N438SW

Service difficulty reports · 145

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 = 'N438SW' 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 SWIA202264770None · crackedPAX DOOR ANGLE, NEAR DOOR HINGE HAS A CRACK. MARKED. (FILED CLOSED) REPLACED PAX DOOR UPPER ANGLE NEAR DOOR HINGE IN REFERENCE TO CRJ 200 SRM 51-42-06Mar 1, 2022 · N438SW · Cndair CL6002B19 · Fuselage, Equipment Attach FittingsSDR SWIA202157732Skin · dentedRH INBOARD FLAP LOWER SKIN HAS DENT APPROX. 6" INBOARD OF INBOARD EDGE AND 2" FWD OF TRAILING EDGE. (FILED CLOSED)COMPLIED WITH PERMANENT REPAIR OF THE RH INBOARD FLAP LOWER SKIN 6" INBOARD OF THE INBOARD EDGE AND 2" FWD OF THE TRAILING EDGE IN REFERENCE TApr 18, 2021 · N438SW · Cndair CL6002B19 · Trailing Edge FlapsSDR SWIA202157729Intercostal · crackedFRAME 621.00 INTERCOSTAL CONNECTING TO Z-MEMBER AT STR 14R CRACKED. (CRJ-200 SRM 53-61-17 ITEM #50) (FILED CLOSED) REMOVED AND REPLACED FRAME 621.00 INTERCOSTAL CONNECTING TO Z-MEMBER AT STR 14R IN REF TO SRM 51-42-06. COMPLIED WITH TASK CARD 51-900-1Apr 18, 2021 · N438SW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA202157728Skin · dentedRH INBOARD FLAP HAS DENT ON LOWER SKIN APPROX. 12" FROM TRAILING EDGE AND 27" FROM INBOARD EDGE. (FILED CLOSED) COMPLIED WITH THE PERMANENT REPAIR OF THE RH INBOARD FLAP LOWER SKIN APPROX 12" FROM THE TRAILING EDGE AND 27" FROM THE INBOARD EDGE IN REApr 18, 2021 · N438SW · Cndair CL6002B19 · Trailing Edge FlapsSDR SWIA202157733Bracket · crackedCARGO COMPARTMENT NET PAN FITTING BRACKET AT FS605.00 AND LBL 38.40 IS CRACKED. (FILED CLOSED) REMOVED AND REPLACED CARGO COMPARTMENT NET PAN FITTING BRACKET AT FS605.00 AND LBL 38.40 IN REF TO SRM 51-42-06. COMPLIED WITH TASK CARD 51-900-1003-SKY. COMApr 16, 2021 · N438SW · Cndair CL6002B19 · Fuselage Main, Attach FittingsSDR SWIA202157731Floor Support · corrodedCARGO COMPARTMENT FLOOR LANDING PLATE HAS SEVERAL AREAS OF CORROSION ALONG TOP SURFACE. (FILED CLOSED) REMOVED AND REPLACED CARGO COMPARTMENT FLOOR LANDING PLATE IN REF TO SRM 51-42-06 AND 51-42-21. COMPLIED WITH TASK CARD 51-900-1003-SKY. COMPLETED M-Apr 16, 2021 · N438SW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA202157730Fairing · chafedCHAFE DAMAGE BETWEEN L/H PYLON TRAILING EDGE FAIRING AND FUSELAGE AT FS 736.00. (FILED CLOSED) REPAIRED CHAFE DAMAGE TO LH FUSELAGE SKIN BETWEEN FS700.00 - FS755.00 AND STR9R - STR12R PER REO 601R-53-61-268, REV A, DATED 2000-07-11. COMPLIED WITH TASK Apr 16, 2021 · N438SW · Cndair CL6002B19 · Nacelle/Pylon, Main FrameSDR SWIA202005150728Door · openEXTREMELY LOUD NOISE AFTER TAKEOFF WITH STALL FAIL CAUTION MESSAGE FLIGHT 4291 - FILED OPEN PLEASE REFERENCE AML 430131. FOUND THE OXY