N677FE

Service difficulty reports · 275

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 = 'N677FE' 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 FDEA201105031711Floorboard · damagedMAIN CABIN COMPARTMENT FLOORBOARD NR 231 QG IS DAMAGED. FABRICATED NEW FLOORBOARD IAW DWG SRZ 25-005, REV "H".May 3, 2011 · N677FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201105031710Floorboard · damagedMAIN CABIN COMPARTMENT FLOORBOARD 231 KG IS DAMAGED. FABRICATED NEW FLOORBOARD IAW DWG SRZ 25-005, REV "H".May 3, 2011 · N677FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201102280794Indicator · failedGOT ALT 1 FAIL ON ECAM ABOUT 20 TIMES ON THIS FLIGHT. SWITCHED TO A/P NR 2 AND ADC NR 2. ALTIMETER NR 1 WAS INTERMITTENT ON THIS FLIGHT. REMOVED AND REPLACED CAPTAINS MAIN ALTIMETER INDICATOR PER MM 34-12-21-04. PERFORMED BITE TEST OF ADS NR 1 PER MM 34-Feb 28, 2011 · N677FE · Airbus A300F4605R · Altimeter, Barometric/EncoderSDR FDEA201012154696Bearing · wornABOVE 15,000 FT THE AIRPLANE BEGAN TO SHAKE. AUTOPILOT, TURBULENCE, ENGINES, AND SPOILERS WERE ELIMINATED AS FACTORS. APPLYING EITHER RT OR LT RUDDER PRESSURE STOPPED THE SHAKING. IDENTICAL SYMPTOMS IN 2 PRIOR INSTANCES PROVED TO BE RUDDER FLUTTER DUE TO ACDec 15, 2010 · N677FE · Airbus A300F4605R · Rudder ActuatorSDR FDEA200902200615Smoke Detector · failedFWD CARGO COMP SMOKE ECAM ALERT AND OVERHEAD LIGHT INDICATION AT CRUISE. HAD RAMP DG PEOPLE LOOK AT ALL OF THE FREIGHT INSIDE THE CANS FROM THE FORWARD LOWER BELLY. PER RAMP MANAGER, NONE OF THE FREIGHT SHOWED ANY SIGNS OF FIRE, SMOKE, OR CHEMICAL DAMAGE. IFeb 20, 2009 · N677FE · Airbus A300F4605R · Smoke DetectionSDR FDEA200902180582Valve · malfunctionedLOW FUEL TANK APPEARS TO BURN FUEL WITH FUEL IN INNER AND CTR TANKS. TRIED MANUAL FUEL FEED PROCEDURES, TURNING OFF LOW PUMPS, BUT LOW TANK FUEL QTY CONTINUED TO DECREASE. REFUEL OUTER TANK AND OBSERVED STEADY FUEL MIGRATION TO INNER TANKS PER A300-600 AMMFeb 18, 2009 · N677FE · Airbus A300F4605R · Aircraft Fuel Distribution SystemSDR FDEA200902030437Smoke Detector · failedAFTER ADVANCING THROTTLES TO 60 PERCENT N1 FOR ENGINE ANTI-ICE CHECK AND 10 KNOTS AVIONICS SMOKE LIGHT ILLUMINATED. FOLLOWED ECAM CLEARED RWY. REPLACED COCKPIT SMOKE DETECTOR 13WA PER MM, 26-15-12-4 TESTED PER MM 26-15-00-5 TEST WAS NORMAL.Feb 3, 2009 · N677FE · Airbus A300F4605R · Smoke DetectionSDR 08FDEA04540Skin · chafedRT WING INBD FLAP UPPER SURFACE 12 INCHES AFT OF FWD SPAR AND 1 INCH OTBD OF RIB 12 HAS 2 CHAFED AREA, 2 SQ INCHES CUT OUT DAMAGED AREA AND INSTALLED FLAPS, SKIN PATCH REPAIR DOUBLER ON RT WING INBD FLAP UPPER SKIN AT RIB 12 IAW A300-600 SRM 57-50-00, FIG 205,Oct 25, 2008 · N677FE · Airbus A300F4605R · Trailing Edge FlapsSDR 08FDEA04440Skin · gougedLT