# Service difficulty reports: N929SW

A list on [N929SW](https://openairdocs.org/aircraft/N929SW.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 6 · 288 reports

- [SDR SWIA202507300022](https://openairdocs.org/sdr/SWIA202507300022.md): A/C Pack · faulted · Jul 22, 2025 · N929SW · Cndair CL6002B19 · Cabin Cooling System
  > WHILE ENROUTE FROM LNK TO DEN AT FLIGHT LEVEL 240,RECEIVED A LEFT PACK OVERPRESS CAUTION MESSAGE AND AIRCRAFT STARTED TO DEPRESSURIZE. PERFORMED EMERGENCY DECENT AND DIVERTED TO EAR. CABIN ALT WARNING AND CAUTION ILLUMINATED. MEL 21-51-1CCAT C. (FLIGHT 4648
- [SDR SWIA20250723002](https://openairdocs.org/sdr/SWIA20250723002.md): A/C Pack · warning message · Jul 22, 2025 · N929SW · Cndair CL6002B19 · Cabin Cooling System
  > WHILE ENROUTE FROM LNK TO DEN AT FLIGHT LEVEL 240,RECEIVED A LEFT PACK OVERPRESS CAUTION MESSAGE AND AIRCRAFT STARTED TO DEPRESSURIZE. PERFORMED EMERGENCY DECENT AND DIVERTED TO EAR. CABIN ALT WARNING AND CAUTION ILLUMINATED. MEL 21-51-1, CAT C. (FLT 4648)
- [SDR SWIA202507150614](https://openairdocs.org/sdr/SWIA202507150614.md): Skin · dented · Jun 14, 2025 · N929SW · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > INADVERTENTLY DENTED SKIN AFT OF FS621 AT STR 13L. REPAIRED DAMAGE IAW REO 601R-53-61-8346 REV -- DATED 202506-17. COMPLETED TASK CARD 51-900-1003-SKY AND ATTACHED COMPLETED FORM 337. NO WEIGHT CHANGE NOTED
- [SDR SWI2025F00898](https://openairdocs.org/sdr/SWI2025F00898.md): Floor Support · out of limits · Jun 10, 2025 · N929SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > BLENDED LOCATION AROUND NUTPLATE ON PRESSURE FLOOR SILL MEMBER AT FS 424 WAS FOUND TO BE OUT OF LIMITS OF GENERIC REO 601R-53-41-666 REV C DATED 2012-11-06 UT THICKNESS CHECK FOUND REMAINING LOWEST THICKNESS TO BE.039 MIN ALLOWED IS.040 UNDER THE 1.2 DISPOSI
- [SDR SWIA20250715607](https://openairdocs.org/sdr/SWIA20250715607.md): Skin · corroded · Jun 7, 2025 · N929SW · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > FUSELAGE RH LOWER SKIN HAS NUMEROUS AREAS OF CORROSION & TOOLING MARKS/GOUGES UNDER SEALANT BED FOR PANEL 192BB FROM FS 409.00+64 STGR 21 TO FS 409.00+80 STGR 27. (C-CHECK RO 07/15/2025)REPAIRED RH LOWER SKIN UNDER 192BB IAW REO 601R-53-31-1338 REV -- DATEF 2
- [SDR SWIA20250715606](https://openairdocs.org/sdr/SWIA20250715606.md): Floor Support · out of limits · Jun 6, 2025 · N929SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > LH PRESSURE FLOOR SILL FS439.00 TO FS473.15 HAS THREE AREAS AROUND NUTPLATES THAT ARE OUT OF REPAIRABLE LIMITS OF REO 601R-53-41-666 AND REQUIRE SPECIFIC ENGINEERING AND REPAIR. (C-CHECK RO 07/15/2025)REPAIRED LH PRESSURE FLOOR FS439 TO FS473.15 IAW MHIRJ REO
