# Service difficulty reports: N905SW, cancelled Jan 17, 2023

A list on [N905SW, cancelled Jan 17, 2023](https://openairdocs.org/deregistered/N905SW-2023-01-17.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 · 144 reports

- [SDR SWIA202163362](https://openairdocs.org/sdr/SWIA202163362.md): None · worn · Dec 30, 2021 · N905SW · Cndair CL6002B19 · Horizontal Stabilizer, Plate/Skin
  > LH AND RH HORZ STAB OUTER PIVOT PINS WEAR OUT OF LIMITS (FILED - CLOSED) REMOVED AND REPLACED LH AND RH HORZ STAB OUTER PIVOT PINS PER CRJ 200 AMM 55-10-27. SEE CP 24085669 FOR INSTALLATION, RII, OPS CHECK, AND TORQUE WRENCH INFO.
- [SDR SWIA2020072451424](https://openairdocs.org/sdr/SWIA2020072451424.md): Window · cracked · Jul 24, 2020 · N905SW · Cndair CL6002B19 · Flight Compartment Windows
  > LEFT SIDE WINDOW INNER PLY CRACKED, REQUIRES REPLACEMENT, FLIGHT 5243. REMOVED AND REPLACED THE LT SIDE WINDOW IAW TASK CARD.
- [SDR SWIA202051368](https://openairdocs.org/sdr/SWIA202051368.md): Window · cracked · Jul 20, 2020 · N905SW · Cndair CL6002B19 · Flight Compartment Windows
  > LEFT SIDE WINDOW INNER PLY CRACKED. FLIGHT 5243. REMOVED AND REPLACED LEFT SIDE WINDOW IAW TASK CARD CP 21268893-1 FOR PRESSURIZATION AND LEAK CHECK.
- [SDR SWIA2019102246548](https://openairdocs.org/sdr/SWIA2019102246548.md): Check Valve · failed · Oct 21, 2019 · N905SW · Cndair CL6002B19 · Cabin Cooling System
  > AFTER TAKE OFF, VISIBLE SMOKE IN THE CABIN AND FLIGHT DECK. ABOUT 1 MINUTE AFTER TAKE OFF SMOKE TOLIET CAUTION MESSAGE. FLT 5336 CLOSEDTROUBLESHOT VISIBLE SMOKE IN CABIN. FOUND RAM AIR INLET, BUTTERFLY VALVES AND DUCTING FROM RAM AIR INLET TO HEAT EXCHANGER T
- [SDR SWIA2019050845842](https://openairdocs.org/sdr/SWIA2019050845842.md): Intercostal · corroded · May 5, 2019 · N905SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > CORROSION ON RT LATCH PIN INTERCOSTAL @ STR 27 BETWEEN FS 349 - FS 364. (C-CHECK) RO: 05/07/2019 REMOVED & INSTALLED NEW SERVICEABLE LATCH PIN INTERCOSTAL STR 27R BETWEEN FS349.00-FS364.00 IAW SRM. LEAK CHECK GOOD.
- [SDR SWIA2019050845837](https://openairdocs.org/sdr/SWIA2019050845837.md): Intercostal · corroded · May 5, 2019 · N905SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > CORROSION ON LT LATCH PIN INTERCOSTAL @ STR 27, BETWEEN FS 349 - FS 364. (C-CHECK) RO: 05/07/2019 REMOVED AND INSTALLED NEW SERVICEABLE LATCH PIN INTERCOSTAL STR 27L BETWEEN FS349.00-FS364.00 IAW SRM. LEAK CHECK GOOD.
- [SDR SWIA2019050845841](https://openairdocs.org/sdr/SWIA2019050845841.md): Door Frame · corroded · Apr 6, 2019 · N905SW · Cndair CL6002B19 · Emergency Exits
  > LT EMERGENCY EXIT DOOR, UPPER AFT CORNER AT AREA COMMON TO STOP FITTING HAS CORROSION ON THE INSIDE OF THE DOOR FRAME AT NUTPLATE LOCATION. (C-CHECK) RO: 05/07/2019 INSTALLED NEW LT OVER WING EMERGENCY DOOR P/N 601R30000-957 S/N SB/RJ/1335 IAW SRM. LK & OP CK
- [SDR SWIA2019050845847](https://openairdocs.org/sdr/SWIA2019050845847.md): Door Sill · corroded · Mar 29, 2019 · N905SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > LT CARGO DOOR, FLOOR SILL HAS CORROSION AROUND NUTPLATES AND AROUND DOOR STOPS FROM FS 559.00+118 - FS 621.00, LBL 46. (C-CHECK) RO: 05/07/2019 REPLACED LT CARGO FLOOR SILL FROM FS559+118 TO FS621 IAW SRM AND REO.
