# Service difficulty reports: N652FE

A list on [N652FE](https://openairdocs.org/aircraft/N652FE.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 · 320 reports

- [SDR FDEA202510182050](https://openairdocs.org/sdr/FDEA202510182050.md): Grip · missing · Oct 18, 2025 · N652FE · Airbus A300F4605R · Flight Compartment Windows
  > CAPTAINS SLIDING WINDOW HANDLE MISSING GRIP. REF IPC 56-12-11-03A ITEM 15 PART 18OCT25 16:30 SDF IDENTIFIED PARTS HANDLE FOR SLIDING WINDOW INSTALLED MISSING GRIP AND SET SCREW PER SMP. REF ERS 25-03162. PER MEM QA, GRIP INSTALLATION IS NOT RII. LH
- [SDR FDEA202409251402](https://openairdocs.org/sdr/FDEA202409251402.md): Seat Track · damaged · Sep 25, 2024 · N652FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach Fittings
  > FLOOR SEAT TRACK DAMAGED AT POSITION 12R FOR LOCK. SEAT TRACK ADAPTER LOBES AT LOCK MT1673 BROKEN. INSTALLED SEAT TRACK SECTION AND REPAIR IAW SRM 53-10-16-201/FIG 201. INSTALLED FLOORBOARDS IAW AMM 53-10-25-04-02 AND HANDLING SYSTEMS IAW AMM 25-58-00-00.
- [SDR FDEA202409251401](https://openairdocs.org/sdr/FDEA202409251401.md): Seat Track · damaged · Sep 25, 2024 · N652FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach Fittings
  > FLOOR SEAT TRACK DAMAGED AT POSITION 12R FOR LOCK. SEAT TRACK ADAPTER LOBES AT LOCK MT1673 BROKEN. INSTALLED SEAT TRACK SECTION AND REPAIR IAW SRM 53-10-16-201/FIG 201. FLOORBOARDS IAW AMM 53-10-25-04-02 AND HANDLING SYSTEMS IAW AMM 25-58-00-00. INSTALLED
- [SDR FDEA202308111550](https://openairdocs.org/sdr/FDEA202308111550.md): Rib · corroded · Aug 11, 2023 · N652FE · Airbus A300* · Spoilers
  > R/H WING SPOILER 4 BEAM I/B JACK RIB UPR BORE INNER FACE CORRODED ACCOMPLISHED THE REINFORCING REPAIR AT RH #4 SPOILER I/B JACK RIB I.A.W FEDEX EA NO:T6- 5740-T0375735 P1,SEQ NO:863, TITLE: WINGS - ATTACH FITTINGS - RH WING #4 SPOILER JACK RIB AT STA ABX 10
- [SDR FDEA202308101567](https://openairdocs.org/sdr/FDEA202308101567.md): Flange · worn · Aug 10, 2023 · N652FE · Airbus A300* · Landing Gear Doors
  > RH MLG DOOR CENTER FITTING AFT SIDE IS WORN INSTALLED THE NEW CENTER HINGE FITTING WITH FASTENERS I.A.W A300-600F SRM 51-40-21-001, PARA.6~7, PAGE.7B-50 & 51-72-10-001, PAGE.2 "MAJOR REPAIR"
- [SDR FDEA202308081566](https://openairdocs.org/sdr/FDEA202308081566.md): Rib · corroded · Aug 8, 2023 · N652FE · Airbus A300* · Spoilers
  > R/H WING SPOILER 3 BEAM O/B JACK RIB UPR BORE INNER FACE CORRODED ACCOMPLISHED THE REINFORCING REPAIR AT RH #3 SPOILER O/B JACK RIB I.A.W FEDEX EA NO:T6-5740-T0375736 P1,SEQ NO:862, TITLE: WINGS - ATTACH FITTINGS - RH WING #3 SPOILER JACK RIB AT STA ABX31.
- [SDR FDEA202308081565](https://openairdocs.org/sdr/FDEA202308081565.md): Rib · corroded · Aug 8, 2023 · N652FE · Airbus A300* · Spoilers
  > R/H WING SPOILER 3 BEAM I/B JACK RIB UPR BORE INNER FACE CORRODED ACCOMPLISHED THE REINFORCING REPAIR AT RH #3 SPOILER I/B JACK RIB I.A.W FEDEX EA NO:T6- 5740-T0375736 P1,SEQ NO:862, TITLE: WINGS - ATTACH FITTINGS - RH WING #3 SPOILER JACK RIB AT STA ABX31.
