N913SW, cancelled Jan 24, 2023

Service difficulty reports · 215

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 = 'N913SW' AND deregistration_id = 'N913SW-2023-01-24'
  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 SWIA202049252Unknown · fireCREATED FROM FORWARD DISCREPANCY. PLEASE REFERENCE AML 397685, WHEN AIRCRAFT WAS BEING REPOSITIONED FROM TERMINAL TO HANGAR FOR MX, APU WAS STARTED AND AS SOON AS THE APU GENERATOR WAS SELECTED ON A POPPING AND HISSING NOISES WERE HEARD FROM BEHIND AND A FIRE Mar 11, 2020 · N913SW · Cndair CL6002B19 · Flight Compartment EquipmentSDR SWIA2020031049250Post · crackedCOMPLY WITH FORM 337 FOR FS409+128 VERTICAL POST CRACKED AT INBOARD LOWER AFT RIVET IN RADIUS AT LBL27. CLASIFIED AS MAJOR REPAIR. (AGING A/C INSP - RO 3/7/2020) COMPLETED FORM M-337 FOR REPAIR AT FS409+128 VERTICAL POST AT LB27.Feb 22, 2020 · N913SW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA2020031049249Post · crackedCOMPLY WITH FORM 337 FOR FS409+128 VERTICAL POST CRACKED AT OUTBOARD LOWER AFT RIVET IN RADIUS AT LBL18. CLASIFIED AS MAJOR REPAIR. (AGING A/C INSP - RO 3/7/2020) COMPLETED FORM M-337 FOR REPAIR AT FS409+128 VERTICAL POST AT LBL18.Feb 22, 2020 · N913SW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA2020031049102Post · cracked***** MAJOR ***** FS409+128 VERTICAL POST CRACKED AT OUTBOARD LOWER AFT RIVET IN RADIUS AT LBL18. (AGING AC INSP - RO 3/7/2020) REPAIRED FS409+128 VERTICAL POST CRACKED AT OUTBOARD LOWER AFT RIVET IN RADIUS AT LBL18 IAW REO.Feb 20, 2020 · N913SW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA2020031049099Post · cracked***** MAJOR ***** FS409+128 VERTICAL POST CRACKED AT INBOARD LOWER AFT RIVET IN RADIUS AT LBL27. (AGING AC INSP - RO 3/7/2020) REPAIRED FS409+128 VERTICAL POST CRACKED AT INBOARD LOWER AFT RIVET IN RADIUS AT LBL27 IAW REO.Feb 20, 2020 · N913SW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA2019061145973Control Handle · failedAFTER TAKEOFF, THE LANDING GEAR FAILED TO RETRACT; FOLLOWED BY A/SKID INBD AND PARK BRAKE SOV CAUTION MESSAGES. RETURNED TO FIELD. (FLT#5399) REMOVED AND REPLACED LANDING GEAR CONTROL HANDLE ASSY IAW AMM. PERFORMED LANDING GEAR EXTENSION AND RETRACTION SEVERALJun 11, 2019 · N913SW · Cndair CL6002B19 · Landing Gear SelectorSDR SWIA2019405065827Servo Valve · failedSTEERING INOP CAUTION IN FLIGHT. COMPLIED WITH QRH. (FLT#5311) CLOSED REMOVED AND REPLACED SERVO VALVE IAW AMM.May 6, 2019 · N913SW · Cndair CL6002B19 · Landing Gear Steering SystemSDR SWIA2018110245220Skin · dentedA DENT WAS FOUND ON THE RT INBD FLAP LOWER SKIN. REPAIRED THE SKIN IAW SRM 57-52-00.Oct 19, 2018 · N913SW · Cndair CL6002B19 · Trailing Edge FlapsSDR SWIA2018110245222Frame · corrodedBS 605 FRAME FOUND CORRODED. REMOVED AND REPLACED THE ENTIRE FRAME SECTOR IAW SRM 51-42-06.Oct 8, 2018 · N913SW · Cndair CL6002B19 · Fuselage Main, FrameSDR SWIA2018110245219Floor Support · corrodedRIGHT FLOOR SUPPORT CORRODE