N367FE

Service difficulty reports · 138

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.

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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 = 'N367FE' AND registry_match = 'registration'
  ORDER BY difficulty_date DESC"

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SDR 06FDEA03194Door Frame · damagedINTERNAL FUSELAGE MAIN CABIN STA 1249-1254 BETWEEN LONG 26 LT TO 27 L3 DOOR JAMB EXISTING REPAIR REMOVER AND REPAIRED IAW SRM 53-50-00 FIG 19 VOL 1.Sep 6, 2006 · N367FE · Doug DC1010 · Fuselage Main, StructureSDR 06FDEA03193Skin · damagedEXTERNAL FUSELAGE AT STA 415 X=-8 LT SIDE LWR SIDE EXISTING REPAIR REMOVED AND REPLACED REPAIR IAW SSRM 53-20-00 FIG 6 VOL 1.Sep 6, 2006 · N367FE · Doug DC1010 · Fuselage Main, Plate/SkinSDR 06FDEA2842Frame · corrodedAIR CONDITIONING COMPT LT FOUND CORROSION WITH EXF ON FRAME AT STA 501 X= 30. REPAIRED FRAME IAW SRM 53-30-00 VOL 1 FIG 5 (REF SRM 53-00-01 VOL 1 FIG 8 ). FABRICATED PARTS IAW DETAIL PARTS TRAVELER I016366/N01366 & IAW SRM 53-30-00 VOL 1 FIG 5.Aug 4, 2006 · N367FE · Doug DC1010 · Fuselage Main, FrameSDR 06FDEA2841Frame · corrodedAIR CONDITIONING COMPT LT FOUND CORROSION WITH EXF ON FRAME AT STA 547 X= 30. REPAIRED FRAME IAW SRM 53-30-00 VOL 1 FIG 5 (REF SRM 53-00-01 VOL 1 FIG 8). FABRICATE PARTS IAW DETAIL PARTS TRAVELER I016354/N01354 & IAW SRM 53-30-00 VOL 1 FIG 5.Aug 4, 2006 · N367FE · Doug DC1010 · Fuselage Main, FrameSDR 06FDEA2840Seat Track · crackedMAIN CABIN AT STA 475 X= - 8.5 Z= -19 ON SEAT TRACK FOUND CRACK 5 INCHES LONG. REMOVED AND REPLACED TRACK IAW SRM 53-70-00 AND REPLACED CHANNEL IAW SRM 51-35-01 VOL 1.Aug 4, 2006 · N367FE · Doug DC1010 · Fuselage, Seat/Cargo Attach FittingsSDR 06FDEA2825Intercostal · crackedAIR CONDITIONING COMPT LT FOUND 1 EA CRACK 2 INCHES LONG ON INTERCOSTAL AT STA 587 Z= -53 X= 70. CUT LOWER JAMB OF AFTER DOOR CUTOUT APPROX MIDWAY AND INSTALLED REPAIR JAMB IAW SRM 53-00-01 VOL 1 FIG 8 SHT 2. FABRICATED PARTS IAW DETAIL PARTS TRAVELER I01634Aug 3, 2006 · N367FE · Doug DC1010 · Fuselage Miscellaneous StructureSDR 06FDEA2823Intercostal · crackedAIR CONDITIONING COMPT LT FOUND 1 EA CRACK 2 INCHES LONG ON INTERCOSTAL AT STA 587 Z= -53 X= 70. CUT LOWER JAMB OF AFTER DOOR CUTOUT APPROX MIDWAY AND INSTALLED REPAIR JAMB IAW SRM 53-00-01 VOL 1 FIG 8 SHT 2. FABRICATED PARTS IAW DETAIL PARTS TRAVELER I01634Aug 3, 2006 · N367FE · Doug DC1010 · Fuselage Miscellaneous StructureSDR 06FDEA2822Membrane · crackedCOCKPIT AREA FOUND 1 EA CRACK 1 INCH LONG ON MEMBRANE OF FLOOR AT STA 303 X=13 RT SIDE. TRIMMED OUT DAMAGED PORTION OF MEMBRANE THEN INSTALLED REPAIR DOUBLER. FABRICATED PARTS IAW DETAIL PART SRM 53-00-01 FIG 4 SHT 2 VOL 1.Aug 3, 2006 · N367FE · Doug DC1010 · Fuselage Miscellaneous