N665FE

Service difficulty reports · 201

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 = 'N665FE' 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 FDEA202610151590Hydraulic System · low quantityDURING TAKEOFF ROLL AT 65 KNOTS, MASTER CAUTION WITH BLUE HYD SYS RSVR LO. REJECTED TAKEOFF AT 75 KIAS. COMPLIED WITH ECAM AND QRH. AMM 12-12-29-00, BLUE HYD QTY LOW. SERVICED BLUE HYD SYS IAW AMM 12-12-29-00.Oct 15, 2026 · N665FE · Airbus A300F4605R · Hydraulic System, MainSDR FDEA202603030308Safety Wire · failedFOUND R1 DOOR SLIDE EJECTOR BAG RELEASE CABLE WITH IMPROPER SAFETY WIRE INSTALLED. EA: 9-2560-T0386431 INSTALLED PROPER SAFETY WIRE MS20995CY16 ON THE R1 DOOR SLIDE SN# 0552 EJECTOR BAG RELEASE CABLE. REF E.A. ABOVE.Mar 3, 2026 · N665FE · Airbus A300F4605R · Emergency EquipmentSDR FDEA202603030307Safety Wire · failedTHE L1 SLIDE PACKBOARD/ACTIVATION SAFETY/BREAKAWAY WIRE REQUIRES REPLACEMENT, IT HAS THE INCORRECT SAFETY WIRE INSTALLED. AMM: 25-61-20-05-01 EA: 9-2560-T0386431 INSTALLED THE CORRECT SAFETY WIRE PER AMM 25-61-20-05-01 AND EA 9-2560-T0386431. AIRCRAFT Mar 3, 2026 · N665FE · Airbus A300F4605R · Emergency EquipmentSDR FDEA202410281594Cargo Track · damagedMAIN DECK CARGO COMPARTMENT - EXISTING SEAT TRACK REPAIR AT -Y450 BETWEEN FR40 AND FR45 REQUIRES EVALUATION FOT CONFORMITY TO APPROVED DATA THE EXISTING REPAIR ON MAIN DECK CARGO COMPARTMENT SEAT TRACK AT -Y450 BETWEEN FR40 AND FR45 WAS EVALUATED AND FOUNDOct 28, 2024 · N665FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR FDEA202410181542Cargo Track · wornMAIN DECK CARGO COMPARTMENT - SEAT TRACK -Y1456 FR53-FR54 INNER SURFACE WORN REPAIRED THE WORN SEAT TRACK AT MAIN DECK CARGO COMPARTMENT -Y1456 BETWEEN FR53 AND FR54 PER A300-600F SRM 53-10-16-201 FIG.201. THIS IS CATEGORY A REPAIR. MAJOR REPAIR IAW FEDEX Oct 18, 2024 · N665FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR FDEA202410181541Crossbeam · corrodedMAIN DECK CARGO - CROSSBEAM LOWER SURFACE FR59 Y953-Y1456 CORRODED. COMPLIED WITH EA: 6-5310-T0381123 P1. TITLE: FUSELAGE - MAINFRAME - CORROSION ON MDCC FR59 CROSSBEAM LOWER FLANGE. REPAIRED THE MAIN DECK CARGO CORRODED CROSSBEAM AT FR59 BETWEEN Y953 AND Oct 18, 2024 · N665FE · Airbus A300F4605R · Fuselage Main, StructureSDR FDEA202410181540Floor Support · no discrepancyEXISTING REPAIR ON MAIN DECK FLOOR SUPPORT AT Y730 BETWEEN FR11 AND FR13A REQUIRES EVALUATION FOR CONFORMITY ENTRY IN ERROR DUPLICATE WITH SDR#: 24-1506Oct 18, 2024 · N665FE · Airbus A300F4605R · Fuselage Miscellaneous StructureSDR FDEA202410151506Floor Support · corrodedEXISTING REPAIR ON MAIN DECK FLOOR SUPPORT AT Y730 BETWEEN FR11 AND FR13A REQUIRES EVALUATION FOR CONFORMITY THE EXISTING REPAIR ON MAIN DECK SUPPORT AT Y730 BETWEEN FR11 AND FR13A WAS EVALUATED AND FOUND