# Service difficulty reports: N658FE

A list on [N658FE](https://openairdocs.org/aircraft/N658FE.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 8 · 352 reports

- [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 FDEA202603240368](https://openairdocs.org/sdr/FDEA202603240368.md): Sdac · inoperative · Mar 24, 2026 · N658FE · Airbus A300F4605R · Passenger/Crew Doors
  > R1 DOOR WILL NOT ARM. AMM 52-10-00-00-02, DURING T/S FOUND THAT ARMING LEVER MOVED TO ARMED POSITION BUT ECAM INDICATION DID NOT SHOW (SLIDE) INDICATION. AMM: 31-55-22-04, R & R SDAC IAW AMM 31-55-22-04, NO SLIDE ARMED INDICATION ON ECAM (DOOR PG). REIN
- [SDR FDEA202603210362](https://openairdocs.org/sdr/FDEA202603210362.md): Battery · failed · Mar 21, 2026 · N658FE · Airbus A300F4605R · Door Warning System
  > BOTH L1 & R1 DOOR SLIDE WARNING LIGHTS INOP. BUZZERS WORK NORMALLY. MEL 20MAR26 19:20 PDX RELEASED FOR SERVICE PER MEL: 52-73-01-01 CATEGORY: C EXPIRATION: 30MAR26 "MEL 52-73-01-01: L1 AND R1 CREW ENTRY DOOR ESCAPE SLIDE WARNING SYSTEM LIGHTS -
- [SDR FDEA202603060322](https://openairdocs.org/sdr/FDEA202603060322.md): Power Supply · faulted · Mar 6, 2026 · N658FE · Airbus A300F4605R · Door Warning System
  > CHECK FOUND BOTH L & R FWD DOOR ESCAPE SLIDE WARNING LIGHT INOP, BUZZER WORK NORMAL. RELEASED FOR SERVICE PER MEL 52-73-01-01, CATEGORY C. REPLACED THE AUTONOMOUS POWER SUPPLY UNIT (70WN) IAW AMM 52-73-18-04. ADJ./TEST PERFORMED IAW AMM 52-73-00-05-02. OK
- [SDR FDEA202603060321](https://openairdocs.org/sdr/FDEA202603060321.md): Power Supply · failed · Mar 6, 2026 · N658FE · Airbus A300F4605R · Escape Slide
  > R1 SLIDE INDICATION ON ECAM WILL NOT DISPLAY WHEN SLIDE IS ARMED. DOOR ESCAPE SLIDE ARMING SYSTEM IS TO BE VERIFIED AS FULLY ARMED PRIOR TO EACH DEPARTURE. MEL: 52-30-04 PHYSICALLY ENSURE THAT THE AFFECTED DOOR ESCAPE SLIDE ARMING HANDLE IS POSITIONED
- [SDR FDEA202603040312](https://openairdocs.org/sdr/FDEA202603040312.md): Power Supply · inoperative · Mar 4, 2026 · N658FE · Airbus A300F4605R · Door Warning System
  > CHECK FOUND BOTH L & R FWD DOOR ESCAPE SLIDE WARNING LIGHT INOP, BUZZER WORK NORMAL. RELEASED FOR SERVICE IAW MEL 52-73-01-01, CATEGORY C.. L1 & R1 CREW ENTRY DOOR ESCAPE SLIDE WARNING SYSTEM LIGHTS INOPERATIVE. REPLACED THE AUTONOMOUS POWER SUPPLY UNIT
- [SDR FDEA202603030309](https://openairdocs.org/sdr/FDEA202603030309.md): Slide · out of position · Mar 3, 2026 · N658FE · Airbus A300F4605R · Emergency Equipment
  > FINISHED CHECK THAT L1 ESCAPE SLIDE PRESSURE INDICATOR IN GREEN BAND. THE ESCAPE SLIDE BUT THE NEW L1 ESCAPE SLIDE PRESSURE GAUGE NOT ALIGNED WITH VIEW PORT. MEL CAN RELEASED FOR SERVICE PER MEL: 52-11-01-01 CREW ENTRY DOOR ESCAPE SLIDE SLIDE REMAINS IN
