N668FE

Service difficulty reports · 250

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 = 'N668FE' 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 FDEA201103171044Floor Panel · damagedMAIN CABIN COMPARTMENT FLOOR PANEL 252 PG IS DAMAGED. FABRICATED NEW FLOOR PANEL 252 PG IAW DWG SRZ 25-005, REV "H".Mar 17, 2011 · N668FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201103171043Floor Panel · damagedMAIN CABIN COMPARTMENT FLOOR PANEL 251 BH IS DAMAGED. FABRICATED NEW FLOOR PANEL 251 BH IAW DWG SRZ 25-005, REV "H".Mar 17, 2011 · N668FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201103171042Floor Panel · damagedMAIN CABIN COMPARTMENT FLOOR PANEL 251 QH IS DAMAGED. FABRICATED NEW FLOOR PANEL 251 QH IAW DWG SRZ 25-005, REV "H".Mar 17, 2011 · N668FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201103171041Floor Panel · damagedMAIN CABIN COMPARTMENT FLOOR PANEL 241 AJ IS DAMAGED. FABRICATED NEW FLOOR PANEL 241 AJ IAW DWG SRZ 25-005, REV "H".Mar 17, 2011 · N668FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201103171040Floor Panel · damagedMAIN CABIN COMPARTMENT FLOOR PANEL 242 ZJ IS DAMAGED. FABRICATED NEW FLOOR PANEL 242 ZJ IAW DWG SRZ 25-005, REV "H".Mar 17, 2011 · N668FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201103171039Floor Panel · damagedMAIN CABIN COMPARTMENT FLOOR PANEL 232 YG IS DAMAGED. FABRICATED NEW FLOOR PANEL 232 YG IAW DWG SRZ 25-005, REV "H".Mar 17, 2011 · N668FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201103171038Floor Panel · damagedMAIN CABIN COMPARTMENT FLOOR PANEL 232 TG IS DAMAGED. FABRICATED NEW FLOOR PANEL 232 TG IAW DWG SRZ 25-005, REV "H".Mar 17, 2011 · N668FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201103171037Floor Panel · damagedMAIN CABIN COMPARTMENT FLOOR PANEL 232 NG IS DAMAGED. FABRICATED NEW FLOOR PANEL 232 NG IAW DWG SRZ 25-005, REV "H".Mar 17, 2011 · N668FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201103171036Floor Panel · damagedMAIN CABIN COMPARTMENT FLOOR PANEL 232 HG IS DAMAGED. FABRICATED NEW FLOOR PANEL 232 HG IAW DWG SRZ 25-005, REV "H".Mar 17, 2011 · N668FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201103171035Floor Panel · damagedMAIN CABIN COMPARTMENT FLOOR PANEL 231 VG IS DAMAGED. FABRICATED NEW FLOOR PANEL 231 VG IAW DWG SRZ 25-005, REV "H".Mar 17, 2011 · N668FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201103171034Floor Panel · damagedMAIN CABIN COMPARTMENT FLOOR PANEL 231 QG IS DAMAGED. FABRICATED NEW FLOOR PANEL 231 QG IAW DWG SRZ 25-005, REV "H".Mar 17, 2011 · N668FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201103171033Floor Panel · damagedMAIN CABIN COMPARTMENT FLOOR PANEL 231 EF IS DAMAGED. FABRICATED NEW FLOOR PANEL 231 EF IAW DWG SRZ 25-005, REV "H".Mar 17, 2011 · N668FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201103161016Intercostal · crackedAFT MAIN CABIN LT SIDE BETWEEN FRAME 79 & FRAME 80/82 AT FLOOR LEVEL; INTERCOSTAL WEB STRUCTURE IS CRACKED, STRINGER 26L-STRINGER 26L. REMOVED CRACKED WEB INTERCOSTAL IAW SRM 51-40-21, PARA 7. RECEIVED NEW WEB IAW DWG 18A53981113, ISSUE "A", PO 686125.1. LOMar 16, 2011 · N668FE · Airbus A300F4605R · Fuselage Miscellaneous StructureSDR FDEA201103150975Frame · crackedFWD CARGO COMPARTMENT OVERHEAD FLOORBEAM; FWD SIDE OF FRAME 30 & LBL 27 IS CRACKED.Mar 15, 2011 · N668FE · Airbus A300B4605R · Fuselage Main, FrameSDR FDEA201103010807Jackscrew · failedDURING FLAP RETRACTION FLAPS STUCK AT 20 DEGS WITH FLAPS FAULT SYS 1 & 2 LIGHT ON OVERHEAD. FOLLOWED ECAM/QRCH FLAPS REMAINED AT 20 DEGS AT 20 DEGS. ON APPROACH SELECTED AND GOT FLAPS 40. AFTER LANDING FLAPS RETRACTED NORMALLY-REPEAT. REMOVED AND REPLACEMar 1, 2011 · N668FE · Airbus A300F4605R · Trailing Edge Flap Control SystemSDR FDEA201102240707Jackscrew · stuckON TAKEOFF, WHEN FLAP HANDLE WAS RAISED, ECAM SHOWED FLAPS 1 AND 2 FAULT WITH FAULT LIGHTS ON OVERHEAD PANEL AS WELL. FLAPS STUCK AT 20 DEGREES, CYCLED HANDLE AND STILL HAD FLAPS STUCK AT 20 DEGREES. RETURNED TO LANDING, NORMAL. INSPECTED THE NR 3 LT FLAP Feb 24, 2011 · N668FE · Airbus A300F4605R · Trailing Edge Flap Control SystemSDR FDEA201101190287Jackscrew · inoperativeFLAP SYSTEM 1, 2, FAULT ON OVERHEAD PANEL ON ECAM. ATTEMPTED TO CYCLE FLAP HANDLE BUT PROBLEM REMAINED. FOLLOWED QRH RETURNED TO DEPARTURE. HAPPENED WHEN FLAPS 15 SELECTED. FLAPS APPEARED STUCK APPROX 13-14 DEG, WOULD NOT MOVE PAST THAT. ACFT BELOW MAX LJan 19, 2011 · N668FE · Airbus A300F4605R · Trailing Edge Flap Control SystemSDR FDEA201012154694Limiter · malfunctionedFLAPS FAULT 1 & 2 STUCK AT 20. SFCC 1 AND 2 INDICATES SLAT 00001 / FLAP 011111. (LT EXTEND SWITCH KRUGER / NOTCH) AND (FLAP JAM) REF TO SFCC BITE CHECK TSM 27-50-00. FOUND LT TORQUE LIMITER POPPED (INDICATING ACTIVATED).Dec 15, 2010 · N668FE · Airbus A300F4605R · Trailing Edge Flap Control SystemSDR FDEA200909263391Indication Sys · malfunctionedON CAT III APP GOT EGPWS TERRAIN WARNING-ACCOMPLISHED EGPWS ESCAPE MANUVER AT APPROX 400 FT AGL WITH FIREWALL POWER, HOWEVER EXCEEDENCE INDICATORS DID NOT EXCEED. OP CHECKED EGPWS 4 TIMES IAW AMM 34-48-01-5. COULD NOT DUPLICATE DISCREPANCY ON THE GROUND. Sep 26, 2009 · N668FE · Airbus A300F4605R · Ground Proximity SystemSDR FDEA200909263387Indication Sys · malfunctionedAPPROACHING ON CAT