- [SDR SWIA2019050845838](https://openairdocs.org/sdr/SWIA2019050845838.md): Floorbeam · corroded · Mar 28, 2019 · N905SW · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > CORROSION ON FLOORBEAM INBOARD FLANGE AT NUTPLATE, LOCATED 2.0" AFT OF FS 409.00+16, RBL9. (C-CHECK) RO: 05/07/2019 PERFORMED SPLICE REPAIR OF FLOORBEAM IAW SRM.
- [SDR SWIA2019050845846](https://openairdocs.org/sdr/SWIA2019050845846.md): Intercostal · corroded · Mar 26, 2019 · N905SW · Cndair CL6002B19 · Passenger/Crew Doors
  > PAX DOOR INTERCOSTAL P/N 601R31902-322 @ DD4 IS CORRODED. (C-CHECK) RO: 05/07/2019 REMOVED AND REPLACED PAX DOOR INTERCOSTAL P/N 601R31902-322 IAW SRM. LEAK CHECK GOOD.
- [SDR SWIA2019050845835](https://openairdocs.org/sdr/SWIA2019050845835.md): Intercostal · corroded · Mar 26, 2019 · N905SW · Cndair CL6002B19 · Passenger/Crew Doors
  > PAX DOOR INTERCOSTAL P/N 601R31902-413 @ DD6 IS CORRODED. (C-CHECK) RO: 05/07/2019 REMOVED AND REPLACED INTERCOSTAL PN 601R31902-413 IAW SRM. PRESSURE CHECK GOOD.
- [SDR SWIA2019050845843](https://openairdocs.org/sdr/SWIA2019050845843.md): Gusset · gouged · Mar 21, 2019 · N905SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > GOUGE ON GUSSET FOR FRAME FS319, APPROX STR-10R. (C-CHECK) RO: 05/07/2019 REPLACED DAMAGED GUSSET WITH NEW P/N: 601R38303-75, AT FRAME FS 319.00 AT APPROX STR-10R IAW SRM.
- [SDR SWIA2019050845834](https://openairdocs.org/sdr/SWIA2019050845834.md): Strap · corroded · Mar 21, 2019 · N905SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > FLOOR STRAP CORRODED FS559 LBL27 €“ LBL 43. (C-CHECK) RO: 05/07/2019 REMOVED AND REPLACED LT FLOOR STRAP AT FS559 LBL27-LBL43 IAW SRM. LEAK CHECK GOOD.
- [SDR SWIA2019050845845](https://openairdocs.org/sdr/SWIA2019050845845.md): Frame · corroded · Mar 20, 2019 · N905SW · Cndair CL6002B19 · Fuselage Main, Frame
  > FRAME CORRODED AT FS 349 BETWEEN STR 25 LEFT AND STR 25 RIGHT. (C-CHECK) RO: 05/07/2019 REMOVED CORRODED FRAME SECTION AND INSTALLED NEW SERVICEABLE LOWER FRAME SECTOR AT FS349.00 BETWEEN STR 23L AND STR 23R IAW SRM. PRESSURE CK GOOD.
- [SDR SWIA2019050845830](https://openairdocs.org/sdr/SWIA2019050845830.md): Frame · corroded · Mar 20, 2019 · N905SW · Cndair CL6002B19 · Fuselage Main, Frame
  > FRAME CORRODED AT FS 364 FORWARD SIDE BETWEEN STR 25 LEFT AND STR 25 RIGHT. (C-CHECK) RO: 05/07/2019 REMOVED CORRODED FRAME SECTION & INSTALLED NEW SERVICEABLE LOWER FRAME SECTOR P/N# 601R32007-11 AT FS364.00 BETWEEN STR 23L AND STR 23R IAW SRM. PRESSURE CK GO
- [SDR SWIA2019050845844](https://openairdocs.org/sdr/SWIA2019050845844.md): Door Sill · corroded · Mar 19, 2019 · N905SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > RT FLOOR SILL RBL43 CORRODED FS559 €“ 559+16. (C-CHECK) RO: 05/07/2019 REMOVED CORROSION AT RT FLOOR SILL RBL43 FS559 - FS 559.00+16 IAW REO.