- [SDR FDEA202602070142](https://openairdocs.org/sdr/FDEA202602070142.md): Skin · damaged · Feb 7, 2026 · N658FE · Airbus A300F4605R · Fuselage Main, Plate/Skin
  > EXISTING REPAIR ON FUSELAGE SKIN AT FRS 19 - 20A, S38R - 42R REQUIRES EVALUATION FOR CONFORMITY. EVALUATED & FOUND NOT IN CONFORMITY WITH SRM 53-13-13 FIG.201. DUE TO ONE ROW FASTENERS MISSING INSTALLED. REMOVED THE EXISTING REPAIR AND RE-REPAIRED THE SKIN I
- [SDR FDEA202602050135](https://openairdocs.org/sdr/FDEA202602050135.md): Frame · unknown · Feb 5, 2026 · N658FE · Airbus A300F4605R · Fuselage Main, Structure
  > EXISTING REPAIR ON FUSELAGE FRAME AT FR28 BETWEEN STGR8LH AND STGR12LH REQUIRES EVALUATION FOR CONFORMITY. EVALUATED AND NO RECORD FOUND. REMOVED THE EXISTING REPAIR AND RE-REPAIRED THE FRAME PER EA 6-5310-T0386358. TITLE: FUSELAGE - MAINFRAME - EXISTIN
- [SDR FDEA202602100160](https://openairdocs.org/sdr/FDEA202602100160.md): Crease Beam · corroded · Feb 4, 2026 · N658FE · Airbus A300F4605R · Standard Practices/Structures
  > EXISTING REPAIR ON MDCC CROSSBEAM AT FR55 BETWEEN Y1456 AND Y1959 REQUIRES EVALUATION FOR CONFORMITY THE EXISTING REPAIR ON MDCC CROSSBEAM AT FR55 BETWEEN Y1456 AND Y1959 WAS EVALUATED AND FOUND IN CONFORMITY WITH EA 6-5310-70959 A. THE REPAIR IS CATEGORY
- [SDR FDEA202602040132](https://openairdocs.org/sdr/FDEA202602040132.md): Repair · no discrepancy · Feb 4, 2026 · N658FE · Airbus A300F4605R · Standard Practices/Structures
  > EXISTING REPAIR ON MDCC CROSSBEAM AT FR55 BETWEEN Y1456 AND Y1959 REQUIRES EVALUATION FOR CONFORMITY THE EXISTING REPAIR ON MDCC CROSSBEAM AT FR55 BETWEEN Y1456 AND Y1959 WAS EVALUATED AND FOUND IN CONFORMITY WITH EA 6-5310-70959 A. THE REPAIR IS CATEGORY
- [SDR FDEA202602010112](https://openairdocs.org/sdr/FDEA202602010112.md): Frame · damaged · Feb 1, 2026 · N658FE · Airbus A300F4605R · Fuselage Main, Frame
  > EXISTING REPAIR ON FUSELAGE FRAME AT FR20A STGR39R-STGR42R REQUIRES EVALUATION FOR CONFORMITY THE EXISTING REPAIR ON FUSELAGE FRAME AT FR20A STGR39R-STGR42R WAS EVALUATED AND FOUND NOT IN CONFORMITY WITH EA 6-5310-T0305871. TITLE: FUSELAGE - MAINFRAME -
- [SDR FDEA202601290157](https://openairdocs.org/sdr/FDEA202601290157.md): Frame · cracked · Jan 29, 2026 · N658FE · Airbus A300F4605R · Fuselage Main, Frame
  > CENTER BOX - INSPECTION OF REAR SPAR AND BOTTOM PANEL AT JUNCTION WITH FUSELAGE FR47 RH SIDE, FASTENER "H" HOLE FOUND CRACK SIGNAL. COMPLIED WITH EA 6-5710-T0386164. REPAIRED THE CRACKED CENTER BOX REAR SPAR RT FRAME 47 HOLE H. CAT -B- REPAIR AND THE POST
