# Service difficulty reports: N918SW

A list on [N918SW](https://openairdocs.org/aircraft/N918SW.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 5 · 210 reports

- [SDR SWIA2026061876244](https://openairdocs.org/sdr/SWIA2026061876244.md): Landing Gear · warning message · Jun 18, 2026 · N918SW · Cndair CL6002B19 · Landing Gear Retraction/Extension System
  > GEAR DISAGREE WARNING ON TAKEOFF NOSE SHOWED UP AND MAIN GEAR SHOWED DN. ALL GEAR CAME DOWN WITH QRHC: MEL 32-30-1CAT A DUE DATE IS 06/19/2026 SMOD APPROVAL REQUIRED BEFORE RELEASE DUE TO GEAR DISAGREE WARNING "ODI"REF EAML 1916880 (FLIGHT 6055). DEFERRED LA
- [SDR J6BA202501200019](https://openairdocs.org/sdr/J6BA202501200019.md): Flap System · malfunctioned · Jan 19, 2025 · N918SW · Cndair CL6002B19 · Trailing Edge Flap Control System
  > D: FLAP FAIL EVENTC: AD 2009-06-12/10, CREW RESETFULL FLAP AD EVALUATION DUE WITHIN 10 CYCLES DUE 40040 TACFLAP FAIL AT ZERO DEGREES.AT 3000 FT SPEED 195KTS. (FLIGHT 3915) RESET AND OPERATED FLAPS 5 FULL CYCLES AND COMPLETED AD 2009-06-12/10 COMPLIANCE F
- [SDR J6BA202406100111](https://openairdocs.org/sdr/J6BA202406100111.md): Flap System · failed · Jan 11, 2024 · N918SW · Cndair CL6002B19 · Trailing Edge Flap Control System
  > ON APPROACH FLAPS 8, FLAPS FAIL CAUTION MESSAGE DISPLAYED (FLIGHT 3360 FILED CLOSED)RESET AND OPERATED FLAPS 5 FULL CYCLES AND COMPLETED AD 2009-06-12/10 COMPLIANCE FORM. OK TO CONTINUE IN SERVICE FOR 10 FLIGHT CYCLES. COMPLIED WITH IN ACCORDANCE WITH FIM FMRP
- [SDR SWIA2024053000111](https://openairdocs.org/sdr/SWIA2024053000111.md): Warning Message · illuminated · Jan 11, 2024 · N918SW · Cndair CL6002B19 · Trailing Flap Position Indicating System
  > ON APPROACH FLAPS 8, FLAPS FAIL CAUTION MESSAGE DISPLAYED (FLIGHT 3360 FILED CLOSED)RESET AND OPERATED FLAPS 5 FULL CYCLES AND COMPLETED AD 2009-06-12/10 COMPLIANCE FORM. OK TO CONTINUE IN SERVICE FOR 10 FLIGHT CYCLES. COMPLIED WITH IN ACCORDANCE WITH FIM FMRP
- [SDR SWIA202301250003](https://openairdocs.org/sdr/SWIA202301250003.md): Control Lever · failed · Jan 23, 2023 · N918SW · Cndair CL6002B19 · Trailing Edge Flap Control System
  > FLAPS FAIL CAUTION ON APPROACH, WHEN ATTEMPTING TO SET 30 DEGREES FLAPS, FLAPS FAILED AT 20 DEGREES. (FILED CLOSED)THIS DISCREPANCY WAS TRANSFERRED TO CAMP ITEM 26117469 WITH THE FOLLOWING CORRECTIVE ACTION: "REMOVED AND REPLACED THE FLAP CONTROL LEVER IAW CRJ
- [SDR SWIA2022122067017](https://openairdocs.org/sdr/SWIA2022122067017.md): Floor Support · out of limits · Dec 9, 2022 · N918SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > FOUND LT FLOOR SSUPPORT NR 10 BLEND-OUT, OUT OF LIMITS. PERFORMED A REPAIR TO PRESSURE FLOOR SUPPORT BETWEEN BS 484 - 499, LHS AND PERFORMED REO 601R-53-41-3101, REV -. PRESSURE CHECK GOOD.