III APP GOT EGPWS TERRAIN WARNING-ACCOMPLISHED EGPWS ESCAPE MANEUVER AT APPROX 400 FT AGL WITH FIREWALL POWER, HOWEVER, EXCEEDENCE INDICATORS DID NOT EXCEED. OP CHECKED EGPWS 4 TIMES IAW AMM 34-48-01-5, COULD NOT DUPLICATE DISCREPANCY OSep 26, 2009 · N668FE · Airbus A300F4605R · ATC Transponder SystemSDR FDEA200905141662Valve · leakingSUSPECT MAJOR FUEL LEAK RT INNER TANK. ALSO IT MAY SOME HOW TRANSFERRED FUEL TO LEFT INNER FOB MINUS FBO ARE VERY CLOSE TO TAKEOFF FUEL. TRANSFERRED FUEL FROM LT TO RT TANK AND DETERMINED THAT FUEL HAD INDEED MIGRATED TO THE LT TANK. BALANCED FUEL LOADS AND May 14, 2009 · N668FE · Airbus A300B4605R · Aircraft Fuel Distribution SystemSDR FDEA200903241025Steering Sys · malfunctionedON TAKEOFF, AFTER TOGA WAS SET, NOSE OF ACFT VEERED RIGHT. TILER WAS INEFFECTIVE IN STRAIGHTENING OUT. SUSPECTED DRAGGING RIGHT BRAKES. ABORTED TAKEOFF AND HAD SAN RAMP LOOK OVER WHEELS AND BRAKES. EVERYTHING CHECKED GOOD. TAXIED OUT AND TAKEOFF REST OF Mar 24, 2009 · N668FE · Airbus A300F4605R · Landing Gear Steering SystemSDR FDEA200812175231Wire · disconnectedDURING CLIMB-OUT, ABOUT 10,000, LT OUTER FUEL QTY BEGAN TO DECREASE. CENTER TANKS (BOTH) FAULTED EVEN THOUGH 400 LBS PRESENT OR INDICATED. LT OUTER DECREASED TO BELOW 1,000 LBS. DURING DESCENT, LT OUTER FUEL QTY INDICATION BEGAN TO INCREASE RISING TO 3,400Dec 17, 2008 · N668FE · Airbus A300F4605R · Fuel System WiringSDR FDEA200812155158Indication Sys · malfunctionedDURING CLIMB, THRU APPROX 18K, NOTICED LT OUTER FUEL QTY DECREASING AT APPROX 500-1000 LBS MIN, THIS WAS ON THE ECAM AND OVHD PANEL. REF QRH UNDER "POSSIBLE FUEL LEAK" PULLED FQI CHAN SUPPLY 1 2 C/B'S. WHEN FUEL INDICATIONS RETURNED LT OUTER RESUMED IT'S STEDec 15, 2008 · N668FE · Airbus A300F4605R · Fuel Quantity IndicatorSDR FDEA200812135138Wire · damagedDURING CLIMB THRU 18K, LOW FUEL QTY DECREASING AT APPX 500-1000 LBS/MIN, THIS WAS ON THE ECAM & OVHD PANEL. REF QRH, "POSSIBLE FUEL LEAK" PULLED FQI CHAN SUPPLY 1 2 C/B'S. WHEN FQI RETURNED LOW RESUMED IT'S STEADY DECREASE. AFTER LANDING, ALL FUEL IND'S RETDec 13, 2008 · N668FE · Airbus A300F4605R · Fuel System WiringSDR 08FDEA04617Floorbeam · damagedGUIDE BROKE AT POS 9L WITH FLOOR DAMAGE REMOVED DAMAGED SECTION AT FLOORBEAM FRAME 64 BETWEEN SEAT TRACK NR 3 LT AND NR 4 LT AND REPAIRED IAW FEDEX EA 6-5310-117443, RELEASE DATE 11/14/07.Oct 29, 2008 · N668FE · Airbus A300F4605R · Fuselage Main, Floor BeamSDR 08FDEA04543Frame · crackedNR 1 ENG INBD T/R FWD FLANGE FOR MOUNTING RING LATCH ASSY HAS 2 INCH CRACK AT 12 O'CLOCK POS REMOVED CRACK AND REPAIRED NR 1 ENG INBD T/R FWD FLANGE IAW FEDEX EA 6-7830-124133, RELEASE