# Service difficulty reports: N917SW

A list on [N917SW](https://openairdocs.org/aircraft/N917SW.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 7 · 309 reports

- [SDR SWIA2026072377766](https://openairdocs.org/sdr/SWIA2026072377766.md): Angle · bent · Jul 23, 2026 · N917SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > LEFT TRU BAY FLOOR ANGLE AT BS 193 BENT AND GOUGED. REPLACED DAMAGED THE LT TRU BAY FLOOR ANGLE WITH NEW FABRICATED ANGLE IAW SRM 51-42-06, & DWG 600-33101, REV R. COMPLIED WITH SKY CARD 51-900-1003-SKY. MAJOR REPAIR.
- [SDR SWIA2026072077763](https://openairdocs.org/sdr/SWIA2026072077763.md): Strap · cracked · Jul 20, 2026 · N917SW · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > FLOORBEAM STRAP CRACKED AT BS 559 BETWEEN RBL 9 & RBL 27. REMOVED AND REPLACED THE FLOORBEAM STRAP WITH NEW IAW DWG 601R31025, REV N, & SRM 51-42-06, REV 38.
- [SDR SWIA2026071677787](https://openairdocs.org/sdr/SWIA2026071677787.md): Seat Track · damaged · Jul 16, 2026 · N917SW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > LBL27 SEAT RAIL SCRATCHED AND CORRODED BETWEEN FS5590094 TO FS56400 C-CHECK RO 10172026REPLACED WITH NEW LBL27 SEAT RAIL BETWEEN FS5590094 TO FS56400 REF CRJ-200 AMM 53-00-49-400-801TOOL USED TORQUE WRENCH IDTUC4978 DUE 31-AUG-26
- [SDR SWIA2026071677786](https://openairdocs.org/sdr/SWIA2026071677786.md): Seat Track · damaged · Jul 16, 2026 · N917SW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > LBL27 SEAT RAIL SCRATCHED AND CORRODED BETWEEN APPROXIMATELY FS56400 TO FS61900 C-CHECK RO 10172026REPLACED WITH NEW LBL27 SEAT RAIL BETWEEN APPROXIMATELY FS56400 TO FS61900 REF CRJ-200 AMM 53-00-49-400-801TOOL USED TORQUE WRENCH IDTUC4978 DUE 31-AUG-26
- [SDR SWIA2026071677785](https://openairdocs.org/sdr/SWIA2026071677785.md): Seat Track · damaged · Jul 16, 2026 · N917SW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > LBL9 SEAT RAIL SCRATCHED AND CORRODED BETWEEN APPROXIMATELY FS559005TO FS5590092 C-CHECK RO 10172026REMOVED ANDINSTALLED NEW LBL9 SEAT RAIL, BETWEEN APPROXIMATELY FS559005 TO FS5590092, REFCRJ 200 AMM 53-01-11-400-802 FOUND THE SEAT TRACK CORROSION IS EXFOL
- [SDR SWIA2026071677784](https://openairdocs.org/sdr/SWIA2026071677784.md): Seat Track · damaged · Jul 16, 2026 · N917SW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > LBL9 SEAT RAIL SCRATCHED AND CORRODED BETWEEN APPROXIMATELY FS5590094 TO FS56400 C-CHECK RO 10172026 REPLACE AND INSTALLED NEW LBL9 SEAT RAIL, BETWEEN APPROXIMATELY FS5590094 TO FS56400, REFCRJ 200 AMM 53-01-11-400-802 FOUND THE SEAT TRACK WITH DEEP PITTING A
- [SDR SWIA2026071677783](https://openairdocs.org/sdr/SWIA2026071677783.md): Seat Track · damaged · Jul 16, 2026 · N917SW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > LBL9 SEAT RAIL SCRATCHED AND CORRODED BETWEEN APPROXIMATELY FS56400 TO FS61900 C-CHECK RO 10172026REMOVED AND INSTALLED NEW LBL9 SEAT RAIL, BETWEEN APPROXIMATELY FS56400 TO FS61900, REFCRJ 200 AMM 53-01-11-400-802 FOUND SEAT TRACK HAS DEEP PITTING AND EXFOL
- [SDR SWIA2026071677782](https://openairdocs.org/sdr/SWIA2026071677782.md): Seat Track · damaged · Jul 16, 2026 · N917SW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > RBL 27 SEAT TRACK SCRATCHED AND CORRODED, BS 559. 48 - 559. 58. REPLACED THE SEAT TRACK IAW AMM 53-01-11-400-802.
