# Service difficulty reports: N674FE A list on [N674FE](https://openairdocs.org/aircraft/N674FE.md). Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first. Page 1 of 7 · 345 reports - [SDR FDEA202602210251](https://openairdocs.org/sdr/FDEA202602210251.md): Block · failed · Feb 21, 2026 · N674FE · Airbus A300F4605R · Drag Control System > DURING LIGHT TURBULENCE, GOT A SPLR 6 FAULT. SPOILER 6 WAS STUCK IN THE DEPLOYED POSITION. QRH PROCEDURE WAS UNSUCCESSFUL WITH RETRACTION. EMERGENCY WAS DECLARED FOR FLIGHT CONTROL ISSUES. TSM: 27-61-00 TSM: 27-61-04 MEL: 27-61-01-B COULD NOT GET #6 SPO - [SDR FDEA202602140205](https://openairdocs.org/sdr/FDEA202602140205.md): Safety Wire · wrong part · Feb 14, 2026 · N674FE · Airbus A300F4605R · Escape Slide > L1 DOOR SLIDE REQUIRES CAD COPPER SAFETY WIRE ON EJECTOR BAG RELEASE CABLE ARM CLIP PER FEA 6-2560-F0386375 A P1. REF WRI 25-60/7721 FACT 14FEB26 22:05 MEM FEA: 6-2560-F0386375 A P1 CMM: 25-60-40 SAFTIED L1 DOOR SLIDE EJECTOR BAG RELEASE CABLE ARM C - [SDR FDEA202510091933](https://openairdocs.org/sdr/FDEA202510091933.md): Arming Lever · stuck · Oct 9, 2025 · N674FE · Airbus A300F4605R · Passenger/Crew Doors > WHEN SECURING AIRCRAFT DOORS BEFORE DEPARTURE, LEFT / CAPTAINS SIDE DOOR ARMING LEVER WOULD NOT MOVE FULLY TO THE ARMED POSITION. LEVER WOULD MOVE SOME AND ECAM DOORS PAGE SHOWED SLIDE BUT LEVER WAS NOT IN ARMED POSITION. REMOVED GIRT BAR AND REINSTALLED - [SDR FDEA202504020549](https://openairdocs.org/sdr/FDEA202504020549.md): Pressure Panel · corroded · Apr 2, 2025 · N674FE · Airbus A300F4605R · Fuselage Main, Structure > BAY AFT OF FWD CARGO COMPARTMENT - HORIZONTAL PRESSURE DECK UPR SURFACE BETWEEN FR39 AND FR40 RH SIDE O/B OF -Y2354 FOUND CORROSION COMPLIED WITH EA 6-5310-T0382790 P1. TITLE: FUSELAGE - MAINFRAME - EXFOLIATED CORROSION ON HORIZONTAL PRESSURE FLOOR PANEL B - [SDR FDEA202504020548](https://openairdocs.org/sdr/FDEA202504020548.md): Pressure Deck · corroded · Apr 2, 2025 · N674FE · Airbus A300F4605R · Fuselage Main, Structure > BAY AFT OF FWD CARGO COMPARTMENT - HORIZONTAL PRESSURE DECK UPR SURFACE BETWEEN FR39 AND FR40 LH SIDE O/B OF Y2354 FOUND CORROSION COMPLIED WITH EA 6-5310-T0382790 P1. TITLE: FUSELAGE - MAINFRAME - EXFOLIATED CORROSION ON HORIZONTAL PRESSURE FLOOR PANEL BT - [SDR FDEA202503310540](https://openairdocs.org/sdr/FDEA202503310540.md): Fitting · damaged · Mar 31, 2025 · N674FE · Airbus A300F4605R · Cargo/Baggage Doors > COMPLY WITH EO 6-5230-E0378588 B P5 FOR MAIN DECK CARGO DOOR ACTUATOR BEARING FITTINGS REPLACEMENT COMPLIED WITH EO 6-5230-E0378588 B P5. TITLE: DOORS - CARGO DOOR/HYD SYS - DETAILED VISUAL INSPECTION OF THE MAIN DECK CARGO DOOR (MDCD) ACTUATOR BEARING FIT - [SDR FDEA202503250490](https://openairdocs.org/sdr/FDEA202503250490.md): Seat Track · none · Mar 25, 2025 · N674FE · Airbus A300F4605R · Standard Practices/Structures > MAIN DECK CARGO COMPARTMENT - EXISTING SEAT TRACK REPAIR AT Y2462 BETWEEN FR18 AND FR27 REQUIRES EVALUATION TO DETERMINE IF MAJOR OR MINOR AND IF REPAIR CONFORMS TO FAA APPROVED DATA. THE EXISTING REPAIR ON MAIN DECK CARGO COMPARTMENT SEAT TRACK AT Y2462 B - [SDR FDEA202503250489](https://openairdocs.org/sdr/FDEA202503250489.md): Bracket · none · Mar 25, 2025 · N674FE · Airbus A300F4605R · Fuselage Miscellaneous Structure > MAIN DECK CARGO COMPARTMENT - EXISTING THRUST BRACKET REPAIR AT Y953 TO Y1456 BETWEEN FR27 AND FR28 REQUIRES EVALUATION TO DETERMINE IF MAJOR OR MINOR AND IF THE REPAIR CONFORMS TO FAA APPROVED DATA THE EXISTING REPAIR ON MAIN DECK CARGO COMPARTMENT THRUST - [SDR FDEA202503200462](https://openairdocs.org/sdr/FDEA202503200462.md): Skin · cracked · Mar 20, 2025 · N674FE · Airbus A300F4605R · Cargo/Baggage Doors > FWD CARGO DOOR INNER SKIN AT FR22-22A, BEAM1-2 CRACKED. COMPLIED WITH EA:6-5230-T0382660 P1. TITLE: DOORS - CARGO DOOR/HYD SYS - FWD CARGO DOOR - CRACK ON INNER SKIN FWD OF FR22A BELOW BEAM #1. REPAIRED THE FWD CARGO DOOR CRACKED INNER SKIN AT FR22-22A, B - [SDR FDEA202503200461](https://openairdocs.org/sdr/FDEA202503200461.md): Seat Track · corroded · Mar 20, 2025 · N674FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach Fittings > MDCC SEAT TRACK CORRODED, AT FR77-80, Y0. REPAIRED THE CORRODED SEAT TRACK IN MDCC AT FR77-80, Y0 PER SRM 53-10-16-201 PARA.4. THIS WAS CATEGORY A REPAIR. MAJOR REPAIR IAW GMM6-2-100. - [SDR FDEA202503200460](https://openairdocs.org/sdr/FDEA202503200460.md): Fitting · cracked · Mar 20, 2025 · N674FE · Airbus A300F4605R · Fuselage Main, Frame > CENTER 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 TO REPAIR THE CENTER WING BOX REAR SPAR AND BOTTOM PANEL AT JUNCTION WITH FUSELAGE - [SDR FDEA202503200459](https://openairdocs.org/sdr/FDEA202503200459.md): Fitting · cracked · Mar 20, 2025 · N674FE · Airbus A300F4605R · Fuselage Miscellaneous Structure > CENTER WING BOX - INSPECTION OF REAR SPAR AND BOTTOM PANEL AT JUNCTION WITH FUSELAGE FR47 RH SIDE, FASTENER "I" HOLE FOUND CRACK SIGNAL COMPLIED WITH EO 6-5710-E0342809 D P2 TO REPAIR THE CENTER WING BOX REAR SPAR AND BOTTOM PANEL AT JUNCTION WITH FUSELAGE - [SDR FDEA202503160430](https://openairdocs.org/sdr/FDEA202503160430.md): Crossbeam · misrepaired · Mar 16, 