N866AS, cancelled Jul 30, 2023
Service difficulty reports · 165
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 = 'N866AS' AND deregistration_id = 'N866AS-2023-07-30' 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 = 'N866AS' AND deregistration_id = 'N866AS-2023-07-30' 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 SWIA2019111246758Pressure Switch · failedABORTED TAKE OFF. LOW FUEL PRESSURE CAUTION MSG. FLT OR GROUND SPOILER MASTER CAUTION WARNING. BRAKE TEMPS LEFT 3/2 RIGHT 3/2. BELOW 80 KIAS. FLIGHT # 5037 CLOSED FOR THE LOW FUEL PRESSURE CAUTION MSG. MXC CONFIRMED WITH THE CREW THAT IT WAS A LH LOW FUEL PSDR SWIA2018111345262Frame · corrodedFS589.00, STGR27 AND STGR26R €“ FRAME SHOWS SIGNS OF CORROSION ON THE FWD SIDE. (C-CHECK) RO: 11/12/2018REPLACED CORRODED FRAME SECTION AT FS 589.00 @STGR 20L IAW REO. PRESSURE LEAK CHECK GOOD.SDR SWIA2018111345258Bulkhead Web · crackedFS.280.00 LOWER WEB HAS CRACKS AT LBL9 AND RBL9. (C-CHECK) RO: 11/12/2018 COMPLIED WITH REPAIR OF THE FS280 BULKHEAD WEB. PERFORMED ALL STEPS IAW REO.SDR SWIA2018111345261Stringer · crackedCLIP ON THE UPPER SIDE OF STGR3L, FS282.00 IS CRACKED. (C-CHECK) RO: 11/12/2018 REMOVED AND INSTALLED NEW CLIP ON THE UPPER SIDE OF STGR3L, FS282.00. IAW SRM. PRESSURE LEAK CHECK GOOD.SDR SWIA2018111345260Doubler · corrodedCORROSION ON DOUBLER FOR THE PASSENGER DOOR LOWER SILL FS349.00. (C-CHECK) RO: 11/12/2018 REMOVED CORROSION FROM DOUBLER LOCATED UNDER FLOOR SILL JUST AFT OF PAX DOOR CUTOUT IAW SRM.SDR SWIA2018111345259Skin · dentedDENT IN FUSELAGE SKIN AT FS639.00 JUST BELOW STGR2R. (C-CHECK) RO: 11/12/2018 DRESSED BACK DENT IN FUSELAGE SKIN AT FS639.00 JUST BELOW STGR2R IAW REO.SDR SWIA201844132Bracket · failedGEAR DISAGREE NOSE GEAR WOULD NOT RETRACT. (FLT#2944) CLOSED REMOVED AND REPLACED BRACKET IAW AMM. SWUNG GEAR OPS GOOD.SDR SWIA201744067Bracket · damagedNOSE GEAR DISAGREE. REMOVED AND REPLACED THE NR 2 WOW AND CENTERED HARNESS ASSY IAW AMM. OPS CHECKED GOOD. REMOVED AND REPLACED CENTERING SENSOR BRACKET IAW CMM. OPS CHECKED GOOD.SDR SWIA201743582Control Unit · failedFLAP FAIL, RETURNED TO THE FIELD. EMERGENCY DECLARED. REPLACED THE FLAP LEVER AND FECU. AND RERIGGED THE RIGHT BPSU. SYSTEM OP CHECKS GOOD.SDR SWIA201743256Carbon Seal · leakingSMOKE IN THE COCKPIT AND A SMOKE CARGO WARNING MESSAGE. DIVERTED. REMOVED AND REPLACED THE NR 1 CARBON SEAL. LEAK CHECKED AND OIL CONSUMPTION CHECKED GOOD.SDR SWIA2017050243256Unknown · smokeSMOKE IN COCKPIT AND SMOKE CARGO WARNING MESSAGE, DIVERTED. OPEN.SDR SWIA201642833Panel · chafedPANEL 684BB CHAFED ON FWD EDGE. REPAIRED IAW EA.SDR SWIA201642831Plate · crackedCARGO SKIN PROTECTIVE PLATE HAS CRACKS AROUND FASTENER HOLES. ( LOCATED & DRILLED HOLES ON NEW CARGO PROTECTIVE PLATE IAW SRM.SDR SWIA201642832Skin · wornRIGHT NACELLE CORE COWL HAS WEAR AT LATCH AREA CAUSED BY BLOCKER DOOR. FABRICATED AND INSTALLED REPAIR PLATE IAW CMM. BLENDED NR 6 BLOCKER DOOR TO OBTAIN THE CORRECT CLEARENCE IAW CMM, CLEARANCE CHECKED GOOD.SDR SWIA201541442Landing