N675FE

Service difficulty reports · 248

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 = 'N675FE' 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 FDEA201401230186Apu · shutdownNUMBER 1 GEN INOPERATIVE DUE TO MEL. APU AUTO SHUT DOWN 30 MIN INTO FLT AT 290 RESULTING IN SINGLE GEN OPERATIONS. AFTER DESCENDING TO FL210, APU RESTARTED RAN OK RTB MEMPHIS. CLEARED FAULTS IN ECB, RAN APU IAW AMM 49-61-11-04 COULD NOT DUPLICATE FAULT. Jan 23, 2014 · N675FE · Airbus A300F4605R · APU Core EngineSDR FDEA201210313791Pin · corrodedRT MLG AFT TRUNNION PIN HAS PITTING CORROSION UNDER PIN HEAD AROUND THE CIRCUMFERANCE. REPLACED RT MLG AFT TRUNION PIN IAW AMM 32-11-11-04, STEPS B-12-D AND D-8-(A- F).Oct 31, 2012 · N675FE · Airbus A300F4605R · Fuselage, Landing Gear Attach FittingsSDR FDEA201210303775Adapter · corrodedMAIN DECK CARGO FLOOR 1 EA CLEVIS ADAPTER AT FR 57.3 BETWEEN SEAT TRACK 2R -3R CORRODED INSIDE THE SCALLOP AREA APPROX 1" SQ AFTER REMOVAL OF LEVEL 1 CORROSION, FOUND FLOOR CLEVIS ADAPTER AT FR 57.3 BETWEEN SEAT TRACK 2R-3R TO BE OUT OF LIMITS IAW FSRM 53-10Oct 30, 2012 · N675FE · Airbus A300F4605R · Fuselage Miscellaneous StructureSDR FDEA201210233720Seat Track · corrodedMAIN DECK CARGO SEAT TRACK 2L BETWEEN FR78 AND FR79 HAS 2IN. AREA OF SURFACE OXIDATION AND 2 AREAS OF BARE METAL BETWEEN FR75 AND FR77 APPROX 8IN. AFTER REMOVAL OF SURFACE OXIDATION AREA WAS FOUND TO HAVE LEVEL 1 CORROSION AND OUT OF LIMITS IAW FSRM 53-10-16,Oct 23, 2012 · N675FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201210203701Floorboard · crackedMAIN DECK CARGO AFT FLOORBOARD 251BH HAS TWO CRACKS AROUND CLEVIS ADAPTERS. FABRICATED REPLACEMENT FLOORBOARD IAW DWG SRZ25-005.Oct 20, 2012 · N675FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201210203699Floor Panel · damagedMAIN DECK CARGO FLOOR PANEL 231EF HAS TWO CRUSHED AREAS, THE DAMAGE WAS FOUND ON REPAIR OF SEAT TRACK 4L, FR 20. FABRICATED REPLACEMENT FLOOR PANEL IAW DWG SRZ 25-005, REV J.Oct 20, 2012 · N675FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201210193691Web · crackedNR 1 ENG PYLON BOTTOM LWR SURFACE 16" FWD OF AFT END, ATTACH WEB CRACKED 3EA PLACES AT PNEUMATIC PRESSURIZATION LINE MEASURED .4", .7", AND 1.0" IN LENGTHS. FOUND CRACKS ON WEB AT NR 1 PYLON BOTTOM LWR SURFACE 16" FWD OF AFT ENDTO BE OUT OF LIMITS IAW FSRM 5Oct 19, 2012 · N675FE · Airbus A300F4605R · Nacelle/Pylon Miscellaneous StructureSDR FDEA201210193690Floor Panel · crackedFLOOR PANEL 232YG CENTER TOP SKIN CRACKED APPROX 8 INCHES FWD OF THE CLEVIS ADAPTER. AFT CLEVIS AREA CRACK APPROX 4". FABRICATED REPLACEMENT FLOOR PANEL IAW DWG SRZ 25-005, REV J.Oct 19, 2012 · N675FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201210193689Floor Panel · damagedFLOOR PANEL 231NG TOP SKIN PUNCTURE APPROX .5" X .2500" AND PANEL 231TG TOP SKIN PUNCTURE APPROX .5" X .5". REPAIRED FLOOR PANEL IAW SRM 53-10-20, PARA 9(A) PG 205 AND FABRICATED. REPLACEMENT FLOOR PANEL IAW DWG SRZ 25-005, REV J.Oct 19, 2012 · N675FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201210193688Floorboard · crackedAFT LEFT FLOORBOARD 251QH HAS AN 8 INCH CRACK AT CLS CUTOUT. FABRICATED REPLACEMENT FLOORBOARD IAW DWG SRZ 25-005, REV J.Oct 19, 2012 · N675FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201210193687Floor Panel · crackedFLOOR PANEL 242UJ TOP SKIN HAS IMPACT DAMAGE AT 5 CLEVIS LOCATIONS AND TOP SKIN CRACKING AROUND THE CLEVIS POINTS. FABRICATED REPLACEMENT FLOOR PANEL IAW DWG SRZ 25-005, REV J.Oct 19, 2012 · N675FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201210183663Seat Track · gougedMAIN DECK CARGO TRACK 3L AT FR 21 HAS 2 SCALLOPS DAMAGE. REPAIRED SEAT TRACK IAW EA6-5313-T0300020.Oct 18, 2012 · N675FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201210183676Floorboard · crackedMAIN DECK CARGO FLOORBOARD 251BH HAS 2 CRACKS 4 & 6 INCHES AROUND CLEVIS ADAPTERS. FABRICATED REPLACEMENT FLOOR PANEL IAW DWG SRZ 25-005 REV J.Oct 18, 2012 · N675FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201210183675Floorboard · crackedMAIN DECK CARGO FLOORBOARD 242PH HAS A 4 INCH CRACK AT CLEVIS CUTOUT. FABRICATED REPLACEMENT FLOOR PANEL IAW DWG SRZ 25-005 REV J.Oct 18, 2012 · N675FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201210183679Floorboard · crackedMAIN DECK CARGO AFT RT FLOORBOARD 252VF HAS TWO CRACKS 8 INCHES LONG AT CLEVIS CUTOUTS. FABRICATED, AND INSTALLED NEW FLOORBOARD IAW AMM 53-10-25-04-02 AND IAW DWG SRZ-005.Oct 18, 2012 · N675FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201210183678Floorboard · crackedMAIN DECK CARGO AFT RIGHT FLOORBOARD 252UH HAS ONE 3 INCH & ONE 6 INCH CRACK AT CLEVIS CUTOUTS. FABRICATED REPLACEMENT FLOOR PANEL IAW DWG SRZ 25-005 REV. J.Oct 18, 2012 · N675FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201210183677Floor Panel · damagedFLOOR PANEL 231AH HAS TWO AREAS OF CRUSHED CORE DAMAGE AT THE CLEVIS ADAPTERS. FABRICATED REPLACEMENT FLOOR PANEL IAW DWG SRZ 25-005, REV J.Oct 18, 2012 · N675FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201210183661Intercostal · crackedAVIONICS COMPARTMENT CEILING AREA AT FR 10, -33" RT OF CENTERLINE INTERCOSTAL HAS A 1" CRACK. FOUND DAMAGE ON INTERCOSTAL TO BE BEYOND ECONOMICAL REPAIR IAW FSRM 51-72-10, PG 1. R & R INTERCOSTAL WEB ON AVIONICS COMPARTMENT CEILING AREA AT FR 10 -33" RT SIDEOct 18, 2012 · N675FE · Airbus A300F4605R · Fuselage Miscellaneous StructureSDR FDEA201210173658Seat Track · damagedMDCC SEAT TRACK 4L AT FRAME 20 HAS 3 SCALLOP DAMAGE. REPAIRED SEAT TRACK IAW EA6-5313-T0300020.Oct 17, 2012 · N675FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201210173654Floor Panel · damagedFLOOR PANEL 242EK CRUSH AT 2 CLEVIS ADAPTER FABBED FLOOR PANEL IAW DWG SRZ 25-005, REV J.Oct 17, 2012 · N675FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201210173653Floor Panel · damagedFLOOR PANEL 242ZJ IMPACT DAMAGE AT 3 CLEVIS ADAPTER. FABRICATED REPLACEMENT FLOOR PANEL IAW DWG SRZ 25-005, REV J.Oct 17, 2012 · N675FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201210173652Floor Panel · damagedMAIN DECK CARGO FLOOR PANEL BETWEEN FR 30 AND FR32 AND SEAT TRACKS 4L & 5L IMPACT DAMAGE APPROX 30 SQUARE INCHES. FABRICATED REPLACEMENT FLOOR PANEL IAW DWG SRZ 25-005, REV J.Oct 17, 2012 · N675FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201210173651Floor Panel · damagedFLOOR PANEL 242RG HAS CRUSH DAMAGE AT CLEVIS AND METAL STRIP ON PANEL CHAFED. FABRICATED REPLACEMENT FLOOR PANEL IAW DWG SRZ 25-005, REV J.Oct 17, 2012 · N675FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201210173633Floor Panel · damagedFLOOR PANEL 242QJ HAS CRUSH CORE DAMAGE AT ALL CLEVIS ADAPTER AREAS AND TOP SKIN CRACKED APPROX 90 PERCENT OF THE PANEL. PANEL FWD TEFLON MISSING. FABRICATED REPLACEMENT PANEL WITH TEFLON STRIPS IAW DWG SRZ-25-005, REV J.Oct 17, 2012 · N675FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201210173632Floor Panel · damagedFLOOR PANEL 242SF TOP SKIN HAS CRUSH DAMAGE AT THE CLEVIS AND TOP PLY CRACK APPROX 12". PANEL FWD TEFLON MISSING AND AFT TEFLON MISSING. FABRICATED REPLACEMENT PANEL WITH TEFLON STRIPS IAW DWG SRZ-25-005, REV J.Oct 17, 2012 · N675FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201210163628Web · crackedINSIDE TAIL SECTION BETWEEN FR 86 & FR 87 ON STR 33R, WEB HAS 1" CRACK. R & R WEB AND STRAP ON INSIDE TAIL SECTION BETWEEN FR 86 AND FR 87, STR 33R IAW SRM 51-72-10, PG 1 -3.Oct 16, 2012 · N675FE · Airbus A300F4605R · Fuselage Miscellaneous StructureSDR FDEA201210123601Seat Track · corrodedSEAT TRACK 3R, BETWEEN FR 57.1 AND 57.2, HAS A 4 INCH AREA OF SURFACE OXIDATION. REMOVED CORROSION IAW SRM 51-74-10 PG 209 AND FOUND TO BE OUT OF LIMITS IAW SRM 53-10-16 FIG 102, PG 105. REMOVED DAMAGED SECTION OF SEAT TRACK AND FABRICATED NEW SEAT TRACK SECOct 12, 2012 · N675FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201210113595Cargo Track · corrodedMAIN DECK CARGO TRACK BETWEEN FR 64- 72 HAS TEN AREAS OF CORROSION ON LOWER SURFACE OF SCALLOPS AND EXTEND UNDER THE SCALLOPS 20 SQUARE INCHES. REMOVED LIGHT CORROSION. FOUND NINE AREAS TO BE WITHIN LIMITS IAW SRM 53-10-16, FIG 102, PG 105. FOUND ONE AREAOct 11, 2012 · N675FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201210103708Adapter · damagedMAIN DECK CARGO CLEVIS ADAPTOR AT FR31 BETWEEN SEAT TRACKS 4L AND 5L HAS BROKEN OUT BETWEEN SCALLOPS, REF AMM 53-10-16-6, R & R DAMAGE CLEVIS ADAPTER FR31 BETWEEN SEAT TRACK 4L AND 5L IAW AMM 53-10-23-4. REPROTECTED AREA IAW SRM 51-75-10.Oct 10, 2012 · N675FE · Airbus A300F4605R · Fuselage Main, Attach FittingsSDR FDEA201104091414Gearbox · dirtyLOWERED FLAPS TO 20*, 5 SEC LATER RECEIVED ECAM FLAPS SYS 1 & 2 FAULT. RECYCLED, WHICH FIXED PROBLEM. THEN TRIED TO CONFIGURE FLAPS 40*, RECEIVED SAME ECAM FLAPS SYS 1 & 2 FAULT. FLAPS STUCK AT 15*/20*. REPLACED LEFT TEE GEARBOX PER AMM 27-54-14. REPApr 9, 2011 · N675FE · Airbus A300F4605R · Trailing Edge Flap Control SystemSDR FDEA201012224739Frame · crackedENG 1 RT THRUST REVERSER COWL FWD RING FLANGE GOT CRACK AT UPPER EDGE, ABOUT 1.5 INCH. REPAIR THE DAMAGE AREA WITH DOUBLER AND FASTENERS IAW DWG NR: SRZ-78-002. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100.Dec 22, 2010 · N675FE · Airbus A300F4605R · Engine Thrust ReverserSDR FDEA201012224738Skin · crackedCLOSE R LT WING SPOILER SHROUD SUPPORT SKIN CRACK ABOUT 0.75 IN BELOW NR3 SPOILER INBD EDGE. FABRICATE A NEW SUPPORT SKIN IAW DWG NR A57240194 AND INSTALL WITH FASTENERS. REF AB6F SRM 51-40-21. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100.Dec 22, 2010 · N675FE · Airbus A300F4605R · SpoilersSDR FDEA201012224737Adapter · crackedTPE CLOSED RT MAIN DECK COMP'T FLOORBEAM FITTED WITH ADAPTER WAS CRACK AT FR64 AND -Y 1456 POSITION. REPLACED WITH NEW ADAPTER AND CHECK CONDITION NORMAL.REF AB6F SRM 51-40-21. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.Dec 22, 2010 · N675FE · Airbus A300F4605R · Fuselage Main, Attach FittingsSDR FDEA201012144659Carriage · misalignedRT WING NR5 FLAP TRACK FWD CARRIAGE UPPER BRIDGE INBD SIDE SHIM MIGRATION. EA6-2750-141650 REPAIR ACCOMPLISHED. IAW GMM 6-2-100, REPAIR CLASSIFIED AS MINOR.Dec 14, 2010 · N675FE · Airbus A300F4605R · Trailing Edge FlapsSDR FDEA201012104628Carriage · misalignedLT WING T/E FLAP NR6 FRONT CARRIAGE UPPER BRIDGE OTBD SHIM EXTRUDED. EA6-2750-141650 REPAIR ACCOMPLISHED. IAW GMM 6-2-100 REPAIR CLASSIFIED AS MINOR.Dec 10, 2010 · N675FE · Airbus A300F4605R · Trailing Edge FlapsSDR FDEA201007012299Line · leakingLOST GREEN SYS HYD PRESSURE DURING CLIMBOUT. RESERVOIR INDICATED EMPTY. FOUND NR 1 ENGINE GREEN HYD PUMP (TOP PUMP) INLET TO PYLON MANIFOLD HOSE CRACKED AND LEAKING. CREW DEBRIEF WHEN HYD PRESS WAS LOST, GREEN PUMPS TURNED OFF. LANDING GEAR MANUALLY EXTENJul 1, 2010 · N675FE · Airbus A300F4605R · Hydraulic System, MainSDR FDEA200904181329Transmitter · failedIN CRUISE FLT, RECEIVED ECAM ALERT "BLUE SYSTEM LO QUANTITY." COMPLIED W/ALL ECAM PROCEDURES AND APPLICABLE QRH PROCEDURES. BLUE SYSTEM QTY INDICATOR AT RED DOT ON OVERHEAD PANEL GAUGE. FOUND BLUE SYS PRIORITY VALVE 2064 LEAKING. PART NIS IN MEM. DURING FApr 18, 2009 · N675FE · Airbus A300F4605R · Hydraulic System, MainSDR 08FDEA02829Web · crackedMAIN CABIN METAL PANEL UNDER FLOOR PANEL 231 WG FROM FRAME 26 TO FRAME 28 IS CRACKED. REMOVED THRUST BRACKETS IAW A300-600 SRM 51-40-21; PARA 6. FOUND TO BE OUT OF LIMITS IAW A300-600 SRM 51-70-10. RECEIVED 2 NEW THRUST BRACKETS P/N A5378198422200, PO 62401Jul 11, 2008 · N675FE · Airbus A300F4605R · Fuselage Miscellaneous StructureSDR 08FDEA02828Web · corrodedMAIN CABIN METAL PANEL UNDER FLOOR PANEL 231 WG FROM FRAME 26 TO FRAME 28 IS CORRODED. REMOVED THRUST BRACKETS IAW A300-600 SRM 51-40-21; PARA 6. FOUND TO BE OUT OF LIMITS IAW A300-600 SRM 51-70-10. RECEIVED 2 NEW THRUST BRACKETS P/N A5378198422200, PO 6240Jul 11, 2008 · N675FE · Airbus A300F4605R · Fuselage Miscellaneous StructureSDR 08FDEA02819Attach Angle · crackedATTACH ANGLE ALONG FRAME 12A RIGHT IS CRACKED ON FWD SIDE