N609FE
Service difficulty reports · 475
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 = 'N609FE' 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 = 'N609FE' 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 04FDEA01281Stop Fitting · crackedLEFT WING - OUTBOARD FLAP STOP FITTING FOUND CRACKED. LEFT WING - OUTBOARD FLAP STOP FITTING REMOVED AND REPLACED AS PER SRM 51-31-01 VOL 2 AND SRM 51-35-01 VOL 2.SDR 04FDEA01280Splice · crackedCTR CARGO COMPT BILGE AREA SPLICE FITTING AT LONGERON 44 LEFT STA 1541. SUSPECT CRACK ORIGINATING FROM THE RIVET AREAS. CRACK SPLICE FITTING REMOVED AT CENTER CARGO COMPARTMENT BILGE AREA SPLICE FITTING AT LONGERON 44 LT STA 1541 AS PER SRM 51-33-01 VOL II ASDR 04FDEA01210Bracket · crackedRT WING LEADING EDGE NR 16 SLAT TRACK ASSY INBOARD BRACKET WEB CRACKED. INBD BRACKET REMOVED AS PER SRM 51-31-01-VOL II AND INSTALLED NEW BRACKET AS PER SRM 51-33-01 VOL II & SRM 51-35-01 VOL II. CARRIED OUT OPERATION CHECK AS PER AMM 27-80-00 AND FOUND SATSDR 04FDEA01209Bracket · crackedLEFT WING LEADING EDGE NR 16 SLAT TRACK ASSY INBOARD BRACKET WEB CRACKED. RIB REMOVED AND REPLACED AS PER SRM 51-31-01 VOL II AND BUSHING REPAIR CARRIED OUT AS PER EA 1-5710-76771 - WINGS - LEADING EDGE SLAT SUPPORT NR 16 (LT) - BUSHING REPAIR.SDR 03FDEA00190Warning System · malfunctionedAFTER TAKEOFF, GEAR RETRACTION RIGHT GEAR UNSAFE RED LIGHT ON PRIMARY PNL ABOVE GEAR HANDLE AND ON CONFIG SYNOPTIC PAGE. RED TABS ACCOMPLISHED, GEAR EXTENDED AND RIGHT GEAR INDICATION IMMEDIATELY WENT GREEN. RAISED GEAR AND ALL INDICATION. T/S FIM 32-30-03,SDR 01FDEA00600Sensor · defectiveON DEPARTURE GOT SLAT DISAGREE AT 300 FLAPS 25 DEG GEAR COMING UP ALERT CONTINUE. RAN CHECKLIST. R&R SLAT POS SENSORS PER MM 27-84-02, 27-84-03.SDR 01FDEA00173Mount · corrodedCTR LAND GEAR - LT PILLOW BLOCK MOUNT HAS CORROSION IN BOLT HOLES, GUIDE PIN HOLE AND MATING SURFACE. REMOVED AND REPLACED BUSHINGS PER SRM 53-40-00 PG 69, CMM 20-20-07.SDR 01FDEA00172Mount · corrodedCTR LAND GEAR - RT PILLOW BLOCK MOUNT HAS CORROSION IN BOLT HOLES, GUIDE PIN HOLE AND MATING SURFACE. *S/D* REMOVED AND REPLACED BUSHING PER SRM 53-40-00 PG 69, CMM 20-20-07.SDR 01FDEA00107Control Unit · failedUPON FLAP/SLAT RETRACT GOT 2 ALERT DEF AIL DISAGREE. REMOVED AND REPLACED NR 2 FCC PER IAW MM 27-01-03-4.SDR 00FDEA00546Seat Track · crackedFWD CARGO COMP, MAIN DECK CARGO TRACK CRACKED AT RBL 8, BS 755. *S/D* REMOVED AND REPLACED PER IAW SRM 53-70-00 VOL I.SDR 00FDEA00545Seat Track · crackedFWD CARGO COMP, MAIN DECK CARGO TRACK CRACKED LBL 47, BS 635 TO BS 755. *S/D* REMOVED AND REPLACED PER IAW SRM 53-70-00 VOL I.SDR 00FDEA00544Seat Track · crackedFWD CARGO COMP, MAIN DECK CARGO TRACK CRACKED LBL 27, BS 635 TO BS 755. *S/D* REMOVED AND REPLACED PER IAW SRM 53-70-00 VOL I.SDR 00FDEA00542Seat Track · crackedFWD CARGO COMP, MAIN DECK CARGO TRACK CRACKED AT LBL 8 BS 755. *S/D* REMOVED AND REPLACED PER IAW SRM 53-70-00 VOL I.SDR 99FDEA00240Line · leakingFUSELAGE NR 2 ENGINE SHROUD DRAIN VALVE FOUND WITH FUEL PRESENT. LEAKAGE TRACED TO 3 LOCATIONS IN CENTER LAND GEAR WHEEL WELL FWD BULKHEAD. *S/D* REMOVED AND REPLACED 1 NR 2 ENG FUEL LINE COUPLING SEAL AS PER MM 28-00-00-4. CARRIED