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 FDEA201708232325Dummy Rail · crackedDUMMY SEAT TRACK LT NR 5 AT FR 54 TO FR54.2 FAILED GAP CHECK. UPON REMOVAL OF LT NR 5 DUMMY SEAT TRACK AND 3EA FLOOR SUPPORTS FOUND DUMMY SEAT TRACK CRACKED. REMOVED AND REPLACED LT NR 5 DUMMY SEAT TRACK FR 54 TO FR54.2 AND REINSTALLED 3EA FLOOR SUPPORTS IAWAug 23, 2017 · N675FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201708222296Dummy Rail · crackedDUMMY SEAT TRACK RT NR 5 AT FR38.2 TO FR40 FAILED GAP CHECK. UPON REMOVAL OF RT NR 5 DUMMY SEAT TRACK AT FR38.2 TO FR40 FOUND CRACKED. NO ESTABLISHED LIMITS PER SRM. REMOVED AND REPLACED RT NR 5 DUMMY SEAT TRACK AT FR38.2 TO FR40 IAW SRM 51-40-21. MAJOR REPAug 22, 2017 · N675FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201708222295Seat Track · gougedMAIN DECK BETWEEN FRAME 57 TO FRAME 57.1 Y 1959. SEAT TRACK HAS GOUGE ON CROWN. CLS ATTACHED AT DAMAGE LOCATION FR57 - FR57.1 Y1959 FOUND TO BE OUT OF LIMITS IAW SRM 53-10-16 FIG 204. REPAIRED SEAT TRACK IAW SRM 53-10-16 FIG 201 USING A53274005-SFS-. MAJOR REAug 22, 2017 · N675FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201703230982Door · unknownR1 DOOR SLIDE WILL NOT ARM. RAN A R1 DOOR SLIDE ARMING TEST AND TEST OF THE ASPSU IAW MM 25-61-20-06-01 AND 52-73-00-05-02. ALL CHECKS WERE NORMAL.Mar 23, 2017 · N675FE · Airbus A300F4605R · Service DoorsSDR FDEA201612164475Switch · stickingL1 DOOR EMERGENCY TEST SWITCH (25WL) STICKS IN THE TEST POSITION. REMOVED AND REPLACED THE SWITCH IAW SMP. SYSTEM OPS CHECKED GOOD IAW MM 33-51-00-05. ACFT OK FOR SERVICE.Dec 16, 2016 · N675FE · Airbus A300F4605R · Emergency LightingSDR FDEA201605031444Not Reported · malfunctionedAS WE LOST A/S THE RUDDER STARTED PULSING LT & RT. NO RUDDER LIMIT LIGHTS ILLUMINATED. IT DAMPED AS WE SLOWED & DESCENDED. NR 2 YAW DAMPER WAS ENGAGED. WE HAD KICKED AUTOPILOT OFF AT THIS POINT, SIGNIFICANT YAWING LT & RT. PRECAUTIONARY R & R NR 2 FAC IAWMay 3, 2016 · N675FE · Airbus A300F4605R · Rudder Control SystemSDR FDEA201603100893Gcu · malfunctionedDUE TO NR 2 GEN FAULT, STARTED APU & THEN APU GEN FAULTED. INFO ONLY, MASSIVE AMOUNT OF RAIN & LIGHTNING STRIKE TWO LEGS PRIOR. APU HAD FAULTED FIRE TRIP ON GND POWER CONTROL UNIT. R & R THE APU GEN CONTROL UNIT IAW A & B AMM CHPT 24-22-12-04. RAN APU GENMar 10, 2016 · N675FE · Airbus A300F4605R · AC InverterSDR FDEA201603100887Gcu · failedAT FL300 NR 2 GEN FAULTED, RESET FAULTED AGAIN. COMPLIED IN ECAM & QRH & PAW. FOUND NR 2 GEN GCU FAILED ON THE GPCU. R & R THE NR 2 ENG GEN GCU IAW A & B AMM CHPT 24-22-12-04. RAN THE NR 2 ENG IAW A & B JRH, NR 2 GEN. OPERATIONS CHECKED SATISFACTORY. ACFMar 10, 2016 · N675FE · Airbus A300F4605R · AC RegulatorSDR FDEA201506242014Stator · failedAFTER TAKEOFF NR 1 BRAKE INDICATOR ROSE TO 300. DROPPED GEAR TO COOL THE BRAKES. AFTER BRAKES WHERE COOL, CONTINUED FLIGHT TO DESTINATION. REMOVED TIRE & FOUND THAT STATOR DISK HAS COME APART & WEDGED BETWEEN THE TWO ROTOR DISK. R & R BRAKE IAW 32-42-27-Jun 24, 2015 · N675FE · Airbus A300F4605R · BrakeSDR FDEA201504111214Spar · damagedLEFT WING ROOT REAR SPAR SPOT FACE DAMAGED. REPAIRED IAW SRM 51-71-80. COMPLIED WITH EA 6-5710-T0316506 PART 1. MAJOR REPAIR IAW GMM 6-2-100.Apr 11, 2015 · N675FE · Airbus A300F4605R · Wing SparSDR FDEA201504111213Spar · damagedLEFT WING ROOT REAR SPAR 47, RIB 1 HOLE U SPOT FACE DAMAGED. SPOTPACED THE HOLE U AT LT WING ROOT SPAR IAW SRM 51-71-80. COMPLIED WITH EA :6-5710-T0316506 PART 1. MAJOR REPAIR IAW GMM 6-2-100.Apr 11, 2015 · N675FE · Airbus A300F4605R · Wing SparSDR FDEA201503271093Seat Track · corrodedMDCC FLOOR STRUCTURE SEAT TRACK CORRODED, FRAME 26 - 38.2, Y0. REMOVED THE CORROSION IAW SRM 51-74-10 EXCEEDED THE ALLOWABLE DAMAGE LIMITS IAW SRM 53-10-16-101 FIG 102. CUT OUT THE DAMAGED SEAT TRACK SECTION AT FRAME 26 - 28 IAW SRM 53-10-16-201 PARA 4. WETMar 27, 2015 · N675FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201503271092Skin · damagedLOWER FUSELAGE, FRAME 36 - 37, STRINGER 43R - 44R,SEVERAL LIGHTING STRIKE BURN MARKS ON SKIN. REPAIRED THE SKIN IAW SRM 53-10-12 FIG 208. INSTALLED THE DOUBLER & FASTENERS ON REPAIRED PART IAW SRM 53-10-12 FIG 208. MAJOR REPAIR IAW GMM 6-2-100.Mar 27, 2015 · N675FE · Airbus A300F4605R · Fuselage Main, Plate/SkinSDR FDEA201503251074Seat Track · corrodedMDCC FLOOR STRUCTURE SEAT TRACK CORRODED, FRAME 54.3 - 58, Y-450. REMOVED THE CORROSION IAW SRM 51-74-10. FOUND DELAMINATION. NEW SEAT TRACK IAW SRM 51-40-21. THIS REPAIR CATEGORY IS A. MAJOR REPAIR IAW GMM 6-2-100.Mar 25, 2015 · N675FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201503231056Rivet · corrodedAGEING INSPECTION, EXISTING REPAIR ON MDCC SEAT TRACK BETWEEN FRAME 65 - 69, Y0 REQUIRES EVALUATION FOR CONFORMITY. THE REPAIR WAS EVALUATED & FOUND THE REPAIR CONFORMED TO SRM 53-10-16 FIG 201 EXCEPT MINOR DEVIATION. NO CHAMFER EDGES, MOREOVER, SOME RIVETS Mar 23, 2015 · N675FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201503221047Fitting · looseRIGHT PYLON OTBD LOWER PYLON TO WING FITTING AT RIB 12, FOUND INBD LUG BUSHING LOOSE. REPAIRED IAW AMM 54-51-72-08-02. MAJOR REPAIR IAW GMM 6-2-100.Mar 22, 2015 · N675FE · Airbus A300F4605R · Nacelle/Pylon, Attach FittingsSDR FDEA201503221046Fitting · looseRIGHT PYLON OTBD LOWER PYLON TO WING FITTING AT RIB 12, FOUND OTBD LUG BUSHING LOOSE. REPAIRED IAW SRM 51-72-20, AND AMM54-51-72-08-02. MAJOR REPAIR IAW GMM 6-2-100.Mar 22, 2015 · N675FE · Airbus A300F4605R · Nacelle/Pylon, Attach FittingsSDR FDEA201503221045Fitting · looseLEFT PYLON OTBD LOWER PYLON TO WING FITTING AT RIB 12, FOUND OTBD LUG BUSHING LOOSE. REMOVED THE BUSHING IN REPAIR AREA IAW SRM 51-72-20. RE-BORED THE RIB 12 FITTING WITHOUT EXCEED 62.23MM IAW AMM 54-51-72-08-02. INSTALLED THE BUSH IAW AMM 54-51-72-08-02. Mar 22, 2015 · N675FE · Airbus A300F4605R · Nacelle/Pylon, Attach FittingsSDR FDEA201503221044Seat Track · crackedMDCC FLOOR STRUCTURE SEAT TRACK CORRODED FRAME 26 - 38.2, Y-1959. REMOVED THE CORROSION IAW SRM 51-74-10. CRACK WAS FOUND AND WAS OUT OF ALLOWABLE IAW SRM 53-10-16-101. CUT OUT SEAT TRACK. REPAIRED IAW SRM 53-10-16 FIG 201. THIS REPAIR WAS CATEGORY "A". Mar 22, 2015 · N675FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201503201029Skin · damagedAGEING INSPECTION, EXISTING REPAIR ON RT WING INBD FLAP UPPER SKIN RIB 11 - RIB 13 REQUIRES EVALUATION FOR CONFORMITY. THE REPAIR WAS EVALUATED & FOUND NOT IN CONFORMITY WITH SRM 57-50-00 FIG 206. WORN MARKS WERE ALSO FOUND ON EXISTING REPAIR DOUBLER, REPORTMar 20, 2015 · N675FE · Airbus A300F4605R · Trailing Edge FlapsSDR FDEA201503201028Skin · damagedAGEING INSPECTION, EXISTING REPAIR ON LT WING MID FLAP UPPER SKIN RIB 13 - 15 REQUIRES EVALUATION FOR CONFORMITY. THE REPAIR WAS EVALUATED & FOUND NOT IN CONFORMITY WITH SRM 57-50-00 FIG 205. MOREOVER WORN MARKS WERE ALSO ON EXISTING REPAIR DOUBLER, REPORTEDMar 20, 2015 · N675FE · Airbus A300F4605R · Trailing Edge FlapsSDR FDEA201503201025Repair · crackedAGEING INSPECTION, EXISTING REPAIR ON MDCC FLOORBEAM BETWEEN FRAME 28, Y-450 TO Y-953 REQUIRES EVALUATION FOR CONFORMITY. THE REPAIR WAS EVALUATED & FOUND NOT IN CONFORMITY WITH EA 6-5310-101017. MOREOVER, THE EXISTING REPAIR FITTING FOUND CRACKED. REPORMar 20, 2015 · N675FE · Airbus A300F4605R · Fuselage Main, Floor BeamSDR FDEA201503201024Repair · damagedAGEING INSPECTION, EXISTING REPAIR ON RT INBD FLAP LE SKIN RIB 12A - 17 REQUIRES EVALUATION FOR CONFORMITY. THE REPAIR WAS EVALUATED & FOUND IN CONFORMITY WITH SRM 57-50-00 FIG 208. HOWEVER, DENTS & NICKS WERE FOUND ON EXISTING REPAIR INSERT. REPORTED TO Mar 20, 2015 · N675FE · Airbus A300F4605R · Trailing Edge FlapsSDR FDEA201503201023Adapter · wornMDCC FLOORBEAM ADAPTOR WORN, FRAME 32 BETWEEN Y1456 & Y1959. REMOVED THE DAMAGED ADAPTER IAW SRM 51-40-21. DRILLED FASTENER HOLES & DEBURRED IAW SRM 51-40-44. INSTALLED NEW ADAPTER IAW SRM 51-40-21. THIS REPAIR CATEGORY IS A MAJOR REPAIR IAW GMM 6-2-100.Mar 20, 2015 · N675FE · Airbus A300F4605R · Fuselage Main, StructureSDR FDEA201503201022Adapter · wornMDCC FLOOR STRUCTURE CROSSBEAM ADAPTOR WORN, FRAME 30 BETWEEN Y1456 & Y1959. REPLACED THE DAMAGE ADAPTOR IAW SRM 51-40-21. MAJOR REPAIR IAW GMM 6-2-100.Mar 