# Service difficulty reports: N971SW

A list on [N971SW](https://openairdocs.org/aircraft/N971SW.md).

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.

Page 1 of 3 · 143 reports

- [SDR SWIA2026062776352](https://openairdocs.org/sdr/SWIA2026062776352.md): Hinge Box · gouged · Jun 27, 2026 · N971SW · Cndair CL6002B19 · Wing, Control Surface Attach Fittings
  > LEFT 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-
- [SDR SWIA2026050676002](https://openairdocs.org/sdr/SWIA2026050676002.md): Fan · odor · May 6, 2026 · N971SW · Cndair CL6002B19 · Air Distribution Fan
  > FA 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. PER
- [SDR SWIA2026012475096](https://openairdocs.org/sdr/SWIA2026012475096.md): Thrust Reverser · warning message · Jan 24, 2026 · N971SW · Cndair CL6002B19 · Engine Thrust Reverser
  > R 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 FAUL
- [SDR SWIA202406100009](https://openairdocs.org/sdr/SWIA202406100009.md): Tire · blown · Jun 9, 2024 · N971SW · Cndair CL6002B19 · Tire
  > ATC 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. P
- [SDR SWIA2023072700006](https://openairdocs.org/sdr/SWIA2023072700006.md): Unknown · damaged · Jul 6, 2023 · N971SW · Cndair CL6002B19 · Fuselage Main, Frame
  > RH 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-
- [SDR SWIA20230727629](https://openairdocs.org/sdr/SWIA20230727629.md): Unknown · damaged · Jun 29, 2023 · N971SW · Cndair CL6002B19 · Fuselage Main, Frame
  > FOUND 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.
- [SDR SWIA2023072700626](https://openairdocs.org/sdr/SWIA2023072700626.md): Unknown · gouged · Jun 26, 2023 · N971SW · Cndair CL6002B19 · Wing Structure
  > EVALUATE 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 PLA
- [SDR SWIA20230612](https://openairdocs.org/sdr/SWIA20230612.md): Unknown · gouged · Jun 12, 2023 · N971SW · Cndair CL6002B19 · Vertical Stabilizer, Spar/Rib
  > VERITCAL 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 (CL60
- [SDR SWIA20230608](https://openairdocs.org/sdr/SWIA20230608.md): Unknown · corroded · Jun 8, 2023 · N971SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > CARGO 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. CRJ2
- [SDR SWI2023F00157](https://openairdocs.org/sdr/SWI2023F00157.md): Unknown · corroded · Jun 8, 2023 · N971SW · Cndair CL6002B19 · Fuselage Internal Mounting Structure
  > *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 GR
- [SDR SWI2023F00156](https://openairdocs.org/sdr/SWI2023F00156.md): Unknown · corroded · Jun 8, 2023 · N971SW · Cndair CL6002B19 · Fuselage Internal Mounting Structure
  > *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 200
- [SDR SWIA20230607](https://openairdocs.org/sdr/SWIA20230607.md): Unknown · cracked · Jun 7, 2023 · N971SW · Cndair CL6002B19 · Fuselage Main, Frame
  > *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
- [SDR SWI2023F00155](https://openairdocs.org/sdr/SWI2023F00155.md): Unknown · cracked · Jun 7, 2023 · N971SW · Cndair CL6002B19 · Fuselage Main, Frame
  > *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 CR
- [SDR SWI2023F00154](https://openairdocs.org/sdr/SWI2023F00154.md): Unknown · corroded · Jun 6, 2023 · N971SW · Cndair CL6002B19 · Passenger/Crew Doors
  > PAX 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 51-4
- [SDR SWI2023F00153](https://openairdocs.org/sdr/SWI2023F00153.md): Unknown · corroded · Jun 6, 2023 · N971SW · Cndair CL6002B19 · Passenger/Crew Doors
  > PAX 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 SK
- [SDR SWI2023F00152](https://openairdocs.org/sdr/SWI2023F00152.md): Unknown · corroded · Jun 6, 2023 · N971SW · Cndair CL6002B19 · Passenger/Crew Doors
  > PAX 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 SKY
- [SDR SWIA20230606](https://openairdocs.org/sdr/SWIA20230606.md): Unknown · dented · Jun 6, 2023 · N971SW · Cndair CL6002B19 · Trailing Edge Flaps
  > R/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.
- [SDR SWI2023F00151](https://openairdocs.org/sdr/SWI2023F00151.md): Unknown · cracked · Jun 4, 2023 · N971SW · Cndair CL6002B19 · Fuselage Main, Frame
