N392FE, cancelled Jan 29, 2024
Service difficulty reports · 70
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 = 'N392FE' AND deregistration_id = 'N392FE-2024-01-29' 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 = 'N392FE' AND deregistration_id = 'N392FE-2024-01-29' 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 FDEA201412114107Battery Pack · failedDURING SERVICE CHECK, FOUND EMERGENCY LIGHT BATTERY NR 1 LOW ALERT. REPLACED THE BATTERY PACK. OPS CHECKED GOOD.SDR FDEA201408052076Skin · crackedLEFT WING FIXED LE VI FOUND EVIDENCE OF CRACKS AT THE TAI. TELESCOPING DUCT CUT OUT TOP CORNERS COMPLIES WITH EA 8-5710-T0309830 P1 BY REPAIRING USING SRM 57-40-01 AS A REFERENCE.SDR FDEA201403270594Lamp · inoperativeR1 DOOR SLIDE LIGHT WILL NOT TEST CORRECTLY. REPLACED LAMP IAW SMP. OPS NORMAL.SDR FDEA201403190533Connector · looseR1 DOOR LIGHT FOR SLIDE INOPERATIVE. SECURED ELECTRICAL CONNECTOR ON WIRE LEAD TO PRESS TO TEST SWITCH. PRESS TO TEST SYSTEM FOR BATTERY AND LIGHT FUNCTION NORMALLY IAW AMM 25-61-01-2.SDR FDEA201311232855Bottle · low pressureRIGHT ENTRY DOOR PNEUMATIC BOTTLE PRESSURE 0. FOUND DOOR R1 HANDLE IN THE EMERGENCY POSITION. RESET DOOR HANDLE & SERVICED DOOR ASSIST BOTTLE IAW MD10-10 MM 52-11-07-2, OPERATIONS NORMAL.SDR FDEA201307101522Fire Detector · false activationTHIRTY MINUTES AFTER TAKEOFF, RECEIVED A LEVEL 3 ALERT, LOWER CARGO FWD FIRE. DISCHARGED FIRE AGENT IAW PHASE 1 PROCEDEURES, RAN RED TABS. DIVERTED, CRASHED. FIRE RESCUE INSPECTED ACFT AND FOUND NO INDICATION OF FIRE. INSPECTED FWD LOWER CARGO BAY FOR ANYSDR FDEA201303010480Windshield · failedON FINAL APPROACH, MODERATE RIM ICE ACCUMULATATED ON F/O WINDSHIELD, ALMOST NO ICE ON CAPT SIDE. WINDSHIELD A/I HAD BEEN ON FOR ABOUT 10 MIN ON LOW ON BOTH SIDES. HIGH WAS THEN SELECTED AND WITHIN 30, " F/O WINDSHIELD CRACKED." REPAIRED IAW AMM 56-11-00-2SDR FDEA201301040012Relay · intermittentAIR MANIFOLD NR 3 FAILED LEVEL 3 ALERT WHEN ANTI-ICE SELECTED ON DURING DESCENT. PERFORMED TEST OF THE PNEUMATIC PRESSURE SW IAW EA 8-3622-114705, SWITCH OPS NORMAL, BUR FOUND FAILED. RELAY R2-5257 INTERMITTENT, REPLACED RELAY AND PERFORMED TESTS IAW FIM 3SDR FDEA201301030011Relay · failedAIR MANIFOLD NR 3 FAILED LEVEL 3 ALERT WHEN ANTI-ICE SELECTED ON, DURING DESCENT. PERFORMED A GVI OF PNUEMATIC DUCTS AND VALVES IN WING AND PYLON AREA. PERFORMED PNEUMATIC DECAY TEST IAW AMM 36-00-01-5 WITH NO FAULTS. DURING SYS TESTS USING APU, FOUND THE MASDR FDEA201107152714Shaft · shearedNR1 ACM PACK RUNS ALMOST FULL HOT REGARDLESS OF RAM AIR DOOR AND PACK VALVE TRANSMITTER POSITIONS. REMOVED NR 1 ACM PACK, FOUND A BROKEN TURNBINE SHAFT. R & R AIR CYCLE MACHINE POSSITION NR 1.SDR FDEA201107072608Spar Cap · crackedRT