DOOR OPEN WHEN THE AIRCRAFT TAXIED BACK TO THE GATE. DUE TO THE DISRUPTION OF THE AIR FLOW FROM THE OXY DOOR. PERFORMED SMay 14, 2020 · N438SW · Cndair CL6002B19 · Service DoorsSDR SWIA2019092746360Angle · damagedREPAIR LH BULKHEAD ANGLE @ F 202 BETWEEN LBL 13.73 -LBL 22.00 9C-CHECK) RO: 06/26/2019 PERFORMED REPAIR TO LH BULKHEAD ANGLE @ F 202 BETWEEN LBL 13.73 -LBL 22.00 IAW REO. LEAK CHECK GOOD,Sep 10, 2019 · N438SW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA2019092746359Structure · damagedPILOTS FLOOR AND NOSE COMPARTMENT FLOOR DAMAGED BETWEEN FS.169.00 - FS.220.00 LHS (C-CHECK) RO: 09/26/2019 PERFORMED REPAIR OF PILOTS FLOOR AND NOSE COMPARTMENT FLOOR BETWEEN FS.169.00 - FS.220.00 LHS IAW SRM.Aug 10, 2019 · N438SW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA2019092746358Skin Panel · damagedDAMAGED SKIN PANEL P/N 601R-33010-107 BETWEEN FS.193.00 - FS.210.00 LHS (C-CHECK) RO: 09/26/2019 REPLACED SKIN PN 601R-33010-107 BETWEEN FS193.00-FS210 LHS IAW SRM. LEAK CHECK GOOD.Aug 10, 2019 · N438SW · Cndair CL6002B19 · Fuselage Main, Plate/SkinSDR SWIA2019092746370Frame · corrodedFS 605.0 FRAME FWD SIDE FROM 22L TO 25R HAS CORROSION (C-CHECK) RO: 09/26/2019 REMOVED CORROSION ON FS 605.0 FRAME FWD SIDE FROM 22L TO 25R, INSTALLED NEW FRAME AT FS605 FROM STGR20L-STGR20R IAW SRM. LEAK CHECK GOOD.May 30, 2019 · N438SW · Cndair CL6002B19 · Fuselage Main, FrameSDR SWIA2019092746357Panel · corrodedRIGHT HAND PRESSURE FLOOR SILL PANEL FROM APPROXIMATELY FS429.0 TO FS559.0 HAS SEVERAL SPOTS OF CORROSION. (C-CHECK) RO: 09/26/2019 REMOVED CORROSION FROM THE RIGHT HAND FLOOR SILL PANEL FROM APROX FS429.0 TO FS559.0 IAW REO. LEAK CHECK GOOD.May 30, 2019 · N438SW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA201946356Panel · corrodedLEFT HAND PRESSURE FLOOR SILL PANEL FROM APPROXIMATELY FS 409.0+133 TO FS559.0 HAS SEVERAL SPOTS OF CORROSION. (C-CHECK) RO: 09/26/2019 BLENDED OUT CORROSION ON LEFT HAND PRESSURE FLOOR SILL PANEL FROM APPROXIMATELY FS 409.0+133 TO FS559.0 IAW REO. LEAK CHECK May 30, 2019 · N438SW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA2019092746369Vane · gougedLEFT INBOARD FLAP. CENTER OUTBOARD VANE CAP GOUGED. (C-CHECK) RO: 09/26/2019 REMOVED AND REPLACED THE LH INBD FLAP CENTER OTBD VANE CAP WITH NEW PART IAW SRM.May 29, 2019 · N438SW · Cndair CL6002B19 · Trailing Edge FlapsSDR SWIA2019092746368Channel · corrodedR/H MLG WHEEL WELL WS 53.60 BATT CHANNEL HAS CORROSION AROUND CANNON PLUGS (C-CHECK) RO: 09/26/2019 REMOVED AND REPLACED R/H BATT RIB ANGLE WS 53.60 WITH NEW PART IAW SRM.May 28, 2019 · N438SW · Cndair CL6002B19 · Wing Miscellaneous StructureSDR SWIA2019092746355Channel · corrodedL/H MLG WHEEL WELL WS 53.60 BATT