION FROM BORE OF LH AILERON I/B PCU FITTING BY OVERSIZING. COMPLIED WITH M-337.Nov 5, 2019 · N679SA · Cndair CL6002B19 · AileronsSDR SWIA2019110546672Fitting · corrodedPCU FITTING ON R/H AILERON HAS CORROSION AROUND THE INNER BUSHINGS. (C-CHECK) RO: 11/04/2019 REMOVED CORROSION ON RH AILERON PCU FITTINGS BY REAMING LUGS. COMPLIED WITH M-337.Nov 5, 2019 · N679SA · Cndair CL6002B19 · AileronsSDR SWIA2019110546671Spar · damagedDAMAGED SPAR, LH IB FLAP BETWEEN WS 58.505 TO WS 61.506. (C-CHECK) RO: 11/04/2019 REPLACED DAMAGED SPAR/INTERCOSTAL. COMPLIED WITH M-337.Nov 5, 2019 · N679SA · Cndair CL6002B19 · Trailing Edge FlapsSDR SWIA2019110546670Rib · damagedDAMAGED RIB LH IB FLAP AT WS 91.338. (C-CHECK) RO: 11/04/2019 REPLACED DAMAGED RIB INSIDE LH I/B FLAP. COMPLIED WITH M-337.Nov 5, 2019 · N679SA · Cndair CL6002B19 · Trailing Edge FlapsSDR SWIA2019110546669Intercostal · corrodedPASSENGER DOOR CUT-OUT AREA-AFT FRAME FS 349.00 TO FS364.00, WL84.206 CORRODED INTERCOSTAL (FWD) FLAGGED. (C-CHECK) RO: 11/04/2019 PERFORMED REPAIR TO PAX DOOR INTERCOSTAL AT FS 349-364 WL 84.206. COMPLIED WITH M-337.Nov 5, 2019 · N679SA · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA2019110546668Pump · damagedL/H BOOST PUMP 4 EA. FLAW INDICATIONS EMITTING FROM SATELLITE HOLES. (C-CHECK) RO: 11/04/2019 COMPLIED WITH CARD 51-900-1003-SKY AND FORM M-337Nov 5, 2019 · N679SA · Cndair CL6002B19 · Fuel Boost PumpSDR SWIA201946667Bulkhead · gougedAFT PRESSURE BULKHEAD WEB GOUGED W.L. 108, RBL 18.00. (C-CHECK) RO: 11/04/2019 ACCOMPLISHED BY VENDOR AVMAXNov 5, 2019 · N679SA · Cndair CL6002B19 · Fuselage Main, Bulkhead
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