N971SW

Service difficulty reports · 143

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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 = 'N971SW'
  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 SWIA2026062776352Hinge Box · gougedLEFT FLAP HINGE BOX (WS178.00), AFT INBOARD LOWER FLANGE GOUGED (NEAR LUG HOLE). BLENDED LH FLAP HINGE BOX (WS178.00), AFT INBOARD LOWER FLANGE GOUGED (NEAR LUG HOLE), IN REFERENCE TO TO REO 601R-57-21-4116 REV-- DATED 2026-06-27. COMPLETED TASK CARD 51-900-Jun 27, 2026 · N971SW · Cndair CL6002B19 · Wing, Control Surface Attach FittingsSDR SWIA2026050676002Fan · odorFA REPORTED A BURNING RUBBER ODORL ON CLIMB OUT OF CHA. ODOR WENT AWAY AFTER APPROX 10 MINS. NO SMOKE OR OTHER INDICATIONS. MEL 21-40-1ACAT C. (FLIGHT 5660) TROUBLESHOT SMOKE SMELL IN CABIN IN REF TO FIM 21-21-00. FA REPORTS SMOKE CAME FROM FWD GALLEY. PERMay 6, 2026 · N971SW · Cndair CL6002B19 · Air Distribution FanSDR SWIA2026012475096Thrust Reverser · warning messageR REV UNLOCKED CAUTION MESSAGE DURING CLIMB. LEVELED AT 17,000?, RAN QRH. QRH RESOLVED MESSAGE WITH EMER STOW.MEL 78-30-1CAT "C" REF AML 1805384: SMOD APPROVED IS REQUIRED DUE TO ODI (RTF)(FLIGHT 5128) RT THRUST REVERSER PER MEL 78-30-1. DUE TO NATURE OF FAULJan 24, 2026 · N971SW · Cndair CL6002B19 · Engine Thrust ReverserSDR SWIA202406100009Tire · blownATC ADVISED US WE HAD BLOWN A TIRE DEPARTING RUNWAY 8. RETURNED TO DENVER. TIRES REPORTED NORMAL BY EMERGENCY VEHICLES. TIRES NEED INSPECTION PLEASE (FLIGHT 5031 FILED CLOSED)VERIFIED AND CONFIRMED THIS AIRCRAFT IS NOT THE AIRCRAFT WITH THE BLOWN TIRE EVENT. PJun 9, 2024 · N971SW · Cndair CL6002B19 · TireSDR SWIA2023072700006Unknown · damagedRH FUSELAGE DRAG ANGLE NEAR DATUM 61.5625% WAS MIS-DRILLED. FABRICATE A NEW RH DRAG ANGLE (C-CHECK RO 7/23/2023) REMOVED & INSTALLED NEWLY FABRICATED RH FUSELAGE DRAG ANGLE REPAIR SECTION NEAR DATUM 61.5625% REF CRJ 200 SRM 51-42-21 ,CRJ 200 SRM 51-42-Jul 6, 2023 · N971SW · Cndair CL6002B19 · Fuselage Main, FrameSDR SWIA20230727629Unknown · damagedFOUND DOUBLE HOLE ON THE LH FUSELAGE DRAG ANGLE NEAR DATUM 61.5625% (C-CHECK RO 7/23/2023) REPLACED AND PERFORMED REPAIR TO LH FUSELAGE DRAG ANGLE NEAR DATUM 61.5625%. PERFORMED AND COMPLIED WITH ALL STEPS OF REO 601R-55-31-445 REV -- DATED 2023-07-04. Jun 29, 2023 · N971SW · Cndair CL6002B19 · Fuselage Main, FrameSDR SWIA2023072700626Unknown · gougedEVALUATE GOUGE/SCRATCH INSIDE LH WING FUEL BAY UNDER PANEL 540CB, FWD SIDE, ON LOWER WING PLANK STRINGER BETWEEN WS85.50 - WS65.75, STGR 15 (C-CHECK RO 7/23/2023) BLENDED GOUGE/SCRATCH INSIDE LH WING FUEL BAY UNDER PANEL 540CB FWD SIDE ON LOWER WING