- [SDR SWIA202267016](https://openairdocs.org/sdr/SWIA202267016.md): Cap · corroded · Nov 22, 2022 · N918SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > FLOOR SILL AT PAX DOOR FWD HANDRAIL CAP HAS INTERGRANULAR CORROSION AND REQUIRES REPLACEMENT. REMOVED AND INSTALLED NEW PAX DOOR FWD HANDRAIL CAP IAW SRM 51-42-06, AND DWG 601R31527, REV AM.
- [SDR SWIA202267015](https://openairdocs.org/sdr/SWIA202267015.md): Bracket · cracked · Nov 12, 2022 · N918SW · Cndair CL6002B19 · Passenger/Crew Doors
  > PAX DOOR SILL AFT HANDRAIL CAP BRACKET BETWEEN FS 333.00 TO FS349.00 HAS CORROSION REMOVED AND REPLACED HANDRAIL CUP BRACKET AND CLEAT IAW SRM 51-42-06, 51-45-00, AND DWG 601R31527, REV AM.
- [SDR SWIA2022122067014](https://openairdocs.org/sdr/SWIA2022122067014.md): Bracket · corroded · Nov 12, 2022 · N918SW · Cndair CL6002B19 · Passenger/Crew Doors
  > PAX DOOR SILL FWD HANDRAIL CAP BRACKET BETWEEN FS 310.00 TO FS319.70 HAS CORROSION. REPLACED PAX DOOR SILL FWD HANDRAIL CAP BRACKET IAW SRM 51-42-06, DWG 601R-31527, REV AM.
- [SDR SWIA2022122067013](https://openairdocs.org/sdr/SWIA2022122067013.md): Floor Support · corroded · Nov 11, 2022 · N918SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > R/H FLOOR SILL ANGLE FROM FS310.00 TO FS319.70 HAS AREAS OF CORROSION. REMOVED AND REPLACED THE FLOOR SILL ANGLES WITH NEW IAW SRM 51-42-06, 51-42-13, DWG 601R31148, REV Y.
- [SDR SWIA202267012](https://openairdocs.org/sdr/SWIA202267012.md): Stiffener · cracked · Nov 11, 2022 · N918SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > FORWARD KEEL BEAM PRESSURE BOX, UPPER STIFFENER WAS DENTED WITH POSSIBLE CRACK. EVALUATED DENT ON FORWARD KEEL BEAM PRESSURE BOX, UPPER STIFFENER OUT OF LIMITS. REMOVED AND INSTALLED A NEW FORWARD KEEL BEAM PRESSURE BOX, STIFFENER IAW SRM 51-42-06, SRM 51-23-0
- [SDR SWIA202267011](https://openairdocs.org/sdr/SWIA202267011.md): Frame · corroded · Nov 11, 2022 · N918SW · Cndair CL6002B19 · Fuselage Main, Frame
  > FRAME BS 319 HAD MULTIPLE SPOTS OF CORROSION FROM STR 25L TO STR 26. REMOVED AND REPLACED THE FRAME IAW SRM 51-42-06, SRM 51-42-21, AND DWG 601R32003, REV P. PRESSURE CHECKS GOOD.
- [SDR SWIA202267010](https://openairdocs.org/sdr/SWIA202267010.md): Frame · corroded · Nov 11, 2022 · N918SW · Cndair CL6002B19 · Fuselage Main, Frame
  > FRAME BS 310 HAD MULTIPLE SPOTS OF CORROSION FROM S24L TO S24R. REMOVED AND REPLACED THE FRAME IAW SRM 51-42-06, SRM 51-42-21, AND DWG 601R32002 REV AD.