2025 · N674FE · Airbus A300F4605R · Fuselage Main, Structure > EXISTING REPAIR ON MAIN DECK CARGO COMPARTMENT FR30 CROSSBEAM BETWEEN -Y450 AND -Y953 REQUIRES EVALUATION FOR CONFORMITY THE EXISTING REPAIR ON MAIN DECK CARGO COMPARTMENT FR30 CROSSBEAM BETWEEN -Y450 AND -Y953 WAS EVALUATED AND FOUND NOT IN CONFORMITY WIT - [SDR FDEA202503160429](https://openairdocs.org/sdr/FDEA202503160429.md): Crossbeam · none · Mar 16, 2025 · N674FE · Airbus A300F4605R · Fuselage Main, Structure > EXISTING REPAIR ON MAIN DECK CARGO COMPARTMENT FR29 CROSSBEAM BETWEEN -Y450 AND -Y953 REQUIRES EVALUATION FOR CONFORMITY THE EXISTING REPAIR ON MAIN DECK CARGO COMPARTMENT FR29 CROSSBEAM BETWEEN -Y450 AND -Y953 WAS EVALUATED AND FOUND NOT IN CONFORMITY WIT - [SDR FDEA202503150587](https://openairdocs.org/sdr/FDEA202503150587.md): Attach Fitting · cracked · Mar 15, 2025 · N674FE · Airbus A300F4605R · Cargo/Baggage Doors > AFT CARGO DOOR - FR61A ACTUATOR ATTACH FITTING FOUND CRACK REPLACED THE AFT CARGO DOOR - FR61A ACTUATOR ATTACH FITTING PER A300-600F SRM51-40- 21 & EA:6-5230-T0382975 P1,EA TITLE: DOORS - CARGO DOORS/HYD SYSTEMS - LOCAL FABRICATION AND REPLACEMENT OF FRAME - [SDR FDEA202503150423](https://openairdocs.org/sdr/FDEA202503150423.md): Hinge Arm · delaminated · Mar 15, 2025 · N674FE · Airbus A300F4605R · Spoilers > RH WING #3 SPOILER CENTER O/B HINGE ARM OUTSIDE SURFACE SKIN FOUND DELAMINATION. SIZE: 50MM*30MM, DEPTH: 0.81MM, CENTER I/B HINGE ARM OUTSIDE SURFACE SKIN FOUND DELAMINATION. SIZE: 53MM*30MM, DEPTH: 1.14MM COMPLIED WITH EA:6-5750-T0382593 P1 TO REPAIR RH W - [SDR FDEA202503150422](https://openairdocs.org/sdr/FDEA202503150422.md): Hinge Arm · delaminated · Mar 15, 2025 · N674FE · Airbus A300F4605R · Spoilers > LH WING #3 SPOILER CENTER O/B HINGE ARM OUTSIDE SURFACE SKIN FOUND DELAMINATION. SIZE: 30MM*17MM, DEPTH: 0.76MM COMPLIED WITH EA:6-5750-T0382592 P1 TO REPAIR LH WING #3 SPOILER CENTER O/B HINGE ARM OUTSIDE SURFACE SKIN DELAMINATION, EA TITLE: WING - FLIGHT - [SDR FDEA202503150421](https://openairdocs.org/sdr/FDEA202503150421.md): Skin · damaged · Mar 15, 2025 · N674FE · Airbus A300F4605R · Trailing Edge Flaps > RH WING O/B FLAP UPPER SKIN AT T/E RIB14A-15A WORN, AS MARKING. REPAIRED THE RH WING O/B FLAP WORN UPPER SKIN AT T/E RIB14A-15A PER A300-600F SRM51- 75-20 & EA 6-5750-T0382575 P1, EA TITLE: WING - FLIGHT SURFACES - RH OUTER FLAP TRAILING EDGE UPPER SKIN WEA - [SDR FDEA202503150420](https://openairdocs.org/sdr/FDEA202503150420.md): Web · cracked · Mar 15, 2025 · N674FE · Airbus A300F4605R · Fuselage Miscellaneous Structure > MDCC UNDERFLOOR 