CHANNEL HAS CORROSION AROUND CANNON PLUGS (C-CHECK) RO: 09/26/2019 REPLACED CORRODED ANGLE WITH NEW ANGLE P/N 601R10203 -33 IAW SRM.May 28, 2019 · N438SW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA2019092746354Channel · crackedL/H MLG WHEEL WELL WS 53.60 BATT CHANNEL CRACKED (C-CHECK) RO: 09/26/2019 REMOVED AND REPLACED L/H MLG WHEEL WELL WS 53.60 BATT CHANNEL IAW SRM. LEAK CHECK GOOD.May 28, 2019 · N438SW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA2019092746367Access Panel · chafedTHE LH WING UPPER SKIN ACCESS PANEL 540AT'S NUTPLATE RING/CHANNEL IS CHAFED AT MULTIPLE AREAS OF ITS UPPER SURFACE. (C-CHECK) RO: 09/26/2019 BLENDED OUT CHAFEF MARKS ON LH WING UPPER SKIN ACCESS PANEL 540AT RING/CHANNEL IAW REO.May 24, 2019 · N438SW · Cndair CL6002B19 · Wing, Plate/SkinSDR SWIA2019092746366Skin · chafedTHE RH INBOARD FLAP VANE'S SKIN HAS 3 CHAFES ALONG THE LEADING EDGE, AND 3 CHAFES ALONG THE TRAILING EDGE UPPER SURFACE. (C-CHECK) RO: 09/26/2019 BLENDED THE RH INBD FLAP VANE LEADING EDGE SKIN AT 3 LOCATIONS IAW REO, AND THE TRAILING EDGE AT 2 LOCATIONS IAW SMay 24, 2019 · N438SW · Cndair CL6002B19 · Trailing Edge FlapsSDR SWIA2019092746365Skin · chafedTHE LH INBOARD FLAP VANE'S SKIN HAS 3 CHAFES ALONG THE LEADING EDGE, AND 2 CHAFES ALONG THE TRAILING EDGE UPPER SURFACE. (C-CHECK) RO: 09/26/2019 BLENDED THE LH INBD FLAP VANE LEADING EDGE SKIN AT 3 LOCATIONS IAW REO, AND THE TRAILING EDGE AT 2 LOCATIONS IAW SMay 24, 2019 · N438SW · Cndair CL6002B19 · Trailing Edge FlapsSDR SWIA2019092746353Angle · crackedLEFT HAND BATT RIB ANGLE CRACKED. (C-CHECK) RO: 09/26/2019 REMOVED AND REPLACED LH BATT RIB ANGLE IAW SRM.May 24, 2019 · N438SW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA2019092746364Skin · chafedL/H AILERON UPPER LEADING EDGE SKIN IS CHAFFED ALL THE WAY ACROSS (C-CHECK) RO: 09/26/2019 BLENDED L/H AILERON UPPER LEADING EDGE SKIN. REPLACED WITH NEW PART, PART NUMBER 601R13031-165 IAW REO AND SRM.May 23, 2019 · N438SW · Cndair CL6002B19 · AileronsSDR SWIA2019092746363Plate · corrodedSERVICE DOOR PROTECTOR PLATE IS CORRODED AROUND THE FASTENER HOLES (C-CHECK) RO: 09/26/2019 REPLACED SERVICE DOOR PROTECTOR PLATE WITH NEW PART FROM STORES P/N: 601R38957-31 P/O: T-48438 IAW SRM.May 23, 2019 · N438SW · Cndair CL6002B19 · Service DoorsSDR SWIA2017120543932Duct · failedCABIN ALTITUDE CAUTION. RIGHT PACK OVER PRESSURE. EMERGENCY DECLARED. EMERGENCY DESCENT. O2 MASKS DEPLOYED. (FLT 4883) REMOVED AND REPLACED RT AC UPPER SUPPLY DUCT ASSY IAW AMM. OPS CHECK GOOD.Oct 29, 2017 · N438SW · Cndair CL6002B19 · Air Distribution SystemSDR SWIA201743319Fitting · corrodedBS 349 FLOORBEAM FITTING HAS CORROSION AT RBL 42. INSTALLED A NEW FITTING IAW