# Service difficulty reports: Airbus A300 F4-605R

A list on [Airbus A300 F4-605R](https://openairdocs.org/model/airbus-a300-f4-605r.md).

Newest first. General aviation reporting is voluntary.

Page 1 of 184 · 9,199 reports

- [SDR FDEA202611011712](https://openairdocs.org/sdr/FDEA202611011712.md): Smoke Detector · failed · Nov 1, 2026 · N657FE · Airbus A300F4605R · Smoke Detection
  > MDIS 657 26-12 9422 01NOV26 19:41 MEM FACT AVIONICS SMOKE DETECTION ALERT DURING MX PRE-FLT FACT 01NOV26 20:34 MEM AMM 26-15-12-04 WITH REF ABOVE. REMOVED AND REPLACED AVIONICS COMPARTMENT SMOKE DETECTOR UNIT 13WA. OPS CHECK GOOD. A/C OK FO
- [SDR FDEA202610231680](https://openairdocs.org/sdr/FDEA202610231680.md): Switch · damaged · Oct 23, 2026 · N672FE · Airbus A300F4605R · Landing Gear Selector
  > SELECTED LANDING GEAR HANDLE DOWN AT 170KTS, 2300FT, DESCENDING ON THE 16R GLIDE SLOPE AT SLC, & NOTHING HAPPENED. NO AIR NOISE, NO LANDING GEAR DOOR INDICATION, RECEIVED 3 RED UNLK LIGHTS ON THE LANDING GEAR INDICATOR. PERFORMED A DISCONTINUED APPROACH, WI
- [SDR FDEA202610151590](https://openairdocs.org/sdr/FDEA202610151590.md): Hydraulic System · low quantity · Oct 15, 2026 · N665FE · Airbus A300F4605R · Hydraulic System, Main
  > DURING 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.
- [SDR FDEA202610041482](https://openairdocs.org/sdr/FDEA202610041482.md): Structure · cracked · Oct 4, 2026 · N670FE · Airbus A300F4605R · Cargo/Baggage Doors
  > MAIN DECK CARGO DOOR UPPER EDGE AT PT1 BTWN FR 22 & 25, FOUND CRACK SIGNAL AT 2 EA FASTENER HOLES. COMPLIED WITH EA 6-5230-T0388992 P1 REPAIR MAIN DECK CARGO DOOR UPR EDGE AT PT1 BETWEEN FR22 AND FR25 2EA CRACK HOLES. EA TITLE: DOORS - CARGO DOOR/HYD SYS -
- [SDR FDEA202609281443](https://openairdocs.org/sdr/FDEA202609281443.md): Fitting · damaged · Sep 28, 2026 · N670FE · Airbus A300F4605R · Cargo/Baggage Doors
  > COMPLY WITH EO 6-5230-E0378588 C P5. DOORS - CARGO DOOR/HYD SYS - DETAILED VISUAL INSPECTION OF THE MAIN DECK CARGO DOOR (MDCD) ACTUATOR BEARING FITTINGS AT FRAME 23 AND 24 - AOT A52W016-24. COMPLIED WITH EO 6-5230-E0378588 C P5. TITLE: DOORS - CARGO DOO
- [SDR FDEA202609221405](https://openairdocs.org/sdr/FDEA202609221405.md): Stiffener · corroded · Sep 22, 2026 · N670FE · Airbus A300F4605R · Fuselage Main, Plate/Skin
  > TOILET SERVICE ACCESS PANEL FWD LOWER CUTOUT CORRODED. REPLACED THE CORRODED STIFFENER AT TOILET SERVICE ACCESS PANEL FWD LOWER CUTOUT PER A300-600F SRM51-40-21 & DWG.A53612375(ISSUE.K). THIS IS CAT A REPAIR. MAJOR REPAIR IAW FEDEX GMM6-2-100.
