N606FE

Service difficulty reports · 403

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 = 'N606FE' 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 04FDEA01967Hinge Bracket · corrodedRT WING, OUTBOARD FLAP INBOARD FORWARD HINGE, SIDE LINK MATING SURFACE FOUND CORRODED. RT WING, OUTBOARD FLAP INBOARD FORWARD HINGE, SIDE LINK MATING SURFACE CORROSION REMOVED AS PER CMM 57-44-08 PAGES 402-407. ORIGINAL THICKNESS=0.380 INCH, MATERIAL REMOVJul 6, 2004 · N606FE · Doug MD11F · Trailing Edge FlapsSDR 04FDEA01996Seat Track · wornMAIN DECK - SEAT TRACK CROWN AT STA 1795 - 1815, RBL 27.5 FOUND DAMAGED. MAIN DECK AT STA 1795 - 1815, RBL 27.5, SEAT TRACK REPAIR CARRIED OUT AS PER SRM 53-70-00 FIG 1 VOL I.Jul 6, 2004 · N606FE · Doug MD11 · Fuselage, Seat/Cargo Attach FittingsSDR 04FDEA01965Hinge Bracket · corrodedRT WING, OUTBOARD FLAP OUTBOARD FORWARD HINGE, INBOARD ACTUATOR HOLE FOUND CORRODED. RT WING, OUTBOARD FLAP OUTBOARD FORWARD HINGE, INBOARD ACTUATOR HOLE CORROSION REMOVED AS PER CMM 57-44-09 PAGES 402-407. ORIGINAL DIAMETER= 1.187 INCH, FINAL DIAMETER= 1.22Jul 6, 2004 · N606FE · Doug MD11F · Trailing Edge FlapsSDR 04FDEA01963Hinge Bracket · corrodedRT WING, OUTBOARD FLAP OUTBOARD FORWARD HINGE, PIVOT HOLE FOUND CORRODED. RT WING, OUTBOARD FLAP OUTBOARD FORWARD HINGE, PIVOT HOLE CORROSION REMOVED AS PER CMM 57-44-09 PAGES 402-407. ORIGINAL DIAMETER = 2.256 INCH, FINAL DIAMETER=2.329 INCH, AND REPAIREDJul 6, 2004 · N606FE · Doug MD11F · Trailing Edge FlapsSDR 04FDEA01962Hinge Bracket · corrodedRT WING, OUTBOARD FLAP OUTBOARD FORWARD HINGE, OUTBOARD LOWER MOUNT HOLE FOUND CORRODED. RT WING, OUTBOARD FLAP OUTBOARD FORWARD HINGE, OUTBOARD LOWER MOUNT HOLE CORROSION REMOVED AS PER CMM 57-44-09 PAGES 402-407. ORIGINAL DIAMETER = 0.516 INCH, FINAL DIAMEJul 6, 2004 · N606FE · Doug MD11F · Trailing Edge FlapsSDR 04FDEA01945Hinge Bracket · corrodedLEFT WING, OUTBOARD FLAP OUTBOARD FORWARD HINGE, OUTBOARD ACTUATOR HOLE FOUND CORRODED. LEFT WING, OUTBOARD FLAP OUTBOARD FORWARD HINGE, OUTBOARD ACTUATOR HOLE CORROSION REMOVED AS PER CMM 57-44-09 PAGES 402-407. ORIGINAL DIAMETER= 1.187 INCH, FINAL DIAMETJul 6, 2004 · N606FE · Doug MD11F · Trailing Edge FlapsSDR 04FDEA01944Hinge Bracket · corrodedLEFT WING, OUTBOARD FLAP OUTBOARD FORWARD HINGE, INBOARD ACTUATOR HOLE SPOT SURFACE FOUND CORRODED. LEFT WING, OUTBOARD FLAP OUTBOARD FORWARD HINGE, INBOARD ACTUATOR HOLE SPOT SURFACE CORROSION REMOVED AS PER CMM 57-44-09 PAGES 402-407. ORIGINAL THICKNESS=Jul 6, 2004 · N606FE · Doug MD11F · Trailing