OUT FUEL SHROUD LEAK CK SDR 98FDEA00740Disagree Light · activated98-298 - AILERON DEFLECTION DISAGREE ALERT AT SLAT RETRACT. ALERT DISAPPEAR FOR 1 MIN THEN RETURN ON THE CONFIG PG NO AILERON DEFLECTION SHOW ON CLEAN WING. A/C DEFER PER MEL 27-2 METHOD A.SDR 98FDEA00665Disagree Light · malfunctioned98-254 - DURING FLAP RETRACTION, REVD LEVEL 2 AILERON DISAGREE ALERT. PERF AILERON DEFLECTION ADJUST TEST IAW 27-16-00-5. TOOK AILERON POS MEAS NEUTRAL, FULL THROW AND DEFLECT POS. COMPARED SENSOR READOUT DURING TEST, ALL WITHIN LIMITS. OPS CK SEVERAL TIMESDR 98FDEA00265Doublers · crackedSNRM N 00345, CENTER GEAR WELL, LEFT TRUNNION SUPPORT ANGLE DOUBLER IS CRACKED AT UPPER AND LOWER FWD SECTIONS AT BS 1458. REMOVED SUPT ANGLE DOUBLERS EDDY CURENT INSP'D PER EA 1-5310-38499 NO DEFECT NOTED, INSTALLED ANGLE DOUBLER PER EA 1-5310-38499.SDR 98FDEA00137Bleed Air Duct · contaminatedSHORTLY AFTER TAKEOFF, EXPERIENCED AN UNKNOWN ODOR THE F/O AND RFO EXPERIENCED A BURNING SENSATION IN THE EYES. CREW WENT ON 100 PERCENT O2 AND ACCOMPLISHED ALL CHECKLIST ITEMS. RETURNED TO EWR. COMPLIED WITH CHECKLIST AND DUMPED APPROX 65.0 LBS FUEL. REMOSDR 97FDEA00640Engine · failedAFTER T/O, NR 2 ENG CVM TURB 5.0 AMBER BOX ACCOMPLISHED BY VIBRATION IN AIRFRAME (3000) PRECAUTIONARY SHUTDOWN AT APPROX 6000 EGT INTERMITTENTLY BLANK BEFORE SHUTDOWN REDUCED PWR TO 60 PERCENT N1 NO CHANGE IN VIBRATION. FOUND MAJOR TURBINE CASE DAMAGE DUE TO SDR 97FDEA00375Duct · rupturedNR 1 ENGINE TURBINE CASE COOLING DUCT RUPTURED. CAUSING HEAT DAMAGE TO COMPONENTS AND ELECTRICAL WIRING FOR THE FOLLOWING SYSTEMS. HYDRAULIC, ENGINE OIL TEMP AND PNEUMATIC. NO ASSOCIATED FIRE WARNINGS OR ALERTS. *S/D* REMOVED AND REPLACED THE NR 1 ENGINE.SDR 97FDEA00048Bracket · failedOUTBD PULLEY SUPPORT BRACKET HAS 3 MISSING MOUNT BOLTS CAUSING AN INCH GAP TO WEB AT FWD SIDE AND SEVERAL SHEARED RIVETS AT LOWER AND UPPER ROWS. LOCATED AT OUTBD WEB OF NR 1 SLAT CENTER TRACK, STA NR X1S204 RT WING. *S/D* FABRICATED SUPPORT BRACKET PER DW-SDR 97FDEA00045Trunnion Pin · corrodedDURING REMOVAL OF LT MLG FORWARD TRUNNION PIN, DURING SCHEDULED MAINTENANCE, FOUND PIN SEVERELY CORRODED WITH ASSOCIATED PLATING LOSS ALONG ENTIRE CIRCUMFERENCE, AT BUSHING CONTACT POINTS. ALSO, THERE IS PLATING LOSS ALONG LIMITED OTHER POINTS ALONG PIN SURFASDR 95FDEA01747Shunt Mount · meltedEMERGENCY POWER TEST WOULD NOT PASS. FOUND BATTERY AMMETER SHUNT S4-1, MOUNT HAD MELTED WHERE SHUNT IS ATTACHED TO THE L EMERGENCY DC BUS FEED RCCB, B1-189. R EPLACED BATTERY EQUIPMENT PANEL AND F/C OK PER MM 21-34-00. ALSO, EPCU R-T-S TEST PASSED PER MM 24SDR 95FDEA01679Bolts · looseINTERCONNECT TORQUE TUBE BETWEEN PILOT'S AND COPILOT'S CONTROL COLUMNS WERE FOUND LOOSE. INSPECTED BOLTS AND HOLES, FOUND NO DISCREPANCIES. TORQUED BOLTS, PER CMM 27-31-02 PAGE 502 AND RETURNED TO SERVICE.SDR 95FDEA00443Retract Mech · out of adjustON GEAR RETRACTION, BOTH RT MAIN IND REMAINED RED, CYCLED GEAR AND GOT BOTH LT AND RT INDICATIONS RED. ALL GREEN IN DOWN POS, RECYCLED GEAR AND GOT SAME INDICATIONS, AFTER 3 MINUTES LT GEAR RETURNED TO NORMAL. THIS SEQUENCE OCCURED TWICE, CONTINUED FLT TO NR
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