# Service difficulty reports: N632SK

A list on [N632SK](https://openairdocs.org/aircraft/N632SK.md).

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.

- [SDR SWIA2026092977788](https://openairdocs.org/sdr/SWIA2026092977788.md): Floorbeam · cracked · Sep 29, 2026 · N632SK · Cndair CL6002C10 · Fuselage Main, Floor Beam
  > FS22000 RBL 12 COCKPIT FLOORBEAM POSSIBLE CRACK, INSIDE PANEL 132AR MARKED FILED CLOSEDREMOVED AND INSTALLED NEW ANGLE REPAIR AT FS22000 RBL12 COCKPIT FLOORBEAM REF REO 670-53-11-2387 REV-- DATE 2026-10-01 COMPLIED WITH TASKCARD 51-900-1002-SKY AND M337 SEE
- [SDR SWIA2026060776666](https://openairdocs.org/sdr/SWIA2026060776666.md): Thrust Shaft · gouged · Jun 7, 2026 · N632SK · Cndair CL6002C10 · Engine (Turbine/Turboprop)
  > LEFT ENG AFT THRUST SHAFT HAS SMALL GOUGING ON SURFACE THAT SLIDES INTO THRUST FITTING. REMOVED AND REPLACED LT ENGINE AFT THRUST SHAFT IN REFERENCE TO AMM 71-22-01. SEE CP 32395243 FOR ENGINE CHANGE TASK CARD.TORQUE WRENCH INFORMATION: S/N: 0304100422 DATE
- [SDR SWIA2025121775491](https://openairdocs.org/sdr/SWIA2025121775491.md): Floorbeam · fom · Dec 17, 2025 · N632SK · Cndair CL6002C10 · Standard Practices/Structures
  > REMOVE FLOORBEAM SECTION AT FS280 LBL12 FOR ACCESS (C-CHECK RO 03/08/2026)PERFORMED REPAIR TO CENTER COCKPIT FLOOR BEAM AT LBL12 IAW CRJ700 AMM 20-70-00, SRM 51-42-06, 51-42-21, 51-21-11, 51-25-06, 51-25-16, BOMBARDIER REO 670-53-11-896, REV --.
- [SDR SWIA2026031075488](https://openairdocs.org/sdr/SWIA2026031075488.md): Floorbeam · cracked · Dec 9, 2025 · N632SK · Cndair CL6002C10 · Fuselage Main, Floor Beam
  > FLIGHT COMPARTMENT FLOORBEAM, BS 280, RBL 12 CRACKED. REPAIRED THE FLOORBEAM IAW AMM 20-70-00, SRM 51-42-06, 51-42-13, 51-42-21, 51-21-11, 51-25-06, 51-25-16, REO 670-53-11-896, REV -,AMM 32-22-05 AND MEMO, ISE-STR-12-004, REV- NC.
- [SDR SWIA2020310275492](https://openairdocs.org/sdr/SWIA2020310275492.md): Stringer · corroded · Dec 2, 2025 · N632SK · Cndair CL6002C10 · Fuselage Main, Longeron/Stringer
  > AVIONICS BAY STR24R SUPPORT AT FS333 HAS SIGNS OF CORROSION. PERFORMED REPAIR STR24R ON AVIONICS BAY AT FS333.00 IAW CRJ700 SRM 53-21-03, 53-00-03,51-23-00, AMM 21-31-00.