- [SDR SWIA2019050845840](https://openairdocs.org/sdr/SWIA2019050845840.md): Door Sill · corroded · Mar 18, 2019 · N905SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > RT AFT CARGO FLOOR SILL HAS MULTIPLE CORROSION AROUND FASTENER HOLES BETWEEN FS559.00+112 TO FS621.00. (C-CHECK) RO: 05/07/2019 REMOVED AND REPLACED RT CARGO FLOOR SILL FROM FS559.00+12 TO FS621.00 IAW REO.
- [SDR SWIA2019050845839](https://openairdocs.org/sdr/SWIA2019050845839.md): Skin · chafed · Mar 17, 2019 · N905SW · Cndair CL6002B19 · Trailing Edge Flaps
  > RIGHT INBD FLAP VANE SKIN LEADING EDGE CHAFED IN THREE SPOTS. (C-CHECK) RO: 05/07/2019 REMOVED AND REPLACED CHAFED RT INBD FLAP VANE SKIN L/E WITH NEW SKIN IAW SRM AND REO.
- [SDR SWIA2019050845831](https://openairdocs.org/sdr/SWIA2019050845831.md): Vane · chafed · Mar 16, 2019 · N905SW · Cndair CL6002B19 · Trailing Edge Flaps
  > INBOARD FLAP VANE LT WING (OUT BOARD SIDE) HAS CHAFE. (C-CHECK) RO: 05/07/2019 INSTALLED NEW LT INBOARD FLAP ASSEMBLY, P/N 601R14002-1 IAW SRM.
- [SDR SWIA2019050845833](https://openairdocs.org/sdr/SWIA2019050845833.md): Door Sill · corroded · Mar 15, 2019 · N905SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > LT FLOOR SILL PANEL FS409+128 THRU FS559 BETWEEN APPROX BL36 AND BL45 CORRODED. (C-CHECK) RO: 05/07/2019 REPAIRED AREAS OF CORROSION ON THE LT FLOOR SILL PANEL BETWEEN FS409+128 THRU FS559.00 AT LBL 36 AND LBL 45 IAW REO.
- [SDR SWIA2019050845829](https://openairdocs.org/sdr/SWIA2019050845829.md): Plate · corroded · Mar 12, 2019 · N905SW · Cndair CL6002B19 · Service Doors
  > SERVICE DOOR PROTECTOR PLATE HAS CORROSION ON BACK SIDE. (C-CHECK) RO: 05/07/2019 LOCATED AND INSTALLED NEW SERVICE DOOR PROTECTOR PLATE P/N: 601R38957-31 IAW SRM.
- [SDR SWIA2019050845836](https://openairdocs.org/sdr/SWIA2019050845836.md): Hinge · worn · Mar 11, 2019 · N905SW · Cndair CL6002B19 · Fuselage, Door Hinge
  > LAV SERVICE DOOR HINGE WORN. (C-CHECK) RO: 05/07/2019 REMOVED AND REPLACED WORN LAV SERVICE DOOR HINGE WITH NEW HINGE AND HARDWARE IAW SRM.
- [SDR SWIA2019050845832](https://openairdocs.org/sdr/SWIA2019050845832.md): Panel · dented · Mar 11, 2019 · N905SW · Cndair CL6002B19 · Wing, Plate/Skin
  > SEVERAL DENTS RIGHT WING OUTBOARD LEADING EDGE PANEL. (C-CHECK) RO: 05/07/2019 REMOVED AND REPLACED THE OUTBD SKIN OF THE RT WING OUTBD LE ASSY IAW SRM.
- [SDR SWIA2019030545584](https://openairdocs.org/sdr/SWIA2019030545584.md): Warning System · false activation · Mar 1, 2019 · N905SW · Cndair CL6002B19 · Smoke Detection
  > ENROUTE SMOKE TOILET CAUTION MSG. (FLT 1357) CLOSED INSPECTED AIRCRAFT FOR SIGNS OF ELECTRICAL ARCING, OR ODOR. NO ISSUES FOUND. RAN AIRCRAFT ENGINES AND AC PACKS. NO SMOKE FOUND IN THE CABIN. PERFORMED OPERATIONAL TEST OF LAV SMOKE DET IAW AMM. SYSTEM OP
- [SDR SWIA2018090745032](https://openairdocs.org/sdr/SWIA2018090745032.md): Warning System · activated · Sep 7, 2018 · N905SW · Cndair CL6002B19 · Landing Gear Position and Warning
  > GEAR DISAGREE ON TAKE OFF. RETURN TO FIELD. NORMAL OPS FOR REMAINDER OF FLIGHT. (FLT 5251) FO: 09/07/2018 CLOSED DEFERRED LANDING GEAR RETRACTION SYSTEM IAW MEL.