  > POSSIBLE 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 C
- [SDR SWI2023F00150](https://openairdocs.org/sdr/SWI2023F00150.md): Unknown · cracked · Jun 4, 2023 · N971SW · Cndair CL6002B19 · Fuselage Main, Structure
  > *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.
- [SDR SWIA20230604](https://openairdocs.org/sdr/SWIA20230604.md): Unknown · cracked · Jun 4, 2023 · N971SW · Cndair CL6002B19 · Fuselage Main, Structure
  > *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.CO
- [SDR SWIA20230727603](https://openairdocs.org/sdr/SWIA20230727603.md): Unknown · gouged · Jun 3, 2023 · N971SW · Cndair CL6002B19 · Elevator Tab, Attach Fittings
  > LH 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 2023-0
- [SDR SWI2023F00147](https://openairdocs.org/sdr/SWI2023F00147.md): Unknown · bent · May 27, 2023 · N971SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > CARGO 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 CONTINUATI
- [SDR SWIA202307207527](https://openairdocs.org/sdr/SWIA202307207527.md): Unknown · corroded · May 27, 2023 · N971SW · Cndair CL6002B19 · Passenger/Crew Doors
  > PAX 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 DRAWIN
- [SDR SWI2023F00149](https://openairdocs.org/sdr/SWI2023F00149.md): Unknown · damaged · May 25, 2023 · N971SW · Cndair CL6002B19 · Aerodynamic Fairings
  > FOUND 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 51-900-1
- [SDR SWI2023F00148](https://openairdocs.org/sdr/SWI2023F00148.md): Unknown · cracked · May 25, 2023 · N971SW · Cndair CL6002B19 · Fuselage Main, Longeron/Stringer
  > POSSIBLE 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 EX
- [SDR SWIA20230525](https://openairdocs.org/sdr/SWIA20230525.md): Unknown · chafed · May 25, 2023 · N971SW · Cndair CL6002B19 · Wing Miscellaneous Structure
  > LEFT 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-
- [SDR SWIA20230522](https://openairdocs.org/sdr/SWIA20230522.md): Unknown · gouged · May 22, 2023 · N971SW · Cndair CL6002B19 · Cargo/Baggage Doors
  > AFT 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-
- [SDR SWIA202305180007](https://openairdocs.org/sdr/SWIA202305180007.md): Flap System · warning message · May 17, 2023 · N971SW · Cndair CL6002B19 · Trailing Flap Position Indicating System
  > FLAPS 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 TRANSFERR
- [SDR SWIA202264075](https://openairdocs.org/sdr/SWIA202264075.md): None · broken · Jan 29, 2022 · N971SW · Cndair CL6002B19 · Doors
  > PASSENGER 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 BRACKE
- [SDR SWIA202161612](https://openairdocs.org/sdr/SWIA202161612.md): None · cracked · Oct 10, 2021 · N971SW · Cndair CL6002B19 · Window/Windshield System
  > CRACKED 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.
- [SDR SWIA202156977](https://openairdocs.org/sdr/SWIA202156977.md): Cable · incorrect · Mar 24, 2021 · N971SW · Cndair CL6002B19 · Power Lever
  > POP 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 REMOV
- [SDR SWIA202156965](https://openairdocs.org/sdr/SWIA202156965.md): Engine · vibration · Mar 18, 2021 · N971SW · Cndair CL6002B19 · Engine (Turbine/Turboprop)
  > RIGHT 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
- [SDR SWIA2020081151727](https://openairdocs.org/sdr/SWIA2020081151727.md): Skin · gouged · Jul 23, 2020 · N971SW · Cndair CL6002B19 · Fuselage Main, Frame
  > FUSELAGE 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.
- [SDR SWIA2020081151726](https://openairdocs.org/sdr/SWIA2020081151726.md): Angle · damaged · Jul 18, 2020 · N971SW · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > RBL 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 CHANGE
- [SDR SWIA2020081151753](https://openairdocs.org/sdr/SWIA2020081151753.md): Seat Track · damaged · Jul 14, 2020 · N971SW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > RBL 9 SEAT TRACK, BETWEEN BS 409+128 TO 559 DAMAGED. FABRICATED A NEW SEAT TRACK IAW REO.
- [SDR SWIA202051752](https://openairdocs.org/sdr/SWIA202051752.md): Seat Track · corroded · Jul 14, 2020 · N971SW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > RBL 9 SEAT TRACK WAS CORRODED BETWEEN BS 559 TO 559+80. FABRICATED A NEW SEAT TRACK IAW REO.