FUSELAGE EXTERIOR SKIN AT FRAME 38.2 STRINGER 40L HAS A GOUGE MEASURING 1/2 INCH BY 1 INCH BY .015 INCH DEEP. CUT OUT DAMAGED SKIN AND INSTALLED A REPAIR DOUBLER AND FILLER IAW A300-600 SRM 53-10-12 FIG 207 SHT 3.Oct 20, 2008 · N677FE · Airbus A300F4605R · Fuselage Main, Plate/SkinSDR 08FDEA04439Seat Track · wornMDCC SEAT TRACK 4L (Y1456) AT FRAME 60 HAS WORN SCALLOP .30 INCH WIDE BY .20 INCH LONG BY .043 INCH DEEP. REMOVED SEAT TRACK SECTION AT FRAME 60 TO 63 AND INSTALLED NEW SECTION AND SPLICE REPAIR IAW SRM 53-10-16 FIG 201 PG 207/208.Oct 20, 2008 · N677FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR 08FDEA04388Seat Track · wornMAIN CARGO DECK SEAT TRACK NR 3 LEFT HAS 2 WORN SCALLOPS BETWEEN FRAMES 59 LEFT AND FRAME 63 LEFT. REMOVED DAMAGED AREA AND INSTALLED SPLICE REPAIR BETWEEN FRAMES 59 AND 63, AT SEAT TRACK 3 LEFT IAW FREIGHTER SRM 53-10-16.Oct 17, 2008 · N677FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR 08FDEA04350Seat Track · damagedMAIN DECK CARGO COMPT SEAT TRACK NR 1 HAS DAMAGED SCALLOP, FR 71, .30 INCH LONG BY .15 INCH WIDE BY .020 IN DEEP. REMOVED DAMAGED SECTION OF SEAT TRACK NR 1 AND INSTALLED SEAT TRACK SPLICE. REPAIR BETWEEN FR 71 AND FR 72 IAW A300-600 SRM 53-10-16, FIG 201, POct 15, 2008 · N677FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR 08FDEA00188Control Panel · chafedDURING T/O ROLL AT KLAX WHEN SELECTING "LIGHTS ON "FOR TAKEOFF, RECEIVED "ELECTRICAL SHOCK" FROM OVERHEAD LIGHT PANEL. REMOVED AND REPLACED OVERHEAD LIGHT PANEL 426 VU, OP'S CHECKED ALL LIGHT SWITCHES 33-40-00-0. COMPLIED WITH EA 6-3000-118153 FOR PANEL INSTJan 17, 2008 · N677FE · Airbus A300F4605R · Flight Compartment LightingSDR 08FDEA00186Control Panel · unknownDURING T/O ROLL AT KLAX WHEN SELECTING "LIGHTS ON" FOR TAKEOFF, RECEIVED "ELECTRICAL SHOCK" FROM OVERHEAD LIGHT PANEL. REMOVED AND REPLACED OVERHEAD LIGHT PANEL 426 VU, OP'S CHECKED ALL LIGHT SWITCHES 33-40-00-0. COMPLIED WITH EA 6-3000-118153 FOR PANEL INSTJan 17, 2008 · N677FE · Airbus A300F4605R · Flight Compartment LightingSDR 07FDEA00490Valve · malfunctionedNR 2 BLEED FAULT DURING CLIMB-OUT. FAULT DUE TO OVERHEAT. PRESSURED CHECKED MUSCLE LINE ON FAN AIR VALVE TO HP VALVE. CHECKED GOOD. REPLACED FAN AIR VALVE IAW MM 36-11-16-4-02. RAN NR 2 ENGINE AT POWER PER JRH. WITH ENGINE STABILIZED AT POWER THE BLEED PFeb 15, 2007 · N677FE · Airbus A300B4605R · Pneumatic Distribution SystemSDR 06FDEA03580Gcu · contaminatedNR 1 GEN INOP, ALL GCU'S WATER LOGGED. REMOVED AND REPLACE ALL 3 GCU'S IAW THE A310-200 MM 24-22-12-4. ENGINE RUN STILL REQUIRED. RAN ALL ENGINES AND APU PER JRH OPS CKED ALL GENERATORS ALL CHECKED NORMAL.Oct 3, 2006 · N677FE · Airbus A300F4605R · Alternator-Generator DriveSDR 06FDEA03414Skin · dentedFUSELAGE RT