N975SW

Service difficulty reports · 184

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 = 'N975SW' 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 SWIA2026050175976Steering Sys · warning messageSTEERING INOPERATIVE CAUTION MESSAGE AFTER TAKEOFF. RAN QRH, CAUTION MESSAGE REAPPEARED. AFTER LANDING IN IAH TRY N/S AGAIN AND IT WORKED (FLIGHT 5110) COMPLIED WITH INSPECTION HARNESS IN REF AMM 32-61-25. NO DEFECT NOTE AT THIS TIME. COMPLIED WITH RVDT RIMay 1, 2026 · N975SW · Cndair CL6002B19 · Landing Gear Steering SystemSDR SWIA2026031975550Landing Gear · warning messageODI EVENT RETURN TO FIELD FOR GEAR DISAGREED, ON DEPARTURE CREW REPORTED A DISAGREE NLG DID NOT RETRACT, USED MANUAL RELEASE TO EXTEND ALL GEAR, MEL 32-30-1CAT A. PLACARD INSTALLED (FLIGHT 6022) INSPECTED OLEO PROX SENSOR & BRACKET. T/S IAW FIM 32-60-09Mar 19, 2026 · N975SW · Cndair CL6002B19 · Nose/Tail Landing GearSDR SWIA202507280001Control Unit · warning messagePLEASE T/S ANTI-ICE DUCT WARNING EVENT AT NEXT MX VISIT. RECOMMEND CHECKING THE LOOPS ON THE LEFT SYSTEMMCI TYPE: TROUBLESHOOTING PRIORITY 1 (FLIGHT 5139 - FILED CLOSED)JUL 26, 2025 STATION: DEN--TROUBLESHOT ANTI-ICE DUCT MSG REFERENCING FIM 36-20-00. PERFORJul 26, 2025 · N975SW · Cndair CL6002B19 · Pneumatic Indicating SystemSDR SWIA202507030624Warning Message · false activationIN SLN, GOT ANTI-ICE DUCT WARNING, RAN QRH. DIVERTED TO SLN TO AVOID CLOUDS (FLIGHT 5824 - FILED CLOSED)AFTER BRIEF INVESTIGATION WITH FLIGHT CREW, IT WAS REPORTED THE LEFT WING WAS INDICATING RED ANTI ICE DUCT WARNING ON EICAS. INSPECTED LEFT WING THERMAL SENJun 24, 2025 · N975SW · Cndair CL6002B19 · Overheat DetectionSDR SWI2025F00767Warning Message · activatedIN SLN, GOT ANTI-ICE DUCT WARNING, RAN QRH. DIVERTED TO SLN TO AVOID CLOUDS (FLIGHT 5824 - FILED OPEN)THIS IS CURRENTLY A WORK IN PROGRESSJun 24, 2025 · N975SW · Cndair CL6002B19 · Central WarningSDR SWIA202505060002Cabin Pressure · malfunctionedCABIN ALT HIGH AT ABOUT 12000 (FLIGHT 5105 - FILED OPEN) THIS DISCREPANCY WAS TRANSFERRED TO CAMP ITEM 30073312. "REFER TO CP 30085873 FOR REMOVAL AND REPLACEMENT OF THE CABIN PRESSURE SELECTOR PANEL ASSEMBLY.May 2, 2025 · N975SW · Cndair CL6002B19 · Cabin Pressure Control SystemSDR SWI2025F00623Cabin Pressure · malfunctionedCABIN ALT HIGH AT ABOUT 12000 (FLIGHT 5105 - FILED OPEN)THIS IS CURRENTLY A WORK IN PROGRESSMay 2, 2025 · N975SW · Cndair CL6002B19 · Cabin Pressure Control SystemSDR SWIA202502070003Warning Message · illuminatedDIVERTED TO SBN ENROUTE TO ORD, RECIEVED ANTI-ICE DUCT WARNING MESSAGE, SYNOPTIC PAGE SHOWED LEFT WING LEADING EDGE INDICATING IN THE RED, RAN QRH, OUT OF ICING CONDITIONS, DIVERTES TO SBN. RECIEVED DURING CLIMB AT AROUND 16,000 FT. (FLIGHT 5687 - FILED CLOFeb 3, 2025 · N975SW · Cndair CL6002B19 · Central WarningSDR SWIA2024062000019Solenoid · faultedD:GEAR DISAGREE ON APPROACH HLN, QRH RESOLVED WITH GEAR UP, THEN DOWN.C:MEL 32-30-1CAT A DUE 6/20/24PSEU CODE DO44DOWN ERRGEAR DISAGREE ON APPROACH HLN, QRH RESOLVED WITH GEAR UP, THEN DOWN. FOUND CODE DO44DOWN ERR ON THE PSEU NOSE GEAR EXTEND SOLENOID, DJun 19, 2024 · N975SW · Cndair CL6002B19 · Nose/Tail Landing GearSDR SWIA202400508419Insert · misalignedFLOOR PANEL 231CLF PAX-DOOR FWD HANDRAIL CUP INSERTS DO NOT ALIGN. (C-CHECK RO 5/6/2024) REMOVED AND INSTALLED NEW PAX-DOOR FWD HANDRAIL CUP AT FLOOR PANEL 231CLF REF CRJ-200 SRM 51-42-06 AND DWG 601R31527 REV AM. COMPLIED WITH 51-900-1003-SKY AND SEE CONApr 19, 2024 · N975SW · Cndair CL6002B19 · Fuselage Floor PanelSDR SWIA202405080417Skin · bentRH WING, OTBD GROUND SPOILER SKIN IS BENT UP BY THE INBD HINGE (C-CHECK RO 5/6/2024) REPAIRED R/H WING OUTBOARD GROUND SPOILER REF EO CL-600-2B19-57-L07907, REV. IR, 4-22-2024.COMPLIED WITH 51-900-1003-SKY.Apr 17, 2024 · N975SW · Cndair CL6002B19 · SpoilersSDR SWI2024050800362Hinge · wornUPON REMOVAL ON JOB HN00144442 CAMP #27928759, FOUND L/H ELEVATOR L/E HINGE FITTING ASSY P/N 600-24043-1 @ ES16.52 TO HAVE PITTING CORROSION IN BEARING BORE. REPLACE HINGE FITTING ASSY. (C-CHECK RO 5/6/2024) ORDERED, RECEIVED, AND INSTALLED 1 EA NEW HINGE Mar 19, 2024 · N975SW · Cndair CL6002B19 · Elevator StructureSDR SWI2024050800394Intercostal · misinstalledEMPENNAGE FS654.50 TO FS672.20 INTERCOSTAL 4L REPAIR IMPROPERLY INSTALLED (C-CHECK RO 5/6/2024) PERFORMED REPAIR PROPERLY AT FS654.50 TO FS672.20 ON INTERCOSTAL 4L REF CRJ-200 SRM 51-42-06 , CRJ-200-SRM 51-42-13 , DWG 601R35003 REV -U, DWG 601R35210 REVMar 14, 2024 · N975SW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWI2024050800393Latch · corrodedCREW ESCAPE HATCH OUTER HANDLE HOUSING IS CORRODED (C-CHECK RO 5/6/2024) REMOVED AND INSTALLED NEW CREW ESCAPE HATCH HANDLE HOUSING P/N 601R33050-1 REF.CRJ-200 SRM 51-42-06 AND DRAWING 600-33046 REV F COMPLIED WITH 51-900-1003-SKY AND PRESSURE CHECK GOOD Mar 14, 2024 · N975SW · Cndair CL6002B19 · Emergency ExitsSDR SWIA202405080314Intercostal · crackedEMPENNAGE FS672.20 INTERCOSTAL 4L