- [SDR FDEA202609221403](https://openairdocs.org/sdr/FDEA202609221403.md): Rib · cracked · Sep 22, 2026 · N670FE · Airbus A300F4605R · Trailing Edge Flaps
  > RIGHT WING CENTER FLAP RIB UPR FLANGE FOUND CRACK AT RIB15 BETWEEN STRINGERS 2.6, 2.7, & 2.8. CLASSIFIED AS MAJOR REPAIR IAW GMM 6-2-100 I.A.W EA T6-5750-T0378801 P1, SEQ 1119, LT CENTER FLAP WITH OVERSIZED HOLE ON UPPER SKIN AT RIB 11. REPAIRED IAW GMM6-2
- [SDR FDEA202609221402](https://openairdocs.org/sdr/FDEA202609221402.md): Rib · cracked · Sep 22, 2026 · N670FE · Airbus A300F4605R · Trailing Edge Flaps
  > LEFT WING CENTER FLAP RIB UPPER FLANGE FOUND CRACKED AT RIB 26 BETWEEN STGR2.6 AND STGR2.7. COMPLIED WITH EA 6-5750-T0388894 P1 REPAIR LT WING CENTER FLAP UPR FLANGE CRACK. THIS IS CAT A REPAIR. MAJOR REPAIR IAW GMM6-2-100.
- [SDR FDEA202609211390](https://openairdocs.org/sdr/FDEA202609211390.md): Stringer Splice · cracked · Sep 21, 2026 · N670FE · Airbus A300F4605R · Fuselage Main, Longeron/Stringer
  > MDCC FR 47, S-18L STRINGER SPLICE CRACKED. REPLACED THE STRINGER SPLICE AT MDCC FR47, S-18L PER A300-600F SRM51-40-21 & DWG.A53833157(ISSUE:F00). THIS IS CAT A REPAIR. MAJOR REPAIR IAW GMM6-2-100.
- [SDR FDEA202609181362](https://openairdocs.org/sdr/FDEA202609181362.md): Gearbox · failed · Sep 18, 2026 · N673FE · Airbus A300F4605R · Trailing Edge Flap Control System
  > FLAPS STUCK LESS THAN 20 DEGRESS. DURING DETENTION PRIOR TO LANDING, DECLARED EMERGENCY, UNEVENTFUL LANDING RUNWAY 28 LEFT AT KBOI. AMM 27-51-19-04, AMM 27-55-12-04, AMM 27-54-00-05, AMM 27-54-13-04, & AMM 27-50-00-03. FOUND COUPLING SHEARED FROM RT FLAP SI
- [SDR FDEA202609171360](https://openairdocs.org/sdr/FDEA202609171360.md): Gfi · failed · Sep 17, 2026 · N677FE · Airbus A300F4605R · Fuel Boost Pump
  > AUTO FUEL FEED FAULTED. USED QRH PROCEDURES TO RESET SYS. NR 2 PUMP FAULTED & WOULD NOT RESET. NR 1 INNER TANK PUMP DEFERRED, LEAVING NO OPERATING PUMP IN RT TANK & APPROX 25,000 POUNDS IN RT TANK UNUSABLE. DECLARED EMERGENCY & TRIED TO ESTABLISH A WAY TO BURN
- [SDR FDEA202609151338](https://openairdocs.org/sdr/FDEA202609151338.md): Pitot Tube · inoperative · Sep 15, 2026 · N667FE · Airbus A300F4605R · Pitot/Static System
  > DURING TAKEOFF CA AIRSPEED INDICATOR INDICATED 0. ABORTED TAKEOFF AND TAXIED BACK TO RAMP. REMOVED AND REPLACED CAPT'S PITOT TUBE EF AMM 34-11-15-04. LEAK CHECK GOOD. ACFT OK FOR CONTINUED SERVICE.
- [SDR FDEA202609081286](https://openairdocs.org/sdr/FDEA202609081286.md): Bottle · low pressure · Sep 8, 2026 · N672FE · Airbus A300F4605R · Passenger/Crew Doors
  > LEFT FWD CREW ENTRY DOOR DAMPER AND EMERGENCY OPERATION CYLINDER REQUIRES SERVICING. SERVICED LEFT FWD DOOR DAMPER AND EMERGENCY OPERATION CYLINDER AS REQUIRES.