WING REAR SPAR CAP HAS 2 HOLES WITH CRACK INDICATION. ACCOMPLISHED LIMITED REPAIR REF EA 8-5710-147784. PERMANENT REPAIR TO BE ACCOMPLISHED WITHIN 24 MONTHS.SDR FDEA201106132224Angle · corrodedAFT CARGO COMPARTMENT AT STA 1841 FLOOR AFT FRAME ANGLE FOUND CORRODED FROM UNDERNEATH AT NUT PLATE HOLES FROM LONGERON 42L TO 42R. FABRICATED NEW ANGLE WITH 7075-0 IAW WITH SRM 53-00-01 AND DWG AGA3874. PART HEAT TREATED TO T6. INSTALLED NEW ANGLE AT STA 1SDR FDEA201106112207Roller Tray · corroded4 ROLLER TRAYS HAVE CORROSION, CENTER PIT BETWEEN STA 1700 TO 1781 CLEANED SURFACE CORROSION ON 3 TRAYS IAW SRM 51-21-01, VOL III. FABRICATED ONE ROLLER TRAY IAW DWG AFJ 7001. INSTALLED NEW TRAY IAW DWG AFJ7001.SDR FDEA201106112206Floorbeam · corrodedCTR CARGO, AFT WALL FLOORBEAM ANGLE CORRODED ON AFT SIDE (AS VIEWED FROM AFT CARGO). R & R LT FLOORBEAM ANGLE SECTION, REF AFA3871, CLEANED AND TREATED CTR AND RT FLOORBEAM ANGLE SECTIONS, REF SRM 51-21-01, VOL II, LT FLOOR SUPPORT ANGLE 13 CORRODED BEYOND RSDR FDEA201106062129Support · corrodedCENTER CARGO AFT WALL, CORROSION ON VERTICAL SUPPORT BEAM JUST RIGHT OF CTR AND JUST ABOVE FLOOR LINE. INSTALLED NEW VERTICAL SUPPORT BEAM AT STA 1781 IAW DWG AFA3225 AND SRM 51-35-01, VOL II.SDR FDEA201006162031Relief Valve · leakingON CLIMBOUT, GOT HYD 3 ELEV OFF ALERT WITH DECREASING HYD 3 QTY. FOLLOW ON ALERTS HYD 3 OFF AND ON FINAL APPROACH BACK TO DEPARTURE GOT HYD 3 FAIL. LOST ALL HYD 3 QTY. ALTN GEAR EXTENSION USED. LDG WT 343,500LBS. AIRPORT CRASH FIRE RESCUE REPORTED SMOKESDR FDEA201004221292Pressure Switch · failedAT CRUISE ALTITUDE, RECEIVED LEVEL 3 MANIFOLD NR 1 FAIL ALERT. AIR SYS ISOLATED PROPERLY AND ALERT WENT AWAY. DIVERTED AND LANDED WITHOUT INCIDENT. R & R LT WING MANIFOLD FAILURE DETECTION PRESSURE SWITCH IAW. MM36-23-03-4. PERFORMED TEST IAW 36-23-03. R &SDR FDEA201002210480Transducer · malfunctionedANTI-SKID R FAIL ON LANDING CYCLED AND NO CHANGE,ON 2ND. ATTEMPT TO LAND CAME ON AGAIN THEN WENT OUT, FLAPS 50 LANDING 4L CKED CFDS FOUND MSG. 324355, NR 7 WHEEL SPEED TRANSDUCER FAIL, NEEDS CPN 3215531, ORDERED PART. REMOVED NR 7 TRANSDUCER, INSPECTED COSDR FDEA201001100077Anti-Skid Sys · failedLEVEL 2 ANTI-SKID R FAIL ON FINAL W/GEAR DOWN. ANTI-SKID WOULD NOT TEST W/GEAR UP AFTER GO AROUND. DID TEST AND FAIL ONCE GEAR DOWN. R & R NR 7 WHEEL SPEED TRANSDUCER IN REF TO AMM32-45-03-2, SPIN CKD GOOD AND NO FAULTS SHOWN ON ASCU. REACTIVATED NR 7 MSDR FDEA201001090064Anti-Skid Sys · failedGOT LEVEL 2 ANTI SKID FAIL ON FINAL. EXECUTED GA RAN QRH. UNEVENTFUL LANDING. HAD FIRE TRUCK LOOK AT BRAKES WITH INFARED. THEY STATED BRAKES WERE WARM NOT HOT. IAW RTS FOUND ASCU HAD INTERNAL FAULT. R & R ASCU IAW AMM 32-45-01-04. ACCOMPLISHED RTS