CONFORMITY WITH DWG: A53612214(ISSUE.V00), BUT THE Oct 15, 2024 · N665FE · Airbus A300F4605R · Fuselage Miscellaneous StructureSDR FDEA202410111486Frame · crackedINSPECTION OF FR40 LOWER JUNCTION FASTENER HOLE #3 LH SIDE FOUND CRACK SIGNAL COMPLIED WITH EA: 6-5710-T0381079 P1. TITLE: WINGS - BASIC WING STRUCTURE - FR40 LH LOWER JUNCTION LOWER HOLE - CRACK REPAIR. REPAIRED THE CRACKED #3 HOLE AT FR40 LH SIDE LOWER JOct 11, 2024 · N665FE · Airbus A300F4605R · Fuselage Main, FrameSDR FDEA202410081441Seat Track · damagedSEAT TRACK LOBES DAMAGED FOR LOCK AT POS MP0754 REPAIRED THE DAMAGED SEAT TRACK AT MAIN DECK -Y953 BETWEEN FR28 AND FR29 PER A300- 600F SRM 53-10-16-201 FIG.201. THIS IS CATEGORY A REPAIR. MAJOR REPAIR IAW FEDEX GMM6-2-100.Oct 8, 2024 · N665FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR FDEA202410071439Frame · crackedCENTER WING BOX - INSPECTION OF REAR SPAR AND BOTTOM PANEL AT JUNCTION WITH FUSELAGE FR47 LH SIDE, FASTENER "C" HOLE FOUND CRACK SIGNAL COMPILED WITH EA: 6-5710-T0381007 P1. REPAIRED THE CENTER WING BOX REAR SPAR AND BOTTOM PANEL AT JUNCTION WITH FUSELAGEOct 7, 2024 · N665FE · Airbus A300F4605R · Fuselage Main, FrameSDR FDEA202410071438Frame · crackedCENTER WING BOX - INSPECTION OF REAR SPAR AND BOTTOM PANEL AT JUNCTION WITH FUSELAGE FR47 LH SIDE, FASTENER "I" HOLE FOUND CRACK SIGNAL COMPLIED WITH EO: 6-5710-E0342809 D P1. REPAIRED THE CRACKED HOLE "I" OF CENTER WING BOX - REAR SPAR AND BOTTOM PANEL ATOct 7, 2024 · N665FE · Airbus A300F4605R · Fuselage Main, FrameSDR FDEA202410071437Rib · crackedRH WING CENTER FLAP RIB UPR FLANGE FOUND 2EA CRACKS AT RIB26 BETWEEN STGR2.7 AND REAR SPAR. COMPLIED WITH EA: 6-5750-T0380847 P1. TITLE: WING - FLIGHT SURFACES - RH CENTER FLAP CRACKS AT UPPER FLANGES OF RIB 26 AT STR. 2.7 / 2.8 - ALI 575306-01-1A. REPAIREOct 7, 2024 · N665FE · Airbus A300F4605R · Trailing Edge FlapsSDR FDEA202410071436Rib · crackedLH WING CENTER FLAP RIB UPR FLANGE FOUND 6EA CRACKS AT RIB25 BETWEEN STGR2.8 AND REAR SPAR, RIB26 BETWEEN STGR2.6 AND REAR SPAR, AND RIB27 BETWEEN STGR2.7 AND REAR SPAR. COMPLIED WITH EA: 6-5750-T0380959 P1. TITLE: WING - FLIGHT SURFACES - LH CENTER FLAP Oct 7, 2024 · N665FE · Airbus A300F4605R · Trailing Edge FlapsSDR FDEA202410071435Rib · crackedLH WING CENTER FLAP RIB UPR FLANGE FOUND 4EA CRACKS AT RIB18 BETWEEN STGR2.8 AND REAR SPAR, RIB19 BETWEEN STGR2.7 AND REAR SPAR, AND RIB20 BETWEEN STGR2.8 AND REAR SPAR. COMPLIED WITH EA: 6-5750-T0380959 P1. TITLE: WING - FLIGHT SURFACES - LH CENTER FLAP Oct 7, 2024 · N665FE · Airbus A300F4605R · Trailing Edge FlapsSDR FDEA202410071434Rib · crackedLH WING CENTER FLAP RIB UPR FLANGE FOUND 7EA CRACKS AT RIB11 BETWEEN STGR2.6 AND REAR SPAR, RIB12 BETWEEN STGR2.7 AND REAR SPAR, AND RIB13 BETWEEN STGR2.6 AND STGR2.7 COMPLIED