- [SDR SWIA2026031075485](https://openairdocs.org/sdr/SWIA2026031075485.md): Stringer · corroded · Nov 29, 2025 · N632SK · Cndair CL6002C10 · Fuselage Main, Longeron/Stringer
  > FWD CARGO COMPARTMENT, BS 589 - 592, S25R SHOWS SIGNS OF CORROSION. PERFORMED REPAIR ON THE STRINGER, FOUND TO BE WITHIN LIMITS IAW SRM 51-42-20, 51-21-06, 53-31-03, 51-42-06, 51-42-21, 53-00-03, 51-40-11, 51-21-11, 51-25-16, 51-25-16, 51-41-02, AMM 53-82-81
- [SDR SWIA2026031075497](https://openairdocs.org/sdr/SWIA2026031075497.md): Slat Track · damaged · Nov 26, 2025 · N632SK · Cndair CL6002C10 · Leading Edge Devices
  > LH WING SLAT TRACK 5 LOWER SURFACE LAND HAS SIGNS OF PITTING AND OB ROLLER LAND HS GROOVES. PERFORMED BLENDED OUT AND EVALUATED AREAS ON LH WING SLAT TRACK 5 LOWER SURFACE LAND AND ROLLER LAND, FOUND TO BE STRUCTURALLY AND FUNCTIONALLY ACCEPTABLE IAW SRM 51-1
- [SDR SWIA2026031075495](https://openairdocs.org/sdr/SWIA2026031075495.md): Web · cracked · Nov 25, 2025 · N632SK · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > FWD EQUIPMENT BAY FLOOR WEB CRACKED ON R/H SIDE. REMOVED AND REPLACED PREVIOUS REPAIR AT FWD EQUIPMENT BAY FLOOR WEB IAW CRJ700 AMM 20-70-00, SRM 51-42-06, 51-25-16, BOMBARDIER REO 670-53-11-509, REV-E,
- [SDR SWIA2025112575494](https://openairdocs.org/sdr/SWIA2025112575494.md): Web · cracked · Nov 25, 2025 · N632SK · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > FWD EQUIPMENT BAY FLOOR WEB CRACKED ON L/H SIDE. PERFORMED REPAIR ON FWD EQUIPMENT BAY FLOOR WEB LH SIDE IAW AMM 52-45-56 20-70-00, SRM 51-42-06, 51-21-11, 51-25-06, 51-25-16, BOMBARDIER REO 670-53-11-509 REV-E DATED: 2018-02-08.
- [SDR SWIA2026031075496](https://openairdocs.org/sdr/SWIA2026031075496.md): Fitting · gouged · Nov 24, 2025 · N632SK · Cndair CL6002C10 · Fuselage Main, Attach Fittings
  > RIGHT MLG SIDE STAY FITTING IS GOUGED ON OB SURFACE. PERFORMED BLENDED OUT AND EVALUATED AREA ON RH MLG SIDESTAY FITTING OB SURFACE,CONDITION IS STRUCTURALLY ACCEPTABLE IAW MHI RJ REO 670-57-11-244 REV-- DATED: 2026-01-23, CRJ700 SRM 51-12-00, 51-24-11, 51-21
- [SDR SWIA2025112475489](https://openairdocs.org/sdr/SWIA2025112475489.md): Skin · gouged · Nov 24, 2025 · N632SK · Cndair CL6002C10 · Fuselage Main, Plate/Skin
  > FUSELAGE EXTERIOR LEFT SIDE BS 969 - 985, ABOVE STRINGER 27. SKIN GOUGED. REPAIRED DAMAGE TO FUSELAGE EXTERIOR BETWEEN BS 969 AND BS 985 STGR 27L IAW REO 670-53-00-290, REV-F AND REO 670-53-00-807, REV-A.
- [SDR SWIA2026031075490](https://openairdocs.org/sdr/SWIA2026031075490.md): Bulkhead · corroded · Nov 23, 2025 · N632SK · Cndair CL6002C10 · Fuselage Main, Bulkhead
  > MAIN CABIN BS 280 BULKHEAD, LBL12, WL79.50, HAD SIGNS OF CORROSION. REMOVED AND REPLACED SECTION LOWER WEB REPAIR ON MAIN CABIN BS 280 BULKHEAD LBL12 AND WL79.50 IAW SRM 53-00-00, AMM 20-70-00, SRM 51-42-06, 51-42-21, 51-42-13, 51-25-16, REO 670-53-11-594
- [SDR SWIA2026031075487](https://openairdocs.org/sdr/SWIA2026031075487.md): Fitting · gouged · Nov 23, 2025 · N632SK · Cndair CL6002C10 · Fuselage, Landing Gear Attach Fittings
  > LEFT MLG SIDE STAY FITTING GOUGED. PERFORMED BLENDED OUT AND EVALUATED AREA ON LT MLG SIDE STAY FITTING, CONDITION IS STRUCTURALLY ACCEPTABLE IAW REO 670-57-11-244, REV--, SRM 51-12-00, 51-24-11, 51-21-11, 51-25-06, 51-25-16.
