# Service difficulty reports: N908SW

A list on [N908SW](https://openairdocs.org/aircraft/N908SW.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 4 · 168 reports

- [SDR SWIA202265973](https://openairdocs.org/sdr/SWIA202265973.md): None · cracked · Jun 28, 2022 · N908SW · Cndair CL6002B19 · Fuselage Structure (General)
  > REFERENCE CP 25064700-1 FOR ORIGINAL DISCREPANCY. CRACK ON RH COCKPIT WINDSHIELD/WINDOW SIDE POST (P/N 601R33223-2) REQUIRES REPAIR/REPLACEMENT. FORM M-337 HAS BEEN INITIATED.THIS IS CLASSIFIED AS A MAJOR REPAIR. (FILED CLOSED) REMOVED AND REPLACED RHS WI
- [SDR SWIA202265371](https://openairdocs.org/sdr/SWIA202265371.md): None · odor · Apr 16, 2022 · N908SW · Cndair CL6002B19 · Fuel Selector/Shut-Off Valve
  > L XFLOW SOV CAUTION MESSAGE IN FLIGHT. RAN THE QRH. TRIED TO MANUAL CROSSFLOW FUEL TO THE RIGHT TANK AND DISCOVERED THE L XFLOW SOV FAILED OPEN. WE ATTEMPTED TO START THE APU DURING THE DESCENT BELOW 10,000 MSL, BUT EXPERIENCED A VERY STRONG SMELL OF JET FUEL
- [SDR SWIA202161314](https://openairdocs.org/sdr/SWIA202161314.md): None · none · Aug 25, 2021 · N908SW · Cndair CL6002B19 · Fuselage Main, Longeron/Stringer
  > NON CONFORMING REPAIR FOUND AT RBL 9.0 OUTBOARD INTERCOSTAL AT FS 280.0 (C-CHECK RO 9-30-21) REMOVED AND REPLACEDRBL9 INTERCOSTAL @ FS280.00. REF DWG 601R31113 REV AC, CRJ200 SRM 51-42-06, AND CRJ200 SRM 51-42-21. COMPLIED WITH TASK CARD 51-900-1003-SKY
- [SDR SWIA2021092961313](https://openairdocs.org/sdr/SWIA2021092961313.md): Retainer · corroded · Aug 16, 2021 · N908SW · Cndair CL6002B19 · Fuselage Main, Structure
  > SERVICE DOOR SURROUND AREA, CORROSION ON CLIP AT AFT CORNER FS349 AND STGR 18R. (C-CHECK RO 9-30-21) REMOVED AND REPLACED CLIP AT FS349, STGR 18R. REF. CRJ200 SRM 51-42-21, SRM 51-41-02 AND DWG# 601R38303 REV. AR TOOL: TUC5659 CAL. DUE DATE 02/28/22 /
- [SDR SWIA202161312](https://openairdocs.org/sdr/SWIA202161312.md): None · cracked · Aug 15, 2021 · N908SW · Cndair CL6002B19 · Fuselage Main, Frame
  > FRAME AT FS333.00 ABOVE PAX DOOR IS CRACKED AT A TOOLING HOLE. LOCATION MARKED WITH FLAG (C-CHECK RO 9-30-21) REMOVED AND INSTALLED NEW FS333.00 FRAME BETWEEN STGR 0 & STGR 3L. REF: CRJ200 SRM 51-42-06, CRJ200 SRM 51-42-21, CRJ200 SRM 51-21-16, AND DWG 6
- [SDR SWIA202161311](https://openairdocs.org/sdr/SWIA202161311.md): None · corroded · Aug 14, 2021 · N908SW · Cndair CL6002B19 · Aileron Tabs
  > R/H OTBD FLAP HAS APPROX. 16 SMOKING RIVETS ON THE UPPER SKIN (C-CHECK RO 9-30-21) REMOVED AND REPLACED 16 EA. FASTENERS ON R/H OTBD FLAP UPR SKIN. REF REO 601R-57-53-1227 REV -- DATED 2021-08-19. COMPLIED WITH TASK CARD 51-900-1003-SKY.
