N664FE

Service difficulty reports · 307

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 = 'N664FE' 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.

SDR 06FDEA2386Seat Track · crackedMC DECK SEAT TRACK FLANGE CRACKED AT FR 60/LBL 38.Jun 22, 2006 · N664FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR 06FDEA1681Generator · faultedWHILE ADVANCING POWER FOR TAKEOFF THE NR 2 GENERATOR FAULTED. AFTER REJECTING TAKEOFF, GENERATOR RESET. RE-ATTEMPTED TAKEOFF, NO FURTHUR PROBLEMS. CHECKED IDG FOR PROPER SERVICING. RAN NR 2 ENG PER JRH NR 5, PERFORMED NR 2 GEN FUNCTIONAL TEST PER JRH NR 8May 2, 2006 · N664FE · Airbus A300F4605R · AC Generation SystemSDR 06FDEA0715Valve · unknownWHILE APPLYING POWER FOR T/O, ECAM ALERT NR 1 REVERSER PRESSURIZE DEACTIVATING T/R MEL. RELEASED FOR SERVICE PER MEL/CDL: 78-30-01-A CATEGORY: C EXPIRATION: "MEL 78-30-01-A: ENGINE 1 THRUST REVERSER INOP. THRUST REVERSER IS DEACTIVATED IN FORWARD THRUST POFeb 17, 2006 · N664FE · Airbus A300F4605R · Engine Thrust ReverserSDR 05FDEA00154Pilot Valve · malfunctionedAFTER MOMENTARY RUNUP OF 60 PERCENT N1, APPLIED TOGA LEVERS & STANDARD POWER SET. ECAM SHOWED NR 1 THRUST REVERSER PRESSURIZED. REJECTED T/O AT 60 KNOTS. PREVIOUS WRITE-UP ON THRUST REVERSER. MEL 25JAN05. RELEASED FOR SERVICE PER MEL/CDL: 78-30-01-A CATJan 25, 2005 · N664FE · Airbus A300F4605R · Engine Thrust ReverserSDR 04FDEA02330Connector · damagedON TAKE OFF ROLL APPROX 60 KTS ECAM MOMENTARALY CAME ON. NR 2 ENG REV PRESSURIZED- INDICATION WENT OUT ABOUT 100 KTS AND CONTINUED NORMAL TAKE OFF. APPROX 800 AGL INDICATION RETURNED TO ECAM AND STAYED ON. PROCEDURE WAS FOLLOWED TO PULL NR 2 THROTTLE TO IDLEJul 31, 2004 · N664FE · Airbus A300* · Electrical ConnectorsSDR 04FDEA01936Hose · leakingON T/O OUT OF MEM , GOT YELLOW HYD RES: LOW AND HYD YELLOW PRESS LOW WARNINGS. COMPLIED WITH ECAM , REVIEWED QRH, AND RETURNED TO MEM. UPON INSPECTION FOUND RT WING AILERON INB MOSTACTUATOR HYD HOSE RUPTURED. ORDERED HOSES AND PLACED IN A/C FOR TURN OVER. Jul 5, 2004 · N664FE · Airbus A300B4605R · Hydraulic System, MainSDR 98FDEA00720Window · crackedCAPT L-1 WINDOW BEGAN ARCING PRIOR TO CRACKING SEVERELY ACROSS THE ENTIRE WINDOW. REMOVED AND REPLACED CAPT L-1 WIND AND TEMP CONTROLLER, PER M/M REF 30-42-11-4, OPS CKD GOOD.Dec 2, 1998 · N664FE · Airbus A300F4605R · Flight Compartment Windows
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