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 FDEA202307121743Fitting · failedCORROSION FOUND IN THE RIB 5 FITTING. REPAIRED PER AIRBUS REPAIR INSTRUCTIONS R57240425Jul 12, 2023 · N675FE · Airbus A300* · Fuselage Structure (General)SDR FDEA202210252655Spar · crackedCENTER WING BOX - INSPECTION OF REAR SPAR AND BOTTOM PANEL AT JUNCTION WITH FUSELAGE FR47 RH SIDE, FASTENER "C" HOLE FOUND CRACK SIGNAL REPAIRED THE CENTER WING BOX REAR SPAR AND BOTTOM PANEL AT JUNCTION WITH FUSELAGE FR47 RH SIDE CRACKED FASTENER Ï¿½CÏ¿½ Oct 25, 2022 · N675FE · Airbus A300F4605R · Fuselage Main, StructureSDR FDEA202210242646Fitting · crackedCENTER WING BOX - INSPECTION OF REAR SPAR AND BOTTOM PANEL AT JUNCTION WITH FUSELAGE FR47 RH SIDE, FASTENER HOLE 165 FOUND CRACK SIGNAL REPAIRED THE CENTER WING BOX REAR SPAR AND BOTTOM PANEL AT JUNCTION WITH FUSELAGE FR47 RH SIDE CRACKED FASTENER HOLE 165Oct 24, 2022 · N675FE · Airbus A300F4605R · Fuselage Main, Attach FittingsSDR FDEA202210242645Seat Track · corrodedMAIN DECK FR54-FR54.2 Y450 SEAT TRACK FOUND HEAVY CORROSION REPLACED THE MAIN DECK FR54-FR54.2 Y450 CORRODED SEAT TRACK WITH A FABRICATED PART PER DWG: A53813127(ISSUE.C00) AND A300-600F SRM51-40-21. THIS IS CATEGORY A REPAIR. MAJOR REPAIR IAW FEDEX GMM6-2Oct 24, 2022 · N675FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR FDEA202210222640Angle · damagedCOMPLY WITH EA 6-5230-T0369311 B P4, MAIN CARGO DOOR LOWER FWD CORNER CONNECTOR CLIP DAMAGE - REWORK, BY REPLACING THE CONNECTION CLIP REPLACED THE MAIN DECK CARGO DOOR LOWER FWD CORNER CONNECTION CLIP WITH A FABRICATED PART PER DWG: A52371130(ISSUE. F)Oct 22, 2022 · N675FE · Airbus A300F4605R · Cargo/Baggage DoorsSDR FDEA202210022443Door Frame · crackedRH FWD CREW DOOR - FRAME SEGMENT CRACKED AT FR14C ITEM 40 REPLACED RH FWD CREW DOOR CRACKED FRAME SEGMENT AT FR14C WITH A FABRICATED PART PER A300-600F SRM51-40-21 AND DWG: F52181297 (ISSUE.K), F52181299 (ISSUE.G). TRACKING EA 6-5210-T0370794 P1 RAISED ANDOct 2, 2022 · N675FE · Airbus A300F4605R · Fuselage Main, StructureSDR FDEA202208181996Engine · smokeAT CRUISE WE NOTICED SOME SORT OF SMOKE IN THE COCKPIT. DECLARED EMERGENCY AND DIVERTED TO PIT. NO SMOKE INDICATOR LIGHTS. EMERGENCY DECLARED. NR 1 ENGINE REMOVED AND REPLACE. COALESCER SOCKS REMOVED AND REPLACED & O2 SERVICED. PERFORMED ENGINE RUNS PER JRH,Aug 18, 2022 · N675FE · Airbus A300F4605R · Engine (Turbine/Turboprop)SDR FDEA202204040829Diaphragm · damagedR1 DOOR EMERGENCY CYLINDER-DAMPNER FOUND AT 0 PSI. SERVICED R1 DOOR ASSIST BOTTLE IAW AMM 52-10-14-03-02. NOTICED PRESSURE SLOWLY DEACREASING. AFTER TEN MIN BOTTLE ONLY INDICATING 500PSI. FOUND DIAPHRAM WITH HOLE IN IT , REPLACED DIAPHRAM & O-RINGS LEAApr 4, 2022 · N675FE · Airbus A300F4605R · Passenger/Crew DoorsSDR FDEA202203160586None · noneDURING DESCENT RECEIVED ENGINE 2 LOOP B FAULT ECAM MESSAGE ACCOMPANIED BY OVERHEAD INDICATION. COMPLIED WITH APPROPRIATE QRH PROCEDURE. RELEASED FOR SERVICE PER MEL : 26-12-XX CATEGORY : C EXP : 26MAR22 "MEL 26-12-XX: ENG 2__LOOP B__ - INOP. FLIGHT CREW MMar 16, 2022 · N675FE · Airbus A300* · Detection SystemSDR FDEA202202180319Slide · failedPDIS 675 25-60 1477 18FEB22 BOS OPEN U WHILE CLOSING THE DOOR, THE DOOR SLIDE DEPLOYED. IT SHOULD BE NOTED THAT THE FO, RAMP, AND MX FOLLOWED PROCEDURES EXACTLY. FURTHERMORE, THE DOOR WAS NOT FULLY CLOSED, NOR WAS THE SLIDE ARMED (IN FACT THE Feb 18, 2022 · N675FE · Airbus A300* · Emergency EquipmentSDR FDEA2020063071374Limiter · malfunctionedAFTER TAKEOFF FROM PDX FLAPS SYS 1 AND 2 FAULT. FLAPS STUCK. CONFIGURATION SLATS 15 FLAPS 20 DIVERTED TO KOAK PER GOC REQUEST. RECORDED FAULT (01111) FLAPS JAM. SFCC2 RECORDED FAULT (01110) HIGH SPEED V (01110). SFCC1 AND SFCC 2 BITE TEST PASSED. FOUND Jun 27, 2020 · N675FE · Airbus A300F4605R · Trailing Edge Flap Control SystemSDR FDEA202006101172Skin Panel · delaminatedLOWER LT SIDE RUDDER LEADING EDGE PANEL HAS DELAM. REPAIRED RUDDER PANEL IAW EA 6-5540-T0354180 AND SRM 55-41-12 AND 51-77-10.Jun 10, 2020 · N675FE · Airbus A300F4605R · Rudder, Plate/SkinSDR FDEA202006031119Skin · gougedLEFT WING NR 1 SLAT LEADING EDGE UPPER SURFACE HAS GOUGE AND MULTIPLE SCRATCHES ALONG ENTIRE SLAT, FROM END TO END. REPAIRED LEADING EDGE OF LT NR 1 SLAT IAW EA 6-5750-T0354063-P1, SRM 51- 73-10, SRM 51-73-11, SRM 51-21-10, SRM 51-23-10, SRM 51-75-10, AND DWGJun 3, 2020 · N675FE · Airbus A300F4605R · Leading Edge DevicesSDR FDEA202006021114Cover · cracked#2 ENGINE PYLON INBD SIDE EXTERIOR TRIM IS CRACKED THROUGH AN EXISTING WELD REPAIR AT THE BOTTOM OF THE PYLON APPROX 38" AFT OF THE FIRE BOTTLE ACCESS OPENING REMOVED AND REPLACED EXTERIOR TRIM IAW A300 SRM 51-40-21 AND AIRBUS DWG A54515187, ISSUE E.Jun 2, 2020 · N675FE · Airbus A300* · Nacelle/Pylon StructureSDR FDEA2020090862114Trim Panel · crackedNR 2 ENGINE PYLON INBOARD SIDE EXTERIOR TRIM IS CRACKED THROUGH AN EXISTING WELD. REPAIR AT THE BOTTOM OF THE PYLON APPROX 38" AFT OF THE FIRE BOTTLE ACCESS OPENING. REMOVED AND REPLACED EXTERIOR TRIM IAW A300 SRM 51-40-21 AND AIRBUS DWG A54515187, ISSUE E.Jun 2, 2020 · N675FE · Airbus A300F4605R · Nacelle/Pylon, Main FrameSDR FDEA2020060321114Trim Panel · crackedNUMBER 2 ENGINE PYLON INBD SIDE EXTERIOR TRIM IS CRACKED THROUGH AN EXISTING WELD. REPAIR AT THE BOTTOM OF THE PYLON APPROX 38" AFT OF THE FIRE BOTTLE ACCESS OPENING. REMOVED AND REPLACED EXTERIOR TRIM IAW SRM 51-40-21 AND DWG A54515187, ISSUE E.Jun 2, 2020 · N675FE · Airbus A300F4605R · Nacelle/Pylon Miscellaneous StructureSDR FDEA2020060321110Plate · crackedNUMBER 1 PYLON INBD FISH PLATE CRACKED. REMOVED FISH PLATE ON NR 1 PYLON INBD SIDE IAW SRM 51-40-21. LOCATED AND DRILLED NEW FISH PLATE PO 962545.4 AND SHIM PO 972481.1 IAW SRM 51-40-44 AND DWG A54612371 ISSUE B, ASSEMBLED FISH PLATE AND SHIM IAW SRM 51-40-2Jun 2, 2020 · N675FE · Airbus A300F4605R · Nacelle/Pylon Miscellaneous StructureSDR FDEA2020060111093Seat Track · corrodedMAIN CABIN SEAT TRACK AT -Y953, BETWEEN FR 56 AND FR 57, HAS CORROSION. REMOVED AND REPLACED DAMAGED