# Service difficulty reports: N982SW

A list on [N982SW](https://openairdocs.org/aircraft/N982SW.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 SWIA2026072076973](https://openairdocs.org/sdr/SWIA2026072076973.md): Step · cracked · Jul 20, 2026 · N982SW · Cndair CL6002B19 · Passenger/Crew Doors
  > PAX DOOR UPPER STEP IS CRACK IN TWO PLACES (C-CHECK RO 08/29/2026)COMPLETED REPAIR WITH REO: 601R-52-11-279 ON THE UPPER STEP OF THE PAX DOOR IAW CRJ 200 SRM 51-24-36,51-24-16,51-40-11,51-21-11,51-25-06,51-25-16.
- [SDR SWIA2026070976982](https://openairdocs.org/sdr/SWIA2026070976982.md): Angle · cracked · Jul 9, 2026 · N982SW · Cndair CL6002B19 · Wing Miscellaneous Structure
  > ANGLE @ WS 48.30 R/H HAS 2 CRACKS (C-CHECK RO 08/29/2026)REMOVED AND REPLACED NEW CAP (ANGLE) ON THE R/H WS 48.30 IAW CRJ 200 SRM 57-21-12,51-42-20,51-40-11,51-23-00.
- [SDR SWIA2026070976978](https://openairdocs.org/sdr/SWIA2026070976978.md): Angle · cracked · Jul 9, 2026 · N982SW · Cndair CL6002B19 · Wing Miscellaneous Structure
  > ANGLE @ WS 48.30 L/H HAS A CRACK (C-CHECK RO 08/29/2026)REMOVED AND REPLACED NEW CAP (ANGLE) ON L/H FROM WS 48.30 IAW CRJ200 SRM 51-42-20,51-40-11,57-21-12.
- [SDR SWIA2026070376981](https://openairdocs.org/sdr/SWIA2026070376981.md): Hinge · damaged · Jul 3, 2026 · N982SW · Cndair CL6002B19 · Fuselage, Door Hinge
  > PAX DOOR HINGE ON A/C SIDE DAMAGED (C-CHECK RO 08/29/2026)REMOVED AND REPLACED DOOR HINGE (FUSELAGE SIDE) ON PAX DOOR IAW CRJ200 SRM 51-42-06,51-42-20,51-40-11,53-21-23,51-23-00. OP'S CHECK GOOD.
- [SDR SWIA2026070376980](https://openairdocs.org/sdr/SWIA2026070376980.md): Vane · damaged · Jul 3, 2026 · N982SW · Cndair CL6002B19 · Ailerons
  > LEFT INBD FLAP VANE SKIN HAS DAMAGES ON THE LEADING EDGE. AFTER EVALUATION FOUND OUTSIDE OF LIMITS AND REPLACED LEADING EDGE SKIN WS56, AND THE LEADING EDGE SKINS WS 105 AND WS 140 FOUND WITHIN LIMITS AND TREATED WITH ALODINE PRIMER AND TOP COAT ON WORKED A
- [SDR SWIA2026070376977](https://openairdocs.org/sdr/SWIA2026070376977.md): Vane · chafed · Jul 3, 2026 · N982SW · Cndair CL6002B19 · Trailing Edge Flaps
  > RT INBD FLAP VANE LE CHAFED/WORN AT RWS 56 (C-CHECK RO 08/29/2026)REMOVED AND REPLACED NEW IB LEADING SKIN FROM R/H IB FLAP WS 56 IAW CRJ200 SRM 51-10-06,51-42-13,51-40-11,57-52-00,51-21-11,51-25-06,51-25-16.
- [SDR SWIA2026070376975](https://openairdocs.org/sdr/SWIA2026070376975.md): Pressure Blkhd · gouged · Jul 3, 2026 · N982SW · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > DURING DETAIL INSPECTION OF AFT PRESS BULKHEAD FOUND GOUGE MARKS ON AREA AS WORKED - RIVET HEADS/HORIZONTAL ANGLE/BETWEEN RIVETS (C-CHECK RO 08/29/2026)COMPLETED REPAIR IAW CRJ 200 REO: 601R-53-61-8590.