- [SDR SWIA2026071677781](https://openairdocs.org/sdr/SWIA2026071677781.md): Seat Track · damaged · Jul 16, 2026 · N917SW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > RBL 27 SEAT TRACK SCRATCHED AND CORRODED BS 559. 94 TO BS 564. REPLACED THE SEAT TRACK, IAW AMM 53-01-11-400-802.
- [SDR SWIA2026071677780](https://openairdocs.org/sdr/SWIA2026071677780.md): Seat Track · corroded · Jul 16, 2026 · N917SW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > RBL 27 SEAT TRACK SCRATCHED AND CORRODED, BS 564 TO 619. REPLACED THE SEAT TRACK, IAW AMM 53-01-11-400-802.
- [SDR SWIA2026071677779](https://openairdocs.org/sdr/SWIA2026071677779.md): Seat Track · scratched · Jul 16, 2026 · N917SW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > LBL 27 SEAT TRACK SCRATCHED AND CORRODED BTWN APPROX BS 559 TO BS 559.94. REPLACED SEAT TRACK, IAW AMM 53-01-11-400-802.
- [SDR SWIA2026071677778](https://openairdocs.org/sdr/SWIA2026071677778.md): Skin · chafed · Jul 16, 2026 · N917SW · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > RIGHT APRON SKIN CHAFED FROM UPPER WING SKIN AND STUB FAIRING CONTACT. REPAIRED RT APRON SKIN IAW SRM 51-42-06, REV 39, AND REO 601R-53-41-115, REV A.
- [SDR SWIA2026071677767](https://openairdocs.org/sdr/SWIA2026071677767.md): Skin · chafed · Jul 16, 2026 · N917SW · Cndair CL6002B19 · Wing, Plate/Skin
  > LEFT APRON SKIN CHAFED FROM UPPER WING SKIN & STUB FAIRING CONTACT. REPAIRED LEFT APRON SKIN UPPER WING SKIN IAW REO 601R-53-41-115, REV A. COMPLIED WITH ALL STEPS OF REO 601R-53-41-115, REV A. COMPLIED WITH 51-900-1003-SKY.
- [SDR SWIA2026071677765](https://openairdocs.org/sdr/SWIA2026071677765.md): Floor Support · corroded · Jul 16, 2026 · N917SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > LEFT FLOOR SUPPORT CORRODED BTWN APPROX BS 559 TO 559.085. REMOVED CORROSION AT LEFT FLOOR SUPPORT IAW SRM 51-21-06. FOUND TO BE OUT LIMITS IAW REO 601R-53-00-526, REV-. REPAIRED LEFT FLOOR SUPPORT IAW REO 601R-53-51-758 REV--, COMPLIED WITH ALL STEPS OF REO
- [SDR SWIA2026070977777](https://openairdocs.org/sdr/SWIA2026070977777.md): Floor Support · corroded · Jul 9, 2026 · N917SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > LEFT PRESSURE FLOOR SUPPORT, BS 449.85 HAD ONE AREA OF CORROSION. REMOVED CORROSION, EVALUATED AND RESTORED IAW STEPS A-F OF REO 601R-53-41-666, REV C. COMPLIED WITH 51-900-1003-SKY.
- [SDR SWIA2026041377776](https://openairdocs.org/sdr/SWIA2026041377776.md): Intercostal · cracked · Apr 13, 2026 · N917SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > AFT SIDE OF AFT PRESSURE BULKHEAD ZEE MEMBER ANGLE AT STR 15L, LBL 36.20 CRACKED. RECEIVED, LOCATED AND DRILLED A NEW INTERCOSTAL IAW SRM 51-42-06. INSTALLED THE NEW INTERCOSTAL IAW DWG 601-35012, REV D, AND SRM 51-42-06. COMPLIED WITH TASK CARD 51-900-10
- [SDR SWIA2026041277775](https://openairdocs.org/sdr/SWIA2026041277775.md): Skin · chafed · Apr 12, 2026 · N917SW · Cndair CL6002B19 · Ailerons
  > LEFT AILERON LEADING EDGE SKIN CHAFED AT MULTIPLE SPOTS. INSTALLED NEW LEADING EDGE SKIN IAW DWG CC670-13000, REV D, SRM 51-42-06, SRM 51-42-21, AND SRM 51-42-22.
