N460SW
Service difficulty reports · 133
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 = 'N460SW' 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.
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 = 'N460SW' AND registry_match = 'registration' ORDER BY difficulty_date DESC
Run it at the DuckDB prompt, or in any tool that reads Parquet over HTTPS. More ways to query the release are on Use the data.
SDR J6BA2024091000008Bpsu · failedON APPROACH TO RWY 22L, WE SELECTED FLAPS 45. WE RECEIVED FLAPS FAIL. WE EXECUTED A GO-AROUND. WE NEVER UTILIZED GO-AROUND THRUST SINCE IT WAS EXECUTED AT OVER 1000 FT. WE PERFORMED ALL CHECKLISTS TO INCLUDE QRH (FLAPS FAIL CHECKLIST) AND APPLICABLE DOCUMENTATSDR SWIA2022122967064Floorbeam · mechanic errorF.S. 280 TOP OF ANGLE BETWEEN LBL27 TO LBL36 HAS A SNOW MAN HOLE AROUND NUTPLATE. REPAIRED FS280 LBL27 TO LBL36 IAW MHIRJ REO 601R-53-11-3815 REV. -.SDR SWIA202267063Floorbeam · corrodedF.S. 280 FLOORBOARD SUPPORT ANGLE IS CORRODED BETWEEN LBL9 TO RBL9. REMOVED AND REPLACED CORRODED FS280 FLOORBOARD SUPPORT ANGLE BETWEEN LBL9 TO RBL9 IAW REO 601R-53-11-926 REV B.SDR SWIA2022122967062Floorbeam · corrodedLBL9 FLOOR BEAM IS CORRODED BETWEEN F.S. 409+64 TO F.S. 409+80. INSTALLED NEW SERVICEABLE FLOOR BEAM IAW REO 601R-53-31-1256 REV.SDR SWIA2022122967061Floorbeam · corrodedRBL9 FLOOR BEAM IS CORRODED BETWEEN F.S. 409+32 TO F.S. 409+48. INSTALLED NEW SERVICEABLE RBL9 FLOOR BEAM CAP FROM F.S 409.00+5 F.S 409.00+118 IAW MHIRJ REO 601R-53-31-1254 DATED: 2022-12-12 REV: -- , CRJ 200 SRM 51-42-21 AND 51-42-06.SDR SWIA2022122967060Hinge · chafedWHILE INSPECTING REPAIR ON PAX DOOR PIANO HINGE HALF ON DOOR SIDE HAS CHAFES ON THE FOLLOWING LUGS (FROM FWD SIDE TO AFT): 1, 2, 4, 5, 12, 13, 15, 16, 19, 20, 22, 24, 25, 26, AND 27. JOB 9780385 OP 00053, CAMP 25881132 FOUND ALL LUGS ON FUSELAGE SIDE OF HINGE SDR SWIA2022122967059Post · crackedFS409+128 RBL18 OUTBD VERTICAL POST HAS AN INDIACTION .2" LONG BY 60% FSH IN THE AFT RADIUS @WL69. FAILED NDT INSPECTION, (C-CHECK RO 12/29/2022) INSTALLED NEW SERVICABLE FS409+128 RBL18 OUTBD VERTICAL POST IAW REO 601R-53-41-889 REV-D DATED 2018-10-04SDR SWIA2022122967058Post · crackedFS409+128 LBL18 OUTBD VERTICAL POST HAS AN INDIACTION .2" LONG BY 50% FSH IN THE AFT RADIUS @WL69. FAILED NDT INSPECTION, REMOVED AND REPLACED INBD AND OUTBD VERTICAL POST AT FS 409+128 LBL18 IAW REO 601R53-41-889D AND CRJ-200 SRM 51-42-06,SDR SWIA2022122967066Bracket · crackedBS 621 REAR PRESSURE BULKHEAD AFT SIDE, AT STGR 15R INTERCOSTAL CENTER ATTACH ANGLE IS CRACKED. REMOVED AND REPLACED THE INTERCOSTAL IAW SRM 51-42-21.SDR SWIA2022122967065Vane · chafedRIGHT