N461SW

Service difficulty reports · 235

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 = 'N461SW' 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 SWIA2020031649296Floorbeam · gouged* FLOOR BEAM CAP FROM FS559+96 THROUGH FS559+112, LBL12, IS GOUGED, MARKED IN RED. (C-CHECK) RO 3/13/2020 REMOVED AND REPLACED FLOOR BEAM CAP (PLATE) BETWEEN FS 559+96 TO FS 559+112 AT LBL 12 REF CRJ-200 SRM, BOMBARDIER DWG. RESTORED FINISH AND APPLIED CIFeb 4, 2020 · N461SW · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR SWIA2020031649295Floorbeam · corroded* FLOOR BEAM AT LBL9, OUTBOARD FLANGE HAS CORROSION BETWEEN FS589 AND FS605, MARKED IN RED (C-CHECK) RO 3/13/2020 REMOVED AND REPACED WITH NEW BEAM CAP AT LBL 9.0 FS589 AND FS605 REF CRJ 200 AND BOMBARDIER REO. COMPLIED WITH TASK CARD.Feb 4, 2020 · N461SW · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR SWIA2020031649294Frame · corroded* AFT SIDE OF FRAME AT FS394, STR27 IS CORRODED, MARKED IN RED. (C-CHECK) RO 3/13/2020 REMOVED AND INSTALLED NEW SERVICEABLE LOWER FRAME SECTOR AT FS394.00 BETWEEN STGR 23L AND STGR 23R REF BOMBARDIER DRAWING, CRJ200 SRM 51-42-06. PRESSURE LEAK CHECKS GOOFeb 4, 2020 · N461SW · Cndair CL6002B19 · Fuselage Main, FrameSDR SWIA2020031649293Floor Panel · corroded* THE RH PRESSURE FLOOR PANEL FROM FS439.00 TO FS559.00 HAS MULTIPLE LOCATIONS OF CORROSION. (MARKED) (C-CHECK) RO 3/13/2020 REMOVED CORROSION ON THE R/H FLOOR PANEL FROM FS439.00 TO FS559.00 AT 11 LOCATIONS. REF: BOMBARDIER REO. PRESSURIZATION LEAK CHECFeb 4, 2020 · N461SW · Cndair CL6002B19 · Fuselage Floor PanelSDR SWIA2020031649292Angle · corroded* THE RH PRESSURE FLOOR SILL ANGLE HAS MULTIPLE LOCATIONS OF CORROSION FROM FS424.00 TO FS513.00. (MARKED) (C-CHECK) RO 3/13/2020 REMOVED CORROSION ON THE R/H FLOOR SILL ANGLE FROM FS424.00 TO FS513.00 AT 16 LOCATIONS. REF: BOMBARDIER REO. PRESSURIZATIONFeb 4, 2020 · N461SW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA2020031649291Panel · corroded* THE LH PRESSURE FLOOR PANEL FROM FS461.00 TO FS559.00 HAS MULTIPLE LOCATIONS OF CORROSION. (MARKED) (C-CHECK) RO 3/13/2020 REMOVED CORROSION ON THE L/H FLOOR SILL PANEL FROM FS461.00 TO FS559.0 AT 10 LOCATIONS. REF: BOMBARDIER REO. BLENDED MATERIAL REMFeb 4, 2020 · N461SW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA2020031649326Attach Fitting · corroded* THE FLOOR BEAM ATTACHMENT TO THE REAR PRESSURE BULKHEAD AT LBL9.00 HAS CORROSION. (MARKED) (C-CHECK) RO 3/13/2020 PERFORMED BLEND REPAIR ON THE FLOOR BEAM ATTACHMENT TO THE REAR PRESSURE BULKHEAD AT LBL9.00 REF APPLICABLE STEPS OF BOMBARDIER REO. SEE CFeb 3, 2020 · N461SW · Cndair CL6002B19 · Fuselage Main, Attach FittingsSDR SWIA2020031649290Support Angle · crackedFS280.00 FLOOR BEAM, FWD FLOOR SUPPORT ANGLE CRACKED AT RBL 9. (C-CHECK) RO 3/13/2020 REMOVED AND INSTALLED NEW F.S 280 FWD FLOOR SUPPORT ANGLE AND REPAIRED F.S 280 FLOORBEAM BETWEEN LBL 20.75 TO RBL 20.75 REF. BOMBARDIER REO. COMPLIED WITH TASK CARD.Feb 3, 2020 · N461SW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA2020031649289Frame · crackedAT FS605.0 FRAME HAS SUSPECT CRACK AT RIVET HOLE LOCATION ABOVE STR 9L AND BELOW STR 9L. (C-CHECK) RO 3/13/2020 PERFORMED F.S 605 FRAME AT STR 9L CRACK REPAIR REF BOMBARDIER REO. REFERENCE THE CONTINUE CARD FOR DETAILS. PRESSURE CHECKS GOOD.Feb 3, 2020 · N461SW · Cndair CL6002B19 · Fuselage Main, FrameSDR SWIA2020031649288Attach Fitting · corroded* THE FLOOR BEAM ATTACHMENT TO THE REAR PRESSURE BULKHEAD AT RBL 27.00 HAS CORROSION. (MARKED) (C-CHECK) RO 3/13/2020 PERFORMED REPAIR OF RBL 27 FLOOR BEAM ATTACHMENT FITTING BETWEEN FS610.00 AND FS621.00 PER BOMBARDIER REO. COMPLIED WITH ALL STEPS. COMPLFeb 3, 2020 · N461SW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA2020031649287Attach Fitting · corroded* THE FLOOR BEAM ATTACHMENT TO THE REAR PRESSURE BULKHEAD AT LBL 27.00 HAS CORROSION. (MARKED) (C-CHECK) RO 3/13/2020 PERFORMED REPAIR OF LBL 27 FLOOR BEAM ATTACHMENT FITTING BETWEEN FS610.00 AND FS621.00 PER BOMBARDIER REO. COMPLIED WITH ALL STEPS. COMPFeb 3, 2020 · N461SW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA2020031649286Frame · corroded* THE FRAME AT FS605.00 HAS MULTIPLE LOCATIONS OF CORROSION FROM STRINGER 21L TO 23R. (MARKED) (C-CHECK) RO 3/13/2020 REPLACED FS605.00 FRAME FROM STRINGER 21L TO 23R. REF BOMBARDIER DWG, BOMBARDIER REO, CRJ200 SRM. LEAK CHECK GOOD AT THIS TIME. COMPLIED Feb 3, 2020 · N461SW · Cndair CL6002B19 · Fuselage Main, FrameSDR SWIA2020031649285Support Fitting · cracked*PASSENGER CABIN FLOOR SUPPORT STRUCTURE O/B OF LBL9 AT FS461.0 SUPPORT FITTING CRACKED. (C-CHECK) RO 3/13/2020 REMOVED AND WET INSTALLED A NEW CABIN FLOOR SUPPORT FITTING AT FS461.0 OUTBD OF LBL9.0 REF. CRJ200 SRM AND BOMBARDIER DRAWING. ALL CHECKS GOOD.Feb 3, 2020 · N461SW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA2020031649284Support Fitting · cracked*PASSENGER CABIN FLOOR SUPPORT STRUCTURE O/B OF RBL9 AT FS461.0 SUPPORT FITTING CRACKED. (C-CHECK) RO 3/13/2020 REMOVED AND WET INSTALLED THE NEW CABIN FLOOR SUPPORT FITTING AT FS461.0 OUTBD OF RBL9.0 REF. CRJ200 SRM AND BOMBARDIER DRAWING. ALL CHECKS GOODFeb 3, 2020 · N461SW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA2020031649283Fitting · cracked*PASSENGER CABIN FLOOR SUPPORT STRUCTURE O/B OF RBL27 AT FS484.0 CLIP CRACKED. (C-CHECK) RO 3/13/2020 REMOVED AND REPLACED CLIP P/N 601R31171-9 REF CRJ 200 SRM AND BOMBARDIER DWG.Feb 3, 2020 · N461SW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA2020031649282Floorbeam · corroded*PASSENGER CABIN FLOOR SUPPORT STRUCTURE I/B OF LBL9 BETWEEN FS409.00 AND 409+128 HAS AREAS OF CORROSION.