- [SDR SWIA2022122067009](https://openairdocs.org/sdr/SWIA2022122067009.md): Frame · corroded · Nov 10, 2022 · N918SW · Cndair CL6002B19 · Fuselage Main, Frame
  > CORROSION NOTED ON FRAME BS 605 BETWEEN S25R-23L. FOUND OUT OF LIMITS. REMOVED AND INSTALLED A NEW LOWER FRAME IAW DWG 601R36026, REV AF, DWG 601R35005 REV Y, SRM 51-42-06, AND SRM 51-42-21. NO LEAKS NOTED.
- [SDR SWIA2022122067008](https://openairdocs.org/sdr/SWIA2022122067008.md): Angle · cracked · Nov 10, 2022 · N918SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > TWO ANGLES FOR INTERCOSTAL AT BS 484 BETWEEN FLOORBEAM LBL 27 AND LBL 36 WERE CRACKED. REMOVED AND INSALLED THE TWO ANGLES IAW DWG 601R31171, REV B, AND SRM 51-42-21. NO LEAKS NOTED
- [SDR SWIA202267007](https://openairdocs.org/sdr/SWIA202267007.md): Angle · cracked · Nov 10, 2022 · N918SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > TWO ANGLES FOR INTERCOSTAL AT BS 484 BETWEEN RBL 27 AND RBL 36 ARE CRACKED. REMOVED AND INSTALLED NEW ANGLES IAW SRM 51-42-06, SRM 51-42-21 AND DWG 601R31171, REV B. NO LEAKS NOTED.
- [SDR SWIA2022122067006](https://openairdocs.org/sdr/SWIA2022122067006.md): Support Fitting · cracked · Nov 10, 2022 · N918SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > SUPPORT FITTING FOR LBL27 FLOOR BEAM AT FS460 HAS A POSSIBLE CRACK. NDT VERIFIED CRACK ON SUPPORT FITTING. REMOVED AND INSTALLED A NEW SUPPORT FITTING WITH REPLACEMENT FASTENERS IAW SRM 51-42-21, AND DWG 600-31143, REV E. NO LEAKS NOTED.
- [SDR SWIA2022122067005](https://openairdocs.org/sdr/SWIA2022122067005.md): Floor Support · corroded · Nov 10, 2022 · N918SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > RIGHT PRESSURE FLOOR SILL FROM BS 409 - 559 HADS AREAS OF CORROSION. REMOVED CORROSION IAW SRM 51-21-06. FOUND PARTS TO BE OUT OF LIMITS. COMPLIED WITH ALL STEPS OF REO 601R-53-41-666 REV-C, DISPOSITION 1.2, AND REO 601R-53-41-3102 REV--, NO LEAKS NOTED.
- [SDR SWIA2022122067004](https://openairdocs.org/sdr/SWIA2022122067004.md): Floor Support · corroded · Nov 10, 2022 · N918SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > LEFT PRESSURE FLOOR SILL FROM BS409+128 - 559 HAD AREAS OF CORROSION. BLENDED OUT CORROSION AND FOUND AREAS TO BE OUT OF LIMITS. COMPLIED WITH ALL STEPS OF REO'S 601R-53-41-666 REV-C AND REO 601R-53-41-3102 REV-. NO LEAKS NOTED. PERFORMED REPAIR ON BLEND-
- [SDR SWIA2022122067003](https://openairdocs.org/sdr/SWIA2022122067003.md): Cleat · corroded · Nov 9, 2022 · N918SW · Cndair CL6002B19 · Passenger/Crew Doors
  > PAX DOOR CLEAT COMMON TO FS320.163 FORMER AND MID LWR CHANNEL CORRODED. REMOVED AND REPLACED THE PAX DOOR CLEAT IAW DWG 601R31702, REV N, AND SRM 51-42-06.
- [SDR SWIA2022122067002](https://openairdocs.org/sdr/SWIA2022122067002.md): Frame · cracked · Nov 7, 2022 · N918SW · Cndair CL6002B19 · Fuselage Main, Frame
  > CRACKED FRAME FS 235.00 BETWEEN STRINGERS 11-12R. REMOVED AND INSTALLED A NEW ANGLE IAW SRM 51-42-06, DWG 601R34032, REV V, AND REO 601R-53-11-3810, REV-. PRESSURE CHECKED GOOD.