- [SDR FDEA202609061267](https://openairdocs.org/sdr/FDEA202609061267.md): Frame · cracked · Sep 6, 2026 · N661FE · Airbus A300F4605R · Fuselage Main, Frame
  > INSPECTION OF FRAME 40 LT, LOWER WING JUNCTION, FOUND A CRACK SIGNAL AT FASTENER HOLE NR 1. COMPLIED WITH EA: 6-5710-T0388595 P1. REPAIRED FRAME 40 LT LOWER JUNCTION, CRACKED FASTENER HOLE NR 1. THIS IS CATEGORY B REPAIR. FOLLOW UP INSPECTION IAW EA 6-5710-
- [SDR FDEA202609061266](https://openairdocs.org/sdr/FDEA202609061266.md): Seat Track · corroded · Sep 6, 2026 · N661FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach Fittings
  > MAIN DECK SEAT TRACK AT Y1959 BETWEEN FR53 AND FR54 CORRODED. REPAIRED THE CORRODED MAIN DECK SEAT TRACK AT Y1959 BETWEEN FR53 AND FR54 PER SRM53-10-16-201 FIG.201 & EA: 6-5310-T0388627 P1. CATEGORY -A- MAJOR REPAIR IAW GMM6-2-100.
- [SDR FDEA202609041263](https://openairdocs.org/sdr/FDEA202609041263.md): Jackscrew · leaking · Sep 4, 2026 · N673FE · Airbus A300F4605R · Leading Edge Slat Actuator
  > ON APPROACH, PUT THE SLATS OUT, GOT SLATS 1 & 2 FAULTS. PER ECAM, CYCLED HANDLE. DID NOT EXTEND. FOLLOWED QRH. DECLARED EMERGENCY. UNEVENTFUL NO SLAT LANDING. PRI.0 DUE TO CAUSING DELAY, SFCC 1 SLAT FAIL INDS SHOW JAM. FLAP FAIL, INDS SHOW SUPPLY P. SW. SFC
- [SDR FDEA202609031261](https://openairdocs.org/sdr/FDEA202609031261.md): Elec Connector · loose · Sep 3, 2026 · N681FE · Airbus A300F4605R · Door System Wiring
  > R1 DOOR SLIDE WILL NOT ARM. RELEASED FOR SERVICE PER MEL, ECAM SLIDE INDICATION SYSTEM FOR R1 DOOR INOPERATIVE. DOOR ESCAPE SLIDE ARMING SYSTEM IS TO BE VERIFIED AS FULLY ARMED PRIOR TO EACH DEPARTURE. VERIFIED R1 DOOR ARMING HANDLE OPS AND THAT INDICATIO
- [SDR FDEA202609011253](https://openairdocs.org/sdr/FDEA202609011253.md): Seat Track · worn · Sep 1, 2026 · N661FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach Fittings
  > MAIN DECK SEAT TRACK AT Y1959 BETWEEN FR 62 AND FR 63 FOUND WORN. SEAT TRACK SECTION AT Y1959 BETWEEN FR62 AND FR63 PER A300-600F SRM51-40-21 & SRM53-10-16-201 FIG.201. THIS IS CATEGORY A REPAIR. MAJOR REPAIR IAW FEDEX GMM6-2-100.