- [SDR SWIA2026041077774](https://openairdocs.org/sdr/SWIA2026041077774.md): Door Frame · cracked · Apr 10, 2026 · N917SW · Cndair CL6002B19 · Fuselage Main, Structure
  > RIGHT HINGE FRAME IS CRACKED ON AFT EQUIPMENT BAY DOOR. REMOVED AND REPLACED FRAME AT RT OTBD SIDE AT THE AFT EQUIPMENT BAY DOOR SURROUND WITH NEW IAW SRM 51-42-06, AND DWG 601-36004, REV K.
- [SDR SWIA2026041077768](https://openairdocs.org/sdr/SWIA2026041077768.md): Skin · dented · Apr 10, 2026 · N917SW · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > AT APPROX BS 663 ON STRINGER 23L THERE WERE 2 EXTERNAL DENTS IN CLOSE PROXIMITY TO EACH OTHER. REPAIRED BS 663 SKIN STRINGER 23L, IAW REO 601R-53-61-8602, REV-. COMPLIED WITH 51-900-1003-SKY.
- [SDR SWIA2026040177773](https://openairdocs.org/sdr/SWIA2026040177773.md): Floor Panel · cracked · Apr 1, 2026 · N917SW · Cndair CL6002B19 · Fuselage Floor Panel
  > RIGHT TRU BAY FLOOR CRACKED AT BS 210. REPAIRED THE FLOOR IAW REO 601R-53-11-245, REV -C. REPAIR TYPE II SHEET 4 STEPS 1- 15.
- [SDR SWIA2026040177772](https://openairdocs.org/sdr/SWIA2026040177772.md): Floor Panel · cracked · Apr 1, 2026 · N917SW · Cndair CL6002B19 · Fuselage Floor Panel
  > LEFT TRU BAY FLOOR CRACKED AT BS 210. REPAIRED THE FLOOR IN THE LT TRU BAY IAW REO 601R-53-11-4090, REV-.
- [SDR SWIA2025121577771](https://openairdocs.org/sdr/SWIA2025121577771.md): Floor Support · damaged · Dec 15, 2025 · N917SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > DAMAGE TO PRESSURE FLOOR SUPPORT AT BS 461.5, LBL 41, COMPLIED WITH A PERMANENT REPAIR ON LT PRESSURE FLOOR SUPPORT IAW REO 601R-53-41-3468, REV-. COMPLIED WITH ALL STEPS OF TASK CARD 51-90-1003-SKY.
- [SDR SWIA2025121577770](https://openairdocs.org/sdr/SWIA2025121577770.md): Frame · out of limits · Dec 15, 2025 · N917SW · Cndair CL6002B19 · Fuselage Main, Frame
  > INSPECTION OF LOWER FLANGE OF FRAME BEAM AT BS 513. COMPLIED WITH SB 601R-53-088, REV NC, REPAIRED THE BS 513 FRAME SECTOR LOWER FLANGE BTWN BL 27 & BL 45 LT & RT IAW REO 601R-53-41-3429, REV -. ALL STEPS COMPLIED WITH 1 THRU 17. COMPLIED WITH 51-900-1003 S
- [SDR SWIA2025121577769](https://openairdocs.org/sdr/SWIA2025121577769.md): Skin · eroded · Dec 15, 2025 · N917SW · Cndair CL6002B19 · Nacelle/Pylon, Plate/Skin
  > RIGHT ENGINE L/E LIP SKIN HAD ERROSION DAMAGE ALL THE WAY AROUND. REPAIRED IAW REO 601R-71-61-2635,
- [SDR SWIA2025121577764](https://openairdocs.org/sdr/SWIA2025121577764.md): Hinge Fitting · damaged · Dec 15, 2025 · N917SW · Cndair CL6002B19 · Spoilers
  > COMPLY WITH PERMANENT REPAIR OF LT WING OTBD GROUND SPOILER, INBD HINGE FITTING ON AUX SPAR, DAMAGE AROUND BONDING STRAP ATTACHMENT. REPAIRED THE LT WING OTBD GROUND SPOILER INBD HINGE FITTING ON AUX SPAR AROUND BONDING STRAP ATTACHMENT IAW REO 601R-57-51-9