- [SDR SWIA2022122067001](https://openairdocs.org/sdr/SWIA2022122067001.md): Frame Angle · cracked · Nov 7, 2022 · N918SW · Cndair CL6002B19 · Fuselage Main, Frame
  > CRACK ON FRAME BS 235 BETWEEN STRINGERS 11-12L. REMOVED AND INSTALLED A NEW ANGLE IAW SRM 51-42-06, AND DWG 601R34032, REV -V. PRESSURE CHECKS GOOD.
- [SDR SWIA2022122067000](https://openairdocs.org/sdr/SWIA2022122067000.md): Skin · damaged · Nov 5, 2022 · N918SW · Cndair CL6002B19 · Elevator, Plate/Skin
  > REPAIR DAMAGED UPPER SKIN ON R/H ELEVATOR INBOARD AFT TRAILING EDGE. PERMEANNTLY REPAIRED RT ELAVATOR INBD AFT EDGE IAW SRM 55-20-00.
- [SDR SWIA202266999](https://openairdocs.org/sdr/SWIA202266999.md): Bracket · cracked · Nov 5, 2022 · N918SW · Cndair CL6002B19 · Fuselage Main, Attach Fittings
  > LEFT MAIN LANDING GEAR WHEEL WELL, BRAKE HYDRAULIC FUSE AFT BRACKET IS CRACKED. REPLACED THE BRACKET IAW SRM 51-42-06 AND DWG 601R75278 REV-G. NO LEAKS NOTED
- [SDR SWIA202266998](https://openairdocs.org/sdr/SWIA202266998.md): Bracket · cracked · Nov 5, 2022 · N918SW · Cndair CL6002B19 · Fuselage Main, Attach Fittings
  > LEFT MAIN LANDING GEAR WHEEL WELL, BRAKE HYDRAULIC FUSE FORWARD BRACKET IS CRACKED. REMOVED THE LT MAIN LANDING GEAR WHEEL WELL, HYDRAULIC FUSE FWD BRACKET IAW SRM 51-42-06, INSTALLED A NEW BRACKET IAW SRM 51-42-06 AND DWG 601R75278 REV-G. LEAK CHECK GOOD
- [SDR SWIA2022122066997](https://openairdocs.org/sdr/SWIA2022122066997.md): Drain Valve · damaged · Nov 5, 2022 · N918SW · Cndair CL6002B19 · Wing Miscellaneous Structure
  > UPON REMOVAL OF LEFT HAND COLLECTOR TANK WATER DRAIN VALVE NOTICED TWO WASHERS UNDER WATER DRAIN VALVE FASTENERS ON WING PLANK SIDE. UPON REMOVAL OF THE WASHERS IDENTIFIED THAT THE LEFT HAND COLLECTOR TANK WATER DRAIN VALVE FASTENER HOLES TWO EACH ARE ELONGAT
- [SDR SWIA2022122066996](https://openairdocs.org/sdr/SWIA2022122066996.md): Hinge Fitting · corroded · Nov 4, 2022 · N918SW · Cndair CL6002B19 · Elevator Structure
  > UPON REMOVAL FOR BEARING REPLACEMENT, FOUND LT ELEVATOR L/E HINGE FITTING ASSY HAVE PITTING CORROSION IN BEARING BORES OF BOTH HINGE HALVES. REMOVED AND REPLACED THE LT ELEVATOR NR 1 HINGE FITTING ASSY WITH NEW HINGE FITTING ASSY IAW DWG 601R24025, REV G, SR
- [SDR SWIA202266995](https://openairdocs.org/sdr/SWIA202266995.md): Hinge Fitting · worn · Nov 4, 2022 · N918SW · Cndair CL6002B19 · Elevator Structure
  > UPON REMOVAL, FOUND RT ELEVATOR L/E HINGE FITTING ASSY TO BE EXCESSIVELY WORN AT BEARING LOCATION. REPLACE HINGE FITTING ASSY IAW DWG 601R24025, REV G, SRM 51-42-06, AND 51-42-21
- [SDR SWIA2022122066994](https://openairdocs.org/sdr/SWIA2022122066994.md): Skin · dented · Nov 3, 2022 · N918SW · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > SMALL DENT ON TOP OF AFT FUSELAGE BETWEEN BS 559+112 AND 574, BETWEEN STR 0 AND STR 1R. COMPLIED WITH PERMANENT REPAIR IAW REO 601R-53-61-7912, REV -., PRESSURE CHECK GOOD.