- [SDR FDEA202601280097](https://openairdocs.org/sdr/FDEA202601280097.md): Crossbeam · misrepaired · Jan 28, 2026 · N658FE · Airbus A300F4605R · Fuselage Main, Structure
  > EXISTING REPAIR ON MDCC CROSSBEAM LOWER FLANGE AT FR60 BETWEEN -Y1456 AND -Y1959 REQUIRES EVALUATION FOR CONFORMITY THE EXISTING REPAIR ON MDCC CROSSBEAM LOWER FLANGE AT FR60 BETWEEN -Y1456 AND - Y1959. NO RECORD FOUND. REMOVED THE EXISTING REPAIR AND RE-RE
- [SDR FDEA202601210089](https://openairdocs.org/sdr/FDEA202601210089.md): Repair · out of limits · Jan 21, 2026 · N658FE · Airbus A300F4605R · Fuselage Main, Plate/Skin
  > EXISTING REPAIR ON FUSELAGE SKIN AT FR22-FR23 STGR51L-STGR53L REQUIRES EVALUATION FOR CONFORMITY THE EXISTING REPAIR ON FUSELAGE SKIN AT FR22 - FR23 STGR51L-STGR53L NO REPAIR RECORD FOUND. REMOVED THE EXISTING REPAIR AND RE-REPAIRED THE SKIN IAWSRM 53-10-
- [SDR FDEA202601160061](https://openairdocs.org/sdr/FDEA202601160061.md): Fastener · missing · Jan 16, 2026 · N658FE · Airbus A300F4605R · Standard Practices/Structures
  > EXISTING REPAIR ON MDCC CROSSBEAM AT FR65 BETWEEN Y953 AND Y1456 REQUIRES EVALUATION FOR CONFORMITY. EVALUATED AND FOUND NOT IN CONFORMITY WITH EA 6-5310-160172.. DUE TO ONE FASTENER MISSING INSTALLED. EO: 6-5100-7-5000 D7 PT1 WAS COMPLETED. DRILLED A N
- [SDR FDEA202601160060](https://openairdocs.org/sdr/FDEA202601160060.md): Seat Track · damaged · Jan 16, 2026 · N658FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach Fittings
  > EXISTING REPAIR ON MDCC SEAT TRACK AT Y0 BETWEEN FR71 AND FR73 REQUIRES EVALUATION FOR CONFORMITY. EVALUATED AND FOUND NOT IN CONFORMITY WITH A300-600F SRM 53-10-16 FIG201. DUE TO 4 FASTENERS MISSING INSTALLED. EO: 6-5100-7-5000 D7 PT1 WAS COMPLETED. TI
- [SDR FDEA202601160050](https://openairdocs.org/sdr/FDEA202601160050.md): Seat Track · no discrepancy · Jan 16, 2026 · N658FE · Airbus A300F4605R · Standard Practices/Structures
  > EXISTING REPAIR ON MDCC SEAT TRACK AT -Y1456 BETWEEN FR26 AND FR31 REQUIRES EVALUATION FOR CONFORMITY. THE EXISTING REPAIR ON MDCC SEAT TRACK AT -Y1456 BETWEEN FR26 AND FR31 WAS EVALUATED AND FOUND IN CONFORMITY IAW SRM 53-10-16-201 FIG201. NO REPAIR RECOR
- [SDR FDEA202601160049](https://openairdocs.org/sdr/FDEA202601160049.md): Seat Track · no discrepancy · Jan 16, 2026 · N658FE · Airbus A300F4605R · Standard Practices/Structures
  > EXISTING REPAIR ON MDCC SEAT TRACK AT Y450 BETWEEN FR32 AND FR34 REQUIRES EVALUATION FOR CONFORMITY. THE EXISTING REPAIR ON MDCC SEAT TRACK AT Y450 BETWEEN FR32 AND FR34 WAS EVALUATED AND FOUND IN CONFORMITY WITH A300-600F SRM 53-10-16-201 FIG201. NO REPAIR