- [SDR SWIA202161310](https://openairdocs.org/sdr/SWIA202161310.md): Rib · gouged · Aug 12, 2021 · N908SW · Cndair CL6002B19 · Wing Structure
  > GOUGE ON RH IB FLAP RIB AT IB END. (C-CHECK RO 9-30-21) REMOVED AND INSTALLED NEW R/H INBOARD RIB AT INBOARD END AND RESTORED FINISH. REF: CRJ200 SRM 51-42-06, CRJ200 SRM 51-45-00, CRJ200 SRM 51-42-15, CRJ200 SRM 51-21-16 AND DWG. # 601R14002 REV K FOUN
- [SDR SWIA202161308](https://openairdocs.org/sdr/SWIA202161308.md): None · corroded · Aug 9, 2021 · N908SW · Cndair CL6002B19 · Doors
  > CORROSION UNDER STOP FITTINGS ON ANGLE AT SERVICE DOOR SURROUND AREA BETWEEN FS319 AND FS349. (C-CHECK RO 9-30-21) REMOVED AND REPLACED WITH SERVICE DOOR LOWER ANGLE REF CRJ200 SRM 51-42-06 AND 51-42-21 AND DRAWING 601R38303, REV AR. COMPLIED WITH 51-900
- [SDR SWIA202161295](https://openairdocs.org/sdr/SWIA202161295.md): None · gouged · Aug 7, 2021 · N908SW · Cndair CL6002B19 · Doors
  > *R/H OTBD FLAP INBD HINGE FITTINGS ON THE WING LOCATED AT WS178 HAVE SMALL GOUGES ON THE CENTER LUGS. (C-CHECK RO 9-30-21) BLENDED OUT GOUGE DAMAGE ON R/H OTBD FLAP HINGE CENTER LUG @ WS178.00 TO A SMOOTH CONTOUR AND RESTORED FINISH. REMAINING MATERIAL I
- [SDR SWIA202161292](https://openairdocs.org/sdr/SWIA202161292.md): None · none · Aug 7, 2021 · N908SW · Cndair CL6002B19 · Doors
  > AFTER REMOVAL OF PAX DOOR FOUND FUSELAGE SIDE HINGE-PIN HOLES TO BE OVERSIZE USING GO-NO/GO GAUGE G670-521104-101 (C-CHECK RO 9-30-21) REMOVED AND REPLACED PAX DOOR HINGE HALF ON THE FUSELAGE SIDE. REF DWG 601R31527 REV AM AND CRJ200 SRM 53-21-23 REPAIR
- [SDR SWIA202161289](https://openairdocs.org/sdr/SWIA202161289.md): None · corroded · Aug 7, 2021 · N908SW · Cndair CL6002B19 · Fuselage Internal Mounting Structure
  > R/H FLOOR SUPPORT STRAP AT FS559, RBL27 TO RBL45 IS CORRODED (C-CHECK RO 9-30-21) REMOVED AND REPLACED R/H FLOOR SUPPORT STRAP @ FS559.00 BETWEEN RBL27 & RBL45. REF DWG 601R31145 REV M & CRJ-200 SRM 51-42-06. PRESSURE LEAK CHECK GOOD. COMPLIED WITH 51-9
- [SDR SWIA202161286](https://openairdocs.org/sdr/SWIA202161286.md): None · corroded · Aug 4, 2021 · N908SW · Cndair CL6002B19 · Fuselage Internal Mounting Structure
  > * R/H PRESSURE FLOOR SILL PANEL HAS MULTIPLE SPOTS OF CORROSION, MARKED (C-CHECK RO 9-30-21) REMOVED CORROSION ON R/H PRESSURE FLOOR SILL PANEL REF REO 601R-53-41-666 REV -C DATED 2012-11-06 AND REO 601R-53-41-2955 REV -- DATED 2021-08-30. FOUND TO BE I
- [SDR SWIA202161284](https://openairdocs.org/sdr/SWIA202161284.md): None · corroded · Aug 4, 2021 · N908SW · Cndair CL6002B19 · Fuselage Internal Mounting Structure
