# Service difficulty reports: N946SW

A list on [N946SW](https://openairdocs.org/aircraft/N946SW.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 · 218 reports

- [SDR SWIA2025041600015](https://openairdocs.org/sdr/SWIA2025041600015.md): Warning Message · illuminated · Apr 15, 2025 · N946SW · Cndair CL6002B19 · Landing Gear Position and Warning
  > NOSE DOOR OPEN MASTER WARNING AFTER SELECTING GEAR UP AFTER TAKEOFF. (FLIGHT 5045) SEE EAML 1583020 FOR CORRECTIVE ACTION.
- [SDR SWIA20250326003](https://openairdocs.org/sdr/SWIA20250326003.md): Skin · dented · Mar 23, 2025 · N946SW · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > FUSELAGE SKIN HAS TWO SMALL DENTS LOCATED BETWEEN FS654.50 & FS672.00 AND STGR'S 0 & 1L. (C-CHECK RO 03/25/2024)COMPLIED WITH TEMPORARY DISPOSITION FOR DENTS TO FUSELAGE SKIN BETWEEN FS654.50 - FS672.00 AND STR 0 - STR 1L WITH REFERENCE TO REO 601R-53-61-8308
- [SDR SWIA202503260018](https://openairdocs.org/sdr/SWIA202503260018.md): Rivet · loose · Mar 18, 2025 · N946SW · Cndair CL6002B19 · Trailing Edge Flaps
  > MULTIPLE SMOKEING RIVETS FOUND ON LH OUTBOARD FLAP UPPER SURFACE BETWEEN WS 162.49 - WS 178.00 AND BETWEEN WS 213.08 - WS 242.00. (C-CHECK RO 03/25/2024)REMOVED AND REPLACED MULTIPLE SMOKING RIVETS FOUND ON LH OUTBOARD FLAP UPPER SURFACE BETWEEN WS 162.49 - WS
- [SDR SWIA202503180015](https://openairdocs.org/sdr/SWIA202503180015.md): Tripler · gouged · Mar 15, 2025 · N946SW · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > REAR PRESSURE BULKHEAD FWD FACE TRIPLERS (FS621.00), LBL27.50, LBL18.00, LBL9.50, RBL9.50, RBL18.00, RBL27.50, RBL36.20 @ WL103.50 AND LBL9.50, RBL9.50 @ WL87.50 HAS GOUGES FROM CARGO LINER SCREWS. (FILED CLOSED) DRESSED DENT BACK ON PANEL 620ML AT W
- [SDR SWIA20250317015](https://openairdocs.org/sdr/SWIA20250317015.md): Pressure Blkhd · gouged · Mar 15, 2025 · N946SW · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > REAR PRESSURE BULKHEAD FWD FACE TRIPLERS (FS621.00), LBL27.50, LBL18.00, LBL9.50, RBL9.50, RBL18.00, RBL27.50, RBL36.20 @ WL103.50 AND LBL9.50, RBL9.50 @ WL87.50 HAS GOUGES FROM CARGO LINER SCREWS. (FILED OPEN) THIS IS CURRENTLY A WORK IN PROGRESS
- [SDR SWIA202503260006](https://openairdocs.org/sdr/SWIA202503260006.md): Skin · dented · Mar 6, 2025 · N946SW · Cndair CL6002B19 · Wing, Plate/Skin
  > RH WING LEADING EDGE AT APPROX. WS127 DENTED ON BOTTOM SURFACE, APPROX. 5 INCHES FROM TRAILING EDGE. (2.5 INCHES LONG X.5 INCHES WIDE.) (C-CHECK RO 03/25/2024)TEMP REPAIRED RH WING LEADING EDGE DENT AT APPROX WS127 APPROX 5.0" FROM TRAILING EDGE ON BOTTOM SUR
- [SDR SWIA202503260222](https://openairdocs.org/sdr/SWIA202503260222.md): Landing · cracked · Feb 22, 2025 · N946SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > UPON REMOVAL OF THE STOPPER FITTING ON THE SILL LANDING, FOUND DENTED (UPWARD AND DOWNWARD) AND CRACKED FASTENER HOLES X(2) LOCATED INBOARD AND FWD OF CARGO BAY DOOR AT FS 574.00, WL 73.00 & LBL 43.00. (C-CHECK RO 03/25/2024)PERFORMED REPAIR OF FLOOR LANDING P