SIDE HAS A 1" AREA OF BARE METAL WITH A SMALL DENT (POSSIBLE LIGHTNING STRIKE) AFT OF SIDE WINDOW AT FRAME 10. REMOVED PITTED AREAS IAW A300-600 SRM 51-22-00. REMOVED FASTENER AND REAMED HOLE TO 0.157. ROTO TESTED IAW NTM 51-10-01 AND PERFORMED HSep 25, 2006 · N677FE · Airbus A300F4605R · Fuselage Main, Plate/SkinSDR 06FDEA03398Skin · damagedFASTENER HOLES ELONGATED AT LANDING OF ACCESS PANEL 650LB (30 EA) RIGHT WING. COMPLIED WITH EA 6-5730-104952 PART 1 FOR ELONGATED HOLES IN PANEL LANDING 650LB.Sep 22, 2006 · N677FE · Airbus A300F4605R · Wing, Plate/SkinSDR 06FDEA03363Skin · tool damageFASTENER HOLES HAVE TOOLING MARKS AT LANDING OF ACCESS PANEL 650NB (7 EACH) RIGHT WING COMPLIED WITH EA 6-5730-104952 PART 1 FOR TOOLING MARKS ON PANEL LANDING FOR 650NB.Sep 19, 2006 · N677FE · Airbus A300B4622R · Wing, Plate/SkinSDR 06FDEA03337Skin · dentedLONG CHAFED DENTS APPROX 1M IN 5 EA SECTIONS W/APPROX DEPTH 0.010, 0.010, 0.020, 0.020, 0.010 BETWEEN FR 34-36 AND STRINGER 54L-45L REMOVED DAMAGE AND INSTALLED 2 DOUBLER REPAIRS IAW A300-600 SRM 53-10-12 AND REPROTECTED SURFACE IAW A300-600 SRM 51-75-10. FSep 18, 2006 · N677FE · Airbus A300F4605R · Fuselage Main, Plate/SkinSDR 06FDEA0200Windshield · crackedCAPTAIN`S WINDSHIELD CRACKED. REMOVED CAPT'S WINDSHIELD IAW MM 56-11-11-4. NEW WINDSHIELD IS ON LIFT TRUCK. NEW HARDWARE IS WITH NEW WINDOW. OLD HARDWARE AND TRIM IS IN COCKPIT. OLD SN OFF IS 98036H6658. REMOVED AND REPLACED WINDOW HEAT PROTECTION UNIT, Jan 15, 2006 · N677FE · Airbus A300F4605R · Flight Compartment WindowsSDR 05FDEA04369Engine · unknownT/O FROM RWY 23R IND WIND 120/09 T/O ROLL SEEMED NORMAL UNTIL ABOUT 110KTS. ACCELERATION SLOWED AT APPROX 125KNTS N1S BOTH ENGS STARTED TO ROLL BACK. TARGET N1 WAS 96.1. ABORTED AT 130KTS WHILE N1 WAS DECELERATING THRU 89%. V1 139, VR 139, V2 143.Dec 14, 2005 · N677FE · Airbus A300B4605R · Engine (Turbine/Turboprop)SDR 04FDEA02568Duct · delaminatedAPU INTAKE ELBOW HAS MULTIPLE DEBONDS AND BULGES. REPAIRED APU INTAKE ASSY IAW A300-600 AMM 49-16-14 AND EA 6-4915-81873.Aug 27, 2004 · N677FE · Airbus A300B4605R · APU Core EngineSDR 04FDEA02565Door Frame · gougedAFT CARGO DOOR CUTOUT ON LOWER FWD FRAME, NOTED GOUGES/DAMAGED SURFACE APPROX 13 INCHES LONG. GOUGES RANGE FROM .080 INCH TO .2 INCH. BLENDED AREA AND FOUND TO BE OUT OF LIMITS IAW A300/600 SRM 53-17-12. FABRICATED AND INSTALLED REPAIR DOUBLERS IAW A300/6Aug 26, 2004 · N677FE · Airbus A300F4605R · Fuselage Main, StructureSDR 04FDEA02560Panel · chippedNR 2 ENGINE O/B T/R, LOWER FWD HINGE PNL IS CHIPPED OFF IN TWO PLACES ON THE FWD SIDE. REPAIRED DAMAGED BLOWOUT DOOR PER EA 6-7830-81874. (OPEN)Aug 24, 2004 · N677FE · Airbus A300B4605R · Engine Thrust Reverser
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