  > * L/H PRESSURE FLOOR SILL PANEL HAS MULTIPLE SPOTS OF CORROSION, MARKED (C-CHECK RO 9-30-21) BLENDED CORROSION DAMAGE FROM L/H PRESSURE FLOOR SILL TO A SMOOTH CONTOUR AND RESTORED FINISH. REMAINING MATERIAL IN REWORKED AREAS IS WITHIN LIMITS. REF REO 60
- [SDR SWIA202161320](https://openairdocs.org/sdr/SWIA202161320.md): None · corroded · Aug 3, 2021 · N908SW · Cndair CL6002B19 · Fuselage Structure (General)
  > FAB TRACK SEAT 601R31032-21 FOR CAMP 23220100 JOB 27540101 OP 210 (C-CHECK RO 9-30-21) FABRICATED AND INSTALLED NEW SEAT TRACK 601R31032-21, USING EXTRUSION 20276-288-0-0A, PO# T55899, REF. BOMBARDIER REO 601R-53-00-485, REV. D, DATED 2018-01-29 A
- [SDR SWIA2021609291282](https://openairdocs.org/sdr/SWIA2021609291282.md): Skin · chafed · Aug 3, 2021 · N908SW · Cndair CL6002B19 · Wing, Plate/Skin
  > * BOTTOM WING PLANK IS CHAFED AT WS45.00R AND REAR SPAR DATUM, MARKED. (C-CHECK RO 9-30-21) BLENDED OUT CHAFE DAMAGE R/H BOTTOM WING PLANK AT WS45.00R TO A SMOOTH CONTOUR AND RESTORED FINISH. REMAINING MATERIAL IN REWORKED AREAS IS WITHIN LIMITS. REF RE
- [SDR SWIA2021092961281](https://openairdocs.org/sdr/SWIA2021092961281.md): Skin · chafed · Aug 3, 2021 · N908SW · Cndair CL6002B19 · Wing, Plate/Skin
  > * BOTTOM WING PLANK IS CHAFED AT WS45.00L AND REAR SPAR DATUM, MARKED. (C-CHECK RO 9-30-21) BLENDED OUT CHAFE DAMAGE L/H BOTTOM WING PLANK AT WS45.00L TO A SMOOTH CONTOUR AND RESTORED FINISH. REMAINING MATERIAL IN REWORKED AREAS IS WITHIN LIMITS. REF RE
- [SDR SWIA202161319](https://openairdocs.org/sdr/SWIA202161319.md): None · corroded · Aug 2, 2021 · N908SW · Cndair CL6002B19 · Fuselage Structure (General)
  > * SEAT RAIL FROM FS559+112 TO FS621 RBL27 IS CORRODED. (C-CHECK RO 9-30-21) REMOVED AND INSTALLED NEW RBL27 SEAT TRACK FROM FS559.00+112 TO FS621.00 IAW CRJ200 AMM 53-01-11-000-802 AND CRJ200 AMM 53-01-11-400-802
- [SDR SWIA202161318](https://openairdocs.org/sdr/SWIA202161318.md): None · corroded · Aug 2, 2021 · N908SW · Cndair CL6002B19 · Fuselage Structure (General)
  > * SEAT RAIL FROM FS559+112 TO FS621 RBL9 IS CORRODED. (C-CHECK RO 9-30-21) REMOVED AND INSTALLED RBL9 SEAT TRACK FROM FS559+112 TO FS621 IAW CRJ200 AMM 53-01-11-000-802 AND CRJ200 AMM 53-01-11-400-802
- [SDR SWIA202161317](https://openairdocs.org/sdr/SWIA202161317.md): None · corroded · Aug 2, 2021 · N908SW · Cndair CL6002B19 · Fuselage Structure (General)
  > * SEAT RAIL FROM FS559+80 TO FS621 LBL27 IS CORRODED. (C-CHECK RO 9-30-21) REMOVED AND INSTALLED NEW LBL27 SEAT TRACK FROM FS567.00 TO FS621 IAW CRJ200 AMM 53-01-11-000-802 AND CRJ200 AMM 53-01-11-400-802. NO CORROSION PRESENT ON LBL27 SEAT TRACK FROM F