(MARKED) (C-CHECK) RO 3/13/2020 PERFORMED CABIN FLOORBEAM CAP SPLICE REPAIR TO F.S 409 TO F.S 409+128 LBL 9 FLOORBEAM REF. CRJ-200 SRM. COMPLIED WITH TFeb 3, 2020 · N461SW · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR SWIA2020031649281Stringer Clip · cracked*PASSENGER CABIN L/H STGR3 AT FS280.0 CLIP CRACKED. (MARKED) (C-CHECK) RO 3/13/2020 REMOVED AND REPLACED CLIP FROM L/H STRGR. 3 COMMON TO FS 280.00 PER REF: CRJ200 SRM AND BOMBARDIER DWG. RESTORED FINISH AND CIC.Feb 3, 2020 · N461SW · Cndair CL6002B19 · Fuselage Main, Attach FittingsSDR SWIA2020031649280Stringer · cracked*PASSENGER CABIN L/H STGR3 AT FS379.0 CRACKED. (MARKED) (C-CHECK) RO 3/13/2020 REPLACED L/H STRINGER 3 BETWEEN FS376.00 TO FS 386.00. REF BOMBARDIER DWG, CRJ 200 SRM. COMPLIED WITH TASK CARD. LEAK CHECK GOOD.Feb 3, 2020 · N461SW · Cndair CL6002B19 · Fuselage Main, Longeron/StringerSDR SWIA2020031649279Door Sill · corroded*PASSENGER CABIN FLOOR SUPPORT R/H FLOOR SILL AT FS319.70 HAS CORROSION. (MARKED) (C-CHECK) RO 3/13/2020 REMOVED AND INSTALLED NEW PASSENGER CABIN FLOOR SUPPORT R/H FLOOR SILL AT FS319.70 REF CRJ-200 SRM AND BOMBARDIER DWG. COMPLIED WITH SKYWEST TASKCARD.Feb 3, 2020 · N461SW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA2020031649278Mount · corroded*PASSENGER CABIN FLOOR SUPPORT STRUCTURE I/B FORWARD AND AFT GALLEY MOUNTS HAVE CORROSION. (C-CHECK) RO 3/13/2020 REMOVED CORROSION & EVALUATED REWORKED AREAS. FWD INBD GALLEY MOUNT WITHIN LIMITS AFTER REWORK. AFT INBD GALLEY MOUNT REPLACED. FINISH RESTOREFeb 3, 2020 · N461SW · Cndair CL6002B19 · Fuselage, Equipment Attach FittingsSDR SWIA2020031649277Mount · corroded*PASSENGER CABIN FLOOR SUPPORT STRUCTURE O/B-I/B FORWARD AND AFT WARDROBE MOUNTS HAVE CORROSION. (C-CHECK) RO 3/13/2020 REMOVED AND REPLACED WITH NEW PASSENGER CABIN FLOOR SUPPORT STRUCTURE AFT I/B & AFT O/B WARDROBE MOUNTS . REF: CRJ-200 SRM AND BOMBARDIFeb 3, 2020 · N461SW · Cndair CL6002B19 · Fuselage, Equipment Attach FittingsSDR SWIA2020061851088Shim · migratedFORWARD STEADY FITTING MOUNTED TO THE TOP OF THE VERTICAL STAB HAS MIGRATED SHIMS ON THE LT SIDE OUTBD BOLTS. REPLACED WITH NEW LT SIDE OUTBOARD SHIM AND NUTS(2(EA) ON FORWARD STEADY FITTING REF RIL AND REF AMM. THIS SDR FOR T/STEADY FITTING IS BEING SUBMITTJan 30, 2020 · N461SW · Cndair CL6002B19 · Vertical Stabilizer Miscellaneous StructureSDR SWIA2020031649322Anchor Fitting · corroded* PAX DOOR ENTRY AFT ANCHOR FITTING HAS EVIDENCE OF CORROSION. (C-CHECK) RO 3/13/2020 REMOVED CORRODED SERRATED PLATE UNDER PAX DOOR AFT ANCHOR FITTING AND INSTALLED NEW SERRATED PLATE,REF CRJ-200 SRM.Jan 30, 2020 · N461SW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA2020031649321Anchor Fitting · corroded* PAX DOOR ENTRYWAY FWD ANCHOR FITTING HAS EVIDENCE OF CORROSION .