- [SDR SWIA202503260213](https://openairdocs.org/sdr/SWIA202503260213.md): Support · damaged · Feb 13, 2025 · N946SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > CARGO LINER SUPPORT - GAS BARRIER FS 574.00 TO FS 621.00 AND STR 3L (REF DWG 601R45105) HAS 6 ELONGATED/GOUGED FASTENER HOLES. (C-CHECK RO 03/25/2024)REMOVED, MADE AND REPLACED THE CARGO LINER SUPPORT - GAS BARRIER FS 574.00 TO FS 621.00 AND STR 3L (REF DWG 60
- [SDR SWIA202503260204](https://openairdocs.org/sdr/SWIA202503260204.md): Skin · dented · Feb 4, 2025 · N946SW · Cndair CL6002B19 · Rudder, Plate/Skin
  > RUDDER HAS A DENT ON THE LH SIDE ABOVE THE TOP PCU RIB (C-CHECK RO 03/25/2024)COMPLIED WITH 601R-55-41-298 DATED: 2025-02-24 REV -- REPAIR TO RUDDER LHS SKIN BETWEEN STA 95.57 & STA 102.52. COMPLETED THE M-337. COMPLIED WITH TASK CARD 51-900-1003-SKY. NDT'S CO
- [SDR SWIA202503260130](https://openairdocs.org/sdr/SWIA202503260130.md): Floor Support · corroded · Jan 30, 2025 · N946SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > FOUND MULTIPLE SPOTS OF SURFACE CORROSION ON THE LH PRESSURE FLOOR SILL ASSY BETWEEN FS 409 + 128 & FS 559.00 AND IN BETWEEN LBL 36.0 & LBL 45.0 (C-CHECK RO 03/25/2024)BLENDED CORROSION ON LH PRESSURE FLOOR SILL ASSY WL73.00 BETWEEN FS409 + 128 TO FS559.00 AND
- [SDR SWI2025F00402](https://openairdocs.org/sdr/SWI2025F00402.md): Floor Support · corroded · Jan 30, 2025 · N946SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > FOUND SURFACE CORROSION ON THE RH PRESSURE FLOOR SILL AFT STRAP @ FS 559.00 AND IN BETWEEN RBL 27.00 & RBL 36.00 (C-CHECK RO 03/25/2024)REMOVED AND REPLACED THE RH PRESSURE FLOOR SILL AFT STRAP @ FS 559.00 AND IN BETWEEN RBL 27.00 & RBL 36.00 IN REFERENCE WITH
- [SDR SWIA202503260122](https://openairdocs.org/sdr/SWIA202503260122.md): Intercostal · cracked · Jan 22, 2025 · N946SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > INTERCOSTAL CRACKED ON AFT SIDE OF REAR PRESSURE BULKHEAD AT FS621.0, JUST OUTBOARD OF LBL36.20 AND INLINE WITH STRINGER 15L (C-CHECK RO 03/25/2024) (FILED CLOSED) REMOVED AND REPLACED INTERCOSTAL / CLIP ON AFT SIDE OF REAR PRESSURE BULKHEAD AT FS621.00 J
- [SDR SWIA202502030022](https://openairdocs.org/sdr/SWIA202502030022.md): Intercostal · cracked · Jan 22, 2025 · N946SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > INTERCOSTAL CRACKED ON AFT SIDE OF REAR PRESSURE BULKHEAD AT FS621.0, JUST OUTBOARD OF LBL36.20 AND INLINE WITH STRINGER 15L (FILED OPEN) THIS IS CURRENTLY A WORK IN PROGRESS
- [SDR SWIA202503260121](https://openairdocs.org/sdr/SWIA202503260121.md): Landing · corroded · Jan 21, 2025 · N946SW · Cndair CL6002B19 · Wing Main, Frame Structure
  > LH WING FUEL CELL ACCESS DOOR LANDING AT PANEL 540EB HAS AN AREA OF MINOR CORROSION ON THE AFT EDGE MID POINT OF LANDING, APPROX 8" IN TOTAL. (C-CHECK RO 03/25/2024) (FILED CLOSED) BLENDED CORRODED AREA OF LH WING FUEL CELL ACCESS DOOR LANDING AT PANEL 54
- [SDR SWIA2025012200021](https://openairdocs.org/sdr/SWIA2025012200021.md): Access Panel · corroded · Jan 21, 2025 · N946SW · Cndair CL6002B19 · Wing, Plate/Skin
  > LH WING FUEL CELL ACCESS DOOR LANDING AT PANEL 540EB HAS AN AREA OF MINOR CORROSION ON THE AFT EDGE MID POINT OF LANDING, APPROX 8" IN TOTAL.