- [SDR SWIA2021092961280](https://openairdocs.org/sdr/SWIA2021092961280.md): Floorbeam · cracked · Aug 2, 2021 · N908SW · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > SUSPECTED CRACK ON FWD SIDE OF FS280 BEAM AT LBL9 (C-CHECK RO 9-30-21) CRACK ON FWD SIDE OF FS 280.0 BEAM AT LBL 9.0 REPAIRED REF BOMBARDIER REO 601R-53-11-926 REV B DATED 2006/05/10 / COMPLIED WITH TASK CARD 51-900-1003-SKY
- [SDR SWIA2021092961276](https://openairdocs.org/sdr/SWIA2021092961276.md): Floorbeam · corroded · Aug 2, 2021 · N908SW · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > * FLOOR BEAM AT RBL27 HAS CORROSIONON OUTBOARD FLANGE AT APPROX FS597. (C-CHECK RO 9-30-21) REPAIRED RBL27 FLOOR BEAM OTBD FLANGE AT APPROX FS597.00 REF CRJ200 SRM 53-00-43 REPAIR NO.1. COMPLIED WITH 51-900-1003-SKY
- [SDR SWIA202161274](https://openairdocs.org/sdr/SWIA202161274.md): Frame · corroded · Aug 2, 2021 · N908SW · Cndair CL6002B19 · Fuselage Main, Frame
  > * FRAME AT FS589 IS CORRODED FROM STR22L TO STR26R (C-CHECK RO 9-30-21) REMOVED/REPLACED FS589.00 LOWER FRAME BETWEEN STGR 20L AND 20R. REF CRJ-200 SRM 51-42-06 AND DWG 601R36025 REV -P. COMPLIED WITH TASK CARD 51-900-1003-SKY. LEAK CHECK GOOD.
- [SDR SWIA202161316](https://openairdocs.org/sdr/SWIA202161316.md): None · corroded · Aug 1, 2021 · N908SW · Cndair CL6002B19 · Fuselage Structure (General)
  > * RBL 9 SEAT RAIL IS CORRODED FROM FS364 TO FS409 (C-CHECK RO 9-30-21) REMOVED SEAT RAIL FS364.00-FS409.00 REF. CRJ200 AMM 53-01-11-000-802. AND INSTALLED SEAT RAIL FS364.00-FS409.00 REF. CRJ200 AMM 53-01-11-400-802, FOUND TO BE BE OUT OF LIMITS PER CR
- [SDR SWIA202161315](https://openairdocs.org/sdr/SWIA202161315.md): None · corroded · Aug 1, 2021 · N908SW · Cndair CL6002B19 · Fuselage Structure (General)
  > * LBL 9 SEAT RAIL IS CORRODED FROM FS364 TO FS409 (C-CHECK RO 9-30-21) REMOVED AND REPLACED LBL9 SEAT RAIL FROM FS364.00 TO FS409.00 REF CRJ200 AMM 53-01-11-000-802 & 53-01-11-400-802
- [SDR SWIA2021092961272](https://openairdocs.org/sdr/SWIA2021092961272.md): Floorbeam · corroded · Aug 1, 2021 · N908SW · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > *FS409.00+64 €“ FS409+80 FLOOR BEAM LBL9 OUTBOARD FLANGE HAS CORROSION. (MARKED) (C-CHECK RO 9-30-21) REPAIRED FS409.00+64 €“ FS409+80 LBL9 FLOOR BEAM OTBD FLANGE REF CRJ-200 SRM 53-00-43 REPAIR NO.- 1. COMPLIED WITH TASK CARD 51-900-1003
- [SDR SWIA2021092961271](https://openairdocs.org/sdr/SWIA2021092961271.md): Bracket · cracked · Aug 1, 2021 · N908SW · Cndair CL6002B19 · Fuselage Main, Attach Fittings
  > BRACKET CRACKED AT LH FS193.0 AT APPROXIMATELY WL 79.50. (MARKED). (C-CHECK RO 9-30-21) REMOVED AND REPLACED LH FS193.0 BRACKET AT APPROXIMATELY WL 79.50. REF DWG 600-33101 REV -R & CRJ200 SRM 51-42-06. COMPLIED WITH TASK CARD 51-900-1003-SKY.