20, 2015 · N675FE · Airbus A300F4605R · Fuselage Main, StructureSDR FDEA201503201021Seat Track · corrodedMDCC FLOOR STRUCTURE SEAT TRACK CORRODED, FRAME 40 - 45, Y-953. REMOVED THE CORROSION IAW SRM 51-74-10, FOUND DELAMINATION. REPLACED THE SEAT TRACK IAW SRM 51-40-21. THIS REPAIR CATEGORY IS A MAJOR REPAIR IAW GMM 6-2-100.Mar 20, 2015 · N675FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201503201020Seat Track · corrodedMDCC FLOOR STRUCTURE SEAT TRACK CORRODED, FRAME 44 - 48, Y-953. REMOVED THE CORROSION IAW SRM 51-74-10. THE REMOVAL WAS WITHIN ALLOWABLE IAW SRM 53-10-16 101. MINOR REPAIR IAW GMM6-2-100.Mar 20, 2015 · N675FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201503201019Seat Track · corrodedMDCC FLOOR STRUCTURE SEAT TRACK CORRODED, FRAME 38.2 - 40, Y-953. REMOVED THE CORROSION IAW SRM 51-74-10 FOUND DELAMINATION. REMOVED THE CORRODED SEAT TRACK IAW SRM 51-40-21. DRILLED THE FASTENER HOLES IN THE NEW PART IAW SRM 51-40-44. INSTALLED THE NEW SEAT Mar 20, 2015 · N675FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201503201018Seat Track · corrodedMDCC FRAME 74 - 75, Y-45.0 SEAT TRACK WITH CORROSION. REMOVED THE CORROSION IAW SRM 51-74-10. FOUND DELAMINATION. REPLACED NEW SEAT TRACK IAW SRM 51-40-21. THIS REPAIR CATEGORY IS A. MAJOR REPAIR IAW GMM 6-2-100.Mar 20, 2015 · N675FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201503201017Seat Track · corrodedMDCC FRAME 65 - 66, -Y95.0 SEAT TRACK WITH CORROSION. REMOVED THE CORROSION IAW SRM 51-74-10. FOUND DELAMINATION. REPLACED NEW SEAT TRACK IAW SRM 51-40-21. THIS REPAIR CATEGORY IS A. MAJOR REPAIR IAW GMM6-2-100.Mar 20, 2015 · N675FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201503201016Seat Track · corrodedMDCC FRAME 70 - 71, Y0 SEAT TRACK WITH CORROSION. REMOVED THE CORROSION IAW SRM 51-74-10. FOUND DELAMINATION. REPLACED NEW SEAT TRACK IAW SRM 51-40-21. THIS REPAIR CATEGORY IS A. MAJOR REPAIR IAW GMM 6-2-100.Mar 20, 2015 · N675FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201503201015Seat Track · corrodedMDCC FRAME 70 - 71, -Y45.0 SEAT TRACK WITH CORROSION. REMOVED THE CORROSION IAW SRM 51-74-10, FOUND DELAMINATION. REPLACED NEW SEAT TRACK IAW SRM 51-40-21, FRAME 68 - 73, -450. THIS REPAIR CATEGORY IS A. MAJOR REPAIR IAW GMM 6-2-100.Mar 20, 2015 · N675FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201503201014Seat Track · corrodedMDCC FRAME 71 - 72, Y124.0 SEAT TRACK WITH CORROSION. REMOVED THE CORROSION PER SRM 51-74-10 ,CRACK FOUND .CUT AND REMOVED THE CORROSION ON SEAT TRACK SECTION FOR FR68-FR69 .PER SRM 53-10-16 FIG 201. MADE THE REPAIR SPLICE AND SEAT .TRACK PER SRM 53-10-16Mar 20, 2015 · N675FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201503201013Seat