1EA WEB AT FR47, Y-953 - Y-1456 CRACKED. REPAIRED THE MDCC UNDERFLOOR CRACKED WEB AT FR47, Y-953 - Y-1456 PER A300-600F SRM53-15-15-201 FIG.201. THIS REPAIR WAS CATEGORY B AND IT MUST BE INSPECTED AT DEFINED INTERVALS PER A300-600F SRI53-1 - [SDR FDEA202503150419](https://openairdocs.org/sdr/FDEA202503150419.md): Web · cracked · Mar 15, 2025 · N674FE · Airbus A300F4605R · Fuselage Miscellaneous Structure > MDCC UNDERFLOOR 1EA WEB AT FR47, Y953 - Y1456 CRACKED. REPAIRED THE MDCC UNDERFLOOR CRACKED WEB AT FR47, Y953 - Y1456 PER A300-600F SRM53-15-15-201 FIG.201. THIS REPAIR WAS CATEGORY B AND IT MUST BE INSPECTED AT DEFINED INTERVALS PER A300-600F SRI53-15-15- - [SDR FDEA202503150418](https://openairdocs.org/sdr/FDEA202503150418.md): Web · cracked · Mar 15, 2025 · N674FE · Airbus A300F4605R · Fuselage Miscellaneous Structure > MDCC UNDERFLOOR 1EA WEB AT FR47, Y0 - Y-450 CRACKED. REPAIRED THE MDCC UNDERFLOOR CRACKED WEB AT FR47, Y0 - Y-450 PER A300-600F SRM53-15-15-201 FIG.201. THIS REPAIR WAS CATEGORY B AND IT MUST BE INSPECTED AT DEFINED INTERVALS PER A300-600F SRI53-15-15-2-0 - [SDR FDEA202503150417](https://openairdocs.org/sdr/FDEA202503150417.md): Web · cracked · Mar 15, 2025 · N674FE · Airbus A300F4605R · Fuselage Miscellaneous Structure > MDCC UNDERFLOOR 1EA WEB AT FR47, Y0 - Y450 CRACKED. REPAIRED THE MDCC UNDERFLOOR CRACKED WEB AT FR47, Y0 - Y450 PER A300-600F SRM53-15-15-201 FIG.201. THIS REPAIR WAS CATEGORY B AND IT MUST BE INSPECTED AT DEFINED INTERVALS PER A300-600F SRI53-15-15-2-002- - [SDR FDEA202503140556](https://openairdocs.org/sdr/FDEA202503140556.md): Frame · misrepaired · Mar 14, 2025 · N674FE · Airbus A300F4605R · Fuselage Main, Frame > EXISTING REPAIR ON FUSELAGE FRAME AT FR20A S37R - S42R REQUIRES EVALUATION FOR CONFORMITY THE EXISTING REPAIR ON FUSELAGE FRAME AT FR20A S37R - S42R WAS EVALUATED AND FOUND NOT IN CONFORMITY WITH DRAWING SR30-53-001 REV.D AND SRM 53-13-13-201 FIG 201. T - [SDR FDEA202503140411](https://openairdocs.org/sdr/FDEA202503140411.md): Crossbeam · misrepaired · Mar 14, 2025 · N674FE · Airbus A300F4605R · Fuselage Main, Structure > EXISTING REPAIR ON MAIN DECK CARGO COMPARTMENT FR64 CROSSBEAM BETWEEN Y953 AND Y1456 REQUIRES EVALUATION FOR CONFORMITY THE EXISTING REPAIR ON MAIN DECK CARGO COMPARTMENT FR64 CROSSBEAM BETWEEN Y953 AND Y1456 WAS EVALUATED AND FOUND NOT IN CONFORMITY WITH - [SDR FDEA202503140405](https://openairdocs.org/sdr/FDEA202503140405.md): Seat Track · misrepaired · Mar 14, 2025 · N674FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach Fittings > EXISTING REPAIR ON MAIN CARGO COMPARTMENT