TAB CRACKED (C-CHECK RO 5/6/2024) REMOVED AND INSTALLED NEW INTERCOSTAL TAB AT FS672.20 STR 4L REF CRJ-200 SRM 51-42-06 AND DWG 601R35210 REV -M. COMPLIED WITH M-337 AND SKYWEST TASK CARD 51-900-1003-SKY.Mar 14, 2024 · N975SW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA202405080313Stringer · crackedPREVIOUS REPAIRED STIFFNER AT LH STRINGER 3 CRACKED AT FS280 MARKED (C-CHECK RO 5/6/2024) REPAIRED L/H STRINGER 3 AT FS 280 REF REO 601R-53-21-3686 REV -- DATE 2024-03-28 . COMPLIED WITH 51-900-1003-SKY AND PRESSURE CHECKS GOOD . SEE CONTINUATION CARD FORMar 13, 2024 · N975SW · Cndair CL6002B19 · Fuselage Main, Longeron/StringerSDR SWI2024050800382Floor Support · corrodedLH PRESSURE FLOOR SILL PANEL HAS SEVERAL AREAS OF CORROSION FROM FS409.00+128 - FS559.00 (MARKED) (C-CHECK RO 5/6/2024) REPAIRED L/H PRESSURE FLOOR SILL PANEL FROM FS409.00+128 - FS449.00 REF REO 601R-53-41-666 REV. -C DATED 2012-11-06 AND REO 601R-53-4Mar 12, 2024 · N975SW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWI2024050800381Attach Angle · crackedFS484.00 RBL27 - 34, FLIGHT CONTROL CABLE ROLLER GUIDE ASSY, INBD ATTACH ANGLE IS CRACKED (MARKED) (C-CHECK RO 5/6/2024) REMOVED AND REPLACED FS484.00 RBL27 - 34, FLIGHT CONTROL CABLE ROLLER GUIDE ASSY, INBD ATTACH ANGLE REF. CRJ 200 SRM 51-42-21, AND DWG Mar 12, 2024 · N975SW · Cndair CL6002B19 · Fuselage Main, Attach FittingsSDR SWI2024050800380Floor Support · corrodedFS499.00 - FS513.00 RBL9, FLOOR SUPPORT CAP CORRODED IN SEVERAL AREAS (MARKED (C-CHECK RO 5/6/2024) )REPAIRED RBL 9 FLOOR SUPPORT FS424.00 TO FS 544.00 REF REO 601R-53-41-3224 REV -- DATED 2024-03-25.COMPLIED WITH 51-900-1003-SKY AND SEE CONTINUATION CARD Mar 12, 2024 · N975SW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWI2024050800379Frame · corrodedCORROSION ON FRAME FS 574.00 BETWEEN STGR 26R - 21L (C-CHECK RO 5/6/2024) REPLACED FRAME AT FS574 REF BOMBARDIER DWG 601R36024 REV N, BOMBARDIER DWG 601R35005 REV AG, BOMBARDIER DWG 601R35031 REV AG, CRJ200 SRM 51-42-06 AND SRM 51-42-21 DRAWING 601R35226Mar 12, 2024 · N975SW · Cndair CL6002B19 · Fuselage Main, FrameSDR SWI2024050800378Frame · corroded* FRAME AT FS319 HAS CORROSION ON FORWARD SIDE BETWEEN STR27 AND STR26L. (C-CHECK RO 5/6/2024) REPAIRED FRAME AT FS319 BETWEEN STR 27 - STR 26L REF REO 601R-53-21-3684 REV - DATED 2024-03-28 AND CRJ-200-SRM 51-42-06. COMPLIED WITH 51-900-1003-SKY AND PRESSMar 12, 2024 · N975SW · Cndair CL6002B19 · Fuselage Main, FrameSDR SWI2024050800377Floor