IAW AMM SDR FDEA201001050014Anti-Skid Sys · failedWHILE CONDUCTING ILS APPROACH TO RWY 36R AT MEM RECEIVED LVL 2 ALERT ANTI SKID RT FAIL EXECUTED MISSED APPROCH, RAN QRH. FAILED MANUAL ANTI-SKID CHECK WERE VECTOR FOR ANOTHER APPROACH AND ANTI-SKID APPEARED TO WORK. REMOVED AND REPLACED ASCU IAW MM 32-45-0SDR FDEA200907042475Fitting · crackedRIGHT WING NR 2 SLAT FOUND CRACKED AT INBOARD FITTING. REMOVED AND REPLACED RT WING NR 2 SLAT AND ADJUSTED IAW AMM 27-80-01-4.SDR FDEA200906152113Web · crackedN/R206- 5 IN CRACK ON UPPER WEB INBD SIDE NR 3 PYLON APPROX 12 IN. FROM AFT PYLON MOUNT. REMOVED UPPER WEB ATNR 3 PYLON REF SRM 51-00-01. FABRICATED NEW WEB REF DRAWING AUB7031. INSTALLED NEW WEB REF 51-00-01 VOL 1, E.O. 5-5410-7-4311 P2 AND EO 8-5410-7-4311 PSDR FDEA200901290379Pressure Panel · crackedLT MLG WHEEL WELL INBD WALL UPPER AFT CORNER HAS CRACK FROM STIFFENER GOING FWD TOWARD PREVIOUS REPAIR, VERIFIED AND MARKED USING ET, LOCATED ABOVE NR 1 HYD SYSTEM RESERVOIR COMPLIED WITH EA 8-5310-123830 TITLE, FUSELAGE-MAIN FRAME- KEEL STRUCTURE/UNDERWING BASDR 06FDEA1650Skin · bulgedFOUND CENTER PIT STA 1731 ABOVE L45R TORQUE BOX WEB (SILL AREA) SKIN BULGE AND SHEARED RIVET. ENTERED IN ERROR WRONG AIRCRAFT, NO NON-ROUTINE N00200 FOR AIRCRAFT N392FE.SDR 06FDEA1245Repair · unknownRT FUSELAGE EXTERNAL REPAIR IS IN CRITICAL AREA OF PRIMARY STATIC PORT. REWORKED REPAIR IAW FEDX EA 8-5330-96383 FUSELAGE - SKIN AT FORWARD CARGO DOOR HAS REPAIR THAT WAS REMOVED - REWORK. MAJOR REPAIR.SDR 06FDEA0535Sensor · out of adjustON APPROACH TO KSMF AT FLAPS 22, SLAT EXTEND SELECTION OF FLAPS 35 CAUSE A SLAT DISAGREE. RAN QRH LANDED FLAPS 22/SLATEXT. FOUND SENSOR GAP BEYOND MAX LIMIT. ADJUST SENSORS L4A AND L4B. RETENSIONED LT WING O/B SLATS AND SAFETIED PER M/M 27-80-00-5-2 CLOSEDSDR 05FDEA00097Computer · malfunctionedDURING APPROACH TO RWY 35R AT MCO GOT TOO LOW TERRAIN WARNING. AT 400 FEET ON GLIDE SLOPE AND LOC EXECUTED MISSED APPROACH AND RETURNED TO SAME RWY. THE SAME THING HAPPENED ON SECOND APPROACH. TOO LOW TERRAIN, WARNING CONTINUED TO TOUCHDOWN. REMOVED & REPLSDR 04FDEA02982Fitting · wornLT WING FLAP SIDE LOAD ROLLER FITTING LOWER LUG FLAT SPOTTED AND ALL HOLES HAVE EVIDENCE OF PITTING. REMOVED CORROSION AND PITTING FROM LUG AND BORES. FABBED AND INSTALLED 2 EACH REPAIR BUSHINGS IAW SRM57-20-00 VOL.I PAGE 16. INSTALLED BUSHINGS ON NR N01175. SDR 04FDEA02981Roller · wornRT WING FLAP SIDE LOAD ROLLER FITTING LOWER LUG FLAT SPOTTED AND HOLES HAVE EVIDENCE OF PITTING. REMOVED PITTING AND CORROSION FROM LUG AND BORE. FABBED AND INSTALLED 2 EACH REPAIR BUSHINGS IAW SRM 57-20-00 VOL. I PAGE 16. BLENDED FLAT SPOTTED AREA IAW EA8-SDR 04FDEA02952Lavatory · not seatedLAVATORY PAPER AND WASTE