- [SDR FDEA202601150066](https://openairdocs.org/sdr/FDEA202601150066.md): Fitting · cracked · Jan 15, 2026 · N658FE · Airbus A300F4605R · Fuselage Main, Frame
  > NDT INSPECTION, MAIN DECK DOOR ACTUATOR BEARING FITTINGS 3EA HOLES FOUND CRACK SIGNAL AT FRAME 23 AND 24. COMPLIED WITH EA 6-5230-T0386195 REPAIRED THE CRACKED MAIN DECK DOOR ACTUATOR BEARING FITTINGS. MAJOR REPAIR IAW FEDEX GMM 6-2-100. SEE WRI 52307839
- [SDR FDEA202601150045](https://openairdocs.org/sdr/FDEA202601150045.md): Repair · no discrepancy · Jan 15, 2026 · N658FE · Airbus A300F4605R · Standard Practices/Structures
  > EXISTING REPAIR ON FWD CARGO DOOR INNER SKIN FR 23A-24A BETWEEN BEAM 1 AND BEAM 2 REQUIRES EVALUATION FOR CONFORMITY. THE EXISTING REPAIR ON FWD CARGO DOOR INNER SKIN FR23A - FR24A BETWEEN BEAM 1 AND BEAM 2 WAS EVALUATED AND FOUND IN CONFORMITY WITH EA 6-
- [SDR FDEA202601140034](https://openairdocs.org/sdr/FDEA202601140034.md): Repair · no discrepancy · Jan 14, 2026 · N658FE · Airbus A300F4605R · Standard Practices/Structures
  > EXISTING REPAIR ON MDCC FLOOR SUPPORT AT -Y1959 BETWEEN FR12A AND FR18 REQUIRES EVALUATION FOR CONFORMITY. THE EXISTING REPAIR ON MDCC FLOOR SUPPORT AT -Y1959 BETWEEN FR12A AND FR18 WAS EVALUATED AND FOUND IN CONFORMITY WITH DWG: A53612213 (ISSUE: G00). E
- [SDR FDEA202601140033](https://openairdocs.org/sdr/FDEA202601140033.md): Repair · no discrepancy · Jan 14, 2026 · N658FE · Airbus A300F4605R · Standard Practices/Structures
  > EXISTING REPAIR ON MDCC FLOOR SUPPORT AT Y0 BETWEEN FR11 AND FR19 REQUIRES EVALUATION FOR CONFORMITY. THE EXISTING REPAIR ON MDCC FLOOR SUPPORT AT Y0 BETWEEN FR11 AND FR19 WAS EVALUATED AND FOUND IN CONFORMITY WITH DWG: A53612213 (ISSUE: G00). EO: 6-5100-
- [SDR FDEA202601140032](https://openairdocs.org/sdr/FDEA202601140032.md): Repair · no discrepancy · Jan 14, 2026 · N658FE · Airbus A300F4605R · Standard Practices/Structures
  > EXISITING REPAIR ON MDCC FLOOR SUPPORT AT Y450 BETWEEN FR11 AND FR15A REQUIRES EVALUATION FOR CONFORMITY. THE EXISTING REPAIR ON MDCC FLOOR SUPPORT AT Y450 BETWEEN FR11 AND FR15A WAS EVALUATED AND FOUND IN CONFORMITY WITH DWG:A53612213 (ISSUE: G00). EO: 6-
- [SDR FDEA202601130031](https://openairdocs.org/sdr/FDEA202601130031.md): Thrust Bracket · damaged · Jan 13, 2026 · N658FE · Airbus A300F4605R · Fuselage Main, Structure
  > EXISTING REPAIR ON FUSELAGE MAIN DECK CARGO COMPARTMENT FR 26 - FR 27 THRUST BRACKET WEB BETWEEN -Y450 AND -Y953 REQUIRES EVALUATION FOR CONFORMITY THE EXISTING REPAIR ON FUSELAGE MAIN DECK CARGO COMPARTMENT FR26-FR27 THRUST BRACKET WEB BETWEEN -Y450 AND -
- [SDR FDEA202601120290](https://openairdocs.org/sdr/FDEA202601120290.md): Fitting · damaged · Jan 12, 2026 · N658FE · Airbus A300F4605R · Cargo/Baggage Doors