- [SDR SWIA2022122066993](https://openairdocs.org/sdr/SWIA2022122066993.md): Bracket · cracked · Nov 1, 2022 · N918SW · Cndair CL6002B19 · Landing Gear Position and Warning
  > RIGHT MLG WHEEL WELL BRAKE PRESSURE TRANSDUCER BRACKET CRACKED & BROKEN IN TWO PLACES. REMOVED AND INSTALLED A NEW BRACKET IAW SRM 51-42-06 AND DWG 601R31146 REV J, PRESSURE CHECKS GOOD.
- [SDR SWIA2022122066992](https://openairdocs.org/sdr/SWIA2022122066992.md): Bracket · cracked · Nov 1, 2022 · N918SW · Cndair CL6002B19 · Landing Gear Position and Warning
  > LEFT MLG WHEEL WELL BRAKE PRESSURE TRANSDUCER BRACKET CRACKED IN TWO PLACES. REMOVED AND INSTALLED A NEW BRACKET IAW SRM 51-42-06, AND DWG 601R31146, REV J. PRESSURE CHECKS GOOD.
- [SDR SWIA2022122066991](https://openairdocs.org/sdr/SWIA2022122066991.md): Intercostal · dented · Oct 29, 2022 · N918SW · Cndair CL6002B19 · Passenger/Crew Doors
  > PAX DOOR DD7 FWD INTERCOSTAL DENTED. REMOVED AND INSTALLED A NEW DD7 FWD INTERCOSTAL IN PASSENGER DOOR IAW DWG 601R31702, REV: N, SRM 51-42-06. PRESSURE CHECK GOOD
- [SDR SWIA202266990](https://openairdocs.org/sdr/SWIA202266990.md): Intercostal · dented · Oct 29, 2022 · N918SW · Cndair CL6002B19 · Passenger/Crew Doors
  > PAX DOOR DD1 AFT INTERCOSTAL DENTED. PAX DOOR DD1 AFT INTERCOSTAL OUT OF LIMITS. REMOVED AND INSTALLED NEW DD1 INTERCOSTAL IAW DWG 601R31702, REV: N, AND SRM 51-42-06. NO LEAKS NOTED.
- [SDR SWIA2022122066989](https://openairdocs.org/sdr/SWIA2022122066989.md): Former · corroded · Oct 29, 2022 · N918SW · Cndair CL6002B19 · Passenger/Crew Doors
  > PAX DOOR AFT FORMER CORRODED. REMOVED AND INSTALLED NEW AFT FORMER IAW SRM 51-42-06, SRM 51-42-21, AND DWG 601R31702, REV N. PRESSURE CHECK GOOD.
- [SDR SWIA2022122066988](https://openairdocs.org/sdr/SWIA2022122066988.md): Intercostal · corroded · Oct 29, 2022 · N918SW · Cndair CL6002B19 · Passenger/Crew Doors
  > PAX DOOR DD3 AFT INTERCOSTAL CORRODED. REMOVED AND INSTALLED NEW DD3 INTERCOSTAL IAW DWG 601R31702, REV: N, AND SRM 51-42-06. PRESSURE CHECKS GOOD.
- [SDR SWIA202266987](https://openairdocs.org/sdr/SWIA202266987.md): Intercostal · corroded · Oct 29, 2022 · N918SW · Cndair CL6002B19 · Passenger/Crew Doors
  > PAX DOOR DD4 AFT INTERCOSTAL CORRODED. PAX DOOR DD4 AFT INTERCOSTAL OUT OF LIMITS. REMOVED AND INSTALLED NEW DD4 AFT INTERCOSTAL IAW DWG 601R31702, REV N AND SRM 51-42-06. NO LEAKS NOTED.