- [SDR SWIA2018090545016](https://openairdocs.org/sdr/SWIA2018090545016.md): Pseu · failed · Sep 5, 2018 · N905SW · Cndair CL6002B19 · Landing Gear Position and Warning
  > GEAR DISAGREE WARNING MESSAGE AFTER DEPARTURE. UPON LANDING GEAR EXTENDED NORMALLY. EMERGENCY DECLARED. (FLT 5151) REMOVED AND REPLACED PSEU IAW AMM. PERFORMED PSEU OPS CHECKS AND OPS CHECK GOOD. PERFORMED NLG SWINGS AND OPS CHECK GOOD. CHECKED GAPS OF NLG PRO
- [SDR SWIA2017031743118](https://openairdocs.org/sdr/SWIA2017031743118.md): Floor Support · corroded · Feb 27, 2017 · N905SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > RIGHT FLOOR SUPPORT CORRODED AT BS 319, RBL 43. INSTALLED A NEW FLOOR SUPPORT FROM BS 310 TO 319 IAW SRM.
- [SDR SWIA201743117](https://openairdocs.org/sdr/SWIA201743117.md): Floor Support · corroded · Feb 25, 2017 · N905SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > FLOOR SUPPORT AT LBL 9 HAS CORROSION AROUND THE NUT PLATE HOLES BETWEEN BS 589 AND 621 OTBD SIDE. REMOVED AND REPLACED THE FLOOR SUPPORT IAW SRM AND REO.
- [SDR SWIA201743116](https://openairdocs.org/sdr/SWIA201743116.md): Vane · chafed · Feb 23, 2017 · N905SW · Cndair CL6002B19 · Trailing Edge Flaps
  > LEFT IBD FLAP VANE LEADING EDGE CHAFED APPROXIMATELY 6 INCHES FROM FROM THE IBD EDGE. REMOVED AND REPLACED THE VANE LEADING EDG IAW SRM.
- [SDR SWIA201743115](https://openairdocs.org/sdr/SWIA201743115.md): Vane · chafed · Feb 23, 2017 · N905SW · Cndair CL6002B19 · Trailing Edge Flaps
  > LEFT INBOARD FLAP VANE CHAFED APPROXIMATELY 43.5 INCHES FROM FROM THE OTBD EDGE. REMOVED AND REPLACED THE THE VANE LEADING EDGE IAW SRM.
- [SDR SWIA201641775](https://openairdocs.org/sdr/SWIA201641775.md): Bracket · bent · Jan 19, 2016 · N905SW · Cndair CL6002B19 · Main Landing Gear
  > FUNCTIONAL FLIGHT RETURNED TO DEPARTURE DUE TO A GEAR DISAGREE. R & R NLG OLEO CENTERING, EXTEND SENSOR BRACKET IAW AMM AND C/W SENSOR ADJUSTMENT IAW AMM, ALL OPS GOOD.
- [SDR SWIA201641766](https://openairdocs.org/sdr/SWIA201641766.md): Landing Gear · no test · Jan 18, 2016 · N905SW · Cndair CL6002B19 · Landing Gear Retraction/Extension System
  > FAILED FUNCTIONAL FLIGHT FOR GEAR RETRACTION/EXTENSION.
- [SDR SWIA201641765](https://openairdocs.org/sdr/SWIA201641765.md): Landing Gear · malfunctioned · Jan 15, 2016 · N905SW · Cndair CL6002B19 · Landing Gear Retraction/Extension System
  > LANDING GEAR DISAGREE. NLG NEVER RETRACTED AND MANUAL EXTENSION WAS REQUIRED.