- [SDR FDEA202608261228](https://openairdocs.org/sdr/FDEA202608261228.md): Attach Fitting · cracked · Aug 26, 2026 · N661FE · Airbus A300F4605R · Cargo/Baggage Doors
  > FWD CARGO DOOR ACTUATOR ATTACH FITTING FOUND 2EA CRACKS BY HFEC INSPECTION. REPLACED THE CRACKED FWD CARGO DOOR ACTUATOR ATTACH FITTING WITH FABRICATED PART PER SRM51-40-21 & DWG: F52370695(ISSUE. J), A52370501(ISSUE. J) & A52370534(ISSUE. F). RSC TRACKING
- [SDR FDEA202608181142](https://openairdocs.org/sdr/FDEA202608181142.md): Processor · faulted · Aug 18, 2026 · N689FE · Airbus A300F4605R · Landing Gear Retraction/Extension System
  > TAKEOFF AT IND, MLG WOULD NOT RETRACT. C-W QRH. RETURNED. EMERG DECLARED. AMM 32-31-00-05, NLG RETRACT FULLY, GREEN ON BOTH MLG INDS, BOTH LT & RT MLG STAYED GREEN DOWN ON INDS. PERFORMED MLG EXTEND & RETRACT AT GATE & VERIFIED ALL MLG DOORS EXTEND & RE
- [SDR FDEA202607301074](https://openairdocs.org/sdr/FDEA202607301074.md): Restraint · broken · Jul 30, 2026 · N679FE · Airbus A300F4605R · Fuselage Main, Structure
  > MAIN CARGO DECK RESTRAINT MC1487 IN 8L HAS A BROKEN TIP. REMOVED DAMAGED RESTRAINT FROM AIRCRAFT COAT CLOSET AND SHIPPED FOR REPAIR. AIRCRAFT HAS SEAT TRACK DAMAGE AND FLOOR PANEL DAMAGE AT RESTRAINT ATTACH POINTS AND WILL REQUIRE SHEETMETAL REPAIR PRIOR
- [SDR FDEA202607220984](https://openairdocs.org/sdr/FDEA202607220984.md): Power Supply · inoperative · Jul 22, 2026 · N658FE · Airbus A300F4605R · Door Warning System
  > RIGHT FORWARD DOOR SLIDE WILL NOT ARM. RELEASED FOR SERVICE PER MEL. ECAM SLIDE INDICATION SYSTEM FOR R1 DOOR - INOP. DOOR ESCAPE SLIDE ARMING SYSTEM IS TO BE VERIFIED AS FULLY ARMED PRIOR TO EACH DEPARTURE. VERIFIED R1 DOOR SLIDE GIRT BAR LOCKS INT
- [SDR FDEA202607200951](https://openairdocs.org/sdr/FDEA202607200951.md): Pressure Deck · corroded · Jul 20, 2026 · N678FE · Airbus A300F4605R · Fuselage Main, Structure
  > FWD CARGO HORIZONTAL PRESSURE DECK UPPER SURFACE FR40, Y-450 CORRODED. REPAIRED THE CORRODED AREA AT FWD CARGO HORIZONTAL PRESSURE DECK UPPER SURFACE AT FR39 - FR40, BETWEEN Y0 AND Y450. THIS IS CATEGORY A REPAIR. MAJOR REPAIR IAW GMM6-2-100. SEE WRI 5310911
- [SDR FDEA202607200950](https://openairdocs.org/sdr/FDEA202607200950.md): Pressure Deck · cracked · Jul 20, 2026 · N678FE · Airbus A300F4605R · Fuselage Main, Structure
  > FWD CARGO HORIZONTAL PRESSURE DECK UPPER SURFACE FR40, Y1456 CRACKED. REPAIR. REPAIRED THE CORRODED AREA AT FWD CARGO HORIZONTAL PRESSURE DECK UPPER SURFACE AT FR39 - FR40, BETWEEN Y0 AND Y450. THIS IS CATEGORY A REPAIR. MAJOR REPAIR IAW GMM6-2-100.