RECEPTACLE DOES NOT SEAL CORRECTLY. RESEALED LAVATORY PAPER AND WASTE RECEPTALE IAW MD10-10 SRM 51-41-01 VOL II AND EA 8-2540- 82478, SEALING OF FORWARD LAVATORY TRASH SHOUT.SDR 04FDEA02951Panel · misalignedNR 1 PYLON PRECOOLER VENTILATOR PANEL ASSY PN AUB7054-501 FASTENER HOLES DO NOT ALIGN TO PYLON STRUCTURE. COMPLIED WITH EA 8-5480-81485 REV. A, NR 1 ENGINE VENTILATOR PANEL REPAIR.SDR 04FDEA02950Frame · crackedNR 2 ENGINE RT THRUST REVERSER TRAILING EDGE AFT FLANGE CRACKED APPROXIMATELY 6 INCHES FROM BOTTOM. COMPLIED WITH MFG EA 8-7830-81496SDR 04FDEA02937Hinge Fitting · corrodedRIGHT HAND INBOARD FLAP PIVOT ATTACH POINT, OUTBOARD LUG FACE, OUTER SURFACE CORRODED. REMOVED CORROSION FROM LUG FACE, FOUND TO BE OUT OF LIMITS IAW DC10 CMM 57-52-01. COMPLIED WITH FEDEX EA 8-5750-81475, WINGS, RIGHT HAND INBOARD FLAP OUTBOARD HINGE PIVOTSDR 04FDEA02914Hinge · corrodedLT IB FLAP OB HINGE PIVOT BORE FACE PITTED AND GOUGED (AIRFRAME SIDE) LOCATION NR 3. REMOVED BUSHING, REMOVED CORROSION, AND COMPLIED WITH EA 8-5750-81473 REF NR N00295.SDR 04FDEA02917Fitting · crackedCRACKED LONGERON END FITTING, AFT OF RIGHT HAND AIR CONDITIONING DOOR CUTOUT, LONGERON 35R, STA 535. REMOVED END FITTING IAW FEDEX SRM 51-35-01 VOLUME II PAGE 1, AREA ALODINED AND TREATED IAW FEDEX DC10 SRM 51-21-01 VOLUME II PAGE 1, RECEIVED NEW END FITTING SDR 04FDEA02916Hinge Fitting · corrodedLEFT WING INBOARD FLAP OUTBOARD SUPPORT PIVOT ATTACH POINT INBOARD BORE GOUGED. REMOVED DAMAGE IAW DACCMM 57-52-01, BORE FOUND OUT OF LIMITS, GENERATED RFTS, RECEIVED FEDEX EA8-5750-81492, REPAIRED BORE IAW DACCMM 57-52-01 AND FEDEX EA8-5750-81492. SEE NR N00SDR 04FDEA02915Support · corrodedRIGHT HAND OUTBOARD FLAP INBOARD SUPPORT PIVOT ATTACH POINT INBOARD BORE CORRODED (INBOARD SUPPORT). REMOVED CORROSION IAW DACCMM 57-52-02. ETCHED AND PEENED IAW DACCMM PERCENT &-52-02 AND 20-11-02. FABBED BUSHING IAW DACCMM 57-52-02 AND EA8-5750-81472. CASDR 04FDEA02913Longeron · wornNR 1 ENGINE LEFT HAND CORE COWL UPPER CHAFE STRIP WORN. FABRICATED DOUBLER, FILLERS, AND STRAP FOR LONGERON REPAIR IAW FEDEX EA8-7110-81487. INSTALLED LONGERON REPAIR IAW DC10 SRM 51-35-01 VOLUME II. FABRICATED RUB STRIP IAW DAC DWG NSL6016. INSTALLED RUB SDR 04FDEA02912Support · corrodedLEFT WING INBOARD FLAP OUTBOARD HINGE AT LOCATION NR 1 INBOARD AND OUTBOARD LUGS HAVE CORROSION. REMOVED CORROSION FROM LOCATION NR 1 MOUNTING SURFACE IAW DACCMM 57-44-07 AND FEDEX EA8-5750-81473. PRIMED LUGS IAW DC109 SRM 57-21-01 VOLUME II. BEGINNING BORESDR 04FDEA02911Support · corrodedRIGHT WING INBOARD FLAP OUTBOARD HINGE AT LOCATION NR 1 INBOARD AND OUTBOARD LUG HAS CORROSION. REMOVED CORROSION IAW DACCMM 57-44-07. FOUND TO BE STRUCTURALLY ACCEPTABLE IAW FEDEX