N678FE
Service difficulty reports · 220
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 = 'N678FE' 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 = 'N678FE' 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 FDEA201012214735Wheel · damagedEXCESSIVE TIRE VIBRATION ON T/O, ROLL-CONTINUED T/O FOR AIR TURN BACK. EXCESSIVE VIBRATION ON LANDING. AFTER TURN OFF RUNWAY FIRE MEM CONFIRMED, BLOWN TIRE ON RT LDG GEAR MAYBE NR 7 WITH HYD FLUID LEAKING. R & R NR 7 MAIN TIRE TEMPORALLY TO REMOVE SAID ACFSDR FDEA200903030811Warning Light · illuminatedABORTED TAKEOFF (MEM) AT 50KTS FOR HIGH BRAKE TEMPERTURE WARNING. ALL LEFT TRUCK TEMPERATURES HIGH NO DIFFERENTIAL TEMPS. ALL UNIFORM. INSPECTED BRAKE ASSY'S AND NO DEFECTS FOUND. PERFORMED NORMAL BRAKING OPS TEST IAW MM 32-42-00-5 ITEM 4 AND BITE TEST OF BSDR FDEA200902190597Seat Track · corrodedMAIN DECK CARGO COMPARTMENT SEAT TRACK NR 6 LT CORRODED 6 INCHES AFT OF FR 20 TO 12 INCHES AFT. REMOVED LEVEL 1 CORROSION AND INSTALLED SEAT TRACK SPLICE REPAIR AT TRACK NR 6 LT, BETWEEN FRAME 19 AND FR 23 IAW SRM 53-10-16, FIG 201A.SDR 08FDEA03884Sequence Valve · malfunctionedON DEPARTURE AND GEAR RETRACTION THE NOSE GEAR DOOR SHOWED IT DID NOT CLOSE. RAN ECAM AND QRH AND LIGHT STAYED. DUPLICATED PROBLEM ON GROUND WITH LEFT NOSE DOOR NOT FULLY CLOSING. ADJUSTED LT GEAR DOOR UPLOCK ASSY PER AMM 32-22-11-5. PERFORMED NOSE GEAR EXSDR 07FDEA00976Smoke Detector · contaminatedAT 240 DESCENDING TO OAKLAND RECEIVED RED ECAM FOR AVIONICS SMOKE. REOCCURRED 3 TIMES. PER CREW DEBRIEF, CREW NEVER SMELLED SMOKE IN COCKPIT, NOR SMELLED SMOKE VIA SNIFFER TUBE. INSPECTED MIN EQUIP BAY, RT AND LT AVIONICS RACKS, NO EVIDENCE OF SMOKE/FIRE SDR 06FDEA04246Rib · crackedNR 1 ENGINE PYLON UPPER LEADING EDGE NR 8 RIB IS CRACKED. STOPPED DRILLED IAW SRM 54-50-1. REMOVED WEB IAW SRM 51-40-21 WELDING REPAIR IAW MAE T6/650912 INSTALLED WEB IAW 51-40-21.SDR 06FDEA04219Floorbeam · crackedFUSELAGE MAIN FRAME FLOORBEAM CRACK REPAIR FR 30 AT -Y690. COMPLIED WITH EA 6-5310-102000, STEPS 1-4 FUSELAGE, MAINFRAME FLOORBEAM CRACK REPAIR FR 30 AT -Y690.SDR 06FDEA04218Crossbeam · damagedFUSELAGE MAIN FRAME CROSSBEAM EXTRANEOUS HOLE REPAIR FS 67;-Y2017. COMPLIED WITH EA 6-5310-101996 FUSELAGE MAIN FRAME CROSSBEAM EXTRANEOUS HOLE REPAIR FR 67 Y-2017.SDR 06FDEA04193Skin · damagedFUSLAGE SKIN REPAIR AT LOWER FWD CARGO DOOR AFT JAMB F25A; STR 28R. COMPLIED WITH EA 6-5330-101987. FUSELAGE SKIN, REPAIR AT LOWER FWD CARGO DOOR AFT JAMB FR 25A;STR28R. COMPLIED WITH EA# 6-5310-101995, STEP 1-3. FUSELAGE-MAIN FRAME CROSS BEAM CRACK REPAISDR 06FDEA04192Crossbeam · crackedFUSELAGE-MAIN FRAME-CROSS BEAM CRACK