N318FE

Service difficulty reports · 311

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 = 'N318FE' 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 08FDEA03013None · noneFWD CARGO COMPARTMENT STRUT SUPPORT BEAM NOT IN CONFIGURATION.Jul 22, 2008 · N318FE · Doug DC1030F · Standard Practices/StructuresSDR 08FDEA03012None · noneFWD CARGO COMPARTMENT EXISTING REPAIR ON STANCHION.Jul 22, 2008 · N318FE · Doug DC1030F · Standard Practices/StructuresSDR 08FDEA03011None · noneFWD CARGO COMPARTMENT EXISTING REPAIR ON STANCHION.Jul 22, 2008 · N318FE · Doug DC1030F · Standard Practices/StructuresSDR 08FDEA03010None · noneFWD CARGO COMPARTMENT EXISTING REPAIR ON STANCHION.Jul 22, 2008 · N318FE · Doug DC1030F · Standard Practices/StructuresSDR 08FDEA03009None · noneFWD CARGO COMPARTMENT EXISTING REPAIR ON STANCHION.Jul 22, 2008 · N318FE · Doug DC1030F · Standard Practices/StructuresSDR 08FDEA02835Channel · corrodedFWD CARGO COMPT CHANNEL WITH SEVERE EXFOLIATION CORROSION. WORK COVERED BY NRC N00418.Jul 12, 2008 · N318FE · Doug DC1030F · Fuselage Miscellaneous StructureSDR FDEA200807092773Skin · dentedEXT FUSELAGE LWR SURFACE FOUND DEEP DENT 2.50 INCH BY 1.50 INCH DEEP .082 INCH ON SKIN. REPAIRED SKIN IAW SRM 53-20-00 FIG 13 SHT 7 VOL I.Jul 9, 2008 · N318FE · Doug DC1030F · Fuselage Main, Plate/SkinSDR FDEA200807092772Skin · dentedEXT FUSELAGE LWR SURFACE FOUND DEEP DENT 2 INCH BY 1 INCH DEEP .074 INCH ON SKIN. REPAIRED AREA IAW SRM 53-20-00 FIG 13 VOL I.Jul 9, 2008 · N318FE · Doug DC1030F · Fuselage Main, Plate/SkinSDR FDEA200807092770Skin · crackedEXT FUSELAGE LWR SURFACE FOUND CRACK ON SKIN (UPPER CORNER). REPAIRED SKIN IAW SRM 53-20-00 VOL I FIG 2.Jul 9, 2008 · N318FE · Doug DC1030F · Fuselage Main, Plate/SkinSDR 08FDEA02773Skin · dentedEXT FUSELAGE LWR SURFACE FOUND DEEP DENT 2.50 INCH BY 1.50 INCH DEEP .082 INCH ON SKIN.Jul 9, 2008 · N318FE · Doug DC1030F · Fuselage Main, Plate/SkinSDR 08FDEA02772Skin · dentedEXT FUSELAGE LWR SURFACE FOUND DEEP DENT 2 INCH BY 1 INCH DEEP .074" ON SKIN.Jul 9, 2008 · N318FE · Doug DC1030F · Fuselage Main, Plate/SkinSDR 08FDEA02771Skin · dentedDURING INSPECTION EXT FUSELAGE LWR SURFACE FOUND DEEP DENT AND NICK 3 INCH BY .75 INCH DEEP .047 INCH ON SKIN.Jul 9, 2008 · N318FE · Doug DC1030F · Fuselage Main, Plate/SkinSDR 08FDEA02770Skin · crackedEXT FUSELAGE LWR SURFACE FOUND CRACK ON SKIN (UPPER CORNER).Jul 9, 2008 · N318FE · Doug DC1030F · Fuselage Main, Plate/SkinSDR 07FDEA02966Fitting · crackedNR 4 MAIN CARGO DOOR JAM SUPPORT FITTING P/N AFA 7132-1, REQUIRES REPLACEMENT DUE TO CRACKS REMAINING AFTER REAMING TO .520. REMOVED SUPPORT BRACE, STRAP, CLIP, INTERCOSTAL AND BACKUP FITTING IAW SRM 51-31-01. INSTALLED NEW BACKUP FITTING AND REINSTALLED SUPAug 18, 2007 · N318FE · Doug DC1030 · Fuselage Main, Attach FittingsSDR 07FDEA02970Fitting · crackedNR 7 MAIN CARGO DOOR