- [SDR SWIA202161270](https://openairdocs.org/sdr/SWIA202161270.md): Floor Support · corroded · Aug 1, 2021 · N908SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > * L/H FLOOR SILL IS CORRODED FROM FS349 TO FS394 (C-CHECK RO 9-30-21) CUT AWAY DAMAGED AREA, FABRICATED AND INSTALLED REPAIR PARTS FOR LH FS349.00 - FS360.00. CORROSION DAMAGE BETWEEN FS360.00 AND FS394.00 TO A SMOOTH CONTOUR AND RESTORED FINISH. REMAI
- [SDR SWIA202161269](https://openairdocs.org/sdr/SWIA202161269.md): Cup · corroded · Aug 1, 2021 · N908SW · Cndair CL6002B19 · Passenger/Crew Doors
  > * AFT PAX DOOR HANDRAIL CUP IS CORRODED (C-CHECK RO 9-30-21) / REMOVED AND REPLACED AFT PAX DOOR HANDRAIL CUP. REF DWG 601R31527 REV AM & CRJ200 SRM 51-42-06. COMPLIED WITH TASK CARD 51-900-1003-SKY.
- [SDR SWIA202161268](https://openairdocs.org/sdr/SWIA202161268.md): None · corroded · Aug 1, 2021 · N908SW · Cndair CL6002B19 · Doors
  > * FORWARD PAX DOOR HANDRAIL CUP IS CORRODED (C-CHECK RO 9-30-21) REMOVED AND REPLACED FWD PAX DOOR HANDRAIL CUP. REF DWG 601R31527 REV AM & CRJ200 SRM 51-42-06. COMPLIED WITH TASK CARD 51-900-1003-SKY.
- [SDR SWIA202161267](https://openairdocs.org/sdr/SWIA202161267.md): None · corroded · Aug 1, 2021 · N908SW · Cndair CL6002B19 · Fuselage Structure (General)
  > * FLOOR BEAM ATTACH "T" BRACKET AT FORWARD CORNER OF PAX DOOR CUTOUT IS CORRODED. (C-CHECK RO 9-30-21) REMOVED AND REPLACED WITH NEW "T" BRACKET, LOCATED AND DRILLED NEW BRACKET REF CRJ200 SRM 51-42-21,51-42-06, DWG 601R32002 REV Y COMPLIED WITH TASK C
- [SDR SWIA202161266](https://openairdocs.org/sdr/SWIA202161266.md): None · corroded · Aug 1, 2021 · N908SW · Cndair CL6002B19 · Fuselage Structure (General)
  > * AFT OUTBOARD WARDROBE MOUNT PLATE IS CORRODED (C-CHECK RO 9-30-21) REMOVED AND REPLACED WITH NE W AFT OTBD WARDROBE MOUNTING PLATE REF CRJ200 SRM 51-42-06, 51-42-13 AND DWG:601R38670, REV -T. COMPIED WITH 51-900-1003-SKY
- [SDR SWIA202161264](https://openairdocs.org/sdr/SWIA202161264.md): None · corroded · Aug 1, 2021 · N908SW · Cndair CL6002B19 · Fuselage Structure (General)