- [SDR SWIA201641757](https://openairdocs.org/sdr/SWIA201641757.md): Warning Light · illuminated · Jan 12, 2016 · N905SW · Cndair CL6002B19 · Landing Gear Position and Warning
  > GEAR DISAGREE ON GEAR RETRACTION, NLG. RETURNED TO THE FIELD. OPEN
- [SDR SWIA201641746](https://openairdocs.org/sdr/SWIA201641746.md): Priority Valve · failed · Jan 11, 2016 · N905SW · Cndair CL6002B19 · Landing Gear Retraction/Extension System
  > AIRCRAFT RETURNED TO THE FIELD DUE TO A GEAR DISAGREE. R & R NLG PRIORITY VALVE, SWUNG GEAR MULTIPLE TIMES, OPS CHECK GOOD.
- [SDR SWIA201540950](https://openairdocs.org/sdr/SWIA201540950.md): Skin · dented · Mar 13, 2015 · N905SW · Cndair CL6002B19 · Ailerons
  > AILERON UPPER SKIN DENTED AT A/STA 304, STS EA, C-CHECK RO 3/27/15, COMPLIED WITH REPAIR OF LT AILERON UPPER SKIN DENT AT WS 304 IAW STS EA. COMPLIED WITH ST 51-900-1003.
- [SDR SWIA201540942](https://openairdocs.org/sdr/SWIA201540942.md): Skin · dented · Mar 12, 2015 · N905SW · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > COMPLY WITH FUSELAGE DENT REPAIR BETWEEN FS652.56- FS672.20 BETWEEN S17L AND S18L IDENTIFIED AS DENT NR 2 ON CAMP MX TRANS 11921491, C-CHECK, RO 3/27/15, COMPLIED WITH PERMANENT REPAIR OF FUSELAGE DENT BETWEEN FS652.56-FS672.20 BETWEEN S17L AND S18L IAW STS EA
- [SDR SWIA201540954](https://openairdocs.org/sdr/SWIA201540954.md): Structure · chafed · Mar 9, 2015 · N905SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > LEFT APRON SKIN HAS CHAFED DAMAGE CAUSED BY UPPER WING PLANK SEAL. C-CHECK, RO 3/27/15, BLENDED OUT, CHECKED AND FOUND LT APRON SKIN OUT OF LIMIT REF REO AND REPLACED WITH NEW APRON SKIN REF STS EA.
- [SDR SWIA201540952](https://openairdocs.org/sdr/SWIA201540952.md): Trunnion · cracked · Mar 4, 2015 · N905SW · Cndair CL6002B19 · Wing, Landing Gear Attach Fittings
  > FOUND 3 EA CRACKED HOLES ON L/WING WHILE PERFORMING SB, C-CHECK RO 3/27/15. REPAIRED 3EA CRACKED HOLES ON LT TRUNNION AT L/WING REF REO.
- [SDR SWIA201540953](https://openairdocs.org/sdr/SWIA201540953.md): Vane · chafed · Mar 3, 2015 · N905SW · Cndair CL6002B19 · Trailing Edge Flaps
  > LT INBD FLAP VANE L/E HAS CHAFE OTBD OF OTBD ACTUATOR, C-CHECK, RO 3/27/15. REMOVED CHAFE FROM LT FLAP VANE OTBD L/E CAP, ORIGINAL THICKNESS 0.050", REMAINING THICKNESS 0.029" MATERIAL REMOVED 0.021" MAX MATERIAL ALLOWED TO BE REMOVED IS 0.020", BEYOND LIMIT
- [SDR SWIA201540948](https://openairdocs.org/sdr/SWIA201540948.md): Structure · corroded · Mar 3, 2015 · N905SW · Cndair CL6002B19 · Passenger/Crew Doors
  > LT FS 349 CUP FOR PAX DOOR AFT HANDRAIL, CORRODED BEYOND LIMITS. C-CHECK, RO 3/27/15. R & R 1 EA. BRACKET AND 1 EA CLEAT TO PAX DOOR LOWER STRUCTURE AT LT FS.349, REF CRJ 200 SRM.