StructureSDR 06FDEA2821Web · crackedCOCKPIT AREA FOUND 1 EA CRACK 1 INCH LONG ON MEMBRANE OF FLOOR AT STA 303 X=13 LT SIDE. TRIMMED OUT DAMAGED PORTION OF MEMBRANE THEN INSTALLED FILLER REPAIRED DOUBLER. FABRICATED PARTS IAW DETAIL SRM 53-00-01 FIG 4 SHT 2 VOL 1.Aug 3, 2006 · N367FE · Doug DC1010 · Fuselage Miscellaneous StructureSDR 06FDEA2819Rib · crackedLEFT WING L/E AT STA XOS 458 ON RIB FOUND CRACK 1 INCH LONG. REPAIRED FORMER IAW SRM 57-20-00 FIG 1 SHT 3 VOL 1.Aug 3, 2006 · N367FE · Doug DC1010 · Wing, Rib/BulkheadSDR 06FDEA2818Rib · crackedRTH WING L/E CRACK LONG .75" ON INTERNAL RIB AT STA XOS 857. REPAIRED FORMER IAW SRM 57-20-00 FIG 1 SHT 1-6 VOL 1.Aug 3, 2006 · N367FE · Doug DC1010 · Wing, Rib/BulkheadSDR 06FDEA2817Rib · crackedFOUND LT WING L/E AT STA XOS 956 ON RIB FOUND CRACK .50" LONG. REPAIRED FORMER IAW SRM 57-20-00 FIG 1 SHT 1-6 VOL 1.Aug 3, 2006 · N367FE · Doug DC1010 · Wing, Rib/BulkheadSDR 06FDEA2816Rib · crackedLT WING L/E AT STA XOS 555 ON RIB FOUND CRACK .75" LONG. REPAIRED FORMER IAW SRM 57-20-00 FIG 1 SHT 1-6 VOL 1.Aug 3, 2006 · N367FE · Doug DC1010 · Wing, Rib/BulkheadSDR 06FDEA2815Rib · crackedFOUND LT WING L/E AT STA XOS 971 ON RIB FOUND CRACK .50" LONG. REPAIRED FORMER IAW SRM 57-20-00 FIG 1 SHT 1-6 VOL 1.Aug 3, 2006 · N367FE · Doug DC1010 · Wing, Rib/BulkheadSDR 06FDEA2814Rib · crackedFOUND LT WING L/E AT STA XOS 879 ON RIB FOUND CRACK .50" LONG. REPAIRED FORMER IAW SRM 57-20-00 FIG 1 SHT 1-6 VOL 1.Aug 3, 2006 · N367FE · Doug DC1010 · Wing, Rib/BulkheadSDR 06FDEA2813Rib · crackedFOUND LT WING L/E AT STA XOS 971 ON RIB FOUND CRACK .50" LONG. REPAIRED FORMER IAW SRM 57-20-00 FIG 1 SHT 1-6 VOL 1.Aug 3, 2006 · N367FE · Doug DC1010 · Wing, Rib/BulkheadSDR 06FDEA2812Rib · crackedFOUND LT WING L/E AT STA XOS 559 ON RIB FOUND CRACK .75" LONG. REPAIRED FORMER IAW SRM 57-20-00 FIG 1 SHT 1-6 VOL 1.Aug 3, 2006 · N367FE · Doug DC1010 · Wing, Rib/BulkheadSDR 06FDEA2811Rib · crackedFOUND LT WING L/E AT STA XOS 636 ON RIB FOUND CRACK .75". REPAIRED FORMER IAW SRM 57-20-00 FIG 1 SHT 1 AND 6 VOL 1.Aug 3, 2006 · N367FE · Doug DC1010 · Wing, Rib/BulkheadSDR 06FDEA2810Doubler · crackedLT WING L/E AT XOS 626 ON DOUBLER FOUND NR 3 EA CRACKS 0.50 INCH LONG. REPAIRED CRACK IAW SRM 57-10-00 FIG 71 VOL 1. FABRICATED PARTS IAW DETAIL PARTS TRAVELER I015512/N00512 AND IAW SRM 57-10-00 FIG 71 VOL 1.Aug 3, 2006 · N367FE · Doug DC1010 · Wing, Plate/SkinSDR 06FDEA2806Doubler · crackedLT WING L/E AT STA XOS 645 ON DOUBLER FOUND NR 3 CRACKS 0.50" LONG. REPAIRED CRACK IAW SRM 57-10-00 FIG 71 VOL 1.Aug 3, 2006 · N367FE · Doug DC1010 · Wing, Plate/SkinSDR 05FDEA03588Panel · crackedNOSE LANDING GEAR WHEEL WELL RT SIDE WEB UPPER FWD CORNER APPROX 2' FROM FWD PRESSURE BULKHEAD HAS 6" DIAGONAL CRACK. CUT OUT DAMAGED SECTION OF RT UPPER