N607FE

Service difficulty reports · 454

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 = 'N607FE' 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 04FDEA02216Beam · corrodedRT MAIN LANDING GEAR TRUCK BEAM FOUND HEAVY PITTING AND CORROSION. REMOVED AND REPLACED AS PER MM 32-12-20-4. OPERATIONAL CHECK OF RT MAIN LANDING GEAR CARRIED OUT DURING RETRACTION AS PER MM 32-31-00-5, FOUND SATISFACTORY.Jul 28, 2004 · N607FE · Doug MD11 · Fuselage, Landing Gear Attach FittingsSDR 04FDEA02215Hinge · corrodedLT WING - OUTBOARD FLAP INBOARD HINGE (FLAP SIDE) HOLE NR 2 OUTBOARD SPOTFACE FOUND CORRODED. CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2 TO 4. ORIGINAL THICKNESS = 0.411, MATERIAL REMOVED = 0.005, REMAINING THICKNESS = 0.406 AND REPAIRED AS PER FEDEX EA 1-5Jul 28, 2004 · N607FE · Doug MD11 · Trailing Edge FlapsSDR 04FDEA02214Skin · corrodedLT WING UPPER SKIN FORWARD OF NR 4 SPOILER OUTBOARD HINGE FOUND CORRODED. BLENDED OUT CORROSION IAW SRM 51-21-01, VOLUME II AND FOUND OUT OF LIMIT AS IAW SRM 57-10-00, FIGURE 32, VOLUME I. ORIGINAL THICKNESS=0.180, MATERIAL REMOVED=0.020 AND REMAINING MATERJul 28, 2004 · N607FE · Doug MD11 · Wing, Plate/SkinSDR 04FDEA02213Hinge · corrodedLT WING UPPER WING SKIN FORWARD OF NUMBER 5 SPOILER CENTER HINGE FOUND CORRODED. BLENDED OUT CORROSION AS PER SRM 51-21-01, VOLUME II AND FOUND OUT OF LIMIT AS PER SRM 57-10-00Jul 28, 2004 · N607FE · Doug MD11 · SpoilersSDR 04FDEA02212Hinge · corrodedLT WING - OUTBOARD FLAP INBOARD HINGE (FLAP SIDE) HOLE NR 2 OUTBOARD BORE FOUND CORRODED. CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2 TO 4. ORIGINAL DIAMETER = 1.062, FINAL DIAMETER = 1.222 AND REPAIRED AS PER FEDEX EA 1-5750-80287, TITLE: WINGS - LT OUTBOARJul 28, 2004 · N607FE · Doug MD11 · Trailing Edge FlapsSDR 04FDEA02211Hinge · corrodedLT WING - OUTBOARD FLAP OUTBOARD HINGE (FLAP SIDE) HOLE NR 1 ACTUATOR INBOARD HOLE FOUND CORRODED. CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2 TO 4. ORIGINAL DIAMETER= 1.062, FINAL DIAMTER= 1.221 AND REPAIRED AS PER FEDEX EA 1-5750-80282, TITLE: WINGS - LT Jul 28, 2004 · N607FE · Doug MD11 · Trailing Edge FlapsSDR 04FDEA02210Hinge · corrodedLT WING - OUTBOARD FLAP INBOARD HINGE (FLAP SIDE) HOLE INBOARD BORE FOUND CORRODED. CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2 TO 4. ORIGINAL DIAMETER = 1.062, FINAL DIAMETER = 1.222 AND REPAIRED AS PER FEDEX EA 1-5750-80287, TITLE: WINGS - LT OUTBOARD FLAPJul 28, 2004 · N607FE · Doug MD11 · Trailing Edge FlapsSDR 04FDEA02209Hinge · corrodedLT WING - OUTBOARD FLAP INBOARD HINGE (FLAP SIDE) HOLE NR 1 INBOARD SPOTFACE FOUND CORRODED. CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2 TO 4. ORIGINAL THICKNESS = 0.413, MATERIAL REMOVED = 0.007, REMAINING THICKNESS = 0.406 AND REPAIRED AS PER FEDEX EA 1-Jul 28, 2004 · N607FE · Doug MD11 · Trailing Edge FlapsSDR 04FDEA02198Hinge · crackedLEFT HAND WING - OUTBOARD FLAP INBOARD HINGE (FLAP SIDE) MIDDLE FITTING FOUND CRACKED. ASSEMBLY REMOVED AND REPLACED AS PER MM 27-50-30-4 AND FLAP STRUCTURAL ADJUSTMENT/TEST CARRIED OUT AS PER MM 27-50-30-5, FOUND SATISFACTORY AND FLAP ADJUSTMENT/TEST CARRIED Jul 27, 2004 · N607FE · Doug MD11 · Trailing Edge FlapsSDR 04FDEA02197Doubler · crackedCENTER LANDING GEAR ZONE 146 LEFT HAND SIDE WALL STA 1380 DOUBLER CRACKED.REMOVED AND REPLACED WITH NEW DOUBLER AS PER SRM 51-31-01, VOLUME II.Jul 27, 2004 · N607FE · Doug MD11 · Fuselage Miscellaneous StructureSDR 04FDEA02196Doubler · crackedCENTER LANDING GEAR ZONE 146 RIGHT HAND SIDE WALL STA 1380 DOUBLER CRACKED. REMOVED AND REPLACED WITH NEW DOUBLER AS PER SRM 51-31-01, VOLUME II.Jul 27, 2004 · N607FE · Doug MD11 · Fuselage Miscellaneous StructureSDR 04FDEA02179Seat Track · damagedCABIN SEAT TRACK FOUND DAMAGED AT STA 910 LBL 48. AREA REMOVED AS PER SRM 53-70-00 FIG 1 VOL I & SRM 51-31-01 VOL II. REPAIR TRACK & PARTS FABRICATED & INSTALLED AS PER SRM 53-70- 00 FIG 1 VOL I & SRM 51-31-01 VOL II.Jul 26, 2004 · N607FE · Doug MD11 · Fuselage, Seat/Cargo Attach FittingsSDR 04FDEA02178Seat Track · damagedCABIN SEAT TRACK FOUND DAMAGED AT STA 894-910 RBL 48. DAMAGED AREA REMOVED AS PER SRM 53-70-00 FIG 1 VOL I & SRM 51-31-01 VOL II. REPAIR TRACK & PARTS FABRICATED & INSTALLED AS PER SRM 53-70-00 FIG 1 VOL I & SRM 51-31-01 VOL II.Jul 26, 2004 · N607FE · Doug MD11 · Fuselage, Seat/Cargo Attach FittingsSDR 04FDEA02177Seat Track · damagedCABIN SEAT TRACK FOUND DAMAGED AT STA 800 RBL 6. REMOVED AS PER SRM 53-70-00 FIG 1 VOL I & SRM 51-31-01 VOL II. REPAIR TRACK & PARTS FABRICATED & INSTALLED AS PER SRM 53-70-00 FIG 1 VOL I & SRM 51-31-01 VOL II.Jul 26, 2004 · N607FE · Doug MD11 · Fuselage, Seat/Cargo Attach FittingsSDR 04FDEA02176Seat Track · damagedCABIN SEAT TRACK FOUND DAMAGED AT STA 1169 LBL 48. REMOVED AS PER SRM 53-70- 00, FIGURE 1, VOLUME I AND 51-31-01, VOLUME II. REPAIR TRACK AND SPLICE FABRICATED, REWORKED AND INSTALLED AS PER SRM 53-70-00, FIGURE 1, VOLUME I