N943SW
Service difficulty reports · 280
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 = 'N943SW' 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 = 'N943SW' 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 SWIA202157248Floor Support · corrodedLH OVER WING FLOOR SILL IS CORRODED AT THE FOLLOWING LOCATIONS: FS429, 441, 447, 452, 459, 478, 494, 507, 519, 522, 531, 536, 542, AND FS555 (C-CHECK RO 4/2/2021) COMPLIED WITH REO 601R-53-41-666 REV-C DATED 2012-11-06 FOR ALL AREAS. FORM 337 AND MAJOR RSDR SWIA202157297Nut · corrodedLIGHT SURFACE CORROSION ON NUT, RH WING SPOILER #3, UPPER PART OF HINGE (C-CHECK RO 4/2/2021) REMOVED CORRODED HARDWARE ON RH WING SPOILER #3 AND REPLACED WITH SERVICABLE HARDWARE IAW CRJ 200 AMM 27-64-05-000/400-801. REFERENCE CONTIUATION CARD FOR WORK PSDR SWIA202157296Bracket · corrodedSURFACE CORROSION, RH WING #4 SPOILER, FASTNER BRACKET BOLTS (2), WS 130.00 (C-CHECK RO 4/2/2021) REPLACED CORRODED FASTENER BRACKET IAW CRJ 200 AMM 57-53-02-400-802. SEE CONTINUE CARD FOR MAINTENANCE PERFORMED.SDR SWIA202157262Frame · corrodedF.S. 310.00 FRAME HAS CORROSION IN MULTIPLE SPOTS BETWEEN STRGR 25L AND 27. (C-CHECK RO 4/2/2021) INSTALLED NEW FS 310 STR 24L-24R IAW CRJ 200 SRM 51-42-06 AND 51-42-21 COMPLETED TASK CARD 51-900-1003-SKY AND ATTACHED COMPLETED FROM 337. NO WEIGHT CHANGESDR SWIA202157256Frame · corrodedF.S. 333.00 FRAME HAS CORROSION IN MULTIPLE SPOTS BETWEEN STRGR 26L AND 26R. (C-CHECK RO 4/2/2021) REMOVED AND REPLACED FRAME SECTOR IAW CRJ 200 SRMS 51-42-06 AND 51-42-21 AND DRAWING 601R32003. SEE ATTACHED STRUCTURAL MAJOR REPAIR TASK 51-900-1003-SKY ANSDR SWIA202157253Frame · corrodedF.S. 319.00 FRAME HAS CORROSION IN MULTIPLE SPOTS BETWEEN STRGR 26L AND 26R. (C-CHECK RO 4/2/2021) REMOVED AND REPLACED FS 319.00 FRAME BETWEEN 24L TO PRODUCTION SPLICE 24R IAW CRJ 200 SRM 51-40-11, 51-42-06, AND SKY CARD 51-900-1003-SKY NO WEIGHT CHANGE SDR SWIA202157250Frame · corrodedF.S. 349.00 FRAME HAS CORROSION IN MULTIPLE SPOTS BETWEEN STRGR 26L AND 26R. (C-CHECK RO 4/2/2021) REMOVED AND REPLACED FRAME SECTOR AT FS 349.00 IAW CRJ 200 SRM 51-42-06 AND 51-42-21. COMPLETED TASK CARD 51-900-1003-SKY AND ATTACHED COMPLETED FORM 337. NSDR SWIA202157325Guide Plate · chafedLH WING PANEL 592BB CHAFFE BRACKET HAS GOUGES. (C-CHECK RO 4/2/2021) REMOVED AND REPLACED L/H WING PANEL 592BB I/B GUIDE PLATE PN# 601R10140-74 IAW CRJ 200 SRM 51-40-11 & CRJ 200 SRM 51-42-06.SDR SWIA202157324Bracket · chafedPAX DOOR SURROUND CUTOUT FUSELAGE SIDE UPPER ROLLER BRACKET IS CHAFED (C-CHECK RO 4/2/2021) REMOVED AND REPLACED PAX DOOR SURROUND CUT OUT FUSELAGE SIDE UPPER ROLLER BRACKET IAW CRJ 200 SRM 51-42-00SDR SWIA202057261Landing · crackedCOMPLY WITH SCHEDULED MAINTENANCE CODE: RA41533-601R-53-11-2381 943SW-PR1 - LEFT TRU DOOR AFT LATCH CUT-OUT CRACKED. COMPLED WITH TEMPORARY REPAIR PER REO 601R-53-11-2381 DATED 2013-04-18 STEP 1 AND 2. PERMANENT REPAIR DUE WITHIN 6000 FLT HRS WITH ESCALATION SDR SWIA202057259Bulkhead · crackedCOMPLY WITH SCHEDULED MAINTENANCE CODE: AD 2019-08-04/02 40000 FC - COMPLY WITH PARAGRAPH (J) OF AD 2019-08-04 BY: (J)(1) DOING A NONDESTRUCTIVE INSPECTION FOR CRACKING OF THE FORWARD FACE OF THE FUSELAGE STATION (FS) 621 PRESSURE BULKHEAD, IN ACCORDANCE WITHSDR SWIA2020020648263Door Frame · corrodedFWD GALLEY SERVICE DOOR CUTOUT- BETWEEN FS 319.00 AND FS 349.00 STR 17R AND STR 18R THERE ARE 2 AREAS OF FLAKING /MISSING PAINT AND LIGHT CORROSION ON FLOOR SUPPORT BEHIND SERVICE DOOR LOWER LATCH FITTINGS. (C-CHECK) RO 2/04/2020 REPAIRED FWD GALLEY SERVICSDR SWIA2020020648258Floorbeam · crackedACCOMPLISH REWORK OF REPAIRS TO CRACK ON 280 BEAM AT FS 280.00 LBL 13 WL 69.5 (C-CHECK) RO 2/04/2020 COMPLIED WITH REWORK OF REPAIR TO CRACK ON 280 BEAN AT FS 280.00 LBL 13 WL 69.5 IAW BOMBARDIER REO. INSTALLATION OF ALTERNATE MLG PULLY ASSY AND GEAR ALTESDR SWIA2020020648262Floorbeam · corrodedFS 559.0 LH FLOOR SUPPORT PLATE CORRODED LBL 27 TO LBL 40 (C-CHECK) RO 2/04/2020 REMOVED CORROSION ON FLOOR SUPPORT PLATE ON FS 559.0 LBL27 TO LBL 40. FOUND TO BE OUT OF LIMITS. ORIGINAL THICKNESS .050", REMAINING .038", WITH TOTAL LOSS OF .012". FABRICATESDR SWIA2020020648257Frame · corrodedCORROSION FOUND ON FRAME SSECTION AT FS 605 ST LH 19 TO RH ST 25 WL 51.5 (C-CHECK) RO 2/04/2020 REMOVED CORRODED FRAME SEGMENT AND REPLACED FRAME SEGMENT AT FRAME 605 FROM LH STR-19 TO RH STR-25 IAW CRJ 200 SRM.SDR SWIA2020020648256Frame · corrodedCORROSION FOUND ON FRAME SECTION AT FS 589 LH STGR 19 TO RH STGR 25 (C-CHECK) RO 2/04/2020 REMOVED CORRODED FRAME SEGMENT AND REPLACED FRAME SEGMENT AT FRAME STATION 589 FROM LH STR 19 TO RH STR 25 IAW CRJ 200 SRM.SDR SWIA2020020648255Floor Support · corrodedCORROSION FOUND ON FLOOR SUPPORT STRUCTURE AT FS 625.3 LBL 45 WL 73.5 (C-CHECK) RO 2/04/2020 UPON FURTHER EVALUATION NO CORROSION FOUND. FLOOR SUPPORT STRUCTURE FOUND TO BE CRACKED AT F.S. 621.00 LBL 45 REMOVED AND REPLACED FLOOR SUPPORT STRUCTURE AT F.S 6SDR SWIA2020020648280Seat Track · corrodedPASSENGER SEAT RAIL ON LBL 9 BETWEEN FS 409+5 AND FS 409+118 IS EXFOLIATED (C-CHECK) RO 2/04/2020 UPON EVAL, FOUND SEAT TRACK CORROSION TO BE OUT OF LIMITS PER CRJ-200 SRM. RECOMMEND REPLACEMENT. SEE WC 1031 FOR FABRICATION.SDR SWIA2020020648279Seat Track · damagedPASSENGER SEAT RAIL ON LBL 9 BETWEEN FS 399.0 AND 409+5 HAS LIGHT DAMAGE IN BOTTOM OF RAIL (C-CHECK) RO 2/04/2020 UPON EVAL, FOUND SEAT TRACK