- [SDR SWIA2025091000001](https://openairdocs.org/sdr/SWIA2025091000001.md): Wire Harness · faulted · Sep 1, 2025 · N917SW · Cndair CL6002B19 · Landing Gear System Wiring
  > D:GEAR DISAGREE NOSE WHEEL. RAN QRH AND AFTER GEAR EXTENSION PULL, NOSE GEAR CAME DOWN AND GREEN.C: MEL 32-30-1CAT A DUE ONE FLT DAY, SMOD APROVAL FOR RTS, ODI EVENT DECLARED EMERGENCY, CAT II DOWNGRADED, GEAR DISAGREE NOSE WHEEL. RAN QRH AND AFTER GEAR EXT
- [SDR SWIA2025090200001](https://openairdocs.org/sdr/SWIA2025090200001.md): Warning Message · illuminated · Sep 1, 2025 · N917SW · Cndair CL6002B19 · Landing Gear Retraction/Extension System
  > GEAR DISAGREE NOSE WHEEL. RAN QRH AND AFTER GEAR EXTENSION PULL, NOSE GEAR CAME DOWN AND GREEN.C: MEL 32-30-1CAT A DUE ONE FLT DAY. SMOD APROVAL FOR RTS. ODI EVENT DECLARED EMERGENCY, CAT II DOWNGRADED. GEAR DISAGREE NOSE WHEEL. RAN QRH AND AFTER GEAR EXT
- [SDR SWIA2025010601209](https://openairdocs.org/sdr/SWIA2025010601209.md): None · none · Dec 9, 2024 · N917SW · Cndair CL6002B19 · Standard Practices/Structures
  > REMOVED LAVATORY DRAIN MAST DOUBLER ASSY (REFERENCE IPC 38-32-00 ITEM 50A) TO F.O.M. WITH REFERENCE TO SRM 51-42-06. (FILED CLOSED) INSTALLED LAVATORY DRAIN MAST DOUBLER ASSY WITH REFERENCE TO SRM 51-42-06. COMPLIED WITH TASK CARD 51-900-1003-SKY. COMP
- [SDR SWIA20250103209](https://openairdocs.org/sdr/SWIA20250103209.md): None · none · Dec 9, 2024 · N917SW · Cndair CL6002B19 · Standard Practices/Structures
  > REMOVED LAVATORY DRAIN MAST DOUBLER ASSY (REFERENCE IPC 38-32-00 ITEM 50A) TO F.O.M. WITH REFERENCE TO SRM 51-42-06. (FILED OPEN) INSTALLED LAVATORY DRAIN MAST DOUBLER ASSY WITH REFERENCE TO SRM 51-42-06. COMPLIED WITH TASK CARD 51-900-1003-SKY. COMPLI
- [SDR SWIA2025010600038](https://openairdocs.org/sdr/SWIA2025010600038.md): Frame · corroded · Dec 3, 2024 · N917SW · Cndair CL6002B19 · Fuselage Main, Frame
  > SEVERAL SMALL SPOTS OF CORROSION ON FRAME FLANGE ON THE FWD SIDE OF FS 605.00 SPANNING BETWEEN STGR 25L AND STGR 25R (FILED CLOSED) COMPLIED WITH REO 601R-53-61-8266 REV "--" DATED: 2024-12-14 SPLICE REPAIR TO FS605.00 LOWER FRAME SECTOR AT STR25R & STR
- [SDR SWIA2025010600037](https://openairdocs.org/sdr/SWIA2025010600037.md): Frame · corroded · Dec 3, 2024 · N917SW · Cndair CL6002B19 · Fuselage Main, Frame
  > CORROSION ON FRAME FLANGE ON THE FWD SIDE OF FS 589.00 BETWEEN STGR 20L AND STGR 21L (FILED CLOSED) PERFORMED REPAIR OF FRAME AND FUSELAGE SKIN ON BTW FS589.00 - FS605.00 AND BTW STR20L - STR27 WITH REFERENCE TO REO 601R-53-61-8267 REV "--" DATED 2024-12