- [SDR SWIA2026070376974](https://openairdocs.org/sdr/SWIA2026070376974.md): Vane · chafed · Jul 3, 2026 · N982SW · Cndair CL6002B19 · Trailing Edge Flaps
  > RIGHT INBD FLAP VANE LE CHAFED/WORN AT R/H WS 140 (C-CHECK RO 08/29/2026)REMOVED AND REPLACED LEADING EDGE SKIN FROM R/H IB FLAP VANE AT WS 140 IAW REO: 601R-57-52-004 AND IAW CRJ200 SRM 51-42-13,51-23-00,51-10-06,51-40-11,57-52-00, 51-21-11,51-25-06,51-25-16
- [SDR SWIA2026070176984](https://openairdocs.org/sdr/SWIA2026070176984.md): Skin · dented · Jul 1, 2026 · N982SW · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > MULTIPLE DENTS & GOUGES AT BS 589 - 605, BTWN STRINGERS 21R AND 27R. COMPLETED REPAIR WITH THE REO 601R-53-61-8591.
- [SDR SWIA2026061276983](https://openairdocs.org/sdr/SWIA2026061276983.md): Skin · dented · Jun 12, 2026 · N982SW · Cndair CL6002B19 · Passenger/Crew Doors
  > THERE IS A DENT ON THE PAX DOOR AT APPROX BS 333, STRINGER 7. FOUND WITHIN LIMITS, ELIMINATE ALL EVIDENCE OF DAMAGE USING AIRCRAFT STANDARD PRACTICES AND/OR PROCEDURES. COMPLETED REPAIR WITH REO 601R-52-10-917.
- [SDR SWIA2026061276979](https://openairdocs.org/sdr/SWIA2026061276979.md): Skin · dented · Jun 12, 2026 · N982SW · Cndair CL6002B19 · Passenger/Crew Doors
  > ADM# N982SW-9157THERE IS A DENT ON THE PAX DOOR AT APPROXIMATELY 15€Œ FWD OF TRAILING EDGE OF THE MCD AND 15€? DOWN FROM THE TOP EDGE OF THE MCD. COMPLETED REPAIR WITH REO: 601R-52-10-917
- [SDR SWIA2026061276976](https://openairdocs.org/sdr/SWIA2026061276976.md): Skin · dented · Jun 12, 2026 · N982SW · Cndair CL6002B19 · Passenger/Crew Doors
  > ADM# N982SW-9158THERE IS A DENT ON THE PAX DOOR AT APPROXIMATELY 12€? AFT OF THE LEADING EDGE OF THE MCD AND 15€? DOWN FROM THE TOP EDGE OF THE MCD. COMPLETED REPAIR WITH REO: 601R-52-10-917
- [SDR SWIA2026031075504](https://openairdocs.org/sdr/SWIA2026031075504.md): Wire Harness · damaged · Mar 10, 2026 · N982SW · Cndair CL6002B19 · Landing Gear System Wiring
  > GEAR DISAGREE WARNING MESSAGE AFTER TAKEOFF WHEN BRINGING GEARS UP (FLIGHT 5958) ISSUE CAUSED BY DAMAGED NOSE LANDING GEAR PROXIMITY HARNESS.