(MARKED) (C-CHECK) RO 3/13/2020 REPLACED PAX DOOR ENTRYWAY FWD ANCHOR FITTING. REF CRJ200 AMM. OPS CHECKS GOOD AT THIS TIME.Jan 30, 2020 · N461SW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA2020031649275Angle · cracked*LH WING BATT RIB WS48.30 IN MLG WELL, UPPER WEB ANGLE CRACKED (MARKED) (C-CHECK) RO 3/13/2020 REMOVED AND REPLACED DAMAGED ANGLE (P/N 601R10204-33) AT LH WING BATT RIB WS48.30 IN MLG WELL REF DWG CRJ200 SRM. COMPLIED WITH TASK CARD.Jan 29, 2020 · N461SW · Cndair CL6002B19 · Wing Miscellaneous StructureSDR SWIA2020031649274Angle · cracked*LH WING BATT RIB WS48.30 IN MLG WELL, CAP CRACKED (MARKED) (C-CHECK) RO 3/13/2020 REMOVED AND REPLACED CAP ANGLE AT LH WING BATT RIB WS48.30 REF CRJ-200 SRM, BOMBARDIER DWG , COMPLIED WITH SKYWEST TASK CARDJan 29, 2020 · N461SW · Cndair CL6002B19 · Wing Miscellaneous StructureSDR SWIA2020031649273Angle · cracked* RIGHT WING BATT RIB WS53.6 ANGLE IS CRACKED IN THE RADIUS OF THE UPPER CORNER. (MARKED) (C-CHECK) RO 3/13/2020 REMOVED AND INSTALLED NEW RIGHT WING BATT RIB @ WS53.6. REF CRJ200 SRM AND BOMBARDIER DWG. COMPLIED WITH TASK CARD. ALL CHECKS GOOD.Jan 29, 2020 · N461SW · Cndair CL6002B19 · Wing Miscellaneous StructureSDR SWIA2020031649272Stiffener · cracked*RIGHT WING BATT RIB WS48.3 CAP IS CRACKED. (MARKED) (C-CHECK) RO 3/13/2020 REMOVED AND REPLACED CRACKED R/WING BATT RIB CAP ANGLE(STIFFENER) WITH NEW CAP ANGLE(STIFFENER P/N 600-10389-2) AT WS48.3 REF CRJ-200 SRM, BOMBARDIER DWG. RESTORED FINISH TO REWORKJan 29, 2020 · N461SW · Cndair CL6002B19 · Wing, Rib/BulkheadSDR SWIA2020031649325Skin · chafed* RIGHT INBOARD FLAP VANE LEADING EDGE SKIN IS CHAFFED IN 4 EA. PLACES. (C-CHECK) RO 3/13/2020 RECEIVED, LOCATED, AND DRILLED NEW INBD FLAP VANE OTBD LEADING EDGE CAP REF CRJ-200 SRM. INSTALLED NEW RIGHT INBOARD FLAP VANE LEADING EDGE REF CRJ-200 SRM.Jan 28, 2020 · N461SW · Cndair CL6002B19 · Trailing Edge FlapsSDR SWIA2020031649271Support Angle · corroded*CORROSION ON RIGHT FLOOR SILL BETWEEN FS310.00 & FS319.70. (MARKED) (C-CHECK) RO 3/13/2020 REMOVED AND INSTALLED NEW RH FLOOR SILL/GALLEY SUPPORT ANGLE BETWEEN FS310.00 & FS319.70 REF CRJ-200 SRM AND BOMBARDIER DWG.Jan 28, 2020 · N461SW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA2020031649270Skin · chafed*LOWER WING PLANK SKIN AT REAR SPAR MATING SURFACE FOR MLG FAIRING 193AB AT RBL45 CHAFED. (MARKED) (C-CHECK) RO 3/13/2020 PERFORMED A REPAIR ON LOWER WING PLANK SKIN AT REAR SPAR MATING SURFACE