  > 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. REPLACED THE MAIN DECK CARGO DOOR ACTUATOR BEARING FITTINGS. C
- [SDR FDEA202601120064](https://openairdocs.org/sdr/FDEA202601120064.md): Panel · cracked · Jan 12, 2026 · N658FE · Airbus A300F4605R · Fuselage Main, Frame
  > NDT INSP, LT CENTER BOX REAR SPAR FR47 FWD FITTING RIB 1 HOLE G FOUND A CRACK SIGNAL. COMPLIED WITH EA 6-5710-T0386165 REPAIRED THE CRACKED HOLE "G" AT LH CENTER WING BOX REAR SPAR FR47 FWD FITTING RIB1. MAJOR REPAIR IAW FEDEX GMM 6-2-100. SEE WRI 57107
- [SDR FDEA202601120048](https://openairdocs.org/sdr/FDEA202601120048.md): Frame · cracked · Jan 12, 2026 · N658FE · Airbus A300F4605R · Fuselage Main, Frame
  > NDT INSP - RT CENTER BOX REAR SPAR FR47 FWD FITTING RIB1 HOLE "C" FOUND CRACK SIGNAL. COMPLIED WITH EA 6-5710-T0386164 REPAIRED THE CRACKED CENTER WING BOX REAR SPAR RHS FR47 FWD FITTING RIB1 HOLE "C". TITLE: WINGS - BASIC WING STRUCTURE - FR47 RH REAR SP
- [SDR FDEA202601100086](https://openairdocs.org/sdr/FDEA202601100086.md): Crossbeam · corroded · Jan 10, 2026 · N658FE · Airbus A300F4605R · Fuselage Main, Structure
  > MDCC CROSSBEAM, LWR SURFACE AT FR54.2 CORRODED. COMPLIED WITH EA 6-5310-T0386271 REPAIRED THE CORRODED CROSSBEAM LOWER FLANGE AT FR54.2 BETWEEN Y1456 AND -Y1456. FUSELAGE - MAINFRAME - CORROSION ON MDCC FR54.2 CROSSBEAM LOWER FLANGE BETWEEN Y1456/YC AND
- [SDR FDEA202601100042](https://openairdocs.org/sdr/FDEA202601100042.md): Hinge Arm · delaminated · Jan 10, 2026 · N658FE · Airbus A300F4605R · Spoilers
  > LEFT WING SPOILER NR 3 CENTER INBD HINGE ARM OUTSIDE SURFACE FOUND DELAMINATION. SIZE: 55MM - 25MM, DEPTH: 0.91MM COMPLIED WITH EA 6-5750-T0386109 P1 TO REPAIR LT WING SPOILER NR 3 CENTER INBD HINGE ARM OUTSIDE SURFACE DELAMINATION, THIS IS CATEGORY A REPAIR.
- [SDR FDEA202601100043](https://openairdocs.org/sdr/FDEA202601100043.md): Hinge Arm · delaminated · Jan 10, 2026 · N658FE · Airbus A300F4605R · Spoilers
  > RIGHT WING SPOILER NR 5 CENTER OTBD HINGE ARM OUTSIDE SURFACE FOUND DELAMINATION. SIZE: 90 MM-24MM, DEPTH: 1.25 MM. COMPLIED WITH EA 6-5750-T0386108 P1 TO REPAIR RT WING SPOILER NR 5 CENTER OTBD HINGE ARM OUTSIDE SURFACE DELAMINATION, THIS IS CATEGORY A REPA
- [SDR FDEA202601090044](https://openairdocs.org/sdr/FDEA202601090044.md): Skin · cracked · Jan 9, 2026 · N658FE · Airbus A300F4605R · Cargo/Baggage Doors
  > FWD CARGO DOOR INNER SKIN AT FR22A, BEAM1-BEAM2 CRACKED. COMPLIED WITH EA 6-5230-T0386127 REPAIRED THE FWD CARGO DOOR FR22A BEAM1-BEAM2 CRACKED INNER SKIN. TITLE: DOORS - CARGO DOOR/HYD SYS - FWD CARGO DOOR - CRACK ON INNER SKIN FWD OF FR22A BELOW BEAM #1.