FR57.1 - FR57.3 SEAT TRACK AT Y1456 REQUIRES EVALUATION FOR CONFORMITY EXISTING REPAIR ON MAIN DECK CARGO COMPARTMENT FR57.1 - 57.3 SEAT TRACK AT Y1456 WAS EVALUATED AND FOUND NOT IN CONFORMITY WITH A300-600F SRM 5 - [SDR FDEA202503140404](https://openairdocs.org/sdr/FDEA202503140404.md): Repair · none · Mar 14, 2025 · N674FE · Airbus A300F4605R · Standard Practices/Structures > EXISTING REPAIR ON MAIN DECK CARGO COMPARTMENT FR57.2 - FR59 SEAT TRACK AT Y1456 REQUIRES EVALUATION FOR CONFORMITY THE EXISTING REPAIR ON MAIN DECK CARGO COMPARTMENT FR57.2 - FR59 SEAT TRACK AT Y1456 WAS EVALUATED AND FOUND IN CONFORMITY WITH A300-600F SR - [SDR FDEA202503140403](https://openairdocs.org/sdr/FDEA202503140403.md): Repair · none · Mar 14, 2025 · N674FE · Airbus A300F4605R · Standard Practices/Structures > EXISTING REPAIR ON MAIN DECK CARGO COMPARTMENT FR74 - FR77 SEAT TRACK AT Y1137.1 REQUIRES EVALUATION FOR CONFORMITY THE EXISTING REPAIR ON MAIN DECK CARGO COMPARTMENT FR74 - FR77 SEAT TRACK AT Y1137.1 WAS EVALUATED AND FOUND IN CONFORMITY WITH A300-600F SR - [SDR FDEA202503140402](https://openairdocs.org/sdr/FDEA202503140402.md): Repair · none · Mar 14, 2025 · N674FE · Airbus A300F4605R · Standard Practices/Structures > EXISTING REPAIR ON MAIN CARGO COMPARTMENT FR65 - FR69 SEAT TRACK AT -Y1456 REQUIRES EVALUATION FOR CONFORMITY THE EXISTING REPAIR ON MAIN DECK CARGO COMPARTMENT FR65 - FR69 SEAT TRACK AT - Y1456 WAS EVALUATED AND FOUND IN CONFORMITY WITH A300-600F SRM 53-1 - [SDR FDEA202503140401](https://openairdocs.org/sdr/FDEA202503140401.md): Seat Track · none · Mar 14, 2025 · N674FE · Airbus A300F4605R · Standard Practices/Structures > EXISTING REPAIR ON MAIN DECK CARGO COMPARTMENT FR26 - FR30 SEAT TRACK AT -Y953 REQUIRES EVALUATION FOR CONFORMITY. THE EXISTING REPAIR ON MAIN DECK CARGO COMPARTMENT FR26 - FR30 SEAT TRACK AT -Y953 WAS EVALUATED AND FOUND IN CONFORMITY WITH A300-600F SRM5 - [SDR FDEA202503140400](https://openairdocs.org/sdr/FDEA202503140400.md): Seat Track · none · Mar 14, 2025 · N674FE · Airbus A300F4605R · Standard Practices/Structures > EXISTING REPAIR ON MAIN DECK CARGO COMPARTMENT FR26-FR30 SEAT TRACK AT -Y450 REQUIRES EVALUATION FOR CONFORMITY. THE EXISTING REPAIR ON MAIN DECK CARGO COMPARTMENT FR26 - FR30 SEAT TRACK AT -Y450 WAS EVALUATED AND FOUND IN CONFORMITY WITH A300-600F SRM53- - [SDR FDEA202503140399](https://openairdocs.org/sdr/FDEA202503140399.md): Repair · none · Mar 14, 2025 · N674FE · Airbus A300F4605R · Standard Practices/Structures > EXISTING REPAIR ON MAIN DECK CARGO COMPARTMENT FR71-FR73 SEAT TRACK AT Y0 REQUIRES