CORROSION TO BE OUT OF LIMITS PER CRJ-200 SRM. RECOMMEND REPLACEMENT. SEE WC 1031 FOR FABRICATION.SDR SWIA2020020648273Vane · chafedCHAFE ON L/E OF LH I/B FLAP VANE AT WS 139.90 FOUND TO BE OUT OF LIMITS (C-CHECK) RO 2/04/2020 REMOVED AND REPLACED L/E SKIN AT WS 139.90 ON L/H INB FLAP VANE IAW CRJ 200 SRM, AND SEALED L/E AREA IAW CRJ 200 SRM.SDR SWIA2020020648272Vane · chafedCHAFE ON L/E OF LH I/B FLAP VANE AT WS 104.00 FOUND TO BE OUT OF LIMITS (C-CHECK) RO 2/04/2020 REMOVED AND REPLACED L/E SKIN AT W.S. 104.00 ON L/H INB FLAP VANE IAW CRJ 200 SRM, WHOLE L/E SKIN CHANGED FROM WS 104.00 TO WS 120.30. SEALED L/E AREA IAW CRJ SDR SWIA2020020648270Vane · chafedCHAFFE ON L/E OF LH I/B FLAP VANE SKIN AT WS 56.00 FOUND TO BE OUT OF LIMITS (C-CHECK) RO 2/04/2020 REMOVED AND REPLACED L/E FLAP VANE AT W.S. 56.00 ON L/H INB FLAP VANE IAW CRJ 200 SRM, AND SEALED AREA IAW CRJ 200 SRM.SDR SWIA2020020648267Seat Track · corrodedPASSENGER SEAT RAIL ON RBL 9 BETWEEN FS 409+5 AND FS 409+118 IS CORRODED (C-CHECK) RO 2/04/2020 UPON EVAL, FOUND SEAT TRACK CORROSION TO BE OUT OF LIMITS PER CRJ-200 SRM. RECOMMEND REPLACEMENT. SEE WC 1031 FOR FABRICATION.SDR SWIA2020020648266Seat Track · corrodedPASSENGER SEAT RAIL ON RBL9 BETWEEN FS 399.0 AND FS 409+5 IS CORRODED (C-CHECK) RO 2/04/2020 UPON EVAL, FOUND SEAT TRACK CORROSION TO BE OUT OF LIMITS PER CRJ-200 SRM. RECOMMEND REPLACEMENT. SEE WC 1031 FOR FABRICATION.SDR SWIA2020020648260Floorbeam · crackedSUPPORT BEAN ANGLE BRACKET CRACKED AT RBL 27-33 AT FS 495.0 I/B OF RBL 33 O/B IF RBL 27 (C-CHECK) RO 2/04/2020 REMOVED OVERWING FAIRING FOR ACCESS TO FASTENERS, REMOVED CRACKED SUPPORT BEAM ANGLE BRACKETS, FABRICATED NEW FLOOR SUPPORT BEAM ANGLE BRACKETS, SDR SWIA2020020648259Floorbeam · crackedSUPPORT BEAM ANGLE BRACKET IS CRACKED AT LBL 37-33 AT FS 495.0 I/B OF LBL 33 AND O/B OF LBL 27 (C-CHECK) RO 2/04/2020 REMOVED OVERWIND ACCESS PANELS, REMOVED ANGLE BRACKETS, FABRICATED NEW ANGLE BRACKETS TREATED PRIMED PAINTED AFTER PERFORMING HFEC INSPECTSDR SWIA2020020648278Seat Track · damagedREMOVE AND REINSTALL PAX SEAT TRACK AT RBL 9 FS 409.00+126 TO FS 559.00+4 (C-CHECK) RO 2/04/2020 REMOVED AND INSTALLED PAX SEAT TRACK @ RBL 9 F.S. 409.00+126 TO F.S. 559.00+4 IAW CRJ 200 AMM.SDR SWIA2020020648277Seat Track · corrodedREMOVE AND REINSTALL PAX SEAT TRACK AT RBL 9 FS 559.00+4 TO FS 559.00+86 (C-CHECK) RO 2/04/2020 INSTALLESD NEW SEAT TRACK AT RBL9 FS 599.4 TO FS 599.00+86 IAW CRJ200 AMM. DIAL TW AV7115 EXP DATE 10/09/2020 TW 30-200IN/LBS AV7139 EXP JAN 2020SDR SWIA2020020648265Seat Track · corrodedPASSENGER SEAT RAIL ON RBL 9 BETWEEN FS 559+4 AND FS 559+86 IS CORRODED (C-CHECK) RO 2/04/2020 UPON EVAL, FOUND SEAT TRACK CORROSION