N936SW

Service difficulty reports · 209

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 = 'N936SW' 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 SWIA2020071751801Windshield · crackedFOUND LH WNDSHLD CRACKED AT CENTER TOP PORTION OF OUTER GLASS PLY. REMOVED AND REPLACED THE PILOTS WINDSHIELD.Aug 13, 2020 · N936SW · Cndair CL6002B19 · Flight Compartment WindowsSDR SWIA2020032749484Skin · corrodedCORROSION FOUND ON BOTTOM RIVET LINE OF BELLY UNDER PANEL 195BB WHICH WAS REMOBE TO FACILITATE STRUCTURES REPAIR OF FRAME AT FS 574 STRG L25 TO STRG 26 (C-CHECK) RO 3/25/2020 REWORKED AREA I.A.W. REO.MAX. BLEND-OUT FOUND AT FS 559+96 STR 27 WITH A REMAININFeb 27, 2020 · N936SW · Cndair CL6002B19 · Fuselage Main, Plate/SkinSDR SWIA2020032749501Nut Plate · brokenBROKEN NUT PLATE ON FLOOR SUPPORT BEAM AT FS 559 LBL 10 (C-CHECK) RO 3/25/2020 REMOVED AND REPLACED DOME NUT ON FLOOR SUPPORT BEAM AT F.S. 559 LBL 10 IAW SRM.Feb 25, 2020 · N936SW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA2020032749495Intercostal · corrodedINTERCOSTAL AT LBL 42 WL 78.0 AND FS 295.0 TO FS 310.0 IS HEAVILY CORRODED (C-CHECK) RO 3/25/2020 REMOVED CORROSION FROM INTERCOSTAL, FOUND TO BE OUT OF LIMITS. REMOVED OLD INTERCOSTAL, DRILLED, LOCATED , AND INSTALLED NEW INTERCOSTAL PER CRJ 200 SRM. DAIFeb 25, 2020 · N936SW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA2020032749502Nut Plate · broken15 BROKEN SHUR-LOK RUBBER ISOLATOR NUT PLATES ON THE FS 621 BULKHEAD (C-CHECK) RO 3/25/2020 REMOVED AND REPLACED 15 BROKEN SHUR-LOK RUBBER ISOLATOR NUTPLATES ON THE F.S. 621 BULKHEAD PER CRJ200 SRM.Feb 24, 2020 · N936SW · Cndair CL6002B19 · Fuselage Main, BulkheadSDR SWIA2020032749485Support Bracket · crackedCRACKED REAR PRESSURE BULKHEAD LINER SUPPORT BRACKET AT LBL 36 APPROX WL 112 (C-CHECK) RO 3/25/2020 REMOVED AND REPLACED LINER SUPPORT BRACKET ON REAR PRESSURE BULKHEAD AT LBL 36 APRROX WL 112 PER CRJ200 SRM.Feb 24, 2020 · N936SW · Cndair CL6002B19 · Fuselage Main, BulkheadSDR SWIA2020032749482Bulkhead · dentedDENT IN FORWARD FACE OF FS 621 BULKHEAD WEB APPROX LBL 14 WL 91 (C-CHECK) RO 3/25/2020 REPAIRED DENT IN FORWARD FACE OF F.S. 621 BULKHEAD WEB APPROX LBL14 WL 91 IAW BOMBARDIER REO. ACCOMPLISHED HFEC OF AFT PRESSURE BULKHEAD (DENTED AREA) LBL14 WL 91 NO DEFeb 24, 2020 · N936SW · Cndair CL6002B19 · Fuselage Main, BulkheadSDR SWIA2020032749494Seat Track · corrodedCORROSION FOUND ON SEAT RAILS ON FLOOR AT FS 569 LBL 9 (C-CHECK) RO 3/25/2020 REMOVED CORROSION ON FLOOR SEAT RAIL IN BETWEEN FS. 559.00 TO FS.559.00+16 LBL9. ORIGINAL FS.569 LBL9 FOUMD TO BE INCORRECT. ORIGINAL THICKNESS .110, REMOVED 0.030 FOUND TO BE OUFeb 23, 2020 · N936SW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR