N677FE

Service difficulty reports · 275

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 = 'N677FE' 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 FDEA2019020540257Girt Bar · out of alignmentPDIS 677 25-60 8067 04FEB19 MEM FACT U LOGPAGES:2851303 R1 DOOR WILL NOT ARM SLIDE FACT 04FEB19 09:11 MEM REALIGNED GIRT BAR PER AMM 25-61-20-00-01. Feb 4, 2019 · N677FE · Airbus A300F4605R · Emergency EquipmentSDR FDEA201810162926Pitot Tube · obstructedDURING TAKEOFF, AT 100 KNOTS, THE CAPTAIN'S AND FIRST OFFICER`S PFDS, READ 50 KNOTS. REJECTED THE TAKEOFF AT APPROXIMATELY 110 KNOTS. FOUND DEBRIS IN THE FIRST OFFICER'S PITOT TUBE. REPLACED THE FIRST OFFICER`S PITOT TUBE IAW AMM 34-11-15-04. PERFORMED Oct 16, 2018 · N677FE · Airbus A300F4605R · Pitot/Static SystemSDR FDEA2018061281430Sensor · faultyCLIMBING OUT GREEN RESV OVHT, COMPLIED WITH QRH OVERHEAT, REMAINED ILLUMINATED UNTIL 50 MILES OUTSIDE OF DSM. TURNED GREEN PUMPS BACK ON AND LANDED. NO FURTHER OVERHEAT. REMOVED AND REPLACED GREEN HYDRAULIC RESERVOIR OVERHEAT SENSOR PER MM 29-33-11-04. SERVICEJun 8, 2018 · N677FE · Airbus A300F4605R · Hydraulic Indicating SystemSDR FDEA2018042601103Controller · inoperativeJUST AFTER TAKEOFF RECEIVED A SYS NR 1 FLAPS FAULT. TROUBLESHOT FAULT IAW TSM 27-50-05. REMOVED AND REPLACED WITH SERVICEABLE UNIT IAW AMM 27-51-18-04. OPS CHECKED GOOD.Apr 24, 2018 · N677FE · Airbus A300F4605R · Trailing Edge Flap Control SystemSDR FDEA201804201073Floor Support · corrodedMAIN DECK, FRAMES 11-13. FLOOR SUPPORT Y1456 HAS CORROSION ON THE UPPER AND LOWER SURFACES. REMOVED AND REPLACED THE FLOOR SUPPORT IAW SRM 51-40-21. CORROSION FOUND OUT OF LIMITS IAW SRM 51-74-10. MAJOR REPAIR.Apr 20, 2018 · N677FE · Airbus A300F4605R · Fuselage Miscellaneous StructureSDR FDEA201804171027Rib · crackedRIGHT WING CENTER FLAP RIB 16 UPPER FLANGE HAS ONE INTERNAL CRACK. FABRICATED AND INSTALLED A REPAIR RIB IAW SRM 57-50-00, FIGURE 201. MAJOR REPAIR.Apr 17, 2018 · N677FE · Airbus A300F4605R · Trailing Edge FlapsSDR FDEA201804171026Rib · crackedRIGHT WING CENTER FLAP RIB 26 UPPER FLANGE HAS TWO INTERNAL CRACKS. REPAIRED THE RIB FLANGES IAW SRM 57-50-00-201 PARA 4.A. MAJOR REPAIR.Apr 17, 2018 · N677FE · Airbus A300F4605R · Trailing Edge FlapsSDR FDEA201804161014Rib · crackedRIGHT WING CENTER FLAP RIB 27 UPPER FLANGE HAS INTERNAL CRACKS, REPAIRED THE RIBS IAW SRM 57-50-00-201, PARA 4.A. MAJOR REPAIR.Apr 16, 2018 · N677FE · Airbus A300F4605R · Trailing Edge FlapsSDR FDEA201804161013Floor Support · corrodedMAIN DECK, FRAMES 11 - 13 FLOOR SUPPORT, Y953, UPPER AND LOWER SURFACES CORRODED. REMOVED AND REPLACED THE FLOOR SUPPORT IAW SRM 