- [SDR SWIA202507150601](https://openairdocs.org/sdr/SWIA202507150601.md): Angle · corroded · Jun 1, 2025 · N929SW · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > FS 409.00+128 PRESSURE BULKHEAD LOWER CAP ANGLE IS CORRODED BETWEEN STRGS 25R AND 26R. (C-CHECK RO 07/15/2025)REPAIRED FS409+128 PRESSURE BULKHEAD LOWER CAP ANGLE IAW MHIRJ REO 601R-53-41-3323 REV. - -, DATED 2025-06-09. COMPLETED SKYCARD 51-900-1003-SKY A
- [SDR SWIA20250715522](https://openairdocs.org/sdr/SWIA20250715522.md): Floor Support · corroded · May 22, 2025 · N929SW · Cndair CL6002B19 · Fuselage Internal Mounting Structure
  > RBL 9.0 FLOOR SUPPORT CAP CORRODED ON OUTBOARD FLANGE FS 559+58 TO FS 559+80 (C-CHECK RO 07/15/2025)REPAIRED RBL 9 CAP AT FS 559+58- FS 559+96 IAW CRJ 200 SRM 53-00-43. COMPLETED MAJOR REPAIR TASK CARD 51-900-1003-SKY AND ATTACHED COMPLED FORM 337. NO WEIGHT
- [SDR SWIA20250715517](https://openairdocs.org/sdr/SWIA20250715517.md): Skin · damaged · May 17, 2025 · N929SW · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > WHILE PERFORMING SKY WEST TASK 53-900-622 SMOKING RIVETS WERE NOTED AT THE RHS LONGITUDINAL SKIN SPLICE AT STGR6R FROM FS409 TO FS409+48 AND MISSING RIVET CSK HEADS AT FS409+32 2EA. AREAS OF SMOKING AND MISSING FASTENERS ARE MARKED ON A/C (C-CHECK RO 07/15/2
- [SDR SWI2025F00902](https://openairdocs.org/sdr/SWI2025F00902.md): Frame · corroded · May 12, 2025 · N929SW · Cndair CL6002B19 · Fuselage Main, Frame
  > CORROSION ON FRAME AT FS 319 BETWEEN STGR 27 -22L (C-CHECK RO 07/15/2025)REPLACED FRAME AT FS 319 P/N 601R32003-65 IAW CRJ 200 SRM 51-42-06, 51-42-21, AND 51-23-00. COMPLETED TASK CARD 51-900-1003-SKY AND ATTACHED COMPLETED FORM 337. NO WEIGHT CHANGE NOTED.
- [SDR SWIA2025071500512](https://openairdocs.org/sdr/SWIA2025071500512.md): Stiffener · chafed · May 12, 2025 · N929SW · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > VERTICAL "Z" STIFFENER AT B.L. 0.00 ON AFT SIDE OF F.S. 621.00 BULKHEAD HAS CHAFE DAMAGE FROM APU SHUTOFF VALVE. (C-CHECK RO 07/15/2025)COMPLETED CHAFE REPAIR OF VERTICAL Z STIFFENER @ BL0 ON AFT SIDE OF FS621 BULKHEAD PER REO 601R-53-61-8338 REV--, DATED 202
- [SDR SWIA2025071500511](https://openairdocs.org/sdr/SWIA2025071500511.md): Floorbeam · corroded · May 11, 2025 · N929SW · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > LBL9 FLOOR BEAM IS CORRODED BETWEEN FS409+5 AND FS409+118. (C-CHECK RO 07/15/2025)REPAIRED LBL 9 FLOORBEAM CAP AT FS 409+5 -FS 409+42 IAW CRJ 200 SRM 53-00-43. FOUND ALL OTHER AREAS WITHIN LIMITS IAW REO 601R-53-00-005 REV A DATE 02-NOV-94. COMPLETED TASK CAR