- [SDR SWIA202266986](https://openairdocs.org/sdr/SWIA202266986.md): Intercostal · corroded · Oct 29, 2022 · N918SW · Cndair CL6002B19 · Passenger/Crew Doors
  > PAX DOOR DD3 MID INTERCOSTAL CORRODED. REMOVED AND INSTALLED PAX DOOR DD3 MID INTERCOSTAL IAW SRM 51-42-06, SRM 51-42-21 AND DWG 601R31702, REV N. PRESSURE CHECKS GOOD
- [SDR SWIA202266985](https://openairdocs.org/sdr/SWIA202266985.md): Intercostal · corroded · Oct 29, 2022 · N918SW · Cndair CL6002B19 · Passenger/Crew Doors
  > PAX DOOR DD4 MID INTERCOSTAL CORRODED. REMOVED AND INSTALLED PAX DOOR DD4 MID INTERCOSTAL IAW SRM 51-42-06, SRM 51-42-21 AND DWG 601R31702, REV N. CHECKED GOOD.
- [SDR SWIA202266984](https://openairdocs.org/sdr/SWIA202266984.md): Cleat · corroded · Oct 29, 2022 · N918SW · Cndair CL6002B19 · Passenger/Crew Doors
  > PAX DOOR DD6 MID CLEAT COMMON TO FS329.76 FORMER CORRODED. REMOVED AND REPLACED PAX DOOR DD6 MID CLEAT COMMON TO BS 329.76 FORMER IAW DWG 601R31702, REV. N AND SRM 51-42-06.
- [SDR SWIA202266983](https://openairdocs.org/sdr/SWIA202266983.md): Intercostal · corroded · Oct 29, 2022 · N918SW · Cndair CL6002B19 · Passenger/Crew Doors
  > PAX DOOR DD6 MID INTERCOSTAL CORRODED. PAX DOOR DD6 INTERCOSTAL OUT OF LIMITS. REMOVED AND INSTALLED NEW DD6 INTERCOSTAL IAW DWG 601R31702 REV: N, SRM 51-42-06, SRM 51-42-21. NO LEAKS NOTED.
- [SDR SWIA202266982](https://openairdocs.org/sdr/SWIA202266982.md): Cleat · corroded · Oct 29, 2022 · N918SW · Cndair CL6002B19 · Passenger/Crew Doors
  > PAX DOOR CLEAT COMMON TO FS320.163 FRAME AND MID LWR CHANNEL CORRODED. REMOVED AND REPLACED PAX DOOR CLEAT COMMON TO FS320.163 FRAME AND MID LWR CHANNEL IAW DWG 601R31702REV. N AND SRM 51-42-06.
- [SDR SWIA202266981](https://openairdocs.org/sdr/SWIA202266981.md): Cleat · corroded · Oct 29, 2022 · N918SW · Cndair CL6002B19 · Passenger/Crew Doors
  > PAX DOOR CLEAT ON DD4 FWD COMMON TO FS313.56 FRAME CORRODED. REMOVED AND REPLACED PAX DOOR CLEAT ON DD4 FWD COMMON TO FS313.56 FRAME REF. DRWG 601R31702 REV. N AND SRM 51-42-06.
- [SDR SWIA202266980](https://openairdocs.org/sdr/SWIA202266980.md): Former · corroded · Oct 29, 2022 · N918SW · Cndair CL6002B19 · Passenger/Crew Doors
  > PAX DOOR FWD FORMER CORRODED. PAX DOOR FWD FORMER FOUND TO BE CORRODED OUT OF LIMITS. REMOVED AND INSTALLED NEW PAX DOOR FWD FORMER REF. DRWG 601R31702 REV. N, SRM 51-42-06 AND SRM 51-42-21. NO LEAKS NOTED.
