# Service difficulty reports: N386FE, cancelled Apr 13, 2024

A list on [N386FE, cancelled Apr 13, 2024](https://openairdocs.org/deregistered/N386FE-2024-04-13.md).

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

- [SDR FDEA201302090312](https://openairdocs.org/sdr/FDEA201302090312.md): Girt Bar · obstructed · Feb 9, 2013 · N386FE · Doug MD1010F · Emergency Equipment
  > OUTSIDE 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 ASSY
- [SDR FDEA201111235006](https://openairdocs.org/sdr/FDEA201111235006.md): Element · failed · Nov 23, 2011 · N386FE · Doug MD1010F · Pneumatic Indicating System
  > AFTER 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 PNE
- [SDR FDEA201103311255](https://openairdocs.org/sdr/FDEA201103311255.md): Warning Light · illuminated · Mar 31, 2011 · N386FE · Doug MD1010F · Engine Bleed Air System
  > CLIMBING 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.
- [SDR FDEA201103181170](https://openairdocs.org/sdr/FDEA201103181170.md): Skin · corroded · Mar 18, 2011 · N386FE · Doug MD1010F · Fuselage Main, Plate/Skin
  > SKIN 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 CORRO
- [SDR FDEA201103020825](https://openairdocs.org/sdr/FDEA201103020825.md): Floorbeam · corroded · Mar 2, 2011 · N386FE · Doug MD1010F · Fuselage Main, Floor Beam
  > CENTER CARGO COMPARTMENT FLOORBEAM CORRODED/EXFOLIATED AT BS 1781, RBL 36.
- [SDR FDEA201103021171](https://openairdocs.org/sdr/FDEA201103021171.md): Fitting · cracked · Mar 2, 2011 · N386FE · Doug MD1010F · Fuselage Main, Attach Fittings
  > CAC 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. ACCOMPLISHED
- [SDR FDEA201102040467](https://openairdocs.org/sdr/FDEA201102040467.md): Power Supply · failed · Feb 4, 2011 · N386FE · Doug MD1010F · Emergency Lighting
  > EMERGENCY 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.
- [SDR FDEA200904021164](https://openairdocs.org/sdr/FDEA200904021164.md): None · none · Apr 2, 2009 · N386FE · Doug MD1010F · Standard Practices/Structures
  > AT 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, G
- [SDR FDEA200902190593](https://openairdocs.org/sdr/FDEA200902190593.md): Spar Cap · cracked · Feb 19, 2009 · N386FE · Doug MD1010F · Wing Spar
  > FUEL 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.
- [SDR FDEA200902020425](https://openairdocs.org/sdr/FDEA200902020425.md): Window Frame · cracked · Feb 2, 2009 · N386FE · Doug MD1010F · Fuselage Main, Structure
  > CAPTAIN SLIDING VIEW WINDOW FRAME AIRPLANE SIDE CRACKED OUTSIDE (MARKED).
- [SDR 07FDEA04975](https://openairdocs.org/sdr/07FDEA04975.md): Control Valve · malfunctioned · Dec 1, 2007 · N386FE · Doug MD1010F · Landing Gear Retraction/Extension System
  > ON 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
- [SDR 07FDEA04381](https://openairdocs.org/sdr/07FDEA04381.md): Engine · damaged · Sep 29, 2007 · N386FE · Doug MD1010F · Engine (Turbine/Turboprop)
  > CLIMBING 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
- [SDR 06FDEA1312](https://openairdocs.org/sdr/06FDEA1312.md): Engine · failed · Apr 5, 2006 · N386FE · Doug MD1010F · Engine (Turbine/Turboprop)
  > ON 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,
- [SDR 06FDEA1310](https://openairdocs.org/sdr/06FDEA1310.md): Engine · failed · Apr 4, 2006 · N386FE · Doug DC1010 · Turbine Engine Reduction Gear
  > ON 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
- [SDR 04FDEA02071](https://openairdocs.org/sdr/04FDEA02071.md): Floorbeam · damaged · Jul 14, 2004 · N386FE · Doug MD1010F · Fuselage, Seat/Cargo Attach Fittings
  > FLOORBEAM 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.
- [SDR 04FDEA02026](https://openairdocs.org/sdr/04FDEA02026.md): Control Cable · crossed · Jul 7, 2004 · N386FE · Doug MD1010F · Flight Control System
  > AFT 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 I
- [SDR 04FDEA02025](https://openairdocs.org/sdr/04FDEA02025.md): Panel · dented · Jul 7, 2004 · N386FE · Doug MD1010F · Wing, Plate/Skin