- [SDR SWIA202503260117](https://openairdocs.org/sdr/SWIA202503260117.md): Access Panel · corroded · Jan 17, 2025 · N946SW · Cndair CL6002B19 · Wing, Plate/Skin
  > RH WING FUEL CELL ACCESS PANE 650FB, LOWER WING PLANK ACCESS HOLE, HAS CORROSION PRESENT FROM 3 O'CLOCK POSITION TO 6 O'CLOCK POSITION. (C-CHECK RO 03/25/2024) (FILED CLOSED) BLENDED CORRODED AREA OF RH WING FUEL CELL ACCESS DOOR LANDING AT PANEL 650FB O
- [SDR SWIA2025012000017](https://openairdocs.org/sdr/SWIA2025012000017.md): Access Panel · corroded · Jan 17, 2025 · N946SW · Cndair CL6002B19 · Wing, Plate/Skin
  > RH WING FUEL CELL ACCESS PANE 650FB, LOWER WING PLANK ACCESS HOLE, HAS CORROSION PRESENT FROM 3 O'CLOCK POSITION TO 6 O'CLOCK POSITION. (FILED OPEN) THIS IS CURRENTLY A WORK IN PROGRESS
- [SDR SWIA202503290114](https://openairdocs.org/sdr/SWIA202503290114.md): Latch · faulted · Jan 14, 2025 · N946SW · Cndair CL6002B19 · Emergency Exits
  > COCKPIT EMERGENCY EXIT HATCH EXTERNAL HANDLE WON'T STAY LATCHED (C-CHECK RO 03/25/2024)REPLACED CREW ESCAPE HATCH LATCH ASSEMBLY IN REFERENCE TO SRM 51-42-06 AND AMM 52-22-02. COMPLIED WITH TASK CARD 51-900-1003-SKY AND COMPLETED M-337. REFERENCE CP 29519786 F
- [SDR SWIA2021120662958](https://openairdocs.org/sdr/SWIA2021120662958.md): Flap System · failed · Dec 5, 2021 · N946SW · Cndair CL6002B19 · Trailing Edge Flap Control System
  > ON APPROACH, WHEN SELECTING FLAPS 30, THE FLAP FAIL CAUTION ILLUMINATED. FLAPS INDICATED FLAP 23. AFTER CONDUCTING A MISSED APPROACH, COMPLIED WITH QRH AND LANDED WITH ABNORMAL FLAP POSITION AT NEW SPEEDS AND 200-300 FPM DECENT. (FLIGHT 4665 - FILED CLOSED)
- [SDR SWIA2021112262669](https://openairdocs.org/sdr/SWIA2021112262669.md): Light · arced · Nov 20, 2021 · N946SW · Cndair CL6002B19 · Emergency Lighting
  > COCKPIT FLOOD LIGHTS WENT INOP, SMOKE AND BURNING SMELL (FLIGHT 5974 - FILED CLOSED) TROUBLESHOOT COCKPIT FLOOD LIGHTS INOP, FOUND R/H AFT FLOOD LIGHT PANEL WITH SIGNS OF ARCHING AND BURN MARKS. REMOVED AND REPLACED R/H AFT MOST FLOOD INSTRUMENT LIGHT PA
- [SDR SWIA202161735](https://openairdocs.org/sdr/SWIA202161735.md): None · damaged · Sep 8, 2021 · N946SW · Cndair CL6002B19 · Fuselage Internal Mounting Structure
  > PERFORM FLOOR BEAM UPPER CAP SPLICE REPAIR ON LBL27 BETWEEN F.S.559+80 AND EXISTING FACTORY SPLICE AT F.S.559+112 (C-CHECK RO 10/8/2021) PERFORMED FLOOR BEAM UPPER CAP SPLICE REPAIR ON LBL27 BETWEEN F.S.559+80 AND EXISTING FACTORY SPLICE AT F.S.559+112