- [SDR FDEA202607170941](https://openairdocs.org/sdr/FDEA202607170941.md): Fcu · failed · Jul 17, 2026 · N656FE · Airbus A300F4605R · Flight Control System
  > DURING CLIMB OUT PASSING 5000 ATS LEVER TRIPPED OFF AND WE LOST POWER TO THE ENTIRE FCP. NO FLIGHT DIRECTORS, NO FMAS. TRIED RESETTING ATS LEVER AND PITCH TRIM AND YD LEVERS. NO LUCK. AIR TURN BACK. MANUALLY FLOWN AND NO AUTO THROTTLES. AMM: 22-15-12-04
- [SDR FDEA202607140936](https://openairdocs.org/sdr/FDEA202607140936.md): Repair · no discrepancy · Jul 14, 2026 · N678FE · Airbus A300F4605R · Standard Practices/Structures
  > EXISTING REPAIR ON LH WING SLAT NR 1 INNER SKIN BETWEEN RIB 10 & RIB 11 REQUIRES EVALUATION FOR CONFORMITY. THE EXISTING REPAIR ON LT WING SLAT NR 1 INNER SKIN BETWEEN RIB10 AND RIB11 WAS EVALUATED AND FOUND IN CONFORMITY WITH EA 6-5740-133777 A. PERFORMED
- [SDR FDEA202607140935](https://openairdocs.org/sdr/FDEA202607140935.md): Repair · no discrepancy · Jul 14, 2026 · N678FE · Airbus A300F4605R · Standard Practices/Structures
  > EXISTING REPAIR ON MAIN DECK CROSSBEAM FR60,-Y1456~-Y2462 REQUIRES EVALUATION FOR CONFORMITY. THE EXISTING REPAIR ON MAIN DECK CROSSBEAM FR60,-Y1456~-Y2462 WAS EVALUATED AND FOUND IN CONFORMITY WITH EA 6-5310-43476 A.UPGRADED TO MAJOR REPAIR. CLASSIFIED
- [SDR FDEA202607140934](https://openairdocs.org/sdr/FDEA202607140934.md): Repair · inaccurate · Jul 14, 2026 · N678FE · Airbus A300F4605R · Standard Practices/Structures
  > EXISTING REPAIR ON MAIN DECK SEAT TRACK FR32-FR38.2,Y450 REQUIRES EVALUATION FOR CONFORMITY. THE EXISTING REPAIR ON MAIN DECK SEAT TRACK FR32-FR38.2,Y450 WAS EVALUATED AND FOUND NOT IN CONFORMITY WITH A300-600F SRM53-10-16 FIG.201.DUE TO ONE FASTENER MI
- [SDR FDEA202607140933](https://openairdocs.org/sdr/FDEA202607140933.md): Repair · inaccurate · Jul 14, 2026 · N678FE · Airbus A300F4605R · Standard Practices/Structures
  > EXISTING REPAIR ON MAIN DECK SEAT TRACK FR30-FR34,Y0 REQUIRES EVALUATION FOR CONFORMITY. THE EXISTING REPAIR ON MAIN DECK SEAT TRACK FR30-FR34,Y0 WAS EVALUATED AND FOUND NOT IN CONFORMITY WITH A300-600F SRM53-10-16 FIG.201.DUE TO TWO FASTENERS MISSING IN
- [SDR FDEA202607140932](https://openairdocs.org/sdr/FDEA202607140932.md): Seat Track · misrepaired · Jul 14, 2026 · N678FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach Fittings