  > * FLOOR BEAM ATTACH "T" BRACKET AT THE FORWARD CORNER OF THE SERVICE DOOR CUTOUT IS CORRODED. (C-CHECK RO 9-30-21) FOUND T BRACKET AT FWD CORNER OF SERVICE DOOR CUTOUT OUT OF LIMITS REF CRJ 200 SRM 53-00-00 AND REPLACED WITH A NEW T BRACKET REF CRJ 200
- [SDR SWIA202161263](https://openairdocs.org/sdr/SWIA202161263.md): None · cracked · Aug 1, 2021 · N908SW · Cndair CL6002B19 · Fuselage Main, Longeron/Stringer
  > * OUTBOARD CLIP RBL9 FLOORBEAM TO FS280 BEAM IS CRACKED. (C-CHECK RO 9-30-21) REMOVED AND INSTALLED NEW RBL9 OTBD CLIP @ FS280.00. REF CRJ200 SRM 51-42-21 & DWG 601R31113 REV AD. COMPLIED WITH TASK CARD 51-900-1003-SKY.
- [SDR SWIA202161259](https://openairdocs.org/sdr/SWIA202161259.md): None · none · Aug 1, 2021 · N908SW · Cndair CL6002B19 · Fuselage Structure (General)
  > * FLIGHT DECK FLOOR SUPPORT ANGLE AT FS280 IS CORRODED (C-CHECK RO 9-30-21) REMOVED/INSTALLED NEW FLIGHT DECK FLOOR SUPPORT ANGLE AT FS280.00 BEAM. REF DWG 600-33100 REV -Y, CRJ200 SRM 51-42-06, & CRJ200 SRM 51-42-21. COMPLIED WITH TASK CARD 51-900-1003
- [SDR SWIA202161256](https://openairdocs.org/sdr/SWIA202161256.md): None · corroded · Aug 1, 2021 · N908SW · Cndair CL6002B19 · Fuselage Structure (General)
  > * INBOARD FORWARD GALLEY MOUNT PLATE IS CORRODED (C-CHECK RO 9-30-21) REMOVED AND REPLACED WITH NEW INBD FWD GALLEY MOUNT PLATE REF CRJ200 SRM 51-42-06 AND DWG: 601R38669, REV N. COMPLIED WITH 51-900-1003-SKY
- [SDR SWIA202161253](https://openairdocs.org/sdr/SWIA202161253.md): None · corroded · Aug 1, 2021 · N908SW · Cndair CL6002B19 · Fuselage Structure (General)
  > * INBOARD AFT GALLEY MOUNT PLATE IS CORRODED (C-CHECK RO 9-30-21) REMOVED AND REPLACED INBD AFT GALLEY MOUNT PLATE. REF DWG 601R38669 REV -N & CRJ200 SRM 51-42-06. COMPLIED WITH TASK CARD 51-900-1003-SKY
- [SDR SWIA202161323](https://openairdocs.org/sdr/SWIA202161323.md): None · corroded · Jul 31, 2021 · N908SW · Cndair CL6002B19 · Flight Control System
  > *LH WING FLIGHT SPOILER OTBD ACTUATOR HAS CORRODED ATTACHING HARDWARE (C-CHECK RO 9-30-21) REPLACED ONE NUT AND COTTER KEY ON THE LH WING FLIGHT SPOILER OTBD ACTUATOR PER THE CRJ 200 AMM 27-64-05-400-801 STEP 1 THRU 3.8(C). / OPERATIONAL TEST GOOD. NO D