- [SDR SWIA202506130012](https://openairdocs.org/sdr/SWIA202506130012.md): Regulator Valve · faulted · Jun 12, 2025 · N982SW · Cndair CL6002B19 · Cabin Cooling System
  > DURING CLIMB OUT AT 7000 WITH ONLY ONE PACK WORKING (RH) THE RIGHT PACK FAILED. CABIN ALT CAUTION. RAN QRH AND DID NOT SOLVED THE ISSUE CABIN ALT WARNING NEXT. (FLIGHT 4641 - FILED CLOSED) PLEASE REFERENCE AML 1627900 REMOVED AND REPLACED RIGHT SIDE FUSEL
- [SDR SWIA2023112719](https://openairdocs.org/sdr/SWIA2023112719.md): Unknown · warning message · Nov 19, 2023 · N982SW · Cndair CL6002B19 · Landing Gear System
  > D: GEAR DISAGREE WARNING AFTER SELECTING GEAR DOWN FOR LANDING. LEFT MAIN GEAR INDICATED IT WAS STILL UP. COMPLIED WITH QRH, ALL GEAR DOWN AND LOCKED AFTER CYCLING ONCE. LANDED NORMALLY.C: 32-30-1CAT A DUE DATE IS 11/20/23CAT II NOT AUTHORIZEDGEAR DISAGREE WAR
- [SDR SWIA2023112019](https://openairdocs.org/sdr/SWIA2023112019.md): Unknown · warning message · Nov 19, 2023 · N982SW · Cndair CL6002B19 · Landing Gear System
  > D: GEAR DISAGREE WARNING AFTER SELECTING GEAR DOWN FOR LANDING. LEFT MAIN GEAR INDICATED IT WAS STILL UP. COMPLIED WITH QRH, ALL GEAR DOWN AND LOCKED AFTER CYCLING ONCE. LANDED NORMALLY.C: 32-30-1CAT A DUE DATE IS 11/20/23CAT II NOT AUTHORIZEDGEAR DISAGREE WAR
- [SDR SWIA2023052615](https://openairdocs.org/sdr/SWIA2023052615.md): Unknown · gouged · May 15, 2023 · N982SW · Cndair CL6002B19 · Doors
  > CARGO DOOR HAS GOUGES ON HANDLE HOUSING (MARKED) (C-CHECK RO 5/23/2023) REMOVED AND REPLACED WITH NEW HANDLE HOUSING ON CARGO DOOR REF. CRJ-200 SRM, 51-42-21, REO 601R-52-31-403 REV--, DATED: 2023-04-25 AND DWG 601R35027 REV Y. COMPLIED WITH TASK CARD 5
- [SDR SWIA20230526420](https://openairdocs.org/sdr/SWIA20230526420.md): Unknown · corroded · Apr 20, 2023 · N982SW · Cndair CL6002B19 · Doors
  > PAX DOOR INTERCOSTAL DD1A CORRODED (C-CHECK RO 5/23/2023) REMOVED PAX DOOR DD1A MID INTERCOSTAL REF. CRJ 200 SRM 51-42-06 AND INSTALLED NEW PAX DOOR DD1A MID INTERCOSTAL REF. DRWG 601R31702 REV. N AND CRJ 200 SRM 51-42-06, LEAK CHECK GOOD,COMPLIED WIT
- [SDR SWIA2023052601419](https://openairdocs.org/sdr/SWIA2023052601419.md): Unknown · cracked · Apr 19, 2023 · N982SW · Cndair CL6002B19 · Fuselage Main, Structure
  > RT WINDSHIELD POST CRACKED AT TOP BARREL NUT. (C-CHECK RO 5/23/2023) REMOVED AND REPLACED RH SIDE WINDSHIELD POST REF. CRJ-200 SRM, 51-42-21, CRJ-200 SRM, 51-41-02 AND DWG 601R33007 REV U. COMPLIED WITH TASK CARDS 51-900-1003-SKY AND 56-220-1000-SKY. PR
- [SDR SWIA2023053000417](https://openairdocs.org/sdr/SWIA2023053000417.md): Unknown · damaged · Apr 17, 2023 · N982SW · Cndair CL6002B19 · Wing Structure
  > REPLACE OUTBOARD L/E SKIN ON L/H INBOARD FLAP VANE, IDENTIFIED OUT OF LIMITS ON CAMP 26402118, JOB 2795691, OP 95 (C-CHECK RO 5/23/2023) REMOVED AND REPLACED OB LEADING EDGE VANE SKIN ON IB FLAP VANE REF. CRJ-200 SRM, 51-42-10, CRJ-200 SRM, 51-42-13 AND
- [SDR SWIA202305260413](https://openairdocs.org/sdr/SWIA202305260413.md): Unknown · chafed · Apr 13, 2023 · N982SW · Cndair CL6002B19 · Wing Structure
  > * L/H INBOARD FLAP, OUTBOARD HINGE ARM, INBOARD GUIDE PLATE IS CHAFED. (C-CHECK RO 5/23/2023) REMOVED AND REPLACED L/H I/B FLAP O/B HINGE ARM I/B GUIDE PLATE AND 4EA NUTPLATES IAW CRJ200 SRM 51-42-06. SEE CONTINUE CARD FOR WORK PERFORMED.