Edge FlapsSDR 04FDEA01943Hinge Bracket · corrodedLT WING, OUTBOARD FLAP OUTBOARD FORWARD HINGE, INBOARD ACTUATOR HOLE FOUND CORRODED. LT WING, OUTBOARD FLAP OUTBOARD FORWARD HINGE, INBOARD ACTUATOR HOLE CORROSION REMOVED AS PER CMM 57-44-09 PAGES 402-407. ORIGINAL DIAMETER= 1.187 INCH, FINAL DIAMETER= 1.Jul 6, 2004 · N606FE · Doug MD11F · Trailing Edge FlapsSDR 04FDEA01942Hinge Bracket · corrodedLT WING, OUTBOARD FLAP OUTBOARD FORWARD HINGE, SIDE LINK MATING SURFACE FOUND CORRODED. LEFT WING, OUTBOARD FLAP OUTBOARD FORWARD HINGE, SIDE LINK MATING SURFACE CORROSION REMOVED AS PER CMM 57-44-09 PAGES 402-407. ORIGINAL THICKNESS=0.495 INCH, MATERIAL REMJul 6, 2004 · N606FE · Doug MD11F · Trailing Edge FlapsSDR 04FDEA01941Hinge Bracket · corrodedLEFT WING, OUTBOARD FLAP OUTBOARD FORWARD HINGE, UPPER SIDE LINK HOLE FOUND CORRODED. LEFT WING, OUTBOARD FLAP OUTBOARD FORWARD HINGE, UPPER SIDE LINK HOLE CORROSION REMOVED AS PER CMM 57-44-09 PAGES 402-407. ORIGINAL DIAMETER= 0.323 INCH, FINAL DIAMETER= 0.Jul 6, 2004 · N606FE · Doug MD11F · Trailing Edge FlapsSDR 04FDEA01995Seat Track · wornMAIN DECK - SEAT TRACK CROWN AT STA 1801, RBL 27.5 FOUND DAMAGED. MAIN DECK AT STA 1801, RBL 27.5 SEAT TRACK REPAIR CARRIED OUT AS PER SRM 53-70-00 FIG 1 VOL I.Jul 6, 2004 · N606FE · Doug MD11 · Fuselage, Seat/Cargo Attach FittingsSDR 04FDEA01993Seat Track · wornMAIN DECK - SEAT TRACK CROWN AT STA 6-80, RBL 47.5 FOUND DAMAGED. MAIN DECK - DAMAGED SEAT TRACK AT STA 6-80, RBL 47.5 REMOVED FROM STA 1129 TO STA 7-0 RBL 4.75 AND REPLACED AS PER SRM 53-70-00 FIGURE 1 VOLUME 1 AND SRM 51-31-01 VOLUME 2.Jul 6, 2004 · N606FE · Doug MD11 · Fuselage, Seat/Cargo Attach FittingsSDR 04FDEA01992Seat Track · wornMAIN DECK - SEAT TRACK CROWN AT STA 6-20, RBL 47.5 FOUND DAMAGED. MAIN DECK - SEAT TRACK AT STA 6-20, RBL 47.5 REPAIRED AS PER SRM 53-70-00 FIGURE 1 VOLUME 1 AND SRM 51-31-01 VOLUME 2.Jul 6, 2004 · N606FE · Doug MD11 · Fuselage, Seat/Cargo Attach FittingsSDR 04FDEA01972Splice · crackedMAIN DECK - SPLICE FITTING AT RT STA 1531 LONGERON 14 CRACKED. MAIN DECK - SPLICE FITTING AT RT STA 1531 LONGERON 14 REMOVED AS PER SRM 51-31-01 VOLUME 2. NEW SPLICE FITTING FABRICATED AS PER DWG A5A7112 AND INSTALLED AS PER SRM 51-31-01 VOLUME 2.Jul 6, 2004 · N606FE · Doug MD11 · Fuselage Miscellaneous StructureSDR 04FDEA01964Hinge Bracket · corrodedRT WING, OUTBOARD FLAP OUTBOARD FORWARD HINGE, SIDE LINK MATING SURFACE FOUND CORRODED. RT WING, OUTBOARD FLAP OUTBOARD FORWARD HINGE, SIDE LINK MATING SURFACE CORROSION REMOVED AS PER CMM 