- [SDR SWI2025F00901](https://openairdocs.org/sdr/SWI2025F00901.md): Floor Support · corroded · May 10, 2025 · N929SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > RBL9 FLOOR SUPPORT IS CORRODED BETWEENFS409+128 AND FS439 (C-CHECK RO 07/15/2025)REPAIRED RBL 9 PRESSURE FLOOR SUPPORT CAP IAW REOS 601R-53-41-3229 REV -- DATED 2025-06-27 ABD 601R-53-41-3228 REV A DATED 2025-06-30. COMPLETED TASK CARD 51-900-1003-SKY AND AT
- [SDR SWI2025F00900](https://openairdocs.org/sdr/SWI2025F00900.md): Floor Support · corroded · May 10, 2025 · N929SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > RH PRESSURE FLOOR SILL PANEL IS CORRODED BETWEEN FS409+128 AND FS559. (C-CHECK RO 07/15/2025)REPAIRED RH PRESSURE FLOOR SILL PANEL CORROSION BETWEEN FS409+128 AND FS559 IAW BOMBARDIER REO 601R-53-41-666 REV C DATED 2012-11-06 COMPLETED TASK CARD 51-900-1003-S
- [SDR SWIA2025071500510](https://openairdocs.org/sdr/SWIA2025071500510.md): Floor Support · corroded · May 10, 2025 · N929SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > LH PRESSURE FLOOR SILL PANEL IS CORRODED BETWEEN FS409+128 AND FS559. REPAIRED LH PRESSURE FLOOR SILL PANEL AT FS 409+128 - FS 559 IAW REO 601R-53-41-666 REV C DATED 2012-11-06. COMPLETED TASK CARD 51-900-1003-SKY AND ATTACHED COMPLETED FORM 337. NO WEIGHT CH
- [SDR SWI2025F00899](https://openairdocs.org/sdr/SWI2025F00899.md): Striker · damaged · May 8, 2025 · N929SW · Cndair CL6002B19 · Passenger/Crew Doors
  > MINOR DAMAGE TO THE SEAL STRIKER FOR PAX DOOR FS 310.00 AND FS 349.00 APPROXIMATELY STR 6L. REPAIRED DAMAGE TO SEAL STRIKER ON PAX DOOR AT FS 310 AND FS 349 AT STR 6L IAW REO 601R-53-22-033 REV D DATED 2014-02-17. COMPLETED TASK CARD 51-900-1003-SKY AND ATTA
- [SDR SWIA202507150508](https://openairdocs.org/sdr/SWIA202507150508.md): Beam · loose · May 8, 2025 · N929SW · Cndair CL6002B19 · Fuselage Main, Structure
  > FUSELAGE FLOOR WING TIE BEAM AT FS 460.00 L/H AND R/H SHIMS ARE LOOSE/MIGRATED. REPAIRED FUSE WING TIE BEAM AT LH AND RH FS 460 IAW REO 601R-53-41-100 REV NC DATED 2002-08-08. COMPLETED TASK CARD 51-900-1003-SKY AND ATTACHED COMPLETED FORM 337. NO WEIGHT CHAN
- [SDR SWIA202507150503](https://openairdocs.org/sdr/SWIA202507150503.md): Vertical Beam · damaged · May 3, 2025 · N929SW · Cndair CL6002B19 · Fuselage Main, Structure
  > DURING INSPECTION OF THE 409+128 VERTICAL POSTS A INDICATION WAS NOTED AT 409+128 RBL18 VERTICAL POST INBD. CHANNEL AT WL69 IN THE RADIUS APPROX.400" IN LENGTH AND 100% FULL SCREEN HEIGHT FAILING NDT. (C-CHECK RO 07/15/2025)REPLACED FS 409+128 RBL 18 POSTS I