- [SDR SWIA202305262412](https://openairdocs.org/sdr/SWIA202305262412.md): Unknown · corroded · Apr 12, 2023 · N982SW · Cndair CL6002B19 · Fuselage Structure (General)
  > RIGHT HAND SIDE SEAT RAIL. SEAT RAIL SECTION FROM FS449.85-FS499.00 HAS NUMEROUS WEAR MARKS AND CORROSION. (C-CHECK RO 5/23/2023) REMOVED AND REPLACED RH SEAT SIDE RAIL SECTION FROM FS449.85 TO FS499.00 REF. CRJ-200 AMM, 53-01-11-000-802 AND CRJ-200 AMM
- [SDR SWIA2023052610412](https://openairdocs.org/sdr/SWIA2023052610412.md): Unknown · corroded · Apr 12, 2023 · N982SW · Cndair CL6002B19 · Fuselage Structure (General)
  > RIGHT HAND SIDE SEAT RAIL. SEAT RAIL SECTION FROM FS499.00-FS544.00 HAS NUMEROUS WEAR MARKS AND CORROSION. (C-CHECK RO 5/23/2023) REMOVED AND REPLACED RH SEAT SIDE RAIL SECTION FROM FS449.00 TO FS544.00 REF. CRJ-200 AMM, 53-01-11-000-802 AND CRJ-200 AMM
- [SDR SWIA2023052611412](https://openairdocs.org/sdr/SWIA2023052611412.md): Unknown · corroded · Apr 12, 2023 · N982SW · Cndair CL6002B19 · Fuselage Structure (General)
  > RIGHT HAND SIDE SEAT RAIL. SEAT RAIL SECTION FROM FS544.00-FS559.00+80 HAS NUMEROUS WEAR MARKS AND CORROSION. (C-CHECK RO 5/23/2023) REMOVED AND REPLACED RH SEAT SIDE RAIL SECTION FROM FS544.00 TO FS559.00+80 REF. CRJ-200 AMM, 53-01-11-000-802 AND CRJ-2
- [SDR SWIA20230526412](https://openairdocs.org/sdr/SWIA20230526412.md): Unknown · corroded · Apr 12, 2023 · N982SW · Cndair CL6002B19 · Elevator Tab, Attach Fittings
  > UPON REMOVAL ON JOB 2795695 OP 76 CAMP 26456851, FOUND L/H ELEVATOR L/E HINGE FITTING ASSY P/N 600-24043-1 @ ES16.52 TO HAVE PITTING CORROSION IN BEARING BORES OF BOTH HINGE HALVES. REPLACE HINGE FITTING ASSY. (C-CHECK RO 5/23/2023) REMOVED L/H ELEVAT
- [SDR SWIA20230530410](https://openairdocs.org/sdr/SWIA20230530410.md): Unknown · unknown · Apr 10, 2023 · N982SW · Cndair CL6002B19 · Fuselage Structure (General)
  > LEFT OVERWING EMER EXIT DOOR CUT- OUT HAS CHAFFING ON AFT UPPER DOOR FITTING ON UPPER SILL (C-CHECK RO 5/23/2023) REMOVED AND REPLACED THE LH AFT UPPER FITTING (LH EMER. DOOR CUT OUT) WITH NEW REF. CRJ 200 AMM 20-21-00-910-801 AND DWG #601R31108 REV. J.