WITH EA: 6-5750-T0380959 P1. TITLE: WING - FLIGHT SURFACES - LH CENTER FLAP CROct 7, 2024 · N665FE · Airbus A300F4605R · Trailing Edge FlapsSDR FDEA202410071433Web · crackedMAIN DECK FR47 Y953-Y1456 UNDERFLOOR WEB CRACKED REPAIRED THE CRACKED WEB AT MAIN DECK FR47 Y953-Y1456 UNDERFLOOR PER A300-600F SRM53-15-15-201-C2 FIG.201. THIS IS CATEGORY B REPAIR AND MUST BE INSPECTED AT DEFINED INTERVALS PER A300-600F SRI53-15-15-2-002Oct 7, 2024 · N665FE · Airbus A300F4605R · Fuselage Miscellaneous StructureSDR FDEA202410071432Web · crackedMAIN DECK FR47 Y0-Y450 UNDERFLOOR WEB CRACKED REPAIRED THE CRACKED WEB AT MAIN DECK FR47 Y0-Y450 UNDERFLOOR PER A300-600F SRM53- 15-15-201-C2 FIG.201. THIS IS CATEGORY B REPAIR AND MUST BE INSPECTED AT DEFINED INTERVALS PER A300-600F SRI53-15-15-2-002-00. IOct 7, 2024 · N665FE · Airbus A300F4605R · Fuselage Miscellaneous StructureSDR FDEA202404020432Power Supply · failedIN THE ATTEMPT TO REMOVE FOR TIME, S/N BATT PACK(S/N 243728 PS3) - THE EMER PWR SUP UNIT(29WL1) P/N 3214-41 INTERNAL CIRCUIT CARD BROKE(FELL OUT OF UNIT). C/W PT1, STEP 1 OF ABOVE EA. ACFT OK FOR SVC ONCE THE MEL OF 33-51-05-01 IS APPLIED. COURIER COApr 2, 2024 · N665FE · Airbus A300F4605R · Emergency LightingSDR FDEA202210082520Retainer · failedCREW REPORTED R1 DOOR DIFFICULT TO DISARM. ON ARRIVAL AT A/C, FOUND DOOR OPENED & GIRT BAR HANGING UNDER DOOR. DURING TROUBLESHOOTING OF DOOR ARM/DISARM SYSTEM, FOUND GIRT BAR RETAINING CLIPS MISSING FROM GIRT EXTENSION. ALLOWING GIRT BAR TO MIGRATE IN Oct 8, 2022 · N665FE · Airbus A300F4605R · Emergency EquipmentSDR FDEA202206011348None · noneRH FWD PAX DOOR FRAME SEGMENT AT FR14C FOUND 2EA CRACKSJun 1, 2022 · N665FE · Airbus A300* · Passenger/Crew DoorsSDR FDEA202206011351None · noneRH WING #5 SPOILER CENTER O/B HINGE ARM O/B SIDE FOUND 2EA DELAMINATIONS. SIZE: (1) 45MM*25MM, DEPTH: 1.57MM (2)45MM*25MM, DEPTH: 1.27MMJun 1, 2022 · N665FE · Airbus A300* · Wing, Control SurfacesSDR FDEA202206011350None · noneLH WING #5 SPOILER CENTER I/B HINGE ARM O/B SIDE FOUND DELAMINATION (SIZE: 20MM*33MM, DEPTH: 1.78MM) AND CENTER I/B & O/B HINGE ARM LWR SURFACE FOUND DELAMINATION (SIZE: (1)18MM*20MM, DEPTH: 2.06MM (2)50MM*40MM, DEPTH: 2.2MM)Jun 1, 2022 · N665FE · Airbus A300* · Wing, Control SurfacesSDR FDEA202206011349None · noneLH WING #3 SPOILER CENTER O/B HINGE ARM O/B SIDE FOUND DELAMINATION (SIZE: 40MM*20MM, DEPTH: 1.9MM) AND CENTER I/B & O/B HINGE ARM LWR SURFACE FOUND DELAMINATION (SIZE: (1)30MM*40MM, DEPTH: 2.6MM (2)30MM*20MM, DEPTH: 2.3MM)Jun 1, 2022 · N665FE · Airbus A300* · Wing, Control SurfacesSDR FDEA202206011347None · noneAFT CARGO COMPT. FLOOR STRUCTURE CROSSBEAM AT FR62 BETWEEN Y140 AND Y300 FOUND CORROSIONJun 1, 2022 · N665FE · Airbus A300* · Fuselage Main, StructureSDR FDEA202008272048Valve · inoperativeLANDING GEAR DID NOT EXTEND. ECAM PROCEDURE LDG GEAR MANUAL EXTENSION. LANDING GEAR DOWN AND LOCKED W/ MANUAL EXT. WHEN GEAR HANDLE WAS PUT DOWN NOTHING HAPPENEDAFTER GO AROUND PERFORMED QRH/ECAM LG GRAVITY EXTENSION. AFTER COMPLETING OF QRH OVERHEAD PANEAug 27, 2020 · N665FE · Airbus A300F4605R · Landing Gear Retraction/Extension SystemSDR FDEA2019120103151Skin · delaminatedRT WING NR 4 SPOILER HINGE ARM AND UPR SURFACE FOUND DELAMINATION. REPAIRED THE RT WING NR 4 SPOILER HINGE ARM AND UPR SURFACE DELAMINATION PER SRM57-72-11/201 PARA 12 AND EA 6-5750-T0350630 P1. TITLE: WING - FLIGHT SURFACE - RT NR 4 SPOILER CENTER HINGE ARMNov 30, 2019 · N665FE · Airbus A300F4605R · SpoilersSDR FDEA2019120103150Skin · delaminatedLT WING NR 5 SPOILER HINGE ARM AND UPR SURFACE FOUND DELAMINATION. REPAIRED THE LT WING NR 5 SPOILER HINGE ARM AND UPR SURFACE DELAMINATION PER SRM57-72-11/201 PARA 12 AND EA 6-5750-T0350601 P1. TITLE: WING - FLIGHT SURFACE - LT NR 5 SPOILER CENTER HINGE ARMNov 30, 2019 · N665FE · Airbus A300F4605R · SpoilersSDR FDEA201911032850Floorbeam · damagedEXISTING REPAIR ON MDCC CROSSBEAM AT FR64 BETWEEN Y953 AND Y1456 REQUIRES EVALUATION FOR CONFORMITY THE EXISTING REPAIR ON MDCC CROSSBEAM AT FR64 BETWEEN Y953 AND Y1456 WAS EVALUATED AND FOUND DID NOT IN CONFORMITY WITH EA: 6-5310-83491. THE REPAIR WAS Nov 3, 2019 · N665FE · Airbus A300F4605R · Fuselage Main, Floor BeamSDR FDEA201911152806None · noneEXISTING REPAIR ON MDCC SEAT TRACK AT Y0 BETWEEN FR53 AND FR54 REQUIRES EVALUATION FOR CONFORMITY THE EXISTING REPAIR ON MDCC SEAT TRACK AT Y0 BETWEEN FR53 AND FR54 WAS EVALUATED. THE REPAIR WAS PERFORMED PER EA: 6-5310-T0322392 A. THE REPAIR BETWEEN FR5Nov 1, 2019 · N665FE · Airbus A300F4605R · Standard Practices/StructuresSDR FDEA201910312791Web · crackedMAIN DECK FR47 -Y953 ~ -Y1456 UNDERFLOOR WEB CRACKED REPAIRED THE MAIN DECK FR47 -Y953 ~ -Y1456 UNDERFLOOR WEB CRACK PER A300-600F SRM53-15-15 FIG201. THIS REPAIR WAS CATEGORY B AND IT MUST BE INSPECTED AT DEFINED INTERVALS PER A300-600F SRI53-15-15-2-002-Oct 31, 2019 · N665FE · Airbus A300F4605R · Fuselage Miscellaneous StructureSDR FDEA201910312790Web · crackedMAIN DECK FR47 Y0 ~ -Y450 UNDERFLOOR WEB CRACKED REPAIRED THE MAIN DECK FR47 Y0 ~ -Y450 UNDERFLOOR WEB CRACK PER A300-600F SRM53- 15-15 FIG201. THIS REPAIR WAS CATEGORY B AND IT MUST BE INSPECTED AT DEFINED INTERVALS PER A300-600F SRI53-15-15-2-002-00. INSPOct 31, 2019 · N665FE · Airbus A300F4605R · Fuselage Miscellaneous StructureSDR FDEA201910252751Floorbeam · crackedMAIN DECK CARGO COMPARTMENT FLOOR STRUCTURE - CROSSBEAM CRACKED, AT FR32, BETWEEN Y1456 AND Y1959 REPAIRED THE MAIN DECK CARGO COMPARTMENT FLOOR STRUCTURE CROSSBEAM CRACK AT FR32 BETWEEN Y1456 AND Y1959 PER A300-600F SRM53-10-15-201 FIGURE 212 & EA: 6-531Oct 25, 2019 · N665FE · Airbus A300F4605R · Fuselage Main, Floor BeamSDR FDEA201910252750Floorbeam · crackedMAIN DECK CARGO COMPARTMENT FLOOR STRUCTURE - CROSSBEAM CRACKED, AT FR31, BETWEEN Y1456 AND Y1959 REPAIRED THE MAIN DECK CARGO COMPARTMENT FLOOR STRUCTURE CROSSBEAM CRACK AT FR31 BETWEEN Y1456 AND Y1959 PER A300-600F SRM53-10-15-201 FIGURE 212 & EA: 6-531Oct 25, 2019 · N665FE · Airbus A300F4605R · Fuselage Main, Floor BeamSDR FDEA201910252749Floorbeam · crackedMAIN DECK CARGO COMPARTMENT FLOOR STRUCTURE - CROSSBEAM CRACKED, AT FR30, BETWEEN Y450 AND Y953 REPAIRED THE MAIN DECK CARGO COMPARTMENT FLOOR STRUCTURE CROSSBEAM CRACK AT FR30 BETWEEN Y450 AND Y953 PER A300-600F SRM53-10-15-201 FIGURE 212 & EA: 6-5310- Oct 25, 2019 · N665FE · Airbus A300F4605R · Fuselage Main, Floor BeamSDR FDEA201910242741Crossbeam · noneEXISTING REPAIR ON MDCC CROSSBEAM AT FR30 BETWEEN -Y450 AND -Y953 REQUIRES EVALUATION FOR CONFORMITY THE EXISTING REPAIR ON MDCC CROSSBEAM AT FR30 BETWEEN -Y450 AND -Y953 WAS EVALUATED. NO REPAIR RECORD WAS FOUND AND THE REPAIR DID NOT SUPPORTED BY CURREOct 24, 2019 · N665FE · Airbus A300F4605R · Fuselage Main, StructureSDR FDEA201910242739Crossbeam · noneEXISTING REPAIR ON MDCC CROSSBEAM AT FR29 BETWEEN -Y450 AND -Y953 REQUIRES EVALUATION FOR CONFORMITY THE EXISTING REPAIR ON MDCC CROSSBEAM AT FR29 BETWEEN -Y450 AND -Y953 WAS EVALUATED. NO REPAIR RECORD WAS FOUND AND THE REPAIR DID NOT SUPPORTED BY CURREOct 24, 2019 · N665FE · Airbus A300F4605R · Fuselage Main, StructureSDR FDEA2019102432731Crossbeam · crackedMAIN DECK CARGO COMPARTMENT FLOOR STRUCTURE - CROSSBEAM CRACKED, AT FR64, BETWEEN -Y1456 AND -Y1959 REPAIRED THE MAIN DECK CARGO COMPARTMENT FLOOR STRUCTURE CROSSBEAM CRACK AT FR64 BETWEEN -Y1456 AND -Y1959 PER A300-600F 53-10-15-201 FIGURE 211. MAJOR REPAOct 23, 2019 · N665FE · Airbus A300F4605R · Fuselage Main, StructureSDR FDEA201811303408Bushing · defectiveR1 DOOR EXTERNAL HANDLE WILL NOT REMAIN LOCKED IN EXTENDED POSITION THAT ALLOWS DOOR TO BE CLOSED FROM OUTSIDE OF AIRCRAFT. INTERNAL OPERATION OF DOOR OR STOWING OF EXTERNAL HANDLE NOT AFFECTED. FACT 06DEC18 18:18 MEM REMOVED AND REPLACED BUSHINGS IN EXTERIOR Nov 30, 2018 · N665FE · Airbus A300F4605R · Passenger/Crew DoorsSDR FDEA201712153397Warning Buzzer · inoperativeMDIS 665 52-70 9733 15DEC17 MEM FACT U RI CREW ENTRY DOOR ESCAPE SLIDE WARNING SYSTEM BUZZER INOP. WARNING LIGHT OPERATE NORMALLY. RELEASED FOR SERVICE PER MEL : 52-73-01-02 CATEGORY : C EXPIRATION : 25DEC17 "MEL 52-73-01-02: R1 CREW ENTRY DDec 15, 2017 · N665FE · Airbus A300F4605R · Escape SlideSDR FDEA201710283089Idg · failedDURING CRUISE FLT, FL 320, NR 1 IDG FAULTED, NR 1 GENERATOR OFF AND AC BUSS 1 FAILED. DOUBLE FAILURE OF GENERATOR 1 AND AC BUSS 1. FOLLOWED ECAM AND QRH, UNABLE