REO.Apr 29, 2017 · N438SW · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR SWIA201743318Floorbeam · corrodedBS 589 FLOORBEAM HAS CORROSION BETWEEN LBL 27 - RBL 36. REPLACED THE THREE CAP STRAPS IAW SRM.Apr 26, 2017 · N438SW · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR SWIA201743317Fairing · chafedLEFT FLAP STUB FAIRING CHAFED. REMOVED THE STUB FAIRING AND REPLACED WITH NEW, IAW AMM.Apr 25, 2017 · N438SW · Cndair CL6002B19 · Trailing Edge FlapsSDR SWIA201743316Seal · tornLEFT INBD FLAP INBD SEAL TORN. REPLACED IAW SRM.Apr 24, 2017 · N438SW · Cndair CL6002B19 · Trailing Edge FlapsSDR SWIA201743315Panel · chafedLEFT AILERON LOWER SKIN LEADING EDGE SHROUDS HAVE CHAFE DAMAGE. REMOVED AND REPLACEED THE FIXED PANELS IAW SRM.Apr 24, 2017 · N438SW · Cndair CL6002B19 · AileronsSDR SWIA201743314Panel · chafedPANEL 699CB CHAFED. INSTALLED A REPLACEMENT PANEL IAW REO AND SRM.Apr 24, 2017 · N438SW · Cndair CL6002B19 · Wing Main, Frame StructureSDR SWIA201743313Intercostal · corrodedPAX DOOR INTERCOSTAL AT DD4 BETWEEN BS 320 AND 338 CORRODED. REMOVED AND REPLACED THE INTERCOSTAL IAW SRM.Apr 24, 2017 · N438SW · Cndair CL6002B19 · Passenger/Crew DoorsSDR SWIA201743312Plate · corrodedSERVICE DOOR FLOOR PLATE IS CORRODED. REPLACED THE PLATE IAW SRM.Apr 23, 2017 · N438SW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA201541204Floor Skin · crackedPRESSURE FLOOR SKIN AT FS 456 BETWEEN BL0 AND LBL9 CRACKED. INSTALLED REPAIR PARTS 601R-53-41-1898-5, 601R-53-41-1898-6, 601R-53-41-1898-7, 601R-53-41-1898-8 JUST FWD OF FS460 AT FS456 IAW REO.May 5, 2015 · N438SW · Cndair CL6002B19 · Fuselage Floor PanelSDR SWIA201541191Floor Panel · damagedDOUBLER COMMON TO PRESSURE FLOOR WEB BETWEEN RBL 27.5 AND RBL 36 AT BS 47. INSTALLED 601R-53-41-1905-1, 601R-53-41-1905-2, 601R-53-41-1905-3, 601R-53-41-19054-4 DOUBLERS AND SHIM COMMON TO PRESSURE FLOOR WEB BETWEEN RBL27.5 AND RBL36.0 AT FS 478.00, IAW REO.May 5, 2015 · N438SW · Cndair CL6002B19 · Fuselage Floor PanelSDR SWIA201541198Frame · damagedLOWER FRAME SECTOR AT BS 333 BETWEEN S23L - 23R DAMAGED. INSTALLED NEW LOWER FRAME SECTOR ASSY IAW SRM.May 3, 2015 · N438SW · Cndair CL6002B19 · Fuselage Main, FrameSDR SWIA201541193Floorbeam · corrodedCORROSION ON TOP SURFACE OF FS 280 BEAM FROM RBL 9 TO LBL 9. R & R SPLICED SECTION, PN 600-34017-595 OF FS280 BEAM FROM RBL 9 TO LBL 9 IAW SRM.May 1, 2015 · N438SW · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR SWIA201541207Stiffener · crackedVERTICAL POST AT FS 409+128, RBL 27 INBD SIDE IS CRACKED IN LOWER RADUIS. REMOVED AND INSTALLED NEW INBD VERT POST AT FS 409.