- [SDR SWIA202305303410](https://openairdocs.org/sdr/SWIA202305303410.md): Unknown · corroded · Apr 10, 2023 · N982SW · Cndair CL6002B19 · Doors
  > * PAX DOOR FORMER FS 329.41 IS CORRODED. (C-CHECK RO 5/23/2023) REMOVED AND INSTALLED NEW PAX DOOR FORMER AT FS329.41 REF. DRWG 601R31702 REV. N, CRJ 200 SRM 51-42-06 AND CRJ 200 SRM 51-42-21 COMPLIED WITH TASK CARD 51-900-1003-SKY.PRESSURIZATION/LEAK C
- [SDR SWIA202305302410](https://openairdocs.org/sdr/SWIA202305302410.md): Unknown · corroded · Apr 10, 2023 · N982SW · Cndair CL6002B19 · Doors
  > * PAX DOOR INTERCOSTAL DD3 MID IS CORRODED. (C-CHECK RO 5/23/2023) REMOVED PAX DOOR DD3 MID INTERCOSTAL REF. CRJ 200 SRM 51-42-06 AND INSTALLED PAX DOOR DD3 MID INTERCOSTAL REF. DRWG 601R31702 REV. N AND CRJ 200 SRM 51-42-06,LEAK CHECK GOOD,COMPLIED WI
- [SDR SWIA202305301410](https://openairdocs.org/sdr/SWIA202305301410.md): Unknown · corroded · Apr 10, 2023 · N982SW · Cndair CL6002B19 · Doors
  > * PAX DOOR INTERCOSTAL DD2 IS CORRODED. (C-CHECK RO 5/23/2023) REMOVED PAX DOOR DD2 MID INTERCOSTAL REF. CRJ 200 SRM 51-42-06 AND INSTALLED PAX DOOR DD2 MID INTERCOSTAL REF. DRWG 601R31702 REV. N AND CRJ 200 SRM 51-42-06, PRESSURE LEAK CHECK GOOD, COMP
- [SDR SWIA202305300410](https://openairdocs.org/sdr/SWIA202305300410.md): Unknown · unknown · Apr 10, 2023 · N982SW · Cndair CL6002B19 · Doors
  > RIGHT OVERWING EMER EXIT DOOR CUT- OUT HAS CHAFFING ON AFT UPPER DOOR FITTING ON UPPER SILL (C-CHECK RO 5/23/2023) BLENDED OUT DAMAGE AT RH EMERGENCY EXIT DOOR FITTINGS ON AFT UPPER SILL. REF CRJ 200 SRM 51-12-00 FOUND TO BE OUT OF LIMIT MORE THAN 10% O
- [SDR SWIA2023053000410](https://openairdocs.org/sdr/SWIA2023053000410.md): Unknown · corroded · Apr 10, 2023 · N982SW · Cndair CL6002B19 · Doors
  > * PAX DOOR INTERCOSTAL DD1 IS CORRODED. (C-CHECK RO 5/23/2023) REMOVED PAX DOOR DD1 MID INTERCOSTAL REF. CRJ 200 SRM 51-42-06 AND INSTALLED NEW PAX DOOR DD1 MID INTERCOSTAL REF. DRWG 601R31702 REV. N AND CRJ 200 SRM 51-42-06, PRESSURE LEAK CHECK,COMPL
- [SDR SWIA202305300409](https://openairdocs.org/sdr/SWIA202305300409.md): Unknown · cracked · Apr 9, 2023 · N982SW · Cndair CL6002B19 · Fuselage Structure (General)
  > NLG WHEEL WELL - FS 193 @ RBL 6 AND TOP OF WELL - BRACKET CRACKED (C-CHECK RO 5/23/2023) LG WHEEL WELL - FS 202 @ RBL 6 AND TOP OF WELL BRACKET PART# 604-33101-188 IS CRACKED AND IS OUT OF LIMITS REF CRJ200 SRM 53-00-00. REMOVED CRACKED BRACKET REF CRJ2
