N946SW

Service difficulty reports · 218

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

Query with SQL
duckdb -csv -c "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"

Prints the whole list as CSV. It reads the release’s Parquet files over HTTPS, so there’s nothing to download first. Install DuckDB to run it.

SDR SWIA2025041600015Warning Message · illuminatedNOSE DOOR OPEN MASTER WARNING AFTER SELECTING GEAR UP AFTER TAKEOFF. (FLIGHT 5045) SEE EAML 1583020 FOR CORRECTIVE ACTION.Apr 15, 2025 · N946SW · Cndair CL6002B19 · Landing Gear Position and WarningSDR SWIA20250326003Skin · dentedFUSELAGE 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 Mar 23, 2025 · N946SW · Cndair CL6002B19 · Fuselage Main, Plate/SkinSDR SWIA202503260018Rivet · looseMULTIPLE 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 - WSMar 18, 2025 · N946SW · Cndair CL6002B19 · Trailing Edge FlapsSDR SWIA202503180015Tripler · gougedREAR 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 WMar 15, 2025 · N946SW · Cndair CL6002B19 · Fuselage Main, BulkheadSDR SWIA20250317015Pressure Blkhd · gougedREAR 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 PROGRESSMar 15, 2025 · N946SW · Cndair CL6002B19 · Fuselage Main, BulkheadSDR SWIA202503260006Skin · dentedRH 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 SURMar 6, 2025 · N946SW · Cndair CL6002B19 · Wing, Plate/SkinSDR SWIA202503260222Landing · crackedUPON 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 PFeb 22, 2025 · N946SW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA202503260213Support · damagedCARGO 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 60Feb 13, 2025 · N946SW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA202503260204Skin · dentedRUDDER 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 COFeb 4, 2025 · N946SW · Cndair CL6002B19 · Rudder, Plate/SkinSDR SWIA202503260130Floor Support · corrodedFOUND 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 ANDJan 30, 2025 · N946SW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWI2025F00402Floor Support · corrodedFOUND 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 WITHJan 30, 2025 · N946SW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA202503260122Intercostal · crackedINTERCOSTAL 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 JJan 22, 2025 · N946SW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA202502030022Intercostal · crackedINTERCOSTAL 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 PROGRESSJan 22, 2025 · N946SW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA202503260121Landing · corrodedLH 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 54Jan 21, 2025 · N946SW · Cndair CL6002B19 · Wing Main, Frame StructureSDR SWIA2025012200021Access Panel · corrodedLH 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.Jan 21, 2025 · N946SW · Cndair CL6002B19 · Wing, Plate/SkinSDR SWIA202503260117Access Panel · corrodedRH 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 OJan 17, 2025 · N946SW · Cndair CL6002B19 · Wing, Plate/SkinSDR SWIA2025012000017Access Panel · corrodedRH 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 PROGRESSJan 17, 2025 · N946SW · Cndair CL6002B19 · Wing, Plate/SkinSDR SWIA202503290114Latch · faultedCOCKPIT 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 FJan 14, 2025 · N946SW · Cndair CL6002B19 · Emergency ExitsSDR SWIA2021120662958Flap System · failedON 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) Dec 5, 2021 · N946SW · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR SWIA2021112262669Light · arcedCOCKPIT 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 PANov 20, 2021 · N946SW · Cndair CL6002B19 · Emergency LightingSDR SWIA202161735None · damagedPERFORM 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 Sep 8, 2021 · N946SW · Cndair CL6002B19 · Fuselage Internal Mounting StructureSDR SWIA202161734None · crackedFOUND 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 ATSep 8, 2021 · N946SW · Cndair CL6002B19 · Wing StructureSDR SWIA202161733None · damagedPERFORM 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-SKYSep 7, 2021 · N946SW · Cndair CL6002B19 · Fuselage Internal Mounting StructureSDR SWIA202161732None · noneWHILE 