INBD. FLAP VANE HAS 3 EA. CHAFS ON L/E AT POSITIONS WHERE BUMPER STOPS MAKE CONTACT. REMOVED AND REPLACED RH I/B FLAP VANE LEADING EDGES IAW SRM 51-42-13.SDR SWIA202264679None · failedON APPROACH LANDING GEAR DISAGREE WHEN LOWERING GEAR, CYCLED GEAR PER QRH AND STILL HAD DISAGREE (NOSE GREEN MAIN WHITE) PROCEEDED WITH QRH AND GOT 3 GREEN WITH MANUAL GEAR EXTENSION (FLIGHT 4234 - FILED CLOSED) TROUBLESHOT LANDING GEAR DISAGREE. PERFORMSDR SWIA202163103None · wornL/H INBOARD FLAP MOVEABLE VANE IS SHOWING WEAR ALONG LEADING EDGE WHERE VANE MEETS STOPS. (FILED - CLOSED) REPLACED L/H INBD FLAP ASSY AS REQUIRED REFERENCING APPLICABLE STEPS OF AMM 57-21-34 AND AMM 27-54-01 AND COMPLIED WITH 27-900-1006. / TORQUE WRENCH SDR SWIA202054136Connector · out of toleranceRT OUTBOARD FLIGHT SPOILER PCU RESISTANCE VALUE MEASURED AT SECU PLUG: 2P1CN-A PINS: 11K/12K WAS FOUND TO BE OUT OF RANGE (1,040 K OHMS). FILED CLOSED. REMOVED AND REPLACED RT FLIGHT SPOILER OUTBOARD PCU, IN REFERENCE TO CRJ 200 AMM. OPERATIONS CHECK GOOD SDR SWIA202054135Connector · out of toleranceRT INBOARD FLIGHT SPOILER PCU RESISTANCE VALUE MEASURED AT SECU PLUG: 1P1CN-B PINS: 1K/2K WAS FOUND TO BE OUT OF RANGE (1,024 K OHMS). FILED CLOSED. REMOVED AND REPLACED RT FLIGHT SPOILER INBOARD PCU, IN REFERENCE TO CRJ 200 AMM. OPERATIONS CHECK GOOD AT THSDR SWIA202054134Connector · out of toleranceLT INBOARD SPOILERON PCU RESISTANCE VALUE MEASURED AT SECU PLUG: 2P1CN-B PINS: 1A/2A WAS FOUND TO BE OUT OF RANGE (6.2M OHMS). FILED CLOSED. REMOVED AND REPLACED LT SPOILERON INBOARD PCU, IAW AMM. OPERATIONS CHECK GOOD, REF CP 21820650 FOR LEAK CHECK.SDR SWIA202054133Connector · out of toleranceLT OUTBOARD SPOILERON PCU RESISTANCE VALUE MEASURED AT SECU PLUG: 1P1CN-A PINS:11A/12A WAS FOUND TO BE OUT OF RANGE (1,029 K OHMS). FILED CLOSED. REMOVED AND REPLACED LT SPOILERON OUTBOARD PCU, IAW AMM. OPERATIONS CHECK GOOD, REF CP 21826310 FOR LEAK CHECKSDR SWIA2019121746900Hinge Fitting · gouged* L/H AILERON INB AND OBD CENTER HINGE FITTINGS ATTACHED TO AFT WING SPAR HAVE SMALL GOUGES ON LOWER SIDES OF FITTINGS. (C-CHECK) RO 12/13/2019 BLENDED GOUGES - EVALUATED REPAIRS, FOUND TO BE OUT OF LIMITS. REQUESTED ENGINEERING SUPPORT AND RECIEVED REO, COMPSDR SWIA2019121746899Door Sill · corroded**PAX DOOR LOWER FLOOR SILL CAP ANGLE IS CORRODED. FLAGGED (C-CHECK) RO 12/13/2019 FOUND NO CORROSION ON PAX DOOR LOWER FLOOR SILL CAP ANGLE ( MADE FROM STEEL PER SRM) AFTER CLEANED RUST FROM CORRODED SCREWS REF AMM.SDR SWIA2019121746898Floor Support · corroded*PAX DOOR LOWER FLOOR SILL IS CORRODED. FLAGGED (C-CHECK) RO 12/13/2019 REPLACED WITH NEW PART PAX DOOR LOWER FLOOR