- [SDR SWIA201540951](https://openairdocs.org/sdr/SWIA201540951.md): Skin · damaged · Mar 2, 2015 · N905SW · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > AFT CARGO DOOR CUTOUT OUTER SKIN HAS SLIGHT DAMAGE AT AFT EDGE OF SKIN APPROXIMATELY FS 621.00. C-CHECK RO 3/27/15, REPAIRED AFT CARGO DOOR CUTOUT OUTER SKIN AFT EDGE OF SKIN APPROXIMATELY FS 621.00, REF STS EA 10. FUNCTIONAL & LEAK CHECKS GOOD, ORIGINAL M
- [SDR SWIA201540947](https://openairdocs.org/sdr/SWIA201540947.md): Access Panel · corroded · Mar 2, 2015 · N905SW · Cndair CL6002B19 · Passenger/Crew Doors
  > PAX DOOR FWD ACCESS PANEL AREA HAS CORROSION BETWEEN NUTPLATE AND INNER SKIN. AT 832AL LOCATION, C-CHECK, RO 3/27/15, BLENDED CORRODED AREAS REF SRM ORIGINAL MATERIAL THICKNESS WAS 0.040" REF SRM, REMOVED 0.006" MATERIAL, REMAINING MATERIAL THICKNESS IS 0.034
- [SDR SWIA201540946](https://openairdocs.org/sdr/SWIA201540946.md): Skin · corroded · Mar 2, 2015 · N905SW · Cndair CL6002B19 · Passenger/Crew Doors
  > PAX DOOR INNER SKIN HAS CORROSION IN BETWEEN NUTPLATE AND INNER SKIN AT ACCESS PANEL LOCATION 832BR. BLENDED CORROSION AND REPLACED NUTPLATES ON PAX DOOR INNER SKIN AT ACCESS PANEL 823BR IAW; SRM. ORIGINAL MATERIAL THICKNESS WAS 0.040" REF SRM, REMOVED 0.00
- [SDR SWIA201540945](https://openairdocs.org/sdr/SWIA201540945.md): Floor Panel · cracked · Mar 2, 2015 · N905SW · Cndair CL6002B19 · Fuselage Floor Panel
  > FORWARD EQUIPMENT COMPARTMENT FLOOR HAS A CRACK AT RT SIDE FS193.00, MARKED, C-CHECK, RO 3/27/15. REPAIRED FORWARD EQUIPMENT COMPARTMENT FLOOR AT RT SIDE FS 193.00 IAW REO.
- [SDR SWIA201540944](https://openairdocs.org/sdr/SWIA201540944.md): Floor Panel · cracked · Mar 2, 2015 · N905SW · Cndair CL6002B19 · Fuselage Floor Panel
  > FORWARD EQUIPMENT COMPARTMENT FLOOR HAS A CRACK AT LT SIDE FS193.00, MARKED, C-CHECK, RO 3/27/15, REPAIRED CRACK AT THE LT SIDE OF THE FORWARD EQUIPMENT, TRU BAY, FLOOR AT FS 193.00 REF REO.
- [SDR SWIA201540949](https://openairdocs.org/sdr/SWIA201540949.md): Skin · gouged · Mar 1, 2015 · N905SW · Cndair CL6002B19 · Passenger/Crew Doors
  > PAX DOOR HAS GOUGES COMMON TO SKIN AND HANDLE HOUSING, MARKED, C-CHECK, RO 3/27/15. COMPLIED WITH PERMANT REPAIR I, STEPS 1-6, REF STS EA.
- [SDR SWIA201540943](https://openairdocs.org/sdr/SWIA201540943.md): Skin · dented · Mar 1, 2015 · N905SW · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > DENT APPROXIMATELY 3 INCH AFT OF GROUND AIR SUPPLY DOOR SKIN CUTOUT. REPAIRED DENT APPROXIMATELY 3" AFT OF GROUND AIR SUPPLY DOOR SKIN CUTOUT REF STS EA.
- [SDR SWIA2014061638198](https://openairdocs.org/sdr/SWIA2014061638198.md): Bulb · inoperative · Jun 15, 2014 · N905SW · Cndair CL6002B19 · Emergency Lighting
  > MULTIPLE INOPERATIVE BULBS IN THE LT AND RT EMERGENCY EXIT DOORS LIGHTED EXIT SIGNS. R & R THE BULBS IAW AMM.
- [SDR SWIA2014051637614](https://openairdocs.org/sdr/SWIA2014051637614.md): Lamp · inoperative · May 16, 2014 · N905SW · Cndair CL6002B19 · Emergency Lighting
  > FRONT LT OTBD EMERGENCY LIGHT INOPERATIVE, REPLACED THE LAMP.

Next page: https://openairdocs.org/deregistered/N905SW-2023-01-17/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 = 'N905SW' AND deregistration_id = 'N905SW-2023-01-17'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N905SW-2023-01-17/reports

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