- [SDR FDEA202601080041](https://openairdocs.org/sdr/FDEA202601080041.md): Rib · cracked · Jan 8, 2026 · N658FE · Airbus A300F4605R · Trailing Edge Flaps
  > RIGHT CENTER FLAP RIB UPPER FLANGE FOUND 5EA CRACKS AT RIB 26 BETWEEN STGR2.6 AND REAR SPAR, RIB 27 BETWEEN STGR 2.7 AND REAR SPAR. RIB27 BETWEEN STGR2.7 AND REAR SPAR COMPLIED WITH EA:6-5750-T0386104 P1 TO REPAIR RH CENTER FLAP RIB UPPER FLANGE 5EA CRACKS AT
- [SDR FDEA202601080040](https://openairdocs.org/sdr/FDEA202601080040.md): Rib · cracked · Jan 8, 2026 · N658FE · Airbus A300F4605R · Trailing Edge Flaps
  > RIGHT CENTER FLAP RIB UPPER FLANGE FOUND CRACK AT RIB 11 BETWEEN S 2.7 AND S 2.8. COMPLIED WITH EA:6-5750-T0386104 P1 TO REPAIR RH CENTER FLAP RIB CRACKED UPPER FLANGE AT RIB11 BETWEEN STGR2.7 AND STGR2.8, EA TITLE: WING - FLIGHT SURFACES - RT CENTER FLAP C
- [SDR FDEA202601060047](https://openairdocs.org/sdr/FDEA202601060047.md): Crossbeam · cracked · Jan 6, 2026 · N658FE · Airbus A300F4605R · Fuselage Main, Structure
  > MDCC CROSSBEAM AT FR64, BETWEEN -Y1456 AND -Y1959 CRACKED. REPAIRED THE MDCC CRACKED CROSSBEAM ON MDCC AT FR64 BETWEEN -Y1456 AND -Y1959 PER A300-600F SRM 53-10-15-201 FIG.211. THIS IS A CATEGORY "A" REPAIR. MAJOR REPAIR IAW GMM 6-2-100.
- [SDR FDEA202505230795](https://openairdocs.org/sdr/FDEA202505230795.md): Slide · failed · May 23, 2025 · N658FE · Airbus A300F4605R · Escape Slide
  > AFTER CLOSING AND ARMING DOORS FOR DEPARTURE, F/O NOTICED THAT THE RAMP AGENT LEFT HER SCANNER. IN AN EFFORT TO RETURN IT TO HER, HE INADVERTENTLY OPENED THE DOOR WHILE IT WAS STILL ARMED. SLIDE DID NOT INFLATE BUT DID COME OUT OF THE CONTAINER. RELEASE
- [SDR FDEA202406110790](https://openairdocs.org/sdr/FDEA202406110790.md): Bolt · missing · Jun 11, 2024 · N658FE · Airbus A300F4605R · Escape Slide
  > LEFT PASSENGER DOOR SLIDE MISSING SLIDE ATTACH BOLT REF IPC 25-61-21-01 ITEM 30-40. GMM: 7-1-100 AMM: 25-61-21-04, INSTALLED SLIDE ATTACHING SCREW PART NUMBER NAS1100E5-14 AND WASHER AN960C516L PER AMM 25-61-21-04. VERIFIED INSTALLATION OF DUAL ESCAPE SLIDE