SILL REF SRM, SEE CONTINUATION CARD FOR DETAILS.SDR SWIA2019121746897Door Frame · corroded*AVIONICS DOOR CUT-OUT AFT SRUCTURE IS CORRODED FRAME "ANGLE. FLAGGED" (C-CHECK) RO 12/13/2019 REMOVED CORROSION FROM AVIONICS CUT-OUT AFT STRUCTURE ANGLE AT FS394.00 REF SRM. FOUND TO BE OUT OF LIMITS REF SRM. MEASURED THICKNESS ..042. ORIGINAL THICKNESS .SDR SWIA2019121746896Retainer · corroded* L/H AILERON OBD HINGE BOLT OBD RETAINER HARDWARE CORRODED. (C-CHECK) RO 12/13/2019 ORDERED AND RECEIVED NEW L/H OBD HINGE BOLTS OBD RETAINER HARDWARE; BOLTS (2EA) AND WASHERS (2EA). INSTALLED ON JOB 2780375 OP 5174 AND TRANS # 19723205.SDR SWIA2019121746895Retainer · corroded* L/H AILERON OBD HINGE BOLT OBD RETAINER HARDWARE CORRODED. (C-CHECK) RO 12/13/2019 ORDERED AND RECEIVED NEW L/H OBD HINGE BOLTS OBD RETAINER HARDWARE; BOLTS (2EA) AND WASHERS (2EA). INSTALLED ON JOB 2780375 OP 5174 AND TRANS # 19723205.SDR SWIA2019121746894Retainer · corroded* L/H AILERON OBD HINGE BOLT OBD RETAINER HARDWARE CORRODED. (C-CHECK) RO 12/13/2019 ORDERED AND RECEIVED NEW L/H OBD HINGE BOLTS OBD RETAINER HARDWARE; BOLTS (2EA) AND WASHERS (2EA). INSTALLED ON JOB 2780375 OP 5174 AND TRANS # 19723205.SDR SWIA2019121746893Retainer · corroded* R/H AILERON OBD HINGE BOLT RETAAINERS HAVE CORRODED HARDWARE, (C-CHECK) RO 12/13/2019 REMOVED RIGHT AILERON OUTBOARD HINGE BOLT RETAINERS HARDWARE REF AMM AND INSTALLED (4EA) NEW BOLTS/WASHERS REF AMM.SDR SWIA2019121746892Bolt · corrodedRIGHT WING OUTBOARD GROUND SPOILER HAS CORRODED ACTUATOR MOUNT HARDWARE. BOLT, NUT, AND WASHER . MARKED WITH ORANGE FLAG. (C-CHECK) RO 12/13/2019 REMOVED CORRODED HARDWARE AND INSTALLED NEW HARDWARE REF AMM. OPS TEST GOOD. RIG GOODSDR SWIA2019121746891Bolt · corroded* RIGHT WING INBOARD GROUND SPOILER HAS CORRODED ACTUATOR MOUNT HARDWARE. BOLT, NUT, AND WASHER. MARKED WITH ORANGE FLAG. (C-CHECK) RO 12/13/2019 REMOVED CORRODED HARDWARE, AND REPLACED WITH NEW HARDWARE REF AMM. OPS CHECK GOOD. RIG CHECK GOODSDR SWIA2019121746890Bolt · corroded* LEFT WING OUTBOARD GROUND SPOILER HAS CORRODED ACTUATOR MOUNT HARDWARE. BOLT, NUT, AND WASHER. MARKED WITH ORANGE FLAG. (C-CHECK) RO 12/13/2019 REMOVED OLD AND INSTALLED NEW HARDWARE ON LH OUTBOARD GROUND SPOILER AMM. OPS TEST GOOD. RIG CHECK GOODSDR SWIA2019121746889Bolt · corroded* LEFT WING INBOARD GROUND SPOILER HAS CORRODED ACTUATOR MOUNT HARDWARE. BOLT, NUT AND WASHER. MARKED WITH ORANGE FLAG. (C-CHECK) RO 12/13/2019 REMOVED OLD HARDWARE AND REPLACED WITH NEW HARDWARE AMM. OPS TEST GOOD. RIG GOODSDR SWIA2019121746888Hinge · corroded* LAVATORY SERVICE DOOR ( 196AR ) HAS UPPER AND LOWER HINGES ( BOTH HALFS ) CORRODED. (C-CHECK) RO 