- [SDR SWIA2023053000409](https://openairdocs.org/sdr/SWIA2023053000409.md): Unknown · corroded · Apr 9, 2023 · N982SW · Cndair CL6002B19 · Fuselage Structure (General)
  > L/H PRESSURE FLOOR SILL PANEL CORROSION FROM FS 409.0+128 TO FS 559.0 ( MARKED WITH READ GREASE PENCIL) (C-CHECK RO 5/23/2023) REPAIRED LH PRESSURE FLOOR SILL FROM FS 409.00+128 TO FS 559.00 REF REO 601R-53-41-666 REV C DATED 2012-11-06 DISPOSITION 1.2
- [SDR SWIA20230526409](https://openairdocs.org/sdr/SWIA20230526409.md): Unknown · corroded · Apr 9, 2023 · N982SW · Cndair CL6002B19 · Fuselage Structure (General)
  > CORROSION ON L/H SEAT RAIL BETWEEN FS 409.0+128 AND FS 559.00 (C-CHECK RO 5/23/2023) REMOVED AND REPLACED LH SEAT RAIL BETWEEN FS409.0+128 AND FS559.00 REF. CRJ-200 AMM, 53-01-11-000-802 AND CRJ-200 AMM, 53-01-11-400-802.
- [SDR SWIA20230530407](https://openairdocs.org/sdr/SWIA20230530407.md): Unknown · cracked · Apr 7, 2023 · N982SW · Cndair CL6002B19 · Fuselage Structure (General)
  > * INTERCOSTAL FROM FS621 TO FS625, STR13L, IS CRACKED. (C-CHECK RO 5/23/2023) REMOVED AND REPLACED INTERCOSTAL FROM FS621 TO FS625, STR13L REF. DRWG 601-35012 REV. D AND CRJ 200 SRM 51-42-21. COMPLIED WITH 53-900-1003-SKY AND SKYWEST FORM M-337
- [SDR SWIA20230530405](https://openairdocs.org/sdr/SWIA20230530405.md): Unknown · dented · Apr 5, 2023 · N982SW · Cndair CL6002B19 · Doors
  > * PASSENGER DOOR SEAL STRIKER DENTED NEAR UPPER AFT CORNER. ( FLAGGED) (C-CHECK RO 5/23/2023) PERFORMED REPAIR OF THE PASSENGER DOOR SEAL STRIKER NEAR UPPER AFT CORNER BY COMPLYING WITH REO 601R-53-22-033 REV -D, DATED 2014/02/17, REPAIR TYPE 1.COMPLIE
- [SDR SWIA202305300405](https://openairdocs.org/sdr/SWIA202305300405.md): Unknown · chafed · Apr 5, 2023 · N982SW · Cndair CL6002B19 · Fuselage Structure (General)
  > CHAFFING DISCOVERED ON INSIDE SURFACE OF DECOMPRESSION PANEL CUT OUT (C-CHECK RO 5/23/2023) COMPLIED WITH REO REPAIR 601R-52-11-2977 REV. - DATED 2023-05-04 SEE CONTINUATION CARD FOR WORK ACCOMPLISHED.C/W 51-900-1003-SKY
- [SDR SWIA202305300403](https://openairdocs.org/sdr/SWIA202305300403.md): Unknown · corroded · Apr 3, 2023 · N982SW · Cndair CL6002B19 · Fuselage Structure (General)
  > CORROSION FOUND AT FRAME STATION 559 ON L/H FLOOR INTERCOSTAL CROSS MEMBER BETWEEN L/H O/B SEAT TRACK AND FLOOR SILL APPROX LBL 27+ (C-CHECK RO 5/23/2023) REMOVED AND INSTALLED NEW STRAP (PN 601R31025-29) AT FS559 BETWEEN LBL27 AND LBL48 PER CRJ200 SRM
