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 FDEA2018082182092Floor Panel · crackedFWD CARGO FLOOR PANEL 151VF 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 FDEA2018082182091Floor Panel · crackedAFT CARGO FLOOR PANEL 152TF 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 FDEA2018082182090Floor Panel · crackedAFT CARGO FLOOR PANEL 152QF 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 FDEA2018082182089Floor Panel · crackedAFT CARGO FLOOR PANEL 152PF 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 FDEA2018082182088Floor Panel · crackedAFT CARGO FLOOR PANEL 151MF 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 FDEA2018082182086Floor Panel · damagedFWD CARGO FLOOR PANEL 132QC HAD EDGE DAMAGE. FABRICATED A FLOOR PANEL IAW SRZ 25-005. CLASSIFED AS A CAT A MAJOR REPAIR.Aug 18, 2018 · N667FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA2018082182085Floor Panel · damagedFWD CARGO FLOOR PANEL 132NG 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 FDEA2018082182084Floor Panel · delaminatedFWD CARGO FLOOR PANEL132LG 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 FDEA2018082182080Floor Panel · delaminatedFWD CARGO FLOOR PANEL 132KG 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 FDEA2018082182079Floor Panel · delaminatedFWD CARGO FLOOR PANEL 131RG 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 FDEA201808182078Floor Panel · delaminatedFWD CARGO FLOOR PANEL 131PG 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 FDEA20180821077Floor Panel · delaminatedFWD CARGO FLOOR PANEL 131MG 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 FDEA201808212075Floor Panel · delaminatedFWD CARGO FLOOR PANEL 131SG WAS CRUSHED ON THE EDGE. FABRICATED A NEW FLOOR PANEL IAW SRZ 25-005. CLASSIFED AS AN -A- MAJOR REPAIR.Aug 18, 2018 · N667FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201808212074Floor Panel · delaminatedFWD CARGO FLOOR PANEL 131QG 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 FDEA201808212073Floor Panel · delaminatedFWD CARGO FLOOR PANEL 131NG 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 FDEA201808212072Floor Panel · delaminatedFWD CARGO FLOOR PANEL 131LG, 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 FDEA2018081752045Floor Panel · crackedMAIN CARGO FLOOR PANEL 242TH WAS CRACKED. FABRICATED A NEW FLOOR PANEL IAW SRZ-25-005. MAJOR REPAIR. INSTALLED ON WORK CARD 240-FL-FIT.Aug 15, 2018 · N667FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA2018081752044Floor Panel · crackedMAIN CARGO FLOOR PANEL 251XG WAS CRACKED. FABRICATED A NEW FLOOR PANEL IAW SRZ-25-005. MAJOR REPAIR. INSTALLED ON WORK CARD 250-FL-FIT.Aug 15, 2018 · N667FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA2018081752043Floor Panel · crackedMAIN CARGO FLOOR PANEL 232TG WAS MISSING AN INSERT AND CRACKED. FABRICATED A NEW FLOOR PANEL IAW SRZ-25-005. MAJOR REPAIR. INSTALLED ON WORK CARD E6-5321-E0339394 PT6.Aug 15, 2018 · N667FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA2018081752042Floor Panel · crackedMAIN CARGO FLOOR PANEL 252GF