AT BS 559. REMOVED AND REPLACED IAW SRM 51-42-06.Oct 7, 2018 · N913SW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA2018110245218Floor Support · corrodedFLOOR SUPPORT CORRODED AT BS 559. REMOVED AND REPLACED IAW SRM 51-42-06.Oct 7, 2018 · N913SW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA2018110245217Floorbeam · corrodedCOCKPIT FLOORBEAM, BS 280 WAS CORRODED. REMOVED AND REPLACED THE COCKPIT FLOORBEAM ANGLE.Oct 6, 2018 · N913SW · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR SWIA2018110245216Vane · gougedRIGHT INBOARD FLAP VANE WAS GOUGED. REPAIRED IAW SRM 51-21-06.Oct 5, 2018 · N913SW · Cndair CL6002B19 · Trailing Edge FlapsSDR SWIA2018110245215Vane · wornLEFT OUTBOARD FLAP, OUTBOARD VANE MOUNT STRUCTURE WAS WORN. MEASURED REMAINING MATERIAL AND FOUND WITHIN LIMITS IAW REO 601R-57-53-195.Oct 5, 2018 · N913SW · Cndair CL6002B19 · Trailing Edge FlapsSDR SWIA2018110245221Stringer Splice · crackedSTRINGER SPLICE WAS CRACKED AT ITS ATTACH POINT TO PASSENGER DOOR UPPER SILL, BS 379. REPAIRED THE STRINGER SPLICE IAW SRM 53-00-03.Oct 4, 2018 · N913SW · Cndair CL6002B19 · Fuselage Main, Longeron/StringerSDR SWIA2018110245214Strap · corrodedCORROSION FOUND ONTHE CIRCUMFERENTIAL STRAP BELOW FRAME BS 333. BLENDED THE STRAP IAW SRM 51-21-06.Oct 4, 2018 · N913SW · Cndair CL6002B19 · Fuselage Main, StructureSDR SWIA2018110245213Bracket · corrodedCORROSION FOUND ON THE BRACKET ATTACHED TO FRAME AT BS 319. REMOVED AND REPLACED THE BRACKET IAW SRM 51-42-21.Oct 4, 2018 · N913SW · Cndair CL6002B19 · Fuselage Main, Attach FittingsSDR SWIA2018110245212Frame · corrodedCORROSION FOUND ON THE FWD AND AFT FACES OF THE FRAME AT BS 333. REMOVED THE CORROSION IAW SRM 51-21-06.Oct 4, 2018 · N913SW · Cndair CL6002B19 · Fuselage Main, FrameSDR SWIA2018110245211Hinge · chafedSERVICE DOOR INTERIOR HINGE CHAFED. REMOVED AND REPLACED THE SERVICE DOOR HINGE PLATE IAW SRM 51-41-21. OPS CHECKED GOODOct 4, 2018 · N913SW · Cndair CL6002B19 · Fuselage, Door HingeSDR SWIA2018110245210Panel · gougedPANEL 326CR GOUGED. REPAIRED THE PANEL IAW REO 601R-55-32-384.Oct 4, 2018 · N913SW · Cndair CL6002B19 · Standard Practices/StructuresSDR SWIA2018110245209Skin · corrodedCORROSION FOUND ON THE INNER SKIN, AROUND FORWARD AND AFT ACCESS DOOR CUT-OUTS. REMOVED AND REPLACED THE PAX DOOR SKIN IAW SRM 51-42-06.Oct 3, 2018 · N913SW · Cndair CL6002B19 · Passenger/Crew DoorsSDR SWIA2018110245208Skin · chafedRIGHT HORIZONTAL STAB PANEL WAS CHAFED ON THE INNER SKIN. R & R THE SKIN PANEL IAW SRM 51-12-00.Oct 3, 2018 · N913SW · Cndair CL6002B19 · Horizontal Stabilizer, Plate/SkinSDR SWIA2018110245207Skin · chafedLEFT ELEVATOR SKIN PANEL WAS CHAFED. REPAIRED THE DAMAGE IAW SRM 51-12-00.Oct 3, 2018 · N913SW · Cndair CL6002B19 · Elevator, Plate/SkinSDR SWIA2018110245206Skin Panel · chafedLEFT WING SKIN PANEL WAS CHAFED. BLENDED THE PANEL IAW SRM 51-41-02.Oct 3, 2018 · N913SW · Cndair CL6002B19 · Wing, Plate/SkinSDR