N667FE

Service difficulty reports · 237

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 = 'N667FE' 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 FDEA202306251403Slat · gougedLH SLAT #2 LOWER SURFACE GOUGE AT T/E -12", I/B CLOSING RIB PLUS 8.5" ACCOMPLISHED THE DOUBLER REPAIR I.A.W FEDEX EA NO:T6-5750-T0375356 P1, SEQ NO:1147, TITLE:WING-FLIGHT SURFACES-LH #2 SLAT-GOUGE DAMAGE ON LOWER SKIN AT RIB2A, APPROX.12-INCHES FWD OF TRAJun 25, 2023 · N667FE · Airbus A300* · Leading Edge DevicesSDR FDEA202306251274Spoiler · damagedL4 SPLR I/B HINGE ARM UPPER FACE FAIRING BROKEN. REMOVED L4 SPLR, REPLACED THE COVER, INSTALLED L4 SPLR, ADJUSTED AND PFMED TEST OF L4 SPLR WITH NORMAL RESULT I.A.W A300-600 AMM 27-61-51-04 AND SRM 51-72-00-001 PAGE 2Jun 25, 2023 · N667FE · Airbus A300* · SpoilersSDR FDEA202306241199Bracket · crackedAFT CGO COMP'T FWD BULKHEAD RH SUPPORT BRACKET CRACKED AT Y-1959,Z-751 FR54 POSITION REMOVED CRACKED BRACKET AND INSTALLED WITH NEW ONE.I.A.W A300-600F SRM 51-72-10-001. PAGE,2Jun 24, 2023 · N667FE · Airbus A300* · Fuselage Miscellaneous StructureSDR FDEA202306241140Bracket · unknownAFT CGO COMP'T FWD BULKHEAD LH SUPPORT BRACKET CRACK AT Y 1959,Z-751 FR54 POSITION REMOVED CRACK BRACKET AND INSTALLED WITH NEW ONE.I.A.W A300-600F SRM 51-72-10-001. PAGE2Jun 24, 2023 · N667FE · Airbus A300* · Fuselage Main, StructureSDR FDEA202306231181Unknown · crackedAVIONICS COMP'T ACCESS DOOR SUPPORT STRUCTURE STOP OMEGA CRACK AT CENTER LINE Z- 1497 POSITION REPLACED THE NEW OMEGA. I.A.W A300-600F SRM 51-72-10-001, PAGE.2Jun 23, 2023 · N667FE · Airbus A300* · Service DoorsSDR FDEA202306231135Angle · crackedAVIONICS COMP'T BELOW COCKPIT FLOOR PICK UP ANGLE CRACK AT Y403,FR10 POSITION. REPLACED THE ANGLE BY NEW ONE WITH RIVETS I.A.W A300-600F SRM 51-72-10-001 PAGE 2.Jun 23, 2023 · N667FE · Airbus A300* · Fuselage Miscellaneous StructureSDR FDEA202306221229Panel · damagedMAINTENANCE PLATFORM SOFT AT TRIM TANK FR87-FR91. FABRICATED THE PLATFORM PANEL I.A.W FEDEX DRAWING SRZ-25-005 "MAJOR REPAIR"Jun 22, 2023 · N667FE · Airbus A300* · Fuselage Miscellaneous StructureSDR FDEA202212062877Warning Message · intermittentON SHORT FINAL, WITH 3 GREEN ON SYS 1, RECEIVED A TOO LOW MLG AT 300 FT. SWITCHED TO SYS 2, SAME WARNING. GO AROUND. NO ECAM, NO QRH RELIEF. EMERGENCY DECLARED. NLG OVRHD PANEL IND INTERMIT. SWITCHED DET SYS, NO HELP. PERFORMED EGPWS LEVEL 1 & 2 SELF TEDec 6, 2022 · N667FE · Airbus A300F4605R · Landing Gear Position and WarningSDR FDEA202208302110Windshield · failedREF 30-40-3905 CAPT WINDSHIELD OUTSIDE PANE SHATTERED. NEEDS REPLACED. REF AMM 56-11-11-04 COMPLETED INSTALLATION OF CAPTAINS WINSHIELD. OPS CHECK GOOD REF AMM 30-42-00-05. AIRCRAFT GOOD FOR SERVICE.Aug 