- [SDR SWIA202161321](https://openairdocs.org/sdr/SWIA202161321.md): None · corroded · Jul 31, 2021 · N908SW · Cndair CL6002B19 · Flight Control System
  > *LH WING SPOILERON INBD AND OTBD ACTUATORS HAVE CORRODED ATTACHING HARDWARE (C-CHECK RO 9-30-21) REMOVED AND INSTALLED NEW SERVICEABLE HARDWARE ON THE LH WING SPOILERON INBOARD AND OUTBOARD ACTUATORS. REF - CRJ 200 AMM 27-64-01-400-801 STEP 1 THRU STEP 2
- [SDR SWIA202161330](https://openairdocs.org/sdr/SWIA202161330.md): None · corroded · Jul 30, 2021 · N908SW · Cndair CL6002B19 · Horizontal Stabilizer Structure
  > *LH HORIZONTAL STAB INBD HINGE ASSY HAS CORRODED ATTACHING HARDWARE (C-CHECK RO 9-30-21) REPLACED CORRODED HARDWARE WITH NEW HARDWARE ON LEFT HORIZONTAL STABILIZER TO ELEVATOR CENTER HINGE REF CRJ 200 AMM 27-34-01-400-801 STEP 3. C. TUC8619 CAL DUE 31 OC
- [SDR SWIA202161327](https://openairdocs.org/sdr/SWIA202161327.md): None · corroded · Jul 30, 2021 · N908SW · Cndair CL6002B19 · Horizontal Stabilizer Structure
  > *RH HORIZONTAL STAB INBD HINGE ASSY HAS CORRODED ATTACHING HARDWARE (C-CHECK RO 9-30-21) REMOVED AND INSTALLED NEW SERVICEABLE HARDWARE ON THE RH HORIZONTAL STAB INBOARD HINGE ASSEMBLY. REF - CRJ 200 AMM 27-34-01-400-801 STEP 1 THRU STEP 3C (1-13). / OPE
- [SDR SWIA202161325](https://openairdocs.org/sdr/SWIA202161325.md): None · corroded · Jul 30, 2021 · N908SW · Cndair CL6002B19 · Horizontal Stabilizer Structure
  > *RH HORIZONTAL STAB CENTER HINGE ASSY HAS CORRODED HARDWARE (C-CHECK RO 9-30-21) REPLACED CORRODED HARDWARE WITH NEW HARDWARE ON RIGHT HORIZONTAL STABILIZER TO ELEVATOR CENTER HINGE REF CRJ 200 AMM 27-34-01-400-801 STEP 3. C. TORQUE WRENCH TUC8619 CAL DU
- [SDR SWIA202161252](https://openairdocs.org/sdr/SWIA202161252.md): None · gouged · Jul 30, 2021 · N908SW · Cndair CL6002B19 · Electrical/Electronic Compartment Doors
  > A BAY DOOR FUSELAGE SIDE RH FWD FITTING GOUGED (C-CHECK RO 9-30-21) BLENDED GOUGE DAMAGE ON R/H FWD A-BAY DOOR FITTING TO A SMOOTH CONTOUR AND RESTORED FINISH, REF REO 601R-53-21-3474 REV -- DATED 2021-08-06. COMPLIED WITH TASK CARD 51-900-1003-SKY.