SWIA2018110245205Skin · chafedLEFT NACELLE SKIN PANEL WAS CHAFED AT MULTIPLE PLACES. REMOVED AND REPLACED THE SKIN IAW SRM 51-42-06.Oct 3, 2018 · N913SW · Cndair CL6002B19 · Nacelle/Pylon, Plate/SkinSDR SWIA2018110245204Cover · nickedTWO NICKS FOUND JUST AFT OF GROUND AIR LOW PRESSURE COVER. COMPLIED WITH PERMANENT REPAIR OF THE AREA IAW REO 601R-53-61-6734.Oct 2, 2018 · N913SW · Cndair CL6002B19 · Fuselage Main, StructureSDR SWIA2018110245203Skin · dentedA DENT WAS FOUND ON THE CARGO DOOR SKIN, AT THE BOTTOM CORNER. REPAIRED THE CARGO DOOR SKIN IAW REO 601R-52-31-299.Oct 2, 2018 · N913SW · Cndair CL6002B19 · Cargo/Baggage DoorsSDR SWIA2018110245202Structure · dentedA DENT WAS FOUND ON THE AFT FUSELAGE TAIL. REPAIRED.Oct 2, 2018 · N913SW · Cndair CL6002B19 · Fuselage Main, StructureSDR SWIA2018110245201Skin · dentedA DENT WAS FOUND AFT AND ABOVE THE LT ACM EXHAUST OPENING. REPAIRED THE DENT IAW REO 601R-51-00-309.Oct 2, 2018 · N913SW · Cndair CL6002B19 · Fuselage Main, Plate/SkinSDR SWIA2018110245200Skin · dentedTWO SMALL DENTS FOUND ON THE RT FUSELAGE BETWEEN BS 589 TO 605. REPAIRED IAW REO 601R-53-61-6734.Oct 2, 2018 · N913SW · Cndair CL6002B19 · Fuselage Main, Plate/SkinSDR SWIA2018110245199Skin · dentedA DENT WAS FOUND ON THE RT BOTTOM FUSELAGE JUST OUTBOARD FROM NLG. REPAIRED IAW REO 601R-53-11-3333.Oct 2, 2018 · N913SW · Cndair CL6002B19 · Fuselage Main, Plate/SkinSDR SWIA2018080744974Skin · damagedFOUND ELONGATED DAMAGED SCREW HOLE UNDER THE LT MLG ACCESS PANEL ADJACENT TO THE MLG OPENING. BETWEEN LT WS 53.60 - 65.75. REPAIRED WING PLANK IAW REO.Jul 30, 2018 · N913SW · Cndair CL6002B19 · Wing, Plate/SkinSDR SWIA2018051744638Engine · flamed outCAPTAIN REPORTED THAT DURING APPROACH, RECEIVED A RT MAIN EJECTOR AND RT SCAVENGE EJECTOR CAUTION MESSAGES AND RIGHT AFTER TOUCH DOWN THE RT ENGINE FLAMED OUT. ENGINE SHUT DOWN AFTER THRUST REVERSER ACTIVATION. REMOVED AND REPLACED THE RT ENGINE ASSY IAW AMMay 6, 2018 · N913SW · Cndair CL6002B19 · Engine (Turbine/Turboprop)SDR SWIA201642644Stringer · damagedDAMAGE TO STR 0 BETWEEN BS 409+80 AND 409.00+96. REMOVED AND INSTALLED THE STRINGER IAW SRM.Sep 16, 2016 · N913SW · Cndair CL6002B19 · Fuselage Main, Longeron/StringerSDR SWIA201642643Stringer · damagedDAMAGE TO STRINGER 16R BETWEEN BS 409 - 409 + 32. REMOVED AND REPLACED THE STRINGER IAW SRM.Sep 16, 2016 · N913SW · Cndair CL6002B19 · Fuselage Main, Longeron/StringerSDR SWIA201642648Vane · chafedRIGHT FLAP VANE OTBD LEADING EDGE IS CHAFED. REMOVED AND REPLACED THE FLAP VANE OTBD LEADING EDGE IAW SRM.Sep 10, 2016 · N913SW · Cndair CL6002B19 · Trailing Edge FlapsSDR SWIA201642647Vane · chafedRIGHT FLAP VANE CENTER OF LEADING EDGE IS CHAFED. REMOVED AND REPLACED THE FLAP VANE CENTER LEADING EDGE IAW SRM.Sep 10, 2016 · N913SW · Cndair CL6002B19 · Trailing Edge FlapsSDR SWIA201642646Vane · chafedRIGHT FLAP VANE INBD LEADING EDGE IS CHAFED. REMOVED AND REPLACED THE FLAP VANE INBD LEADING EDGE IAW