N386FE, cancelled Apr 13, 2024

Service difficulty reports · 34

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 = 'N386FE' AND deregistration_id = 'N386FE-2024-04-13'
  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 FDEA201302090312Girt Bar · obstructedOUTSIDE INDICATOR OF SAFE OR EMERGENCY (RED LEVER) LT SIDE OF JET STICKS TO "EMERGENCY". EMERGENCY OVERRIDE LEVER DOES NOT CORRESPOND TO ACTION ON DISARM LEVER INSIDE CABIN DOOR. UPON REMOVING ACCESS PANEL, FOUND DIRT & DEBRIS ALONG SIDE CABLE & SPRING ASSYFeb 9, 2013 · N386FE · Doug MD1010F · Emergency EquipmentSDR FDEA201111235006Element · failedAFTER TAKEOFF, WITH NR 2 PACK OFF, CLIMBING PASSED 14000' MSL. RECEIVED NR 2 MANIFOLD FAILURE LEVEL ALERT, RTB LANDED WITHOUT INCIDENT. REMOVED AND REPLACED NR 2 ENGINE MANIFOLD SENSING ELEMENT IAW MM 36-23-02-4. RAN NR 2 ENGINE REF JRH AND PERFORMED PNENov 23, 2011 · N386FE · Doug MD1010F · Pneumatic Indicating SystemSDR FDEA201103311255Warning Light · illuminatedCLIMBING THRU 13,000' GOT LVL 3" BLD AIR 1 TEMP HI", COMPLIED WITH QRH. PERFORMED RTS ON ALL 3 AIU'S, ALL TESTS PASSED. PERFORMED RTS ON PNEUMATIC SYS CONTROLLER NR 1. INSPECTED NR 1 ENGINE BLEED CONTROL VALVE SENSE LINES AND CONNECTORS, NO DEFECTS NOTED. Mar 31, 2011 · N386FE · Doug MD1010F · Engine Bleed Air SystemSDR FDEA201103181170Skin · corrodedSKIN BULGING AT APPROX STA 859, STRINGER 43R FWD OF FWD CARGO DOOR, 6 INCHES IN LENGTH. INSPECTED, FOUND EXTERIOR SKIN OK. CORROSION FOUND UNDER SKIN AT RAIL AREA. REMOVED SKIN & DOUBLER TO GAIN ACCESS TO RAIL, REF SRM 51-21-00, VOL 2. BLENDED/REMOVED CORROMar 18, 2011 · N386FE · Doug MD1010F · Fuselage Main, Plate/SkinSDR FDEA201103020825Floorbeam · corrodedCENTER CARGO COMPARTMENT FLOORBEAM CORRODED/EXFOLIATED AT BS 1781, RBL 36.Mar 2, 2011 · N386FE · Doug MD1010F · Fuselage Main, Floor BeamSDR FDEA201103021171Fitting · crackedCAC COMPARTMENT FITTING AT THE PRESSURE DOME ADJACENT TO THE "SUGAR SCOOP" HAS A 2 IN CRACK IN THE LOWER LARGE RADIUS. (PN AYB7000-1) REMOVED CRACKED FITTING AND INSTALLED NEW FITTING PART NR AYB7000 IAW DWG NYB60472, SRM 51-31-01, SRM53-40-00. ACCOMPLISHEDMar 2, 2011 · N386FE · Doug MD1010F · Fuselage Main, Attach FittingsSDR FDEA201102040467Power Supply · failedEMERGENCY LIGHT TEST FAIL MEL 04FEB11. RELEASED FOR SERVICE IAW MEL: 33-50-02, CATEGORY: C. R & R EMERGENCY EXIT LIGHTS POWER-SUPPLY IAW AMM 33-51-01-4. OPS CHECKS GOOD IAW AMM. OK FOR SERVICE.Feb 4, 2011 · N386FE · Doug MD1010F · Emergency LightingSDR FDEA200904021164None · noneAT BEGINNING OF TAKEOFF ROLL, LEVEL 1 'UNABLE RNP'. DURING TAX IN, RNP INDICATED 4.1 NM. UPON RETURN TO BLOCKS, TROUBLESHOT THE CFDS/ MCDU: NO FAULTS PERFORMED RTS ON ADIRU 1,2, AND 3; MMR 1,2, AND 3, NO FAULTS FOUND. ALL TESTS PASS POS REF SHOWS 6 SAT'S, GApr 2, 2009 · N386FE · Doug MD1010F · Standard Practices/StructuresSDR FDEA200902190593Spar Cap · crackedFUEL LEAK LT WING LOWER REAR SPAR CAP AT WS XORS 346, INDICATION OF CRACK AT THE POINT OF LEAK. REAR SPAR REPAIRED AS PER E.A. 8-5710-126158. SEQ.