EVALUATION FOR CONFORMITY THE EXISTING REPAIR ON MAIN DECK CARGO COMPARTMENT FR71-FR73 SEAT TRACK AT Y0 WAS EVALUATED AND FOUND IN CONFORMITY WITH A300-600F SRM53-10-16-201 - [SDR FDEA202503140398](https://openairdocs.org/sdr/FDEA202503140398.md): Skin · misrepaired · Mar 14, 2025 · N674FE · Airbus A300F4605R · Fuselage Main, Plate/Skin > EXISTING REPAIR ON FUSELAGE SKIN FR19-FR20A S37R-S42R REQUIRES EVALUATION FOR CONFORMITY THE EXISTING REPAIR ON FUSELAGE SKIN FR19 - FR20A S37R - S42R WAS EVALUATED AND FOUND NOT IN CONFORMITY WITH FEDEX DRAWING S30-53-001 REV.D AND A300-600F SRM 53-13-1 - [SDR FDEA202503140397](https://openairdocs.org/sdr/FDEA202503140397.md): Skin · misrepaired · Mar 14, 2025 · N674FE · Airbus A300F4605R · Fuselage Main, Plate/Skin > EXISTING REPAIR ON FUSELAGE SKIN FR61-FR64 S42L-S45L REQUIRES EVALUATION FOR CONFORMITY. EXISTING REPAIR ON FUSELAGE SKIN FR61 - FR64 S42L - S45L WAS EVALUATED AND FOUND NOT IN CONFORMITY WITH A300-600 SRM 53-10-12 FIG 213. DUE TO SOME DEVIATIONS WERE FOUN - [SDR FDEA202503140396](https://openairdocs.org/sdr/FDEA202503140396.md): Crossbeam · none · Mar 14, 2025 · N674FE · Airbus A300F4605R · Fuselage Main, Structure > EXISTING REPAIR ON MAIN CARGO COMPARTMENT FR64 CROSSBEAM BETWEEN -Y1456 AND -Y1959 REQUIRES EVALUATION FOR CONFORMITY THE EXISTING REPAIR ON MAIN DECK CARGO COMPARTMENT FR64 CROSSBEAM BETWEEN -Y1456 AND -Y1959 WAS EVALUATED AND FOUND NOT IN COMFORMITY WITH A - [SDR FDEA202503140395](https://openairdocs.org/sdr/FDEA202503140395.md): Crossbeam · misrepaired · Mar 14, 2025 · N674FE · Airbus A300F4605R · Fuselage Main, Structure > EXISTING REPAIR ON MAIN DECK CARGO COMPARTMENT FR31 CROSSBEAN BETWEEN Y1456 AND Y1959 REQUIRES EVALUATION CONFORMITY THE EXISTING REPAIR ON MAIN DECK CARGO COMPARTMENT FR31 CROSSBEAM BETWEEN Y1456 AND Y1959 WAS EVALUATED AND FOUND NOT IN COMFORMITY WITH A3 - [SDR FDEA202503140394](https://openairdocs.org/sdr/FDEA202503140394.md): Skin · misrepaired · Mar 14, 2025 · N674FE · Airbus A300F4605R · Standard Practices/Structures > EXISTING REPAIR ON FUSELAGE SKIN FR59-FR60 S38R-S41R REQUIRES EVALUATION FOR CONFORMITY THE EXISTING REPAIR ON FUSELAGE SKIN FR59 - FR60 S38R - S41R WAS EVALUATED AND FOUND NOT IN CONFORMITY WITH A300-600F SRM 53-17-12-201-2 FIG 201. REPAIRED IT PER A300-6 - [SDR FDEA202501270139](https://openairdocs.org/sdr/FDEA202501270139.md): Bottle · low pressure · Jan 27, 2025 · N674FE · Airbus A300F4605R · Passenger/Crew Doors > R/H PASSENGER DOOR DAMPER/EMERGENCY OPERATION CYLINDER REQUIRES SERVICING. AMM: 52-10-14-03-02 SERVICED R/H DOOR DAMPER/EMERGENCY