DATE 8 OCTOBER, 2008.Oct 25, 2008 · N668FE · Airbus A300F4605R · Engine Thrust ReverserSDR 08FDEA04541Frame · crackedNR 1 ENG OTBD T/R FWD FLANGE FOR MOUNTING RING LATCH ASSY HAS 2.25 IN CRACK AT 12 O'CLOCK POS REMOVED CRACK AND REPAIRED NR 1 OTBD T/R FWD FLANGE IAW FEDEX EA 6-7830-124134, RELEASE DATE 8 OCTOBER, 2008.Oct 25, 2008 · N668FE · Airbus A300F4605R · Engine Thrust ReverserSDR 08FDEA04501Seat Track · wornFUSELAGE AUXILIARY STRUCTURES, 2 WORN LOBES ON SEAT TRACK Y2462 RT AT FRAME 20. REMOVED DAMAGED SEAT TRACK SECTION FROM BETWEEN FRAMES 18/19 TO BETWEEN FRAME 27/28 AND REPLACED IAW SRM 53-13-16 CONFIG 2 ITEM 40 AND EA6-5320-105302C PT3.Oct 23, 2008 · N668FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR 08FDEA04500Seat Track · wornMDCC SEAT TRACK (Y1959) LT NR 5 AT FRAME 30 HAS 1 ELONGATED SCALLOP. REPAIRED SEAT TRACK (Y1959) LT NR 5 AT FRAME 30 BY USING SPLICE FROM FRAME 27 TO BETWEEN FR 32 AND 33 IAW A300-600 FREIGHTER SRM 53-10-16 FIG 201A PGS 203-208.Oct 23, 2008 · N668FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR 08FDEA04499Track · damagedRT NR 5 (-Y1959) AFT DUMMY TRACK AT FRAME 54.1 HAS 6 FASTENERS IMPROPERLY INSTALLED AND 1 HOLE IS ELONGATED ON INBD AFT FLANGE OF DUMMY TRACK. REPAIRED RT NR 5 (-Y1959) AFT DUMMY TRACK AT FRAME 54.1 IAW A300-600 FREIGHTER SRM 53-10-16 FIG 202.Oct 23, 2008 · N668FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR 08FDEA04484Frame · crackedNR 2 ENG OTBD T/R FWD FLANGE FOR MOUNTING RING LATCH ASSY HAS 2.750 INCH CRACK AT 12 O'CLOCK POSITION. REPAIRED CRACK ON NR 2 OTBD T/R FLANGE IAW FEDEX EA 6-7830-124135, RELEASE DATE 8 OCTOBER, 2008.Oct 22, 2008 · N668FE · Airbus A300F4605R · Engine Thrust ReverserSDR 08FDEA04482Floorbeam · crackedFWD CARGO COMPT FR 31 BETWEEN SEAT TRACK NR 4 LT AND TRACK NR 5 LT FLOORBEAM HAS .25 INCH CRACK. REMOVED CRACK AND INSTALLED CROSSBEAM REPAIR AT CRACKED STIFFENER AT FR 31, BETWEEN SEAT TRACK NR 4 LT AND NR 5 LT IAW SRM 53-10-15, FIG 212, PAGE 397/398.Oct 22, 2008 · N668FE · Airbus A300F4605R · Fuselage Main, Floor BeamSDR 08FDEA04383Floorbeam · crackedMAIN DECK CARGO COMPT FLOORBEAM CRACKED AT FR 64, BETWEEN SEAT TRACK NR 3 RT AND NR 4 RT, .25 INCH LONG. CUT OUT DAMAGED AREA AND INSTALLED CROSSBEAM REPAIR AT FR 64, BETWEEN SEAT TRACKS NR 3 RT AND NR 4 RT IAW SRM 53-10-15, FIG 211, PAGE 389/390.Oct 16, 2008 · N668FE · Airbus A300F4605R · Fuselage Main, Floor BeamSDR 08FDEA04349Frame · crackedNR 2 ENG INBD THRUST REVERSER HAS A CRACK .225 INCH LONG ON UPPER FWD END FRAME ROUTED CRACK ON NR 2 ENG INBD T/R TORQUE BOX FWD FRAME AND REPAIRED IAW FEDEX EA 6-7830-124136, RELEASE DATE 8 OCTOBER, 