N654FE
Service difficulty reports · 237
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 = 'N654FE' 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 = 'N654FE' 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 08FDEA04700Frame · gougedMAIN CARGO DECK FR 20 HAS GOUGE 3.5 INCHES BELOW STR 12R. REPAIR COMPLIED WITH ON EA6-5310-124032.SDR 08FDEA04698Frame · gougedMAIN CARGO DECK HAS 2 GOUGES ON FR 22, 1 IS 4.25 INCHES BELOW STR 13R AND 1 IS 2.75 INCH BELOW STR 14R. REMOVED AND REPLACED FRAME PROFILE BETWEEN STR 12R AND STR 15R IAW SRM 51-40-21. FABRICATED NEW SECTION ON TRAVELER T8/765537.SDR 08FDEA04645Frame · gougedMAIN CARGO DECK HAS GOUGE ON FRAME SPLICE 2.5 INCH BELOW STR 12 L ON FR 32. REMOVED AND REPLACED FRAME SPLICE IAW SRM 51-40-21, LOCATED AND DRILLED IAW SRM 51-40-45. TREATED AND PRIMED IAW SRM 51-21-10. FABRICATED NEW SPLICE ON TRAVELER T8/765595.SDR 08FDEA04644Seat Track · corrodedMAIN CARGO DECK SEAT TRACK RBL 38 HAS CORROSION 7.0 INCH FWD OF FR 49. REMOVED AND REPLACED SEAT TRACK IAW SRM 51-40-21.SDR 08FDEA04643Seat Track · corrodedMAIN CARGO DECK SEAT TRACK AT RBL 38 HAS CORROSION 12.0 INCH FWD OF FR 43. REMOVED AND REPLACED SEAT TRACK IAW SRM 51-40-21.SDR 08FDEA04642Frame · gougedMAIN CARGO DECK HAS GOUGE ON FRAME SPLICE AT FR 29 3.5 INCH BELOW STR 12. REMOVED AND REPLACED FRAME SPLICE IAW SRM 51-40-21, LOCATED AND DRILLED IAW SRM 51-40-44. TREATED AND PRIMED IAW SRM 51-21-10. SPLICE FABRICATED ON TRAVELER T8/765592.SDR 08FDEA04629Frame · gougedMAIN CARGO DECK HAS GOUGE ON FRAME SPLICE ON FRAME 30 2.5 INCH BELOW STR 12. REMOVED AND REPLACED FRAME SPLICE IAW SRM 51-40-21. NEW SPLICE FABRICATED ON TRAVELER T8/ 765593. LOCATED AND DRILLED IAW SRM 51-40-44. TREATED AND PRIMED IAW SRM 51-21-10.SDR 08FDEA04628Frame · gougedMAIN CARGO DECK HAS GOUGE ON FRAME SPLICE ON FRAME 29 2.5 INCH BELOW STR 12 L. REMOVED AND REPLACED SPLICE IAW SRM 51-40-21. NEW SPLICE FABRICATED ON TRAVELER T8/765594 MAT.2024-0 .063C BATCH NR 3976. LOCATED AND DRILLED IAW SRM 51-40-45. TREATED AND PRIMESDR 08FDEA04588Seat Track · corrodedMAIN CARGO DECK SEAT TRACK RBL 38 HAS CORROSION 9.0 INCH FWD OF FRAME 42. REMOVED SEAT TRACK IAW SRM 51-40-21. LOCATED AND DRILLED NEW SEAT TRACK IAW SRM 51-40-44. INSTALLED SEAT TRACK IAW SRM 51-40-21.SDR 08FDEA04012Unknown · unknownRUDDER TRIM WOULD NOT OPERATE, NOTICED DURING CRUISE FLIGHT, INOP WITH A/P ON AND OFF. DEBRIEFED FLIGHT CREW IN DETAIL. IN CRUISE FLIGHT, WITH AUTO PILOT IN COMMAND THEY NOTICED THEY COULD NOT GET THE RUDDER TRIM TO OPERATE, NO FAULTS ON PANEL OR ECAM, INDSDR 07FDEA04865Display · malfunctionedON RUNWAY WHEN POWER WAS ADVANCED NR 1 REV PRESSURIZED ON ECAM. REMOVED AND REPLACED NR 1 ENGINE RT CDU SWITCH PER MM 78-31-04-4-07. T/R OPS GOOD PER JRH CHAPTER 7.SDR 07FDEA00007Gcu · failedNR 2 GEN FAILED ON T/O ROLL. AFTER T/O PWR SET WOULD NOT RESET. REMOVED AND REPLACED NR 2 GEN CONTROL UNIT. OPS CK GOOD PER MM A300 24-22-12-4 PREMATURE REMOVAL/INSTALLATION.SDR 