- [SDR SWIA20250715427](https://openairdocs.org/sdr/SWIA20250715427.md): Skin · chafed · Apr 27, 2025 · N929SW · Cndair CL6002B19 · Wing, Plate/Skin
  > CENTER WING, LOWER WING PLANK HAS MINOR CHAFE DAMAGE UNDER PANEL 193AB, L/H AND R/H SIDES AT MLG WHEEL WELL. (C-CHECK RO 07/15/2025)REPAIRED CHAFE DAMAGE AT LH AND RH WING PLANKS UNDER PANEL 193AB IAW REO 601R-57-21-880-REV D DATED 2017/03/06. COMPLETED TASK
- [SDR SWIA20250715426](https://openairdocs.org/sdr/SWIA20250715426.md): Panel · mechanic error · Apr 26, 2025 · N929SW · Cndair CL6002B19 · Trailing Edge Flaps
  > MIS-DRILLED FASTENER ON PANEL 584 CB MARKED WITH RED TAPE REQS REMOVAL. (C-CHECK RO 07/15/2025)REMOVED DAMAGE FROM LH WING IB FLAP LOWER SKIN DOUBLER AND RIB AT ST 135.512 IAW REO 6015-57-52-2518 REV -- DATED 2025-06-15. COMPLETED TASK CARD 51-900-1003-SKY AN
- [SDR SWIA202501220076](https://openairdocs.org/sdr/SWIA202501220076.md): Landing Gear · warning message · Jan 20, 2025 · N929SW · Cndair CL6002B19 · Landing Gear Retraction/Extension System
  > GEAR DISAGREE AND NOSE DOOR OPEN WARNING MESSAGES AFTER GEAR UP ACTION AFTER TAKEOFF.C: DEFERRED THE LANDING GEAR RETRACTION SYSTEM PER MEL 32-30-1. MX ACITONS COMPLIED WITH. PLACARDS INSTALLED.CAT: AREPAIRS DUE WITHIN ONE FLIGHT DAY. CAT II NOT AUTHORISED,
- [SDR SWIA2024121701369](https://openairdocs.org/sdr/SWIA2024121701369.md): A/C Pack · faulted · Dec 16, 2024 · N929SW · Cndair CL6002B19 · Cabin Cooling System
  > LEFT PACK WOULD NOT TURN ON DURING THE CLIMB. LEVELED OFF AT 12000 FT WOULD STILL NOT COME ON. CABIN ALT WARNING AND CAUTION MESSAGE CAME ON. WENT INTO MANUAL AND COULD NOT FIX THE ISSUE. (FLIGHT 5078 - FILED CLOSED) INSPECTED LEFT ACM, DUCTING, AND SEN
- [SDR SWIA2024102500004](https://openairdocs.org/sdr/SWIA2024102500004.md): Rib · chafed · Oct 24, 2024 · N929SW · Cndair CL6002B19 · Wing, Fuselage Attach Fittings
  > L/H INBOARD FLAP INBOARD CLOSING RIB AND INBOARD VANE ARE CHAFED. (FILED CLOSED)REMOVED AND REPLACED L/H INBOARD FLAP IAW AMM 27-54-01AND TASK 27-900-1006-SKY OPS CHECK GOOD AT THIS TIME.
- [SDR SWIA202408210001](https://openairdocs.org/sdr/SWIA202408210001.md): Switch · faulted · Aug 20, 2024 · N929SW · Cndair CL6002B19 · Flight Control System
  > AFTER TAKE OFF ON DEPARTURE WE RECEIVED A MACH TRIM, STAB TRIM, AND STALL FAIL MESSAGE. QRH DID NOT RESOLVE, MOVING AND PULLING ON CAPTAIN SIDE STAB TRIM DISCONNECT SWITCH ALLOWED STAB/MACH TRIM TO BE REENGAGED. (FLIGHT 4735 - FILED CLOSED) REMOVED AND
- [SDR SWIA2023101900118](https://openairdocs.org/sdr/SWIA2023101900118.md): Unknown · warning message · Oct 18, 2023 · N929SW · Cndair CL6002B19 · Landing Gear System