51-40-21. FRAME FOUND OUT OF LIMITS IAW SRM 51-74-10. MAJOR REPAIR.Apr 16, 2018 · N677FE · Airbus A300F4605R · Fuselage Miscellaneous StructureSDR FDEA201804161009Seat Track · no testLEFT NR 4 DUMMY TRACK, FRAMES 54 TO 54.2 FAILED A GAP INSPECTION. REMOVED AND REPLACED WITH A NEW DUMMY TRACK IAW SRM 51-40-21. MAJOR REPAIR.Apr 16, 2018 · N677FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201804080945Seat Track · corrodedMAIN DECK BETWEEN FR26 AND FR28 Y-1456 SEAT TRACK FLANGE HAS CORROSION. REPAIRED Y-1456 SEAT TRACK BETWEEN FR26.5 TO FR30.5 IAW SRM 53-10-16 FIG 201A SEAT TRACK SPLICE REPAIR. MAJOR REPAIR.Apr 8, 2018 · N677FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201804080944Seat Track · damagedMAIN DECK BETWEEN FR26 AND FR27 Y1959 SEAT TRACK CROWN BROKEN. CUT OUT SEAT TRACK SECTION Y1959 BETWEEN FR26 TO FR32 IAW SRM 53-10-16 FIG 208. FABRICATED NEW SEAT TRACK SECTION P/N A53274005-SFS-DAP IAW SRM 53-10-16 FIG 208. INSTALLED NEW SEAT TRACK SECTIOApr 8, 2018 · N677FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201804070917Floor Panel · brokenMAIN CABIN FLOOR PANEL 242DF BROKEN. FABRICATED A NEW FLOOR PANEL IAW SRZ-25-005. THE NEW FLOOR PANEL WAS INSTALLED. MAJOR REPAIR.Apr 7, 2018 · N677FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201804070916Floor Panel · crackedMAIN CABIN FLOOR PANEL 242PF HAD A CORNER BROKEN. FABRICATED A NEW FLOOR PANEL IAW SRZ-25-005. INSTALLED THE NEW FLOOR PANEL. MAJOR REPAIR.Apr 7, 2018 · N677FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201804070915Floor Panel · crackedMAIN CABIN FLOOR PANEL 241YJ HAD A BROKEN CORNER. FABRICATED A NEW FLOOR PANEL IAW SRZ-25-005. THE NEW FLOOR PANEL WAS INSTALLED. MAJOR REPAIR.Apr 7, 2018 · N677FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201804070914Floor Panel · crackedMAIN CABIN FLOOR PANLE 242UJ HAD A DAMAGED CORNER. FABRICATED A NEW FLOOR PANEL IAW SRZ-25-005. THE FLOOR PANEL WAS INSTALLED. MAJOR REPAIR.Apr 7, 2018 · N677FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201804070912Floor Panel · crackedMAIN CABIN FLOOR PANEL 241JG CORNER BROKEN. FABRICATED A NEW FLOOR PANEL IAW SRZ-25-005. MAJOR REPAIR. THE FLOOR PANEL WAS INSTALLED.Apr 7, 2018 · N677FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201804060899Adapter · damagedSEAT TRACK ADAPTER AT FRAME 59 BETWEEN Y1456 AND Y1959 DAMAGED. REMOVED AND REPLACED THE SEAT TRACK ADAPTER IAW SRM 51-40-21. MAJOR REPAIR.Apr 6, 2018 · N677FE · Airbus A300F4605R · Fuselage Miscellaneous StructureSDR FDEA201804060898Seat Track · damagedSEAT TRACK AT FRAME 57.3 BETWEEN Y1456 AND Y1959, DAMAGED. REMOVED AND REPLACED THE SEAT TRACK IAW