- [SDR SWIA202501061203](https://openairdocs.org/sdr/SWIA202501061203.md): Frame · corroded · Dec 3, 2024 · N917SW · Cndair CL6002B19 · Fuselage Main, Frame
  > CORROSION ON FRAME FLANGE ON THE FWD SIDE OF FS 559.00 +112 BETWEEN STGR 26L AND STGR 26R (FILE CLOSED) COMPLIED WITH REO 601R-53-51-698 DATED: 2024-12-07 REV-- REMOVED RIVETS AS NEEDED AND BLENDED SURFACE CORROSION ON FWD SIDE OF FRAME FLANGE AT FS559.00
- [SDR SWIA20250103203](https://openairdocs.org/sdr/SWIA20250103203.md): Frame · corroded · Dec 3, 2024 · N917SW · Cndair CL6002B19 · Fuselage Main, Frame
  > CORROSION ON FRAME FLANGE ON THE FWD SIDE OF FS 559.00 +112 BETWEEN STGR 26L AND STGR 26R (FILE OPEN) COMPLIED WITH REO 601R-53-51-698 DATED: 2024-12-07 REV-- REMOVED RIVETS AS NEEDED AND BLENDED SURFACE CORROSION ON FWD SIDE OF FRAME FLANGE AT FS559.00 +
- [SDR SWIA20250103009](https://openairdocs.org/sdr/SWIA20250103009.md): Frame · corroded · Dec 3, 2024 · N917SW · Cndair CL6002B19 · Fuselage Main, Frame
  > SEVERAL SMALL SPOTS OF CORROSION ON FRAME FLANGE ON THE FWD SIDE OF FS 605.00 SPANNING BETWEEN STGR 25L AND STGR 25R (FILED OPEN) COMPLIED WITH REO 601R-53-61-8266 REV "--" DATED: 2024-12-14 SPLICE REPAIR TO FS605.00 LOWER FRAME SECTOR AT STR25R & STR 26
- [SDR SWIA2025010600013](https://openairdocs.org/sdr/SWIA2025010600013.md): Pressure Deck · damaged · Dec 2, 2024 · N917SW · Cndair CL6002B19 · Fuselage Main, Structure
  > TOOLING DAMAGE TO PRESSURE FLOOR SILL ASSY ANGLE LOCATED JUST FORWARD OF FS473.15 BETWEEN LBL 36.00 - 45.00 ON OUTER EDGE OF FASTENER HOLE. (FILED CLOSED) REPAIRED TOOLING DAMAGE TO PRESSURE FLOOR SILL ASSY ANGLE LOCATED JUST FORWARD OF FS473.15 BETWEEN
- [SDR SWIA20250106012](https://openairdocs.org/sdr/SWIA20250106012.md): Pressure Deck · corroded · Dec 2, 2024 · N917SW · Cndair CL6002B19 · Fuselage Main, Structure
  > CORROSION DAMAGE ON RH PRESSURE FLOOR SILL ASSY BETWEEN AT FS499.00 BETWEEN RBL36.0 AND RBL45.0 AND AT WL 73.0 BEYOND LIMITS OF REO 601R-53-41-666. (FILED CLOSED) REPAIRED CORROSION DAMAGE ON RH PRESSURE FLOOR SILL ASSY AT FS499.00 BETWEEN RBL36.0 AND RB
- [SDR SWIA20250106202](https://openairdocs.org/sdr/SWIA20250106202.md): Pressure Deck · corroded · Dec 2, 2024 · N917SW · Cndair CL6002B19 · Fuselage Main, Structure
  > CORROSION DAMAGE ON LH PRESSURE FLOOR SILL ASSY AT FS 461.50 BETWEEN LBL36.0 AND LBL45.0 AND AT WL 73.0 BEYOND LIMITS OF REO 601R-53-41-666. (FILED CLOSED) BLENDED CORROSION DAMAGE ON LH PRESSURE FLOOR SILL ASSY AT FS 461.50 BETWEEN LBL36.0 AND LBL45.0 A
- [SDR SWIA20250103202](https://openairdocs.org/sdr/SWIA20250103202.md): Floor Support · damaged · Dec 2, 2024 · N917SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > TOOLING DAMAGE TO PRESSURE FLOOR SILL ASSY ANGLE LOCATED JUST FORWARD OF FS473.15 BETWEEN LBL 36.00 - 45.00 ON OUTER EDGE OF FASTENER HOLE. (FILED OPEN) REPAIRED TOOLING DAMAGE TO PRESSURE FLOOR SILL ASSY ANGLE LOCATED JUST FORWARD OF FS473.15 BETWEEN LB