57-44-09 PAGES 402-407. ORIGINAL THICKNESS=0.460 INCH, MATERIAL REMOJul 6, 2004 · N606FE · Doug MD11F · Trailing Edge FlapsSDR 04FDEA01976Hinge Bracket · corrodedLEFT WING, OUTBOARD FLAP INBOARD FORWARD HINGE, SIDE LINK MATING SURFACE FOUND CORRODED. LEFT WING, OUTBOARD FLAP INBOARD FORWARD HINGE, SIDE LINK MATING SURFACE CORROSION REMOVED AS PER CMM 57-44-08 PAGES 402-407. ORIGINAL THICKNESS=0.410 INCH, MATERIAL REMJul 6, 2004 · N606FE · Doug MD11F · Trailing Edge FlapsSDR 04FDEA01966Hinge · corrodedRIGHT WING - OUTBOARD FLAP OUTBOARD FORWARD HINGE, OUTBOARD ACTUATOR HOLE FOUND CORRODED.Jul 6, 2004 · N606FE · Doug MD11 · Trailing Edge FlapsSDR 04FDEA01902Support Fitting · corrodedRT OUTBOARD FLAP, INBOARD FLAP SIDE HINGE AT ATTACHMENT AREA, FORWARD MOUNT FITTING, OUTBOARD AFT HOLE FOUND CORRODED. RT OUTBOARD FLAP, INBOARD FLAP SIDE HINGE AT ATTACHMENT AREA, FORWARD MOUNT FITTING, OUTBOARD AFT HOLE REPAIRED PER FEDEX EA NR 1-5750-7675Jul 1, 2004 · N606FE · Doug MD11F · Trailing Edge FlapsSDR 04FDEA01903Fitting · corrodedRT OUTBOARD FLAP, INBOARD FLAP SIDE HINGE ATTACHMENT AREA, FORWARD MOUNT FITTING, THREE (3) HOLES FOUND CORRODED. RT OUTBOARD FLAP, INBOARD FLAP SIDE HINGE ATTACHMENT AREA, FORWARD MOUNT FITTING CORROSION REMOVED AS PER SRM 51-21-00 VOLUME II. (1) OUTBOARD MJul 1, 2004 · N606FE · Doug MD11F · Trailing Edge FlapsSDR 04FDEA01908Hinge · corrodedRIGHT OUTBOARD FLAP OUTBOARD FLAP SIDE HINGE ATTACHMENT AREA FORWARD MOUNT FITTING OUTBOARD AFT HOLE FOUND CORRODED. CORROSION REMOVED PER SRM 51-21-01 VOLUME II. ORIGINAL DIAMETER = 0.443, FINAL DIAMETER = 0.517. COMPLIED WITH FEDEX EA 1-5750-76755, WINGS - Jul 1, 2004 · N606FE · Doug MD11 · Trailing Edge FlapsSDR 04FDEA01907Hinge · corrodedRIGHT OUTBOARD FLAP OUTBOARD FLAP SIDE HINGE ATTACHMENT AREA FORWARD MOUNT FITTING INBOARD MIDDLE HOLE FOUND CORRODED. CORROSION REMOVED PER SRM 51-21-01 VOLUME II. ORIGINAL DIAMETER = 0.458, FINAL DIAMETER = 0.517. COMPLIED WITH FEDEX EA 1-5750-76755, WINGS Jul 1, 2004 · N606FE · Doug MD11 · Trailing Edge FlapsSDR 04FDEA01906Hinge · corrodedRIGHT OUTBOARD FLAP INBOARD FLAP SIDE HINGE ATTACHMENT AREA FORWARD MOUNT FITTING OUTBOARD AFT HOLE FOUND CORRODED. CORROSION REMOVED PER SRM 51-21-01 VOLUME II. ORIGINAL DIAMETER = 0.521, FINAL DIAMETER = 0.620. COMPLIED WITH FEDEX EA 1-5750-76755, WINGS - RJul 1, 2004 · N606FE · Doug MD11 · Trailing Edge FlapsSDR 04FDEA01905Hinge · corrodedRIGHT OUTBOARD FLAP INBOARD FLAP SIDE HINGE ATTACHMENT AREA FORWARD MOUNT FITTING INBOARD AFT HOLE FOUND CORRODED. CORROSION