WAS CRACKED. FABRICATED A NEW FLOOR PANEL IAW SRZ-25-005. MAJOR REPAIR. INSTALLED ON WORK CARD 250-FL-FIT.Aug 15, 2018 · N667FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201808152041Floor Panel · crackedMAIN CARGO FLOOR PANEL 252NH WAS CRACKED. FABRICATED A NEW FLOOR PANEL IAW SRZ-25-005. MAJOR REPAIR. INSTALLED ON WORK CARD 250-FL-FIT.Aug 15, 2018 · N667FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA2018081752040Floor Panel · crackedMAIN CARGO FLOOR PANEL 252DF WAS CRACKED. FABRICATED A NEW FLOOR PANEL IAW SRZ-25-005. MAJOR REPAIR. INSTALLED IAW WC 250-FL-FIT.Aug 15, 2018 · N667FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201808152039Floor Panel · crackedMAIN CARGO FLOOR PANEL 252HH WAS CRACKED. FABRICATED A NEW FLOOR PANEL IAW SRZ-25-005. MAJOR REPAIR. INSTALLED ON WORK CARD 250-FL-FIT.Aug 15, 2018 · N667FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA2018081752038Floor Panel · crackedMAIN CARGO FLOOR PANEL 252PH WAS CRACKED. FABRICATED A NEW FLOOR PANEL IAW SRZ-25-005. CLASSIFIED AS A CAT A MAJOR REPAIR.Aug 15, 2018 · N667FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201808142025Floor Panel · delaminatedCOURIER FLOOR PANEL 221QF WAS DELAMINATED. FABRICATED A NEW FLOOR PANEL IAW DWG SRZ-25-005. MAJOR REPAIR.Aug 14, 2018 · N667FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201808142024Floor Panel · delaminatedCOURIER FLOOR PANEL 221GF DELAMINATED. FABRICATED A NEW FLOOR PANEL IAW DWG SRZ-25-005. MAJOR REPAIR.Aug 14, 2018 · N667FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201808142023Floor Panel · delaminatedCOURIER FLOOR PANEL 222QF WAS DELAMINATED. FABRICATED A NEW FLOOR PANEL IAW DWG SRZ-25-005. MAJOR REPAIR.Aug 14, 2018 · N667FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201808142022Floor Panel · delaminatedCOURIER FLOOR PANEL 221LF WAS DELAMINATED. FABRICATED A NEW FLOOR PANEL IAW DWG SRZ-25-005. MAJOR REPAIR.Aug 14, 2018 · N667FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201808142021Floor Panel · delaminatedCOURIER FLOOR PANEL 221HF WAS DELAMINATED. FABRICATED A NEW FLOOR PANEL IAW DWG SRZ-25-005. MAJOR REPAIR.Aug 14, 2018 · N667FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA2018082302001Floor Panel · crackedMAIN CARGO FLOOR PANEL 241JF WAS CRACKED. FABRICATED A NEW FLOOR PANEL IAW DWG SRZ-25-005, REV M. MAJOR REPAIR.Aug 10, 2018 · N667FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA2018121891977Seat Track · corrodedMAIN DECK COMPARTMENT FRAME 41-44, SEAT TRACK Y0 HAS CORROSION AS MAKED 7 PLACES. SEAT TRACK FOUND TO BE CORRODED OUT OF LIMITS IAW SRM 53-10-16 FIG 103. TRACK REMOVED AND REPLACED IAW SRM 51-40-21 FR41-44 MAJOR REPAIRAug 9, 2018 · N667FE · Airbus A300F4605R · Fuselage Structure (General)SDR FDEA2018081491968Floor Panel · crackedMAIN CARGO FLOOR PANEL 241DF HAD A BROKEN INSERT, AND CRACKED. FABRICATED A NEW FLOOR PANEL IAW DWG SRZ-25-005 REV M. MAJOR REPAIR.Aug 9, 2018 · N667FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA2018080761926Doubler · damagedDAMAGE FOUND ON THE DOUBLER AT THE