- [SDR SWIA2026031075486](https://openairdocs.org/sdr/SWIA2026031075486.md): Bulkhead Web · corroded · Nov 23, 2025 · N632SK · Cndair CL6002C10 · Fuselage Main, Bulkhead
  > MAIN CABIN FS280 BULKHEAD WEB AT WL79.50 RBL25 "AND RBL46" HAS SIGNS OF CORROSION. REMOVED AND REPLACED SECTION LOWER WEB REPAIR ON MAIN CABIN FS280.00 AT WL79.50 RBL25 AND RBL46 IAW AMM 20-70-00, SRM 51-42-13, 53-00-00, 51-42-06, 51-41-02, 51-42-21, 51-42-2
- [SDR SWIA2026031075498](https://openairdocs.org/sdr/SWIA2026031075498.md): Cowling · gouged · Nov 18, 2025 · N632SK · Cndair CL6002C10 · Nacelle/Pylon, Main Frame
  > RT ENG LOWER COWLING FWD LATCH HOUSING GOUGED (C-CHECK RO 03/08/2026)PERFORMED BLENDED OUT AND EVALUATED AREA ON RH ENG LOWER COWLING FWD LATCH HOUSING IAW SRM 51-12-00, REO 670-54-22-136 REV--.
- [SDR SWIA2026031075493](https://openairdocs.org/sdr/SWIA2026031075493.md): Drag Angle · cracked · Nov 17, 2025 · N632SK · Cndair CL6002C10 · Vertical Stabilizer
  > VERTICAL STAB LEFT SIDE FWD DRAG ANGLE IS CRACKED AT AFT END (C-CHECK RO 03/08/2026)PERFORMED REPAIR ON VERTICAL STAB LEFT SIDE FWD DRAG ANGLE IAW BOMBARDIER REO 670-55-31-018, REV -A, DATE 2016/11/10, CRJ700 AMM 20-70-00. SRM 51-42-06, 51-42-21
- [SDR SWIA20240909](https://openairdocs.org/sdr/SWIA20240909.md): Skin · damaged · Sep 9, 2024 · N632SK · Cndair CL6002C10 · Fuselage Main, Plate/Skin
  > TRANSFER FROM EAML 1426725: REO 670-53-61-2360 - SCRATCH / DENT (32.25€?L WITH 10.125€?L THROUGH THE PAINT ONLY) ON FUSELAGE SKIN (DWG. MM670-35131, 0.080€? THK AT DISCREPANT AREA, REF) BETWEEN FS1031.00 AND FS1069.75 AND BETWEEN ST
- [SDR SWIA2024072200597](https://openairdocs.org/sdr/SWIA2024072200597.md): Terminal · out of position · Jul 19, 2024 · N632SK · Cndair CL6002C10 · Fire Protection System Wiring
  > LEFT BLEED DUCT WARNING. FOLLOWED BY LEFT BLEED DUCT CAUTION. RAN QRH PROCEDURE RTF. NO EMERGENCY DECLARED. NO OVERWEIGHT LANDING. (FLIGHT 6214 - FILED CLOSED)INTERROGATED MDC FOUND B1 CODES 349537 AND 349536. FOLLOWED B1 CODES PER FIM 36-21-01 AND FOUND MT14
- [SDR SWIA202264776](https://openairdocs.org/sdr/SWIA202264776.md): None · failed · Mar 6, 2022 · N632SK · Cndair CL6002C10 · Landing Gear Door Actuator