Support · corrodedRH PRESSURE FLOOR SILL PANEL HAS SEVERAL AREAS OF CORROSION FROM FS409.00+128 - FS449.00 (MARKED) (C-CHECK RO 5/6/2024) REPAIRED R/H PRESSURE FLOOR SILL PANEL FROM FS409.00+128 - FS449.00 REF REO 601R-53-41-666 REV. -C DATED 2012-11-06. PRESSURE CHECK GMar 12, 2024 · N975SW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWI2024050800376Attach Angle · crackedFS484.00 LBL27 - 34, FLIGHT CONTROL CABLE ROLLER GUIDE ASSY, INBD ATTACH ANGLE IS CRACKED (MARKED) (C-CHECK RO 5/6/2024) REMOVED AND REPLACED FS484.00 LBL27 - 34, FLIGHT CONTROL CABLE ROLLER GUIDE ASSY, INBD ATTACH ANGLE REF. CRJ 200 SRM 51-42-21, AND DWGMar 12, 2024 · N975SW · Cndair CL6002B19 · Fuselage Main, Attach FittingsSDR SWIA20240508312Frame · corroded* FRAME AT FS310 HAS CORROSION ON AFT SIDE BETWEEN STR27 AND STR26L. (C-CHECK RO 5/6/2024) REMOVED AND INSTALLED NEW FRAME SECTOR AT FS 310 REF DRAWING 601R32002 REV AD , CRJ-200-SRM 51-42-06 AND CRJ-200-SRM 51-42-21 . COMPLIED WITH 51-900-1003-SKY AND PMar 12, 2024 · N975SW · Cndair CL6002B19 · Fuselage Main, FrameSDR SWI2024050800389Bulkhead · crackedCLIP BETWEEN FS621 BULKHEAD AND FRAME FS625.00 BETWEEN THE INTERCOSTAL AND SKIN AT STGR16 SUSPECTED TO BE CRACKED IN THE RADIUS AT THE AFT END. (C-CHECK RO 5/6/2024) REMOVED AND INSTALLED NEW CLIP P/N 601-35012-39 BETWEEN FS621 AND FS625 AT STGR 16R. REF. Mar 11, 2024 · N975SW · Cndair CL6002B19 · Fuselage Main, BulkheadSDR SWI2024050800388Strap · corrodedFLOOR SUPPORT STRAP CORRODED AT FS559.00, LBL27 (C-CHECK RO 5/6/2024) REMOVED AND INSTALL NEW FLOOR SUPPORT STRAP AT FS559.00 LBL27 REF CRJ200 SRM 51-42-06 DRAWING NUMBER 601R31025 REV N. COMPLIED WITH 51-900-1003-SKY AND PRESSURE CHECK GOOD. SEE CONTINUAMar 11, 2024 · N975SW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWI2024050800387Floor Support · corrodedCP 27938404 - DURING AUDIT OF 96_72MO TASK CARD 53-900-511(DETAILED INSPECTION OF THE RIGHT LONGERON "T" BRACKETS AND UPPER SURFACE OF PRESSURE FLOOR SILL STRUCTURE) FOUND SUSPECTED CORROSION AT AROUND NUTPLATE HOLES AT APPROXIMATELY FS449.00(MARKED). (C-CHMar 11, 2024 · N975SW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWI202405080389Bulkhead · crackedCLIP BETWEEN FS621 BULKHEAD AND FRAME FS625.00 BETWEEN THE INTERCOSTAL AND SKIN AT STGR16 SUSPECTED TO BE CRACKED IN THE RADIUS AT THE AFT END. (C-CHECK RO 5/6/2024) REMOVED AND INSTALLED NEW CLIP P/N 601-35012-39 BETWEEN FS621 AND FS625 AT STGR 16R. REF. Mar 11, 2024 · N975SW · Cndair CL6002B19 · Fuselage Main, BulkheadSDR SWI2024050800354Channel · bentAFT COMPARTMENT DOOR FORWARD DOOR GUIDE STRUCTURE CENTER CHANNEL FLANGES ARE BENT. (FLAGGED) (C-CHECK RO 5/6/2024) REMOVED AND INSTALLED NEW AFT CARGO DOOR FWD CHANNEL PART # 601R35050-21 REF DWG NO 601R35050 REV AC AND CRJ200 SRM 51-42-06. COMPLIED WITH 5Mar 10, 2024 · N975SW · Cndair CL6002B19 · Cargo/Baggage DoorsSDR SWIA202405080309Drag Angle · crackedPASSENGER DOOR. SUSPECT AFT DRAG ANGLE CRACKED BY THE MOTOR ASSIST PULLEY (C-CHECK RO 5/6/2024) REPAIRED PASSENGER DOOR AFT DRAG ANGLE REF CRJ-200 SRM 51-42-06 ,SRM 51-42--13, SRM 51-42-22 AND REO 601R-52-11-513 REV -C DATE 2020-10-22 FOR FASTENER AND FABRMar 9, 2024 · N975SW · Cndair CL6002B19 · Passenger/Crew DoorsSDR SWI2024050800390Window Post · crackedCRACK NOTED AT L/H WINDSHIELD SIDE POST SUPPORT ANGLE BELOW WL110 (MARKED) (C-CHECK RO 5/6/2024) REMOVED AND INSTALLED NEW SUPPORT ANGLE P/N 601R34032-21 REF CRJ200 SRM 51-42-06 AND DWG# 601R34032 REV-P. COMPLIED WITH 51-900-1003-SKY AND PRESSURE CHECKS GOMar 8, 2024 · N975SW · Cndair CL6002B19 · Fuselage Main, StructureSDR SWIA202405080308Window Post · crackedCRACK NOTED AT L/H WINDSHIELD SIDE POST (MARKED), (C-CHECK RO 5/6/2024) REMOVED AND INSTALLED NEW LH WINDSHIELD SIDE POST. REF. CRJ200 SRM 51-41-02, SRM 51-42-21 AND DWG# 601R33007 REV. U. PRESSURE CHECK GOOD AT THIS TIME. SEE CONTINUATION CARD FOR WORK AMar 8, 2024 · N975SW · Cndair CL6002B19 · Fuselage Main, StructureSDR SWIA2024050800307Skin · dentedR/H INBD GRND SPOILER HAS MULTIPLE DENTS AND EROSION NOTED ON INNER SKIN (MARKED) (C-CHECK RO 5/6/2024) REMOVED RH INBD GROUND SPOILER & INSTALLED NEW/ SERVICEABLE RH INBD GROUND SPOILER, PN 601R10822-2, S/N SB/RJ/802. REF CRJ 200 AMM 27-65-01-400-801 TORQMar 7, 2024 · N975SW · Cndair CL6002B19 · SpoilersSDR SWIA202266740Shutoff Valve · faultedCABIN ALT CAUTION AT 14000FT FOLLOWED BY CABIN ALT WARNING. OBSERVED EICAS CABIN ALT 10000FT. MASKS DEPLOYED. EXECUTED EMERGENCY DESCENT. PRESSURE RETURNED TO NORMAL BELOW 10000FT. LT PACK MELD. RT PACK THE ONE FAILED. (FLIGHT 5030) TROUBLESHOT LOSS OF PNov 9, 2022 · N975SW · Cndair CL6002B19 · Cabin Pressure Control SystemSDR SWIA202264820None · crackedL/H ENG LWR O/B THRUST REVERSER MAIN TRACK IS CRACKED (FILED CLOSED) REMOVED AND REPLACED LH ENGINE LOWER O/B THRUST REVERSER MAIN TRACK I REF TO CRJ200 AMM 78-34-15 / OPS CHECK GOOD AT THIS TIME.Mar 10, 2022 · N975SW · Cndair CL6002B19 · Engine Exhaust