2008.Oct 15, 2008 · N668FE · Airbus A300F4605R · Engine Thrust ReverserSDR 08FDEA02095Bracket · failedREPEAT WRITE-UP- DURING FINAL APPROACH PHASE, LEFT LANDING GEAR WOULD NOT INDICATE DOWN AND LOCKED AFTER GEAR SELECTED DOWN. RECYCLED GEAR HANDLE WITH SAME RESULT, COMPLIED WITH ALL ECAM AND QRH ITEMS. TRIED SIDE SLIPS AFTER MANUALLY LOWERING GEAR. NO HELPJun 2, 2008 · N668FE · Airbus A300F4605R · Fuselage Miscellaneous StructureSDR 08FDEA02076Sequence Valve · failedON FINAL APPROCH DURING LANDING GEAR EXTENSION, LEFT MAIN GEAR WOULD NOT EXTEND. RED GEAR NOT DOWN INDICATION ON BOTH POSITION 1 AND 2 AND OVERHEAD PANEL. PROCEEDED WITH LANDING GEAR GRAVITY EXTENSION PROCEDURE. ALL GEAR DOORS OPENED BUT LEFT MAIN GEAR STILJun 1, 2008 · N668FE · Airbus A300F4605R · Landing Gear Retraction/Extension SystemSDR 07FDEA00379Unknown · unknownON T/O ROLL ECAM SHOWED NR 2 ENGINE REVERSER PRESSURIZED. CYCLED REVERSER WITH NO HELP. RELEASED FOR SERVICE PER MEL/CDL: 78-30-01-A CATEGORY: C EXPIRATION: 18FEB07 "MEL 78-30-01-A: ENGINE NR 2 THRUST REVERSER INOP. THRUST REVERSER IS DEACTIVATED IFeb 8, 2007 · N668FE · Airbus A300B4622R · Engine Thrust ReverserSDR 07FDEA00206Thrust Reverser · inoperativeAT 75 KNOTS, THE NR 2 ENG REV PRESSURE LIGHT CAME ON. ACN RELEASED FOR SERVICE PER MEL/CDL: 78-30-01-A CATEGORY: C EXPIRATION: 10FEB07 "MEL 78-30-01-A: ENGINE (IDENTIFY 1 OR 2) NR 2 THRUST REVERSER, INOP. THRUST REVERSER IS DEACTIVATED IN FORWARD THRUST POSJan 31, 2007 · N668FE · Airbus A300F4605R · Engine Thrust ReverserSDR 06FDEA04257Line · rupturedAFTER TAKEOFF, WHEN GEAR UP WAS SELECTED THE NOSE GEAR RETRACTING WAS EXCESSIVELY NOISY. SHORTLY THEREAFTER, ALL GREEN HYD QUANTITY WENT TO ZERO, WITH ECAM. ECAM AND OVERHEAD DISPLAYED ZERO QUANTITY. GREEN PRESSURE 3200 PSI FOR 3 MINUTES. QRH DIRECTED PUMPDec 16, 2006 · N668FE · Airbus A300F4605R · Hydraulic System, MainSDR 06FDEA04158Unknown · contaminatedLANDED ON ORD RW09R WITH CONTAMINATED RW. STOPPED WITH LEFT MAIN GEAR OFF THE LEFT SIDE OF THE RW. RT GEAR STILL ON THE RW. NOSE SLIGHTLY OFF THE LEFT. PSC COMPLIED INSPECTION IAW AMM 05-51-24-0. AIRCRAFT FOUND TO BE AIRWORTHY.Dec 2, 2006 · N668FE · Airbus A300F4605R · Standard Practices/StructuresSDR 06FDEA0690Line · failedSLOWING TO 250 KNTS FOR DESCENT NOTICED AN INCREASED VIBRATION THAT FELT LIKE IT WAS ENGINE. NORMAL LANDING KMHT (NOT A DIVERSION). FOUND T/R -Y- CHK VALVE NR 1 ENGINE LOWER SUPPLY LINE BLOWN APART. REMOVED LINE AND ORDERED PARTS. UPON FURTHER INVESTIGATIOFeb 11, 2006 · N668FE · Airbus A300F4605R · Engine Thrust ReverserSDR 06FDEA0703Line · failedSLOWING TO 250 KNTS FOR DESCENT, NOTICED AN INCREASED