  > EXISTING REPAIR ON MAIN DECK SEAT TRACK FR18-FR22,Y2462 REQUIRES EVALUATION FOR CONFORMITY. THE EXISTING REPAIR ON MAIN DECK SEAT TRACK FR18-FR22,Y2462 WAS EVALUATED AND FOUND NOT IN CONFORMITY WITH A300-600F SRM53-10-16 FIG.201A.DUE TO 4 FASTENERS MISSIN
- [SDR FDEA202607140931](https://openairdocs.org/sdr/FDEA202607140931.md): Repair · no discrepancy · Jul 14, 2026 · N678FE · Airbus A300F4605R · Cargo/Baggage Doors
  > EXISTING REPAIR ON BULK CARGO DOOR SKIN BETWEEN FR67-FR69,BEAM4-LOWER EDGE REQUIRES EVALUATION FOR CONFORMITY. THE EXISTING REPAIR ON BULK CARGO DOOR SKIN BETWEEN FR67-FR69,BEAM4-LOWER EDGE WAS EVALUATED AND FOUND IN CONFORMITY WITH EA 6-5234-102006..THE
- [SDR FDEA202607140920](https://openairdocs.org/sdr/FDEA202607140920.md): Hinge Arm · delaminated · Jul 14, 2026 · N678FE · Airbus A300F4605R · Spoilers
  > LH WING #3 SPOILER O/B CENTER HINGE ARM O/B DELAMINATION (AREA: 25MM*15MM,DEPTH: 1.40MM), I/B CENTER HINGE ARM O/B DELAMINATION ( AREA: 30MM*12MM, DEPTH: 1.50MM). PERFORMED THE REPAIR ON LH WING #3 SPOILER CENTER HINGE ARM PER FEDEX EA:6-5750- T0387988 P1
- [SDR FDEA202607130923](https://openairdocs.org/sdr/FDEA202607130923.md): Skin · misrepaired · Jul 13, 2026 · N678FE · Airbus A300F4605R · Fuselage Main, Plate/Skin
  > EXISTING REPAIR ON FUSELAGE SKIN BETWEEN FR54.2-FR54.3,STGR46L-STGR49L REQUIRES EVALUATION FOR CONFORMITY THE EXISTING REPAIR ON FUSELAGE SKIN BETWEEN FR54.2-FR54.3,STGR46L-STGR49L. NO RECORD FOUND. REMOVED THE EXISTING REPAIR AND PERFORMED THE NEW REPAIR
- [SDR FDEA202607100915](https://openairdocs.org/sdr/FDEA202607100915.md): Warning System · malfunctioned · Jul 10, 2026 · N681FE · Airbus A300F4605R · Door Warning System
  > R1 DOOR WON T SHOW SLIDE WHEN DOOR IS ARMED. MEL 52-30-04: ECAM SLIDE INDICATION SYSTEM FOR R1 DOOR - INOP. DOOR ESCAPE SLIDE ARMING SYSTEM IS TO BE VERIFIED AS FULLY ARMED PRIOR TO EACH DEPARTURE. AMM 52-73-13-04-02 AMM 31-55-22-04 SLAVED IN SWITCH 1
- [SDR FDEA202607100898](https://openairdocs.org/sdr/FDEA202607100898.md): Glide Slope · malfunctioned · Jul 10, 2026 · N654FE · Airbus A300F4605R · Glide Slope System
  > ON RNAV APPROACH RW 21, ON GLIDEPATH AND CONFIGURED FOR LANDING GOT GLIDESLOPE GLIDESLOPE REPEATEDLY STARTING AT 100 FEET UNTIL TOUCHDOWN.
- [SDR FDEA202607100896](https://openairdocs.org/sdr/FDEA202607100896.md): Sensor · faulted · Jul 10, 2026 · N662FE · Airbus A300F4605R · Hydraulic Reservoir, Main
  > GREEN SYSTEM OVERHEAT LIGHT FLASHING AND CHIME WARINING.