WEB IN NOSE WHEEL WELL LANDING GEAR. INSTALLED REPAIR DOUBLER REF: SRM 53-00-01. SNRM N00025 EMP. 3565Oct 28, 2005 · N367FE · Doug DC1010 · Fuselage Main, StructureSDR 05FDEA02695Warning Light · illuminatedON ROTATE STICK SHAKER ACTIVATED 140KTS A/C FULL BUFFET TO 3000 FT 180 KTS. DID NOT CHANGE T/O CONFIG. A/C STALL AT 15DGS AOB 210 KTS 15DGS FLAP. FLAPS 50, A/C BUFFETED AT 160KTS IN A FULL STALL LANDING, 20KTS FASTER THAN BUG. CKD FOR FULL EXT OF FLAPS /SLAug 27, 2005 · N367FE · Doug DC1010 · Stall Warning SystemSDR 05FDEA02166Attach Fitting · brokenRT I/B FLAP, I/B ACTUATOR AFT ATTACH FITTING BROKEN. REMOVED RT I/B FLAP I/B ACTUATOR SUPPORT FITTING PER MM 27-52-01-2 STEPS A1 THRU ALL. INSTALLED NEW R/H I/B FLAP I/B ACTUATOR SUPPORT FITTING PER MM 27-52-1-2. ENLARGED & REAMED FOUR HOLES IN FITTING PEAug 1, 2005 · N367FE · Doug DC1010 · Wing, Attach FittingsSDR 04FDEA03020Longeron · chafedFOUND LONGERON FLANGE CHAFED BEYOND LIMITS, AREA 2.5 INCHED LONG BY 0.250 INCHES WIDE, COMPLETELY THROUGH .063 INCH FLANGE, NR 2 RIGHT HAND COWL, JUST AFT OF CENTER HINGE POINT. FABRICATED REPAIR AND INSTALLED REPAIR IAW FEDEX EA 8-5410-81503.Nov 4, 2004 · N367FE · Doug DC1010 · Nacelle/Pylon, Main FrameSDR 04FDEA03019Longeron · wornREMOVED UPPER COWL CHAFE STRIPS AND FOUND LONGERON FLANGE CHAFED AREA 2.5 INCHES LONG BY 1.5 INCHES WIDE JUST AFT OF CENTER LINE, NR 1 ENGINE RIGHT HAND COWL. REPAIRED DAMAGED LONGERON IAW FEDEX EA 8-5410-81504.Nov 4, 2004 · N367FE · Doug DC1010 · Nacelle/Pylon, Main FrameSDR 04FDEA03017Duct · brokenNR3 ENGINE PNEUMATIC DRIVE MOTOR PNEUMATIC SUPPLY DUCT ADEL CLAMP MOUNT TAB BROKEN OFF. REMOVED, WELD REPAIRED AND REINSTALLED NR 3 ENGINE PNEUMATIC DRIVE MOTOR SUPPLY DUCT IAW DC10 MM 36-14-02-4 AND FEDEX EA 8-7830-81506. REFERENCE NON-ROUTINE N01094.Nov 4, 2004 · N367FE · Doug DC1010 · Engine Thrust ReverserSDR 04FDEA03010Panel · debondedRIGHT WING PANEL NR 661 EB IS DISBONDED AT FINGER DOUBLER AT MIDDLE FASTENER HOLE. REPAIRED BY FABRICATING AND BONDING NEW INNER AND OUTER SKIN, DOUBLER AND CORE IAW DAC DWG ARC0633 AND FEDEX EA 8-5710-81508. REMOVED AND REINSTALLED HINGED PANEL 661 EB SEAL Nov 2, 2004 · N367FE · Doug DC1010 · Wing, Plate/SkinSDR 04FDEA02941Hinge Fitting · corrodedLEFT WING INBOARD FLAP, OUTBOARD SUPPORT, PIVOT ATTACH POINT, OUTBOARD BORE PITTED. REMOVED DAMAGE, BORE FOUND OUT OF LIMITS. REPAIRED BORE I/A/W DOUGLAS CMM 57- 52-01 AND FED-EX EA 8-5750-81492 REFERENCE NON-ROUTINE NR N00417.Oct 15, 2004 · N367FE · Doug DC1010 · Trailing Edge FlapsSDR 04FDEA02940Hinge Fitting · corrodedRIGHT WING INBOARD FLAP, OUTBOARD SUPPORT, PIVOT ATTACH POINT, OUTBOARD BORE GOUGED. REMOVED DAMAGE I/A/W DOUGLAS CMM 57-52-01, BORE FOUND OUT OF LIMITS. REPAIRED BORE I/A/W DOUGLAS CMM 57-52-01 AND FED-EX EA 8-5750-81491 