VIBRATION THAT FELT LIKE IT WAS ENGINE. FOUND T/R -Y- CHECK VALVE NR 1 ENGINE LOWER SUPPLY LINE BLOWN APART. REMOVED LINE AND ORDERED PARTS. UPON FURTHER INVESTIGATION ON WHY THE T/R V AIR TUBE CAME APARFeb 11, 2006 · N668FE · Airbus A300F4605R · Engine Thrust ReverserSDR 05FDEA03900Indicator · malfunctionedFL320, THE RT BRAKE PRESS GAUGE INCREASED O TO 2000 PSI. AFTER 12 MIN IT DECREASED TO 1500 PSI. AFT 30 MIN IT DECREASED TO 400 PSI. BRAKE A/S SELECTOR WAS IN THE NORMAL ON POS. ALL WHEEL BRAKES SHOWED REL ON ECAM. PARKING BRAKE WAS VERIFIED OFF. LATER INov 18, 2005 · N668FE · Airbus A300F4605R · Landing Gear Brake SystemSDR 05FDEA00319Windshield · failedFO'S WINDSHIELD SHATTERED. DECLARED EMERGENCY. NO OVERWEIGHT LANDING. MEM R CHECK RESISTANCE VALUES ON NEW WINDSHIELD AND ALL CHECK GOOD PER AIRBUS TSM 30-42-00. REMOVED AND REPLACED F/O'S_WINDSHIELD IN REFERENCE T TO A300 AMM 56-11-11-4. OPS CHECKED GOOFeb 26, 2005 · N668FE · Airbus A300B4605R · Flight Compartment WindowsSDR 04FDEA02674Throttle · obstructedRTO DUE TO LOW POWER NR 2, ENG NR 2 THROTTLE WOULD NOT ADVANCE PAST REF. POINT 30 AND N1 ADVANCED TO 93 PERCENT VS 108 PERCENT REQUIRED. RTO OCCURRED AT 90 KTS. ENT BY: 273927 RPT BY: 096714 SHGN 11SEP04 02:40 GDL U IN WORK, ENT BY: 273927 RPT BY: 27392Sep 10, 2004 · N668FE · Airbus A300F4605R · Power LeverSDR 02FDEA00771Fire Loop · out of positionON CLIMB OUT NR 1 FIRE WARN/BELL WARN LT RET'D THROTTLE AND WARN STOPPED. COMPLETED FIRE S/D CKLIST AND RTO TO MEM FOR LD. LT & BELL EXT WHEN THROTTLE RTO, BUT ACTIVATED WHEN THROTTLE ADVANCED. INSP FIRE LOOPS NR 1 ENG FOUND LOOP MAKING PHYSICAL CONTACT WITOct 27, 2002 · N668FE · Airbus A300F4605R · Fire DetectionSDR 00FDEA00873Bleed Valve · malfunctioned00-354 NR 2 HP BLEED VALVE ON ECAM, NR 1 HP ECAM NOT CLOSED WARNING. DUAL HP VLV FAULTS. ** S/D ** COMINGDec 13, 2000 · N668FE · Airbus A300F4605R · Compressor Bleed ValveSDR 99FDEA00316Sensor · failed99-195 - GEAR WOULD NOT RAISE WITH INTERLOCK WARNING SWITCH TO SYS 2, GEAR RAISED, LOST NR 1 PITCH TRIM, AUTO THROTTLES, AUTOPILOT, NR 1 PRESS REG. REMOVED AND REPLACED 64GB SENSOR, 32-00-00-4 AND OPS CK 32-00-00-5 AFS LAND TEST PASSED, 22-00-00-5.Aug 5, 1999 · N668FE · Airbus A300F4605R · Landing Gear Retraction/Extension SystemSDR 96FDEA01704Pilot Valve · malfunctionedON POWER APPLICATION, NR 1 REV PRESS LIGHT CAME ON AND THEN WENT OUT, ON THE ECAM AT APPROX 200-300 FT AGL WARNING CAME BACK ON. REMOVED AND REPLACED NR 1 THRUST REVERSER DIRECTIONAL PILOT VALVE. OPS CHECK GOOD.Dec 18, 1996 · N668FE · Airbus A300* · Engine Thrust Reverser
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