30, 2022 · N667FE · Airbus A300F4605R · Flight Compartment WindowsSDR FDEA202208302109Windshield · failedCA WINDSHIELD HEAT FAULT AT FL350. CRACK APPEARED IN WINDSHIELD FROM TOP LEFT TO BOTTOM RIGHT. THEN WINDSHIELD OUTSIDE PANE SHATTERED. QRH COMPLIED WITH AND PRECAUTIONARY SPEED REDUCTION AND ALTITUDE REDUCTION EXECUTED. WINDOW PAYNE HELD FOR REMAINDER OFAug 30, 2022 · N667FE · Airbus A300F4605R · Flight Compartment WindowsSDR FDEA202102010259Hinge Arm · delaminatedLEFT WING NR 5 SPOILER CENTER IB HINGE ARM OB SURFACE AND CENTER OB HINGE ARM OB SURFACE FOUND DELAMINATION, SIZE: 20MM*10MM D: 1.6MM, 25MM*15MM D:1.33MM. COMPLIED WITH EA 6-5750-T0359226 P1,TITLE: WING - FLIGHT SURFACE - LT NR 5 SPOILER CENTER HINGE, CENTER Feb 1, 2021 · N667FE · Airbus A300F4605R · SpoilersSDR FDEA202102010258Spoiler · delaminatedLEFT WING NR 5 SPOILER CENTER IB HINGE ARM OB SURFACE AND CENTER OB HINGE ARM OB SURFACE FOUND DELAMINATION, SIZE: 20MM*10MM D: 1.6MM, 25MM*15MM D:1.33MM. COMPLIED WITH EA 6-5750-T0359226 P1, TITLE: WING - FLIGHT SURFACES - LT 5 SPOILER CENTER HINGE ARMS OUTSFeb 1, 2021 · N667FE · Airbus A300F4605R · SpoilersSDR FDEA202008041766Bolt · failedMDIS 667 72-30 2005 04AUG20 MEM FACT U REF B CHECK WORK SEQ #163 VBV UNISON RING BOLTS AT POSITION 7,8,9 OCLCOCK, TORQUE STRIPE HAS BEEN COMPROMISED SHGN 04AUG20 07:13 MEM U TORQUE CHECK CHECKED GOOD ON BOLTS #7 AND# 9 BOLTS NEED TORQUE STAug 4, 2020 · N667FE · Airbus A300* · Turbine Engine Compressor SectionSDR FDEA2020080541766Bolt · failedVBV UNISON RING BOLTS AT POSITION 7,8,9 OCLCOCK, TORQUE STRIPE HAS BEEN COMPROMISED SHGN 04AUG20 07:13 TORQUE CHECKED GOOD ON BOLTS #7 AND# 9 BOLTS NEED TORQUE STRIPE. BOLT # 8 MOVED DURING TORQUE CHECK. #8 BOLT REQUIRES REMOVAL AND NEW BOLT INSTALLED.Aug 4, 2020 · N667FE · Airbus A300F4605R · Turbine Engine Compressor SectionSDR FDEA202003050494Terminal · dirtyPDIS 667 52-10 1650 05MAR20 RSW OPEN U LOGPAGES:3194614 RIGHT CABIN DOOR SLIDE WILL NOT ARM ASM 52-73-00 SH 1 FOUND HIGH RESISTANCE ON GROUND PINS B,T & U. CLEANED GROUND SURFACE AND TERMINALS Mar 5, 2020 · N667FE · Airbus A300F4605R · Door Warning SystemSDR FDEA2020012180166Idg · inoperativeNR 2 GENERATOR AND AC BUSS NR 2 FAILED. COMPLIED WITH ECAM AND QRH. ON ARRIVAL; DEPARTING CREW NOTIFIED MTC OF ELEC PROBLEM, GROUND CREW UNABLE TO OPEN CARGO DOORS DUE TO NO EXTERNAL POWER. FOUND FAULT MESSAGE WHEN DOING BITE CHECK OF GCU 2 - DP TRIP.Jan 18, 2020 · N667FE · Airbus A300F4605R · AC Generator-AlternatorSDR FDEA201902200460Power Unit · faultyON CLOSE UP - R1 DOOR SLIDE INDICATION NOT SHOWING ON EXAM WHEN DOOR IS ARMED. DOOR ESCAPE SLIDE ARMING SYSTEM IS TO BE VERIFIED AS FULLY ARMED PRIOR TO EACH DEPARTURE. R1 SLIDE INDICATION