N617FE

Service difficulty reports · 467

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 = 'N617FE' 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 02FDEA00667Frame · crackedFUSELAGE TRANSVERSE FRAME AT STA Y-1701 RT SIDE DENTED & CRACKED APPROX 2 INCHES LONG. R&R FRAME PER SRM 53-30-00 VOL I.Sep 17, 2002 · N617FE · Doug MD11 · Fuselage Main, FrameSDR 02FDEA00657Frame · crackedFUSELAGE TRANSVERSE FRAME LT CRACKED AT 2 PLACES STA Y= 535, LONGERON 19L-20L WAS 1.531 INCHES AND AT LONGERON 23L-24L WAS 2.781 INCHES. R&R FRAME PER DWG SRZ-53-503, SRM 51-21-01 VOL II.Sep 17, 2002 · N617FE · Doug MD11 · Fuselage Main, FrameSDR 02FDEA00656Seat Track · corrodedFWD CABIN BOTTOM OF PORTABLE FIRE EXTINGUISHER MOUNTING BRACKET, FOUND SEAT TRACK CORRODED AT BS 475-495. R&R SEAT TRACK PER SRM 51-33-01 VOL II.Sep 16, 2002 · N617FE · Doug MD11 · Fuselage, Seat/Cargo Attach FittingsSDR 02FDEA00010Fire Warning · activated2-2 ALERT BELL NR 2 THROTTLE TO IDLE AND LIGHT WENT OUT. ENGINE IND NORMAL. SHUTDOWN NR 2.Jan 4, 2002 · N617FE · Doug MD11F · Fire DetectionSDR 01FDEA01102Warning System · malfunctionedON FINAL FLAPS GOT DISAGREE ALERT. CHECKED CFDS, NO FAULT FOUND PERFORMED TEST ON PSEU PER FIM 31-71-07-00.Dec 24, 2001 · N617FE · Doug MD11F · Trailing Flap Position Indicating SystemSDR 01FDEA00369Stall Warning · faultyON SHORT FINAL GOT STICK SHAKER. AMBER SLATS WERE ILLUM ON PFD. PREF RTS ON FCC NR 1 AND 2 AOA TESTS AND AUTOLAND TESTS ALL PASSED OK TO CONTINUE.May 13, 2001 · N617FE · Doug MD11F · Stall Warning SystemSDR 01FDEA00292Pump · overtempAFT T/O HYD NR 2 LEFT PUMP OFF FOR HIGH TEMP. SWITCH TO AUTO PUMPS TURNED OFF, TEMP WENT BACK UP AGAIN.Apr 20, 2001 · N617FE · Doug MD11F · Hydraulic Pump (Electric/Engine), MainSDR 01FDEA00257Sensing Element · faultyLEVEL 3 ENG 2 A-ICE DUCT ALERT IND. SHUTDOWN ENG 3. *S/D* REMOVED AND REPLACED SENSING ELEMENT D190 (LOWER SIDE) PER MD11 MM 30-22-11-4.Apr 7, 2001 · N617FE · Doug MD11F · Air Intake Anti/De-Ice SystemSDR 00FDEA00789Manifold · brokenLEVEL 1 ALERT HYDRO 2 QTY LOW. FOUND HYD LEAK FROM NR 2 EDP MANIFOLD ASSY. REMOVED AND REPLACED PER MM 29-12-30-21, 29-11-20. NO LEAK FOUND.Nov 24, 2000 · N617FE · Doug MD11F · Hydraulic System, MainSDR 00FDEA00550Engine · overheatedON T/O, NR 1 ENGINE OVERHEATED (MASTER CAUTION, LEVEL 3 ALERT). REMAIN HIGH UNTIL THROTTLE RETURN TO IDLE, ENGINE SHUTDOWN. NO LEAK AND CRACK NOTED. EGT WITHIN LIMIT PER JRH ENGINE TEST AND CKS PG 608 FIG 3. CLOSED NR 1 ENGINE PER MM 71-1-00. AC OK FOR SEAug 15, 2000 · N617FE · Doug MD11F · Engine Temperature Indicating SystemSDR 00FDEA00549Engine · overheatedON T/O MSL ENGINE OVERHEATED (MASTER CAUTION & EGT ALERT) REACH 966C. REMAIN HIGH, ENG SHUTDOWN.Aug 15, 2000 · N617FE · Doug MD11F · Engine Temperature Indicating SystemSDR 99FDEA00257Seat Track · crackedSNRM 431, 430, 355, 354 CRACK ON SEAT TRACK BS 635, X=8.5 RT, X=47.5 RT, X=27.5 LT, X=47.5 LT. REPAIRED SEAT TRACK IN ACCORD WITH SRM 53-70-00.Jul 12, 1999 · N617FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR 99FDEA00130Filters · contaminatedLEVEL 1 ENG 3 FUEL FILTER ALERT AND LEVEL 1 FUEL CONTAMINATION ALERT DISPLAY. CREW DUMP FUEL TO REDUCE DOWN TO MAX WT. REMOVED AND REPLACED ALL THREE ENG FILTERS PER 73-11-04-04-1.Apr 2, 1999 · N617FE · Doug MD11F · Engine Fuel DistributionSDR 98FDEA00565Fire Loop · failed98-219 - FIRE DET 2 FAIL ILLUM ON T/O B LOOP WAS PLACARD INOP FOR DISPATCH. REMOVED AND REPLACED A LOOP HARNESS 224W9726-517. REMOVED AND REPLACED UPPER LT DET ASSY P/N 224-9743-509, SYS, OPS CHECK GOOD.Sep 8, 1998 · N617FE · Doug MD11F · Fire DetectionSDR 96FDEA00526Retract Mech · slowARRIVAL, GEAR HANDLE DOWN AND IN-GEAR DID NOT EXTEND ALL RED LIGHT, CONFIRMED GEAR WAS STILL UP ON CONFIG PAGE. CYCLE GEAR, GEAR CAME DOWN MUCH SLOWER THAN NORMAL, NOSE FIRST, CENTER, THEN MAIN. HYDRO PRESS NORMAL.Mar 18, 1996 · N617FE · Doug MD11 · Landing Gear Retraction/Extension SystemSDR 95DEA001893Nose Cowl · separatedEN ROUTE FROM VANCOUVER TO MEMPHIS, THE TOP OF THE NR 2 ENGINE INTAKE COWLING SEPARTED FROM THE AIRCRAFT, RESULTING IN DAMAGE TO NOSE COWL AND THE LEADING EDGE OF THE VERTICAL STABILIZER. NOSE COWL REMOVED AND REPLACED. BULKHEAD BLANKETS REPLACED AND REPAIREDec 20, 1995 · N617FE · Doug MD11F · Engine Cowling SystemSDR 95FDEA01893Intake Cowl · separatedEN ROUTE FROM VANCOUVER TO MEM, THE TOP OF THE NR 2 ENGINE INTAKE COWLING SEPARATED FROM THE A/C RESULTING IN DAMAGE TO THE NOSE COWL AND THE LEADING EDGE OF THE VERTICAL STABILIZER.Dec 11, 1995 · N617FE · Doug MD11F · Engine Cowling System
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