N614FE
Service difficulty reports · 388
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 = 'N614FE' 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 = 'N614FE' 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 03FDEA01718Bracket · corrodedLEFT WING O/B FLAP I/B HINGE (FLAP SIDE) BRACKET- I/B LUG AND HOLE FOUND CORRODED. LEFT WING O/B FLAP I/B HINGE (FLAP SIDE) BRACKET- I/B LUG AND HOLE CORROSION REMOVED AND REPAIRED AS PER FEDEX EA 1-5750-71755, TITLE: WINGS - LEFT AND RIGHT OUTBOARD FLAP SDR 03FDEA01719Hinge · corrodedLT WING OB FLAP IB HINGE (FLAP SIDE) BRACKET- OB HINGE LUG AND HOLE FOUND CORRODED. LT WING O/B FLAP I/B HINGE (FLAP SIDE) BRACKET- O/B HINGE LUG AND HOLE CORROSION REMOVED AND REPAIRED AS PER FEDEX EA 1-5750-71755, WINGS- LEFT AND RIGHT OUTBOARD FLAP- SDR 03FDEA01720Hinge · corrodedLH WING O/B FLAP I/B HINGE (FLAP SIDE) BRACKET- O/B ACTUATOR LUG AND HOLE CORRODED. LT WING O/B FLAP I/B HINGE (FLAP SIDE) BRACKET- O/B ACTUATOR LUG AND HOLE CORROSION REMOVED AND REPAIRED AS PER FEDEX EA 1-5750-71755, LEFT AND RIGHT OUTBOARD FLAP- INSDR 03FDEA01722Hinge · corrodedLT WING OB FLAP OB HINGE FITTING (FLAP SIDE) IB ACTUATOR ATTACHMENT LUG HOLE CORRODED. LT WING O/B FLAP O/B HINGE FITTING (FLAP SIDE) - I/B ACTUATOR ATTACHMENT LUG HOLE CORRODED. LT WING O/B FLAP O/B HINGE FITTING (FLAP SIDE) - I/B ACTUATOR ATTACHMENT SDR 03FDEA01721Hinge · corrodedLT WING OB FLAP IB HINGE (FLAP SIDE) BRACKET- IB ACTUATOR LUG AND HOLE FOUND CORRODED. LT WING O/B FLAP I/B HINGE (FLAP SIDE) BRACKET- I/B ACTUATOR LUG AND HOLE CORROSION REMOVED AND REPAIRED AS PER FEDEX EA 1-5750-71755, WINGS- LEFT AND RIGHT OUTBOARD SDR 03FDEA01723Fitting · corrodedLT WING OB FLAP OB HINGE FITTING (FLAP SIDE)- IB HINGE LUG HOLE AND SURFACE CORRODED. LT WING O/B FLAP O/B HINGE FITTING (FLAP SIDE)- I/B HINGE LUG HOLE AND SURFACE CORROSION REMOVED AND REPAIRED AS PER FEDEX EA 1-5750-71742 TITLE: WINGS- LEFT AND RIGHSDR 03FDEA01716Hinge · corrodedRIGHT I/B FLAP O/B HINGE (FLAP SIDE) BRACKET- I/B HINGE PIN HOLE CORRODED. COMPLIED WITH FEDEX EA 1-5750-71761 - WINGS - RIGHT INBOARD TRAILING EDGE FLAP - HINGE BRACKETS CORRODED.SDR 03FDEA01724Fitting · corrodedLT WING OB FLAP OB HINGE FITTING (FLAP SIDE)- OB HINGE LUG HOLE AND SURFACE CORRODED. LT WING O/B FLAP O/B HINGE FITTING (FLAP SIDE)- O/B HINGE LUG HOLE AND SURFACE CORROSION REMOVED AND REPAIRED AS PER FEDEX EA 1-5750-71742 TITLE: WINGS- LEFT AND RISDR 03FDEA01729Hinge · corrodedRT WING O/B FLAP I/B HINGE (FLAP SIDE) BRACKET- I/B HINGE LUG AND HOLE FOUND CORRODED. RT WING O/B FLAP I/B HINGE (FLAP SIDE) BRACKET- I/B HINGE LUG AND HOLE CORROSION REMOVED AND REPAIRED AS PER FEDEX EA 1-5750-71755, TITLE: WINGS- LEFT AND RIGHT OUTBOASDR 03FDEA01731Hinge · corrodedRT WING O/B FLAP I/B HINGE (FLAP SIDE) BRACKET- I/B ACTUATOR ATTACHMENT HOLE AND LUG SURFACES FOUND CORRODED. RT WING O/B FLAP I/B HINGE (FLAP SIDE) BRACKET- I/B ACTUATOR ATTACHMENT HOLE AND LUG SURFACES CORROSION REMOVED AND REPAIRED AS PER FEDEX EA 1SDR 03FDEA01715Fitting · crackedRIGHT WING - SLAT TRACK NR 16 I/B