AND 51-31-01, VOLUME II.Jul 26, 2004 · N607FE · Doug MD11 · Fuselage, Seat/Cargo Attach FittingsSDR 04FDEA02175Seat Track · damagedCABIN SEAT TRACK FOUND DAMAGED AT STA 1209 LBL 48. REMOVED AT STA 1266 TO LBL48 AS PER SRM 53-70-00, FIGURE 1, VOLUME I AND SRM 51-31-01, VOLUME II. REPAIR TRACK AND SPLICE FABRICATED, REWORKED AND INSTALLED AS PER SRM 53-70-00, FIGURE 1, VOLUME I AND Jul 26, 2004 · N607FE · Doug MD11 · Fuselage, Seat/Cargo Attach FittingsSDR 04FDEA02174Seat Track · damagedCABIN SEAT TRACK FOUND DAMAGED AT STA 1059 RBL 48. DAMAGED SEAT TRACK AT CABIN STA 1059 RBL 48 REMOVED AS PER SRM 51-31- 01 VOL II & SRM 53-70-00 FIG 1 VOL I. REPAIR TRACK & PARTS FABRICATED & INSTALLED AS PER SRM 53-70-00 FIG 1 VOL I & SRM 51-31-01 VOL IJul 26, 2004 · N607FE · Doug MD11 · Fuselage, Seat/Cargo Attach FittingsSDR 04FDEA02173Seat Track · damagedCABIN SEAT TRACK FOUND DAMAGED AT STA 1089 RBL 48. DAMAGED SEAT TRACK AT CABIN STA 1089 RBL 48 REMOVED AS PER SRM 53-70- 00 FIG 1 VOL I & SRM 51-31-01 VOL II. REPAIR TRACK & PARTS FABRICATED AS PER SRM 53-70-00 FIG 1 VOL I & SRM 51-31-01 VOL II.Jul 26, 2004 · N607FE · Doug MD11 · Fuselage, Seat/Cargo Attach FittingsSDR 04FDEA02172Seat Track · damagedCABIN SEAT TRACKS FOUND DAMAGED AT STA 1301 RBL 47. DAMAGED SEAT TRACK AT CABIN STA 1301 RBL 47 REMOVED AS PER SRM 53-70- 00 FIG 1 VOL I. REPAIR PARTS FABRICATED & ISNTALLED AS PER SRM 53-70-00 FIG 1 VOL I & SRM 51-31- 01 VOL II.Jul 26, 2004 · N607FE · Doug MD11 · Fuselage, Seat/Cargo Attach FittingsSDR 04FDEA02168Structure · crackedFORWARD TAIL CONE RIGHT HAND DOOR CUTOUT JAMB CRACKED. FORWARD TAILCONE RIGHT HAND DOOR CUT OUT CRACKED FRAMES AND DOUBLER REMOVED AS PER SRM 51-31-01 VOL II, AND NEW FRAMES AND DOUBLER INSTALLED AS PER SRM 51-35-01 VOL II.Jul 26, 2004 · N607FE · Doug MD11 · Fuselage Main, StructureSDR 04FDEA02171Seat Track · damagedCABIN SEAT TRACK FOUND DAMAGED AT STA 1259 RBL 48 AT 3 LOCATIONS. DAMAGED SEAT TRACK AT CABIN STA 1259 RBL 48 AT 3 LOCATIONS REMOVED AS PER SRM 53-70-00 FIG 1 VOL I & SRM 51-31-01 VOL II. REPAIR TRACK & PARTS FABRICATED & INSTALLED AS PER SRM 51-31-01 VOL IJul 26, 2004 · N607FE · Doug MD11 · Fuselage, Seat/Cargo Attach FittingsSDR 04FDEA02167Frame · crackedFORWARD TAIL CONE FORWARD FRAME CRACKED. REMOVED AND REPLACED AS PER SRM 51-35-01 VOL II.Jul 26, 2004 · N607FE · Doug MD11 · Aerodynamic FairingsSDR 04FDEA02170Seat Track · damagedCABIN SEAT TRACK FOUND DAMAGED AT STA 1089 RBL 28. REMOVED AS PER