- [SDR SWIA202161734](https://openairdocs.org/sdr/SWIA202161734.md): None · cracked · Sep 8, 2021 · N946SW · Cndair CL6002B19 · Wing Structure
  > FOUND A CRACKED SATELLITE HOLE AT R/WING WS 85.50 AFT SIDE (AS MARKED). HOLE IS AT PRE-COLD WORK SIZE.235" AND ALREADY COUNTERSUNK FOR HILITE, WHILE WORKING WITH SB 601R-57-054. (C-CHECK RO 10/8/2021) REPAIRED MID WING PLANK LOWER WATER DRAIN HOLE AT
- [SDR SWIA202161733](https://openairdocs.org/sdr/SWIA202161733.md): None · damaged · Sep 7, 2021 · N946SW · Cndair CL6002B19 · Fuselage Internal Mounting Structure
  > PERFORM REPAIR TO FLOOR BEAM FLANGE AT FS605.0-FS621.0, LBL27.0 (C-CHECK RO 10/8/2021) PERFORMED REPAIR TO FLOOR BEAM FLANGE AT FS605.0-FS621.0, LBL27.0. REF REO 601R-53-61-7713 REV. -- DATED 2021-09-12. COMPLIED WITH 51-900-1003-SKY
- [SDR SWIA202161732](https://openairdocs.org/sdr/SWIA202161732.md): None · none · Sep 1, 2021 · N946SW · Cndair CL6002B19 · Engine Cowl Flaps
  > WHILE REMOVING FASTENERS FOR LH ENGINE NOSE COWL ASSY. ATTACHMENT CLIP, MISDRILLED TWO FASTENER HOLES IN ATTACHMENT FLANGE. (C-CHECK RO 10/8/2021) REPAIRED LH ENGINE NOSE COWL ASSY. REF REO 601R-71-61-4336 REV -- 2021-09-10 COMPLIED WITH ALL STEPS. COM
- [SDR SWIA202161731](https://openairdocs.org/sdr/SWIA202161731.md): None · nicked · Aug 26, 2021 · N946SW · Cndair CL6002B19 · Wing, Landing Gear Attach Fittings
  > *LH OUTBOARD FLAP HINGE ARM AT WS 220 €“ NICK ON OUTBOARD FLAP HINGE ARM AT CONNECTION TO HINGE BOX. (C-CHECK RO 10/8/2021) NICK ON LH OUTBOARD FLAP HINGE ARM AT WS 220 €“ ON OUTBOARD FLAP HINGE ARM AT CONNECTION TO HINGE BOX IS BLENDED AND RESTORED
- [SDR SWIA202161730](https://openairdocs.org/sdr/SWIA202161730.md): None · gouged · Aug 26, 2021 · N946SW · Cndair CL6002B19 · Wing, Landing Gear Attach Fittings
  > *RH INBOARD FLAP GOUGED AT ATTACHMENT TO HINGE BOX (MARKED). (C-CHECK RO 10/8/2021) BLENDED GOUGE ON RH INBOARD FLAP AT ATTACHMENT TO HINGE BOX. RE WORK AREA IS WITHIN LIMITS AND RESTORED TO ORIGINAL REF REO 601R-57-54-337 REV.-- DATED 2021-09-07. COMP
- [SDR SWIA202161729](https://openairdocs.org/sdr/SWIA202161729.md): None · damaged · Aug 25, 2021 · N946SW · Cndair CL6002B19 · Fuselage Internal Mounting Structure