FITTING FOUND CRACKED. RIGHT WING - SLAT TRACK NR 16 I/B FITTING REMOVED AND REPLACED AS PER DRAWING ARB 7565 AND SRM 51-33-01 VOL II.SDR 03FDEA01714Fitting · crackedLEFT WING - FOUND NR 16 SLAT TRACK INBOARD FITTING WITH CRACK. LEFT WING NR 16 SLAT TRACK INBOARD FITTING CRACK RIB REMOVED AND REPLACED AS PER DWG ARB7565, SRM 51-33-01 VOL II AND SRM 51-35-01 VOL II.SDR 03FDEA01781Spar · corrodedRIGHT WING - REAR SPAR UPPER SURFACE O/B OF O/B AILERON FOUND CORRODED. COMPLIED WITH FEDEX EA 1-5710-74238 - WINGS, BASIC STRUCTURE - RIGHT REAR SPAR UPPER SURFACE CORROSION - XORS 1044.800.SDR GK42003F00000Charger · malfunctionedCREW REPORT ON AML: BEFORE START GOT (BATT CHARGER INOP) AND (EMER PWR TST FAIL) ALERTS. TROUBLESHOOTING IAW F/M 24-30-03-00 CARRIED OUT. BOTH MAIN REPLACED IAW AMM 24-32-02 IAW MMDC AD. BATTERY CHARGER REPLACED IAW AMM 24-34-03. EPCU REMOVED AND REPLACED SDR 02FDEA00389Hinge · damagedMAIN DECK CARGO DOOR FUSELAGE HALF HINGE, HINGE LOBES ELONGATED AND ID EXCEEDED FITS CLEARANCE LIMITS. REMOVED AND REPLACED HINGE PER JAMB INSTL DRAWING ACA7211.SDR 02FDEA00390Hinge · damagedMAIN DECK CARGO DOOR FWD SUPPORT ASSY, HINGE LOBES ELONGATED AND BORE ID EXCEEDED CLEARANCE LIMIT. REMOVED AND REPLACED CARGO DOOR FWD SUPPORT ASSY PER 51-35-01 VOL II.SDR 02FDEA00388Hinge · crackedMAIN DECK CARGO DOOR HINGE (AFT HINGE) CRACKED APPROX 0.025 INCH.SDR 02FDEA00376Bolt · shearedNR 3 PYLON FWD WING TO PYLON ATTACHMENT BULKHEAD FOUND 2 EA BOLT SHEARED BELOW LOWER BEARING. R&R WING PER EA 1-5450-62179.SDR 02FDEA00375Fitting · crackedNR 2 ENG LT T/R COWL UPPER TRANSLATING SLEEVE CHANNEL END FOUND CRACK. HFEC CARRIED OUT CRACK LENGTH APPROX .625 INCH LONG. R&R COWL & INSTALLED FITTING AT UPPER TRACK BEAM.SDR 02FDEA00239Stop Fitting · brokenLT INBOARD FLAP VANE SPRING CARTRIDGE STOP ASSY BROKEN FROM STOP FASTENER HOLES. DISCONNECTED CARTRIDGE.SDR 01FDEA00901Battery · failed01-346 AFTER T/O 1 BAT CHARGING ANNUNCIATED. BATTERY DISCHARGED. VOLTAGE DROPPED. ** S/D ** COMINGSDR 01FDEA00594Warning System · activated01-246 AFT T/O DURING FLAP/SLAT RETRACT GOT AILERON DEFLECT DISAGREE ALERT. RAN CHECKLIST UNABLE TO CORRECT.SDR 01FDEA00045Angle · crackedSNRM N 76 LWR VERTICAL STABILIZER INTERNAL SUPPORT FRAME CRACKED AT RT END AS VIEW THRU ACCESS PNL 364FR BS 2069. *S/D* REMOVED AND REPLACED PER SRM 51-00-01.SDR 01FDEA00041Clip · crackedSNRM N 75 ABOVE HORIZONTAL STAB IN UPPER TORQUE BOX STA 2047 ANGLE CLIP FROM BULKHEAD TO CROWN AREA TO BE NDT FOR SUSPECT CRACK. *S/D* PERF HFEC OF ANGLE, NO DEFECT IND.SDR 01FDEA00040Clip · crackedSNRM N 69 ABOVE HORIZONTAL STAB UPPER TORQUE BOX AREA STA 2084 ANGLES CLIP CRACKED RT SIDE FROM FRAME TO CROWN AREA. *S/D* REMOVED AND REPLACED PER SRM 53-3-00 FIG 8.SDR 01FDEA00039Angle · crackedSNRM N 67 ABOVE HORZ STAB IN UPPER TORQUE BOX AREA STA 2122 (DOG HOUSE) TOP ANGLE FROM BULKHEAD TO CROWN AREA HAS CRACKS, LT AND RT ENDS. LT CRACK APPROX .625 INCH LONG AND RT CRACK APPROX 1 INCH LONG. *S/D* REMOVED AND REPLACED PER SRM 53-30-00BB WORKED WISDR 00FDEA00071Seat Track · corrodedSNRM 