SystemSDR SWIA202264819None · missingAFT CARGO DOOR IS MISSING THE STOP RETAINER FROM FWD TRACK (FILED CLOSED) REPLACED AFT CARGO DOOR STOP RETAINER AT FWD TRACK IN REFERENCE TO CRJ 200 AMM 52-31-00.Mar 10, 2022 · N975SW · Cndair CL6002B19 · DoorsSDR SWIA2020041050110Spring · corrodedRH OVER WING EMERGENCY EXIT DOOR OPENING MECHANISM SPRINGS ARE CORRODED. (C-CHECK) RO 4/9/2020 REMOVED RH LATCH OVERWING EMERGENCY EXIT DOOR (EES), REMOVED CORRODED SPRINGS ON RH LATCH OVERWING EMERGENCY EXIT DOOR (EES), INSTALLED NEW SPRINGS P/N: 600-3140Feb 13, 2020 · N975SW · Cndair CL6002B19 · Emergency ExitsSDR SWIA2020041050085Support Bracket · crackedR/H OUTBOARD FLAP CENTER HINGE SUPPORT BRACKET FOUND TO BE CRACKED. REF CAMP # 20390223 (C-CHECK) RO 4/9/2020 R/H OUTBOARD FLAP IS BEING REPLACED ON NR0219 CAMP# 20262710 FLAP ORDERED/RECIEVED ON REQ# 00028611Feb 1, 2020 · N975SW · Cndair CL6002B19 · Trailing Edge FlapsSDR SWIA2020041050109Seat Track · corrodedON THE MAIN DECK. SEAT TRACK CORRODED BETWEEN FS 409.00+112 AND FS559.00+3 RBL9 (C-CHECK) RO 4/9/2020 REMOVED & REPLACED SEAT TRACK PN# 7075-T6511 BETWEEN FS 409+112 FS 559 RBL 9 IAW CRJ200 SRM.Jan 28, 2020 · N975SW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR SWIA2020041050108Seat Track · corrodedON THE MAIN DEACK, SEAT TRACK CORRODED BETWEEN FS409.00+128 AND FS559.00 LBL9 (C-CHECK) RO 4/9/2020 REMOVED & REPLACE SEAT TRACK PN# 7075-T6511 BETWEEN FS STA 409.00+128 AND FS 559 LBL 9 IAW CRJ200 SRMJan 28, 2020 · N975SW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR SWIA2020041050117Fitting · brokenBROKEN ACTUATOR FITTING FORWARD HANDRAIL PASSENGER DOOR REF IPC 52-11-05 ITEM # 170 (C-CHECK) RO 4/9/2020 INSTALLED NEW ACTUATOR FITTING ON PASSENGER DOOR FORWARD HANDRAIL IAW CRJ-200 AMMJan 24, 2020 · N975SW · Cndair CL6002B19 · Passenger/Crew DoorsSDR SWIA2020041050084Door Sill · crackedUPPER INTERIOR PAX DOOR SILL F.S. 282 @ STRGR 4 LT. IS CRACKED THROUGH FASTENERS BOTH SIDES. (C-CHECK) RO 4/9/2020 REMOVED ANGLE CRACKED AT UPPER INTERIOR PAX DOOR SILL AREA FS 282 AND STGR 4 LT AND INSTALLED NEW BRACKET P/N 600-31057-19. IAW CRJ200 SRMJan 21, 2020 · N975SW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA2020041050107Fastener · corrodedRUDDER POSITION POTENTIOMETER LINKAGE HAS CORRODED HARDWARE AND THE LINKAGE IS HARD TO MOVE AT THE VERTICLE STABILIZER LOWER REAR SPAR. (C-CHECK) RO 4/9/2020 REMOVED AND REPLACED HARDWARE ON RUDDER POSITION POTENTIOMETER LINKAGE IAW CRJ200 