  > FLOOR BEAM FROM FS 574 TO FS 605 ON LBL 27.00 REQUIRES REPLACEMENT (C-CHECK RO 10/8/2021) FLOOR BEAM P/N 601R35031-263 FROM FS574.00 TO FS605.00 ON LBL 27.00 WAS REMOVED AND REPLACED WITH A NEW BEAM IAW REO 601R-53-61-3778 REV. B, DATE: 2016-12-19, R
- [SDR SWIA202161728](https://openairdocs.org/sdr/SWIA202161728.md): None · chafed · Aug 22, 2021 · N946SW · Cndair CL6002B19 · Fuselage, Equipment Attach Fittings
  > * THE PASSENGER DOOR HINGE HALF (FUSELAGE SIDE) HAS CHAFES AND SCRATCHES ON ALL 27 OF ITS LUGS, AND HAS CHAFES AND SCRATCHES ON ALL 27 OF ITS LANDS, WITH A DEEP GOUGE IN THE AFT MOST LAND. (C-CHECK RO 10/8/2021) INSTALLED NEW PASSENGER DOOR HINGE ( FUSE
- [SDR SWIA202161727](https://openairdocs.org/sdr/SWIA202161727.md): None · cracked · Aug 21, 2021 · N946SW · Cndair CL6002B19 · Fuselage Main, Keel
  > CRACK ON STGR 3L AFT OF FS 280.00 (C-CHECK RO 10/8/2021) REMOVED CRACKED CLEAT, VERIFIED STRINGER 3L AT FS280 IS CRACK FREE, INSTALLED NEW CLEAT AT STRINGER 3L AND FS280 P/N 600-34017-589 REF CRJ 200 SRM 51-42-10, CRJ 200 SRM 51-42-06, DRAWING 600-34017
- [SDR SWIA202161726](https://openairdocs.org/sdr/SWIA202161726.md): None · cracked · Aug 21, 2021 · N946SW · Cndair CL6002B19 · Doors
  > CARGO DOOR SURROUND STRUCTURE - FS 574 CARGO DOOR TRACK SUPPORT BRACKET HAS A CRACK @ BOTTOM RIVET (C-CHECK RO 10/8/2021) REMOVED AND INSTALLED NEW CHANNEL PN: 601R35050-25 AT FS 574 CARGO DOOR TRACK STRUCTURE IAW DWG: 601R35050 REV Y. AND CRJ200 SRM 51
- [SDR SWIA202161725](https://openairdocs.org/sdr/SWIA202161725.md): None · torn · Aug 20, 2021 · N946SW · Cndair CL6002B19 · Elevator, Tab Structure
  > LH ELEVATOR LEADING EDGE SKIN AT #2 HINGE POINT IS TORN. (MARKED) (C-CHECK RO 10/8/2021) REPAIRED LH ELEVATOR LEADING EDGE SKIN REF REO 601R-55-21-553 REV -- DATED 2021-08-27. COMPLIED WITH 51-900-1003-SKY AND SEE CONTINUATION CARD FOR DETAILS
- [SDR SWIA202161724](https://openairdocs.org/sdr/SWIA202161724.md): None · chafed · Aug 20, 2021 · N946SW · Cndair CL6002B19 · Elevator Tab, Attach Fittings
  > RH ELEVATOR HINGE #4 ON HORIZONTAL STABILIZER AT BL95.793 HAS 1 CHAFE (C-CHECK RO 10/8/2021) REMOVED CHAFE FROM RH ELEVATOR HINGE #3 ON HORIZONTAL STABILIZER AT BL55.8865 REF MHIRJ REO 601R-55-11-696 REV - - DATED 2021-09-03 FOR DETAILS SEE ATTACHED CON
- [SDR SWIA202161723](https://openairdocs.org/sdr/SWIA202161723.md): None · chafed · Aug 20, 2021 · N946SW · Cndair CL6002B19 · Elevator Tab, Attach Fittings