- [SDR SWIA202266979](https://openairdocs.org/sdr/SWIA202266979.md): Hinge Arm · chafed · Oct 28, 2022 · N918SW · Cndair CL6002B19 · Trailing Edge Flaps
  > LEFT INBOARD FLAP, OUTBOARD HINGE ARM, INBOARD GUIDE PLATE IS CHAFED. REPLACED INBOARD GUIDE PLATE AT LT INBOARD FLAP, OUTBOARD HINGE ARM IAW SRM 51-42-06 AND DWG 601R14116 REV H.
- [SDR SWIA202266978](https://openairdocs.org/sdr/SWIA202266978.md): Hinge Arm · chafed · Oct 28, 2022 · N918SW · Cndair CL6002B19 · Trailing Edge Flaps
  > LEFT INBOARD FLAP, INBOARD HINGE ARM, INBOARD GUIDE PLATE IS CHAFED. INSTALLED A NEW INBOARD HINGE ARM,INBD GUIDE PLATE IAW SRM 51-42-06 AND DWG 601R14116, REV H.
- [SDR SWIA202266977](https://openairdocs.org/sdr/SWIA202266977.md): Hinge · damaged · Oct 27, 2022 · N918SW · Cndair CL6002B19 · Fuselage, Door Hinge
  > PAX DOOR PIANO HINGE (FUSELAGE SIDE) HAS NUMEROUS ELONGATED HINGE PIN HOLES (C-CHECK) REMOVED AND INSTALLED NEW PAX DOOR HINGE HALF IAW SRM 53-21-23 STEPS 4. R-V AND REO 601R-53-21-656 REV A. NO LEAKS NOTED.
- [SDR SWIA202266976](https://openairdocs.org/sdr/SWIA202266976.md): Skin · chafed · Oct 27, 2022 · N918SW · Cndair CL6002B19 · Trailing Edge Flaps
  > LEFT INBD FLAP VANE HAS CHAFING ON LEADING EDGE AT MID LOCATION AT APPROXIMATELY WS 104.099. (C-CHECK) REMOVED AND INSTALLED NEW LT INBD FLAP VANE CAP, LEADING EDGE MID LOCATION PER DWG 601R14303, REV J AND SRM 51-42-13.
- [SDR SWIA2022122066975](https://openairdocs.org/sdr/SWIA2022122066975.md): Skin · chafed · Oct 27, 2022 · N918SW · Cndair CL6002B19 · Trailing Edge Flaps
  > LEFT INBD FLAP VANE HAS CHAFING ON LEADING EDGE AT INBD LOCATION AT APPROXIMATELY WS 56.30. (C-CHECK) UPON BLENDING LT INBD FLAP VANE IB LOCATION, MATERIAL LOSS AT 100%, THROUGH PART AND REQUIRES REPLACEMENT IAW SRM 51-12-00. REMOVED BAD VANE CAP IAW SR
- [SDR SWIA2022122067018](https://openairdocs.org/sdr/SWIA2022122067018.md): Skin · cracked · Oct 26, 2022 · N918SW · Cndair CL6002B19 · Passenger/Crew Doors
  > REMOVE AND REPLACE PAX DOOR INNER SKIN DUE TO CRACKED. REMOVED AND REPLACED PAX DOOR INNER SKIN IAW SRM 51-42-06, SRM 51-42-10, SRM 51-42-21, AND SRM 51-42-22.
- [SDR SWIA2022122066974](https://openairdocs.org/sdr/SWIA2022122066974.md): Skin · chafed · Oct 26, 2022 · N918SW · Cndair CL6002B19 · Ailerons
  > LEFT AILERON LOWER FWD EDGE HAS 3 SPOTS THAT ARE CHAFED. (C-CHECK) BLENDED CHAFING ON LT AILERON LOWER FWD LEADING EDGE SKINS IAW SRM 51-12-00, TWO AREAS FOUND IN LIMITS IAW SRM 57-60-00 AND LOCATION AILS 370 TO 375 FOUND OUT OF LIMITS, REPLACED WITH NEW

Next page: https://openairdocs.org/aircraft/N918SW/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 = 'N918SW' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N918SW/reports

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