- [SDR SWIA2020081151732](https://openairdocs.org/sdr/SWIA2020081151732.md): Seat Track · corroded · Jul 14, 2020 · N971SW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > FLOOR SEAT TRACK CORRODED IN SEVERAL LOCATIONS AT RBL 9 BETWEEN BS 409 TO 409+128. FABRICATED A NEW SEAT TRACK IAW REO.
- [SDR SWIA2020081151750](https://openairdocs.org/sdr/SWIA2020081151750.md): Seat Track · corroded · Jul 10, 2020 · N971SW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > SEAT TRACK CORRODED AT LBL 9 BETWEEN BS 409 TO 409+128. REPLACED SEAT TRACK IAW AMM.
- [SDR SWIA2020081151749](https://openairdocs.org/sdr/SWIA2020081151749.md): Seat Track · corroded · Jul 10, 2020 · N971SW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > FLOOR 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.
- [SDR SWIA2020081151748](https://openairdocs.org/sdr/SWIA2020081151748.md): Seat Track · corroded · Jul 10, 2020 · N971SW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > CABIN SEAT TRACK CORRODED AND GOUGED. REMOVED & REPLACED THE SEAT TRACK IAW AMM. REPLACED WITH NEW SERVICABLE FABRICATED SEAT TRACK.
- [SDR SWIA2020081151747](https://openairdocs.org/sdr/SWIA2020081151747.md): Angle · corroded · Jul 10, 2020 · N971SW · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > BS 280 J ANGLE WAS CORRODED ALONG ENTIRE LENGTH, REMOVED AND REPLACED THE FWD J CHANNEL IAW SRM
- [SDR SWIA2020081151737](https://openairdocs.org/sdr/SWIA2020081151737.md): Angle · cracked · Jul 10, 2020 · N971SW · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > F.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.
- [SDR SWIA2020081151733](https://openairdocs.org/sdr/SWIA2020081151733.md): Mount · corroded · Jul 10, 2020 · N971SW · Cndair CL6002B19 · Fuselage, Equipment Attach Fittings
  > GALLEY 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.
- [SDR SWIA2020081151725](https://openairdocs.org/sdr/SWIA2020081151725.md): Crossbeam · corroded · Jul 10, 2020 · N971SW · Cndair CL6002B19 · Fuselage Main, Structure
  > BS 280 CROSSBEAM IS CORRODED BETWEEN LBL 9 AND RBL 9. COMPLIED WITH REPAIR IAW REO.
- [SDR SWIA2020081151724](https://openairdocs.org/sdr/SWIA2020081151724.md): Frame · corroded · Jul 9, 2020 · N971SW · Cndair CL6002B19 · Fuselage Main, Frame
  > FRAME 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.
- [SDR SWIA2020081151723](https://openairdocs.org/sdr/SWIA2020081151723.md): Stringer · cracked · Jul 9, 2020 · N971SW · Cndair CL6002B19 · Fuselage Main, Longeron/Stringer
  > FUSELAGE STRINGER 3L IS CRACKED AT F.S. 379.00. REPAIRED CRACKED FUSELAGE STRINGER 3L AT F.S.379.00 IAW SRM.
- [SDR SWIA2020081151751](https://openairdocs.org/sdr/SWIA2020081151751.md): Seat Track · corroded · Jul 8, 2020 · N971SW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > RBL 9 SEAT TRACK WAS CORRODED BETWEEN BS 559 TO 559+80. REMOVED AND REPLACED THE SEAT TRACK WITH NEWLY FABRICATED SEAT TRACK IAW AMM.
- [SDR SWIA2020081151746](https://openairdocs.org/sdr/SWIA2020081151746.md): Cargo Track · corroded · Jul 8, 2020 · N971SW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > RBL 9 CARGO SEAT TRACK IS CORRODED BETWEEN BS. 559+96 TO 574. REMOVED & REPLACED CARGO SEAT TRACK IAW AMM
- [SDR SWIA2020081151745](https://openairdocs.org/sdr/SWIA2020081151745.md): Seat Track · corroded · Jul 8, 2020 · N971SW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > RBL 9 CARGO SEAT TRACK IS CORRODED BETWEEN BS 574 TO 621. REMOVED & REPLACED SEAT TRACK IAW CRJ AMM.
- [SDR SWIA2020081151731](https://openairdocs.org/sdr/SWIA2020081151731.md): Cargo Track · corroded · Jul 8, 2020 · N971SW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > LBL 9 CARGO TRACK IS CORRODED BETWEEN F.S. 559+96 TO F.S. 574. REMOVED AND REPLACED THE CARGO TRACK IAW AMM.

Next page: https://openairdocs.org/aircraft/N971SW/reports.md?page=2

## The whole list in SQL

Runs in DuckDB 1.2 or later on the release's Parquet files over HTTPS:

```sql
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' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N971SW/reports

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