PLAJun 26, 2023 · N971SW · Cndair CL6002B19 · Wing StructureSDR SWIA20230612Unknown · gougedVERITCAL STAB REAR SPAR AS A GOUGE WITH RAISED METAL ON THE RH TRAILING EDGE (MARKED). (C-CHECK RO 7/23/2023) REPAIRED VERTICAL STAB REAR SPAR GOUGE TO MHIRJ REO 601R-55-31-448 REV -- DATED 2023-06-20COMPLIED WITH SKYWEST TASK CARD 51-900-1003-SKY (CL60Jun 12, 2023 · N971SW · Cndair CL6002B19 · Vertical Stabilizer, Spar/RibSDR SWIA20230608Unknown · corrodedCARGO COMPARTMENT FS621 BULKHEAD FLOOR SUPPORT ANGLE BETWEEN RH FLOOR SILL AND RBL27.00 HAS CORROSION (MARKED) (C-CHECK RO 7/23/2023) REMOVED AND REPLACED CARGO COMPARTMENT FS621 BULKHEAD FLOOR SUPPORT ANGLE BETWEEN RH FLOOR SILL AND RBL27.00 REF. CRJ2Jun 8, 2023 · N971SW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWI2023F00157Unknown · corroded*R/H PRESSURE FLOOR SILL HAS 2EA AREAS OF CORROSION AT APPROX FS424 AND FS529. (C-CHECK RO 7/23/2023) BLENDED OUT CORROSION AT 2EA LOCATIONS ON RH PRESSURE FLOOR SILL AT F.S. 424.00 AND F.S. 554.00. CORROSION AT F.S. 554.00 WAS FOUND WITHIN LIMITS OF GRJun 8, 2023 · N971SW · Cndair CL6002B19 · Fuselage Internal Mounting StructureSDR SWI2023F00156Unknown · corroded*FLOOR SUPPORT STRAP AT FS559 BETWEEN FLOOR BEAM AT LBL27 AND PRESSURE FLOOR SILL IS CORRODED. (C-CHECK RO 7/23/2023) REMOVED AND REPLACED THE FLOOR SUPPORT STRAP AT FS 559 BETWEEN LBL 27 AND THE PRESSURE FLOOR SILL REF DRAWING 601R31025 REV: N, CRJ 200Jun 8, 2023 · N971SW · Cndair CL6002B19 · Fuselage Internal Mounting StructureSDR SWIA20230607Unknown · cracked*FRAME ABOVE PAX DOOR AT FS333 IS CRACKED. (C-CHECK RO 7/23/2023) REMOVED AND INSTALLED NEW FRAME AND ALL REPAIR PARTS WET WITH SEALANT PER REO 601R-53-21-3636 REV -- DATED 2023/06/17.LEAK CHECK GOOD.SEE CONTINUATION CARD FOR DETAILS.COMPLIED WITH TASK Jun 7, 2023 · N971SW · Cndair CL6002B19 · Fuselage Main, FrameSDR SWI2023F00155Unknown · cracked*CLIP ANGLE IN ATF ACCESSORY COMPARTMENT ATTACHING INTERCOSTAL TO FRAME AT FS625, STGR 14L IS CRACKED. (C-CHECK RO 7/23/2023) REMOVED AND REPLACED CRACKED CLIP ANGLE IN AFT ACCESSORY COMPARTMENT ATTACHING INTERCOSTAL TO FRAME AT FS 625 & STGR 14L REF CRJun 7, 2023 · N971SW · Cndair CL6002B19 · Fuselage Main, FrameSDR SWI2023F00154Unknown · corrodedPAX DOOR SILL ANGLE IS CORRODED. FLAGGED (C-CHECK RO 7/23/2023) CORROSION ON PAX DOOR SILL ANGLE FOUND TO BE OUT OF LIMITS DUE TO 100% MATERIAL LOSS. REMOVED DAMAGE SILL ANGLE. LOCATED DRILLED AND INSTALLED NEW PAX DOOR SILL ANGLE. REF CRJ-200 SRM 51-4Jun 6, 2023 · N971SW · Cndair CL6002B19 · Passenger/Crew DoorsSDR SWI2023F00153Unknown · corrodedPAX DOOR AFT HAND RAIL CUP CORRODED. FLAGGED (C-CHECK RO 