  > GEAR DISAGREE ON CLIMB OUT, RTF TO AUS. RAN QRH PROCEDURE, STEERING INOP APPEARED ALONG WITH THE GEAR DISAGREE. (FLIGHT 3065 - FILED CLOSED) DEFERRED LANDING GEAR RETRACTION SYSTEM IN REFERENCE TO MEL 32-30-1. INSTALLED/SAFETY WIRED LANDING GEAR PINS AND I
- [SDR SWIA202053798](https://openairdocs.org/sdr/SWIA202053798.md): Beam · corroded · Oct 18, 2020 · N632SK · Cndair CL6002C10 · Fuselage Main, Structure
  > CORROSION FOUND AT LBL 9 FS 295 LONG BEAM, MARKED. C-CHECK RO 11/1/2020. REMOVED CORROSION, REF CRJ700 SRM. ALL STEPS COMPLIED WITH OF FINAL REO. SEE CONTINUE CARD FOR DETAILS OF WORK PERFORMED. O2 SYSTEM FAILED LEAK CHECK. SEE JOB 71033061 OP 245 MXTRAN
- [SDR SWIA202053797](https://openairdocs.org/sdr/SWIA202053797.md): Plate · corroded · Oct 7, 2020 · N632SK · Cndair CL6002C10 · Fuselage Main, Structure
  > FORWARD CARGO DOOR SURROUND STRUCTURE. LOWER AFT JOINING PLATE HAS CORROSION. C-CHECK RO 11/1/2020. FWD CARGO DOOR SURROUND STRUCTURE, LOWER AFT JOINT PLATE WAS FOUND TO BE OUT OF LIMITS OF CRJ700 SRM. INSTALLED NEW FWD CARGO DOOR SURROUND STRUCTURE LOWER
- [SDR SWIA202053796](https://openairdocs.org/sdr/SWIA202053796.md): Web · corroded · Oct 7, 2020 · N632SK · Cndair CL6002C10 · Fuselage Main, Bulkhead
  > AFTER REMOVING THE LT CORROSION CAP ON FS 280.00 TO ACCESS LT WEB CORROSION, FOUND PITTING CORROSION ON FS 280.00 LT CROSSBEAM. C-CHECK RO 11/1/2020. REMOVED CORROSION ON LT CROSSBEAM AT FS 280. FOUND TO BE OUT OF LIMITS. REMOVED AND INSTALLED NEW LT CROSS
- [SDR SWIA202053795](https://openairdocs.org/sdr/SWIA202053795.md): Web · corroded · Oct 7, 2020 · N632SK · Cndair CL6002C10 · Fuselage Main, Bulkhead
  > AFTER REMOVING THE RT CORROSION CAP ON FS 280.00 TO ACCESS RT WEB CORROSION, FOUND PITTING CORROSION ON FS 280.00 RT CROSSBEAM. C-CHECK RO 11/1/2020. REMOVED CORROSION FROM RT CROSSBEAM AT FS 280 FOUND TO BE OUT OF LIMITS. REMOVED & INSTALLED NEW CROSSBEAM,
- [SDR SWIA202053805](https://openairdocs.org/sdr/SWIA202053805.md): Seat Track · corroded · Oct 5, 2020 · N632SK · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION AND PITTING, EVIDENCE OF PREVIOUS BLENDING, GOUGES AND SCRATCHES, AT RT VISIBLE SEAT RAIL SEGEMENTS FROM APPROXIMATELY FS 477.40 THRU FS 693.00, MARKED. C-CHECK RO 11/1/2020. REMOVED AND REPLACED RT SEAT RAIL AT APPROXIMATELY FS 477.10 THRU FS 693.