AMM. TORQUE WRENJan 17, 2020 · N975SW · Cndair CL6002B19 · Rudder Miscellaneous StructureSDR SWIA2020041050106Strap · corrodedCORROSION ON UPPER PRESSURE FLOOR SILL ASSEMBLY ON THE RT.SIDE FROM FS STA. 557 TO FS STA. 562 RBL 40R TO RBL 47R. (C-CHECK) RO 4/9/2020 REMOVE AND REPLACED UPPER PRESSURE FLOOR STRAP ON THE RT SIDE FROM FS STA 557 TO STA 562 RBL 40 R TO RBL 47 R IAW CRJan 16, 2020 · N975SW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA2020041050105Fastener · corrodedRIGHT OUTBOARD GROUND SPOILER CENTER HINGE FITTING HARDWARE CORRODED. (C-CHECK) RO 4/9/2020 REMOVED AND REPLACED CORRODED HARDWARE ON R/H WING OUTBOARD GROUND SPOILER CENTER HINGE FITTING I.A.W. CRJ200 AMM. TORQUED TO 80 IN/LB TORQUE WRENCH: STS 3744 DUJan 16, 2020 · N975SW · Cndair CL6002B19 · SpoilersSDR SWIA2020041050104Nut · corrodedRIGHT INBOARD GROUND SPOILER OUTBOARD HINGE FITTING HARDWARE CORRODED. (C-CHECK) RO 4/9/2020 REMOVED AND REPLACED RIGHT INBOARD GROUND SPOILER OUTBOARD HINGE FITTING NUT, AND 2 WASHERS. TORQUED AND INSTALLED NEW COTTER PIN. IAW CRJ200 AMM. TORQUE WRENCH Jan 16, 2020 · N975SW · Cndair CL6002B19 · SpoilersSDR SWIA2020041050103Fastener · corrodedRIGHT FLIGHT SPOILER OUTBOARD HINGE FITTING HARDWARE CORRODED. (C-CHECK) RO 4/9/2020 REMOVED AND REPLACED RIGHT FLIGHT SPOILER OUTBOARD HINGE FITTING HARDWARE IAW CRJ200 AMM. TORQUE WRENCH S/N: 0518901770 CAL DUE: 05-APR-2020Jan 16, 2020 · N975SW · Cndair CL6002B19 · SpoilersSDR SWIA2020041050102Fastener · corrodedRIGHT FLIGHT SPOILER #3 HINGE FITTING HARDWARE CORRODED. (C-CHECK) RO 4/9/2020 REMOVED & REPLACED CORRODED HARDWARE ON R/H FLIGHT SPOILER #3 HINGE FITTING IAW CRJ200 AMM. TORQUE WRENCH: STS-3744 S/N: 06100333638 DUE DATE: 14-JAN-2021Jan 16, 2020 · N975SW · Cndair CL6002B19 · SpoilersSDR SWIA2020041050101Fastener · corrodedRIGHT FLIGHT SPOILER #2 HINGE FITTING HARDWARE CORRODED. (C-CHECK) RO 4/9/2020 REMOVED & REPLACED CORRODED HARDWARE ON R/H FLIGHT SPOILER #2 HINGE FITTING IAW CRJ200 AMM. ORQUE WRENCH: STS-3818 S/N: 518901775 DUE DATE: 05-APRIL-20Jan 16, 2020 · N975SW · Cndair CL6002B19 · SpoilersSDR SWIA2020041050100Nut · corrodedRIGHT FLIGHT SPOILER INBOARD HINGE FITTING HARDWARE CORRODED. (C-CHECK) RO 4/9/2020 REPLACED CORRODED NUT ON RIGHT FLIGHT SPOILER INBOARD HINGE AND BOLTS ON OUTBOARD ANTI-ROTATION PLATE IAW CRJ200 AMM. TORQUE WRENCH STS-0381 CAL. DATE 10-DEC-91Jan 16, 2020 · N975SW · Cndair CL6002B19 · Spoilers
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