434 - MAIN DECK LAVATORY, RT BS 484, RBL 75.25, INBD AFT LAVATORY TIE DOWN FITTING SEAT TRACK CORRODED. REMOVED AND REPLACED PER SRM 51-31-01 VOL 11 AND SRM 53-70-00 VOL 1.SDR 00FDEA00048Seat Track · crackedSNRM 452/572, FOUND CRACK MAIN DECK SEAT TRACK, BS 695 X EQUALS 8.5 LT-452. CRACK SEAT TRACK, BS LT 635, LBL 8.5 - 572. SEAT TRACK TRIMMED OUT AND REPAIRED PER SRM 53-70-00 VOL 1.SDR 98FDEA00716Wire · chafedDEFECTIVE AUTO PILOT, AUTOTHROTTLES, FLIGHT DIR SYS, TAT PROBE HEAT, FLAPS ALERT, PRESS, AVIONICS FAN, TRANSPONDER, AUTO BRAKE. FOUND DEFECT CAUSE BY CHAFING AND SHORTING OF THREE WIRES.SDR 98FDEA00701Bolt · shearedDURING LT MLG SHOCK STRUT LWR BEARING SEAL REPLACEMENT, ANTI-ROTATION BOLT SHEARED FROM CHAMBER (ARG 7477-1) UPPER CYL ASSY. DAMAGED FOUND ON UPPER CHAMBER (NRG 6720-5) AND UPPER BEARING (ARG 7607-1). LEFT MLG CHAMBER ASSY REPLACED PER CMM 32-11-12.SDR 98FDEA00699Bolt · shearedDURING LT MLG SHOCK-STRUT LWR BEARING SEAL REPLACEMENT, ANTI-ROTATION BOLT (P/N NAS 4504 U11) FOUND SHEAR FROM CHAMBER (ARG 7477-1) OF UPPER CYLINDER ASSY. *S/D* LT MLG CHAMBER ASSY REPLACED PER CMM 32-11-12.SDR 98FDEA00012Wire · fireCENTER CARGO COMPARTMENT NR 4L ROLLER INOP., PAP5 C/B. REMOVED FLOOR BOARDS, FOUND THE WIRING, UNDER THE FLOOR HAD A FIRE. WIRING WAS BURNED UP, ALSO BELLFRAME HAD HOLE BURNED THRU FRAME AT STA 1641, BETWEEN LONG 47 AND 48. NOTED ON NO. 02 AND 24, DURING BSDR 97FDEA00631Frame · crackedN00098 CENTER GEAR LT DOOR CORNER CRACKED, FRAME OUTER FLANGE RADIUS I/B FWD CORNER. REMOVED CORNER SECTION AND DRILLED OUT NEW CORNER SECTION OF DOOR AND INSTALLED NEW CORNER SECTION PER SRM 51-00-00.SDR 97FDEA00374Egt Indication · malfunctionedSHUT DOWN NUMBER 2 ENGINE BECAUSE OF FLUCTUATING EGT, THEN COMPLETE FAILURE OF THE EGT GAUGE. ALL OTHER ENGINE PARAMETERS WERE NORMAL. NO FAULTS LISTED ON NR 2 ECU A AND B CHANNELS. INSPECTED THERMOCOUPLES TERMINAL AND FOUND SEVERAL TERMINALS ENDS LOOSE. SSDR 96FDEA01659Hydraulic Tube · leakingHYD SYS NR 3 FAIL ALERT DISPLAYED. REMOVED AND REPLACED LEAKING PRESSURE LINE AT NR 3 HYD MANIFOLD. REMOVED AND REPLACED HYD FILTERS AND BOTH ENGINE DRIVEN PUMPS.SDR 96FDEA00999Structure · damagedHARD LANDING WITH TAIL STRIKE. STRUCTURAL DAMAGE BEING EVALUATED IN ANC BY ENGINEERING AND DAC RAMS TEAM. *S/D* DURING MAINTENANCE C-CHECK, A HARD LANDING INSPECTION WAS ACCOMPLISHED. ALSO, DURING THE C-CHECK THE STRUCTURAL DAMAGE CAUSED AS A RESULT OF HARSDR 95FDEA00423Splice Plate · gougeCENTER WING TO RT LOWER WING LONGITUDINAL SPLICE PLATE HAS A WEAR MARK APPROX 5 FEET IN LENGTH, WITH L/E TIP OF SPLICE PLATE WORN APPROX 90 PERCENT OF MATERIAL THICKNESS AT XCW118 INTERSECTING FUSE STA 1156. C/W EA 1-5710-24326 WING OUBT TO CENTER, SPLICE PLASDR 95FDEA00105O-Ring · failedHYD NR 1 OFF ALERT AFTER 50 MINUTES OF FLIGHT AT FLT LEVEL 320. QUANTITY FELL TO 2.8, PRESS DROPPED TO 40 PSI, NR 2, NR 3 NORMAL. HYD TEMP NR 1 - 48C TEMP ROSE TO 92C, THEN CAME BACK DOWN. FOUND HYD LEAK FROM LINE FITTING ON FILTER HEAD TO NR 1L HYD PUMP PR
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