- [SDR SWIA202412021318](https://openairdocs.org/sdr/SWIA202412021318.md): Floor Support · corroded · Dec 2, 2024 · N917SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > CORROSION DAMAGE ON RH PRESSURE FLOOR SILL ASSY BETWEEN AT FS499.00 BETWEEN RBL36.0 AND RBL45.0 AND AT WL 73.0 BEYOND LIMITS OF REO 601R-53-41-666. (FILED OPEN) THIS IS CURRENTLY A WORK IN PROGRESS
- [SDR SWIA20241202001](https://openairdocs.org/sdr/SWIA20241202001.md): Floor Support · corroded · Dec 2, 2024 · N917SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > CORROSION DAMAGE ON LH PRESSURE FLOOR SILL ASSY AT FS 461.50 BETWEEN LBL36.0 AND LBL45.0 AND AT WL 73.0 BEYOND LIMITS OF REO 601R-53-41-666. (FILED OPEN) THIS IS CURRENTLY A WORK IN PROGRESS
- [SDR SWIA202501061128](https://openairdocs.org/sdr/SWIA202501061128.md): Intercostal · not reported · Nov 28, 2024 · N917SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > REMOVED INTERCOSTAL RUNNING BETWEEN LBL 36.00 AND LBL 47.00 AT FS 471.00 TO FOM. FOR ITEM ID REFERENCE SRM 53-41-45 FIGURE 1 (SHEET 4) FIGURE J, ITEM 5 ON PAGE 5. (FILED CLOSED) INSTALLED INTERCOSTAL RUNNING BETWEEN LBL 36.00 AND LBL 47.00 AT FS 471.00
- [SDR SWIA20250103128](https://openairdocs.org/sdr/SWIA20250103128.md): None · none · Nov 28, 2024 · N917SW · Cndair CL6002B19 · Standard Practices/Structures
  > REMOVED INTERCOSTAL RUNNING BETWEEN LBL 36.00 AND LBL 47.00 AT FS 471.00 TO FOM. FOR ITEM ID REFERENCE SRM 53-41-45 FIGURE 1 (SHEET 4) FIGURE J, ITEM 5 ON PAGE 5. (FILED OPEN) INSTALLED INTERCOSTAL RUNNING BETWEEN LBL 36.00 AND LBL 47.00 AT FS 471.00 (
- [SDR SWIA2025010600011](https://openairdocs.org/sdr/SWIA2025010600011.md): Pressure Deck · corroded · Nov 19, 2024 · N917SW · Cndair CL6002B19 · Fuselage Internal Mounting Structure
  > CORROSION DAMAGE ON LH PRESSURE FLOOR SILL ASSY BETWEEN FS409+128 AND FS559 BETWEEN LBL36.0 AND LBL45.0 AND AT WL 73.0. (FILED CLOSED) BLENDED CORROSION ON THE LH PRESSURE FLOOR SILL ASSY BETWEEN FS409+128 AND FS559 BETWEEN LBL36.0 AND LBL45.0 AND AT WL
- [SDR SWIA2025010600010](https://openairdocs.org/sdr/SWIA2025010600010.md): Pressure Deck · corroded · Nov 19, 2024 · N917SW · Cndair CL6002B19 · Fuselage Main, Structure
  > CORROSION DAMAGE ON RH PRESSURE FLOOR SILL ASSY BETWEEN FS409+128 AND FS559 BETWEEN RBL36.0 AND RBL45.0 AND AT WL 73.0. (FILED CLOSED) BLENDED CORROSION ON THE RH PRESSURE FLOOR SILL ASSY BETWEEN FS409+128 AND FS559 BETWEEN RBL36.0 AND RBL45.0 AND AT WL