  > RH ELEVATOR HINGE #3 ON HORIZONTAL STABILIZER AT BL55.8865 HAS 2 CHAFED AREAS (C-CHECK RO 10/8/2021) REMOVED CHAFE FROM RH ELEVATOR HINGE #3 ON HORIZONTAL STABILIZER AT BL55.8865 REF MHIRJ REO 601R-55-11-695 REV - - DATED 2021-09-03 FOR DETAILS SEE ATT
- [SDR SWIA202161722](https://openairdocs.org/sdr/SWIA202161722.md): None · gouged · Aug 20, 2021 · N946SW · Cndair CL6002B19 · Wing Structure
  > LH AILERON POSITION TRANSMITTER FITTING IS GOUGED. (MARKED ON AILERON) (C-CHECK RO 10/8/2021) REMOVED DAMAGE TO LH AILERON POSITION TRANSMITTER FITTING REF REO 601R-57-61-796 REV -- DATED 2021-09-10 AND COMPLIED WITH ALL STEPS, NO FURTHER DEFECTS AT THI
- [SDR SWIA202161721](https://openairdocs.org/sdr/SWIA202161721.md): None · corroded · Aug 20, 2021 · N946SW · Cndair CL6002B19 · Fuselage Structure (General)
  > * AFT WING TO BODY FAIRING 195BB HAS MULTIPLE CORRODED DOME NUTS A/C SIDE (MARKED) (C-CHECK RO 10/8/2021) REMOVED AND INSTALLED NEW AFT WING TO BODY FAIRING NUTPLATES REF CRJ-200-SRM 51-42-06 AND INSTALLED ALTERNATE FASTENERS FOR THE GROUND AIR CONDITI
- [SDR SWIA202161720](https://openairdocs.org/sdr/SWIA202161720.md): None · cracked · Aug 20, 2021 · N946SW · Cndair CL6002B19 · Fuselage Main, Frame
  > * SUSPECTED CRACK ON CLIP AT APPROXIMATELY FS200 LBL22 WL72 (C-CHECK RO 10/8/2021) OLD BRACKET REMOVED PER CRJ 200 SRM 51-42-06 / NEW BRACKET INSTALLED PER CRJ 200 SRM 51-42-06, CRJ 200 SRM 51-42-21 AND BOMBARDIER DRAWING #K601R34014 REV F / COMPLIED WI
- [SDR SWIA202161719](https://openairdocs.org/sdr/SWIA202161719.md): None · chafed · Aug 20, 2021 · N946SW · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > * FS280 BULKHEAD CHAFED ON AFT SIDE BETWEEN RBL11 €“ RBL 15 AT APPROXIMATELY WL93 (C-CHECK RO 10/8/2021) REPAIRED FS280 BULKHEAD AFT SIDE BETWEEN RBL11 €“ RBL 15 AT APPROXIMATELY WL93 REF CRJ200 SRM 51-42-06 AND REO 601R-53-11-1727 REV -E 2011-01-1
- [SDR SWIA202161718](https://openairdocs.org/sdr/SWIA202161718.md): None · bent · Aug 20, 2021 · N946SW · Cndair CL6002B19 · Fuselage Structure (General)
  > * LH TRU BAY DOOR AFT SEAL LANDING IS BENT/DEFORMED (C-CHECK RO 10/8/2021) REMOVED AND REPLACED THE LH TRU BAY DOOR AFT SEAL LANDING WITH 1EA. NEW PART REF. CRJ200 SRM 51-42-06 & DWG 600-34011 REV -K. COMPLIED WITH 51-900-1003-SKY.