OPERATION CYLINDER PER AMM: 52-10-14-03-02. NO DEFECTS NOTED. - [SDR FDEA202402210254](https://openairdocs.org/sdr/FDEA202402210254.md): Pin · misinstalled · Feb 21, 2024 · N674FE · Airbus A300F4605R · Service Doors > RIGHT CABIN ENTRY DOOR, DOOR PIN MISSING GROMMET WHICH DOESN T ALLOWING DOOR ARMING LEVER TO ALIGN CORRECTLY. NO REFERENCE REQUIRED CORRECTLY CONFIGURED PIN AS NEEDED AND REINSTALLED PIN. OPS CHECKS NORMAL. AIRCRAFT OKAY TO CONTINUE SERVICE. - [SDR FDEA202402130185](https://openairdocs.org/sdr/FDEA202402130185.md): Seat Track · damaged · Feb 13, 2024 · N674FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach Fittings > SEAT TRACK DAMAGE UNDER MAIN CARGO LOCK MC1467. REMOVED AND REPLACED DAMAGED SECTION OF SEAT TRACK, REF A300 SRM 53-10-16 FIG 201 - [SDR FDEA202301290172](https://openairdocs.org/sdr/FDEA202301290172.md): Slide · none · Jan 29, 2023 · N674FE · Airbus A300F4605R · Escape Slide > L1 DOOR SLIDE PRESSURE IN THE RED DURING POST FLIGHT INSP. INSPECTED L1 DOOR SLIDE AND FOUND WHITE NEEDLE WITHIN THE LIMITS OF GREEN TEMPERATURE COMPENSATED MOVABLE CURSOR REF A300 MM 25-61-20-06-01 STEP 1-C-2-A, ALSO FIG 601. NO MAINTENANCE REQUIRED, ACFT - [SDR FDEA202211232830](https://openairdocs.org/sdr/FDEA202211232830.md): Jackscrew · contaminated · Nov 23, 2022 · N674FE · Airbus A300F4605R · Leading Edge Slat Control System > AT 6000 FT & 210 KNOTS ATTEMPTED TO EXTEND SLATS INFLT. SLATS FAILED TO EXTEND WITH ECAM & ASSOCIATED CHIME. ECAM SHOWED SLATS SYS 1 & 2 FAULTED. FOLLOWED ECAM PROCEDURE WITH NO SUCCESS. RAN QRH & ABLE TO GET FLAPS TO 40 DEGREES WITH SLATS RETRACTED. LANDE - [SDR FDEA202210092521](https://openairdocs.org/sdr/FDEA202210092521.md): None · none · Oct 9, 2022 · N674FE · Airbus A300* · Fuselage Main, Structure > MAIN DECK CARGO COMPARTMENT FLOOR STRUCTURE - CROSS BEAM CRACKED AT FR27, BETWEEN Y-450 AND Y-953. - [SDR FDEA202210012429](https://openairdocs.org/sdr/FDEA202210012429.md): Hinge Arm · delaminated · Oct 1, 2022 · N674FE · Airbus A300F4605R · Spoilers > RH WING - #5 SPOILER CENTER O/B HINGE ARM LOWER SURFACE FOUND DELAMINATION (AREA: 22MM*35MM,DEPTH:2.0MM) AND CENTER I/B HINGE ARM LOWER SURFACE FOUND DELAMINATION (AREA: 11MM*15MM,DEPTH: 2.3MM). COMPLIED WITH EA:6-5750-T0370909 P1. TITLE:WING - FLIGHT SURF - [SDR FDEA202210012427](https://openairdocs.org/sdr/FDEA202210012427.md): Hinge Arm · delaminated · Oct 1, 2022 · N674FE · Airbus A300F4605R · Spoilers > LH WING - #5 SPOILER CENTER O/B HINGE ARM LOWER SURFACE FOUND DELAMINATION. (AREA: 30MM*45MM,DEPTH:2.59MM) COMPLIED WITH EA:6-5750-T0370908 P1. THIS IS CAT A