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.
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
Run it at the DuckDB prompt, or in any tool that reads Parquet over HTTPS. More ways to query the release are on Use the data.
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".SDR FDEA201103171043Floor Panel · damagedMAIN CABIN COMPARTMENT FLOOR PANEL 251 BH IS DAMAGED. FABRICATED NEW FLOOR PANEL 251 BH IAW DWG SRZ 25-005, REV "H".SDR FDEA201103171042Floor Panel · damagedMAIN CABIN COMPARTMENT FLOOR PANEL 251 QH IS DAMAGED. FABRICATED NEW FLOOR PANEL 251 QH IAW DWG SRZ 25-005, REV "H".SDR FDEA201103171041Floor Panel · damagedMAIN CABIN COMPARTMENT FLOOR PANEL 241 AJ IS DAMAGED. FABRICATED NEW FLOOR PANEL 241 AJ IAW DWG SRZ 25-005, REV "H".SDR FDEA201103171040Floor Panel · damagedMAIN CABIN COMPARTMENT FLOOR PANEL 242 ZJ IS DAMAGED. FABRICATED NEW FLOOR PANEL 242 ZJ IAW DWG SRZ 25-005, REV "H".SDR FDEA201103171039Floor Panel · damagedMAIN CABIN COMPARTMENT FLOOR PANEL 232 YG IS DAMAGED. FABRICATED NEW FLOOR PANEL 232 YG IAW DWG SRZ 25-005, REV "H".SDR FDEA201103171038Floor Panel · damagedMAIN CABIN COMPARTMENT FLOOR PANEL 232 TG IS DAMAGED. FABRICATED NEW FLOOR PANEL 232 TG IAW DWG SRZ 25-005, REV "H".SDR FDEA201103171037Floor Panel · damagedMAIN CABIN COMPARTMENT FLOOR PANEL 232 NG IS DAMAGED. FABRICATED NEW FLOOR PANEL 232 NG IAW DWG SRZ 25-005, REV "H".SDR FDEA201103171036Floor Panel · damagedMAIN CABIN COMPARTMENT FLOOR PANEL 232 HG IS DAMAGED. FABRICATED NEW FLOOR PANEL 232 HG IAW DWG SRZ 25-005, REV "H".SDR FDEA201103171035Floor Panel · damagedMAIN CABIN COMPARTMENT FLOOR PANEL 231 VG IS DAMAGED. FABRICATED NEW FLOOR PANEL 231 VG IAW DWG SRZ 25-005, REV "H".SDR FDEA201103171034Floor Panel · damagedMAIN CABIN COMPARTMENT FLOOR PANEL 231 QG IS DAMAGED. FABRICATED NEW FLOOR PANEL 231 QG IAW DWG SRZ 25-005, REV "H".SDR FDEA201103171033Floor Panel · damagedMAIN CABIN COMPARTMENT FLOOR PANEL 231 EF IS DAMAGED. FABRICATED NEW FLOOR PANEL 231 EF IAW DWG SRZ 25-005, REV "H".SDR 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. LOSDR FDEA201103150975Frame · crackedFWD CARGO COMPARTMENT OVERHEAD FLOORBEAM; FWD SIDE OF FRAME 30 & LBL 27 IS CRACKED.SDR 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 REPLACESDR 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 SDR 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 LSDR 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).SDR 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. SDR 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 OSDR 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 SDR 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 SDR 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 3,400SDR 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 STESDR 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 RETSDR 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.SDR 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.SDR 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.SDR 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.SDR 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.SDR 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.SDR 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.SDR 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.SDR 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.SDR 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.SDR 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 HELPSDR 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 STILSDR 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 ISDR 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 POSSDR 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 PUMPSDR 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.SDR 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 INVESTIGATIOSDR 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 APARSDR 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 ISDR 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 GOOSDR 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: 27392SDR 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 WITSDR 00FDEA00873Bleed Valve · malfunctioned00-354 NR 2 HP BLEED VALVE ON ECAM, NR 1 HP ECAM NOT CLOSED WARNING. DUAL HP VLV FAULTS. ** S/D ** COMINGSDR 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.SDR 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.
Back to N668FE