#924.Feb 19, 2009 · N386FE · Doug MD1010F · Wing SparSDR FDEA200902020425Window Frame · crackedCAPTAIN SLIDING VIEW WINDOW FRAME AIRPLANE SIDE CRACKED OUTSIDE (MARKED).Feb 2, 2009 · N386FE · Doug MD1010F · Fuselage Main, StructureSDR 07FDEA04975Control Valve · malfunctionedON INITIAL GEAR EXTENSION GOT ALL RED AND NO GREEN ON LIGHTS AND CONFIG PAGE. SAME ON SECOND ATTEMPT. NO WIND NOISE ON 1ST AND SECOND TIME, THIRD TIME ALL GREEN INDICATIONS. CHECKED MECHANICAL CONTROL TO LANDING GEAR CONTROL VALVE NO FAULTS FOUND. CHECKED Dec 1, 2007 · N386FE · Doug MD1010F · Landing Gear Retraction/Extension SystemSDR 07FDEA04381Engine · damagedCLIMBING THROUGH FL190 AIRCRAFT SHUDDERED TWICE WITH SLIGHT YAW TO LEFT. LOOKED DOWN AND "ENG 1 EXCEEDENCE" ALERT AND RED BOXED ENG 1 EGT "951". PULLED ENG 1 TO IDLE AND RAN ENG FIRE SEVERE DAMAGE CHECKLIST. SHUTDOWN NR 1, PULLED NR 1 FIRE HANDLE AND RTBED Sep 29, 2007 · N386FE · Doug MD1010F · Engine (Turbine/Turboprop)SDR 06FDEA1312Engine · failedON CLIMBOUT TO CRUISE ALTITUDE PASSING 28,000 FT HEARD A THUD & EXPERIENCED AIRCRAFT YAW TO THE RIGHT. ENGINE INSTRUMENTS INDICATED NR 3 ENGINE FAILURE. SHUT DOWN ENGINE IN ACCORDANCE WITH QRH. FIRED NR 3 ENGINE FIRE EXTINGUISHER PER QRH. RETURNED TO MEM, Apr 5, 2006 · N386FE · Doug MD1010F · Engine (Turbine/Turboprop)SDR 06FDEA1310Engine · failedON CLIMB-OUT TO CRUISE, ALTITUDE PASSING 28000' HEARD A "THUD" AND EXPERIENCED AIRCRAFT YAW TO THE RIGHT. ENGINE INSTRUMENTS INDICATED NR 3 ENGINE FAILURE. SHUT DOWN ENGINE IN ACCORDANCE WITH QRH. FIRE EXTINGUSHING AGENT TO NR 3 ENGINE PER QRH, RETURNED TO Apr 4, 2006 · N386FE · Doug DC1010 · Turbine Engine Reduction GearSDR 04FDEA02071Floorbeam · damagedFLOORBEAM AT FUSELAGE STATION 1921, LBL 50, FOUND DAMAGED ON EDGE OF CUTOUT, AT CABLE LOCATION. COMPLIED WITH FEDEX EA 8-5310-77598, FUSELAGE STATION 1921, X=-50, FLOORBEAM LIGHTENING HOLE REPAIR.Jul 14, 2004 · N386FE · Doug MD1010F · Fuselage, Seat/Cargo Attach FittingsSDR 04FDEA02026Control Cable · crossedAFT PIT BEHIND STATION 1967, 36 INCHES, LEFT BUTT LINE CABLES CROSSED BELOW MAIN CABIN FLOOR. OPENED CEILING PANELS AND REMOVED LEFT HAND VERTICAL ACCESS PANELS. REMOVED AND REPLACED PULLEYS AND 2 EACH CABLES, RIGGED AND OPS CHECKED GOOD, ROUTE CHECKED AND IJul 7, 2004 · N386FE · Doug MD1010F · Flight Control SystemSDR 04FDEA02025Panel · dentedRIGHT HAND WING TRAILING EDGE INBOARD LOWER PANEL NUMBER 641 BB