SRM 51-40-21. MAJOR REPAIR.Apr 6, 2018 · N677FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201804060897Floor Panel · damagedFLOOR PANEL 221MF DAMAGED IN SEVERAL AREAS. FABRICATED A NEW FLOOR PANEL IAW DWG SRZ-25-005. MAJOR REPAIR.Apr 6, 2018 · N677FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201804060896Floor Panel · crackedMAIN CABIN FLOOR PANEL 252YH CRACKED. FABRICATED A NEW FLOOR PANEL IAW SRZ-25-005. MAJOR REAIR.Apr 6, 2018 · N677FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201804060895Floor Panel · brokenMAIN CABIN FLOOR PANEL 252BH HAS A BROKEN CORNER. FABRICATED A NEW FLOOR PANEL IAW SRZ-25-005. MAJOR REPAIR.Apr 6, 2018 · N677FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201804060893Floor Panel · crackedMAIN CABIN FLOOR PANEL 242ZJ CRACKED. FABRICATED A NEW FLOOR PANEL IAW SRZ-25-005. MAJOR REPAIR.Apr 6, 2018 · N677FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201804060892Floor Panel · crackedMAIN CABIN FLOOR PANEL 252DF CRACKED. FABRICATED A NEW FLOOR PANEL IAW SRZ-25-005. MAJOR REPAIR.Apr 6, 2018 · N677FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201804060891Floor Panel · crackedMAIN CABIN FLOOR PANEL 241MF CRACKED. FABRICATED A NEW FLOOR PANEL IAW SRZ-25-005. MAJOR REPAIR.Apr 6, 2018 · N677FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201804060890Floor Panel · crackedMAIN CABIN FLOOR PANEL 242TH BROKEN. FABRICATED A NEW FLOOR PANEL IAW SRZ-25-005. MAJOR REPAIR.Apr 6, 2018 · N677FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201804050872Floor Panel · brokenMAIN CABIN FLOOR PANEL 261ZF WAS BROKEN. FABRICATED A NEW FLOOR PANEL IAW SRZ 25-005. MAJOR REPAIR.Apr 5, 2018 · N677FE · Airbus A300B4605R · Fuselage Floor PanelSDR FDEA201804050871Floor Panel · brokenMAIN CABIN FLOOR PANEL 242JF BROKEN. FABRICATED A NEW FLOOR PANEL IAW SRZ 25-005. MAJOR REPAIR.Apr 5, 2018 · N677FE · Airbus A300B4605R · Fuselage Floor PanelSDR FDEA201804050870Floor Panel · brokenMAIN CABIN FLOOR PANEL 231HH BROKEN. FABRICATED A NEW FLOOR PANEL IAW SRZ 25-005. MAJOR REPAIR.Apr 5, 2018 · N677FE · Airbus A300B4605R · Fuselage Floor PanelSDR FDEA201804050869Floor Panel · brokenMAIN CABIN FLOOR PANEL 231RG BROKEN. FABRICATED A NEW FLOOR PANEL IAW SRZ 25-005. MAJOR REPAIR.Apr 5, 2018 · N677FE · Airbus A300B4605R · Fuselage Floor PanelSDR FDEA201804050867Floor Panel · damagedMAIN CABIN FLOOR PANEL 231VG DAMAGED AND PUNCTURED. FABRICATED A NEW FLOOR PANEL IAW SRZ 25-005. MAJOR REPAIR.Apr 5, 2018 · N677FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201804050866Floor Panel · puncturedMAIN CABIN FLOOR PANEL 231FF HAD NUMEROUS PUNCTURES. FABRICATED A NEW