  > RIGHT 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. REF
- [SDR 04FDEA02022](https://openairdocs.org/sdr/04FDEA02022.md): Skin · dented · Jul 7, 2004 · N386FE · Doug MD1010F · Fuselage Main, Plate/Skin
  > SEVERAL 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.
- [SDR 04FDEA02021](https://openairdocs.org/sdr/04FDEA02021.md): Skin · dented · Jul 7, 2004 · N386FE · Doug MD1010F · Fuselage Main, Plate/Skin
  > SEVERAL 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.
- [SDR 04FDEA02019](https://openairdocs.org/sdr/04FDEA02019.md): Door Frame · corroded · Jul 7, 2004 · N386FE · Doug MD1010F · Fuselage Main, Structure
  > FORWARD 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,
- [SDR 04FDEA02018](https://openairdocs.org/sdr/04FDEA02018.md): Static Port · damaged · Jul 7, 2004 · N386FE · Doug MD1010F · Pitot/Static System
  > RIGHT 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 MD10-1
- [SDR 04FDEA02016](https://openairdocs.org/sdr/04FDEA02016.md): Skin · corroded · Jul 7, 2004 · N386FE · Doug MD1010F · Ailerons
  > RIGHT 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.
- [SDR 04FDEA02015](https://openairdocs.org/sdr/04FDEA02015.md): Beam · cracked · Jul 7, 2004 · N386FE · Doug MD1010F · Wing Main, Frame Structure
  > RIGHT 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 AND
- [SDR 04FDEA00468](https://openairdocs.org/sdr/04FDEA00468.md): Warning System · activated · Feb 20, 2004 · N386FE · Doug DC1010 · Fuel Indicating System
  > AT 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 UNEVENTFULLY
- [SDR 03FDEA01948](https://openairdocs.org/sdr/03FDEA01948.md): Selector Valve · failed · Nov 18, 2003 · N386FE · Doug DC1010 · Landing Gear Selector
  > AT 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
- [SDR 03FDEA00780](https://openairdocs.org/sdr/03FDEA00780.md): Engine · malfunctioned · May 20, 2003 · N386FE · Doug DC1010 · Turbine Engine Oil System
  > CRUISE 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 SH
- [SDR 02FDEA00953](https://openairdocs.org/sdr/02FDEA00953.md): Motor · failed · Dec 17, 2002 · N386FE · Doug MD1010F · Passenger/Crew Doors
  > R1 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.
- [SDR 02FDEA00954](https://openairdocs.org/sdr/02FDEA00954.md): Bearing · worn · Dec 17, 2002 · N386FE · Doug MD1010F · Trailing Edge Flaps
  > RT WING OUTBOARD FLAP CARRIAGE ASSY HAS 2 SMALL ROLLER BEARINGS WORN. REMOVED AND REPLACED 2 SMALL ROLLER BEARINGS.
- [SDR 02FDEA00948](https://openairdocs.org/sdr/02FDEA00948.md): Brake Assy · damaged · Dec 16, 2002 · N386FE · Doug MD1010F · Brake
  > NUMBER 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.
- [SDR 02FDEA00918](https://openairdocs.org/sdr/02FDEA00918.md): Duct · overheated · Dec 4, 2002 · N386FE · Doug DC1010 · Air Distribution System
  > RADIO 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.
- [SDR 02FDEA00921](https://openairdocs.org/sdr/02FDEA00921.md): Motor · failed · Dec 4, 2002 · N386FE · Doug DC1010F · Passenger/Crew Doors
  > DOOR 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.
- [SDR 02FDEA00772](https://openairdocs.org/sdr/02FDEA00772.md): O-Ring · damaged · Oct 26, 2002 · N386FE · Doug DC1010 · Hydraulic System, Main
  > NR 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). M
- [SDR 98FDEA00475](https://openairdocs.org/sdr/98FDEA00475.md): Fitting · corroded · Jul 29, 1998 · N386FE · Doug DC1010 · Engine Mount Section
  > SNRM 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.
- [SDR 98FDEA00324](https://openairdocs.org/sdr/98FDEA00324.md): Fitting · cracked · May 3, 1998 · N386FE · Doug DC1010 · Nacelle/Pylon Structure
  > STA-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.

## The whole list in SQL

Runs in DuckDB 1.2 or later on the release's Parquet files over HTTPS:

```sql
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
```

This list as a web page: https://openairdocs.org/deregistered/N386FE-2024-04-13/reports

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