Track · corrodedMDCC FRAME 71 - 72, Y88.0 SEAT TRACK WITH CORROSION. REMOVED THE CORROSION PER SRM 51-74-10 FOUND DELAMINATION. REPLACED NEW SEAT TRACK AT FR 69-72 Y852.4. PER SRM 51-40-21.THIS REPAIR CATEGORY IS "A" .MAJOR REPAIR IAW GMM 6-2-100.Mar 20, 2015 · N675FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201503201012Seat Track · corrodedMDCC FRAMES 76 - 77, Y79.0 SEAT TRACK CORRODED. REMOVED THE CORROSION IAW SRM 51-74-10 FOUND DELAMINATION. REPLACED NEW SEAT TRACK AT FRAME 73 - 77 IAW SRM 51-40-21. THIS REPAIR CATEGORY IS A MAJOR REPAIR IAW GMM 6-2-100. .Mar 20, 2015 · N675FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201503201011Floor Support · corrodedMAIN DECK, FWD COURIER AREA FRAME 12A - 17, Y1959 FLOOR SUPPORT CORRODED. REMOVED CORROSION IAW SRM 51-74-10. FOUND DELAMINATION & REMOVED THE CORRODED SUPPORT IAW SRM 51-40-21. DRILLED FASTENER HOLES & DEBURRED IAW SRM 51-40-44. INSTALLED THE NEW FLOOR SUMar 20, 2015 · N675FE · Airbus A300F4605R · Fuselage Miscellaneous StructureSDR FDEA201503201010Floor Support · corrodedMAIN DECK, FWD COURIER AREA FRAME 12A - 17, Y-1959 FLOOR SUPPORT CORRODED. REMOVED THE CORRODED SUPPORT IAW SRM 51-40-21. DRILLED FASTENER HOLES & DEBURRED IAW SRM 51-40-44. INSTALLED THE NEW SUPPORT IAW SRM 51-40-21. THIS REPAIR CATEGORY IS A MAJOR REPAIRMar 20, 2015 · N675FE · Airbus A300F4605R · Fuselage Miscellaneous StructureSDR FDEA201503201008Floorbeam · crackedMDCC FRAME 31, Y157 FLOORBEAM CRACKED. REMOVED ADAPTER IAW SRM 51-40-21. CUT & REMOVE THE CRACK IAW SRM 53-10-15 FIG 212. FABRICATED THE REPAIR ANGLE & FILLER IAW SRM 53-10-15 FIG 212. WET INSTALLED THE REPAIR ANGLE FILLER & ADAPTER IAW SRM 53-10-15 FIG 21Mar 20, 2015 · N675FE · Airbus A300F4605R · Fuselage Main, Floor BeamSDR FDEA201503201007Floorbeam · crackedMDCC FRAME 32, Y157 FLOORBEAM CRACKED. REMOVED ADAPTER IAW SRM 51-40-21. CUT & REMOVE THE CRACK IAW SRM 53-10-15 FIG 212. FABRICATED THE REPAIR ANGLE & FILLER IAW SRM 53-10-15 FIG 212. WET INSTALLED THE REPAIR ANGLE FILLER & ADAPTER IAW SRM 53-10-15 FIG 21Mar 20, 2015 · N675FE · Airbus A300F4605R · Fuselage Main, Floor BeamSDR FDEA201503201006Floorbeam · crackedMDCC FRAME 64 Y-112 FLOORBEAM CRACKED. CUT & REMOVED THE CRACK IAW SRM 53-10-15 FIG 211, NO CRACK FOUND. REPAIRED THE FLOORBEAM IAW SRM 53-10-15 FIG 211. WET INSTALLED THE REPAIR PARTS IAW SRM 53-10-15 FIG 211. THIS REPAIR CATEGORY IS A MAJOR REPAIR IAW GMMMar 20, 2015 · N675FE · Airbus A300F4605R · Fuselage Main, Floor BeamSDR FDEA201503201005Seat Track · corrodedMDCC SEAT TRACK CORRODED ,FRAMES 40 - 42, Y-1456. REMOVED THE CORRODED SEAT TRACK IAW SRM 51-40-21. DRILLED THE FASTENER HOLES IN THE NEW PART IAW SRM 51-40-44. INSTALLED NEW SEAT TRACK IAW