REPAIR FRAME 59;Y1600. COMPLIED WITH EA# 6-5310-101995, STEP 1-3 FUSELAGE-MAIN FRAME CROSSBEAM CRACK REPAIR FRAME 59;Y1600. COMPLIED WITH EA NR 6-5310-101995, STEP 1-3, FUSELAGE-MAIN FRAME CROSSBEAM CRACK REPAIR FRAME 59;SDR 06FDEA04191Frame · gougedCOMPLY WITH EA 6-5310-102004 FUSELAGE-MAINFRAME- REWORK OF 2 GOUGES ON FS 27 RING FRAME. COMPLIED WITH EA 6-5310-102004 FUSELAGE MAIN FRAME 2 GOUES ON FS 27.SDR 06FDEA3001Transmitter · malfunctionedGREEN SYS HYD QUANTITY APPEARED TO LEAK EXCESSIVELY DURING FLT ON GAUGE AND ECAM BUT STAYED IN GREEN BAN CHECKED HYD ACCUMULATOR'S IAW MM 29-00-00-6. ALL CHECK GOOD. PERFORMED HYD OPS TEST WITH ENGINE PUMPS REMOVED AND REPLACED GREEN RESERVOIR HYDRAULIC QUANSDR 06FDEA1654Generator · faultedON T/O ROLL, F/O'S ND AND FD BLANKED AT 90KTS, RTO COOLED BRAKES, BOTH SCREENS RETURNED WITH NO MORE PROBLEMS. NORMAL T/O ON RWY 23R KIND. ACN RELEASED FOR SERVICE PER MEL/CDL: 34-73-01. EFIS SGU 3 INOP. UNABLE TO DUPLICATE FAULT. PRECAUTIONARY SWAPPED SDR 05FDEA01777Pump · failedNR 1 GREEN HYD PUMP FAILED. LOST ALL GREEN HYDRAULIC FLUID. R & R NR 1 ENGINE GREEN SYSTEM EDP PER MM 29-11-32-4-02, ALSO REPLACED NR 1 ENGINE CASE DRAIN FILTER PER MM 29-11-36-4-02, ACP DRY MOTOR AND LEAK CHECKED REF JRH 5-37. CHECKED GOOD. ALSO CHECKED NSDR 02FDEA00874Skin · dentedRT WING CENTER FLAP LOWER SKIN TRAILING EDGE AREA AT TRACK 3, 5 EA DENTS BET TRAILING EDGE RIBS 12A AND 13A. REPAIRED LOWER RIGHT CENTER FLAP SKIN IAW EA. CUT DAMAGED SKIN AT DENTS. EDDY CURRENT INSPECTED DENTS, NO CRACKS EXISTED. FLAP PEENED REWORKED ARSDR 02FDEA00873Skin · dentedRT WING CENTER FLAP LWR SKIN AREA AT TRACK 4 HAS 2 EA DENTS BETWEEN T/E RIBS 23 & 21A. REPAIRED LWR R/CENTER FLAP SKIN IAW FEDEX EA 6-5750-66761. CUT DAMAGED SKIN AT DENT NR 2 PER SRM. EDDY CURRENT INSP'D DENTS. FOUND NO CRACKS EXISTED. FLAP PEENED REWORKESDR 02FDEA00758Connector · installedNR 1 ENG THRUST REV PRESSURIZED ON T/O. BROUGHT NR 1 TO IDLE PER ECAM & QRH AND RETURNED TO MEM. FOUND CANNON PLUGS CONNECTED TO DPV PRESSURE SWITCH AND SOLENOID TO BE CONNECTED. DISCONECTED CANNON PLUGS AND CONNECTED TO STORAGE BRACKETS. OK FOR SERVICE.SDR 00FDEA00892Warning System · illuminated00-371 DUR T/O MASTER CAUTION LIGHT CAME ON + ECAM WARN ENG 1 REV PRESSURIZED ILLUM. ** S/D ** COMINGSDR 00FDEA00891Thrust Reverser · inoperative00-370 REJECTED T/O FOR M/C ENG REV PRESSURIZED ON ECAM. ** S/D ** COMINGSDR 00FDEA00889Control Unit · faulty00-368 DUR T/O MASTER CAUTION LIGHT CAME ON AND ECAM WARN NR 1 ENGINE THRUST REVERSER PRESSURIZED ILLUMINATED. ** S/D ** REPLACED BRAKE SYSTEM CONTROL UNIT.
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