LOWER JAMB SUPPORT FITTING P/N AFA7132-1 REQUIRES REPLACEMENT DUE TO CRACKS REMAINING AFTER REAMING TO .520. REMOVED BACKUP FITTING, SUPPORT BRACE, STRAP, VERTICAL STRAP, SEAT TRACK SPLICE, INTERCOSTAL IAW SRM 51-31-01. CUT WEB IAW SAug 18, 2007 · N318FE · Doug DC1030 · Fuselage Main, Attach FittingsSDR 07FDEA02969Fitting · crackedNR 6 MAIN CARGO DOOR JAMB SUPPORT FITTING P/N AFA 7132-1 REQUIRES REPLACEMENT DUE TO CRACKS REMAIN AFTER REAMING TO .520. REMOVED BACKUP FITTING, ANGLE, INTERCOSTAL AND WEB IAW SRM 51-31-01. INSTALLED NEW BACKUP FITTING AND REINSTALLED ANGLE, INTERCOSTAL, ANAug 18, 2007 · N318FE · Doug DC1030 · Fuselage Main, Attach FittingsSDR 07FDEA02968Fitting · crackedNR 5 MAIN CARGO DOOR LOWER JAMB SUPPORT FITTING P/N AFA 7132-1 REQUIRES REPLACEMENT DUE TO CRACKS REMAINING AFTER REAMING TO .520. REMOVED 2 EACH SUPPORT BRACES, STRAP, WEB, INTERCOSTAL, AND BACKUP FITTING IAW SRM 51-31-01. INSTALLED NEW BACKUP FITTING ANDAug 18, 2007 · N318FE · Doug DC1030 · Fuselage Main, Attach FittingsSDR 07FDEA02967Fitting · crackedNR 3 MAIN CARGO DOOR JAMB SUPPORT FITTING P/N AFA7132-1 REQUIRES REPLACEMENT DUE TO CRACKS REMAINING AFTER REAMING TO .520. REMOVED SUPPORT BRACE, STRAP, VERTICAL STRAP, 2 EACH INTERCOSTALS, CLIP, WEB AND BACKUP FITTING IAW SRM 51-31-01. INSTALLED NEW BACKAug 18, 2007 · N318FE · Doug DC1030 · Fuselage Main, Attach FittingsSDR 06FDEA03915Support Fitting · crackedLT O/B FLAP I/B HINGE FWD SUPPORT FITTING CRACKED AT FWD NOSE SECTION REMOVED FASTENERS FOR NDT ACCESS. PERFORMED HFEC INSPECTION ON FWD HINGE SUPPORT FITTING I/B AND O/B HALVES FROM FWD END TO PERIPHERY AND IMMEDIATE AREAS OF THE FIRST THREE FASTENERS (3EA).Nov 7, 2006 · N318FE · Doug DC1030 · Trailing Edge FlapsSDR 06FDEA03787Transmitter · malfunctionedLEVELED AT FL290 ATC SLOWED US TO 250 KNOTS. S/O REPORTED NR 3 ENGINE FUEL PRESSURE GAUGE STARTED TO FLUCTUATE. NOTICED NR 3 N1 RPM DROPPING AND ASSOCIATED REDUCTION IN EGT AND N2. PERFORMED IN FLIGHT ENG SHUT DOWN. RETURNED AND LANDED MEM WITHOUT INCIDENOct 25, 2006 · N318FE · Doug DC1030 · Engine Oil PressureSDR 06FDEA2907Bulkhead · crackedNR 3 PYLON AFT BULKHEAD IB HORIZONTAL FLANGE AT RADIUS IS CRACKED FROM FWD EDGE TO AFT RADIUS, APPROX 2 INCHES IN LENGTH H.F.E.C. INDICATION AND VARIFED WITH BOROSCOPE. (PICTURE TAKEN) ENGINEERING NOTIFIED. REPLACED BULKHEAD PER WO 00033604 AND EA 8-5410-90Aug 8, 2006 · N318FE · Doug DC1030 · Nacelle/Pylon, Bulkhead/FirewallSDR 06FDEA0495Drive Assy · malfunctionedSEPERATING GREASE ON RETAINER RING ON LT WING OUTBOARD SLAT DRIVE MECHANISM CENTER-FWD BEARING . REMOVED AND REPLACED LT O/B SLAT DRIVE MECHANISM IAW DC10-30 MM 27-83-02-2 RIG CHECKED AND LEAK CHECKS GOOD IAW DC10-30 MM 27-83-02-2 .Feb 2, 2006 · N318FE · Doug DC1030 · Leading Edge Slat Control SystemSDR 06FDEA0468Frame · damagedFWD CARGO PIT AFT FRAME STA 959 IS DAMAGED