- [SDR FDEA202403290409](https://openairdocs.org/sdr/FDEA202403290409.md): Bottle · low pressure · Mar 29, 2024 · N658FE · Airbus A300F4605R · Emergency Equipment
  > MDIS 658 52-10 6061 29MAR24 12:02 LRD FACT L1 DOOR ASSIST BOTTLE PRESSURE LOW FACT 29MAR24 18:22 LRD AMM: 52_10_14_03_02 SERVICED L1 EMERGENCY OPERATION CYLINDER TO 1700PSI PER A300 AMM 52_10_14_03_02
- [SDR FDEA202311261927](https://openairdocs.org/sdr/FDEA202311261927.md): Pin · loose · Nov 26, 2023 · N658FE · Airbus A300* · Equipment/Furnishings Wiring
  > THERE IS A RED FLAG PROTRUDING FROM UNDER THE R1 DOOR SLIDE. 26NOV23 - REMOVED RED TAG LABELED - REMOVE BEFOREINSTALLATION - ON R1 DOOR SLIDE REF ABOVE AMM REFERENCE. A/C OK FOR SERVICE. PER MOC PERF INSP / CHECK OF R1 DOOR SLIDE. AMM: 25-61-20-06-1 PER
- [SDR FDEA202310091735](https://openairdocs.org/sdr/FDEA202310091735.md): Crossbeam · cracked · Oct 9, 2023 · N658FE · Airbus A300* · Fuselage Main, Structure
  > MDCC C59, Y650 CROSS BEAM CRACKED. REPAIRED THE MAIN DECK CARGO COMPARTMENT FLOOR STRUCTURE CRACKED CROSSBEAM AT FR58 BETWEEN Y1456 AND Y1959 PER A300-600F SRM53-10-15-201 PARA.14. FIG.211. THIS IS CATEGORY A REPAIR. MAJOR REPAIR IAW FEDEX GMM6-2-100
- [SDR FDEA202310091734](https://openairdocs.org/sdr/FDEA202310091734.md): Spoiler · delaminated · Oct 9, 2023 · N658FE · Airbus A300* · Spoilers
  > RH WING #5 SPOILER CENTER I/B HINGE O/B FOUND DELAMINATION. SIZE: 30MMX20MM, DEPTH: 1.80MM PERFORMED THE REPAIR ON RH WING #5 SPOILER CENTER I/B & O/B HINGE ARM LWR SURFACE AS PER FEDEX EA: 6-5750-T0373835 P1, TITLE: WING-FLIGHT SURFACES-RH 5# SPOILER CEN
- [SDR FDEA202310041699](https://openairdocs.org/sdr/FDEA202310041699.md): Crossbeam · cracked · Oct 4, 2023 · N658FE · Airbus A300* · Fuselage Main, Structure
  > MDCC FR30, Y650 CROSS BEAM CRACKED. REPAIRED THE MDCC CRACKED CROSSBEAM AT FR30 Y650 PER A300-600F SRM53-10-15-201 PARA.15 FIG.212 & EA:6-5310-T0376581 P1. THIS IS CAT A REPAIR. MAJOR REPAIR IAW FEDEX GMM6-2-100.