06FDEA3005Floorbeam · crackedMAIN DECK FS 30 FLOORBEAM CRACKED APPROX 2.75 INCHES LONG LOCATED AT RBL27 AND 1 INCH BELOW UPPER CHORD. COMPLIED WITH EA 6-5310-101957 INSTRUCTIONS. REPAIRED FS 30 RBL 27 FLOORBEAM.SDR 06FDEA3006Floorbeam · crackedMAIN DECK FS 29 FLOORBEAM CRACKED APPROX 1 INCH LONG LOCATED AT RBL 27 AND 1 INCH BELOW UPPER CHORD. COMPLIED WITH EA 6-5310-101957 INSTRUCTIONS. REPAIRED FS 29 AT RBL27.SDR 06FDEA3007Floorbeam · crackedMAIN DECK FS 30 FLOORBEAM CRACKED APPROX 1 INCH LONG LOCATED AT LBL 27 AND 1 INCH FROM UPPER CHORD. COMPLIED WITH EA 6-5310-101957 INSTRUCTIONS. REPAIRED FS 30 AT LBL 27 FLOORBEAM.SDR 06FDEA3008Floorbeam · crackedMAIN DECK FLOORBEAM WEB AND STIFFENER CRACKED APPROX .5 INCH AT FS 27 RBL27. COMPLIED WITH EA 6-5310-101957 INSTRUCTIONS. REPAIRED FS 27 RBL27 FLOORBEAM.SDR 06FDEA3009Floorbeam · crackedMAIN DECK FS 28 FLOORBEAM CRACKED APPROX 1.0 INCHES LONG LOCATED AT RBL 27 AND 1 INCH BELOW UPPER CHORD. COMPLIED WITH EA 6-5310-101957 INSTRUCTIONS. REPAIRED FS 28 RBL27 FLOORBEAM.SDR 06FDEA3010Floorbeam · crackedMAIN DECK FS 31 FLOORBEAM CRACKED APPROX .5 INCHES LONG LOCATED AT RBL 27 AND 1.0 INCHES BELOW UPPER CHORD. COMPLIED WITH EA 5310-101957 INSTRUCTIONS. REPAIRED FS 31 RBL 27 FLOORBEAM.SDR 06FDEA2987Floorbeam · crackedMAIN DECK FRAME 30 FLOORBEAM CRACKED APPROX 0.75 INCH LONG LOCATED AT LBL 67 AND 1.0 INCH BELOW UPPER CHORD. REPAIRED FLOORBEAM AT FR 30 LBL 67 PER EA 6-5310-101951.SDR 06FDEA2913Seat Track · gougedMCD FR.32-FR.33 LBL 37.5 SEAT TRACK GOUGED. BLENDED DAMAGED AREA AND CHECKED LIMITS. MAX ALLOWABLE DAMAGE .016. ACTUAL MAT. LOSS .185 FOUND OUT OF LIMITS IAW SRM 53-10-16. MARKED AND CUTOUT DAMAGED SECTION OF SEAT TRACK AND LOCATED AND DRILLED NEW SECTIONSDR 05FDEA02580Fuel Control · fluctuatesON INITIAL CLIMB-OUT, PASSING APPROX 11000 FT MSL, A/T SYSTEM DISENGAGED. WHEN THAT HAPPENED, NOTICED A FLUCTUATION IN NR 1 FUEL FLOW. CONTINUED CLIMB WHILE EVALUATING PROBLEM. NR 2 FUEL FLOW WAS APPROX 12000PPH NR 1 WAS FLUCTUATING BETWEEN 7000 PPH AND 15SDR 05FDEA01119Uplock · failedNOSE GEAR DOORS UNLOCKED LIGHT REMAINED ILLUMINATED WHEN GEAR UP AND LOCKED ON BOTH GEAR INDICATION PANELS. RETRACTED GEAR AND CONFIRMED RIGHT GEAR DOOR UPLOCK WAS BAD. REMOVED AND REPLACED UPLOCK PER A300-600 MM 32-31-14. SWUNG GEAR SEVERAL TIMES, INDICATISDR 05FDEA00107Filter · cloggedTAKEOFF REJECTED AT 90 KTS FOR NR 1 FUEL ENG FUEL CLOG ECAM & WARNING. REMOVED AND REPLACED MAIN FUEL FILTER AS PER MM 73-12-02-4F. NO CONTAMINATION FOUND. ENG RUN AND LEAK CHECK GOOD. OK FOR SERVICE. FILTER CPN 41823.SDR 05FDEA00098Fuel Filter · cloggedTAKEOFF REJECTED AT 90 KTS FOR NR 1 FUEL ENG FUEL CLOG ECAM & WARNING. REMOVED AND REPLACED MAIN FUEL FILTER AS PER MM 73-12-02-4F. NO CONTAMINATION FOUND. ENGINE RUN AND LEAK CHECK GOOD. OK FOR SERVICE. FILTER CPN 41823.SDR 05FDEA00062Bleed Valve · malfunctionedON CLIMBOUT NR 2 HP BLEED VALVE FAULTED, APP FL 280 LOSS BOTH PACKS. RESET OF PACKS AT 10,000 