SRM.Sep 10, 2016 · N913SW · Cndair CL6002B19 · Trailing Edge FlapsSDR SWIA201642645Vane · chafedLEFT FLAP VANE INBD LEADING EDGE IS CHAFED. REMOVED AND REPLACED LT FLAP VANE INBD LEADING EDGE IAW SRM.Sep 10, 2016 · N913SW · Cndair CL6002B19 · Trailing Edge FlapsSDR SWIA201440370Skin · gougedBS 627, OTBD OF STRINGER 4L, TWO GOUGES ON SKIN. REPAIRED IAW EADec 6, 2014 · N913SW · Cndair CL6002B19 · Fuselage Main, Plate/SkinSDR SWIA201440379Panel · crackedPANEL 221BLC CRACKED AND MISSING 6 EA SPACERS. REPAIRED CRACKED PANEL IAW EA AND SRM.Dec 4, 2014 · N913SW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA201440388Door · chafedRIGHT MLG DOOR HAS CHAFE ON AFT EDGE THRU INNER SKIN NEAR BRUSH. RT MLG DOOR WORKED IAW STS EA COMPLIED WITH STEPS 1 THRU END, IAW SRM, REPAIR COMPLETED. THIS IS A PERMANANT REPAIR.Nov 29, 2014 · N913SW · Cndair CL6002B19 · Landing Gear DoorsSDR SWIA201440384Vane · damagedLT INBD FLAP VANE CENTER CAP FOUND TO BE OUT OF LIMITS. R & R LT INBD FLAP VANE CENTER L/E SKIN, CAP, IAW SRM AND DWG 601R14303, REV J.Nov 25, 2014 · N913SW · Cndair CL6002B19 · Trailing Edge FlapsSDR SWIA201440390Seat Track · corrodedSEAT TRACK RBL9 FS 559+86 TO 559+112 CORRODED. REPLACED THE SEAT TRACK IAW AMM AND REO.Nov 24, 2014 · N913SW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR SWIA201440382Pressure Panel · crackedPRESSURE FLOOR CRACKED IN 2 PLACES AT FS 460 OTBD OF LBL 0.0 AND RBL 0.0. COMPLIED WITH REPAIR OF PRESSURE FLOOR 2 PLACES AT FS 460 OTBD OF BL 0.0. RT & LT SIDES REF REO. PRESSURE LEAK CHECK GOOD. COMPLIED WITH ST CARD LEAK CHECK GOOD. MATERIAL REMOVED WEINov 24, 2014 · N913SW · Cndair CL6002B19 · Fuselage Floor PanelSDR SWIA201440380Lever · wornPAX DOOR PULL IN LEVER IS WORN. REPAIRED THE PASSENGER DOOR PULL IN LEVER IAW REO.Nov 24, 2014 · N913SW · Cndair CL6002B19 · Passenger/Crew DoorsSDR SWIA201440378Fairing · damagedLEFT HORIZONTAL TIP FAIRING 333AL HAS MULTIPLE ELONGATED HOLES. REPAIRED IAW EA.Nov 24, 2014 · N913SW · Cndair CL6002B19 · Horizontal Stabilizer StructureSDR SWIA201440377Door Sill · corrodedLEFT CARGO DOOR SILL HAS CORROSION AROUND NUTPLATE HOLES FS 574 TO 621. C-CHECK, RO 12/10/14, BLENDED LT CARGO DOOR SILL CORROSION AROUND NUTPLATE HOLES FS 574 TO 621 REF SRM , BLEND OUT OF LIMITS. R & R LT CARGO DOOR SILL REF SRM & REO.Nov 24, 2014 · N913SW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA201440371Bulkhead · damagedFWD FACE OF FS 621 REAR PRESSURE BULKHEAD HAS SCREW STRIKES BETWEEN ISOLATOR MOUNTS AS MARKED. C-CHECK, RO 12/10/14. BLENDED SEVERAL AREAS OF SCREW NICKS ON FS 621 AT ISOLATOR MOUNTS REF SRM. FOUND TO BE WITHIN LIMITS REF REO.Nov 24, 2014 · N913SW · Cndair CL6002B19 · Fuselage Main, BulkheadSDR SWIA201440369Trunnion · damagedFOUND AN OVERSIZED HOLE ON LT TRUNNION. REPAIRED THE LT TRUNION IAW REO.Nov 24, 2014 · N913SW · Cndair CL6002B19 · Fuselage, Landing Gear Attach Fittings
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