HAS NUMEROUS DENTS IN ITS UPPER SURFACE. REPAIRED BY FABRICATING AND BONDING NEW METAL OUTER SKIN, CORE, INNER SKIN AND INNER DOUBLER IAW TPS 1001 REV E AND DWG ARC 2067 AND EA 8-5710-77592. REFJul 7, 2004 · N386FE · Doug MD1010F · Wing, Plate/SkinSDR 04FDEA02022Skin · dentedSEVERAL DENTS IN REPAIR DOUBLER, JUST AFT OF LOWER FWD CARGO DOOR. REMOVED DOUBLER AND TRIPLER. FABRICATED AND INSTALLED DOUBLER AND TRIPLER IAW DC10 SRM 53-20-00 VOL 1 AND 51-21-01 VOL 2.Jul 7, 2004 · N386FE · Doug MD1010F · Fuselage Main, Plate/SkinSDR 04FDEA02021Skin · dentedSEVERAL DENTS IN REPAIR DOUBLER, JUST AFT OF LOWER FWD CARGO DOOR. REMOVED DOUBLER AND TRIPLER. FABRICATED AND INSTALLED DOUBLER AND TRIPLER IAW DC10 SRM 53-20-00 VOL 1 AND 51-21-01 VOL 2.Jul 7, 2004 · N386FE · Doug MD1010F · Fuselage Main, Plate/SkinSDR 04FDEA02019Door Frame · corrodedFORWARD PIT, FORWARD DOOR FRAME STATION 886 HAS CORROSION. DOOR FRAME FOUND TO BE OUT OF LIMITS. CUT AND REMOVED CORRODED FRAME SECTION, CUT WEB TO FOM. FABRICATED -15, -13 AND WEB REPAIR DOUBLER AND INSTALLED REPAIR COMPONENTS IAW DC10 SRM 51-31-01 VOL II,Jul 7, 2004 · N386FE · Doug MD1010F · Fuselage Main, StructureSDR 04FDEA02018Static Port · damagedRIGHT PRIMARY STATIC PORT FAILS RVSM CONVEXITY AND CONCAVITY AND WAVINESS INSPECTION IAW WORK CARD 34C1501 STEP 9 AND 10. REMOVED AND REPLACED RIGHT HAND PRIMARY STATIC PORT IAW FEDEX MD10-10 MM 34-11-01-2, PERFORMED WAVINESS INSPECTION IAW FEDEX MD10-1Jul 7, 2004 · N386FE · Doug MD1010F · Pitot/Static SystemSDR 04FDEA02016Skin · corrodedRIGHT HAND WING INBOARD AILERON LOWER SKIN BULGED/CORRODED AND I EACH FASTENER POPPED. REMOVED AND REPLACED INBOARD AILERON LOWER SKIN PER FEDEX EA 8-5750-77595. REMOVE AND REPLACE LEADING EDGE SKIN PER FEDEX DC10-10 SRM 51-35-01 VOL 2.Jul 7, 2004 · N386FE · Doug MD1010F · AileronsSDR 04FDEA02015Beam · crackedRIGHT WING INBOARD AILERON LOWER BEAM CRACKED AT END. REMOVE TEE-CAP IAW DC10 SRM 51-35-01 VOL I, FABRICATED -4 TEE CAP IAW DCA DWG ARC 3012 AND DC10 SRM 51-10-01 FIG 13 VOL 3. TRIMMED, LOCATED, DRILLED AND DEBURRED -4 TEE CAP IAW DC10 SRM 57-31-01 VOL 2 ANDJul 7, 2004 · N386FE · Doug MD1010F · Wing Main, Frame StructureSDR 04FDEA00468Warning System · activatedAT 6000 FT ON DOWN WIND LEG WITH SLATS EXTENED AND 180 KTS,THE LEVEL 2 FUEL USED ALERT CAME ON. FUEL USED AND FUEL REMAINING EQUALLED DEPARTURE FUEL. APPROXIMATELY 5 MIN LATER, GOT A TANK NR 3 FUEL QTY LO ALERT. DECLARED AN EMERGENCY AND LANDED UNEVENTFULLYFeb 20, 2004 · N386FE · Doug DC1010 · Fuel Indicating SystemSDR 03FDEA01948Selector Valve · failedAT 180 KTS ON FINAL DROPPED LANDING GEAR AND GOT UNSAFE ON BOTH PRI-SEC. CYCLED GEAR WITH SAME RESULT. INITIATED GO-AROUND. AT 210 KTS ON VECTORS CYCLED