  > GEAR DISAGREE WARNING MSG WHEN SELECTING GEAR DOWN ON APPROACH. COMPLIED WITH QRH. GEAR CAME DOWN. (FLIGHT 5768 FILED CLOSED) PLEASE REFERENCE AML 1230956INTERROGATED THE PSEU IAW FIM 32-60-07, FLAGGED, DO44 DOWN, DI20 DOWN ON, SOV DOWN NEAR, DIO9 DOWN OFF, D
- [SDR SWIA202266388](https://openairdocs.org/sdr/SWIA202266388.md): None · damaged · Jul 29, 2022 · N929SW · Cndair CL6002B19 · Doors
  > FOUND DAMAGE PROPAGATION ON PREVEOUSLY DOCUMENTED DAMAGE ON CARGO DOOR. REF. CP 24464106 AND ADM TRACKING #: N929SW7867. (FILED CLOSED) COMPLIED WITH PERMANANT REPAIR TO CARGO DOOR P/N 601R35027 S/N 7712 OUTER SKIN UPPER EDGE BETWEEN FS 574.00 AND FS605.0
- [SDR SWIA202264322](https://openairdocs.org/sdr/SWIA202264322.md): None · damaged · Jan 12, 2022 · N929SW · Cndair CL6002B19 · Fuselage Internal Stairs
  > RH CARGO FLOOR SILL FROM FS559+80 FS 559.00+112 REQURE REPLACEMENT (C CHECK RO 02-12-2022) REMOVED AND INSTALL NEW R/H CARGO FLOOR SILL FROM FS559+80 FS 559.00+112 IAW CRJ-200 SRM 51-42-21, CRJ-200 SRM 51-42-06, CRJ-200-SRM 51-45-00 AND DRW# 601R31133
- [SDR SWIA202264339](https://openairdocs.org/sdr/SWIA202264339.md): None · damaged · Jan 10, 2022 · N929SW · Cndair CL6002B19 · Aileron Tabs
  > FOUND DAMAGED HARDWARE ON RH FLAP HINGE ARM AT WS 220.0. REPLACE MOUNTING HARDWARE. (C CHECK RO 02-12-2022) REPLACED DAMAGED HARDWARE ON RH FLAP HINGE ARM AT WS220 IN REF TO CRJ200 AMM 57-53-02-400-803 / CAL TOOL TUC4822 DUE 30 JUN 2022
- [SDR SWIA202264321](https://openairdocs.org/sdr/SWIA202264321.md): None · damaged · Jan 10, 2022 · N929SW · Cndair CL6002B19 · Fuselage, Door Hinge
  > INCORPORATION OF SB 601R-57-048 REV C IS REQUIRED ON THE RH MLG TRUNNION WEB DUE TO THE REPLACEMENT OF THE RH MLG TRUNNION FITTING. (C CHECK RO 02-12-2022) COMPLIED WITH INCORPORATION OF SB 601R-57-048 REV C INTO NEW R/H TRUNNION WEB REF BOMBARDIER RIL # 3
- [SDR SWIA202264320](https://openairdocs.org/sdr/SWIA202264320.md): None · corroded · Jan 5, 2022 · N929SW · Cndair CL6002B19 · Fuselage Structure (General)
  > WHILE REMOVAL OF RH APRON SKIN FOR REPALCEMENT,FOUND A BOTTOM SUPPORT CHANEL CORRODED. (C CHECK RO 02-12-2022) INSTALLED NEW R/H BOTTOM SUPPORT CHANEL REF DWG 601R31058 REV.R AND CRJ 200 SRM 51-42-06 REV.38 DATED JUL 10/19. COMPLIED WITH 51-900-1003
- [SDR SWIA202264319](https://openairdocs.org/sdr/SWIA202264319.md): None · corroded · Jan 5, 2022 · N929SW · Cndair CL6002B19 · Fuselage Main, Longeron/Stringer
  > *EVIDENCE OF CORROSION BETWEEN INTERCOSTAL AND INTERNAL FUSELAGE SKIN, FS 394.00 €“ 409.00, STGR27 €“ 26L (C CHECK RO 02-12-2022) REMOVED AND INSTALLED NEW INTERCOSTAL ON FS 394.00 - 409.00 STGR 27- 26L REF DWG 601R31049 REV C, CRJ-200-SRM 51-42-06, AND