FLOOR PANEL IAW SRZ 25-005. MAJOR REPAIR.Apr 5, 2018 · N677FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201804050865Floor Panel · crackedMAIN CABIN FLOOR PANEL 232LG HAD A DAMAGED CORNER. FABRICATED A FLOOR PANEL IAW SRZ 25-005. MAJOR REPAIR.Apr 5, 2018 · N677FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201804050864Floor Panel · brokenMAIN CABIN FLOOR PANEL 231GG CORNER BROKEN. FABRICATED A NEW FLOOR PANEL IAW SRZ 25-005. MAJOR REPAIR.Apr 5, 2018 · N677FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201804050863Floor Panel · crackedMAIN CABIN FLOOR PANEL 232UG BROKEN. FABRICATED A NEW FLOOR PANEL IAW SRZ 25-005. MAJOR REPAIR.Apr 5, 2018 · N677FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201702280675Flap System · malfunctionedAFTER TAKE OFF AT FLAPS 15/0, RETRACTED THE SLATS & THE SLATS RETRACTED BUT THE UPPER ZIPPER MOVED TO 255 KTS ON BOTH PFD'S. TRIED A RECYCLE BUT THE SAME RESULT. THE SFPI SHOWED THE SLATS UP & RECEIVED NO ECAMS. ON POST FLIGHT INSPECTION FOUND THE LG VMFeb 28, 2017 · N677FE · Airbus A300F4605R · Trailing Edge Flap Control SystemSDR FDEA201702210622Battery Pack · no testEMERGENCY LIGHT TEST FAILED IAW SERVICE CHECK. TROUBLESHOT IAW TSM 33-51-00 FIG 107, FOUND POWER SUPPLY 29WL FAILING PRESS TO TEST, REMOVED AND REPLACED THE BATTER PACK IAW AMM 33-51-14-04, OPS CHECKED GOOD IAW AMM 33-51-00-05.Feb 21, 2017 · N677FE · Airbus A300F4605R · Emergency LightingSDR FDEA201511283808Frame · chafedMAIN DECK CARGO FRAME 27 CHAFED, BETWEEN STRINGERS 13 - 15R. REPAIRED IAW EA 6-5310-T0321552 PT1. MAJOR REPAIR IAW GMM 6-2-100.Nov 28, 2015 · N677FE · Airbus A300F4605R · Fuselage Main, FrameSDR FDEA201511283807Frame · gougedMAIN DECK CARGO FRAME 28 FOUND GOUGED, BETWEEN STRINGERS 8 - 22L. REPAIRED IAW EA 6-5310-T0321552 PT1. MAJOR REPAIR IAW GMM 6-2-100.Nov 28, 2015 · N677FE · Airbus A300F4605R · Fuselage Main, FrameSDR FDEA201511283806Frame · chafedMAIN DECK CARGO BAY FRAME 54 FOUND GOUGED, BETWEEN STRINGERS 12 - 13R. REPAIRED IAW EA 6-5310-T0321552 PT1. MAJOR REPAIR IAW GMM 6-2-100.Nov 28, 2015 · N677FE · Airbus A300F4605R · Fuselage Main, FrameSDR FDEA201511283805Frame · gougedMAIN DECK CARGO COMPARTMENT MAIN FRAME 47 FOUND GOUGED, BETWEEN STRINGERS 12 - 13R. REPAIRED IAW EA 6-5310-T0321552 PT1. MAJOR REPAIR IAW GMM 6-2-100.Nov 28, 2015 · N677FE · Airbus A300F4605R · Fuselage Main, FrameSDR FDEA201511283804Frame · chafedMAIN DECK CARGO COMPARTMENT, MAIN FRAME FOUND GOUGE FRAME 54, BETWEEN STRINGER 12L & 13L. REPAIRED THE MDCC MAINFRAME FR54 S12L-S13L. THIS REPAIR CATEGORY "C". MAJOR REPAIR IAW GMM 6-2-100.Nov 28, 2015 · N677FE · Airbus A300F4605R · Fuselage