- [SDR SWIA202161251](https://openairdocs.org/sdr/SWIA202161251.md): None · chafed · Jul 29, 2021 · N908SW · Cndair CL6002B19 · Ailerons
  > RH FLAP VANE INBD CHAFFED (C-CHECK RO 9-30-21) BLENDED OUT CHAFFING ON RH IB FLAP VANE IB END, FOUND OUT OF LIMITS REF REO 601R-57-52-004 REV D 2012-12-19, AND REPLACED VANE CAP IB END REF CRJ 200 SRM 51-42-13 AND DRAWING 601R14302 REV E. / COMPLIED WI
- [SDR SWIA202161250](https://openairdocs.org/sdr/SWIA202161250.md): None · chafed · Jul 29, 2021 · N908SW · Cndair CL6002B19 · Ailerons
  > LH INBD FLAP VANE OUTBD END CHAFFED (C-CHECK RO 9-30-21) BLENDED OUT CHAFFING ON LH IB FLAP VANE OB END REF CRJ 200 SRM 51-12-00.FOUND TO BE OUT OF LIMITS REF SRM57-00-31. REMOVED AND INSTALLED NEW LH INBOARD FLAP VANE OUTBOARD CAP P/N 601R14303-43. REF
- [SDR SWIA202161332](https://openairdocs.org/sdr/SWIA202161332.md): None · damaged · Jul 12, 2021 · N908SW · Cndair CL6002B19 · Wing Structure
  > REMOVE AND INSTALL RIGHT WING OUTBOARD FLAP HINGE BOX ASSEMBLY WS178.00, WS220.00 AND WS264.00 TO FOM PER AMM (C-CHECK RO 9-30-21) REMOVED RH OUTBOARD FLAP HINGE BOX AT WS 264.00 REF. CRJ 200 AMM 57-21-35-000-803.AND INSTALLED RH OUTBOARD FLAP HINGE BOX
- [SDR SWIA202161248](https://openairdocs.org/sdr/SWIA202161248.md): None · cracked · Jun 25, 2021 · N908SW · Cndair CL6002B19 · Fuselage, Door Hinge
  > COMPLY WITH SCHEDULED MAINTENANCE CODE: AD 2019-08-04/02 40000 FC - COMPLY WITH PARAGRAPH (J) OF AD 2019-08-04 BY: (J)(1) DOING A NONDESTRUCTIVE INSPECTION FOR CRACKING OF THE FORWARD FACE OF THE FUSELAGE STATION (FS) 621 PRESSURE BULKHEAD, IN ACCORDANCE WITH
- [SDR SWIA202161249](https://openairdocs.org/sdr/SWIA202161249.md): None · blocked · Jun 25, 2021 · N908SW · Cndair CL6002B19 · Doors
  > COMPLY WITH SCHEDULED MAINTENANCE CODE: RA44565-601R-52-41-295 N908SW CP17142390-PR - BLENDED AFT LWR PAN OF THE SERVICE DR REF REO 601R-52-41-295. PERM REPAIR REQUIRED WITHIN 6000 FH OF INCORPORATION OF THIS REO., PART NUMBER: 601R38302-91 - DOOR ASSY, SRVC/E
- [SDR SWIA2019111246756](https://openairdocs.org/sdr/SWIA2019111246756.md): Warning Message · false activation · Nov 12, 2019 · N908SW · Cndair CL6002B19 · Trailing Flap Position Indicating System
  > FLAPS FAIL CAUTION MESSAGE CLIMBING THROUGH 13000. FLIGHT # 5422 CLOSEDPERFORMED RESET OF FLAP FAIL MESSAGE IAW FIM, MESSAGE CLEARED. CYCLED FLAPS 5 FULL CYCLES NO DEFECTS NOTED. MCI CREATED FOR 10 FC FLY ON.
- [SDR SWIA201904295789](https://openairdocs.org/sdr/SWIA201904295789.md): Switch · failed · Apr 29, 2019 · N908SW · Cndair CL6002B19 · Engine Thrust Reverser
  > R/H ENG T/R UNLOCK IN FLIGHT PERFORMED QRH DID NOT CLEAR. (FLT#5228) RE-RIGGED THROTTLE LOCKOUT SWITCH IAW AMM. OPS CHECK GOOD, NO DEFECTS NOTED.
- [SDR SWIA2018091245058](https://openairdocs.org/sdr/SWIA2018091245058.md): Web · corroded · Aug 6, 2018 · N908SW · Cndair CL6002B19 · Passenger/Crew Doors
  > PAX DOOR AFT WEB CORRODED. (C-CHECK) RO: 09/11/2018. REMOVED AND REPLACED PAX DOOR AFT WEB IAW SRM.

Next page: https://openairdocs.org/aircraft/N908SW/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 = 'N908SW' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N908SW/reports

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