EA8-5750-81474. ALODINED AND PRIMED LUG FACES IAW DC10 SRM 51-21-01 VOLUME ISDR 04FDEA02910Support · corrodedLEFT WING INBOARD FLAP OUTBOARD HINGE AT LOCATION NR 3 HAS CORROSION IN BORE. REMOVED CORROSION IAW DACCMM 57-44-07. BEGINNING BORE 2.5850 INCH FINAL 2.626 INCH MATERIAL. REMOVED .041 INCH. FABRICATED BUSHING IAW DACCMM 57-44-07 AND EA8-5750-81473. ACCOMPSDR 04FDEA02908Support · corrodedLEFT WING INBOARD FLAP OUTBOARD HINGE AT LOCATION NR 1 INBOARD AND OUTBOARD LUGS HAVE CORROSION. REMOVED CORROSION FROM LOCATION NR 1 MOUNTING SURFACE IAW DACCMM 57-44-07 AND FEDEX EA8-5750- 81473. PRIMED LUGS IAW DC10 SRM 57-21-01 VOLUME I, BEGINNING BORESDR 04FDEA02907Hinge Fitting · corrodedRIGHT HAND INBOARD FLAP PIVOT ATTACH POINT INBOARD BORE CORRODED. REMOVED CORROSION BEGINNING BORE 1.1875 INCH FINAL 1.2583 INCH MATERIAL REMOVED .0708 INCH IAW DACCMM 57-52-01. FABBED REPAIR BUSHING IAW DACCMM 57-52-01 AND EA8-5750-81475. PERFORMED MPI IAWSDR 04FDEA02906Support · corrodedBORE CORRODED RIGHT WING INBOARD FLAP OUTBOARD HINGE LOWER SWIVEL BEARING. REMOVED CORROSION IAW DACCMM 57-44-07. ORIGINAL BORE 2.530 INCH FINAL 2.543 INCH MATERIAL LOSS .013 INCH. FABBED BUSHING IAW DACCMM 57-44-07 AND EA8-5750-81474. PERFORMED MPI IAW DPSDR 04FDEA02905Support · corrodedRIGHT WING INBOARD FLAP OUTBOARD HINGE LOCATION NR 1 INBOARD AND OUTBOARD LUG HAS CORROSION. REMOVED CORROSION IAW DACCMM 57-44-07. FOUND TO BE STRUCTURALLY ACCEPTABLE IAW EA8-8750-81474. ALODINED AND PRIMED LUG FACES IAW DC10 SRM 51-21-01 VOLUME II. BEGINSDR 04FDEA02904Skin · misrepairedRIGHT HAND PRIMARY STATIC PORT FAILS RVSM INSPECTION FOR EXTERNAL DOUBLER MISMATCH RATIO IAW DC10 SRM 53-00-02 NOTE 2 (FIG 1 SHEET 2). REMOVED EXISTING FUSELAGE SKIN REPAIR ON FORWARD EDGE OF FORWARD CARGO DOOR CUTOUT DOUBLERS, FABRICATED NEW EXTERNAL DOUBLERSDR 04FDEA02903Hinge · corrodedLEFT WING OUTBOARD FLAP INBOARD HINGE, LOCATION NR 4 BORE CORRODED. REMOVED CORROSION IAW DACCMM 57-44-08, INSPECTED IAW DACCMM 57-44-08 AND 20-11-02. PEENED IAW DACCMM 57-44-08 AND 20-11-01. PRIMED IAW DC10 SRM 51-21-01 VOL. II. FABBED BUSHING IAW DACCMM SDR 04FDEA02902Fitting · damagedRIGHT HAND INBD FLAP PIVOT POINT OUTBOARD BORE HAS GROOVE MARK. REMOVED CORROSION IAW DAC CMM 57-52-01. BEGINNING DIAMETER 1.1875 INCH FINAL 1.2552 INCH . FABBED REPAIR BUSHING IAW DACCMM 57-52-01 AND EA8-5750-81475 MPI IAW DACCMM 5752-01 AND DPS 4.704 CAD PSDR 04FDEA02901Skin · corrodedLEFT WING SKIN LOWER SURFACE IS CORRODED, STATION XORS 799 APPROX 19 INCHES AFT OF FORWARD SPAR CAP. SKIN HAS SMALL AMOUNTS OF PITTING. REMOVED CORROSION AND FOUND TO BE WITHIN LIMITS IAW EA 8-5710-81493. ORIGINAL MATERIAL THICKNESS IS .096 INCH, REMOVED .0
Back to N392FE, cancelled Jan 29, 2024