- [SDR FDEA202308081559](https://openairdocs.org/sdr/FDEA202308081559.md): Rib · gouged · Aug 8, 2023 · N652FE · Airbus A300* · Wing Structure
  > R/H WING SPOILER 5 BEAM I/B JACK RIB LWR BORE INNER FACE GOUGE ACCOMPLISHED THE REINFORCING REPAIR AT RH #5 SPOILER I/B JACK RIB I.A.W FEDEX EA NO:T6- 5740-T0375737 P1,SEQ NO:865, TITLE:WINGS - ATTACH FITTINGS - RH WING #5 SPOILER JACK RIB AT STA ABX 175.8
- [SDR FDEA202308081558](https://openairdocs.org/sdr/FDEA202308081558.md): Rib · corroded · Aug 8, 2023 · N652FE · Airbus A300* · Wing, Rib/Bulkhead
  > R/H WING SPOILER 5 BEAM I/B JACK RIB UPR BORE INNER FACE CORRODED ACCOMPLISHED THE REINFORCING REPAIR AT RH #5 SPOILER I/B JACK RIB I.A.W FEDEX EA NO:T6- 5740-T0375737 P1,SEQ NO:865, TITLE:WINGS - ATTACH FITTINGS - RH WING #5 SPOILER JACK RIB AT STA ABX 17
- [SDR FDEA202308081549](https://openairdocs.org/sdr/FDEA202308081549.md): Rib · gouged · Aug 8, 2023 · N652FE · Airbus A300* · Spoilers
  > R/H WING SPOILER 4 BEAM O/B JACK RIB UPR BORE INNER FACE GOUGE ACCOMPLISHED THE REINFORCING REPAIR AT RH #4 SPOILER O/B JACK RIB I.A.W FEDEX EA NO:T6-5740-T0375735 P1,SEQ NO:863, TITLE: WINGS - ATTACH FITTINGS - RH WING #4 SPOILER JACK RIB AT STA ABX 103.7
- [SDR FDEA202308061551](https://openairdocs.org/sdr/FDEA202308061551.md): Rib · corroded · Aug 6, 2023 · N652FE · Airbus A300* · Spoilers
  > LH WING NO.4 SPOILER I/B JACK RIB UPPER RIB BORE INNER SURFACE CORRODED ACCOMPLISHED THE REINFORCING REPAIR AT LH#4 SPOILER I/B JACK RIB I.A.W FEDEX EA NO:T6- 5740-T0375643 P1,SEQ NO:861, TITLE:WINGS - ATTACH FITTINGS - LH WING #4 SPOILER JACK RIB AT STA AB
- [SDR FDEA202308061370](https://openairdocs.org/sdr/FDEA202308061370.md): Seat Track · worn · Aug 6, 2023 · N652FE · Airbus A300* · Fuselage, Seat/Cargo Attach Fittings
  > FR54/FR54.2 LH NO.3 DUMMY SEAT TRACK FOUND GAP OVER 1.0MM AND LESS THAN 2.15MM. AUTUAL MEASUREMENT:1.27MM I.A.W A300-600F SRM 53-15-16-201-2 PARA 5A FIG.201 PAGE 201-210 PERFORM REPAIR ACCOMPLISHED.
- [SDR FDEA202308061369](https://openairdocs.org/sdr/FDEA202308061369.md): Seat Track · worn · Aug 6, 2023 · N652FE · Airbus A300* · Fuselage, Seat/Cargo Attach Fittings
  > FR54/FR54.2 RH NO.2 DUMMY SEAT TRACK FOUND GAP OVER 1.0MM AND LESS THAN 2.15MM. AUTUAL MEASUREMENT:1.22MM
- [SDR FDEA202308061368](https://openairdocs.org/sdr/FDEA202308061368.md): Seat Track · worn · Aug 6, 2023 · N652FE · Airbus A300* · Fuselage, Seat/Cargo Attach Fittings
  > FR54/FR54.2 RH NO.3 DUMMY SEAT TRACK FOUND GAP OVER 1.0MM AND LESS THAN 2.15MM. AUTUAL MEASUREMENT:1.27MM
- [SDR FDEA202308061367](https://openairdocs.org/sdr/FDEA202308061367.md): Seat Track · worn · Aug 6, 2023 · N652FE · Airbus A300* · Fuselage, Seat/Cargo Attach Fittings
  > FR54/FR54.2 RH NO.4 DUMMY SEAT TRACK FOUND GAP OVER 1.0MM AND LESS THAN 2.15MM. AUTUAL MEASUREMENT:1.44MM I.A.W A300-600F SRM 53-15-16-201-2 PARA 5A FIG.201 PAGE 201-210 PERFORM REPAIR ACCOMPLISHED.