REMOVED PER SRM 51-21-01 VOLUME II. ORIGINAL DIAMETER = 0.568, FINAL DIAMETER = 0.628. COMPLIED WITH FEDEX EA 1-5750-76755, WINGS - RJul 1, 2004 · N606FE · Doug MD11 · Trailing Edge FlapsSDR 04FDEA01904Hinge · corrodedRIGHT OUTBOARD FLAP INBOARD FLAP SIDE HINGE ATTACHMENT AREA FORWARD MOUNT FITTING INBOARD MIDDLE HOLE FOUND CORRODED. CORROSION REMOVED PER SRM 51-21-01 VOLUME II. ORIGINAL DIAMETER = 0.568, FINAL DIAMETER = 0.656. COMPLIED WITH FEDEX EA 1-5750-76755, WINGS -Jul 1, 2004 · N606FE · Doug MD11 · Trailing Edge FlapsSDR 04FDEA01897Rib · crackedRIGHT WING, FOUND OUTBOARD FLAP, ATTACHING RIB STOP FITTING CRACKED. RIGHT WING, FOUND OUTBOARD FLAP, ATTACHING RIB STOP FITTING REMOVED AND REPLACED AS PER SRM 51-33-01 VOL 2.Jun 30, 2004 · N606FE · Doug MD11 · Wing, Rib/BulkheadSDR 03FDEA02199Coalescer Bag · damagedDEPARTED CDG, ENGINE ANTI-ICE ON MAX PWR AT 3000 AGL SMOKE ODOR DETECTED THEN SMOKE ENTERED THE COCKPIT TURNED ON THE LIGHTS AND THE COCKPIT HAUL FILLED WITH SMOKE. WENT ON OXYGEN, RAN APPROPIATE CHECKLISTS. RAN NR 1 ENG FOR 20 MIN AND HAD A VERY LITE ODOR.Dec 16, 2003 · N606FE · Doug MD11 · Humidity Control SystemSDR 02FDEA00981Seat Track · damagedMAIN CABIN, SEAT TRACK DAMAGED AT FS 1350.5 X=-47.50. TRIMMED OUT DAMAGED SEAT TRACK IAW SRM. FABRICATED SEAT TRACK AND SPLICE HAT IAW SRM. INSTALLED SEAT TRACK AND SPLICE HAT IAW SRM.Dec 30, 2002 · N606FE · Doug MD11 · Fuselage, Seat/Cargo Attach FittingsSDR 02FDEA00967Stringer · crackedMAIN DECK CARGO COMPARTMENT, RIGHT FUSELAGE FRAME, BS Y 1139-1159, STRINGER 17, CRACKED. R/R MDCC RT FUSELAGE FRAME BS Y 1139-1159 STRINGER.Dec 26, 2002 · N606FE · Doug MD11 · Fuselage Main, Longeron/StringerSDR 02FDEA00966Seat Track · corrodedMDCC FLOOR SEAT TRACK FOUND WITH CORROSION AT STA 585 - 685, X=-107.25. TRIMMED DAMAGED AREA ON FLANGE AT STA 653 RBL 107.25 IAW SRM. FABRICATED FILLER AND STRAP IAW SRM. INSTALLED FILLER AND STRAP IAW SRM.Dec 23, 2002 · N606FE · Doug MD11 · Fuselage, Seat/Cargo Attach FittingsSDR 02FDEA00965Seat Track · corrodedMDCC FLOOR SEAT TRACK FOUND WITH CORROSION AT STA 585, 685 X -75.25. TRIMMED OUT DAMAGED AREA ON SEAT TRACK FLANGE IAW SRM, FABRICATED FILLER AND STRAP IAW SRM. INSTALLED FILLER AND STRAP IAW SRM.Dec 23, 2002 · N606FE · Doug MD11 · Fuselage, Seat/Cargo Attach FittingsSDR 02FDEA00980Stringer · crackedMDCC FUSELAGE FRAME STA 1139-1159, STRINGER 17R, FOUND WITH CRACK.Dec 20, 2002 · N606FE · Doug MD11 · Fuselage Main, Longeron/StringerSDR 02FDEA00963Strap · corrodedMDCC LT FUSELAGE FRAME STA Y 