N664FE

Service difficulty reports · 307

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 = 'N664FE' 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 FDEA2019111522927Floorboard · delaminatedFLOORBOARD 261VF IS DELAMED FABRICATED NEW FLOORBOARD 261VF IAW FEDEX DWG SRZ-25-005 REV. R AND PART MARKED IAW GMM 07-0-1000 7.B.(2)&(6)Nov 12, 2019 · N664FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201911112919Door Frame · dentedAFT CARGO PIT DOOR FRAME 63A HAS DENT APPROXIMATELY BETWEEN STR 28 - STR 29R IN DOOR CUT OUT AREA REPAIRED DAMAGED AREA PER A300-600 SRM 53-17-17-201 FIG 201 SHEET 1Nov 11, 2019 · N664FE · Airbus A300F4605R · Fuselage Main, StructureSDR FDEA201911112920Seal Depressor · damagedAFT CARGO COMPARTMENT DOOR CUTOUT @ FR63A UPPER SEAL DEPRESSOR DAMAGED REMOVED DAMAGED UPPER SEAL DEPRESSOR AT FR 63A IAW A300-600 SRM 51-40-21. RECEIVED NEW SEAL DEPRESSOR P/N A5397822420051 PER A300-600 IPC 53-17-88-05 ITEM 010. INSTALLED NEW SEAL DNov 11, 2019 · N664FE · Airbus A300F4605R · Fuselage Main, StructureSDR FDEA2019110752867Floorboard · damagedPARTS RACK: MAIN WHEEL WELL FLOORBOARD PANEL 147AF MISSING EDGE FILLER REPLACED MISSING EDGE FILLER ON MAIN WHEEL WELL FLOORBOARD PANEL #147AF IAW SRZ-25-005 REV: R MAJOR REPAIR REMOVED DOTNov 5, 2019 · N664FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA2019110752855Angle · corrodedAFT CARGO PIT DOOR SEAL CHORD UPPER SURFACE HAS CORROSION IN SEVERAL AREAS REMOVED CORROSION IAW A300-600 SRM 51-74-10 AT CHORD ON FR63, ORIGINAL MAT 0.157 IAW SRM 53-17- 18 MA 18 MAT LOSS 0.015, REMAINING 0.142 IN LIMITS IAW A300 18 MAT LOSS 0.015, REMAININov 5, 2019 · N664FE · Airbus A300F4605R · Fuselage Miscellaneous StructureSDR FDEA201910242734Bracket · crackedAVIONICS COMPARTMENT FR10 @ RBL37 HAS CRACKED BRACKET REMOVED CRACKED BRACKET AT FR10 RBL37 IAW A300-600 SRM 51-40-21, RECEIVED NEW BRACKET P/N# A5361235620100. INSTALLED NEW BRACKET IAW A300 SRM 51-40-21Oct 24, 2019 · N664FE · Airbus A300F4605R · Fuselage Main, Attach FittingsSDR FDEA2019102422727Rib · gouged#1 ENGINE, INBOARD THRUST REVERSER, INNER SHELL, FORWARD RIB IS GOUGED/ CRACKED REMOVED EXISTING DOUBLER AND CLEANED RIB PER MRA CMM 78-32-02 REP 033. DAMAGE FOUND TO BE ON EXISTING DOUBLER. REPAIRED WITH NEW DOUBLER PER MRA CMM 78-32-02 REPAIR 033 02 ROct 22, 2019 · N664FE · Airbus A300F4605R · Engine Thrust ReverserSDR FDEA201905251162Floor Panel · delaminatedMAIN CABIN FLOOR PANEL 232CF IS CRUSHED ON TOP IN 2 PLACES. FABRICATED NEW FLOOR PANEL 232CF PER DWG SRZ-25-005 REV P.May 25, 2019 · N664FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201905251161Floor Panel · delaminatedMAIN CABIN FLOOR PANEL 232AH IS DELAMINATED ON BOTTOM SIDE. FABRICATED NEW FLOOR PANEL PER DWG SRZ-25-005 REV P.May 25, 2019 · N664FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201905251160Floor