Main, FrameSDR FDEA201511283803Frame · chafedMAIN DECK CARGO COMPARTMENT, MAIN FRAME FOUND GOUGE FRAME 47, BETWEEN STRINGER 12L & 13L. REPAIRED THE MDCC MAINFRAME FR47 S12L-S13L. THIS REPAIR CATEGORY "C". REPAIR IAW GMM 6-2-100.Nov 28, 2015 · N677FE · Airbus A300F4605R · Fuselage Main, FrameSDR FDEA201511273797Adapter · wornMDCC FLOOR STRUCTURE CROSSBEAM ADAPTOR WORN, FRAME 42, BETWEEN Y-450 & Y-953. REMOVE CROSSBEAM ADAPTOR IAW AMM 20-21-12-00. DRILL FASTENER HOLES & DEBURR IAW SRM 51-40-44. APPLY ALODINE TO THE FASTENER HOLES IAW SRM51-21-10. APPLY PRIMER TO THE FASTENER HONov 27, 2015 · N677FE · Airbus A300F4605R · Fuselage Miscellaneous StructureSDR FDEA201511093523Pressure Deck · crackedMAIN DECK CARGO COMPARTMENT, HORIZONTAL PRESS DECK, VERTICAL WEB CRACKED AT FRAME 47, BETWEEN Y-953 & Y-1456. REPAIRED THE CRACKED VERTICAL WEB IAW SRM 53-15-15 FIG 201. THIS REPAIR CATEGORY B. THE FIRST INSPECTION THRESHOLD FROM REPAIR EMBODIMENT 24000FC &Nov 9, 2015 · N677FE · Airbus A300F4605R · Fuselage Main, BulkheadSDR FDEA201511093522Pressure Deck · crackedMAIN DECK CARGO COMPARTMENT, HORIZONTAL PRESS DECK, VERTICAL WEB CRACKED AT FRAME 47, BETWEEN Y953 & Y1456. REPAIRED IAW SRM 53-15-15 FIG 201. MAJOR REPAIR IAW GMM 6-2-100.Nov 9, 2015 · N677FE · Airbus A300F4605R · Fuselage Main, BulkheadSDR FDEA201511093521Pressure Deck · crackedMAIN DECK CARGO COMPARTMENT, HORIZONTAL PRESS DECK, VERTICAL WEB CRACKED AT FRAME 47, BETWEEN Y0 & Y-450. REPAIRED IAW SRM 53-15-15 FIG 201. MAJOR REPAIR IAW GMM 6-2-100.Nov 9, 2015 · N677FE · Airbus A300F4605R · Fuselage Main, BulkheadSDR FDEA201511093520Pressure Deck · crackedMAIN DECK CARGO COMPARTMENT, HORIZONTAL PRESS DECK, VERTICAL WEB CRACKED AT FRAME 47, BETWEEN Y0 & Y450. REPAIRED IAW SRM 53-15-15 FIG 201.Nov 9, 2015 · N677FE · Airbus A300F4605R · Fuselage Main, BulkheadSDR FDEA201511063499Repair · crackedEXISTING REPAIR ON MDCC FLOOR STRUCTURE CROSSBEAM FRAME 58, BETWEEN Y-450 & Y-953. THE EXISTING REPAIR WAS EVALUATED & CRACK WAS FOUND IN REPAIR AREA. REPAIRED THE CRACK EO 6-5100-7-5000 D1 PT 1. THE REPAIR WAS CATEGORY A & WAS CLASSIFIED AS MAJOR IAW GMM 6Nov 6, 2015 · N677FE · Airbus A300F4605R · Fuselage Miscellaneous StructureSDR FDEA201511063500Seat Track · damagedEXISTING REPAIR ON MDCC FLOOR STRUCTURE SEAT TRACK, BETWEEN FRAME 58 & 61, Y1456. THE EXISTING REPAIR WAS EVALUATED & FOUND IN CONFORMITY IAW SRM 53-10-16 FIGURE 201, BUT DAMAGE WAS FOUND IN REPAIR AREA. REPAIRED THE DAMAGED SEAT TRACK IAW SRM 53-10-16 FIGNov 6, 2015 · N677FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach Fittings
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