GEAR AND GOT 3 GREEN. REMOVED AND REPLACED LANDING GEAR SELECTOR VALVE PER AMM 32-31-03-2 OPS CHECK Nov 18, 2003 · N386FE · Doug DC1010 · Landing Gear SelectorSDR 03FDEA00780Engine · malfunctionedCRUISE ALT (FL370) ANC -- SEA 2+19 ENROUTE TIME "ENG NR 3 OIL PRESS LOW" ALERT. FOLLOWED APPROPRIATE CHECKLIST & LANDED AT DESTINATION. EMERGENCY DECLARED. FOUND ANGLE GEARBOX LOOSE ON HORIZONTAL SHAFT ANGLE GEARBOX CASE SEALS BLOWN, SEVERAL OIL LINES SHMay 20, 2003 · N386FE · Doug DC1010 · Turbine Engine Oil SystemSDR 02FDEA00953Motor · failedR1 ENTRY DOOR HARD TO OPEN, MOTOR SOUNDS LIKE IT SPINS, CLUTCH SLIPS. REMOVED AND REPLACED R1 DOOR ELECTRIC MOTOR, SHAFT, BEARINGS, AND PNEUMATIC MOTOR REF MM.Dec 17, 2002 · N386FE · Doug MD1010F · Passenger/Crew DoorsSDR 02FDEA00954Bearing · wornRT WING OUTBOARD FLAP CARRIAGE ASSY HAS 2 SMALL ROLLER BEARINGS WORN. REMOVED AND REPLACED 2 SMALL ROLLER BEARINGS.Dec 17, 2002 · N386FE · Doug MD1010F · Trailing Edge FlapsSDR 02FDEA00948Brake Assy · damagedNUMBER 2 BRAKE BINDING. DURING TIRE CHANGE, FOUND FIRST THREE SETS OF ROTORS FROZEN & STUCK. REMOVED OLD DEFECTIVE NR 2 BRAKE AND INSTALLED NEW BRAKE IAW MM.Dec 16, 2002 · N386FE · Doug MD1010F · BrakeSDR 02FDEA00918Duct · overheatedRADIO RACK FAN EXHAUST DUCT EXHIBITS SIGNS OF FIRE AND OVERHEATING, INSULATION BLANKETS AND FOAM MATERIAL FROM INSIDE OF DUCT BELOW MAIN CABIN FLOORING AT BS 475 THRU BS 495. R&R DUCT ASSY, BLACK FOAM DETERIORATED. INSPECTION FOUND NO EVIDENCE OF FIRE.Dec 4, 2002 · N386FE · Doug DC1010 · Air Distribution SystemSDR 02FDEA00921Motor · failedDOOR HARD TO OPEN. MOTOR SOUNDS LIKE SPINS, CLUTCH SLIPS. R/R R1 DOOR ELECTRIC MOTOR, SHAFT, BEARINGS AND PNEU MOTOR REF MM 52-11-01-02.Dec 4, 2002 · N386FE · Doug DC1010F · Passenger/Crew DoorsSDR 02FDEA00772O-Ring · damagedNR 3 HYDRAULIC QUANTITY DROPPED TO 4.9 GAL. WITH HYDRAULIC 3 ELEVATOR OFF LEVEL 2 ALERT, DECLARED EMERGENCY. APPROACH, LANDING AND TAXI NORMAL. ON BLOCK IN NR 3 HYDRAULIC QUANTITY WAS DOWN TO 3.4 GAL. FOUND PRESSURE TRANSDUCER LEAKING AT SEALS (O-RINGS). MOct 26, 2002 · N386FE · Doug DC1010 · Hydraulic System, MainSDR 98FDEA00475Fitting · corrodedSNRM 042 STA-LAX - CORROSION FOUND TO EXCEED LIMITS ON NR 1 PYLON AFT MOUNT BULKHEAD FITTING. REMOVED AND REPLACED NR 1 PYLON AFT BULKHEAD FITTING PER SRM 51-00-01.Jul 29, 1998 · N386FE · Doug DC1010 · Engine Mount SectionSDR 98FDEA00324Fitting · crackedSTA-LAX - NR 3 PYLON HAS A HIGH FREQUENCY EDDY CURRENT CRACK INDICATION IN THE OUTBOARD ENGINE TRUSS FITTING AS PER FED-EX EO 8-5410-7-3323 PT W. COMPLIED WITH REPAIR AND TERMINATING MOD EO 8-5410-7-3323 PT 4.May 3, 1998 · N386FE · Doug DC1010 · Nacelle/Pylon Structure
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