SECTION OF SEAT TRACK IAW SRM 53-10-16 FIG 201.May 31, 2020 · N675FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR FDEA2020052981073Seat Track · corrodedMAIN CABIN FLOOR SUPPORT STRUCTURE, UPPER SURFACE IS CORRODED AT FRAME 30, LOCATION AT APPROXIMATELY -Y 2425.7. REMOVED DAMAGE IAW SRM 51-73-10 AND FOUND TO BE OUT OF LIMITS IAW SRM 53-10-16, WITH A MAX MATERIAL REMOVED OF .024". REPAIRED SEAT TRACK IAW SRM May 28, 2020 · N675FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR FDEA2020052961055Skin · damagedWHILE ACCOMPLISHING TASK CARD 53309364 RE-INSPECTION OF PREVIOUSLY BLENDED EXTERIOR FUSELAGE SKIN DAMAGE, FOUND DAMAGE STILL EXISTS BETWEEN FRAMES 29 AND 30 AND BETWEEN STRINGER 45R AND 46R, PREVIOUS BLENDED OUT AREA. ACCOMPLISHED REPAIR DOUBLER IAW SRM 53-10May 26, 2020 · N675FE · Airbus A300F4605R · Fuselage Main, Plate/SkinSDR FDEA202005261049Floor Panel · delaminatedMAIN GEAR WELL FLOOR PANEL 147BF IS DELAMINATED. REPAIRED FLOOR PANEL 147BF BY FABRICATION IAW SRZ-25-005 REV: R.May 26, 2020 · N675FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA202005261048Rib · crackedLEFT HAND WING CENTER FLAP SHOWING INDICATION AT RIB 27 AFT CRACKED. REPAIRED LEFT CENTER FLAP RIB 27 IAW SRM 57-50-00 PG 203 AND PG 220 AND EA 6-5750-T0354210-P1.May 26, 2020 · N675FE · Airbus A300F4605R · Trailing Edge FlapsSDR FDEA2020052641041Floorboard · punctured(PARTS RACK) FLOORBOARD 231GG HAS PUNCTURES. FABRICATED NEW FLOOR PANEL 231GG PER SRZ-25-005 REV R.May 24, 2020 · N675FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA202005180979Attach Angle · crackedATTACHING ANGLE FOR CUSP WEB JUST AFT OF FRA 79 L/H IS CRACKED REMOVED AND REPLACED ANGLE PER AIRBUS DWG A53981418 ISSUE KMay 18, 2020 · N675FE · Airbus A300F4605R · Fuselage Miscellaneous StructureSDR FDEA202005180978Cusp Web · crackedCUSP WEB ON AFT SIDE OF FRA 79 L/H IS CRACKED REMOVED AND REPLACED WEB PER AIRBUS DWG A53981360 ISSUE KMay 18, 2020 · N675FE · Airbus A300F4605R · Fuselage Miscellaneous StructureSDR FDEA202005180977Floorboard · damaged(PARTS RACK) FLOORBOARD 231FF HAS PUNCTURES REPLACED FLOOR PANEL IAW A300-600 AMM 06-41-53, SRM 53-10-20, SRZ-25-005May 18, 2020 · N675FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA202005180976Floorboard · damaged(PARTS RACK) FLOORBOARD 232WG IS PUNCTURED REPLACED FLOOR PANEL IAW A300-600 AMM 06-41-53, SRM 53-10-20, SRZ-25-005May 18, 2020 · N675FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA202005180975Floorboard · damaged(PARTS RACK) FLOORBOARD 232SG IS PUNCTURED REPLACED FLOOR PANEL IAW A300-600 AMM 06-41-53, SRM 53-10-20, SRZ-25-005May 18, 2020 · N675FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA2020051870965Floorboard · damaged(PARTS RACK) FLOORBOARD 231YG IS MISSING EDGE FILL FABRICATED NEW FLOOR PANEL PER FEDEX SRZ-25-005 REV R AND PART MARKED NEW PANEL PER FEDEX GMM 07-0-1001May 17, 2020 · N675FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA2020051870964Crossbeam · damagedCENTER CABIN BELOW FLOOR OVER WING