TO BE OUT OF LIMITS PER CRJ-200 SRM. RECOMMEND REPLACEMENT. SEE WC 1031 FOR FABRICATION.SDR SWIA2020020648264Seat Track · corrodedPASSENGER SEAT RAIL ON RBL 9 BETWEEN FS 409+126 AND FS 559+4 IS CORRODED (C-CHECK) RO 2/04/2020 UPON EVAL, FOUND SEAT TRACK CORROSION TO BE OUT OF LIMITS PER CRJ-200 SRM. RECOMMEND REPLACEMENT. SEE WC 1031 FOR FABRICATION.SDR SWIA2020020648261Seat Track · corrodedPASSENGER SEAT RAIL ON RBL 9 BETWEEN FS 364.0 AND FS 399.0 IS CORRODED (C-CHECK) RO 2/04/2020 PASSENGER SEAT RAIL AT RBL9 FS 364.00 TO FS 399.00 FOUND TO BE OUT OF LIMITS. CORROSION DAMAGE IS 0.035" DEEP. ORIGINAL 0.115" REMAINING 0.080". MAX ALLOWABLE RESDR SWIA2020020648254Access Panel · gougedLH WING ACCESS OPENING 540AB HAS GOUGE ON THE LANDING (C-CHECK) RO 2/04/2020 ACCOMPLISHED REPAIR TO LH WING FUEL TANK ACCESS PANEL 540AB WING PLANK LANDING. IAW REO. ORIGINAL THICKNESS .182" REMAINING MATERIAL THICKNESS .179" GAP AND LEAK CHECKS: GOOD.SDR SWIA2020020648253Access Panel · gougedLH WING OPENING ACCESS 540BB HAS GOUGES ON THE LANDINGS (C-CHECK) RO 2/04/2020 ACCOMPLISHED REPAIR TO LH WING FUEL TANK ACCESS PANEL 540BB WING PLANK LANDING. IAW CRJ-200 REO. ORIGINAL MATERIAL THICKNESS .182" REMAINING MATERIAL THICKNESS .181". GAP AND SDR SWIA2020020648276Floorbeam · crackedCRACK FOUND ON 280 BEAM AT FS 280 LBL 13 WL 69.5 (C-CHECK) RO 2/04/2020 REMOVED CRACKED AREA IAW BOMBARDIER REO. CRACK WAS FOUND TO BE WITHIN HORIZONTAL FLANGE ONLY ON LOWER SECTION OF 280 BEAM. PREFORMED REPAIR SCHEME "A" IAW BOMBARDIER REO. RESTORED AIRSDR SWIA2020020648275Vane · chafedCHAFE ON L/E OF RH I/B FLAP VANE SKIN AT WS 139.90 FOUND TO BE OUT OF LIMITS (C-CHECK) RO 2/04/2020 REMOVED AND REPLACED R/H, I/B FLAP VANE L/E, AT W/S 139.90, PER CRJ-200, SRM TR 51-42SDR SWIA202020648274Vane · chafedCHAFFE ON L/E OF RH I/B FLAP VANE SKIN AT WS 104.00 FOUND TO BE OUT OF LIMITS (C-CHECK) RO 2/04/2020 REMOVED AND REPLACED R/H, I/B FLAP VANE L/E PER CRJ-200, SRM TR 51-42 AT W/S 104.00.SDR SWIA2020020648271Vane · chafedCHAFFE ON L/E OF RH I/B FLAP VANE SKIN AT WS 56.00 FOUND TO BE OUT OF LIMITS (C-CHECK) RO 2/04/2020 REMOVED AND REPLACED L/E ON R/H I/B FLAP VANE AT WS 56.00 IAW CRJ 200 SRM.SDR SWIA2020020648269Vane · chafedCHAFING MARKS ON L/E OF RH I/B FLAPS VANE SKIN AT WS 56.00,WS 104.00 AND WS 139.90 (C-CHECK) RO 2/04/2020 ALL THREE AREAS CHAFING AT WS 56.00 WS 104.00 AND WS 139.90 ARE OUT OF LIMITS (OVER .030 MATERIAL LOSS) PER BOMARDIER REO EFFECTIVITY CL601R ALL. SEE SDR SWIA2020020648268Vane · chafedCHAFING MARKS ON L/E OF LH I/B FLAPS VANE SKIN AT WS 56.30,WS 104.00 AND WS 139.90 (C-CHECK) RO 2/04/2020 ALL THREE AREAS CHAFFING AT WS 56.3, WS104.00 AND WS 139.90ARE OUT OF LIMITS (OVER .030 MATERIAL LOSS. PER BOMBARDIER REO EFFECTIVITY ALL. SEE NR# 500SDR SWIA2019080846170Strut · failedGEAR DISAGREE AND NOSE DOOR OPEN WARNING MESSAGE AFTER TAKE OFF. COMPLETED QRH AND RETURNED TO FIELD. FLT 5673. INSTALLED NLG SHOCK STRUT IAW AMM. INSTALLED LH AND RH NOSE TIRE ASSY IAW AMM. OPS CHECK GOOD.SDR SWIA2019010845414Bracket · bentGEAR DISAGREE WARNING AFTER T/O ALONG WITH NOSE DOOR OPEN WARNING MSG. COMPLIED WITH QRH. NOSE GEAR WOULD NOT RETRACT. SELECTED GEAR HANDLE DOWN ALL GEAR EXTENDED NORMALLY. (FLT#5466) CLOSED REMOVED AND REPLACED BENT BRACKET FOR NLG CENTERED EXTENDED PROXIMITYSDR SWIA2018112745272Landing Gear · icedGEAR DISAGREE WARNING MESSAGE AFTER TAKE OFF. (FLT#5015) CLOSED LT MLG NOT UP AND LOCKED. CLEARED ALL ICE FROM GEAR AND INSPECTED ALL LANDING GEAR EXTENSION AND RETRACTION COMPONENTS, NO FAULT NOTED IAW FIM. PERFORMED LANDING GEAR RETRACTION AND EXTENSION CHECSDR SWIA2018052444716Acm · seizedON TAXI OUT, FLIGHT DECK AND CABIN CREW NOTICED SIGNIFICANT SMOKE AND SMELL IN CABIN AND FLIGHT DECK. AIRCRAFT WAS STOPPED ON THE TAXIWAY AND SHUTDOWN. ALL PERSONNEL EXITED THROUGH THE MAIN CABIN DOOR. AIRFIELD FIRE RESCUE AND CAPTAIN CLEARED THE AIRCRAFT ANDSDR SWIA201541761Rib · damagedRT INBD FLAP HAS 3 HOLES UNDER SEAL AT INBD AFT EDGE MISSING FASTENERS. R & R RIB IAW SRM.SDR SWIA201541763Skin · corrodedCORROSION ON EXTERNAL SKIN, AROUND SCREW HOLE FS409+87 BETWEEN STR 23L AND STR 24L. REMOVED CORROSION IAW SRM.SDR SWIA201541762Skin · dentedONE OUTWARD DENT LOCATED ON AFT FUSLEAGE TOP SKIN BETWEEN BS 574 AND 585, BETWEEN STR 5-6L. PERMANENTLY REPAIRED ONE DENT OUT OF LIMITS IAW SRM AND EA.SDR SWIA201439733Unknown · vibrationRETURNED TO THE FIELD DUE TO CREW REPORTED VIBRATIONS INFLIGHT. FELT IN THE AIRFRAME AND YOKE. PILOT SAYS THEY WERE VERY AGGRESIVE 200 AGL AND ABOVE 270 KTS. INSPECTED ACFT FLIGHT CONTROLS NO DEFECTS NOTED. RESEALED FWD MLG FAIRING FWD EDGE IAW AMM AND SDR SWIA201438708Shutoff Valve · failedCLIMBING THROUGH 11,000 FT, THE RT PACK CLOSED AND ACFT RETURNED TO FIELD. THE ENGINE 10TH STAGE BLEED AIR SHOWED CLOSED ON THE SYNOPTIC PAGE WITH THE SWITCH SELECTED OPEN. R & R LT PRSOV IAW AMM. OPS CHECKS GOOD. CONDUCTED POWER RUNS TO GET MANIFOLD PRESSDR SWIA201438707Bleed Valve · failedDURING CLIMB OUT BETWEEN 24-25,000 FT, THE RT PACK CLOSED AND THE ACFT STARTED TO DEPRESSURIZE. STARTED A DESCENT AND RESET THE PACK AROUND 18,000 FT & IT STARTED TO PRESSURIZE THE CABIN. CABIN ALTITUDE REACHED 9000 FT. NO MASKS DROPPED. R & R RT 10TH STASDR SWIA201437401Lens · missingRED LENS ON THE CENTER CABIN OVERHEAD EMERGENCY EXIT SIGN IS MISSING. REPLACED RED LENS.
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