SRM 51-31- 01, VOLUME II AND SRM 53-70-00, FIGURE 1, VOLUME I. REPAIR TRACK AND PARTS FABRICATED AND INSTALLED AS PER SRM 53-70-00, FIGURE 1, VOLUME I AND SRM 51-31-01, VOLUME II.Jul 26, 2004 · N607FE · Doug MD11 · Fuselage, Seat/Cargo Attach FittingsSDR 04FDEA02169Skin · crackedFORWARD TAIL CONE RIGHT HAND FORWARD LOWER SKIN CRACKED. REMOVED AND REPLACED AS PER SRM 51-35-01 VOL II.Jul 26, 2004 · N607FE · Doug MD11 · Aerodynamic FairingsSDR 04FDEA02163Stop Fitting · crackedRT WING OUTBOARD FLAP STOP FITTING FOUND CRACKED 2 PLACES. REMOVED CRACKED STOP FITTING AS PER SRM 51-31-01, VOLUME II AND INSTALLED NEW FITTING AT RIGHT HAND WING OUTBOARD FLAP AS PER SRM 51-33-01, VOLUME II.Jul 23, 2004 · N607FE · Doug MD11 · Wing Main, Frame StructureSDR 04FDEA02162Fitting · crackedLT WING - OUTBOARD FLAP STOP FITTING CRACKED 2 PLACES. REPLACED AS PER MM 27-50-30- 4. ON P/N: NRC6753-503 AND ON S/N: 047. OFF P/N: NRC6753-503 AND OFF S/N: 006. FUNCTIONAL CHECK REFER TO SNRM N0508 FOR WORK DETAILS.Jul 23, 2004 · N607FE · Doug MD11 · Wing, Attach FittingsSDR 04FDEA02161Frame · crackedEMP - FORWARD TAIL CONE FRAME CRACKED.Jul 22, 2004 · N607FE · Doug MD11 · Aerodynamic FairingsSDR 04FDEA01216Controller · malfunctionedAT ALTITUDE LOST GOOD AIRSPEED INDICATIONS ON CADC2 AND STBY AIRSPEED INDICATORS CAPT HAD SWAPPED TO CADC2 EARLIER, GOT STICK SHAKER FOLLOWED BY BUFFET. CORRECTED FOR HIGH SPEED, SITUATION WORSENED. LOST ALL AIRSPEED INDICATIONS ON F/O, CAPT, AND STBY INDICAMay 10, 2004 · N607FE · Doug MD11 · Central ComputersSDR 03FDEA01920B-Nut · looseABOUT 2 HRS AFTER DEPARTURE NOTICED NR 1 OIL QTY DROPPING AND GOING TO ZERO. AT THAT TIME PRESSURE AND TEMP WERE NORMAL, 1 HR AFTER THAT NR 1 OIL PRESSURE STARTED A VERY SLOW DROP, EVENTUALLY TURNED AMBER. DIVERTED TO BKK. ON DESCENT PRESSURE DROPPED TO REDNov 17, 2003 · N607FE · Doug MD11 · Engine Oil Distribution (Airframe Furnished)SDR 03FDEA01117Reservoir · leakingDURING CRUISE, HYD 3 ELEV OFF LEVEL 1 LIGHT CAME ON AT 4.4 GAL, INDICATING THE 3-2 NRMP INOP. ONE HOUR LATER THE HYD 3 OFF LEVEL 1 ALERT LIGHT AT 2.5 GAL, CAME ON. TWO HOURS LATER THE HYD 3 FAIL LEVEL 2 ALERT LIGHT CAME ON AT 1.0 GAL. RESET ALT GEAR EXTENJul 19, 2003 · N607FE · Doug MD11 · Hydraulic Reservoir, MainSDR 03FDEA00080Fitting · crackedRT HORIZONTAL STAB NR 26 BARREL NUT HOLE FOUND FITTING WITH CRACK. COMPLIED WITH FEDEX EA 1-5510-67565, STABILIZERS, HORIZONTAL STABILIZER, BARREL NUT BORE 26 RT FITTING FABRICATION.Jan 