Gear · malfunctionedGEAR DISAGREE MESSAGE WITH WOW MESSAGE. RETURNED TO DEPARTURE. SERVICED NLG, BLED SYSTEM. OPS CHECKED GOOD.SDR SWIA201541008Warning Message · false activation"RT REV UNLOCKED" CAUTION MSG IN FLIGHT. COMPLIED WITH QRH PROCEDURE ON EMER1-16, LANDED NEAREST SUITABLE AIRPORT. TROUBLESHOT RIGHT THRUST REVERSER UNLOCK MESSAGE DURING FLIGHT IN REFERENCE TO FIM, CHECK FOR GROUND ONTHROTTLE LOCKOUT GEARBOX SOLENOID, NO DSDR SWIA201439820Tube · damagedSERVICE DOOR CONVOLEX DAMAGED. C-CHECK, R & R CONVOLEX TUBING WITH NEW, IAW REO.SDR SWIA201439879Piccolo Tube · chafedLEFT WING OTBD PICCOLO TUBE HAS CHAFING FROM L/E RIB BETWEEN 530JZ AND 530KZ. C-CHECK, REPAIRED CHAFE ON OTBD PICCOLO TUBE IAW STS EA.SDR SWIA201439878Piccolo Tube · damagedLT WING OTBD PICCOLO TUBE HAS DRILL START 38.5" FROM OTBD EDGE. C-CHECK, CLEANED AND WELDED DRILL START IAW STS EA.SDR SWIA201439877Piccolo Tube · dentedLT WING OTBD PICCOLO TUBE HAS A DENT 38.5" FROM OTBD EDGE. C-CHECK, REPAIRED DENT IN OTBD PICCOLO TUBE IAW STS EA.SDR SWIA201439876Piccolo Tube · gougedLEFT WING OTBD PICCOLO TUBE HAS GOUGE NEAR WELD AT INBD FLANGE. C-CHECK, REPAIRED GOUGE ON INBD FLANGE IAW STS EA.SDR SWIA201439875Skin · gougedFUSELAGE SKIN, LOWER FORWARD AREA, RT LOWER DME ANTENNA FOOT PRINT HAS A MINOR GOUGE. C-CHECK, REPAIRED LWR FUSELAGE BETWEEN FS 409.0+48 & 409.00+64, S25R-S26R IAW STS EA.SDR SWIA201439874Skin · gougedON FUSELAGE SKIN LOWER FORWARD AREA, LT LOWER DME ANTENNA FOOT PRINTS HAS MINOR GOUGES 2 LOCATIONS. C-CHECK, REPAIRED LWR FUSELAGE BETWEEN FS 409.0+48 & 409.00+64, S25L-S26L IAW STS EA.SDR SWIA201439873Skin · nickedFWD LOWER CORNER OF PAX DOOR CUT OUT HAS NICKS. C-CHECK, BLENDED FWD LOWER CORNER FUSELAGE SKIN AT PAX DOOR CUT OUT TO A SMOOTH FINISH, IAW STS EA.SDR SWIA201439872Hinge · gougedPAX DOOR MOUNTED PIANO HINGE HALF HAS WEAR GROOVES AND GOUGES ON LUGS 12 LOCATIONS SEEN WITH DOOR OPENED AND CLOSED. BLENDED DAMAGED AREA TO A SMOOTH FINISH, IAW REO.SDR SWIA201439871Hinge · gougedFUSELAGE MOUNTED PAX DOOR PIANO HINGE HALF HAS A GOUGE ON LUG, 6TH FROM AFT END. C-CHECK, BLENDED DAMAGED AREA TO A SMOOTH FINISH, IAW REO.SDR SWIA201439870Floor Support · corrodedRIGHT FUSELAGE FLOOR ANGLE HAS CORROSION AT FS529.00, RBL 47. C-CHECK, CORROSION ON RT FLOOR ANGLE AT FS 529.00, RBL 47, WAS BLENDED IAW REO.SDR SWIA201439869Floor Support · corrodedRIGHT FUSELAGE FLOOR ANGLE HAS CORROSION AT FS 499 TO 513, RBL 47. C-CHECK, CORROSION ON RT FLOOR ANGLE AT FS 499 TO FS 513, RBL 47, WAS BLENDED IAW REO.SDR SWIA201439868Floor Support · corrodedRIGHT FUSELAGE FLOOR ANGLE HAS CORROSION AT FS 473.15 RBL 47. REMOVED CORROSION BY BLENDING IAW REO.SDR SWIA201439867Floor Support · corrodedRIGHT FUSELAGE FLOOR ANGLE HAS CORROSION AT FS 461, RBL 47. BLENDED OUT CORROSION IAW REO.SDR SWIA201439866Floor Support · corrodedRIGHT FUSELAGE FLOOR ANGLE HAS CORROSION AT FS449.85, RBL 47. C-CHECK CORROSION ON RIGHT FLOOR ANGLE AT FS 449.85, RBL 47, WAS BLENDED IAW REO.SDR SWIA201439865Floor Support · corrodedLEFT FUSELAGE