- [SDR SWIA202053804](https://openairdocs.org/sdr/SWIA202053804.md): Seat Track · gouged · Oct 5, 2020 · N632SK · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION AND PITTING, PREVIOUS BLENDS, GOUGES AND SCRATCHES VISIBLE SEAT RAILS SEGMENTED SECTIONS LT FROM APPROXIMATELY FS 477.40 THRU FS 693, MARKED. C-CHECK RO 11/1/2020. REMOVED AND REPLACED LT SEAT RAIL AT APPROXIMATELY FS 477.40 THRU FS 693, REF CRJ700
- [SDR SWIA202053794](https://openairdocs.org/sdr/SWIA202053794.md): Door Frame · corroded · Oct 5, 2020 · N632SK · Cndair CL6002C10 · Fuselage Main, Structure
  > FORWARD CARGO DOOR SURROUND STRUCTURE: LOWER FORWARD JOINING PLATE HAS CORROSION AROUND MULTIPLE FASTENERS. C-CHECK RO 11/1/2020. FORWARD CARGO DOOR SURROUND STRUCTURE: LOWER FORWARD JOINING PLATE WAS FOUND OUT OF LIMITS OF CRJ700 SRM REPLACED JOINING PLATE,
- [SDR SWIA202053807](https://openairdocs.org/sdr/SWIA202053807.md): Post · corroded · Oct 4, 2020 · N632SK · Cndair CL6002C10 · Fuselage Main, Structure
  > RT FS 280 BL 11.0L POST HAS EVIDENCE OF CORROSION ON INBOARD SIDE AT FLOOR LEVEL. C-CHECK RO 11/1/2020. WHILE REMOVING CORROSION ON RT FS 280.00 BL 11. POST FOUND 100% MATERIAL LOSS AT THE BOTTOM OF THE POST. OUT OF LIMITS, REF CRJ700 SRM. INSTALLED REPAI
- [SDR SWIA202053806](https://openairdocs.org/sdr/SWIA202053806.md): Post · corroded · Oct 4, 2020 · N632SK · Cndair CL6002C10 · Fuselage Main, Structure
  > LT FS 280 BL 11.0L POST HAS EVIDENCE OF CORROSION ON INBOARD SIDE AT FLOOR LEVEL. C-CHECK RO 11/1/2020. WHILE REMOVING CORROSION ON LT FS 280.00 BL 11. POST FOUND 100% MATERIAL LOSS AT THE BOTTOM OF THE POST. OUT OF LIMITS, REF CRJ700 SRM. INSTALLED REPAI
- [SDR SWIA202053803](https://openairdocs.org/sdr/SWIA202053803.md): Door Sill · corroded · Oct 4, 2020 · N632SK · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > SERVICE DOOR SILL UPPER FLOOR SUPPORT ANGLE HAS EVIDENCE OF CORROSION AT APPROXIMATELY FS 340. C-CHECK RO 11/1/2020. REPLACED SERVICE DOOR SILL UPPER FLOOR SUPPORT ANGLE, REF CRJ700 SRM REF CRJ700 SRM.
- [SDR SWIA202053802](https://openairdocs.org/sdr/SWIA202053802.md): Floor Support · corroded · Oct 4, 2020 · N632SK · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > SERVICE DOOR SILL FLOOR SUPPORT ANGLE HAS EVIDENCE OF CORROSION AT APPROXIMATELY FS 342. C-CHECK RO 11/1/2020. REPLACED SERVICE DOOR SILL FLOOR SUPPORT ANGLE, REF CRJ700 SRM.
- [SDR SWIA202053801](https://openairdocs.org/sdr/SWIA202053801.md): Door Sill · corroded · Oct 4, 2020 · N632SK · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > PAX DOOR SILL UPPER FLOOR SUPPORT ANGLE HAS EVIDENCE OF CORROSION AROUND FASTENER HOLES FOR TOP STEP HINGE AND ALONG OUTBOARD EDGE. C-CHECK RO 11/1/2020. PAX DOOR SILL UPPER FLOOR SUPPORT ANGLE WAS REPLACED FOR A NEW PART, DOOR MID CAP ANGLE, REF DWG AND CRJ
- [SDR SWIA202053800](https://openairdocs.org/sdr/SWIA202053800.md): Angle · corroded · Oct 4, 2020 · N632SK · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > PAX DOOR SILL LOWER FLOOR SUPPORT ANGLE HAS EVIDENCE OF CORROSION ALONG ENTIRE LENGTH. C-CHECK RO 11/1/2020. PAX DOOR SILL LOWER FLOOR SUPPORT ANGLE. REPLACED PASSENGER LOWER SILL ANGLE, REF DWG AND CRJ 700 SRM.
- [SDR SWIA202053793](https://openairdocs.org/sdr/SWIA202053793.md): Intercostal · corroded · Oct 4, 2020 · N632SK · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > STRINGER 20R INTERCOSTAL BETWEEN FRAMES FS 310 AND FS 319 HAS EVIDENCE OF CORROSION. C-CHECK RO 11/1/2020. BLENDED DAMAGE TO A SMOOTH CONTOUR AT STGR 20R ON INTERCOSTAL BETWEEN FS 310-FS 319, REF CRJ700 SRM. FOUND ARE TO BE WIH IN LIMITS. REQUESTED AND REC
- [SDR SWIA202053792](https://openairdocs.org/sdr/SWIA202053792.md): Bulkhead Web · corroded · Oct 4, 2020 · N632SK · Cndair CL6002C10 · Fuselage Main, Bulkhead
  > FS 280 RT WEB HAS EVIDENCE OF CORROSION AT FLOOR LEVEL AT APPROXIMATELY BL42RH. C-CHECK RO 11/1/2020. REMOVED WEB, EVAULATED AND FOUND TO BE OUT OF LIMITS. INSTALLED NEW WEB, PER REO. COMPLIED WITH SKYWEST TASK CARD.