12/13/2019 REMOVED AND REPLACED BOTH SIDES OF THE HINGES ON LAV SERVICE DOOR 196AR REF SRM. ALL PARTS PART FOUND TO BE EXFOLIATED. BOND CHECKS GOODSDR SWIA2019121746887Bolt · corroded* LEFT WING CORRODED MOUNTING HARDWARE LEFT WING , GROUND, FLIGHT AND SPOILERONS. HINGE FITTINGS HAVE CORRODED MOUNT BOLTS, NUTS , WASHERS. (C-CHECK) RO 12/13/2019 REMOVED AND REPLACED HINGE HARDWARE ON LH OUTBOARD GROUND SPOILER, LH FLIGHT SPOILER, AND LH SDR SWIA2019121746886Bolt · corroded* RIGHT WING CORRODED MOUNTING HARDWARE RIGHT WING, GROUND, FLIGHT AND SPOILERONS. HINGE FITTINGS HAVE CORRODED MOUNT BOLTS, NUTS, WASHERS. (C-CHECK) RO 12/13/2019 REPLACED CORRODED MOUNTING HARDWARE AT RIGHT WING GROUND SPOILERS, FLIGHT SPOILER AND SPOILERONSDR SWIA2019121746885Trunnion · crackedWHILE PERFORMING SB 601R-57-046 FOUND CRACK INDICATIONS IN HOLE #20 LH MLG TRUNNION. (C-CHECK) RO 12/13/2019 REPAIRED HOLE 20 LH MLG TRUNNION REF REO, NO MEASURABLE WIEGHT CHANGES NOTED.SDR SWIA2019121746884Angle · crackedRH WING TRAILING EDGE IB CAP ANGLE ( BATT RIB) IS CRACKED, FOUND WHILE ACCESSING TRUNNION REPLACEMENT. (C-CHECK) RO 12/13/2019 REMOVED CRACKED CAP ANGLE( BATT RIB) ON RH WING AND INSTALLED A NEW CAP ANGLE REF SRM.SDR SWIA2019121746883Stringer · cracked*STGR 3 L IS CRACKED WHERE IT ATTACHES TO PAX DOOR UPPER SILL/LONGERON AT FS379. (C-CHECK) RO 12/13/2019 CUT OUT DAMAGE STRINGER SECTION OF 3L AT FS 386 APPRX RREF SRM. FABRICATED REPLACEMENT STRINGER SECTION USING S6807 P.O.#62664. REF:SRM. WEIGHT OF REMOVESDR SWIA2019121746882Frame · cracked*FRAME ABOVE THE PAX DOOR AT FS333 BETWEEN STGR O AND STGR 1 L IS CRACKED AT TOOLING HOLE. (C-CHECK) RO 12/13/2019 REMOVED AND INSTALLED REPLACEMENT FRAME AT FS333.00 FROM STR0 TO STR1L REF: SRM. SEE CONTINUATION CARD FOR DETAILS.SDR SWIA2019121746881Duct · cracked* APU UPPER AIR INLET DUCT HAS CRACKED STIFFENER. (C-CHECK) RO 12/13/2019 CLEANED AND WELDED CRACK ON APU UPPER INLET REF. MEGGITT CMM 49-14-01 REPAIR 8-BSDR SWIA2019121746880Duct · cracked* APU LOWER AIR INLET DUCT HAS MULTIPLE CRACKED STIFFENERS. (C-CHECK) RO 12/13/2019 ORDERED AND RECEIVED APU AIR INLET DUCT, INSTALLED ON JOB 2780375, OP/23, MX TRANS #19808669.SDR SWIA2019121746879Attach Angle · cracked* L/H WING CENTER LEADING EDGE PANEL INB ATTACHMENT ANGLE CRACKED. ( FLAGGED ) (C-CHECK) RO 12/13/2019 LOACATED AND DRILLED A NEW ATTACH ANGLE FOR THE LH WING CENTER LEADING EDGE, IB END REF SRM AND INSTALLED IT REF SRM.SDR SWIA2019121746878Window Frame · cracked* R/H WINDSHIELD SIDE POST SUPPORT CRACKED. (C-CHECK) RO 12/13/2019 REMOVED AND INSTALLED NEW RIGHT SIDE POST SUPPORT PN# 601R34032-22 PER REFERENCE DRAWING AND SRM. SEE