FLOOR ANGLE HAS CORROSION AT FS 544, LBL47. C-CHECK, BLENDED CORROSION IAW REO.SDR SWIA201439864Floor Support · corrodedLEFT FUSELAGE FLOOR ANGLE HAS CORROSION AT AFT SIDE OF FS 513. C-CHECK, CORROSION ON LEFT FLOOR ANGLE AFT OF FS 513 WAS BLENDED IAW REO.SDR SWIA201439863Floor Support · corrodedLEFT FLOOR ANGLE HAS CORROSION AT FS499 TO 513 LBL47. C-CHECK, CORROSION ON LT FLOOR ANGLE FS 499-FS 513 AT LBL 47 WAS BLENDED IAW REO.SDR SWIA201439862Floor Support · corrodedLEFT FUSELAGE FLOOR ANGLE CORRODED AT FS461, LBL 47. C-CHECK, REMOVED CORROSION ON LT FUSELAGE FLOOR ANGLE AT FS 461, LBL47 IAW REO.SDR SWIA201439861Floor Support · corrodedLEFT FUSELAGE FLOOR ANGLE CORRODED AT BS 449.85, LBL 47. REMOVED CORROSION BY BLENDING IAW REO.SDR SWIA201439840Seat Track · corrodedLEFT FUSELAGE SEAT TRACK CORRODED AT BS 559+112 LBL 9. REPLACED THE SEAT TRACK IAW REO.SDR SWIA201439839Seat Track · corrodedRT FUSELAGE SEAT TRACK CORRODED BS 559+80 - 559+96. R & R THE SEAT TRACK SECTION IAW REO.SDR SWIA201439838Seat Track · corrodedLEFT FUSELAGE SEAT TRACK CORRODED AT BS 559+80 - 559+96 LBL 9. R & R THE SEAT TRACK SECTION IAW REO.SDR SWIA201439837Seat Track · corrodedLEFT FUSELAGE SEAT TRACK CORRODED AT BS 612 - 617 LBL 9. R & R THE SEAT TRACK SECTION, IAW REO AND SRM.SDR SWIA201439836Floor Support · corrodedRT FUSELAGE FLOOR SUPPORT IS CORRODED AROUND NUTPLATE HOLE BS 605 - 621. REMOVED CORROSION IAW REO.SDR SWIA201439835Floor Support · corrodedRT FLOOR SUPPORT BS 559+80 - 559+112 IS CORRODED. CORROSION WAS BLENDED AND FOUND WITHIN LIMITS IAW REO AND SRM.SDR SWIA201439834Line · crackedAPU FUEL LINE HAS A CRACKED WELD AT SUPPORT BRACKET INSIDE PRESSURE BOX. C-CHECK, REINFORCED FUEL LINES FUEL PRESSURE BOX IAW REO.SDR SWIA201439833Attach Angle · gougedAFT CARGO FLOORBEAM ATTACHMENT TO THE BS 621 PRESSURE BULKHEAD AT LBL27 HAS GOUGE. C-CHECK, REPAIRED AFT CARGO FLOOR RAIL FITTING ON FS 621 LBL 27.00 IAW REO.SDR SWIA201439832Angle · crackedFS 484, RBL 36, OTBD CLIP IS CRACKED. C-CHECK, INSTALLED REPAIR ANGLE IAW REO.SDR SWIA201439860Link · chafedLEFT ENGINE BLOCKER BLOCKER DOOR LINKS HAVE CHAFE DAMAGE AT FORWARD END. REPAIRED DAMAGE ON LT ENG BLOCKER DOOR LINKS IAW REO.SDR SWIA201439831Post · crackedVERTICAL POST AT FS 409+128, RBL 18 OBD SIDE IS CRACKED. C-CHECK R & R THE VERTICAL POST AT FS409+128, RBL18 OTBD IAW REO.SDR SWIA201439830Bulkhead Web · crackedCRACK NOTED ON FS 621 BULKHEAD WEB, FWD FACE, ALONG HEEL LINE AT RBL27.5, APPROXIMATELY WL90. C-CHECK, INSTALLED ALL REPAIR PARTS IAW REO.SDR SWIA201439829Skin · chafedRT AILERON UPPER SKIN SHROUD CHAFED IN 2 LOCATION, BOTH SIDES OF OTBD HINGE. C-CHECK, BLENDED RT AILERON UPPER SKIN SHROUD IN 2EA LOCATIONS, BOTH SIDES OF OTBD HINGE IAW REO.SDR SWIA201439828Skin · chafedLEFT AILERON UPPER SKIN SHROUD CHAFED IN 2 LOCATION, INBD OF INBD HINGE AND OTBD OF CENTER HINGE. C-CHECK, BLENDED THE LT AILERON UPPER SKIN SHROUD, 2EA, CHAFES, INBD OF INBD HINGE AND OT OTBD CENTER HINGE IAW REO.
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