C/7175127. REMOVED AND REPLACED AUTONOMOUS STANDBY POWER UNIT (70WN) IFeb 20, 2019 · N667FE · Airbus A300F4605R · Door Warning SystemSDR FDEA2019021170310Seat Track · wornMDIS 667 53-21 0630 07FEB19 PHL FACT U REF WRI 25-50/0629 MAIN DECK RESTRAINT C1488, FOUND LOBES WORN IN SHORT LATERAL SEAT TRACK SECTION APPROX 65" LEFT OF C/L AND STA. 1488 FRAME 57.2 FACT 07FEB19 20:51 MEM Feb 7, 2019 · N667FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201811233356Pressure Switch · inoperativeNUMBER 1 ENGINE FUEL CLOG LIGHT WAS OUT AT 70% N1 PART 23. C/W MEL PROCEDURES R&R ENGINE FUEL FILTER IAW AMM 73-12-02-04 ONCE EACH FLIGHT DAY. REPLACED NR 1 ENG DIFFERENTIAL PRESSURE SWITCH, MFR P/N 21SN04-333, S/N CFL1014B AS REQ. REF AMM 73-34-11 AND TSM 73-Nov 23, 2018 · N667FE · Airbus A300F4605R · Fuel Pressure SensorSDR FDEA201810313061Dampener · malfunctionedLANDING GEAR WOULD NOT RETRACT. ECAMS: LDG GEAR RETRACTION INOP. LANDING GEAR RETRACTION SYSTEM - INOP. MAX SPEED 255 KIAS / 0.65 M. DO NOT USE FMS PROFILE MODE. CHECKED PROX BOX AND FOUND NO FAULTS LOGGED. FOUND DPI ON RIGHT BOGGIE PITCH DAMPER POPPEDOct 31, 2018 · N667FE · Airbus A300F4605R · Landing Gear Retraction/Extension SystemSDR FDEA2018082102133Fairing · damagedRIGHT WING FLAP FAIRING 632BB, AFT INNER SURFACE HAD COMPOSITE CHAFED. A SECTION WAS MISSING. BONDED AND REPAIRED THE RT WING FLAP FAIRING IAW SRM 57-20-35, AND EA T 6-5710-T0341633. MAJOR REPAIR.Aug 20, 2018 · N667FE · Airbus A300F4605R · Trailing Edge FlapsSDR FDEA2018082182123Floor Panel · crackedMAIN CARGO FLOOR PANEL 242RJ WAS CRACKED. FABRICATED A NEW FLOOR PANEL IAW SRZ 25-005. CLASSIFIED AS CAT A REPAIR. INSTALLED ON W/C 240- FL- FIT.Aug 18, 2018 · N667FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA2018082182122Floor Panel · crackedMAIN CARGO FLOOR PANEL 241MJ WAS CRACKED. FABRICATED A NEW FLOOR PANEL IAW SRZ 25-005. CLASSIFIED AS A CAT A MAJOR REPAIR.Aug 18, 2018 · N667FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA2018082182121Floor Panel · puncturedMAIN DECK FLOOR PANEL 241AJ WAS PUNCTURED. FABRICATED A NEW FLOOR PANEL IAW SRZ 25-005. CLASSIFIED AS A CAT A MAJOR REPAIR.Aug 18, 2018 · N667FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA2018082182120Floor Panel · crackedAFT CARGO FLOOR PANEL 251YG HAD A CRACK. FABRICATED A NEW FLOOR PANEL IAW SRZ 25-005. CLASSIFIED AS CAT A REPAIR.Aug 18, 2018 · N667FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA2018082182087Floor Panel · damagedFWD CARGO FLOOR PANEL 132SG HAD EDGE DAMAGE. FABRICATED A NEW FLOOR PANEL IAW SRZ 25-005. CLASSIFED AS A CAT A MAJOR REPAIR.Aug 18, 2018 · N667FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA2018082182083Floor Panel · delaminatedFWD CARGO FLOOR PANEL 