FROM PREVIOUS REPAIR. REPAIRED FRAME IAW EA 8-5310-91333, FUSELAGE - FWD LOWER CARGO DOOR JAMB STA 959 CHORD AND SKIN - REPAIR AND DC10 SRM 51-39-01 PG 5 STEP 10 VOL II AND DC10 SRM 53-50-00 FIG 22 SHEET 9 VOL I.Feb 1, 2006 · N318FE · Doug DC1030 · Fuselage Main, FrameSDR 06FDEA0376Unknown · unknownREPAIR LOCATED AT STA. 859 , LONG. 41L-42R REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA . VISUALLY INSPECTED REPAIR AT STA. 859 , LONG 41R-42R , FOUND TO BE WITHIN LIMITS IAW SRM 53-20-00 FIG. 13 Jan 25, 2006 · N318FE · Doug DC1030 · Fuselage Miscellaneous StructureSDR 06FDEA0359Sealant · missingSEALANT MISSING AND RUSTY UPPER FLANGE AT AFT END OF UPPER CARGO DOOR HINGE. REMOVED AND REPLACED HINGE SECTION IAW DC10-30 SRM 51-33-01 VOL II, AND FED EX AMM 20-50-02-2. REMOVED AND REINSTALLED DOOR LINER IAW DC10-30 AMM 20-50-02-2 FIG 203. TORQUE WRENCH Jan 24, 2006 · N318FE · Doug DC1030 · Fuselage, Door HingeSDR 06FDEA0340Tripler · corrodedREPAIR LOCATED AT STA 999-1026 LONG 51L-50R, REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION USING FAA APPROVED DATA. FOUND REPAIR TO BE MAJOR, REMOVED TRIPLER TO GAIN ACCESS AND FOUND CORROSION IAW DC10-30 SRM 51-33-01 VOL I AND SRM 51-35-01 VOL I. REMOVEJan 23, 2006 · N318FE · Doug DC1030 · Fuselage Main, Plate/SkinSDR 06FDEA0339Repair · unknownREPAIR LOCATED AT STA LT INBD FLAP LOWER SURFACE XIFH 189-195 REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION USING FAA APPROVED DATA. INSPECTED REPAIR FOUND TO BE OUT OF LIMITS WITH REGARDS TO FAA APPROVED DATA. REMOVED AND REPLACED REPAIR DOUBLER IAW DJan 23, 2006 · N318FE · Doug DC1030 · Aircraft StructuresSDR 06FDEA0338Skin · corrodedLOWER SKIN AT STA 1069 AT ADF ANTENNA CORRODED. REMOVED CORROSION IAW DC10-30 SRM 51-21-01 VOL II. ORIGINAL THICKNESS .068, AFTER BLENDING .047 , .021 MATERIAL LOST OUT OF LIMITS IAW DC10-30 SRM 53-00-01 VOL II. FABED REPAIR DOUBLER IAW DC10-30 SRM 53-20-00Jan 23, 2006 · N318FE · Doug DC1030 · Fuselage Main, Plate/SkinSDR 06FDEA0335Repair · misinstalledREPAIR LOCATED AT LEFT OUTBOARD AILERON OUTBOARD END T/E WEDGE REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. REMOVED OLD REPAIR NOT WITHIN FAA APPROVED DATA. FABRICATED NEW WEDGE SECTION AND ZEE IAWJan 23, 2006 · N318FE · Doug DC1030 · Wing StructureSDR 06FDEA0330Hinge · corrodedSEALANT MISSING AND RUSTY AT UPPER FLANGE FORWARD AND AFT END OF CENTER CARGO DOOR. REMOVED AND REPLACED HINGE SECTION IAW DC10-30 SRM 51-33-01 VOL II AND DC10-30 MM 20-50-02-2 FIG 203. TORQUE WRENCH T8481I, N/R N00712, WORK ORDER 00031289.Jan 23, 2006 · N318FE · Doug DC1030 · Fuselage, Door HingeSDR 06FDEA0326Rail · crackedLOWER CARGO DOOR CUTOUT RAIL STA 1682 L-43R HAS CRACK ON END IN RADIUS. REPAIRED RAIL WITH REPAIR ANGLE IAW DC10-30 SRM 53-00-01 FIG 9 VOL I SHEET 7. ALODINED AND PRIMED IAW DC10-30 SRM 51-21-01 PAR 31 VOL I.Jan 23, 