Panel · delaminatedMAIN CABIN FLOOR PANEL 232RG CORNER IS CRACKED AND BOTTOM SKIN HAS A PUNCTURE. FABRICATED NEW FLOOR PANEL PER DWG SRZ-25-005 REV P.May 25, 2019 · N664FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201905251159Floor Panel · delaminatedMAIN CABIN FLOOR PANEL 232KG DELAMINATED CORNER ON BOTTOM SIDE. FABRICATED NEW FLOOR PANEL 232KG PER DWG SRZ-25-005 REV P.May 25, 2019 · N664FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201905241154Floor Panel · crackedMAIN CABIN FLOOR PANEL 232NG IS BROKEN AT CENTER. FABRICATED NEW FLOOR PANEL 232NG PER DWG SRZ 25-005 REV P.May 24, 2019 · N664FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201905241153Floor Panel · brokenMAIN CABIN FLOOR PANEL 231WG HAS A PIECE BROKEN OFF THE END OF THE PANEL. FABRICATED NEW FLOOR PANEL PER 231WG PER SRZ 25-005.May 24, 2019 · N664FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201812283613Mount · corrodedNR 2 ENGINE FWD MOUNT , FORWARD INBOARD ATTA COMPLY WITH E..A. 6-5451-T0344330 REV NO. POS. P1 EA. T6-5451-T0344330. CORROSION REMOVAL OF OVER SIZE HOLE EA TO ADDRESS REPAIR. EXCEDED MAX OVER SIZE HOLE PER SRM.Dec 28, 2018 · N664FE · Airbus A300F4605R · Engine Mount SectionSDR FDEA201810092877Window · crackedF/O'S OUTER WINDSCREEN SHATTERED AT FL330. COMPLIED WITH QRH. COMPLIED WITH R&R OF F/O'S WINDOW PER AMM 56-11-11-04 UP TO STEP 2 (A) 12.Oct 9, 2018 · N664FE · Airbus A300F4605R · Flight Compartment WindowsSDR FDEA2018100522771O-Ring · missingPDIS 664 29-10 0858 02OCT18 OAK FACT U LOGPAGES:2943168 CRUISE AT FL 320, YELLOW HYD PUMP PRESSURE LOW DUE TO NO HYDRAULIC FLUID IN THE YELLOW SYSTEM, CONFIRMED ON GAUGES. SHGN 03OCT18 00:33 OAK U FOUND FLUID DRIPPING OUT OF RT GEAR WELL AT BLOCK IN. FOUND FLOct 2, 2018 · N664FE · Airbus A300F4605R · Hydraulic System, MainSDR FDEA201704071110Web · crackedAFT CARGO DOOR SUPPORT WEB HAS 2EA CRACKS LOCATED FWD AND AFT OF CARGO DOOR ACTUATOR ATTACH FITTING. REPAIRED 2EA CRACKED WEBS ON AFT CARGO DOOR UPPER AREA LT / RT SIDES OF ACTUATOR FITTING IAW EA 6-5230-T0332374 STEPS 1-13 DOORS - CARGO DOOR / HYD SYS - Apr 7, 2017 · N664FE · Airbus A300F4605R · Cargo/Baggage DoorsSDR FDEA201704051084Floor Panel · brokenMAIN CABIN FLOOR PANEL 252BF BROKEN. FABRICATED NEW FLOOR PANEL ON T17/1266511 IAW SRZ-25-005 CAT "A" MAJOR REPAIR.Apr 5, 2017 · N664FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201704051083Floor Panel · brokenMDCC 241DF FLOOR PANEL BROKEN. FABRICATED NEW FLOOR PANEL ON T17/1265489 IAW SRZ-25-005 CAT "A" MAJOR REPAIR.Apr 5, 2017 · N664FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201704051082Floor Panel · damagedMDCC 251QH FLOOR PANEL DAMAGED. FABRICATED NEW FLOOR PANEL ON T17/1265511 IAW SRZ-25-005 CAT "A" MAJOR REPAIR.Apr 5, 2017 · N664FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201704051081Floor