CONTINUATION CARD FOR DETAILS. LEAK AND OPS CHECKS GOOD.SDR SWIA2019121746877Window Frame · cracked* L/H WINDSHIELD SIDE POST SUPPORT CRACKED. (C-CHECK) RO 12/13/2019 REMOVED AND INSTALLED NEW SIDE POST SUPPORT PN# 601R34032-21 PER REFERENCE DRAWING# 601R34032 REV V AND SRM. SEE CONTINUATION CARD FOR DETAILS. LEAK AND OPS CHECKS GOOD.SDR SWIA2019121746876Shroud · cracked* FLIGHT COMPARTMENT SEATS , CO-PILOTS SEAT STRUCTURE PLASTIC SEAT BACK SHROUDS / BOTH INBD AND OUTBOARD ARE CRACKED. (C-CHECK) RO 12/13/2019 REMOVED AND REPLACED (2) NEW BACKREST ASSEMBLY SHROUD PN #1C3076-1AJT AND PN #1C3076-2AJT ON CO-PILOT SEAT REF SRM.SDR SWIA2019121746875Shroud · cracked* FLIGHT COMPARTMENT SEATS, CAPTAINS SEAT STRUCTURE PLASTIC SEAT BACK SHROUDS / INBOARD AND OUTBOARD CRACKED , BROKEN. (C-CHECK) RO 12/13/2019 REMOVED AND REPLACED (2) NEW BACKREST ASSEMBLY SHROUD ON CAPTAIN SEAT REF SRM.SDR SWIA2019121746874Drag Angle · cracked*PAX DOOR AFT DRAG ANGLE IS CRACKED. FLAGGED (C-CHECK) RO 12/13/2019 REMOVED AND INSTALLED NEW PAX DOOR AFT DRAG ANGLE REF REO. SEE CONTINUE CARD FOR DETAILS.SDR SWIA2019121746873Seal · cracked*SEAL AROUND CO- PILOTS WINDSHIELD IS CRACKED AND WIND CHAFED. FLAGGED (C-CHECK) RO 12/13/2019 REPAIRED AND APPLIED NEW SEALANT AROUND CO-PILOTS WINDSHIELD REF AMM, SEE CONTINUATION CARD FOR DETAILS.SDR SWIA2019121746872Seal · cracked*SEAL AROUND PILOTS WINDSHIELD IS CRACKED AND WIND CHAFED. FLAGGED (C-CHECK) RO 12/13/2019 REPAIRED SEAL AROUND PILOTS WINDSHIELD REF AMM, SEE CONTINUATION CARD FOR DETAILS.SDR SWIA2018052944717Sensor · failedAFTER TAKE OFF, RECEIVED A NOSE WHEEL STEERING INOPERATIVE, WOW INPUT CAUTION AND WOW OUTPUT FAIL STATUS MESSAGE. NOSE WHEEL STEERING WOULDN'T RE-ARM. ADJUSTED THE NR 2 NLG WOW SENSOR IAW AMM. PERFORMED NLG SWINGS OPS CHECKED GOOD IAW AMM. NO FURTHER DEFECTSSDR SWIA2017111343975Floor Skin · crackedPRESSURE FLOOR SKIN IS CRACKED AT BS 460, LBL 9 TO BL 0. REPAIRED THE PRESSURE FLOOR SKIN IAW SRM. MAJOR REPAIR. LEAK CHECKED GOOD.SDR SWIA201642768Smoke Detector · false activationDECLARED EMERGENCY - LAV SMOKE ALARM ON LANDING. SMOKE TOILET CAUTION MESSAGE ON ARRIVAL. NO SMOKE OR FIRE PRESENT. PERFORMED OPERATIONAL TEST OF LAV SMOKE DETECTION SYSTEM IAW AMM. INSPECTED BOTH ENGINES FOR OIL CONTAMINATION IN BLEEDS. NONE FOUND. INSPECTSDR SWIA201541551Vane · chafedRT INBD FLAP VANE L/E OTBD SKIN SECTION CHAFED. R & R RT INBD FLAP VANE L/E SKIN OTBD SECTION IAW SRM AND STS EA.SDR SWIA201541550Vane · chafedRT INBD FLAP VANE L/E SKIN CENTER SECTION CHAFED. R & R RT INBD FLAP VANE L/E SKIN CENTER SECTION IAW SRM AND STS EA.
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