- [SDR FDEA202306280914](https://openairdocs.org/sdr/FDEA202306280914.md): Power Supply · dirty · Jun 28, 2023 · N658FE · Airbus A300F4605R · Passenger/Crew Doors
  > R1 ENTRY DOOR NOT SHOWING ARMED ON ECAM WITH DOOR IN ARMED POSITION. RELEASED FOR SERVICE PER MEL: 52-30-04 CATEGORY: C EXPIRATION: 08JUL26 "MEL 52-30-04: ECAM SLIDE INDICATION SYSTEM FOR (R1)DOOR - INOP. DOOR ESCAPE SLIDE ARMING SYSTEM IS TO BE VERIF
- [SDR FDEA202207201787](https://openairdocs.org/sdr/FDEA202207201787.md): Controller · faulted · Jul 20, 2022 · N658FE · Airbus A300F4605R · Compressor Bleed Valve
  > PDIS 658 36-10 4286 19JUL22 BOS FACT U DURING DEPARTURE PASSING 4,000 MSL IN HIGH THRUST SETTING, BLEED VALVE #1 FAULT. COMPLIED WITH ECAM WHICH
- [SDR FDEA202107091709](https://openairdocs.org/sdr/FDEA202107091709.md): Selector Valve · inoperative · Jul 9, 2021 · N658FE · Airbus A300F4605R · Landing Gear Retraction/Extension System
  > GEAR WOULD NOT COME DOWN ON FINAL, ECAM DIRECTED MANUAL CRANK DOWN. WE COMPLIED WITH ECAM AND RAN THE CHECKLIST AND THE GEAR CAME DOWN WITH THE CRANK. GEAR DOORS REMAINED OPEN AS INDICATED IN THE CHECKLIST. I REPLACED SELECTOR VALVE 3GA IAW A300 AMM 32-
- [SDR FDEA202104281065](https://openairdocs.org/sdr/FDEA202104281065.md): Attach Fitting · damaged · Apr 28, 2021 · N658FE · Airbus A300F4605R · Wing, Attach Fittings
  > WHILE ACCOMPLISHING STEP 9 OF E0 6-5710-7-3301 PT1 THE CUTTER INCREMENTS WERE NOT NOT FOLLOWED THEREFORE CUTTING MORE MATERIAL THAN REQUIRED ON ATTACHED FITTING ACCOMPLISHED EA 6-5740-T0361294 P1. WINGS - ATTACH FITTING - DAMAGE TO REAR SPAR FITTING.
- [SDR FDEA202102150358](https://openairdocs.org/sdr/FDEA202102150358.md): Skin · damaged · Feb 15, 2021 · N658FE · Airbus A300F4605R · Trailing Edge Flaps
  > DURING INSTALL OF R/H WING CENTER FLAP FOUND SKIN PUNCTURED, LOWER SURFACE CENTER OF FLAP. REPAIRED DAMAGE/PUNCTURED ON LOWER SURFACE OF CENTER FLAP IAW A300 SRM 57-50- 00, FIG. 205, MAJOR REPAIR.
- [SDR FDEA202102030284](https://openairdocs.org/sdr/FDEA202102030284.md): Roller Tray · corroded · Feb 3, 2021 · N658FE · Airbus A300F4605R · Fuselage Main, Structure
  > AFT PIT ROLLER TRAY FR 56 RH (I/B OF PDU) CORRODED LWR SURFACE. DOT NO. 17-62 BLENDED ROLLER TRAY LOWER SURFACE AT FR 56 R/H SIDE IAW SRM 51-74-10. FOUND TO BE OUT OF LIMITS IAW SRM 53-10-15, FIG. 101. ACCOMPLISHED ROLLER TRAY SPLICE REPAIR IAW SRM 53-10-1
- [SDR FDEA202102010260](https://openairdocs.org/sdr/FDEA202102010260.md): Crossbeam · corroded · Feb 1, 2021 · N658FE · Airbus A300F4605R · Fuselage Main, Structure
  > AFT PIT FLOOR STRUCTURE FR 56 RH END CORRODED. DOT NO. 17-59 REPAIRED FLOOR SUP. AFT PIT FR. 56 R.H. IAW A-300 SRM 53-10-15 FIG. 208, REMOVED CORROSION IAW SRM 51-74-10 100% OUT OF LIMITS IAW A-300 SRM 53-10-15 FIG. 101, MAJOR REPAIR.
- [SDR FDEA202101300247](https://openairdocs.org/sdr/FDEA202101300247.md): Floor Panel · delaminated · Jan 30, 2021 · N658FE · Airbus A300F4605R · Fuselage Floor Panel
  > COURIER FLOOR PANEL 221MF DELAMINATED FABRICATED COURIER FLOOR PANEL 221MF ON VTMAE TRAVELER T21/1531290 MAJOR REPAIR. REPAIR CAT A IAW DWG SRZ-25-005 REV R.

Next page: https://openairdocs.org/aircraft/N658FE/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 = 'N658FE' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N658FE/reports

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