Panel · brokenMDCC 231NG FLOOR PANEL BROKEN FABRICATED NEW FLOOR PANEL ON T17/1265490 IAW SRZ -25-005 CAT "A" MAJOR REPAIR.Apr 5, 2017 · N664FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201703301017Seat Track · corrodedMAIN DECK FROM FRAMES 25 AND 28, BETWEEN SEAT TRACKS -Y1959 AND -Y1456, SEAT TRACK ADAPTER BASE DECK PLATE, AND SEAT TRACK FLANGE HAVE CORROSION AND ALSO HAS ONE NUT PLATE DAMAGED. DECK PLATE REPLACED. SEAT TRACK AT -Y1456 FRAMES 26-28 WAS REPLACED IAW SRM 5Mar 30, 2017 · N664FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201703250991Floor Panel · tornCOURIER FLOOR PANEL 221GF UPPER SKIN TORN. FABRICATED A NEW FLOOR PANEL IAW DWG SRZ-25-005. MAJOR REPAIR.Mar 25, 2017 · N664FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201703250990Floor Panel · crackedCOURIER FLOOR PANEL 221PF IS CRACKED. FABRICATED A NEW FLOOR PANEL IAW DWG SRZ-25-005. MAJOR REPAIR.Mar 25, 2017 · N664FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201703230980Floor Panel · brokenMAIN CARGO FLOOR PANEL 252AH BROKEN. FABRICATED A NEW FLOOR PANEL IAW SRZ-25-005. MAJOR REPAIR.Mar 23, 2017 · N664FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201703230979Floor Panel · brokenMAIN CARGO FLOOR PANEL 251DH BROKEN. FABRICATED A NEW FLOOR PANEL IAW SRZ-25-005. MAJOR REPAIR.Mar 23, 2017 · N664FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201703230978Floor Panel · brokenMAIN CARGO FLOOR PANEL 252VH BROKEN. FABRICATED A NEW FLOOR PANEL IAW SRZ-25-005. MAJOR REPAIR.Mar 23, 2017 · N664FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201703230977Floor Panel · damagedMAIN CARGO FLOOR PANEL 242LH BROKEN. FABRICATED A NEW FLOOR PANEL IAW SRZ-25-005. MAJOR REPAIR.Mar 23, 2017 · N664FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201703230976Floor Panel · brokenMAIN CARGO FLOOR PANEL 241AJ BROKEN. FABRICATED A NEW FLOOR PANEL IAW SRZ-25-005. MAJOR REPAIR.Mar 23, 2017 · N664FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201703230975Floor Panel · brokenMAIN CARGO FLOOR PANEL 242VG BROKEN. FABRICATED A NEW FLOOR PANEL IAW SRZ-25-005. MAJOR REPAIR.Mar 23, 2017 · N664FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201703230974Floor Panel · brokenMAIN CARGO FLOOR PANEL 242UJ BROKEN. FABRICATED A NEW FLOOR PANEL IAW SRZ-25-005. MAJOR REPAIR.Mar 23, 2017 · N664FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201703230973Seat Track · gougedFWD MAIN DECK SEAT TRACK GOUGED Y0 FRAME 27. FOUND TO BE OUT OF LIMITS IAW SRM 53-10-16, FIG 101. REMOVED THE DAMAGE IAW SRM 51-40-21. FABRICATED A NEW SEAT TRACK. LOCATED, AND DRILLED IAW SRM 51-40-44, AND SRM 53-10-16 FIG 201. INSTALLED THE NEW SEAT TRACK Mar 23, 2017 · N664FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201605041450Brake · failedDURING CLIMBING, APPROX 16,000', RECEIVED ECAM WARNING ON HIGH BRAKE