132RG HAD EDGE DAMAGE. FABRICATED A NEW FLOOR PANEL IAW SRZ 25-005. CLASSIFED AS AN -A- MAJOR REPAIR.Aug 18, 2018 · N667FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA2018082182082Floor Panel · delaminatedFWD CARGO FLOOR PANEL 132PG HAD EDGE DAMAGE. FABRICATED A NEW FLOOR PANEL IAW SRZ 25-005. CLASSIFED AS AN -A- MAJOR REPAIR.Aug 18, 2018 · N667FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA2018082182081Floor Panel · delaminatedFWD CARGO FLOOR PANEL 132MG HAD EDGE DAMAGE. FABRICATED A NEW FLOOR PANEL IAW SRZ 25-005. CLASSIFED AS AN -A- MAJOR REPAIR.Aug 18, 2018 · N667FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201808212076Floor Panel · delaminatedFWD CARGO FLOOR PANEL 131KG EDGE WAS DAMAGED. FABRICATED A NEW FLOOR PANEL IAW SRZ 25-005. CLASSIFED AS AN -A- MAJOR REPAIR.Aug 18, 2018 · N667FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201808182119Floor Panel · damagedAFT CARGO FLOOR PANEL 152VF EDGE DAMAGE. FABRICATED FLOOR PANEL 152VF ON VTMAE TRAVLER T18/1358266 PER SRZ 25-005. CAT A MAJOR REPAIR.Aug 18, 2018 · N667FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA2018082182118Floor Panel · damagedAFT CARGO FLOOR PANEL 152UF EDGE DAMAGE. FABRICATED FLOOR PANEL IAW SRZ 25-005. CAT A MAJOR REPAIR.Aug 18, 2018 · N667FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA2018082182117Floor Panel · damagedAFT CARGO FLOOR PANEL 152MF HAD EDGE DAMAGE. FABRICATED A NEW FLOOR PANEL IAW SRZ 25-005. CAT A MAJOR REPAIR.Aug 18, 2018 · N667FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201808182116Floor Panel · damagedAFT CARGO FLOOR PANEL 151UF HAD EDGE DAMAGE. FABRICATED A NEW FLOOR PANEL IAW SRZ 25-005. CAT A MAJOR REPAIR.Aug 18, 2018 · N667FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA2018082182115Floor Panel · damagedAFT CARGO FLOOR PANEL 152XF HAD EDGE DAMAGE. FABRICATED A NEW FLOOR PANEL IAW SRZ 25-005. CAT A MAJOR REPAIR.Aug 18, 2018 · N667FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA2018082182114Floor Panel · crackedMAIN CARGO FLOOR PANEL 241QJ WAS CRACKED. FABRICATED A NEW FLOOR PANEL IAW SRZ-25-005. CLASSIFIED AS A CAT A MAJOR REPAIR.Aug 18, 2018 · N667FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA2018082182113Floor Panel · crackedMAIN CARGO FLOOR PANEL 241BF WAS CRACKED. FABRICATED A NEW FLOOR PANEL 241BF IAW SRZ-25-005. CLASSIFIED AS A CAT A MAJOR REPAIR.Aug 18, 2018 · N667FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA2018082182112Floor Panel · crackedMAIN CARGO FLOOR PANEL 241BF WAS CRACKED. FABRICATED A NEW FLOOR PANEL 241BF IAW SRZ-25-005. CLASSIFIED AS A CAT A MAJOR REPAIR.Aug 18, 2018 · N667FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA2018082182111Floor Panel · crackedMAIN CARGO