REPAIR. MINOR REPAIR IAW FEDEX GMM 6 6082 RO3 CONFIGURATION, SO THE DAMAGE IS WITHIN THE ALLOWABL - [SDR FDEA202209302400](https://openairdocs.org/sdr/FDEA202209302400.md): Rib · dented · Sep 30, 2022 · N674FE · Airbus A300F4605R · Leading Edge Devices > LH WING - #3 SLAT RIB7 L/E SKIN (ADJACENT TO TRACK RIB8 SKIN PATCH) 1EA DENT WAS FOUND. PERFORMED THE REPAIR ON LH SLAT 3 LEADING EDGE SKIN BETWEEN RIB 7 AND 8 AS PER FEDEX EA #: 6-5750-T0371151 P1, THIS REPAIR WAS CLASSIFIED AS A CAT C REPAIR PER AIRBUS R - [SDR FDEA202209302399](https://openairdocs.org/sdr/FDEA202209302399.md): Floorbeam · cracked · Sep 30, 2022 · N674FE · Airbus A300F4605R · Fuselage Main, Floor Beam > MAIN DECK CARGO COMPARTMENT FLOOR STRUCTURE - CROSS BEAM CRACKED AT FR32, BETWEEN Y1456 AND 1959. - [SDR FDEA202209302398](https://openairdocs.org/sdr/FDEA202209302398.md): Crossbeam · cracked · Sep 30, 2022 · N674FE · Airbus A300F4605R · Fuselage Main, Structure > E/E COMPT FR15A LH CROSS BEAM ON NLG WEB FACE FOUND CRACKED. REPAIRED THE CRACK ON NLG FR15A CROSSBEAM WEB FACE AT ATTACHMENT FITTING OF RACK 107VU PER FEDEX A300-600F SRM 51-40-21 AND EA:6-5310-T0370840 P1. TITLE: FUSELAGE - MAINFRAME - SB A300-53-6164 - - [SDR FDEA202204150963](https://openairdocs.org/sdr/FDEA202204150963.md): None · failed · Apr 15, 2022 · N674FE · Airbus A300* · Emergency Lighting > MDIS 674 33-50 3860 15APR22 ABE OPEN U COURIER AREA EMERGENCY LIGHTS TEST PUSHSWITCH DOES NOT ILLUMINATE DURING TEST. FACT 15APR22 17:01 ABE AMM: 33-51-14-04 - [SDR FDEA202204050854](https://openairdocs.org/sdr/FDEA202204050854.md): Brake · overtemp · Apr 5, 2022 · N674FE · Airbus A300F4605R · Landing Gear Brake System > CLIMBING, 12,000 FEET, ECAM FOR HOT BRAKES W/ WHEELS PAGE, NR 1 BRAKE TEMP AT 310. ECAM DIRECTED GEAR EXTENDED & BRAKE FANS ON. BY THE TIME GEAR EXTENDED, NR 1 BRAKE TEMP 325 & CLIMBING. HIGHEST TEMP ON OTHER BRAKES 75. RETRACTED GEAR WHEN TEMP DOWN TO 175 - [SDR FDEA202110192577](https://openairdocs.org/sdr/FDEA202110192577.md): Pylon · corroded · Oct 19, 2021 · N674FE · Airbus A300* · Engine Mount Section > #2 ENGINE FWD SPIGOT HOLE HAS TWO POT HOLES ON FWD UPR SIDE REPAIRED PER SRM 54-51-81BUSHING REPAIR Next page: https://openairdocs.org/aircraft/N674FE/reports.md?page=2 ## The whole list in SQL Runs in DuckDB 1.2 or later on the release's Parquet files over HTTPS: ```sql 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 = 'N674FE' AND registry_match = 'registration' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/aircraft/N674FE/reports --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.