TEMP. LOWERED LG TO COOL BRAKES & RETURNED TO TAKEOFF AIRPORT. WHILE ACFT PARKED AT THE GATE, SUSPECT NR 4 MLG TIRE FUSE PLUG BLOWN. A BRAKE OVERHEAT INSPECTION IS REQUIRED IAW AMM 05-51-1May 4, 2016 · N664FE · Airbus A300F4605R · BrakeSDR FDEA201602110502Unknown · vibrationCLIMBING THRU FL 320, NOTICEABLE VIB BEGAN LEVELED AT 340, VIBS CONTINUED, SLOWED & EVENTUALLY DESCENDED BACK TO 320, VIBS CONTINUED. NO SECONDARY’S INDICATED, ENG VIBS NORMAL. NO OTHER INDICATIONS, NO FLIGHT CLT INDICATIONS. VIBS INCREASED SIGNIFICANTLY WFeb 11, 2016 · N664FE · Airbus A300F4605R · Flight Control SystemSDR FDEA201501290491Brake Sys · malfunctionedABORTED TAKEOFF ON RNWY 23L. IMMEDIATELY AFTER STARTING TAKEOFF ROLL, RT BRAKES ALL SEEMED TO BE BINDING & TEMPS ROSE, HIGHEST WENT TO 180C. TAXIED CLEAR OF RNWY & STOPPED. RECYCLED PARKING BRAKE WHICH WAS DEF OFF AT START OF TAKEOFF ROLL, BRAKES STILL BIJan 29, 2015 · N664FE · Airbus A300F4605R · Landing Gear Brake SystemSDR FDEA201412044057Floorbeam · corrodedBULK CARGO FLOORBEAM CORRODED AT FRAME 64. REMOVED CORROSION IAW SRM 51-74-10, FOUND OUT OF LIMITS IAW DWG A53974322. REPLACED THE FLOORBEAM IAW SRM 51-40-21, MAJOR REPAIR IAW GMM 6-2-100.Dec 4, 2014 · N664FE · Airbus A300F4605R · Fuselage Main, Floor BeamSDR FDEA201411203823Crossbeam · crackedMAIN DECK FRAME 64 CROSSBEAM FOUND CRACK BETWEEN -Y1456 & -Y1959.Nov 20, 2014 · N664FE · Airbus A300F4605R · Fuselage Miscellaneous StructureSDR FDEA201411183744Splice · crackedFUSELAGE FRAME 47 SPLICE FITTING BETWEEN STRINGER 24 & 26 RT THE FASTENER HOLE NR 10 JUST BELOW THE HOLE L FOUND CRACK SIGNAL. COMPLIED WITH EA 6-5310-T0314014 A PT1, TITLE: FUSELAGE - MAINFRAME - AD 2004- 20-14 - FASTENER HOLES CRACKED C/T FRAME 47 SPLICENov 18, 2014 · N664FE · Airbus A300F4605R · Fuselage Miscellaneous StructureSDR FDEA201411183743Splice · crackedFUSELAGE FRAME 47 SPLICE FITTING BETWEEN STRINGER 24 & 26 RT THE FASTENER HOLE NR 1 JUST BELOW THE HOLE I FOUND CRACK SIGNAL. COMPLIED WITH EA 6-5310-T0314014 A PT1, TITLE: FUSELAGE - MAINFRAME - AD 2004- 20-14 - FASTENER HOLES CRACKED C/T FRAME 47 SPLICE FINov 18, 2014 · N664FE · Airbus A300F4605R · Fuselage Miscellaneous StructureSDR FDEA201411143686Frame · crackedFRAME 40 TO CTR WING JOINT AT UPPER SKIN LEVEL TENSION BOLT JUNCTION, LT LOWER FASTENER HOLE FOUND CRACK SIGNAL. COMPLIED WITH EA 6-5710-T0313797 PT1, TITLE: WINGS - BASIC WING STRUCTURE - CRACK HOLES IN CENTER WING JOINT - FR40LH , REPAIRED THE FRAME 40 TONov 14, 2014 · N664FE · Airbus A300F4605R · Fuselage Main, FrameSDR FDEA201411143685Frame · crackedFRAME 40 TO CTR WING JOINT AT UPPER SKIN LEVEL TENSION BOLT JUNCTION, LT MIDDLE FASTENER HOLE FOUND CRACK SIGNAL. COMPLIED WITH EA 6-5710-T0313797 PT1, TITLE: WINGS - BASIC WING STRUCTURE - CRACK HOLES IN CENTER WING JOINT - FR40LT , REPAIRED THE FRAME 40 TO Nov 