SWIA2020032749481Frame · corrodedCORROSION FOUND ON FRAME AT FS 605 STRG 20L TO STRG 19R FWD AND AFT (C-CHECK) RO 3/25/2020 BLENDED CORROSION ON FRAME AT FS 605 STR 20L TO 19R. FRAME 605 STR 21L TO 21R ORIGINAL THICKNESS IS .050, REMAINING IS .040 WITH TOTAL LOSS OF .010. FRAME IS OUT OF Feb 23, 2020 · N936SW · Cndair CL6002B19 · Fuselage Main, FrameSDR SWIA2020032749480Frame · corrodedCORROSION FOUND ON SRAME 589 AT FS 589 STGR R21-STRG L19 FWD AND AFT (C-CHECK) RO 3/25/2020 BLENDED CORROSION ON FRAME 589 STR 21R TO 19L. ORIGINAL THICKNESS IS .050, REMAINING IS .032 WITH TOTAL LOSS OF .018. REWORK WAS OUT OF LIMITS PER SRM. REMOVED AND Feb 23, 2020 · N936SW · Cndair CL6002B19 · Fuselage Main, FrameSDR SWIA2020032749493Seat Track · corrodedCORROSION FOUND ON FLOOR SEAT RAIL AT FS 386 RBL 9 (C-CHECK) RO 3/25/2020 REMOVED AND REPLACED CABIN SEAT TRACK RBL9 STATIONS FS. 364.00 TO FS. 399.00. / IAW CRJ 200 AMM/ SRM/ BOMBARDIER DRAWING. CALIBRATED TOOLING: TORQUE WRENCH AV7624 NOV. 2020/ DEPTHFeb 21, 2020 · N936SW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR SWIA2020032749492Fastener · corrodedDURING INSPECTION CORROSION WAS FOUND ON FLOOR SILL PANEL FASTENERS AT FS 280 - 283 LBL 43 (C-CHECK) RO 3/25/2020 REMOVED AND REPLACED 3 FASTENERS AT FS 280 - 283 LBL 43. RESTORED SURFACE FINISH.Feb 21, 2020 · N936SW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA2020032749491Cleat · corrodedCORROSION FOUND ON PASSENGER DOOR EXTREME FLOOR CLEATS ( 2 ) (C-CHECK) RO 3/25/2020 REMOVED AND REPLACED CORRODED PASSENGER DOOR ENTRANCE FLOOR CLEATS IAW CRJ 200 SRM.Feb 21, 2020 · N936SW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA2020032749490Fastener · corrodedCORROSION FOUND ON FLOOR SUPPORT FASTENER AT FS 349 LBL 39 (C-CHECK) RO 3/25/2020 REMOVED AND REPLACED FASTENERS AT F.S. 349 LBL 39 PER CRJ200 SRM.Feb 21, 2020 · N936SW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA2020032749489Seat Track · corrodedCORROSION FOUND ON FLOOR SEAT TRACK FS 409 + 10 - 409 + 42 RBL 9 (C-CHECK) RO 3/25/2020 REMOVED AND REPLACED SEAT TRACK AT RBL9 STATIONS FS. 399.00 TP FS. 409.00+128. IAW CRJ 200 AMM. BOMBARDIER DRAWING. CALIBRATED TOOLING: TORQUE WRENCH AV3967 JULY 2020Feb 21, 2020 · N936SW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR SWIA2020032749479Door Frame · corrodedCORROSION FOUND ON PASSENGER AFT DOOR FRAME AT FS 349 LBL 40 (C-CHECK) RO 3/25/2020 REMOVED (1) FASTENER TO ACCESS CORROSION AT FS 349 LBL 40. BLENDED OUT CORROSION I.A.W. REO.NDT PERFORMED FOUND NO DEFECTS. ORIGINAL THICKNESS: .160", MATERIAL REMOVED: .03Feb 21, 2020 · N936SW · Cndair CL6002B19 · Fuselage Main, StructureSDR SWIA2020032749478Support Fitting · crackedCRACK FOUND ON 280 SUPPORT CLIP AT FS 280 RBL 10 WL 72 (C-CHECK) RO 3/25/2020 REPLACED 280 SUPPORT CLIP IAW CRJ200 REO. CRJ200 REO.Feb 21, 2020 · N936SW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA2020032749477Support Fitting · crackedCRACKS FOUND ON 280 SUPPORT CLIP FS 280 LBL 11 WL 72 (C-CHECK) RO 3/25/2020 REPLACED 280 SUPPORT CLIP IAW CRJ200 REO. CRJ200 REO.Feb 21, 2020 · N936SW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA2020032749475Floor Support · corrodedCORROSION FOUND ON FASTENER SERVICE DOOR AFT FLOOR SUPPORT AT FS 349 RBL 42 (C-CHECK) RO 3/25/2020 REMOVED FASTENER FROM FLOOR SUPPORT, AFT OF SERVICE DOOR AT FS 349 RBL 42. BLENDED CORROSION ON FLOOR SUPPORT. NOMINAL 0.063, REMOVED 0.012, REMAINING 0.051.Feb 21, 2020 · N936SW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA2020032749474Support Bracket · corrodedCORROSION FOUND ON FLOOR SUPPORT BRACKET AT FS 280 LBL3 AND RBL3 (C-CHECK) RO 3/25/2020 REPLACED FLOOR SUPPORT BRACKET AT FS 280 IAW CRJ200 REO. CRJ200 REOFeb 21, 2020 · N936SW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA2020032749488Fastener · corrodedPAX DOOR CUTOUT-AREAS OF LIGHT CORROSION ALONG FLOOR SUPPORT ANGLE BETWEEN FS 310.00 AND FS 349.00 LBL 43 (C-CHECK) RO 3/25/2020 CLEANED AND REMOVED SURFACE CONTAMINATIONS. DAMAGE WAS FOUND TO BE CONTAINED WITHIN FASTENERS WITH NO MATERIAL LOSS TO SURROUNDFeb 19, 2020 · N936SW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA2020032749487Support Angle · corrodedSERVICE DOOR CUTOUT-AREAS OF LIGHT CORROSION ON FLOOR SUPPORT ANGLE BETWEEN FS 319.70 AND FS 349.00 RBL 43 (C-CHECK) RO 3/25/2020 REMOVED DOOR STOP FITTINGS FROM FLOOR SUPPORT ANGLE, BETWEEN FS 319.70 AND FS349. RBL 43. CORROSION BLEND IS OUTSIDE OF ALLOWAFeb 19, 2020 · N936SW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA2020032749486Floorbeam · corrodedREMOVABLE FLOOR BEAM THAT GOES OVER MAIN FEED MANIFOLD HAS EVIDENCE OF CORROSION (C-CHECK) RO 3/25/2020 REMOVED CORROSION ON FLOOR BEAM CAP STRIP FS 589 LBL9 TO RBL9, FOUND TO BE OUT OF LIMITS PER SRM. REMOVED CAP STRIP PER SRM. FABRICATED REPLACEMENT CAP Feb 19, 2020 · N936SW · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR SWIA2020032749500Vane · chafedLH INBD FLAP VANE IS CHAFFED ON L/E AT APPROX WS 95.0 (C-CHECK) RO 3/25/2020 REMOVED CHAFFE DAMAGE ON L/H, I/B FLAP VANE L/E AT W/S 95.0 PER CRJ-200 SRM. ORIGINAL MATERIAL THICKNESS IS 050". REMAINING THICKNESS IS .025". MATERIAL LOSS IS .025". AREA FFeb 18, 2020 · N936SW · Cndair CL6002B19 · Trailing Edge FlapsSDR SWIA2020032749499Vane · chafedLH INBD FLAP VANE IS CHAFFED ON L/E AT APPROX WS 55.0 (C-CHECK) RO 3/25/2020 REMOVED CHAFFE DAMAGE ONE L/H, I/B FLAP VANE