- [SDR SWIA202053791](https://openairdocs.org/sdr/SWIA202053791.md): Floorbeam · corroded · Oct 4, 2020 · N632SK · Cndair CL6002C10 · Fuselage Main, Floor Beam
  > FS 280 FLOOR SUPPORT ANGLE FOR COCKPIT FLOOR PANEL 221ALF HAS EVIDENCE OF CORROSION. C-CHECK RO 11/1/2020. REMOVED AND REPLACED THE FS 280 COCKPIT FLOOR SUPPORT ANGLE, REF CRJ700 SRM DRAWING.
- [SDR SWIA202053790](https://openairdocs.org/sdr/SWIA202053790.md): Bulkhead Web · corroded · Oct 4, 2020 · N632SK · Cndair CL6002C10 · Fuselage Main, Bulkhead
  > LT FS 280 WEB HAS BULGE WITH EVIDENCE OF INTERNAL EXFOLIATION CORROSION AT INBOARD EDGE/FLOOR LEVEL. C-CHECK RO 11/1/2020. PERFORMED EVAL OF THE LT FS 280 WEB. FOUND TO BE OUT OF LIMITS. REMOVED AND INSTALLED FABRICATED BUTTSTRAP (WEB) LT AT FS 280, PER RE
- [SDR SWIA202053789](https://openairdocs.org/sdr/SWIA202053789.md): Stringer · dented · Oct 3, 2020 · N632SK · Cndair CL6002C10 · Fuselage Main, Longeron/Stringer
  > DENT ON LT SIDE OF STGR 27 BETWEEN FS 977.00 TO 969.00. C-CHECK RO 11/1/2020. COMPLIED WITH REO FOR BLEND ON LT SIDE OF STGR 27 BETWEEN FS 977.00 TO 969.00. DAMAGE WAS PREVIOUS BLEND, NO WEIGHT CHANGE.
- [SDR SWIA202053788](https://openairdocs.org/sdr/SWIA202053788.md): Structure · corroded · Sep 29, 2020 · N632SK · Cndair CL6002C10 · Emergency Exits
  > LT OVERWING EMERGENCY EXIT DOOR HAS CORROSION AND GOUGE AT LOWER NUTPLATE LOCATIONS, MARKED QTY: 2. C-CHECK RO 11/1/2020. REPAIRED THE LT OVERWING EMERGENCY DOOR AT THE LOWER NUTPLATE LOCATION BY CUTTING AWAY THE DAMAGE. FABRICATING AND INSTALLING A DOUBLER
- [SDR SWIA202053787](https://openairdocs.org/sdr/SWIA202053787.md): Bushing · not reported · Sep 9, 2020 · N632SK · Cndair CL6002C10 · Ailerons
  > ROUTE RT AILERON TO BACK SHOP TO REMOVE AND REPLACE SWEDGED BEARINGS AND BUSHINGS AT HINGE POINTS (INBOARD, MID, OUTBOARD) ON RT AILERON, PER AMM. C-CHECK RO 11/1/2020. REMOVED AND REPLACED WORN BUSHINGS AND BEARINGS IN RT AILERON, REF CRJ 700 AMM FOR BEARIN
- [SDR SWIA2019062546003](https://openairdocs.org/sdr/SWIA2019062546003.md): Window · cracked · Jun 25, 2019 · N632SK · Cndair CL6002C10 · Flight Compartment Windows
  > RIGHT WINDOW CRACKED IN FLIGHT. COMPLIED WITH QRH. DESCENDED TO 13000 FT TO EQUALIZE PRESSURE. CONTINUED TO DESTINATION. EMERGENCY DECLARED. LANDED WITHOUT INCIDENT. FLT 4624. REMOVED AND REPLACED RIGHT SIDE WINDOW IAW AMM.