14, 2014 · N664FE · Airbus A300F4605R · Wing Main, Frame StructureSDR FDEA201411143673Seat Track · corrodedMAIN DECK FRAMES 45 - 50 Y1456 SEAT TRACK CORRODED. REPLACED THE SEAT TRACK IAW SRM 51-40-21 AND EA 6-5310-T0313462. MAJOR REPAIR IAW GMM6-2-100.Nov 14, 2014 · N664FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201411143683Crossbeam · crackedMAIN DECK FRAME 60 CROSSBEAM FOUND CRACK BETWEEN -Y1456 & -Y1959. REPAIRED THE MAIN DECK FR60 CROSSBEAM PER A300-600F SRM 53-10-15 FIG211, MAJOR REPAIR IAW GMM 6-2-100.Nov 14, 2014 · N664FE · Airbus A300F4605R · Fuselage Miscellaneous StructureSDR FDEA201411143682Seat Track · corrodedMAIN DECK FR46-FR47 -Y1959 SEAT TRACK CORRODED REMOVED THE CORROSION PER A300-600F SRM51-74-10, EXCEED LIMIT BY VISUAL INSPECTION, REPLACED THE CORRODED SEAT TRACK PER A300-600F SRM51-40-21 AND AIRBUS DWG A53832211204, MAJOR REPAIR IAW GMM 6-2-100Nov 14, 2014 · N664FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201411143681Seat Track · corrodedMAIN DECK FR40-FR41 Y0 SEAT TRACK CORRODED REMOVED THE CORROSION PER A300-600F SRM51-74-10, EXCEED LIMIT BY VISUAL INSPECTION, REPLACED THE CORRODED SEAT TRACK PER A300-600F SRM51-40-21 AND AIRBUS DWG A53832020204, MAJOR REPAIR IAW GMM 6-2-100Nov 14, 2014 · N664FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201411143680Seat Track · corrodedMAIN DECK FR43-FR44 Y1456 SEAT TRACK CORRODED REMOVED THE CORROSION PER A300-600F SRM51-74-10, EXCEED LIMIT BY VISUAL INSPECTION, REPLACED THE CORRODED SEAT TRACK PER A300-600F SRM51-40-21 AND AIRBUS DWG A53832020204, MAJOR REPAIR IAW FEDEX GMM 6-2-100Nov 14, 2014 · N664FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201411143684Crossbeam · crackedMAIN DECK FRAME 64 CROSSBEAM FOUND CRACK BETWEEN -Y953 & -Y1456.Nov 14, 2014 · N664FE · Airbus A300F4605R · Fuselage Miscellaneous StructureSDR FDEA201411133668Seat Track · crackedMAIN DECK FRAME 41 - 42 Y953 SEAT TRACK CORRODED. REPLACED THE SEAT TRACK IAW SRM 51-40-21 & DRAWING A53932020204, MAJOR REPAIR IAW GMM 6-2-100Nov 13, 2014 · N664FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201408282346Transmitter · malfunctionedLOST GREEN HYD QTY AT CRUISE NOTIFIED BY ECAM, CONFIRMED ON OVERHEAD PANEL. COMPLIED WITH QRH. TURNED PUMPS OFF AT 1614Z LANDED AT 1713Z. R&R GREEN RESERVOIR HYD QTY TRANSMITTER. LEAK & OPERATIONS CHECKED GOOD IAW AMM.Aug 28, 2014 · N664FE · Airbus A300F4605R · Hydraulic Quantity SensorSDR FDEA201311272884Engine · failedPDIS 664 79-310005832 27NOV13 IND OPEN U LOG PAGES 02343904. ENG ADVISORY FOR NR 2 ENG OIL QTY ZERO & FLUCTUATING OIL PRESS ON ECAM & ENG INSTRUMENTS. ADVISORY OCCURRED AT FL 370 EGT REMAINED NORMAL. OIL QTY & PRESS RETURNED TO NORMAL ON FINAL APPROACH. WNov 27, 2013 · N664FE · Airbus A300F4605R · Engine (Turbine/Turboprop)
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