N616FE

Service difficulty reports · 267

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 = 'N616FE' 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 02FDEA00309Relay · failedON APPROACH PRIMARY & SECONDARY GEAR IND UNSAFE (RED). REMOVED AND REPLACED GEAR HANDLE INTERLOCK RELAY-3 FOR PRIMARY GEAR POS IND SYS PER MM 32-31-00. RESET ALTERNATE GEAR EXTENSION LEVER PER MM 32-32-00.May 6, 2002 · N616FE · Doug MD11F · Landing Gear Retraction/Extension SystemSDR 01FDEA00601Frame · crackedLT FRAME AT BS 1761, STR 12 FOUND WITH 4.25 INCH CRACK. *S/D* REMOVED AND REPLACED FRAME PER SRM 53-30-00 FIG 3 VOL 1.Jul 24, 2001 · N616FE · Doug MD11F · Fuselage Main, FrameSDR 01FDEA00612Frame · crackedLT FRAME AT BS 1621 STR 12 FOUND 3 INCH CRACK. *S/D* REMOVED AND REPLACED FRAME PER SRM 53-30-30 FIG 1 VOL 1.Jul 24, 2001 · N616FE · Doug MD11F · Fuselage Main, FrameSDR 01FDEA00512Warning Light · illuminatedTAXI OUT RT OUTBOARD FLAP SHOW AMBER X NO GREEN BOX DURING FLT CONTROL CK FOR RT SPOILER. AFTER FLAP RETRACTION, RT FLAP IND SHOW 0 AND AN AMBER X.Jun 30, 2001 · N616FE · Doug MD11F · Trailing Flap Position Indicating SystemSDR 01FDEA00505Control Cable · disconnectedDURING WALKAROUND, FOUND CABLE HANGING FROM LEFT INBD FLAP FAIRING.Jun 26, 2001 · N616FE · Doug MD11F · Trailing Edge Flap Control SystemSDR 01FDEA00042Turbine · damagedON T/O, NR 1 ENG HAD SEVERE VIBRATION AND EVM TURBINE INDICATIONS. NO REDUCTION WITH REDUCED POWER, SECURED NR 1 ENGINE AND RETURNED TO PEK. MX FOUND METAL IN TAILPIPE AND LAST STAGE TURBINE SEVERELY DAMAGED. *S/D* REMOVED AND REPLACED NR 1 ENG PER WORK CAJan 24, 2001 · N616FE · Doug MD11F · Turbine SectionSDR 00FDEA00619Igniter · failedNR 1 ENG FLAMED OUT WHILE DESCENDING. RPM LO ALERT IGN OVERRIDE WAS ON AT TIME OF FLAME-OUT. REMOVED AND REPLACED A SYS IGN BOX AND FUEL FILTER PRECAUTIONARY PER MM 74-10-01 AND MM 73-11-02.Sep 1, 2000 · N616FE · Doug MD11F · Ignition SystemSDR 00FDEA00533Generator · failedAFT T/O AT APPROX 500 FT ADG DEPLOYED. RETURNED TO HKG. NORMAL LANDING. ADJUSTED AIR DRIVEN GENERATOR, ADG DEPLOY AND STOW OK.Aug 9, 2000 · N616FE · Doug MD11F · AC Generation SystemSDR 00FDEA00537Generator · deployedUPON ARRIVAL FOUND ADG DEPLOYED. STOWED THE AIR DRIVEN GENERATOR AS PER MM 24-25-01-2. ACFT OK FOR SERVICE.Aug 8, 2000 · N616FE · Doug MD11F · AC Generation SystemSDR 00FDEA00511Generator · will not testAIR DRIVEN GENERATOR WOULD NOT DEPLOY DURING TEST FLIGHT. *S/D* REMOVED AND REPLACED ROLLER PER CMM 24-27-06. ADG DEPLOY AND STOW FUNCTIONAL CK PER MM 24-25-01-02 FOUND SATISFACTORY.Aug 2, 2000 · N616FE · Doug MD11F · AC Indicating SystemSDR 00FDEA00483Actuator · dislodgedVERTICAL STAB LWR RUDDER ACTUATOR UPPER ATTACHMENT BLOCK ASSY FOUND BUSHING, WASHER RETAINER AND ATTACHMENT BOLT FOUND DISLODGED. *S/D* REMOVED AND REPLACED PARTS PER AMM 20-50-02.Jul 24, 2000 · N616FE · Doug MD11F · Rudder ActuatorSDR 00FDEA00510Floor Support · corrodedCORROSION FOUND AROUND FLOOR SUPPORT ALONG BS 415 LHS JUST AFT OF COURIER SEAT AREA AS MARKED. REMOVED AND REPLACED, FAB AND INSTALLED PER EA 1-5320-52065, FUSELAGE - AUXILIARY STRUCTURE - SUPPORT REPAIR.Jul 24, 2000 · N616FE · Doug MD11F · Fuselage Miscellaneous StructureSDR 00FDEA00417Duct · cracked00-172- NR 2 ENGINE FIRE LIGHT & HORN CAME ON. DUMPED FUEL TO 60,000 LBS. & LANDED. FIRE LIGHT WENT OUT AFTER THROTTLE WAS PULLED TO IDLE. R&R BLOWN & CRACKED DUCTING PER JRH 4,5,6,7 DPM 112721. NR 2 EVM OPS NORMAL NO OTHER DEFECTS NOTED.Jul 1, 2000 · N616FE · Doug MD11F · Engine Bleed Air SystemSDR 99FDEA00495Transmitter · failed99-279 - DURING CLIMB, NR 1 ENG OIL PRESS DROPPED TO 0. REMOVED AND REPLACED NR 1 ENG OIL PRESS TRANSMITTER PER MM 79-33-01-4. OPS CK SATISFACTORY.Dec 3, 1999 · N616FE · Doug MD11F · Engine Oil QuantitySDR 99FDEA00217Floorbeam · crackedFWD CARGO DOOR ENTRY MID UPPER FLOORBEAM LWR CHORD AT BS 939, X=78.0, RHS FOUND WITH ABOUT ONE-INCH CRACK AND DENT. *S/D* CARRIED OUT REPAIR ON FWD CARGO DOOR IN ACCORDANCE WITH FEDEX AUTH NR 1-5310-42383.Jun 14, 1999 · N616FE · Doug MD11F · Fuselage Main, Floor BeamSDR 98FDEA00696Transmitter · inopFLAP DISAGREE ALERT, LEFT FLAP SHOW 20 DEG, RT FLAP SHOW 25 DEG. ACCOMP FLAP 25 LAND AT PANC FLAP HANDLE REMAIN AT T/O. REMOVED AND REPLACED LT O/B FLAP POS TRANSMITTER AS PER MM 27-54-02-4 IND SAT AS PER ADJ TEST.Nov 14, 1998 · N616FE · Doug MD11F · Trailing Edge Flap Control SystemSDR 97FDEA00172Prox Switch · failedAFTER TAKEOFF, WE GOT AN UNSAFE CENTER GEAR ON CONFIG PAGE. RECYCLED GEAR UNSAFE UP AND DOWN CENTER GEAR ON CONFIG PAGE. SAFE UP AND DOWN ON GEAR LIGHTS. RETURNED TO NRT DUE ATC UNABLE 240 TO 250 FOR SPEED POSITION. PERFORMED BITE TEST ON PROXIMITY SWITCH Mar 16, 1997 · N616FE · Doug MD11F · Landing Gear Position and Warning
Back to N616FE