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. COMSep 1, 2021 · N946SW · Cndair CL6002B19 · Engine Cowl FlapsSDR SWIA202161731None · nicked*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 Aug 26, 2021 · N946SW · Cndair CL6002B19 · Wing, Landing Gear Attach FittingsSDR SWIA202161730None · gouged*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 . COMPAug 26, 2021 · N946SW · Cndair CL6002B19 · Wing, Landing Gear Attach FittingsSDR SWIA202161729None · damagedFLOOR 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, RAug 25, 2021 · N946SW · Cndair CL6002B19 · Fuselage Internal Mounting StructureSDR SWIA202161728None · chafed* 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 ( FUSEAug 22, 2021 · N946SW · Cndair CL6002B19 · Fuselage, Equipment Attach FittingsSDR SWIA202161727None · crackedCRACK 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 600-34017Aug 21, 2021 · N946SW · Cndair CL6002B19 · Fuselage Main, KeelSDR SWIA202161726None · crackedCARGO 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 51Aug 21, 2021 · N946SW · Cndair CL6002B19 · DoorsSDR SWIA202161725None · tornLH 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 DETAILSAug 20, 2021 · N946SW · Cndair CL6002B19 · Elevator, Tab StructureSDR SWIA202161724None · chafedRH 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 CONAug 20, 2021 · N946SW · Cndair CL6002B19 · Elevator Tab, Attach FittingsSDR SWIA202161723None · chafedRH 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 ATTAug 20, 2021 · N946SW · Cndair CL6002B19 · Elevator Tab, Attach FittingsSDR SWIA202161722None · gougedLH 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 THIAug 20, 2021 · N946SW · Cndair CL6002B19 · Wing StructureSDR SWIA202161721None · corroded* 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 CONDITIAug 20, 2021 · N946SW · Cndair CL6002B19 · Fuselage Structure (General)SDR SWIA202161720None · cracked* 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 WIAug 20, 2021 · N946SW · Cndair CL6002B19 · Fuselage Main, FrameSDR SWIA202161719None · chafed* 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 2011-01-1Aug 20, 2021 · N946SW · Cndair CL6002B19 · Fuselage Main, BulkheadSDR SWIA202161718None · bent* 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.Aug 20, 2021 · N946SW · Cndair CL6002B19 · Fuselage Structure (General)SDR SWIA202161749None · corroded*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 Aug 19, 2021 · N946SW · Cndair CL6002B19 · DoorsSDR SWIA202161717None · corrodedFRAME 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.Aug 19, 2021 · N946SW · Cndair CL6002B19 · Fuselage Main, FrameSDR SWIA202161716None · damagedFLOOR 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 51Aug 19, 2021 · N946SW · Cndair CL6002B19 · Fuselage Internal Mounting StructureSDR SWIA202161715None · corroded*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 FOUNDAug 19, 2021 · N946SW · Cndair CL6002B19 · Galley DoorsSDR SWIA202161748None · corroded*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 51-41-02Aug 18, 2021 · N946SW · Cndair CL6002B19 · DoorsSDR SWIA202161747None · corroded*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 LIMIAug 18, 2021 · N946SW · Cndair CL6002B19 · DoorsSDR SWIA202161714None · corroded*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 51-900-100Aug 18, 2021 · N946SW · Cndair CL6002B19 · DoorsSDR SWIA202161713None · corrodedMAIN 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.Aug 17, 2021 · N946SW · Cndair CL6002B19 · Fuselage, Door HingeSDR SWIA202161712None · corrodedMAIN 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 FOUNAug 17, 2021 · N946SW · Cndair CL6002B19 · Fuselage Main, FrameSDR SWIA202161711None · cracked* 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 51-42-21-00Aug 16, 2021 · N946SW · Cndair CL6002B19 · Fuselage Main, Longeron/StringerSDR SWIA202161710None · cracked* 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 SAug 16, 2021 · N946SW · Cndair CL6002B19 · Fuselage Main, Longeron/StringerSDR SWIA202161709None · gouged* 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. Aug 16, 2021 · N946SW · Cndair CL6002B19 · Wing, Landing Gear Attach Fittings
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