- [SDR SWIA202264318](https://openairdocs.org/sdr/SWIA202264318.md): None · chafed · Jan 3, 2022 · N929SW · Cndair CL6002B19 · Ailerons
  > RH APRON CHAFED FROM UPPER AND LOWER WING PLANK P SEAL. (C CHECK RO 02-12-2022) REMOVED AND INSTALLED NEW R/H APRON SKIN REF MHIRJ EO DWG 601R31058 SNIEO S13 DATED.2022-01-05. COMPLIED WITH 51-900-1003-SKY AND CRJ 200 SRM 51-42-06 REV.38 DATED JUL 10/19
- [SDR SWIA202264317](https://openairdocs.org/sdr/SWIA202264317.md): None · damaged · Jan 2, 2022 · N929SW · Cndair CL6002B19 · Fuselage Main, Longeron/Stringer
  > DEFECTS NOTED AND MARKED ON PART FS 409.00+32.00 FRAME JOINT ANGLE AT STGR 6 RH (C CHECK RO 02-12-2022) REMOVED AND REPLACED 1EA NEW FRAME JOINT ANGLE P/N 601R32201-12 ON FS 409+32 STGR 6RH CRJ-200 SRM 51-42-06. DWG 601R32202 REV -J. COMPLIED WITH 51-900-
- [SDR SWIA202264316](https://openairdocs.org/sdr/SWIA202264316.md): None · damaged · Jan 2, 2022 · N929SW · Cndair CL6002B19 · Fuselage Main, Longeron/Stringer
  > DEFECTS NOTED AND MARKED ON PART FS 409.00+16 FRAME JOINT ANGLE AT STGR 6 RH (C CHECK RO 02-12-2022) REMOVED AND REPLACED 1EA NEW FRAME JOINT ANGLE P/N 601R32201-12 ON FS 409+16 STGR 6RH CRJ-200 SRM 51-42-06 DWG 601R32201 REV G DWG 601R32202 REV -J COMPLI
- [SDR SWIA202164315](https://openairdocs.org/sdr/SWIA202164315.md): None · corroded · Dec 27, 2021 · N929SW · Cndair CL6002B19 · Fuselage Internal Mounting Structure
  > UPON REMOVAL OF THE PAX DOOR FLOOR SILL ANGLE FOUND CORROSION ON FLOOR STRIKER SEAL AFT CORNER. (C CHECK RO 02-12-2022) REMOVED CORROSION ON FLOOR STRIKER SEAL AFT CORNER REF CRJ200 SRM 51-21-06. FOUND TO BE WITHIN LIMITS REF CRJ200 SRM 53-00-00. RESTOR
- [SDR SWIA202164314](https://openairdocs.org/sdr/SWIA202164314.md): None · corroded · Dec 27, 2021 · N929SW · Cndair CL6002B19 · Fuselage Internal Mounting Structure
  > UPON REMOVAL OF THE PAX DOOR FLOOR SILL ANGLE FOUND CORROSION ON CROSSBEAM AT FS349 APROX LBL41 (C CHECK RO 02-12-2022) REPAIRED CROSSBEAM AT FS349 APROX LBL41 REF. REO 601R-53-21-3521 REV-- DATED: 2022-01-06. COMPLIED WITH 51-900-1003-SKY AND SEE CONTINU
- [SDR SWIA202164312](https://openairdocs.org/sdr/SWIA202164312.md): None · corroded · Dec 27, 2021 · N929SW · Cndair CL6002B19 · Fuselage Internal Mounting Structure
  > UPON REMOVAL OF PAX DOOR FLOOR SILL ANGLE FOUND CORROSION ON PAX DOOR FLOOR SILL APPROX FS 349 (C CHECK RO 02-12-2022) CORROSION REMOVED AT PAX DOOR FLOOR SILL APPROX FS 349 REF CRJ200 SRM 51-21-06, WITHIN LIMITS REF CRJ200 SRM 53-00-00. FINISH RESTORED ON
- [SDR SWIA202164311](https://openairdocs.org/sdr/SWIA202164311.md): None · gouged · Dec 23, 2021 · N929SW · Cndair CL6002B19 · Ailerons