- [SDR FDEA202607100884](https://openairdocs.org/sdr/FDEA202607100884.md): Floorbeam · corroded · Jul 10, 2026 · N678FE · Airbus A300F4605R · Fuselage Main, Floor Beam
  > EXISTING REPAIR ON BULK CARGO COMPARTMENT FLOOR BEAM FR66, Y1456 - Y1456 REQUIRES EVALUATION FOR COMFORMITY. EVALUATED AND FOUND NOT IN CONFORMITY WITH DWR:A53974322(ISSUE:T).FOUND CORROSION ON THE FLANGE SURFACE.PERFORMED THE NEW REPAIR PER EA 6-5321-T03
- [SDR FDEA202607100883](https://openairdocs.org/sdr/FDEA202607100883.md): Floor Panel · cracked · Jul 10, 2026 · N678FE · Airbus A300F4605R · Fuselage Floor Panel
  > MDCC UNDER FLOOR PANEL FR47, Y-953 - Y-1456 FOUND 1EA WEB CRACKED. REPAIRED THE CRACKED WEB AT MDCC UNDER FLOOR PANEL FR47, Y-953 - Y-1456 PER A300-600F SRM53-15-15-201-C2 FIG.201 & SRM51-40-21. THIS IS CAT B REPAIR. INSPECTION THRESHOLD FROM REPAIR: 2400
- [SDR FDEA202607100882](https://openairdocs.org/sdr/FDEA202607100882.md): Web · cracked · Jul 10, 2026 · N678FE · Airbus A300F4605R · Fuselage Floor Panel
  > MDCC UNDER FLOOR PANEL FR47, Y0 - Y450 FOUND 1EA WEB CRACKED. REPAIRED THE CRACKED WEB AT MDCC UNDER FLOOR PANEL FR47, Y-953 - Y-1456 PER A300-600F SRM53-15-15-201-C2 FIG.201 & SRM51-40-21. THIS IS CAT B REPAIR. INSPECTION THRESHOLD FROM REPAIR: 24000FC,
- [SDR FDEA202607050840](https://openairdocs.org/sdr/FDEA202607050840.md): Crossbeam · cracked · Jul 5, 2026 · N678FE · Airbus A300F4605R · Fuselage Main, Structure
  > MDCC FR64, Y1456 - Y1959 CROSSBEAM CRACKED. REPAIRED THE CRACKED CROSSBEAM AT MDCC FR64, Y1456 - Y1959 PER SRM 53-10-15- 201 PARA.14 & SRM51-40-21. THIS IS CAT A REPAIR. MAJOR REPAIR IAW GMM6-2-100.
- [SDR FDEA202607030830](https://openairdocs.org/sdr/FDEA202607030830.md): Pressure Switch · leaking · Jul 3, 2026 · N690FE · Airbus A300F4605R · Hydraulic System, Main
  > ON TAKEOFF ROLL AT ABOUT 60KTS ECAM ALERT OF GREEN HYDRAULIC SYSTEM LOW PRESSURE. WE GOT TWO ECAM WARNINGS, ONE RIGHT AFTER THE OTHER. RTO, AUTO BRAKES DID NOT ENGAGE BEC OF LOW SPEED. TSM 29-32-00 FIG 105 AMM 29-14-00-03 JRH CH5 WITH REF ABOVE RAN NR 1 A
- [SDR FDEA202606280938](https://openairdocs.org/sdr/FDEA202606280938.md): Spoiler · delaminated · Jun 28, 2026 · N680FE · Airbus A300F4605R · Wing, Control Surfaces
  > LH WING #3 SPOILER CENTER HINGE OUTBD ARM OUTBD WEB FOUND DELAMINATION. SIZE:40MM*25MM, DEPTH: 1.1MM COMPLIED WITH EA 6-5750-T0387764 P1, EA TITLE:WING - FLIGHT SURFACES - LH #3 SPOILER CENTER HINGE ARM OUTSIDE SURFACE DELAMINATION. REPAIRED THE DELAMINATI
- [SDR FDEA202606280930](https://openairdocs.org/sdr/FDEA202606280930.md): Spoiler · delaminated · Jun 28, 2026 · N680FE · Airbus A300F4605R · Spoilers
  > RH WING #5 SPOILER CENTER OUTBD HINGE ARM OUTBD WEB FOUND DELAMINATION. SIZE: A:40MM*25MM,B:30MM*20MM, DEPTH: A:1.6MM,B:1.2MM COMPLIED WITH EA 6-5750-T0387765 P1, EA TITLE:WING - FLIGHT SURFACES - RH #5 SPOILER CENTER HINGE ARM OUTSIDE SURFACE DELAMINATION
- [SDR FDEA202606240829](https://openairdocs.org/sdr/FDEA202606240829.md): Seat Track · damaged · Jun 24, 2026 · N680FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach Fittings