L/E AT APPROX W/S 55.0. PER CRJ-200 SRM 51-12-00. ORIGINAL MATERIAL THICKNESS IS .050". REMAINING THICKNESS IS .023". MATERIAL LOSSFeb 18, 2020 · N936SW · Cndair CL6002B19 · Trailing Edge FlapsSDR SWIA2020032749498Vane · chafedRH INBD FLAP VANE IS CHAFFED ON L/E AT APPROX WS 95. (C-CHECK) RO 3/25/2020 REMOVED CHAFFE DAMAGE ON R/H, I/B FLAP VANE L/E AT APPROX W/S 95.0 PER CRJ-200 SRM. ORIGINAL MATERIAL THICKNESS IS .050". REMAINING THICKNESS IS .025". MATERIAL LOSS IS .025". Feb 18, 2020 · N936SW · Cndair CL6002B19 · Trailing Edge FlapsSDR SWIA2020032749497Vane · chafedRH INBD FLAP VANE IS CHAFFED ON L/E AT APPROX WS 141.0 (C-CHECK) RO 3/25/2020 REMOVED CHAFFE DAMAGE ON R/H, I/B FLAP VAN L/E AT APPROX W/S 141.0 PER CRJ-200 SRM-200 51-12-00. ORIGINAL MATERIAL THICKNESS IS .050". REMAINING MATERIAL THICKNESS IS .024". MAFeb 18, 2020 · N936SW · Cndair CL6002B19 · Trailing Edge FlapsSDR SWIA2019052845923Reservoir · defectiveGEAR DISAGREE WARNING. LEFT MAIN LANDING GEAR SLOW. COMPLIED WITH QRH GEAR DISAGREE. (FLT#3587) CLOSED REMOVED AND REPLACED RESERVOIR. PERFORMED FULL GEAR SWINGS, IAW AMM. NO DEFECTS NOTED.May 28, 2019 · N936SW · Cndair CL6002B19 · Landing Gear Retraction/Extension SystemSDR SWIA2019012945477Actuator · slowGEAR DISAGREE MESSAGE ON GEAR RETRACTION. LEFT MAIN SLOW TO RETRACT. MESSAGE WAS ILLUMINATED ONLY FOR A FEW SECONDS. (FLT 7359) CLOSED REMOVED AND REPLACED LEFT MLG SIDESTAY ACTUATOR IAW AMM. SYSTEM OPS CHECKS GOOD NO FURTHER FAULTS NOTED.Jan 29, 2019 · N936SW · Cndair CL6002B19 · Landing Gear ActuatorSDR SWIA201845187None · noneOUTBOUND PILOT REPORTS A DENT IN THE RT. WING LEADING EDGE DUE TO A BIRD STRIKE. FLIGHT # 7389 FO: 10/29/2018. CLOSED REMOVED AND REPLACED RT O/B LEADING EDGE SKIN IAW SRM.Oct 25, 2018 · N936SW · Cndair CL6002B19 · Standard Practices/StructuresSDR SWIA201437543Lamp · burned outLEFT CENTER OVER WING EXTERIOR EMERGENCY LIGHT IS BURNED OUT, REPLACED THE LAMP.May 13, 2014 · N936SW · Cndair CL6002B19 · Emergency LightingSDR SWIA201436790Lamp · burned outNR 3 EMERGENCY OVERHEAD LIGHT IS BURNED OUT, REPLACED LAMP.Mar 21, 2014 · N936SW · Cndair CL6002B19 · Emergency LightingSDR SWIA201436744Vane · chafedRIGHT INBD FLAP VANE L/E CHAFED. BLENDED FLAP VANE IAW REO.Mar 3, 2014 · N936SW · Cndair CL6002B19 · Trailing Edge FlapsSDR SWIA201436743Vane · chafedLEFT INBD FLAP VANE CHAFED. BLENDED FLAP VANE IAW REO.Mar 3, 2014 · N936SW · Cndair CL6002B19 · Trailing Edge FlapsSDR SWIA201436742Vane · chafedLEFT INBD FLAP VANE CHAFED. BLENDED FLAP VANE IAW REO.Mar 3, 2014 · N936SW · Cndair CL6002B19 · Trailing Edge FlapsSDR SWIA201436741Vane · chafedLEFT INBD FLAP VANE CHAFED AT FLAP. BLENDED FLAP VANE IAW REO.Mar 3, 2014 · N936SW · Cndair CL6002B19 · Trailing Edge FlapsSDR SWIA201436740Attach Angle · crackedANGLE ON OTBD END OF INTERCOSTAL CRACKED BS 621. REPLACED INTERCOSTAL ANGLE IAW SRM.Mar 3, 2014 · N936SW · Cndair CL6002B19 · Fuselage Main, Attach FittingsSDR SWIA201436739Intercostal · crackedCRACK IN INTERCOSTAL AFT OTBD CORNER AT LT AFT SIDE OF BS 621, REPLACED INTERCOSTAL IAW SRM.Mar 3, 2014 · N936SW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA201436746Hinge · gougedPAX DOOR HINGE GOUGED. BLENDED HINGE IAW REO.Mar 2, 2014 · N936SW · Cndair CL6002B19 · Fuselage, Door HingeSDR SWIA201436745Floor Support · corrodedCORROSION ON RT FLOOR SUPPORT. BLENDED CORROSION IAW SRM AND REO.Mar 2, 2014 · N936SW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA201436520Light · inoperative3RD OVERHEAD EMERGENCY LIGHT IS BURNED OUT. FLT 5540 RELAMPED.Feb 27, 2014 · N936SW · Cndair CL6002B19 · Emergency LightingSDR SWIA201334202Light · inoperativeNR 2 OVERHEAD EMERGENCY LIGHT IS BURNED OUT. FLT#5228 RELAMPED.Aug 12, 2013 · N936SW · Cndair CL6002B19 · Emergency LightingSDR SWIA201334045Light · inoperativeOVERHEAD EMERGENCY LIGHT ROW 5 IS BURNED OUT. FLT#6204 RELAMPED.Jul 19, 2013 · N936SW · Cndair CL6002B19 · Emergency LightingSDR SWIA201333696Tire · failedRT NOSE TIRE BLOWN AT 140 KTS. REPLACED LEFT AND RIGHT NOSE TIRE ASSEMBLY IAW AMM.Jun 13, 2013 · N936SW · Cndair CL6002B19 · TireSDR SWIA201333501Light · inoperativeFORWARD SECTION OF EMERGENCY LIGHTS DO NOT ILLUMINATE. RELAMPED.May 15, 2013 · N936SW · Cndair CL6002B19 · Emergency LightingSDR SWIA201332823Light · inoperativeNR 1 EMERGENCY OVERHEAD LIGHT BURNED OUT. (FLT 5337) RELAMPED EMERGENCY LIGHT.Feb 15, 2013 · N936SW · Cndair CL6002B19 · Emergency LightingSDR SWIA201232449Light · inoperativeNR 1 EMERGENCY OVERHEAD LIGHT BURNED OUT. (SERVICE) RELAMPED EMERGENCY LIGHT.Dec 25, 2012 · N936SW · Cndair CL6002B19 · Emergency LightingSDR SWIA201232174Uplock · failedGEAR DISAGREE UPON GEAR RETRACTION. (FLT 5633) REPLACED LEFT MLG UPLOCK ASSEMBLY IAW AMM.Nov 18, 2012 · N936SW · Cndair CL6002B19 · Landing Gear Retraction/Extension SystemSDR SWIA201232102Light · inoperativeAFT EMERGENCY FLOOD LIGHT BURNED OUT. (FLT 6473) RELAMPED EMERGENCY LIGHT.Nov 4, 2012 · N936SW · Cndair CL6002B19 · Emergency LightingSDR SWIA201232016Bypass Valve · failedSELECTED GEAR DOWN AND RECEIVED GEAR DISAGREE MESSAGE. MAIN GEAR SHOWING UP AND NOSE GEAR DOWN. (FLT 6362) REPLACED THE MLG RUNAROUND BYPASS VALVE, MLG SELECTOR VALVE, RIGHT MLG UPLOCK ASSEMBLY IAW AMM. P/N: 750004000-003 S/N OFF: 1110A, P/N OFF: 750005000Oct 19, 2012 · N936SW · Cndair CL6002B19 · Landing Gear Retraction/Extension System
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