REFERENCE NON-ROUTINE NR N00412.Oct 15, 2004 · N367FE · Doug DC1010 · Trailing Edge FlapsSDR 04FDEA02939Roller · wornRIGHT WING INBOARD FLAP INBOARD MOST FORWARD TOP ROLLER IS WORN. REMOVED AND REPLACED RIGHT WING INBOARD FLAP INBOARD TRACK MOST FORWARD TOP ROLLER I/A/W DC10-10 MAINTENANCE MANUAL 20-50-02-2 AND EA 8-5750-81490. REFERENCE NON-ROUTINE NR N00776.Oct 15, 2004 · N367FE · Doug DC1010 · Trailing Edge FlapsSDR 04FDEA02938Hinge Fitting · corrodedLEFT WING INBOARD FLAP OUTBOARD SUPPORT PIVOT ATTACH POINT INBOARD BORE GOUGED. REMOVED DAMAGE IAW DOUGLAS CMM 57-52-01, BORE FOUND OUT OF LIMITS. REPAIRED BORE I/A/W DOUGLAS CMM 57-52-01 AND FED-EX EA 8-5750-81492 REFERENCE NON-ROUTINE NR N00416.Oct 15, 2004 · N367FE · Doug DC1010 · Trailing Edge FlapsSDR 03FDEA01761Sensor · malfunctionedCARGO BAY TEMP AFT WAS PEGGED AT 170 DEG. RETURNED FLIGHT TO LAX. REMOVED AND REPLACED CARGO COMPARTMENT TEMP SENSOR (TRANSMITTER) PER MM 21-41-01-2, OP'S CK'D GOOD.Oct 16, 2003 · N367FE · Doug DC1010 · Heating SystemSDR 03FDEA00693Warning Light · illuminatedIN CRUISE AT FL330 30 MIN AFTER TAKEOFF THE AIR COND DOORS CAUTION LIGHT ILLUMINATED. CABIN PRESS WAS ON SCHED IN STBY MODE. RED TABS RAN, DIVERT TO KMEM. DUPLICATED INTERMITTENT LIGHT AT PACK NR 3 COMPARTMENT DOOR. FOUND PLUG P1-1616 CORRODED. REPLACED PMay 7, 2003 · N367FE · Doug DC1010 · Door Warning SystemSDR 01FDEA001001Gearbox · malfunctionedNR 1 THRUST REVERSER FAILED TO STOW AFTER LANDING. REMOVED AND REPLACED ALL CABLES AND GEAR BOX ASSY PER MM 78-32-07.Nov 13, 2001 · N367FE · Doug DC1010 · Engine Thrust ReverserSDR 00FDEA00904Proximity Switch · faulty00-378 LEFT GEAR UNSAFE LIGHT ILLUM. R&R PROX SWITCH ELECTRONIC CONTROL UNIT IAW DC10-10 MM 32-61-01-2. PERF GEAR RETRACTION AFT PROX ELEC UNIT REPLACEMENT NO DEFECTS NOTED. SYS OPERATES NORM PER MM 7-11-00 & MM 32-30-00.Dec 24, 2000 · N367FE · Doug DC1010F · Landing Gear Position and WarningSDR 00FDEA00001Switch · inoperative00-1 - UPON GEAR EXT, 3 RED LIGHTS BOTH PNLS PERF RED TABLS 2-6-5. ALT GEAR EXT LEVER WAS RAISED AND 3 GREEN LIGHTS ILLUM BOTH PNLS. REMOVED AND REPLACED SWITCH ACTUATOR IAW MM 32-61-04-2. REMOVED 3 JACKS AND PADS FROM AC.Jan 4, 2000 · N367FE · Doug DC1010F · Landing Gear SelectorSDR 99FDEA00511Lever · stickingLOWERED GEAR DIDN'T GET LIGHT ON EITHER PNL. WHEN GEAR ALT HANDLE IS STOW AFT LAND RED LIGHTS ILLUM. LUBED LANDING GEAR CONTROL LEVER MECHANISM. OPS CK GOOD. GROUND LIGHT ON BOTH POS.Dec 23, 1999 · N367FE · Doug DC1010F · Landing Gear SelectorSDR 99FDEA00488Terminal · failedAC WOULD NOT PRESSURIZE. ALL DOORS CLOSED. REPAIRED TERMINAL END IAW SMP. IND LIGHT WORKS NORM, SYS CK NORM.Nov 24, 1999 · N367FE · Doug DC1010F · Cabin Pressure Control System
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