L/H SIDE C44 TRACK SUPPORT GOUGED (STREAMER) REMOVED AND REPLACED CROSSBEAM PER AIRBUS DWG A53812846 ISS. A.May 17, 2020 · N675FE · Airbus A300F4605R · Fuselage Miscellaneous StructureSDR FDEA2020051540937Floorboard · damaged(PARTS RACK) FLOORBOARD 261PF IS BROKEN ON THE EDGE FABRICATED NEW FLOOR PANEL 261PF IAW FEDEX SRZ 25-005 REV - R, PART MARKED PER FEDEX GMM 07-0-1001May 14, 2020 · N675FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA2020042961056Skin · damagedWHILE ACCOMPLISHING TASK CARD 53309364, RE- INSPECTION OF PREVIOUSLY BLENDED EXTERIOR FUSELAGE SKIN DAMAGE, FOUND DAMAGE STILL EXISTS BETWEEN FRAMES 32 AND 33 AND STRINGER 45R AND 46R, PREVIOUS BLENDED OUT AREA. ACCOMPLISHED REPAIR DOUBLER IAW SRM 53-10-12,Apr 26, 2020 · N675FE · Airbus A300F4605R · Fuselage Main, Plate/SkinSDR FDEA2020042961054Skin · damagedWHILE ACCOMPLISHING TASK CARD 53309364, RE-INSPECTION OF PREVIOUSLY BLENDED EXTERIOR FUSELAGE SKIN DAMAGE, FOUND DAMAGE STILL EXISTS APPROX 7" FWD OF FRAME 35 AND BETWEEN STRINGER 45R AND 46R, PREVIOUS BLENDED OUT AREA. ACCOMPLISHED REPAIR DOUBLER IAW SRM 53-Apr 26, 2020 · N675FE · Airbus A300F4605R · Fuselage Main, Plate/SkinSDR FDEA2020042961053Skin · damagedWHILE ACCOMPLISHING TASK CARD 53309364, RE-INSPECTION OF PREVIOUSLY BLENDED EXTERIOR FUSELAGE SKIN DAMAGE, FOUND DAMAGE STILL EXISTS BETWEEN FRAMES 33 AND 34 AND BETWEEN S45R AND S46R, PREVIOUS BLEND OUT AREA. ACCOMPLISHED REPAIR DOUBLER IAW SRM 53-10-12, FIGApr 26, 2020 · N675FE · Airbus A300F4605R · Fuselage Main, Plate/SkinSDR FDEA202004261052Skin · damagedWHILE ACCOMPLISHING TASK CARD 53309364, RE-INSPECTION OF PREVIOUSLY BLENDED EXTERIOR FUSELAGE SKIN, FOUND DAMAGE STILL EXISTS BETWEEN FRAMES 30 AND 31 AND BETWEEN S45R AND S46R, PREVIOUS BLEND OUT AREA. ACCOMPLISHED REPAIR DOUBLER IAW SRM 53-10-12 FIG 208. AApr 26, 2020 · N675FE · Airbus A300F4605R · Fuselage Main, Plate/SkinSDR FDEA2020060531123Intercostal · crackedFORWARD CARGO PIT, INTERCOSTAL BETWEEN FRAMES C26-C27, BELOW RT OUTBOARD ROLLER TRACK IS CRACKED ON AFT UPPER CORNER. REMOVED AND REPLACED INTERCOSTAL BETWEEN FRAMES C26-C27, BELOW OUTBOARD ROLLER TRACK IAW SRM 51-40-21 AND DWG 14A53778347.Apr 23, 2020 · N675FE · Airbus A300F4605R · Fuselage Miscellaneous StructureSDR FDEA201802270573Power Supply · inoperativePRIOR TO PUSHBACK, RIGHT SLIDE INDICATION WILL NOT SHOW ARMED. TROUBLESHOT IAW ASM 52-73-00. REMOVED AND REPLACED THE AUTONOMOUS POWER SUPPLY IAW MM 52-73-18-04, AND 52-73-00-05-02. OPS CHECKED GOOD.Feb 27, 2018 · N675FE · Airbus A300F4605R · Emergency EquipmentSDR FDEA201708292408Floor Panel · brokenMDCC 251TH FLOOR PANEL BROKEN. FABRICATED NEW FLOOR PANEL 251TH P/N FX-B5327027700200 ON T17/1291751 IAW DWG SRZ-25-005 CAT "A" MAJOR REPAIR.Aug 29, 2017 · N675FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201708292407Floor Panel · brokenMDCC 252NH FLOOR PANEL BROKEN. FABRICATED NEW FLOOR PANEL 252NH P/N FX-B5327027500300 ON T17/1291764 IAW DWG SRZ-25-005 CAT "A" MAJOR REPAIR.Aug 29, 2017 · N675FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201708292406Floor Panel · brokenMDCC 241FJ FLOOR PANEL BROKEN. FABRICATED FLOOR PANEL P/N FX- -B5327062003200 ON T17/1291757 IAW DWG SRZ-25-005 CAT "A" MAJOR REPAIR (241FJ).Aug 29, 2017 · N675FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201708292405Floor Panel · brokenMDCC 241GJ FLOOR PANEL BROKEN. FABRICATED NEW FLOOR PANEL 241GJ P/N FX-B5327062002000 ON T17/1291773 IAW DWG SRZ-25-005 CAT "A" MAJOR REPAIR.Aug 29, 2017 · N675FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201708292404Floor Panel · brokenMDCC 241RJ FLOOR PANEL BROKEN. FABRICATED 241RJ FLOOR PANEL P/N FX-B5327062400000 ON T17/1291849 IAW DWG SRZ-25-005 CAT "A" MAJOR REPAIR.Aug 29, 2017 · N675FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201708292403Floor Panel · brokenMDCC 241TH FLOOR PANEL BROKEN. FABRICATED 241TH FLOOR PANEL P/N FX-B5327060000200 ON T17/1291847 IAW DWG SRZ-25-005 REV M CAT "A" MAJOR REPAIR.Aug 29, 2017 · N675FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201708292402Floor Panel · brokenMDCC 251BH FLOOR PANEL BROKEN. FABRICATED FLOOR PANEL P/N FX-B5327028700200 ON T17/1291842 IAW DWG SRZ-25-005 CAT "A" MAJOR REPAIR (251BH).Aug 29, 2017 · N675FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201708292401Floor Panel · brokenMDCC 252GF FLOOR PANEL BROKEN. FABRICATED 252GF FLOOR PANEL P/N FX-B5327027300000 ON T17/1291843 IAW DWG SRZ-25-005 REV M CAT "A" MAJOR REPAIR.Aug 29, 2017 · N675FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201708292400Floor Panel · brokenMDCC 242KK FLOOR PANEL BROKEN. FABRICATED FLOOR PANEL 242KK P/N FX-B5327063600000 ON T17/1291838 IAW DWG SRZ-25-005 CAT "A" MAJOR REPAIR.Aug 29, 2017 · N675FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201708292399Floor Panel · brokenMDCC 241GF FLOOR PANEL BROKEN. FABRICATED NEW FLOOR PANEL 241GF ON T17/1291767 IAW DWG SRZ-25-005 CAT "A" MAJOR REPAIR P/N FX-B5327048001600.Aug 29, 2017 · N675FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201708242353Crossbeam · crackedCROSSBEAM CRACKED IN 2EA PLACES FR41 -Y450 TO -Y953 RT. REMOVED AND REPLACED CROSSBEAM AT FR41 BETWEEN SEAT TRACKS -Y450 TO -Y953 IAW SRM 51-40-21. MAJOR REPAIR.Aug 24, 2017 · N675FE · Airbus A300F4605R · Fuselage Miscellaneous StructureSDR FDEA201708232328Seat Track · corrodedMAIN DECK CARGO SEAT TRACK Y450 FR 55 HAS A BUILDUP OF CORROSIVE MATERIAL. REPLACED SEAT TRACK FROM FR54.2 TO FR57.5 IAW SRM 51-40-21. REMOVED CORROSION FOUND OUT OF LIMITS IAW SRM 53-10-16. MAJOR REPAIR.Aug 23, 2017 · N675FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201708232326Seat Track · crackedDUMMY SEAT TRACK LT NR 4 AT FR 38.2 TO FR40 FAILED GAP CHECK. REMOVED DUMMY SEAT TRACK CRACKED AT LT NR 4 FR38.2 TO FR40. LOCATED AND DRILLED NEW DUMMY SEAT TRACK AND INSTALLED IAW SRM 51-40-44 AND SRM 51-40-21. MAJOR REPAIR.Aug 23, 2017 · N675FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach Fittings
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