  > * THE RH INBD FLAP INBD HINGE ARM ASSEMBLY IS GOUGED BY THE ATTACHMENT POINT. (MARKED) (C CHECK RO 02-12-2022) REPAIRED RH INBD FLAP INBD HINGE ARM ASSEMBLY BY THE ATTACHMENT POINT REF REO 601R-57-54-344 REV -- 2022-01-12 AND CRJ-200-SRM 51-12-00. COMPLIE
- [SDR SWIA202164310](https://openairdocs.org/sdr/SWIA202164310.md): None · damaged · Dec 19, 2021 · N929SW · Cndair CL6002B19 · Fuselage Internal Mounting Structure
  > PAX DOOR FLOOR SILL FS310-FS349 IS EXFOLIATED NEEDS REPLACED. (C CHECK RO 02-12-2022) REMOVED AND REPLACED PAX DOOR FLOOR SILL ANGLE AT FS 310- FS 349 IAW CRJ 200 SRM 51-42-06, CRJ 200 SRM 51-42-21 AND DWG 601R31527 REV AM COMPLIED WITH TASK CARD 51-900-10
- [SDR SWIA202164329](https://openairdocs.org/sdr/SWIA202164329.md): None · gouged · Dec 18, 2021 · N929SW · Cndair CL6002B19 · Doors
  > * THE CREW ESCAPE HATCH RH HINGE ARM FITTING IS CHAFFED. (MARKED) (C CHECK RO 02-12-2022) REPLACED RIGHT HAND HINGE ARM FITTING WITH NEW FITTING P/N 600-33217-1001 AND RESTORED FINISH TO FITTING REF. CRJ200 SRM 51-41-02 & CRJ200 SRM 51-25-16
- [SDR SWIA202164309](https://openairdocs.org/sdr/SWIA202164309.md): None · cracked · Dec 18, 2021 · N929SW · Cndair CL6002B19 · Fuselage Main, Longeron/Stringer
  > * AFT EQUIPTMENT BAY FS 625 STR 14R CLIP IS CRACKED. (C CHECK RO 02-12-2022) REMOVED AND REPLACED NEW INSTALLED NEW CLIP AT FS 625.00 STGR 14R REF CRJ200 SRM 51-42-21 AND REO 601R-53-61-422 REV NC DATE 2001-08-23. COMPLIED WITH TASK CARD 51-900-1003-SKY AN
- [SDR SWIA202164308](https://openairdocs.org/sdr/SWIA202164308.md): None · cracked · Dec 18, 2021 · N929SW · Cndair CL6002B19 · Fuselage Main, Longeron/Stringer
  > * AFT EQUIPTMENT BAY FS 625 STR 14L CLIP IS CRACKED. (C CHECK RO 02-12-2022) REMOVED AND REPLACED NEW INSTALLED NEW CLIP AT FS 625.00 STGR 14L REF CRJ200 SRM 51-42-21 AND REO 601R-53-61-422 REV NC DATE 2001-08-23. COMPLIED WITH TASK CARD 51-900-1003-SKY AN
- [SDR SWIA202164341](https://openairdocs.org/sdr/SWIA202164341.md): None · worn · Dec 17, 2021 · N929SW · Cndair CL6002B19 · Doors
  > *LH OVERWING EMER DOOR SURROUND DOOR STOP PADS WORN (C CHECK RO 02-12-2022) REMOVED AND REPLACED 6EA NEW STOP PADS P/N: 600-31385-3 AT LH OVERWING EMERGENCY DOOR SURROUND CRJ-200 AMM 52-21-00-400-803.
- [SDR SWIA202164340](https://openairdocs.org/sdr/SWIA202164340.md): None · worn · Dec 17, 2021 · N929SW · Cndair CL6002B19 · Doors
  > *RH OVERWING EMER DOOR SURROUND DOOR STOP PADS WORN (C CHECK RO 02-12-2022) REMOVED AND REPLACED 6EA NEW STOP PADS P/N: 600-31385-3 AT RH OVERWING EMERGENCY DOOR SURROUND CRJ-200 AMM 52-21-00-400-803.