1199 STR 16 FOUND TIE STRAP WITH CORROSION.Dec 20, 2002 · N606FE · Doug MD11 · Fuselage Miscellaneous StructureSDR 02FDEA00962Seat Track · corrodedMDCC FLOOR SEAT TRACK FLANGE FOUND WITH CORROSION AT STA 1521, LBL 8. TRIMMED CORRODED FLANGE AT STA 1521, LBL 8 IAW SRM. NON DESTRUCTIVE TESTING CARRIED OUT AT TRIMMED AREA IAW DAC NDT SPM. FAB FILLER AND STRAP IAW SRM. INSTALLED IAW SRM.Dec 20, 2002 · N606FE · Doug MD11 · Fuselage, Seat/Cargo Attach FittingsSDR 02FDEA00946Rib · crackedLT WING L/E SLAT TRACK NR 16 I/B STRUCTURAL RIB FOUND CRACKED APPROX 0.125 INCH.Dec 16, 2002 · N606FE · Doug MD11 · Leading Edge DevicesSDR 02FDEA00945Rib · crackedRIGHT WING LEADING EDGE SLAT TRACK NR 16 INBOARD STRUCTURAL RIB FOUND CRACKED APPROXIMATELY (0.125).Dec 15, 2002 · N606FE · Doug MD11 · Leading Edge DevicesSDR 02FDEA00012Bolt · looseDURING PFM NR 61 B-CK FOUND BOTH LT & RT AFT MOUNTING BOLT OF CTR LANDING GEAR TRUNNION PIN PILLOW BLOCK LOOSE.Jan 1, 2002 · N606FE · Doug MD11F · Main Landing Gear Attach SectionSDR 00FDEA00660Seat Track · crackedCABIN MAIN DECK CARGO SEAT TRACK FLANGE FOUND CRACKED ALONG BS 755, LBL 47. *S/D* REMOVED AND REPLACED PER IAW SRM 53-42-01 VOL III.Sep 11, 2000 · N606FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR 00FDEA00659Seat Track · crackedCABIN MAIN DECK CARGO SEAT TRACK FLANGE AREA FOUND CRACKED ALONG LBL 47, BETWEEN BS 925 & 935. *S/D* REMOVED AND REPLACED PER IAW SRM 53-42-01 VOL III & 53-70-00 VOL I.Sep 11, 2000 · N606FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR 00FDEA00658Seat Track · crackedCABIN MAIN DECK CARGO SEAT TRACK FLANGE FOUND CRACKED ALONG BS 7552 LBL 28. *S/D* REMOVED AND REPLACED PER IAW SRM 53-42-01 VOL III & 53-70-00 VOL I.Sep 11, 2000 · N606FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR 00FDEA00657Seat Track · crackedCABIN MAIN DECK CARGO SEAT TRACK FLANGE FOUND CRACKED ALONG BS 755, RBL 9. *S/D* REMOVED AND REPLACED PER IAW SRM 53-42-01 VOL III & 53-70-00 VOL I.Sep 11, 2000 · N606FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR 00FDEA00656Seat Track · crackedCABIN MAIN DECK CARGO SEAT TRACK FLANGE FOUND CRACKED AT 2 PLACES, ALONG RBL 45, BETWEEN BS 969 & 999. *S/D* REMOVED AND REPLACED PER 53-42-01 VOL III & 53-70-00 VOL I.Sep 11, 2000 · N606FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR 00FDEA00655Seat Track · crackedCABIN MAIN DECK CARGO SEAT TRACK FLANGE AREA FOUND CRACKED ALONG BS 755, LBL 9. *S/D* REMOVED AND REPLACED PER IAW SRM 53-42-01 VOL III & SRM 53-70-00 VOL I.Sep 11, 2000 · N606FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR 00FDEA00523Relay · failedLEVEL 2 ALERT IN-FLT AILERON DEFLECT DISAGREE. *S/D* REMOVED AND REPLACED RELAY R2-5060 PER SMP. REMOVED AND REPLACED FLAP HANDLE POS TRANSMITTER PER MD-11 MM 27-54-03. OPS CK OK.Aug 6, 2000 · N606FE · Doug MD11F · Aileron Control SystemSDR 99FDEA00285Wire · damagedSNRM 322,444,321 - FWD CARGO EXTERNAL PWR CABLE NR C507-3-OC (AL), FOUND INSULATION BREAKDOWN AND OH SIGN (ARCING) AT BS 899, LBL 20 BELOW FLOORBOARD. INSULATION BLANKET AT BILGE AREA BURNT. REMOVED AND REPLACED EXT PWR SYS OPER CK FOUND SATISFACTORY PER 24-Jul 27, 1999 · N606FE · Doug MD11F · Electrical Power System WiringSDR 99FDEA00280Seat Track · crackedFOUND CRACK ON SEAT TRACK. SEAT TRACK SPLICE CUT AND REWORKED PER SRM 53-42-01.Jul 26, 1999 · N606FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR 99FDEA00124Warning Light · illuminatedAIL DEFLECT DISAG LVL 2 ALERT ON FLAP RETRACTION, STAYED ON SLAT RETRACTION, GOES AWAY WHEN FLAPS EXT FOR LANDING. A/C RELEASED FOR SERV PER MEL/CDL 27-2 CATEGORY C EXP 4APR99 FCC1-FCC2 REPT NO FAULTS LAST LEG. PERF'D FCC1/FCC2 AIL SYS TEST PER MM 22-00-00-8Mar 26, 1999 · N606FE · Doug MD11F · Aileron Control SystemSDR 97FDEA00142Bulkhead Doubler · crackedCENTER L/G, RT BULKHEAD DRAG LINK SUPPORT WEB DOUBLER IS CRACKED AFT RT DRAG LINK ATTACH POINT, VERIFIED BY NDT. REMOVED AND REPLACED SUPPORT WEB DOUBLER PER SRM 51-00-01 VOL II.Mar 2, 1997 · N606FE · Doug MD11 · Emergency Flotation SectionSDR 97FDEA00126Bulkhead Doubler · crackedN 00081, CENTER L/G, RT BULKHEAD DRAG LINK SUPPORT WEB DOUBLER IS CRACKED AFT RT DRAG LINK ATTACH POINT. VERIFIED BY NDT. *S/D* REMOVED AND REPLACED SUPPORT WEB DOUBLER PER SRM 51-00-01 VOL II. REPAIR COMPLIED WITH ON 03-06-1997.Mar 2, 1997 · N606FE · Doug MD11 · Emergency Flotation SectionSDR 97FDEA00018Fire Detector · malfunctionedAPPROACHING NRT, CARGO FIRE LOWER AFT ALERT DISPLAYED, AGENT DISCHARGED IAW PROCEDURE. AFTER LANDING NO INDICATION OF FIRE OBSERVED. ALERT OCCURRED AT 3,000 FEET, CARGO TEMPERTURE NORMAL. FOUND NO FAULTS ON CURRENT AND FAULT REVIEW IN MSC AND DEU 1, 2, 3. Jan 5, 1997 · N606FE · Doug MD11F · Fire DetectionSDR 95FDEA01697Harness · chafedNR 1 ENG ELECTRICAL HARNESS, BLACK AT THE SIX O'CLOCK POSITION IS CHAFING HARD AGAINST TRAIN LINES THROUGH THE COATING AND WIRE MESH. REMOVED AND REPLACED CABLE (P/N 7161M60G04) INSTALLED PER MM 71-50-04-4-1. PERFORMED POWER ASSURANCE RUN REQUIRED PER MM 71-Nov 6, 1995 · N606FE · Doug MD11 · Electrical Power System
Back to N606FE