  > EXISTING REPAIR ON MAIN DECK SEAT TRACK FR62-FR65,-Y953 REQUIRES EVALUATION FOR CONFORMITY. THE EXISTING REPAIR ON MAIN DECK SEAT TRACK FR62-FR65,-Y953 WAS EVALUATED AND FOUND NOT IN CONFORMITY WITH A300-600F SRM53-10-16-201 FIG.201 DUE TO FOUND SEAT TRACK
- [SDR FDEA202606240799](https://openairdocs.org/sdr/FDEA202606240799.md): Frame · damaged · Jun 24, 2026 · N680FE · Airbus A300F4605R · Fuselage Main, Frame
  > EXISTING REPAIR ON FUSELAGE FRAME FR0 BETWEEN 8-9 O'CLOCK REQUIRES EVALUATION FOR CONFORMITY. THE EXISTING REPAIR ON FUSELAGE FRAME FR0 BETWEEN 8-9 O'CLOCK WAS EVALUATED AND CANNOT BE IDENTIFIED TO A REPAIR IN THE SRM.NO RECORD FOUND.RE-REPAIRED PER EA 6-
- [SDR FDEA202606240798](https://openairdocs.org/sdr/FDEA202606240798.md): Pressure Deck · not reported · Jun 24, 2026 · N680FE · Airbus A300F4605R · Fuselage Main, Structure
  > EXISTING REPAIR ON HORIZONTAL PRESSURE DECK UPPER SURFACE BETWEEN FR51-FR52,Y0~- Y450 REQUIRES EVALUATION FOR CONFORMITY. THE EXISTING REPAIR ON HORIZONTAL PRESSURE DECK UPPER SURFACE BETWEEN FR51- FR52,Y0~-Y450 WAS EVALUATED AND CANNOT BE IDENTIFIED TO A R
- [SDR FDEA202606230797](https://openairdocs.org/sdr/FDEA202606230797.md): Seat Track · none · Jun 23, 2026 · N680FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach Fittings
  > EXISTING REPAIR ON MAIN DECK SEAT TRACK FR40-FR45,Y1456 REQUIRES EVALUATION FOR CONFORMITY. THE EXISTING REPAIR ON MAIN DECK SEAT TRACK FR40-FR45, Y1456 WAS EVALUATED AND FOUND IN CONFORMITY WITH DWG: A53832020(ISSUE: J00), NO RECORD FOUND. EO: 6-5100-7-
- [SDR FDEA202606230796](https://openairdocs.org/sdr/FDEA202606230796.md): Crossbeam · not reported · Jun 23, 2026 · N680FE · Airbus A300F4605R · Fuselage Main, Structure
  > EXISTING REPAIR ON MAIN DECK CROSSBEAM FR20,Y1959~Y2462 REQUIRES EVALUATION FOR CONFORMITY.
- [SDR FDEA202606200788](https://openairdocs.org/sdr/FDEA202606200788.md): Cvr · malfunctioned · Jun 20, 2026 · N679FE · Airbus A300F4605R · Audio/Video Monitoring
  > CVR WOULD NOT TEST PROPERLY DURING PREFLIGHT. RELEASED FOR SERVICE PER MEL: 23-71-01 CATEGORY: A EXPIRATION: 23JUN26 MEL 23-71-01: CVR - INOP.AMM: 23-71-00-05 PERFORMED ADJ/TEST OF CVR IAW AMM 23-71-00-5 AND OPS CHECK WAS GOOD. NO FAULT FOUND.
- [SDR FDEA202606190795](https://openairdocs.org/sdr/FDEA202606190795.md): Seat Track · no discrepancy · Jun 19, 2026 · N680FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach Fittings
  > EXISTING REPAIR ON MAIN DECK SEAT TRACK FR18-FR21,-Y1959 REQUIRES EVALUATION FOR CONFORMITY. THE EXISTING REPAIR ON MAIN DECK SEAT TRACK FR18-FR21,Y1959 WAS EVALUATED AND FOUND NOT IN CONFORMITY WITH EA 6-5313-69642.

Next page: https://openairdocs.org/model/airbus-a300-f4-605r/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 aircraft_model_key = 'A300F4605R'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/model/airbus-a300-f4-605r/reports

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