- [SDR SWIA202164338](https://openairdocs.org/sdr/SWIA202164338.md): None · corroded · Dec 17, 2021 · N929SW · Cndair CL6002B19 · Doors
  > *LH OVERWING EMER DOOR HAS CORRODED HARDWARE ON INNER HANDLE ASSY. AREAS MARKED (C CHECK RO 02-12-2022) REMOVED AND REPLACED CORRODED HARDWARE ON INNER HANDLE ASSY REF CRJ200 SRM 51-41-02. OP'S CHECK GOOD.
- [SDR SWIA202164337](https://openairdocs.org/sdr/SWIA202164337.md): None · corroded · Dec 17, 2021 · N929SW · Cndair CL6002B19 · Galley Doors
  > *SERVICE DOOR AFT LOWER ROLLER FITTING HAS CORRODED ATTACHING HARDWARE (FS 349.00) (C CHECK RO 02-12-2022) REPLACED HARDWARE AROUND FITTING AT SERVICE DOOR AFT LOWER ROLLER FITTING (FS349.00) REF CRJ200 SRM 51-41-02. OPS TEST GOOD. TORQUE WRENCH TUC8416 D
- [SDR SWIA202164306](https://openairdocs.org/sdr/SWIA202164306.md): None · corroded · Dec 17, 2021 · N929SW · Cndair CL6002B19 · Fuselage Floor Panel
  > *CORROSION ON FLOOR BEAM FITTING FS 310.00 STGR 18L (C CHECK RO 02-12-2022) REMOVED CORROSION FROM FLOOR BEAM FITTING FS 310 STGR 18L IAW CRJ 200 SRM 51-21-06. FOUND TO BE WITHIN LIMITS. REF REO 601R-53-21-3519 REV -- DATE 2021-12-30. ACCOMPLISHED REPAIR
- [SDR SWIA202164305](https://openairdocs.org/sdr/SWIA202164305.md): None · gouged · Dec 17, 2021 · N929SW · Cndair CL6002B19 · Fuselage Main, Longeron/Stringer
  > *GOUGE ON CLIP ATTACHED TO FS 310.00 AND INTERCOSTAL STGR 5L (C CHECK RO 02-12-2022) INSTALLED NEW CLIP ATTACHED TO FS310 AND INTERCOSTAL AT STGR 5L IAW CRJ200 SRM 51-42-06 PAGE.14 AND CRJ200 SRM 51-42-21 PAGE. 23-24 AND DWG 601R31096 REV D. ALL CHECKS G
- [SDR SWIA202164302](https://openairdocs.org/sdr/SWIA202164302.md): None · corroded · Dec 17, 2021 · N929SW · Cndair CL6002B19 · Fuselage Main, Longeron/Stringer
  > *CORROSION ON GUSSET ATTACHED TO FRAME FS 409.00 AT STGR 25R (C CHECK RO 02-12-2022) REMOVED CORROSION AT GUSSET FRAME FS 409.00 AT STGR 25R REF CRJ 200 SRM 51-21-06. FRAME IS WITHIN LIMITS IAW CRJ-200 SRM 53-00-00 AND SRM 53-21-15. RESTORED FINISH REF SRM
- [SDR SWIA202164300](https://openairdocs.org/sdr/SWIA202164300.md): None · corroded · Dec 17, 2021 · N929SW · Cndair CL6002B19 · Fuselage Main, Longeron/Stringer
  > *CORROSION ON GUSSET ATTACHED TO FS 364.00 BETWEEN STGR 26L €“ 27 (C CHECK RO 02-12-2022) REMOVED CORROSION AT GUSSET FRAME FS 364.00 BETWEEN STGR 26L-27 REF CRJ 200 SRM 51-21-06. / GUSSET IS WITHIN LIMITS IAW CRJ-200 SRM 53-00-00. RESTORED FINISH TO AR

Next page: https://openairdocs.org/aircraft/N929SW/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 = 'N929SW' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N929SW/reports

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