APPROX 6 INCHES BELOW THE FLOOR. REMOVED ANGLE IN REF TO A300-600F SRM 51-40-21; PARA 6. RECEIVED A NEW ANGLE, PO 624972.1. LOCATED AND DRILLED IN REF TO A300-600F SRM 51-40-21; PARA 6. INSTALLED INJul 10, 2008 · N675FE · Airbus A300F4605R · Fuselage Main, Attach FittingsSDR 08FDEA02797Floor Panel · damagedMAIN CARGO DECK FLOOR PANEL 232 TG; TOP SURFACE IS CRUSHED AFT OF FRAME 21. MATERIAL ID A 402 H 35039-003, PO 613022.1 IAW FEDEX DWG SRZ 25-005, REV F. PART MARKED NEW FLOOR PANEL IAW FEDEX GMM 7-0-1000.Jul 9, 2008 · N675FE · Airbus A300F4605R · Fuselage Floor PanelSDR 08FDEA02798Floor Panel · damagedMAIN DECK FLOORBOARD 261 UF IS BROKEN. MAT ID N 407 35039-003, PO 613022.1. FABBED A NEW PANEL IAW FEDEX SRZ 25-005; REV F. PART MARKED IAW FEDEX GMM 7-0-1000.Jul 9, 2008 · N675FE · Airbus A300F4605R · Fuselage Floor PanelSDR 08FDEA02795Floorboard · crackedMAIN DECK FLOOR BOARD NR 251 RT IS CRACKED. MAT ID N 407 35039-003, PO 613022.1. FABBED A NEW PANEL IAW FEDEX SRZ 25-005; REV F. PART MARKED IAW FEDEX GMM 7-0-1000.Jul 9, 2008 · N675FE · Airbus A300F4605R · Fuselage Floor PanelSDR 08FDEA02794Floorboard · crackedMAIN DECK FLOORBOARD NR 251 XF IS CRACKED. MAT ID N 407 35039-003, PO 613022.1. FABBED A NEW PANEL IAW SRZ 25-005; REV F. PART MARKED IAW GMM 7-0-1000.Jul 9, 2008 · N675FE · Airbus A300F4605R · Fuselage Floor PanelSDR 08FDEA02793Floor Panel · damagedMAIN DECK FLOORBOARD 262 WF IS BROKEN. MATERIAL ID N 407 35039-003, PO 613022.1 AND FABBED A NEW PANEL IAW FEDEX DWG SRZ 25-- 5; REV F. PART MARKED IAW FEDEX GMM 7-0-1000.Jul 9, 2008 · N675FE · Airbus A300F4605R · Fuselage Floor PanelSDR 08FDEA02730Floor Panel · crackedMAIN DECK FLOORBOARD NR 251 QH IS CRACKED. FABRICATED A NEW FLOOR PANEL IAW FEDEX DWG SRZ 25-005; REV F. MATERIAL ID A 402 H 35039-003, PO 622013.1 IAW FEDEX DWG SRZ 25-005; REV F. PART MARKED IAW FEDEX GMM 7- 0-1000.Jul 7, 2008 · N675FE · Airbus A300F4605R · Fuselage Floor PanelSDR 08FDEA02689Floor Panel · damagedMAIN CARGO DECK FLOOR PANEL 232 AH HAS BELL BEARINGS STUCK AND PUNCTURES ON THE TOP SURFACE. REPAIRED DAMAGED FLOOR PANEL IN REF TO A300-600 FIG 202.Jul 3, 2008 · N675FE · Airbus A300F4605R · Fuselage Floor PanelSDR 08FDEA02688Floorboard · damagedMAIN CARGO DECK FLOOR PANEL 232 ZG HAS BALL BEARINGS STUCK AND PUNCTURES ON THE TOP SURFACE. REPAIRED DAMAGED FLOOR PANEL IN REF TO A300-600 SRM 53-10-20, FIG 202.Jul 3, 2008 · N675FE · Airbus A300F4605R · Fuselage Floor PanelSDR 08FDEA02687Floorboard · damagedMAIN CARGO DECK FLOOR PANEL 232 XG HAS BALL BEARINGS STUCK AND PUNCTURES ON THE TOP SURFACE. REPAIRED DAMAGED AREA PER A300-600 SRM 53-10-20, FIG 201.Jul 3, 2008 · N675FE · Airbus A300F4605R · Fuselage Floor PanelSDR 08FDEA02686Floorboard · damagedMAIN CABIN FLOOR PANEL 231 XG UPPER SURFACE HAS PUNCTURES FROM BALL BEARINGS. REPAIRED DAMAGED FLOOR PANEL IN REF TO A300-600 SRM 53-10-20, FIG 202.Jul 3, 2008 · N675FE · Airbus A300F4605R · Fuselage Floor Panel
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