27, 2003 · N607FE · Doug MD11 · Horizontal Stabilizer StructureSDR 03FDEA00129Hinge · corrodedLT WING OUTBOARD, FLAP OUTBOARD HINGE, (AIRFRAME SIDE) ACTUATOR HINGE, INBOARD AND OUTBOARD HINGE BORE CORRODED. REMOVED AND REPLACED OUTBOARD FLAP HINGE IAW EA. 1-5750-67564.Jan 21, 2003 · N607FE · Doug MD11F · Trailing Edge FlapsSDR 03FDEA00128Hinge · looseLT WING OUTBOARD FLAP, INBOARD HINGE (AIRFRAME SIDE) AT ACTUATOR HINGE INBOARD AND OUTBOARD BORE CORRODED. REMOVED AND REPLACED INBOARD FLAP HINGE IAW EA. 1-5750-67563.Jan 21, 2003 · N607FE · Doug MD11F · Trailing Edge FlapsSDR 03FDEA00095Hinge Bracket · corrodedSNRM N0957 - RT WING INBOARD FLAP, INBOARD AND OUTBOARD BORE OF THE FLAP SIDE OF THE HINGE BRACKET PIVOT BORES FOUND WITH CORROSION. ** S/D ** COMINGJan 20, 2003 · N607FE · Doug MD11F · Trailing Edge FlapsSDR 03FDEA00096Hinge Bracket · corrodedSNRM N0927, LT WING INBOARD FLAP OUTBOARD HINGE PIVOT BORES FOUND CORROSION. SNRM N0927 REPAIR CARRIED OUT AT LT WING INBOARD FLAP OUTBOARD HINGE PIVOT BORES IAW EA 1-5750-67559: WING TRAILING EDGE AND TRAILING EDGE DEVICES, LT INBOARD FLAP HINGE BRACKET REPAJan 19, 2003 · N607FE · Doug MD11F · Trailing Edge FlapsSDR 03FDEA00127Hinge · looseRT WING OUTBOARD FLAP, OUTBOARD HINGE, ACTUATOR HINGE, INBOARD AND OUTBOARD BUSHING (AIRFRAME SIDE) LOOSE. REMOVED AND REPLACED OUTBOARD FLAP HINGE IAW EA. 1-5750-67564.Jan 18, 2003 · N607FE · Doug MD11F · Trailing Edge FlapsSDR 03FDEA00046Rib · crackedLT WING NR 16 SLAT TRACK INBOARD STRUCTURAL RIB FOUND CRACKED (CRACK LENGTH APPROX 0.5 INCHES). REMOVED DAMAGED RIB NR 16 AND REPLACED NEW RIB NR 16 AT LT WING TRACK INBOARD STRUCTURAL AS PER SRM 51-33-01 VOL 2.Jan 15, 2003 · N607FE · Doug MD11 · Wing, Rib/BulkheadSDR 03FDEA00045Rib · crackedRT WING NR 16 SLAT TRACK INBOARD STRUCTURAL RIB CRACKED (CRACK LENGTH APPROX 0.5 INCHES). RT WING NR 16 TRACK I/B STRUCTURAL CRACK RIB REMOVED AND NEW RIB INSTALLED AS PER SRM 51-31-01 VOL 2. RIB FABRICATED AS PER DWG ARB 2850.Jan 14, 2003 · N607FE · Doug MD11 · Wing, Rib/BulkheadSDR 01FDEA00939Attach Fitting · out of positionRT WING INBOARD FLAP OUTBOARD HINGE ATTACH FITTING TO REAR WING SPAR MIGRATED. REMOVED AND REPLACED PER DWG ARB0621 & MM 27-50-20-4.Oct 29, 2001 · N607FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR 01FDEA00861Actuator · failedAFTER T/O AILERON DEFLECT DISAGREE ALERT DISPLAYED. CYCLED FLAPS NO HELP. R&R LT O/B DEF AILERON ACT ASSY.Sep 26, 2001 · N607FE · Doug MD11F · Aileron Control SystemSDR 01FDEA00532Aileron · malfunctionedDURING FLAP/SLAT RET AFT T/O (AIL DEFLECT DISAG) ALERT LVL 2 CK LIST COMPLIED. REINSTALLED P1-880 FOR PRECAUTION A/C STILL DEFER, AC RELEASE PER MEL.Jul 10, 2001 · N607FE · Doug MD11F · Aileron Control SystemSDR 01FDEA00513Warning System · malfunctionedANTI-SKID FAIL ALERT AFT ENGINES START. CYCLE ANTI-SKID CONTROL SYS NR 1 & 2 C/B'S. PER ASCU R-T-S ON ALL IND TEST. ALL TEST PASSED. A/C OK FOR SERVICE.Jun 30, 2001 · N607FE · Doug MD11F · Brake Anti-Skid SectionSDR 00FDEA00749Spar Cap · corrodedRT WING UPPER ACCESS PNL FWD OF NR 4 SPOILER LIFTED. CORRODED AT XORS 683 REAR SPAR TOP SURFACE PER SRM 51-21-01 VOL II. *S/D* BLENDED AS PER FEDEX EA 1-5750-53258.Oct 23, 2000 · N607FE · Doug MD11F · Wing SparSDR 00FDEA00731Seat Track · crackedMAIN DECK CARGO COMPARTMENT, FLOOR TRACK AT BS 635, RBL 25 FOUND CRACKED APPROX 4 INCHES LONG.Oct 23, 2000 · N607FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR 00FDEA00730Seat Track · crackedMAIN DECK CARGO COMPARTMENT, FLOOR TRACK AT BS 695, LBL 8.5 IN FOUND WITH CRACKED APPROX 3 INCHES LONG.Oct 23, 2000 · N607FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR 00FDEA00688Engine · failedNR 2 ENGINE FAILURE ON T/O FIRE IND AND SEVERE DAMAGE. RAN CKLIST, FIRE EXT ENGINE SECURED. *S/D* REPLACED ENGINE. OPS CK GOOD.Sep 29, 2000 · N607FE · Doug MD11F · Engine (Turbine/Turboprop)SDR 00FDEA00583Controller · malfunctionedON T/O, NR 2 ENG FIRE LIGHT ILLUM. NO OVERTEMPS WERE NOTED. FIRE IND CEASED WITH NR 2 THROTTLE IN IDLE. FIRE WARN LIGHT CHECK GOOD. REMOVED AND REPLACED FDCU 2 AND RTS OK AS PER MM 26-11-02-5. AC OK FOR SERVICE.Aug 23, 2000 · N607FE · Doug MD11F · Detection SystemSDR 99FDEA00517Compressor · stalled99-299, COMPRESSOR STALLS NR 3 ENG, FLT LEVEL 320.Dec 31, 1999 · N607FE · Doug MD11F · Turbine Engine Compressor SectionSDR 99FDEA00401Fitting · crackedSNRM 712, 719, 720, NR 4 BANJO FITTING CRACK AT RT - 712, 719, 720. REPAIR PER SRM 55-20-00 712, UPPER HOLE OVERSIZE NO CRACK FOUND 719, MID HOLE OVERSIZE NO CRACK FND 720.Sep 29, 1999 · N607FE · Doug MD11 · Vertical StabilizerSDR 98FDEA00767Coalescer Bag · contaminatedAFT T/O AC FILLED WITH SMOKE. EMER DECLARED. REMOVED AND REPLACED COALESCER BAGS IN ALL THREE AIR COND PACK SYS PER MM 21-54-05 LEAK CKD GOOD. RAN PACKS USING APU AND ENG AIR PER MD11 JRD, NO SMOKE PRESENT. A/C OK FOR SERVICE.Dec 27, 1998 · N607FE · Doug MD11 · Humidity Control System
Back to N607FE