SRM 51-40-21. THIS REPAIR CATEGORY IS A MAJOR REPAIR IAW GMM 6-2-1Mar 20, 2015 · N675FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201503201004Adapter · crackedMDCC FLOORBEAM CRACKED, FRAME 67 BETWEEN Y1456 & Y1959. CUT & REMOVED THE CRACK IAW SRM 53-10-15 FIG 211. PERFORMED HFEC INSPECTION TO THE CUT OUT IAW NTM 51-10-08. NO CRACK FOUND. FABRICATED THE REPAIR ANGLE & FILLER SRM 53-10-15 FIG 211. WET INSTALLED TMar 20, 2015 · N675FE · Airbus A300F4605R · Fuselage Main, StructureSDR FDEA201503201003Adapter · crackedMDCC FLOORBEAM ADAPTOR CRACKED, FRAME 59 BETWEEN Y-953 & Y-1456. REMOVED THE CRACKED ADAPTER IAW SRM 51-40-21. DRILLED THE FASTENER HOLES IN THE NEW PART IAW SRM 51-40-44. INSTALLED NEW ADAPTER IAW SRM 51-40-21. THIS REPAIR CATEGORY IS A MAJOR REPAIR IAW GMar 20, 2015 · N675FE · Airbus A300F4605R · Fuselage Main, StructureSDR FDEA201503201002Frame · crackedCENTER WING JOINT AT FRAME 40 RT SIDE LOWER FASTENER HOLE WITH CRACK SIGNAL. COMPLIED WITH EA 6-5710-T0316343 PT 1. MAJOR REPAIR IAW GMM 6-2-100.Mar 20, 2015 · N675FE · Airbus A300F4605R · Fuselage Main, FrameSDR FDEA201503201001Frame · crackedCENTER WING JOINT AT FRAME 40 RT SIDE MID FASTENER HOLE WITH CRACK SIGNAL. COMPLIED WITH EA 6-5710-T0316343 PT 1. MAJOR REPAIR IAW GMM 6-2-100.Mar 20, 2015 · N675FE · Airbus A300F4605R · Fuselage Main, FrameSDR FDEA201503201000Frame · crackedCENTER WING JOINT AT FRAME 40 RT SIDE UPPER FASTENER HOLE WITH CRACK SIGNAL. COMPLIED WITH EA 6-5710-T0316343 PT 1. MAJOR REPAIR IAW GMM 6-2-100.Mar 20, 2015 · N675FE · Airbus A300F4605R · Fuselage Main, FrameSDR FDEA201503200999Frame · crackedCENTER WING JOINT AT FRAME 40 LT SIDE LOWER FASTENER HOLE WITH A CRACK SIGNAL. COMPLIED WITH EA 6-5710-T0316343 PT 1. MAJOR REPAIR IAW GMM 6-2-100.Mar 20, 2015 · N675FE · Airbus A300F4605R · Fuselage Main, FrameSDR FDEA201503200998Frame · crackedCENTER WING JOINT AT FRAME 40 LT SIDE MID FASTENER HOLE WITH CRACK SIGNAL. COMPLIED WITH EA 6-5710-T0316343 PT 1. MAJOR REPAIR IAW GMM 6-2-100.Mar 20, 2015 · N675FE · Airbus A300F4605R · Fuselage Main, FrameSDR FDEA201503200997Frame · crackedCENTER WING JOINT AT FRAME 40 LT SIDE UPPER FASTENER HOLE WITH A CRACK SIGNAL. COMPLIED WITH EA:6-5710-T0316343 PT1. MAJOR REPAIR IAW GMM 6-2-100.Mar 20, 2015 · N675FE · Airbus A300F4605R · Fuselage Main, FrameSDR FDEA201503200996Adapter · crackedMDCC FLOORBEAM ADAPTOR CRACKED, FRAME 62 BETWEEN Y953 & Y1456. REMOVED THE CRACKED ADAPTER IAW SRM 51-40-21. FABRICATED THE NEW ADAPTER IAW DWG A53278288. INSTALLED NEW ADAPTER IAW SRM 51-40-21. THIS REPAIR CATEGORY IS A MAJOR REPAIR IAW GMM6-2-100.Mar 20, 2015 · N675FE · Airbus A300F4605R · Fuselage Main, Structure
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