- [SDR SWIA201438605](https://openairdocs.org/sdr/SWIA201438605.md): Light · inoperative · Jun 18, 2014 · N632SK · Cndair CL6002C10 · Emergency Lighting
  > RT NR 4 EXTERNAL EMERGENCY LIGHT INOPERATIVE. R & R RT NR 4 EXTERNAL EMERGENCY LIGHT IAW AMM.
- [SDR SWIA2014061838220](https://openairdocs.org/sdr/SWIA2014061838220.md): Bracket · damaged · Jun 7, 2014 · N632SK · Cndair CL6002C10 · Landing Gear Doors
  > AFT BRACKET TO RT NOSE GEAR DOOR SUSTAINED DAMAGE FROM BIRD STRIKE. R & R AFT NOSE DOOR BRACKET IAW AMM.
- [SDR SWIA201335713](https://openairdocs.org/sdr/SWIA201335713.md): Sign · missing · Dec 18, 2013 · N632SK · Cndair CL6002C10 · Emergency Lighting
  > CEILING FWD FACING EMERGENCY EXIT SIGN MISSING. FLT 4796 FOUND THE CEILING FWD FACING EMERGENCY LIGHT SIGN & INSTALLED.
- [SDR SWIA201333494](https://openairdocs.org/sdr/SWIA201333494.md): Roller Cam · lack of lube · May 14, 2013 · N632SK · Cndair CL6002C10 · Passenger/Crew Doors
  > MAIN CABIN DOOR COULD NOT BE OPENED. FINALLY THE DOOR RELEASE HANDLE CYCLED AND THE DOOR OPENED BUT THE RELEASE HANDLE WAS BINDING OR HANGING UP DURING ITS MOVEMENT. LUBED PAX DOOR PINS AND ROLLED CAMS, OPS CK GOOD.
- [SDR SWIA201332602](https://openairdocs.org/sdr/SWIA201332602.md): Unknown · odor · Jan 15, 2013 · N632SK · Cndair CL6002C10 · Air Distribution System
  > FLIGHT ATTENDANTS NOTICED BURNING PLASTIC SMELL IN THE AREA OF THE FIRST CLASS CLOSET, BUT NOT IN CLOSET. NO SMOKE. (FLT 4454) INSPECTED BEHIND PSU AISLE CEILING PANEL NO SIGN OF SMOKE NOTED. ALL ELECTRICAL SYSTEM LIGHTING WORKING PROPERLY, NO SIGN OF OVER
- [SDR SWIA201232458](https://openairdocs.org/sdr/SWIA201232458.md): Seat Belt · faulty · Dec 22, 2012 · N632SK · Cndair CL6002C10 · Flight Compartment Equipment
  > F/O'S LAP BELT IS EXTREMELY DIFFICULT TO UNBUCKLE. (FLT 4679) REPLACED F/O SEAT BELT.
- [SDR SWIA201232094](https://openairdocs.org/sdr/SWIA201232094.md): Light · inoperative · Oct 31, 2012 · N632SK · Cndair CL6002C10 · Emergency Lighting
  > NR 1 EMERGENCY OVERHEAD LIGHT IS BURNED OUT. (FLT 4800) RELAMPED EMERGENCY LIGHT.
- [SDR SWIA201231908](https://openairdocs.org/sdr/SWIA201231908.md): Light · inoperative · Oct 3, 2012 · N632SK · Cndair CL6002C10 · Emergency Lighting
  > NR 1 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 4662) RELAMPED EMERGENCY LIGHT.
- [SDR SWIA201231418](https://openairdocs.org/sdr/SWIA201231418.md): Latch · dirty · Jul 26, 2012 · N632SK · Cndair CL6002C10 · Flight Compartment Equipment
  > FIRST OFFICERS SEAT BELT/SHOULDER HARNESS IS VERY HARD TO UNLATCH. (FLT 4608) CLEANED FLIGHT OFFICER'S SHOULDER HARNESS LATCH ASSEMBLY.

## 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 = 'N632SK' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N632SK/reports

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