+128 RBL 27 IAW SRM AND STS EA.Apr 30, 2015 · N438SW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA201541206Stiffener · crackedVERTICAL POST AT FS 409+128, LBL 27 OTBD SIDE IS CRACKED IN LOWER RADIUS. REMOVED AND INSTALLED NEW VERTICAL POST AT FS 409+128, LBL 27 OTBD IAW STS EA.Apr 30, 2015 · N438SW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA201541205Stiffener · crackedVERTICAL POST AT 409+128, LBL 27 INBD SIDE IS CRACKED IN LOWER RADIUS. REMOVED AND INSTALLED NEW INBD VERTICAL POST AT FS 409 +128 LBL 27 IAW SRM.Apr 30, 2015 · N438SW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA201541190Skin · gougedFUSELAGE SKIN GOUGED AND DENTED AT BS 684 BETWEEN STR 8 - 9R. REPAIRED DAMAGED SKIN , CUT-OUT AND COLD WORKED DAMAGED FUSELAGE, NDT REPAIR AREA NO DEFECTS NOTED, INSTALLED REPAIR DOUBLER, RESTORED FINISH IAW STS EA.Apr 29, 2015 · N438SW · Cndair CL6002B19 · Fuselage Main, Plate/SkinSDR SWIA201541192Angle · corrodedAFT SPLICE ANGLE AT BS 364 BETWEEN S25L - 25R IS CORRODED. C-CHECK, REPLACED AFT SPLICE ANGLE AT FS 364, STR 25L TO STR 25R IAW REO.Apr 28, 2015 · N438SW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA201541203Floor Support · crackedCRACK IN AFT CARGO DOOR FLOOR SILL PLATE. R & R CARGO FLOOR SILL IAW SRM.Apr 27, 2015 · N438SW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA201541200Floor Skin · crackedPRESSURE FLOOR SKIN CRACKED AT BS 456 BETWEEN BL 0 AND RBL 9. INSTALLED REPAIR IAW REO.Apr 27, 2015 · N438SW · Cndair CL6002B19 · Fuselage Floor PanelSDR SWIA201541201Door Frame · crackedRIGHT FORWARD AVIONICS BAY LANDING CRACKED AT FS 193 FRAME. REPAIRED RT FORWARD AVIONICS BAY LANDING CRACK AT FS 193, FRAME IAW REO.Apr 26, 2015 · N438SW · Cndair CL6002B19 · Fuselage Main, StructureSDR SWIA201541208Vane · chafedRT INBD FLAP VANE CHAFED L/E MIDDLE. INSTALLED NEW RT INBD FLAP VANE MIDDLE L/E IAW SRM.Apr 25, 2015 · N438SW · Cndair CL6002B19 · Trailing Edge FlapsSDR SWIA201541202Vane · chafedRIGHT INBD FLAP VANE CHAFED L/E OTBD. R & R RT INBD FLAP VANE OTBD L/E PANEL 601R14303-44 IAW SRM.Apr 25, 2015 · N438SW · Cndair CL6002B19 · Trailing Edge FlapsSDR SWIA201541199Support Bracket · crackedPASSENGER DOOR HAS HANDLE MOUNTING ASSEMBLY SUPPORT BRACKET CRACK. REMOVED AND INSTALLED NEW SUPPORT BRACKET FOR PASSENGER DOOR MOUNTING HANDLE IAW SRM AND REO.Apr 25, 2015 · N438SW · Cndair CL6002B19 · Passenger/Crew DoorsSDR SWIA201541197Vane · chafedLEFT INBD FLAP VANE CHAFED L/E OTBD. INSTALLED NEW LT INBD FLAP VANE OTBD L/E PANEL IAW SRM.Apr 25, 2015 · N438SW · Cndair CL6002B19 · Trailing Edge FlapsSDR SWIA201541196Vane · chafedLEFT INBD FLAP VANE CHAFED L/E MIDDLE. REPLACED LT INBD FLAP VANE L/E MIDDLE SECTION IAW REO.Apr 25, 2015 · N438SW · Cndair CL6002B19 · Trailing Edge Flaps
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