N306FE

Service difficulty reports · 167

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 = 'N306FE' 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 07FDEA04652Frame · crackedAIR CONDITIONING COMPT RT SIDE ON FRAME JAMB DOOR FOUND CRACK.Oct 19, 2007 · N306FE · Doug DC1030F · Fuselage Main, FrameSDR 07FDEA04649Frame · crackedFWD AVIONICS COMPT ON FRAME FOUND CRACK.Oct 19, 2007 · N306FE · Doug DC1030F · Fuselage Main, FrameSDR 07FDEA04511Skin · crackedDURING VISUAL INSP OF HORIZONTAL STAB SKIN PANEL INSPECTION, FOUND CRACK ON PANEL P/N 7439-2 SERIES -10, REPAIRED AREA IAW EA# 8-5510-111620.Oct 5, 2007 · N306FE · Doug DC1030F · Horizontal Stabilizer, Plate/SkinSDR 07FDEA04509Panel · crackedDURING U/S INSP OF HORIZONTAL STAB, FOUND CRACK ON PANEL P/N 7227-1, POSITION 14, CRACK IS IN FLYABLE LIMITS, ATTACHED INSPECTION FINDING FORM FOR A11 DETAIL. REPAIRED AREA IAW EA 8-5510-111537.Oct 5, 2007 · N306FE · Doug DC1030F · Horizontal Stabilizer StructureSDR FDEA200710014430Skin · looseDURING INSPECTION ON LT WING OTBD FLAP UPPER SKIN FOUND 200 LOOSE FASTENERS. REPAIRED AREA IAW SRM 51-35-01 PAR 1-5 VOL II.Oct 1, 2007 · N306FE · Doug DC1030F · Trailing Edge FlapsSDR FDEA200710014429Skin · looseDURING INSPECTION ON LT WING OTBD FLAP LWR SKIN FOUND 100 LOOSE FASTENERS. REPAIRED AREA IAW SRM 51-35-01 PAR 1-5 VOL II.Oct 1, 2007 · N306FE · Doug DC1030F · Trailing Edge FlapsSDR FDEA200710014425Skin · looseDURING INSPECTION ON RT WING OTBD FLAP LWR SKIN FOUND 50 LOOSE FASTENERS. REPAIRED AREA IAW SRM 57-00-01 VOL I FIG 4 SHT 5.Oct 1, 2007 · N306FE · Doug DC1030F · Wing, Plate/SkinSDR 07FDEA04430Skin · looseDURING INSPECTION ON LT WING OUTBD FLAP UPPER SKIN FOUND 200 LOOSE FASTENERS.Oct 1, 2007 · N306FE · Doug DC1030 · Trailing Edge FlapsSDR 07FDEA04429Skin · looseDURING INSPECTION ON LT WING OUTBD FLAP LWR SKIN FOUND 100 LOOSE FASTENERS.Oct 1, 2007 · N306FE · Doug DC1030F · Trailing Edge FlapsSDR 07FDEA04425Skin · looseDURING INSPECTION ON RT WING OUTBD FLAP LWR SKIN FOUND 50 LOOSE FASTENERS.Oct 1, 2007 · N306FE · Doug DC1030 · Trailing Edge FlapsSDR 06FDEA04285Skin · gougedLWR SURFACE OF WING JUST O/B OF AFT PYLON HAS DEEP GAUGE FROM DEPARTURE OF PYLON "V" PANEL DURING FLIGHT NR 3 PYLON. GOUGE LOCATION ON RIGHT WING BOTTOM SKIN BETWEEN S41 AND S40 AT XORS 372.0. GOUGE MEASURES 5.5 IN LONG AND 0.060 DEEP AT DEEPEST POINT. GODec 19, 2006 · N306FE · Doug DC1030 · Wing, Plate/SkinSDR 06FDEA1570Valve · leakingAFTER TAKEOFF HEARD LOUD BANG AND PRONOUNCED BURNT RUBBER SMELL IN PERMEATE FLIGHT DECK, SUSPECTED BLOWN TIRE. LOWERED GEAR AND RETURNED FOR LANDING. INSP NOSE GEAR, NOSE TIRES, AND NOSE STEERING, NOSE BRAKES, PACK COMPTS, CANS, FWD AVI COMPT ALL RACKS, CNTApr 22, 2006 · N306FE · Doug DC1030 · Standard Practices/StructuresSDR 04FDEA03389Filter · cloggedAFTER T/O DURING LANDING GEAR RETRACTION, OBSERVED BOTH NR 1 AND 3 ENG FUEL FILTER PRESSURE DROP LIGHTS WERE ILLUMINATED. AFTER SELECTING CLIMB POWER. THE NR 3 LIGHT EXTINGUISHED AND NR 1 REMAINED ILLUMINATED. LEVELED OFF AT 5000 FT AND WHEN THE POWER WAS Dec 7, 2004 · N306FE · Doug DC1030F · Engine Fuel DistributionSDR 04FDEA01439Warning Light · intermittentLEFT MAIN GEAR LIGHT REMAINED ILLUMINATED WITH GEAR HANDLE UP/IN, S/O PANEL LEFT GEAR (MAIN) LIGHT WAS INTERMITTENTLY ON. COMPLETED RED TABS, ALL LIGHTS CHECKED OUT. PERFORMED SELF CHECK OF PSEU CHECK CHANNELS 8, 12, 16 AND 20, NO FAULTS NOTED AND PER DC-10-May 25, 2004 · N306FE · Doug DC1030 · Landing Gear Position and WarningSDR 03FDEA0043Beam · corrodedTEE CAP AEA 7097-1, STA.1521 WAS FOUND CORRODED AT RT STA.-80.125 WHERE VERTICLE BEAM A0024-2 ATTACHES. THE BEAM ATTCHMENT TO THE TEE CAP CREATES A (V) WHERE WATER CAN PUDDLE. AWAITING APPROVED REPAIR FROM BOEINGJan 16, 2003 · N306FE · Doug DC1030F · Fuselage Main, StructureSDR 00FDEA00459Control Cable · damagedDURING DESCENT, NR 2 THROTTLE STUCK AT 88 PERCENT N2. THROTTLE WILL MOVE BUT N2 REMAINS AT 88 PERCENT N2 AND THROTTLE RETURNS TO ORIG POS. REMOVED AND REPLACED NR 2 ENG PUSH PULL CABLE REF MM 76-11-01-2. RIGGED PER DC-10 MM 76-11-01-2 AND SECURED ALL ROD ENJul 13, 2000 · N306FE · Doug DC1030F · Power LeverSDR 98FDEA00227Hose Assy · brokenAPPROXIMATELY 20 MIN INTO FLIGHT, NR 2 HYD QUANTITY AND PRESSURE WENT TO ZERO. ENGINE RAN APPROXIMATELY 55 MINUTES BEFORE SHUTING DOWN. T/S FOUND NR 2 ENG FIRE-RESISTANT HOSE ASSY BROKEN. REPLACED NEW HOSE ASSY AND REPLACED BOTH ENG DRIVE PUMP AND FILTERS CMar 31, 1998 · N306FE · Doug DC1030F · Hydraulic System, Main
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