FWD CARDO DOOR CUTOUT, FRAME 20 LOWER SECTION. REMOVED AND REPLACED THE DOUBLER IAW SRM 51-40-21, DRAWING SR30-53-001, SRM 51-40-21, AND SRM 51-23-00. MAJOR REPAIR.Aug 6, 2018 · N667FE · Airbus A300F4605R · Fuselage Main, Plate/SkinSDR FDEA2018061281431Window · crackedON DEPARTURE, DURING CLIMB OUT AT 3500FT CAPTIANS SLIDING WINDOW INSIDE SURFACE CRACKED. ENTIRE WINDOW SPIDER WEBBED. REPLACED LEFT HAND (CAPTAINS) SLIDING WINDOW PER AMM 56-12-11-04. CKS OK FOR SVC.Jun 8, 2018 · N667FE · Airbus A300F4605R · Flight Compartment WindowsSDR FDEA201712033331Outflow Valve · failedPDIS 667 21-30 9291 03DEC17 MEM OPEN U LOGPAGES:2686339 DURING CLIMBOUT AIRCRAFT FAILED TO PRESSURIZE W/ EITHER AUTO PRESSURE CONTROLLER. LEVELED OFF AT 10,000, CONSULTED QRH, CHECK APU BLEED SWITCH, DOOR PAGE, AND PRESSURE OF PACKS, ALL OKADec 3, 2017 · N667FE · Airbus A300F4605R · Pressure Regulator/Outflow ValveSDR FDEA201710132937Autothrottle Sys · malfunctionedDURING TAKE OFF, OVERHEAD ATS LEVER POPPED OFF TWICE. WOULD NOT RESET. ABORTED TAKEOFF AND RAN QRH, SECOND ATTEMP SUCCESFUL. PERFORMED AN ADJUSTMENT AND TEST OF AUTOTHROTTLE IAW AMM 22-30-00-05-01, NO DEFECTS NOTED. PERFORMED AFS - LAND TESTS IAW AMM 22-4Oct 13, 2017 · N667FE · Airbus A300F4605R · Auto Throttle SystemSDR FDEA201706131630Slide · out of positionR1 DOOR WILL NOT ARM. REPOSITIONED SLIDE MATERIAL AT GIRT BAR, ALL SYSTEMS OPERATED NORMALY IAW AMM 52-10-00-03-02, AND AMM 52-10-00-00-02 ACFT OK FOR CONTINUED SERVICE.Jun 13, 2017 · N667FE · Airbus A300F4605R · Escape SlideSDR FDEA201702100506Idg · leakingLOW SPEED (75KTS) REJECT DUE TO A NR 2 IDG FAULT, FOLLOWED BY A NR 2 GENERATOR FAULT ON ECAM. RECONNECTED NR 2 IDG. FOUND FIREWALL CONNECTOR VC4962P LOOSE. TIGHTED IAW WDM 24-11-02. RAN ENGINE IAW JRH. VOLTS/FREQS GOOD UNDER LOAD. NO FAULTS ON GPCU. AFTER EFeb 10, 2017 · N667FE · Airbus A300F4605R · AC Generator-AlternatorSDR FDEA201601110112Crossbeam · crackedMDCC CROSSBEAM CRACKED AT FRAME 64, Y-1150. REMOVE THE CRACK IAW SRM 51-73-10. REWORK THE REPAIR AREA IAW SRM 53-10-15 FIG 211. CHECK FOR CRACKS TO CUT EDGE & REWORKED AREA IAW NTM 51-10-08 & NO CRACK FOUND. MAKE THE REPAIR PROFILE IAW SRM 53-10-15 FIG 211Jan 11, 2016 · N667FE · Airbus A300F4605R · Fuselage Miscellaneous StructureSDR FDEA201601110111Crossbeam · crackedMDCC CROSSBEAM CRACKED AT FRAME 67, Y1700. CUT THE CRACKED AREA & DEBURR IAW SRM 53-10-15 FIG 211. REWORK THE REPAIR AREA IAW SRM 53-10-15 FIG 211. CHECK FOR CRACKS TO CUT EDGE & REWORKED AREA IAW NTM 51-10-08 & NO CRACK FOUND. MAKE THE REPAIR PROFILE IAW Jan 11, 2016 · N667FE · Airbus A300F4605R · Fuselage Miscellaneous StructureSDR FDEA201601110110Crossbeam · crackedMDCC CROSSBEAM CRACKED AT FRAME 27, Y-700. CUT THE CRACKED PARTIAL IAW SRM 53-10-15 FIG 212. PERFORM HEFC INSPECTION TO THE CUT OUT IAW NTM 51-10-08 & NO CRACK FOUND. FABRICATE THE REPAIR PARTS & DRILL THE FASTENER HOLES & INSTALLED THE REPAIR PARTS IAW SRJan 11, 2016 · N667FE · Airbus A300F4605R · Fuselage Miscellaneous StructureSDR FDEA201601110109Crossbeam · crackedMDCC CROSSBEAM