7/23/2023) REMOVED AND REPLACED PAX DOOR AFT HAND RAIL CUP WITH NEW, REF CRJ 200 SRM 51-42-06 AND DWG 601R31527 REV AMCOMPLIED WITH SKYWEST TASK CARD 51-900-1003-SKY (CL600-2B19)COMPLIED WITH SKJun 6, 2023 · N971SW · Cndair CL6002B19 · Passenger/Crew DoorsSDR SWI2023F00152Unknown · corrodedPAX DOOR FWD HAND RAIL CUP CORRODED. FLAGGED (C-CHECK RO 7/23/2023) REMOVED AND REPLACED PAX DOOR FWD HAND RAIL CUP WITH NEW, REF CRJ 200 SRM 51-42-06 AND DWG 601R31527 REV AMCOMPLIED WITH SKYWEST TASK CARD 51-900-1003-SKY (CL600-2B19)COMPLIED WITH SKYJun 6, 2023 · N971SW · Cndair CL6002B19 · Passenger/Crew DoorsSDR SWIA20230606Unknown · dentedR/H SIDE INBOARD FLAP CENTER LOWER SKIN HAS DENT (MARKED) (C-CHECK RO 7/23/2023) REPAIRED DENT ON R/H I/B FLAP LOWER SKIN REF CRJ 200 SRM 57-52-00, REPAIR #3, FIGURE 202. COMPLIED FULLY W/SKYCARD 51-900-1003-SKY.Jun 6, 2023 · N971SW · Cndair CL6002B19 · Trailing Edge FlapsSDR SWI2023F00151Unknown · crackedPOSSIBLE CRACKED CLIP AT L/H APPROX. FS280 STGR3. FLAGGED (C-CHECK RO 7/23/2023) REMOVED AND INSTALLED 2EA ANGLES AND 1EA CLIP AT APPROX. FS 280 AND STGR 3L REF CRJ200 SRM 51-42-06, CRJ200 SRM 51-42-21 AND DWG# SH600-31057 REV-P. COMPLIED WITH TASK CJun 4, 2023 · N971SW · Cndair CL6002B19 · Fuselage Main, FrameSDR SWI2023F00150Unknown · cracked*CO-PILOTS WINDSHEILD SIDE POST LOWER SUPPORT STUCTURE IS CRACKED (MARKED) (C-CHECK RO 7/23/2023) REPLACED LOWER SUPPORT ANGLE AT CO-PILOT WINDSHIELD SIDE POST. PER CRJ200 SRM 51-42-06 AND BOMBARDIER DWG 601R34032 REV. V. ALL CHECKS GOOD.Jun 4, 2023 · N971SW · Cndair CL6002B19 · Fuselage Main, StructureSDR SWIA20230604Unknown · cracked*PILOTS WINDSHEILD SIDE POST LOWER SUPPORT STUCTURE IS CRACKED (MARKED) (C-CHECK RO 7/23/2023) REMOVED AND INSTALLED NEW PILOT'S WINDSHIELD SIDE POST LOWER SUPPORT STRUCTURE ANGLE PER CRJ 200 SRM 51-42-06 AND DRAWING 601R34032 REV -U, LEAK CHECK GOOD.COJun 4, 2023 · N971SW · Cndair CL6002B19 · Fuselage Main, StructureSDR SWIA20230727603Unknown · gougedLH ELEVATOR FRONT SPAR CENTER HINGE FITTING OUTBOARD FLUTTER DAMPER LUG RADIUS GOUGED (MARKED) (C-CHECK RO 7/23/2023) REPAIRED THE LH ELEVATOR FRONT SPAR CENTER HINGE FITTING INBOARD FLUTTER DAMPER LUG RADIUS REF REO 601R-55-21-582, REV-A, DATED 2023-0Jun 3, 2023 · N971SW · Cndair CL6002B19 · Elevator Tab, Attach FittingsSDR SWI2023F00147Unknown · bentCARGO DOOR FORWARD DOOR TRACK SUPPORT "CHANNEL" IS BENT . FS574.00. (MARKED) (C-CHECK RO 7/23/2023) REMOVED AND REPLACED CARGO DOOR FWD DOOR TRACK SUPPORT CHANNEL@FS574.00 WITH A NEW ON PER DWG 601R35050 REV AC AND CRJ 200 SRM 51-42-06. SEE CONTINUATIMay 27, 2023 · N971SW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA202307207527Unknown · corrodedPAX DOOR, INTERCOSTAL INSIDE THE PRESSURE VALVE CUTOUT APPEARS TO BE CORRODED. (MARKED & FLAGGED) (C-CHECK RO 7/23/2023) REMOVED AND INSTALLED NEW PAX DOOR INTERCOSTAL DD4 FS320.00 - FS338.00. REF: CRJ-200 SRM 51-42-06, CRJ-200 SRM 51-42-21, AND DRAWINMay 27, 2023 · N971SW · Cndair CL6002B19 · Passenger/Crew DoorsSDR SWI2023F00149Unknown · damagedFOUND DOUBLE HOLE ON TAIL CONE 361AL (MARKED) (C-CHECK RO 7/23/2023) REPAIRED DOUBLE HOLES IN TAILCONE PANEL 361AL PER MHIRJ REO 601R-53-84-335 REV -- DATED 07-10-2023, SEE CONTINUE CARD FOR DETAILS OF REO REPAIR.COMPLIED WITH SKYWEST TASK CARD 51-900-1May 25, 2023 · N971SW · Cndair CL6002B19 · Aerodynamic FairingsSDR SWI2023F00148Unknown · crackedPOSSIBLE CRACK ON INTERCOSTAL FOR AC EXTERNAL POWER RECEPTACLE (MARKED) (C-CHECK RO 7/23/2023) REMOVED AND REPLACED THE INTERCOSTAL FOR THE AC EXTERNAL POWER RECEPTACLE, REF CRJ 200 SRM 51-42-06, 51-42-21, AND DRAWING #600-33283 REV -F. ENERGIZED THE EXMay 25, 2023 · N971SW · Cndair CL6002B19 · Fuselage Main, Longeron/StringerSDR SWIA20230525Unknown · chafedLEFT CENTER WING LOWER SKIN IS CHAFED AT THE OUTBOARD AFT END. (MARKED) (C-CHECK RO 7/23/2023) BLENDED LH CENTER WING LOWER SKIN AT OUTBD AFT END. REF CRJ200 SRM 51-12-00. FOUND TO BE OUT OF LIMITS. PERFORMED AND COMPLIED WITH ALL STEPS OF GREO 601R-57-May 25, 2023 · N971SW · Cndair CL6002B19 · Wing Miscellaneous StructureSDR SWIA20230522Unknown · gougedAFT BAGGAGE BAY EXTERIOR DOOR HAS A GOUGE ALONG THE TOP, CENTER OF THE DOOR ON A PREVIOUS REPAIR. FLAGGED (C-CHECK RO 7/23/2023) BLENDED AREA ON AFT BAGGAGE BAY EXTERIOR DOOR ALONG THE TOP, CENTER OF THE DOOR ON A PREVIOUS REPAIR. REF CRJ200 SRM 51-12-May 22, 2023 · N971SW · Cndair CL6002B19 · Cargo/Baggage DoorsSDR SWIA202305180007Flap System · warning messageFLAPS FAIL AT 0 DEGREES DURING CLIMB OUT. RAN QRH. PER THE QRH, OUR MAX LANDING WEIGHT (LIMITED BY MAXIMUM TIRE SPEED) WAS 37,000 LBS. OUR ZFW WAS 42,692, AND WE LANDED AT ABOUT 45,000 LBS. NORMAL LANDING. (FLT 5291, FILED CLOSED)THIS DISCREPANCY WAS TRANSFERRMay 17, 2023 · N971SW · Cndair CL6002B19 · Trailing Flap Position Indicating SystemSDR SWIA202264075None · brokenPASSENGER DOOR INNER HANDLE MOUNTING ASSY BRACKET BROKEN ON INBD SIDE. (FILED - CLOSED) REMOVED PASSENGER DOOR INNER HANDLE MOUNTING ASSEMBLY AFT ANGLE IN REFERENCE TO SRM 51-42-06. SEE CP 24257171 FOR INSTALLATION OF PAX DOOR INNER HANDLE AFT ANGLE BRACKEJan 29, 2022 · N971SW · Cndair CL6002B19 · DoorsSDR SWIA202161612None · crackedCRACKED RH WINDSHIELD, DIVERTED TO DEN. DECLARED EMERGENCY. / NO OVERWEIGHT LANDING (FLIGHT 4682 - FILED CLOSED) REMOVED