- [SDR SWIA202161749](https://openairdocs.org/sdr/SWIA202161749.md): None · corroded · Aug 19, 2021 · N946SW · Cndair CL6002B19 · Doors
  > *PAX DOOR ANCHOR FITTING AT FS 349.00 HAS CORRODED HARDWARE (C-CHECK RO 10/8/2021) REMOVED AND INSTALLED PAX DOOR AFT ANCHOR FITTING. REF CRJ 200 AMM 52-11-17-000-803, AND NEW 6 BOLTS 12 WASHERS 6 NUTS. 1 SCREW 1 NUT 1 WASHER. 1 ADJUSTER BOLT 1 WASHER
- [SDR SWIA202161717](https://openairdocs.org/sdr/SWIA202161717.md): None · corroded · Aug 19, 2021 · N946SW · Cndair CL6002B19 · Fuselage Main, Frame
  > FRAME AT FS424 STR0 HAS CORROSION ON SPLICE PLATE (MARKED) (C-CHECK RO 10/8/2021) CORROSION BLENDED AND AREA REPAIRED IAW WITH STEPS 1-5 OF MHIRJ REPAIR ENGINEERING ORDER 601R-53-41-2961 REV --, DATED 2021-09-07. COMPLIED WITH 51-900-1003-SKY.
- [SDR SWIA202161716](https://openairdocs.org/sdr/SWIA202161716.md): None · damaged · Aug 19, 2021 · N946SW · Cndair CL6002B19 · Fuselage Internal Mounting Structure
  > FLOOR BEAM AT FS409+64 TO FS409+80 LBL28 HAS 2 ELONGATED / "SNOWMANNED" RIVET HOLES (MARKED) (C-CHECK RO 10/8/2021) REMOVED AND INSTALLED NEW FLOOR BEAM CAP AT LBL27 BETWEEN FS409+5 & FS409+118 REF CRJ200 SRM 51-42-21, CRJ200 SRM 51-42-22, CRJ200 SRM 51
- [SDR SWIA202161715](https://openairdocs.org/sdr/SWIA202161715.md): None · corroded · Aug 19, 2021 · N946SW · Cndair CL6002B19 · Galley Doors
  > *SERVICE DOOR DOUBLER ON LOWER SILL STGR18R HAS AREAS OF CORROSION ON FS 319.00 AND FS 349.00 (C-CHECK RO 10/8/2021) CORROSION AT SERVICE DOOR DOUBLERS ON LOWER SILL STGR18R FS319.00 AND FS349.00 WAS BLENDED IAW CRJ200 SRM 51-21-06. EVALUATED AND FOUND
- [SDR SWIA202161748](https://openairdocs.org/sdr/SWIA202161748.md): None · corroded · Aug 18, 2021 · N946SW · Cndair CL6002B19 · Doors
  > *CORROSION ON PAX DOOR UPPER STOP BRACKET AND STOP BOLT (C-CHECK RO 10/8/2021) REMOVED AND INSTALLED NEW UPPER STOP BRACKET (P/N 601R38921-15) AND BOLT PAX DOOR IAW SRM 51-42-13 AND 51-41-02
- [SDR SWIA202161747](https://openairdocs.org/sdr/SWIA202161747.md): None · corroded · Aug 18, 2021 · N946SW · Cndair CL6002B19 · Doors
  > *CORROSION ON PAX DOOR LOWER STOP BRACKET AND STOP BOLT (C-CHECK RO 10/8/2021) REMOVED CORROSION ON PAX DOOR LOWER STOP BRACKET REF CRJ200 SRM 51-21-06. ORIGINAL MATERIAL THICKNESS OF BLENDED AREA IS 0.100" REMAINING MATERIAL MEASURED IS 0.085" OUT LIMI
- [SDR SWIA202161714](https://openairdocs.org/sdr/SWIA202161714.md): None · corroded · Aug 18, 2021 · N946SW · Cndair CL6002B19 · Doors