- [SDR SWIA20230530403](https://openairdocs.org/sdr/SWIA20230530403.md): Unknown · corroded · Apr 3, 2023 · N982SW · Cndair CL6002B19 · Fuselage Structure (General)
  > CORROSION FOUND AT FRAME STATION 559 ON FLOOR INTERCOSTAL CROSS MEMBER BETWEEN R/H O/B SEAT TRACK AND FLOOR SILL APPROX. RBL 27+ (C-CHECK RO 5/23/2023) REPARED PER BOMBARDIER REO 601R-53-41-3157 REV -- DATE 2023-04-24, AND BOMBARDIER DWG 601R31025 REV N
- [SDR SWIA20230530401](https://openairdocs.org/sdr/SWIA20230530401.md): Unknown · cracked · Apr 1, 2023 · N982SW · Cndair CL6002B19 · Doors
  > * GROUND POWER PLUG MOUNTING BRACKET IS CRACKED, MARKED. (C-CHECK RO 5/23/2023) REMOVED & REPLACED WITH NEW GROUND POWER MOUNTING PLATES (BRACKET) PN 600-33283-33. REF CRJ 200 SRM 51-42-21 AND SRM 51-42-06 AND PER DWG NO. PL 600-33283, REV-F. COMPLIED
- [SDR SWIA202305300401](https://openairdocs.org/sdr/SWIA202305300401.md): Unknown · cracked · Apr 1, 2023 · N982SW · Cndair CL6002B19 · Fuselage Structure (General)
  > *FS235.00 STRG 26R POSSIBLE EXTERIOR SKIN CRACK AT NLG AFT DOOR CUT OUT RADIUS (MARKED) (C-CHECK RO 5/23/2023) TRIMMED SKIN TO REMOVE CRACKAND INSTALLED REPAIR, APPLIED FILLET SEAL REF REO 601R-53-11-048 REV D DATED 2015-06-10,LEAK CHECK GOOD.C/W 51-
- [SDR SWIA20230530328](https://openairdocs.org/sdr/SWIA20230530328.md): Unknown · cracked · Mar 28, 2023 · N982SW · Cndair CL6002B19 · Fuselage Structure (General)
  > UPON REMOVAL OF PROTECTIVE BARRIER AT FS621 BULKHEAD, 2EA HOLES ARE ELONGATED/CRACKED AT APPROX WL120 (C-CHECK RO 5/23/2023) REPAIRED 13EA. ELONGATED/CRACKED HOLES AT FS.621 BULKHEAD APPROX WL120 REF. REO 601R-53-61-7999 REV.--, DATED 2023-05-05 STEPS 1
- [SDR SWIA20230530327](https://openairdocs.org/sdr/SWIA20230530327.md): Unknown · torn · Mar 27, 2023 · N982SW · Cndair CL6002B19 · Wing Structure
  > L/H I/B FLAP I/B RUB STRIP IS TORN (C-CHECK RO 5/23/2023) REMOVED AND REPLACED L/H I/B FLAP I/B RUB STRIP REF. CRJ-200 SRM, 51-42-06, CRJ-200 SRM, 51-42-13 AND REO 601R-57-52-2486 REV--, DATED: 2023-04-28 AND DWG 601R14002 REV K. COMPLIED WITH TASK CARD
- [SDR SWIA2023053027](https://openairdocs.org/sdr/SWIA2023053027.md): Unknown · chafed · Mar 27, 2023 · N982SW · Cndair CL6002B19 · Wing Structure
  > LEFT I/B FLAP VANE SKIN IS CHAFFED IN MULTIPLE LOCATIONS COMMON TO BUMP STOPS (C-CHECK RO 5/23/2023) REMOVED AND REPLACED LH IB FLAP OUTER MID L/E VANE SKIN REF. CRJ-200 SRM, 51-42-10 AND DWG 601R14302 REV E. I/B SIDE VANE L/E SKIN FOUND TO BE WITHIN LI