FOR MLG FAIRING 193AB AT RBL45 CHAFED REF BOMBARDIER REO. REPJan 28, 2020 · N461SW · Cndair CL6002B19 · Wing, Plate/SkinSDR SWIA2020031649269Skin · chafed*LOWER WING PLANK SKIN AT REAR SPAR MATING SURFACE FOR MLG FAIRING 193AB AT LBL45 CHAFED. (MARKED) (C-CHECK) RO 3/13/2020 PERFORMED A REPAIR ON LOWER WING PLANK SKIN AT REAR SPAR MATING SURFACE FOR MLG FAIRING 193AB AT LBL45 CHAFED REF BOMBARDIER REO. LEAKJan 28, 2020 · N461SW · Cndair CL6002B19 · Wing, Plate/SkinSDR SWIA2020031649324Stop Fitting · chafed* THE AVIONICS BAY DOOR SURROUND STRUCTURE'S FWD LH AND FWD RH STOP FITTING ASSY'S ARE CHAFED. (MARKED WITH RED SHARPIE) (C-CHECK) RO 3/13/2020 REMOVED AND REPLACED THE AVIONICS BAY DOOR SURROUND STRUCTURE'S FWD LH AND FWD RH STOP FITTING REF CRJ-200 SRMJan 27, 2020 · N461SW · Cndair CL6002B19 · Fuselage Main, StructureSDR SWIA2020031649318Fitting · cracked* THE AVIONICS BAY DOOR SURROUND STUCTURE'S PLASTIC GUIDE FITTINGS, AT ALL 4 LOCATIONS, ARE CRACKED. (MARKED WITH ORANGE FLAG TAPE) (C-CHECK) RO 3/13/2020 REMOVED 4 EA. CRACKED GUIDE FITTINGS AND INSTALLED 4 EA. NEW GUIDE FITIINGS AT AVIONICS DOOR SURROUNDJan 27, 2020 · N461SW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA2020031649268Striker · dented* THE PASSENGER DOOR SURROUND STRUCTURE'S FWD SEAL STRIKER HAS A DENT AT A PREVIOUS REPAIR, NEAR THE UPPER PIN STOP FITTING. (MARKED WITH ORANGE FLAG TAPE) (C-CHECK) RO 3/13/2020 PERFORMED REPAIR OUTLINED IN BOMBARDIER REO. COMPLIED WITH TASK CARD/LEAK CHEJan 27, 2020 · N461SW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA2020031649267Skin · dentedADM #6743. 5.125" AFT OF FS625, 4.5" BELOW STGR 20L. DENT MEASURING 1.625" LONG X .5" WIDE X .010" DEEP. PLOT, MAP, AND EVALUATE DAMAGE IF WITHIN ACCEPTABLE LIMITS OR REWORKED, ELIMINATE EVIDENCE USING STANDARD ACFT PRACTICES. (C-CHECK) RO 3/13/2020 PERFOJan 21, 2020 · N461SW · Cndair CL6002B19 · Fuselage Main, Plate/SkinSDR SWIA2020031649266Bulkhead · crackedCOMPLY WITH SCHEDULED MAINTENANCE CODE: AD - COMPLY WITH PARAGRAPH (J) OF AD BY: (J)(1) DOING A NONDESTRUCTIVE INSPECTION FOR CRACKING OF THE FORWARD FACE OF THE FUSELAGE STATION (FS) 621 PRESSURE BULKHEAD, IN ACCORDANCE WITH AWL. (J)(2) MODIFYING THE RPB ADec 30, 2019 · N461SW · Cndair CL6002B19 · Fuselage Main, BulkheadSDR SWIA201844273Tee Fitting · corrodedBELLY FAIRING SUPPORT TEE ANGLE MISSING LARGE AMOUNT OF MATERIAL FROM CORROSION LOCATED ON AFT SIDE OF RT WHEEL WELL AT BS 559. REMOVED AND REPLACED THE TEE ANGLE IAW SRM.Jan 27, 2018 · N461SW · Cndair CL6002B19 · Fuselage Main, Attach FittingsSDR SWIA201844272Strap · corrodedLH FLOORBEAM STRAP CORRODED. BS 559 BETWEEN LBL 27 TO LBL 45. REMOVED AND REPLACED THE STRAP IAW SRM.Jan 21, 2018 · N461SW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA201844271Floorbeam · corrodedRIGHT FLOORBEAM CORRODED, BS 559 BETWEEN RBL 27 TO RBL 45. INSTALLED A NEW FLOORBEAM IAW SRM.Jan 21, 2018 · N461SW · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR SWIA201844269Door Sill · corrodedSERVICE DOOR SILL CORRODED. REMOVED AND REPLACED THE SERVICE DOOR LOWER SILL ANGLE IAW SRM.Jan 21, 2018 · N461SW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA201844270Vane · chafedCHAFED AT THE RT INBD FLAP VANE CAP INBD EDGE. REPLACED THE FLAP VANE INBD CAP IAW SRM.Jan 20, 2018 · N461SW · Cndair CL6002B19 · Trailing Edge FlapsSDR SWIA201844268Vane · gougedLEFT INBOARD FLAP VANE. INBOARD LEADING EDGE FOUND GOUGED. REPLACED THE FLAP VANE LEADING EDGE CAP IAW SRM.Jan 20, 2018 · N461SW · Cndair CL6002B19 · Trailing Edge FlapsSDR SWIA201844267Skin · dentedTHREE CONSECUTIVE DENTS ON THE BOTTOM OF THE LT FUSELAGE AFT OF NLG BAY, BS 200. REPAIRED THE SKIN IAW REO.Jan 18, 2018 · N461SW · Cndair CL6002B19 · Fuselage Main, Plate/SkinSDR SWIA201844266Skin · dentedDENT ON THE LEFT FUSELAGE, JUST BELOW HYDRAULIC BRAKE ACCUMULATOR ACCESS PANEL. REPAIRED THE SKIN IAW REO.Jan 18, 2018 · N461SW · Cndair CL6002B19 · Fuselage Main, Plate/SkinSDR SWIA201844265Skin · dentedDENT FOUND ON THE LT WING LEADING EDGE WS 200, JUST OUTBOARD FROM OVERWING FUEL CAP. REWORKED THE DAMAGE IAW SRM AND REO.Jan 18, 2018 · N461SW · Cndair CL6002B19 · Wing, Plate/SkinSDR SWIA201844264Skin · dentedDENT FOUND ON THE LEFT SIDE OF THE FUSELAGE AFT OF AIR SERVICE DOOR BS 640. CUT OUT THE DAMAGED AREA, FABRICATED AND INSTALLED A REPAIR DOUBLER, BETWEEN BS 640 & 672.2, STRINGERS 16 & 19L IAW REO.Jan 18, 2018 · N461SW · Cndair CL6002B19 · Fuselage Main, Plate/SkinSDR SWIA201642830Check Valve · failedLEFT ENGINE EXPERIENCED AN IN FLIGHT EMERGENCY SHUT DOWN DUE TO HIGH OIL TEMP (199 IN RED) INDICATION ON EICAS. ALL OTHER ENGINE INDICATIONS NORMAL. CREW FOLLOWED QRH UNABLE TO GET TEMP INTO AMBER RANGE & SHUTDOWN THE ENGINE. DECLARED EMERGENCY & DIVERTED. Nov 14, 2016 · N461SW · Cndair CL6002B19 · Turbine Engine Oil SystemSDR SWIA201642735Probe · malfunctionedLEFT HIGH OIL TEMP. DECLARED AN EMERGENCY AND RETURNED TO THE FIELD. REMOVED AND REPLACED THE LEFT ENGINE OIL LEVEL PROBE IAW AMM. SERVICED LEFT ENGINE OIL AND VERIFIED OPERATION . RAN LEFT ENGINE AT TAKEOFF POWER SETTING. ALL ENGINE PARAMETERS NORMAL AT THOct 24, 2016 · N461SW · Cndair CL6002B19 · Engine Oil TemperatureSDR SWIA201641853Intercostal · corrodedPAX DOOR INTERCOSTAL AT DD3 HAS CORROSION. R & R THE PAX DOOR INTERCOSTAL DD3 IAW SRM. LEAK CHECK GOOD.Jan 18, 2016 · N461SW · Cndair CL6002B19 · Passenger/Crew Doors
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