  > *CORROSION ON PAX DOOR FORMER 327.00 BETWEEN DD4 €“ DD5 (C-CHECK RO 10/8/2021) REMOVED AND REPLACED WITH NEW PAX DOOR FORMER AT 327.00 BETWEEN DD4 €“ DD5 REF DWG 601R31702 REV.-N, CRJ 200 SRM 51-42-06 AND CRJ 200 SRM 51-42-21. COMPLIED WITH 51-900-100
- [SDR SWIA202161713](https://openairdocs.org/sdr/SWIA202161713.md): None · corroded · Aug 17, 2021 · N946SW · Cndair CL6002B19 · Fuselage, Door Hinge
  > MAIN AVIONICS COMPARTMENT - DOOR CUTOUT INTERIOR STRUCTURE HAS SUSPECTED CORROSION ON FORWARD MIDDLE SECTION OF STGR 27 AT FS409.0. (C-CHECK RO 10/8/2021) REMOVED CORROSION ON DOOR CUTOUT INTERIOR STRUCTURE ON FORWARD MIDDLE SECTION OF STGR 27 AT FS409.
- [SDR SWIA202161712](https://openairdocs.org/sdr/SWIA202161712.md): None · corroded · Aug 17, 2021 · N946SW · Cndair CL6002B19 · Fuselage Main, Frame
  > MAIN AVIONICS COMPARTMENT - DOOR CUTOUT INTERIOR STRUCTURE HAS SUSPECTED CORROSION ON FORWARD LEFT SIDE OF LOWER FS349.0. LOCATION MARKED AND FLAGGED. (C-CHECK RO 10/8/2021) REMOVED CORROSION FROM FS349 FRAME REF. CRJ200 SRM 51-21-06. EVALUATED AND FOUN
- [SDR SWIA202161711](https://openairdocs.org/sdr/SWIA202161711.md): None · cracked · Aug 16, 2021 · N946SW · Cndair CL6002B19 · Fuselage Main, Longeron/Stringer
  > * IN THE AFT EQUIPMENT BAY, THE INTERCOSTAL BETWEEN FS 621 AND FS 625, INBOARD OF STRINGER 14R, IS CRACKED. (C-CHECK RO 10/8/2021) REMOVED AND INSTALLED 1EA. NEW INTERCOSTAL BETWEEN FS621-FS625 INBOARD OF 14R IAW DWG 601-35012 REV D AND SRM 51-42-21-00
- [SDR SWIA202161710](https://openairdocs.org/sdr/SWIA202161710.md): None · cracked · Aug 16, 2021 · N946SW · Cndair CL6002B19 · Fuselage Main, Longeron/Stringer
  > * IN THE AFT EQUIPMENT BAY, THE INTERCOSTAL BETWEEN FS 621 AND FS 625, INBOARD OF STRINGER 14L, IS CRACKED. (C-CHECK RO 10/8/2021) REMOVED AND INSTALLED 1EA. NEW INTERCOSTAL BETWEEN FS621-FS625 INBOARD OF STRINGER 14L IAW DWG 601-35012 REV D. & CRJ200 S
- [SDR SWIA202161709](https://openairdocs.org/sdr/SWIA202161709.md): None · gouged · Aug 16, 2021 · N946SW · Cndair CL6002B19 · Wing, Landing Gear Attach Fittings
  > * R/H INBOARD FLAP, INBOARD AFT FLAP BOX ATTACH FITTING, 2 EA. CENTER AFT ATTACH LUGS ARE GOUGED ON THEIR AFT SIDES, MARKED. (C-CHECK RO 10/8/2021) REMOVED CHAFE FROM R/H INBOARD FLAP, INBOARD AFT FLAP BOX ATTACH FITTING, 2 EA. CENTER AFT ATTACH LUGS.

Next page: https://openairdocs.org/aircraft/N946SW/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 = 'N946SW' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N946SW/reports

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