2006 · N318FE · Doug DC1030 · Fuselage Main, StructureSDR 06FDEA0274Seat Track · gougedMAIN CABIN SEAT TRACK GOUGED BS 744 LBL 47.0. REMOVED FLOORBOARDS TO FOM IAW DC10-30 SRM 51-31-01 VOL II. FOUND SEAT TRACK TO BE OUT OF LIMITS AND FABBED IAW DC10 SRM 53-42-01 VOL II. ALODINED AND PRIMED IAW DC10 SRM 51-21-01 VOL II. INSTALLED SEAT TRACK, Jan 19, 2006 · N318FE · Doug DC1030 · Fuselage, Seat/Cargo Attach FittingsSDR 06FDEA0266Wedge · damagedLEFT OUTBOARD FLAP WEDGE STA XOFH 681 TO STA 747 HAS SEVERAL SKIN REPAIRS WITH LEAKING FASTENERS, AND LARGE AREA OF LEAKING FASTENERS ON TOP SKIN. REMOVED DAMAGED SKIN IAW DC 10 SRM 51-31-01 VOL II. FABRICATED NEW SKIN ASSEMBLY IAW DAC DRAWING ARC1953. INSTJan 18, 2006 · N318FE · Doug DC1030 · Trailing Edge FlapsSDR 06FDEA0254Frame · corrodedCORROSION AT STA BS 1997 FRAME, FORWARD SIDE/LOWER LEG/BOTTOM SIDE AT LONGERON L43-R AND EXTENDING 2 FASTENERS EITHER SIDE OF LONGERON. REMOVED FRAME AND SPLICES IAW DC 10 SRM 51-35-01 VOL II. REMOVED CORROSION IAW DC10 SRM 51-21-01 VOL II. FOUND OUT OF LIMJan 18, 2006 · N318FE · Doug DC1030 · Fuselage Main, FrameSDR 04FDEA02866Engine · overtempNR 3 ENGINE OVERTEMP ON TAKEOFF AT 700 FT AGL. TEMP ROSE TO 984 DEG FOR 30 SECONDS. SHUT DOWN ENGINE. TRIED RETARDING THROTTLE TO COOL ENGINE BUT WHEN THROTTLE WAS INCREASED N1 AND N2 CONTINUED TO DETERIORATE. NR 3 ENG IS APPROVED FOR REMOVAL. DURING INSPOct 3, 2004 · N318FE · Doug DC1030 · Engine (Turbine/Turboprop)SDR 04FDEA01273Generator · contaminatedAT ROTATION (MAIN WHEEL LIFTOFF), CAPTAIN LOST ALL INSTRUMENTS. THE FOLLOWING LIGHTS ILLUMINATED ON S/O PANEL: GEN 1 OFF, L EMER AC BUS OFF, AC BUS 1 OFF, AC BUS TIE 1 ISOL, L EMER DC BUS OFF, DC BUS 1 OFF. SEVERAL WARNING HORNS GOING OFF THAT COULD NOT BE May 15, 2004 · N318FE · Doug DC1030 · AC Generator-AlternatorSDR 03FDEA00108Skin · corrodedLEFT WING UPPER SKINS HAVE PATCHES OF LOCAL INTERGRANULAR CORROSION FROM THE WING LEADING EDGE, AFT TO THE AFT SPAR AREAS. *S/D* REMOVED CORROSION IN SUBJECT AREA OF ARB3121 AND ARB3108, LT WING PANEL, AT STATION XIS 168.66 TO XORS 130.40, STRINGER 7L AND 19Feb 4, 2003 · N318FE · Doug DC1030 · Wing, Plate/SkinSDR 03FDEA00107Skin · corrodedRIGHT WING UPPER SKINS HAVE PATCHES OF LOCAL INTERGRANULAR CORROSION FROM THE WING LEADING EDGE, AFT TO THE AFT SPAR AREAS. *S/D* REMOVED CORROSION IN SUBJECT AREA OF ARB3121 AND ARB3108 RT WING SKIN PANEL AT STA XIS 168.66 TO XORS 130.40, STRINGER 1R AND 22Feb 4, 2003 · N318FE · Doug DC1030 · Wing, Plate/SkinSDR 02FDEA00813Compressor · damagedON TAKEOFF AND JUST 5 AFTER ROTATION HEARD LOUD NOISE AND ENGINE NR 3 ROLLED BACK TO APPROXIMATELY 35 PERCENT N1. ENGINE OVER TEMP LIGHT CAME ON MOMENTARILY. ENGINE CONTINUED TO WINDMILL. DUE TO NOISE AND VIBRATION PULLED ENGINE FIRE HANDLE AND BLEW NR 1 BONov 8, 2002 · N318FE · Doug DC1030 · Turbine Engine Compressor