FLOOR PANEL 252VH HAD A CRACK, FABRICATED A NEW FLOOR PANEL IAW SRZ-25-005. CLASSIFIED AS CAT A MAJOR REPAIR.Aug 18, 2018 · N667FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA2018082182110Skin · crackedRT CENTER FLAP, RIB 11 HAD TWO CRACKS, AT FIRST AND SECOND STRINGER FWD OF THE REAR SPAR. REPAIRED THE FLAP IAW SRM 57-50-00, FIG 201, AND FIG 205. MAJOR REPAIR.Aug 18, 2018 · N667FE · Airbus A300F4605R · Trailing Edge FlapsSDR FDEA2018082182109Floor Panel · crackedMAIN CARGO FLOOR PANEL 252UH HAD A CRACK. FABRICATED A NEW FLOOR PANEL IAW SRZ-25-005. CLASSIFIED AS A CAT A MAJOR REPAIR.Aug 18, 2018 · N667FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA2018082182108Floor Panel · crackedMAIN CARGO FLOOR PANEL 252VF HAD A CRACK. FABRICATED A NEW FLOOR PANEL IAW SRZ-25-005. CLASSIFIED AS A CAT A MAJOR REPAIR.Aug 18, 2018 · N667FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA2018082182107Floor Panel · delaminatedAFT CARGO FLOOR PANEL 151QF WAS DELAMINATED. FABRICATED A NEW FLOOR PANEL IAW SRZ-25-005. CAT A MAJOR REPAIR.Aug 18, 2018 · N667FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA2018082182105Floor Panel · crackedAFT CARGO FLOOR PANEL 151SF WAS CRACKED. FABRICATED A NEW FLOOR PANEL IAW SRZ-25-005. CAT A MAJOR REPAIR.Aug 18, 2018 · N667FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA2018082182104Floor Panel · crackedAFT CARGO FLOOR PANEL 151TF WAS CRACKED. FABRICATED A FLOOR PANEL IAW SRZ-25-005. CAT A MAJOR REPAIR.Aug 18, 2018 · N667FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA2018082182103Floor Panel · crackedAFT CARGO FLOOR PANEL 152SF WAS CRACKED. FABRICATED A NEW FLOOR PANEL IAW SRZ 25-005. CAT A MAJOR REPAIR.Aug 18, 2018 · N667FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA2018082182096Floor Panel · delaminatedAFT CARGO FLOOR PANEL 152WF WAS DELAMINATED. FABRICATED A NEW FLOOR PANEL IAW SRZ 25-005. CLASSIFED AS A CAT A MAJOR REPAIR.Aug 18, 2018 · N667FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA2018082182095Floor Panel · crackedAFT CARGO FLOOR PANEL 151RF WAS CRACKED. FABRICATED A NEW FLOOR PANEL IAW SRZ 25-005. CLASSIFED AS A CAT A MAJOR REPAIR.Aug 18, 2018 · N667FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA2018082182094Floor Panel · crackedAFT CARGO FLOOR PANEL 151PF WAS CRACKED. FABRICATED A NEW FLOOR PANEL IAW SRZ 25-005. CLASSIFED AS A CAT A MAJOR REPAIR.Aug 18, 2018 · N667FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA2018082182093Floor Panel · crackedAFT CARGO FLOOR PANEL 151WF WAS CRACKED. FABRICATED A NEW FLOOR PANEL IAW SRZ 25-005. CLASSIFED AS A CAT A MAJOR REPAIR.Aug 18, 2018 · N667FE · Airbus A300F4605R · Fuselage Floor Panel
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