AND REPLACED RH WINDSHIELD IN PER SKYWEST TASK CARD 56-220-1000-SKY.Oct 10, 2021 · N971SW · Cndair CL6002B19 · Window/Windshield SystemSDR SWIA202156977Cable · incorrectPOP SOUND AT IDLE AT 14000 FEET. RIGHT ENGINE LO PRESS WARNING AND HIGH ITT. ENGINE SHUTDOWN INFLIGHT PERFORMED. FLIGHT 4676 REFERENCE AML 604626 REFERENCE AML 604683 REFERENCE AML 604711, AML 606556, FOR WORK PERFORMED. RIGHT ENGINE FUEL CONTROL REMOVMar 24, 2021 · N971SW · Cndair CL6002B19 · Power LeverSDR SWIA202156965Engine · vibrationRIGHT ENGINE €ŒN2 VIB€? MESSAGE DURING CLIMB. N1 ROLLED BACK BELOW 30%. WE FOLLOWED THE QRH/QRC AND SHUT THE ENGINE DOWN. NO INDICATIONS OF FIRE DISPLAYED AND NO BOTTLES WERE BLOWN. FLIGHT 4710 - FILED CLOSED THIS DISCREPANCY WAS TRANSFERRED TO Mar 18, 2021 · N971SW · Cndair CL6002B19 · Engine (Turbine/Turboprop)SDR SWIA2020081151727Skin · gougedFUSELAGE SKIN GOUGED AT FS 341 BETWEEN STR 24R AND STR 25R. REPAIRED GOUGE IN FUSELAGE SKIN AT FS 341 BETWEEN STR 24R AND STR 25R IAW MHIRJ REO AND SKYWEST TASK CARD.Jul 23, 2020 · N971SW · Cndair CL6002B19 · Fuselage Main, FrameSDR SWIA2020081151726Angle · damagedRBL 9 O/B ATTACH BRACKET @ FS 280 UPPER AFT HOLE HAS NO ED, BREAKS THROUGH EDGE OF INNER L ANGEL (C-CHECK) RO 8/8/2020 REPAIRED BRACKET AT RBL 9 O/B @ F.S. 280 IAW REO FORM 337 FILED AND SKYCARD C/W AND ATTACHED NO WT CHANGEJul 18, 2020 · N971SW · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR SWIA2020081151753Seat Track · damagedRBL 9 SEAT TRACK, BETWEEN BS 409+128 TO 559 DAMAGED. FABRICATED A NEW SEAT TRACK IAW REO .Jul 14, 2020 · N971SW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR SWIA202051752Seat Track · corrodedRBL 9 SEAT TRACK WAS CORRODED BETWEEN BS 559 TO 559+80. FABRICATED A NEW SEAT TRACK IAW REO.Jul 14, 2020 · N971SW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR SWIA2020081151732Seat Track · corrodedFLOOR SEAT TRACK CORRODED IN SEVERAL LOCATIONS AT RBL 9 BETWEEN BS 409 TO 409+128. FABRICATED A NEW SEAT TRACK IAW REO.Jul 14, 2020 · N971SW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR SWIA2020081151750Seat Track · corrodedSEAT TRACK CORRODED AT LBL 9 BETWEEN BS 409 TO 409+128. REPLACED SEAT TRACK IAW AMM.Jul 10, 2020 · N971SW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR SWIA2020081151749Seat Track · corrodedFLOOR SEAT TRACK CORRODED IN SEVERAL LOCATIONS AT RBL9 BETWEEN FS409 TO FS409+128. (C-CHECK) RO 8/8/2020 REMOVED CORRODED SEAT TRACK AT RBL 9 BETWEEN FS 409 TO FS409+128 AND INSTALL NEWLY FABRICATED SERVICEABLE SEAT TRACK IAW CRJ 200 AMM.Jul 10, 2020 · N971SW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR SWIA2020081151748Seat Track · corrodedCABIN SEAT TRACK CORRODED AND GOUGED. REMOVED & REPLACED THE SEAT TRACK IAW AMM. REPLACED WITH NEW SERVICABLE FABRICATED SEAT TRACK.Jul 10, 2020 · N971SW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR SWIA2020081151747Angle · corrodedBS 280 J ANGLE WAS CORRODED ALONG ENTIRE LENGTH, REMOVED AND REPLACED THE FWD J CHANNEL IAW SRMJul 10, 2020 · N971SW · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR SWIA2020081151737Angle · crackedF.S.280.00 FLOORBEAM CLIPS ON THE INBOARD SIDE OF LBL 9.00 AND RBL 9.00 ARE CRACKED. REMOVED AND REPLACED LBL9 AND RBL9 IB CLIPS IAW SRM.Jul 10, 2020 · N971SW · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR SWIA2020081151733Mount · corrodedGALLEY MOUNT PADS, FWD AND AFT, INBOARD OF RBL 9.00 ARE CORRODED AROUND BOLT HOLES. FWD GALLEY MOUNT PAD WAS FOUND TO HAVE NO CORROSION .AFT PAD WAS REMOVED AND REPLACED IAW SRM.Jul 10, 2020 · N971SW · Cndair CL6002B19 · Fuselage, Equipment Attach FittingsSDR SWIA2020081151725Crossbeam · corrodedBS 280 CROSSBEAM IS CORRODED BETWEEN LBL 9 AND RBL 9. COMPLIED WITH REPAIR IAW REO.Jul 10, 2020 · N971SW · Cndair CL6002B19 · Fuselage Main, StructureSDR SWIA2020081151724Frame · corrodedFRAME AT F.S. 349.00 CORRODED BETWEEN STGR 27 AND STGR 26L. (C-CHECK) RO 8/8/2020 REMOVED AND REPLACED F.S.349 FRAME IAW CRJ 200 SRM AND DWG ( FASTENER CALL OUT). COMPLETED AND ATTACHED TASK CARD AND M- 337. NO WEIGHT CHANGE.Jul 9, 2020 · N971SW · Cndair CL6002B19 · Fuselage Main, FrameSDR SWIA2020081151723Stringer · crackedFUSELAGE STRINGER 3L IS CRACKED AT F.S. 379.00. REPAIRED CRACKED FUSELAGE STRINGER 3L AT F.S.379.00 IAW SRM.Jul 9, 2020 · N971SW · Cndair CL6002B19 · Fuselage Main, Longeron/StringerSDR SWIA2020081151751Seat Track · corrodedRBL 9 SEAT TRACK WAS CORRODED BETWEEN BS 559 TO 559+80. REMOVED AND REPLACED THE SEAT TRACK WITH NEWLY FABRICATED SEAT TRACK IAW AMM.Jul 8, 2020 · N971SW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR SWIA2020081151746Cargo Track · corrodedRBL 9 CARGO SEAT TRACK IS CORRODED BETWEEN BS. 559+96 TO 574. REMOVED & REPLACED CARGO SEAT TRACK IAW AMMJul 8, 2020 · N971SW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR SWIA2020081151745Seat Track · corrodedRBL 9 CARGO SEAT TRACK IS CORRODED BETWEEN BS 574 TO 621. REMOVED & REPLACED SEAT TRACK IAW CRJ AMM.Jul 8, 2020 · N971SW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR SWIA2020081151731Cargo Track · corrodedLBL 9 CARGO TRACK IS CORRODED BETWEEN F.S. 559+96 TO F.S. 574. REMOVED AND REPLACED THE CARGO TRACK IAW AMM.Jul 8, 2020 · N971SW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
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