TO RECOVER EQUIPMENT ON AC BUSS NR 1. REMOVED AND REPLACED NR 1 ENGINE IDG IAW AMM 24-11-11-0Oct 28, 2017 · N665FE · Airbus A300F4605R · AC Generator-AlternatorSDR FDEA201706201718Processor · inoperativeON APPROACH AFTER EXTENDING LANDING GEAR, NOTICED THERE WERE NO "BRAKE RELEASE" BARS ON ANY OF THE WHEELS. CYCLED BRAKE & ANTI-SKID SWITCH, NO HELP. SELECTED BRAKE & ANTI-SKID SWITCH OFF AS A PRECAUTION. LANDING WAS GOOD. LOST NOSE WHEEL STEERING ON ROJun 20, 2017 · N665FE · Airbus A300F4605R · Landing Gear Position and WarningSDR FDEA201705131405Proximity Sensor · unknownDURING DEPARTURE, LANDING GEAR WOULD NOT RETRACT WITH SYS 1 POSITION DETECTION, SWITCHED TO SYSTEM 2 POSITION DETECTION, STILL WOULD NOT RETRACT, CYCLED SYS 1 AND SYS 2 SEVERAL TIMES, ON FINAL ATTEMPT WITH SYS 2 GEAR RETRACTED. BITE CHECKED PROXIMITY PMay 13, 2017 · N665FE · Airbus A300F4605R · Landing Gear Retraction/Extension SystemSDR FDEA201704271280Stiffener · corrodedFWD LAV PANEL LOWER O/B HAS CORROSION. REMOVED CORRODED STIFFENER PER SRM 51-40-21, LOCATED AND DRILLED HOLES IN NEW STIFFENER, INSTALLED NEW STIFFENER IAW SRM 51-40-21, PAINTED AREA EXTERNAL SKIN IAW SRM 51-75-10, CLASSIFIED AS MAJOR REPAIR.Apr 27, 2017 · N665FE · Airbus A300F4605R · Fuselage Main, Plate/SkinSDR FDEA201704141185Floor Panel · damagedMAIN CARGO FLOOR PANEL 231SG HAS MULTIPLE HOLES. FABRICATED FLOOR PANEL 231SG ON T17/1268908 IAW SRZ-25-005. CLASSIFIED AS CAT "A" MAJOR REPAIR.Apr 14, 2017 · N665FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201704141199Floor Panel · crackedMAIN CARGO FLOOR PANEL 242AJ HAS A CRACK AT THE FASTENER HOLE. FABRICATED A NEW FLOOR PANEL IAW SRZ-25-005. MAJOR REPAIRApr 14, 2017 · N665FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201704141194Frame · dentedMAIN CABIN, FRAME 58 BETWEEN STRINGER 13L AND 14L DENTED AND GOUGED. REMOVED DAMAGE IAW SRM 53-10-13 FIG 202. FABRICATED A REPAIR ANGLE, TREATED AND PRIMED THE REPAIR ANGLE IAW SRM 51- 21-10. INSTALLED THE REPAIR ANGLE IAW SRM 53-10-13 FIG 202 MAJOR REPAApr 14, 2017 · N665FE · Airbus A300F4605R · Fuselage Main, FrameSDR FDEA201704141186Floor Panel · crackedMAIN CABIN FLOOR PANEL 221PF CRACKED. FABRICATED A NEW FLOOR PANEL. MAJOR REPAIRApr 14, 2017 · N665FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201704131179Floor Panel · delaminatedAFT CARGO BAY FLOOR PANEL 152TF EDGE DELAMINATED. A NEW FLOOR PANEL WAS FABRICATED IAW SRZ-25-005. MAJOR REPAIR.Apr 13, 2017 · N665FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201704131178Floor Panel · brokenAFT CARGO BAY FLOOR PANEL 151SF BROKEN ON THE CORNER. A NEW FLOOR PANEL WAS FABRICATED IAW SRZ-25-005. MAJOR REPAIR.Apr 13, 2017 · N665FE · Airbus A300F4605R · Fuselage Floor Panel
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