- [SDR SWIA20250106119](https://openairdocs.org/sdr/SWIA20250106119.md): Track · damaged · Nov 19, 2024 · N917SW · Cndair CL6002B19 · Cargo/Baggage Doors
  > CARGO DOOR SURROUND, FORWARD TRACK, LOWER FORWARD CHANNEL AT FS574.00 FOUND DAMAGED WHILE REPLACEING CHANEL ON AFT SIDE OF CARGO DOOR FORWARD TRACK LOWER AFT CHANNEL (REFERENCE SRM 53-61-23 ITEM 50A). (FILED CLOSED) REMOVED AND REPLACED CARGO DOOR SURROUN
- [SDR SWI20250103008](https://openairdocs.org/sdr/SWI20250103008.md): Floor Support · corroded · Nov 19, 2024 · N917SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > CORROSION DAMAGE ON LH PRESSURE FLOOR SILL ASSY BETWEEN FS409+128 AND FS559 BETWEEN LBL36.0 AND LBL45.0 AND AT WL 73.0. (FILED OPEN) BLENDED CORROSION ON THE LH PRESSURE FLOOR SILL ASSY BETWEEN FS409+128 AND FS559 BETWEEN LBL36.0 AND LBL45.0 AND AT WL 73
- [SDR SWIA20250103119](https://openairdocs.org/sdr/SWIA20250103119.md): Floor Support · corroded · Nov 19, 2024 · N917SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > CORROSION DAMAGE ON RH PRESSURE FLOOR SILL ASSY BETWEEN FS409+128 AND FS559 BETWEEN RBL36.0 AND RBL45.0 AND AT WL 73.0. (FILED OPEN) BLENDED CORROSION ON THE RH PRESSURE FLOOR SILL ASSY BETWEEN FS409+128 AND FS559 BETWEEN RBL36.0 AND RBL45.0 AND AT WL 73
- [SDR SWI2024F01282](https://openairdocs.org/sdr/SWI2024F01282.md): Channel · damaged · Nov 19, 2024 · N917SW · Cndair CL6002B19 · Cargo/Baggage Doors
  > CARGO DOOR SURROUND, FORWARD TRACK, LOWER FORWARD CHANNEL AT FS574.00 FOUND DAMAGED WHILE REPLACEING CHANEL ON AFT SIDE OF CARGO DOOR FORWARD TRACK LOWER AFT CHANNEL (REFERENCE SRM 53-61-23 ITEM 50A). (FILED OPEN) THIS IS CURRENTLY A WORK IN PROGRESS
- [SDR SWIA2025010600036](https://openairdocs.org/sdr/SWIA2025010600036.md): Mount · cracked · Nov 15, 2024 · N917SW · Cndair CL6002B19 · Fuselage Main, Structure
  > CARGO DOOR AFT BALANCE SPRING MOUNT BRACKET, CRACK EMANATING FROM MOUNT HOLE TO EDGE OF BRACKET. (FILED CLOSED) REMOVED AND REPLACED CARGO DOOR AFT BALANCE SPRING MOUNT BRACKET WITH REFERENCE TO SRM 51-42-22 AND WITH REFERENCE TO REO 601R-53-61-8262 REV
- [SDR SWIA2025010601115](https://openairdocs.org/sdr/SWIA2025010601115.md): Mount · cracked · Nov 15, 2024 · N917SW · Cndair CL6002B19 · Fuselage Main, Structure
  > CARGO DOOR FWD BALANCE SPRING MOUNT BRACKET, CRACKED AROUND MOUNT HOLE. (FILED CLOSED) REMOVED AND REPLACED CARGO DOOR FWD BALANCE SPRING MOUNT BRACKET WITH REFERENCE TO SRM 51-42-06 AND SRM 53-61-15. COMPLIED WITH TASK CARD 51-900-1003-SKY. COMPLIED W

Next page: https://openairdocs.org/aircraft/N917SW/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 = 'N917SW' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N917SW/reports

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