CRACKED AT FRAME 30, Y1700. CUT THE CRACKED PARTIAL IAW SRM 53-10-15 FIG 21. PERFORM HEFC INSPECTION TO THE CUT OUT IAW NTM51-10-08 & NO CRACK FOUND. FABRICATE THE REPAIR PARTS & DRILL THE FASTENER HOLES & INSTALLED THE REPAIR PARTS IAW SRM 5Jan 11, 2016 · N667FE · Airbus A300F4605R · Fuselage Miscellaneous StructureSDR FDEA201601110108Crossbeam · crackedMDCC CROSSBEAM CRACKED AT FRAME 31, Y1700. CUT THE CRACKED PARTIAL IAW SRM 53-10-15 FIG 212. PERFORM HEFC INSPECTION TO THE CUT OUT IAW NTM 51-10-08 & NO CRACK FOUND. FABRICATE THE REPAIR ANGLE & FILLER & DRILL THE FASTENER HOLES & INSTALL THE REPAIR ANGLE Jan 11, 2016 · N667FE · Airbus A300F4605R · Fuselage Miscellaneous StructureSDR FDEA201601110107Crossbeam · crackedMDCC CROSSBEAM CRACKED AT FRAME 32, Y1700. REWORK THE REPAIR AREA IAW SRM 53-10-15 FIG 212. CHECK FOR CRACKS TO CUT EDGE & REWORKED AREA IAW NTM 51-10-08 & NO CRACK FOUND. MAKE THE REPAIR PROFILE IAW SRM 53-10-15 FIG 212. PERFORMED PENETRANT INSPECTION TO Jan 11, 2016 · N667FE · Airbus A300F4605R · Fuselage Miscellaneous StructureSDR FDEA201601100094Frame · crackedCENTER WING JOINT AT FRAME 40 LT, UPPER FASTENER HOLE FOUND CRACK SIGNAL. COMPLIED WITH EA 6-5710-T0322811 P 1. REPAIR CATEGORY IS B. THRESHOLD INTERVAL 2250 FC & 4860 FH. METHOD IN THE REPAIRED HOLE, ROTO TEST IAW NTM 51-10-01, BASED ON NTM 57-10-39 PART 6Jan 10, 2016 · N667FE · Airbus A300F4605R · Fuselage Main, FrameSDR FDEA201512033878Unknown · malfunctionedRIGHT CABIN DOOR SLIDE WILL NOT SHOW ARMED ON RT ECAM WHEN PUT IN THE ARMED POSITION. PERFORMED TEST OF R1 DOOR SLIDE ARMING / DISARMING IAW MM 52-73-13-05-02, SYSTEM CHECKS GOOD. NO HISTORY 99 DAYS. A/C OK FOR SERVICE.Dec 3, 2015 · N667FE · Airbus A300F4605R · Emergency EquipmentSDR FDEA201510203280Warning Message · false activationREJECTED TAKEOFF BELOW 80 KTS, FOR A MOMENTARY YELLOW HYD LOW PRESSURE ECAM ALERT. ANOTHER SUCCESSFUL TAKEOFF ATTEMPT WAS MADE. SYSTEM OPS NORMAL THROUGHOUT ALL PHASES OF FLIGHT. PERFORMED HYDRAULIC PRESSURE INDICATING FUNCTIONAL TEST PER AMM 29-32-00-05Oct 20, 2015 · N667FE · Airbus A300F4605R · Hydraulic Indicating SystemSDR FDEA201510053075Floor Panel · crackedMAIN DECK FLOOR PANEL 232YG HAS CRACK, BETWEEN FRAME 28 - 30, -Y450, -Y953. FABRICATED NEW PANEL 232YG ON T15 1165123 IAW DWG SRZ 25-005 REV L. CLASSIFIED AS MAJOR CAT A REPAIR.Oct 5, 2015 · N667FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201510053074Floor Panel · damagedMAIN DECK FLOOR PANEL 242EK HAS MISSING INSERTS, BETWEEN FRAME 51 - 54, -Y450, -Y953. FABRICATED NEW PANEL 242EK ON T15 1165124 IAW DWG SRZ 25-005 REV L. CLASSIFIED AS MAJOR CAT A REPAIR.Oct 5, 2015 · N667FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201510053073Floor Panel · damagedMCD BETWEEN FRAME 47 & 51, BETWEEN -Y450 & -Y953 FLOOR PANEL IS SPONGY & HAS MOVEMENT WHEN STEPPED ON. FABRICATED NEW PANEL 242ZJ ON T15 1165068 IAW DWG SRZ 25-005 REV L. CLASSIFIED AS MAJOR CAT A REPAIR.Oct 5, 2015 · N667FE · Airbus A300F4605R · Fuselage Floor Panel
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