RESULTED IN NORMAL OPS. DID BITE CHECK OF PNEUMATIC CONTROLLERS, PER TSM 26-00-00, FAULTED NR 2 HP VALVE, DID BITE CHECK OF PACK CONTROLLER PER 21-60-00, NO FAULTSSDR 05FDEA00023Engine · leakingAPPROACHING LEVEL OFF AT FL330 THE NR 2 OIL QUANTITY ON BOTH THE DIAL AND ECAM WAS 4 GALLONS. OVER THE NEXT TWO MINUTES BOTH INDICATORS DROPPED SLOWLY TO ZERO (WITH ENGINE ADVISORY). THEN THE OIL PRESSURE ON THE NR 2 ENGINE DROPPED FROM 36 TO 24 PSI AND STARSDR 04FDEA02816Tachometer · malfunctionedON TAKEOFF SETTING OF STANDARD POWER, ENG 2 N1 GAUGE STOPPED AT APPROX 80 PERCENT (ANALOG/DIGITAL). RTO AT APPROX 100 KTS, NO ADVERSE YAW NOTED. ALL OTHER ENG 2 GAUGES APPEARED NORMAL AND CLOSE TO ENG 1 READINGS, ENT BY: 446285 RPT BY: 075405 FACT. REMOVEDSDR 01FDEA00031Smoke Detector · malfunctionedON LAND RNO AVIONICS SMOKE WARNING ON LEFT ECAM CAME ON. REMOVED SMOKE DETECTOR 13WA AVIONICS COMPT DET PER MM 26-15-12-4.SDR 00FDEA00880Detector · inoperative00-361 SMOKE INDICATION ON ECAM UPON ARRIVAL. INDICATION OF SMOKE COMING FROM SNIFFER TAB OR IN COCKPIT. R&R DUCT DETECTOR 13WA PER AIRBUS A300/600 MM. OK TO CONTINUE.SDR 00FDEA00761Window · crackedCAPT SIDE WINDOW CRACKED DURING CRUISE. REMOVED AND REPLACED LT SIDE FIXED WINDOW AND WINDOW HEAT PROTECTION UNIT. WINDOW OPS CHECK GOOD.SDR 00FDEA00416Pitot Tube · clogged00-171 REJECTED T/O AT 55 KTS DUE TO NO AIRSPEED INDICATION ON F/O PFD. PURGED NR 2 PITOT TUBE WITH NITROGEN PER A300 MM 34-10-00-3 & 34-10-00-5 FOR SYS LEAK CK. OK FOR SERVICE.SDR 99FDEA00212Mechanism · unlatched99-130 - RIGHT PASSENGER DOOR OPEN ECAM AND SHIME SOUNDED. CHECK DOOR PER AMM 52-10-20-5 ALL LATCHES OPER NORM. SUSPECT DOOR WAS NOT LATCHED ALL THE WAY. A/C OK FOR SERVICE.SDR 99FDEA00127Warning Light · illuminatedON GEAR RETRACT AT SJC, GOT AMBER DOOR OPEN LIGHT ECAM. ALSO, CONFIRMED SAME. BOTH SYS AGREED WITH AMBER LIGHTS.SDR 98FDEA00744Switch · out of adjustR1 DOOR WARN LIGHT AT 18,000 FT WITH NO PRESSURE LOSS. RETURN TO ATL. *S/D* ADJUSTED R1 DOOR SWITCH 8WS PER MM 52-71-11.SDR 98FDEA00202Compressor · burnedREJECTED T/O AT APPROX 120 KTS, (18R MEM) DUE TO FIRE ON NR 2 ENGINE. AFTER BOTH BOTTLES WERE FIRED THE FIRE WENT OUT. A/C NOT EVACUATED EMERGENCY CREW CONFIRMED NO FURTHER SMOKE. FOUND HOLE BURNED THROUGH REAR COMPRESSOR STAGE AT 8 O'CLOCK FUEL NOZZLE POSISDR 98FDEA00180Fire Warn · malfunction98-0067, AT APPROX 11000 FT ON CLIMB-OUT GOT A MOMENTARY FIRE WARN IN THE NR 2 ENG AS POWER WAS REDUCED WARN WENT OUT. ALL ENG INSTRUMENTS WERE NORMAL. PERFORM FIRE TEST ON NR 2 ENG PLUS IT WAS NORM BROUGHT PWR BK TO CLIMB TO CLIMB SET WITH NO REOCCURENCE. ISDR 95FDEA00178Prox Det Unit · malfunctionedT/O AUTO THROTTLES DROPPED OFF, REENGAGED AFTER T/O, DROPPED AGAIN, L/GEAR INTERLOCK SELECTED SYS 2. NR 1 A/P AND PITCH TRIM TRIPPED OFF. F/O'S PITOT HEAT O/H ON, WHEN A/P REENGAGED. SELECTED NR 2 A/P, O/H LT OUT, BACK ON. TURNED OFF PER ECAM. CAPTS FLT D
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