SectionSDR 02FDEA00788O-Ring · damagedLOST ALL FLUID ON HYDRAULIC NR 2 SYS, RUDDER STANDBY POWER OFF LIGHT ILLUMINATED. DUMPED FUEL AND LANDED AT AIRPORT. PERFORMED HYDRAULIC SYSTEM NR 2 LEAKAGE FAULT ISOLATION AND TRACED PROBLEM AT NON-REV SHUTOFF VALVE. REMOVED AND REPLACED DEFECTIVE O-RING, Oct 31, 2002 · N318FE · Doug DC1030 · Hydraulic System, MainSDR 02FDEA00781O-Ring · damagedLOST HYDRAULIC NR 2 FLUID, RUDDER STANDBY POWER OFF, LIGHT ILLUMINATED, LANDED WITHOUT INCIDENT. PERFORMED HYDRAULIC SYSTEM NR 2 FAULT ISOLATION AND TRACED PROBLEM TO NONREVERSIBLE S/O VALVE. REPLACED DEFECTIVE O-RING, SERVICED HYDRAULICS TO PROPER LEVEL. Oct 28, 2002 · N318FE · Doug DC1030 · Hydraulic System, MainSDR 01FDEA00277Warning Light · illuminatedAFT T/O RED NOSE GEAR IND LIGHT STAY ILLUM.Apr 16, 2001 · N318FE · Doug DC1030 · Landing Gear Position and WarningSDR 00FDEA00850A/C Pack · smoke00-338 NR 2 AC PACK INTRODUCED SMOKE INTO COCKPIT WHEN UTILIZED IN FLT. AS PER PREVIOUS WRITE UP COMPLIED WITH RED TAB PROC FOR AIR COND SMOKE. RELEASE FOR SERVICE PER MEL/CDL:12-1. CK AND CLEANED COALESCER RAN NR 2 PACK FOR 1 HOUR. NO SMOKE OR ODOR NOTICEDec 5, 2000 · N318FE · Doug DC1030 · Cabin Cooling SystemSDR 00FDEA00527Longeron · corrodedCORROSION FOUND ON LONGERON 32R, FS 1481. *S/D* REMOVED AND REPLACED PER SRM 53-10-00 FIG A, VOL 1.Aug 3, 2000 · N318FE · Doug DC1030 · Fuselage Main, Longeron/StringerSDR 00FDEA00526Longeron · corrodedCORROSION FOUND ON LONGERON 30R BETWEEN FS 1421 & 1441. *S/D* REMOVED AND REPLACED PER SRM 53-10-00 FIG 2, VOL 1.Aug 3, 2000 · N318FE · Doug DC1030 · Fuselage Main, Longeron/StringerSDR 00FDEA00525Longeron · corrodedCORROSION FOUND ON LONGERON 31R BETWEEN FS 1421 & FS 1441. *S/D* REMOVED AND REPLACED PER SRM 53-10-00 FIG 2 VOL 1.Aug 3, 2000 · N318FE · Doug DC1030 · Fuselage Main, Longeron/StringerSDR 00FDEA00530Skin · crackedLT WING TRAILING EDGE O/B FLAP UPPER SKIN FOUND WITH CRACK LOCATED AT APPROX 16 INCHES FROM O/B EDGE. *S/D* REMOVED AND REPLACED PER SRM 57-10-00 VOL.Aug 1, 2000 · N318FE · Doug DC1030 · Trailing Edge FlapsSDR 00FDEA00529Skin · crackedRT WING LEAD EDGE LWR SKIN CRACK AT CUTOUT OF SLAT TRACK NR 14. *S/D* REMOVED AND REPLACED PER SRM 57-10-00 FIG 68 VOL 1.Aug 1, 2000 · N318FE · Doug DC1030 · Wing, Plate/SkinSDR 00FDEA00528Skin · crackedNR 1 ENGINE LT CORE COWL FWD SKIN FOUND CRACKED. *S/D* REMOVED AND REPLACED PER EA 1-7110-52071.Aug 1, 2000 · N318FE · Doug DC1030 · Engine Cowling SystemSDR 00FDEA00083Relay · stuck00-47 - AUTO THROTTLES RETARDED TO HOLD SPD. ALL FOUR RED WARNING GEAR LIGHTS ILLUMINATED WHEN CLIMB BEGAN, WITH THROTTLE RED WARNING LIGHT FOR GEAR WOULD NOT GO OUT. REMOVED AND REPLACED RELAY AND OPS CK LANDING GEAR HANDLE TEST, OPS CK OK.Feb 15, 2000 · N318FE · Doug DC1030 · Landing Gear Position and Warning
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