- [SDR SWIA20230530326](https://openairdocs.org/sdr/SWIA20230530326.md): Unknown · chafed · Mar 26, 2023 · N982SW · Cndair CL6002B19 · Ailerons
  > R/H I/B FLAP VANE SKIN CHAFFED ON L/E AT 3 LOCATIONS COMMON TO BUMP STOPS (C-CHECK RO 5/23/2023) REMOVED AND REPLACED RH IB FLAP VANE, MID FLAP VANE CAP REF. CRJ-200 SRM, 51-42-13 AND DWG 601R14303 REV J. RH IB FLAP, OB AND IB FLAP VANE CAPS FOUND TO BE
- [SDR SWIA202266444](https://openairdocs.org/sdr/SWIA202266444.md): None · odor · Sep 7, 2022 · N982SW · Cndair CL6002B19 · Air Conditioning System
  > SMELL OF BURNING PLASTIC FROM ELECTRIC POWER SERVICE PANEL AREA. (FLIGHT #5571 FILED CLOSED) UPON ARRIVAL TO AIRCRAFT, OBSERVED NO SMELL OR ODOR OF BURNING PLASTIC OR ELECTRICAL IN COCKPIT (OR ELECTRIC POWER SERVICE PANEL AREA) AS CREW REPORTED. OPERATED A
- [SDR SWIA2019122747234](https://openairdocs.org/sdr/SWIA2019122747234.md): Intercostal · corroded · Dec 6, 2019 · N982SW · Cndair CL6002B19 · Passenger/Crew Doors
  > CORROSION FOUND ON THE PAX DOOR FWD INTERCOSTAL, AFTER NUTPLATE REMOVAL. REMOVED AND REPLACED THE INTERCOSTAL IAW SRM AND DWG.
- [SDR SWIA2019122747232](https://openairdocs.org/sdr/SWIA2019122747232.md): Intercostal · corroded · Dec 6, 2019 · N982SW · Cndair CL6002B19 · Passenger/Crew Doors
  > CORROSION FOUND ON PAX DOOR FWD INTERCOSTAL DD2 AFTER NUTPLATE REMOVAL. REMOVED AND REPLACED THE INTERCOSTAL IAW SRM AND DWG REV N.
- [SDR SWIA2019122747306](https://openairdocs.org/sdr/SWIA2019122747306.md): Intercostal · corroded · Nov 26, 2019 · N982SW · Cndair CL6002B19 · Passenger/Crew Doors
  > PASSENGER DOOR INTERNAL STRUCTURE, INTERCOSTAL DD7A AT FS320-FS327 HAS NUMEROUS AREAS OF CORROSION. REMOVED AND REPLACED INTERCOSTAL DD7A REF SRM AND DWG, COMPLETED TASK CARD, CHECKS OKAY
- [SDR SWIA2019122747304](https://openairdocs.org/sdr/SWIA2019122747304.md): Intercostal · corroded · Nov 26, 2019 · N982SW · Cndair CL6002B19 · Passenger/Crew Doors
  > PASSENGER DOOR INTERNAL STRUCTURE, INTERCOSTAL DD6 AT FS320-FS338 HAS NUMEROUS AREAS OF CORROSION. REMOVED AND REPLACED INTERCOSTAL DD6 REF SRM AND DWG, COMPLETED TASK CARD, CHECKS OKAY

Next page: https://openairdocs.org/aircraft/N982SW/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 = 'N982SW' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N982SW/reports

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