- [SDR FDEA202308061366](https://openairdocs.org/sdr/FDEA202308061366.md): Seat Track · worn · Aug 6, 2023 · N652FE · Airbus A300* · Fuselage, Seat/Cargo Attach Fittings
  > FR54/FR54.2 RH NO.5 DUMMY SEAT TRACK FOUND GAP OVER 1.0MM AND LESS THAN 2.15MM. AUTUAL MEASUREMENT:1.09MM. I.A.W A300-600F SRM 53-15-16-201-2 PARA 5A FIG.201 PAGE 201-210 PERFORM REPAIR ACCOMPLISHED.
- [SDR FDEA202308061365](https://openairdocs.org/sdr/FDEA202308061365.md): Seat Track · worn · Aug 6, 2023 · N652FE · Airbus A300* · Fuselage, Seat/Cargo Attach Fittings
  > FR38.2/FR40 LH NO.3 DUMMY SEAT TRACK FOUND GAP OVER 1.0MM AND LESS THAN 2.15MM. AUTUAL MEASUREMENT:1.06MM. I.A.W A300-600F SRM 53-15-16-201-2 PARA 5A FIG.201 PAGE 201-210 PERFORM REPAIR ACCOMPLISHED.
- [SDR FDEA202308061364](https://openairdocs.org/sdr/FDEA202308061364.md): Seat Track · worn · Aug 6, 2023 · N652FE · Airbus A300* · Fuselage, Seat/Cargo Attach Fittings
  > FR38.2/FR40 LH NO.2 DUMMY SEAT TRACK FOUND GAP OVER 1.0MM AND LESS THAN 2.15MM. AUTUAL MEASUREMENT:1.57MM. I.A.W A300-600F SRM 53-15-16-201-2 PARA 5A FIG.201 PAGE 201-210 PERFORM REPAIR ACCOMPLISHED.
- [SDR FDEA202308061363](https://openairdocs.org/sdr/FDEA202308061363.md): Seat Track · worn · Aug 6, 2023 · N652FE · Airbus A300* · Fuselage, Seat/Cargo Attach Fittings
  > FR38.2/FR40 RH NO.2 DUMMY SEAT TRACK FOUND GAP OVER 1.0MM AND LESS THAN 2.15MM. AUTUAL MEASUREMENT:1.47MM. I.A.W A300-600F SRM 53-15-16-201-2 PARA 5A FIG.201 PAGE 201-210 PERFORM REPAIR ACCOMPLISHED.
- [SDR FDEA202308061362](https://openairdocs.org/sdr/FDEA202308061362.md): Seat Track · worn · Aug 6, 2023 · N652FE · Airbus A300* · Fuselage, Seat/Cargo Attach Fittings
  > FR38.2/FR40 RH NO.3 DUMMY SEAT TRACK FOUND GAP OVER 1.0MM AND LESS THAN 2.15MM. AUTUAL MEASUREMENT:1.09MM. I.A.W A300-600F SRM 53-15-16-201-2 PARA 5A FIG.201 PAGE 201-210 PERFORM REPAIR ACCOMPLISHED.
- [SDR FDEA202308051525](https://openairdocs.org/sdr/FDEA202308051525.md): Flap · cracked · Aug 5, 2023 · N652FE · Airbus A300* · Trailing Edge Flaps
  > 2EA CRACKS (30MM & 4MM) WERE FOUND AT L/H WING CENTER FLAP RIB26 AFT AREA OF TOP SURFACE RIB FLANGE. ACCOMPLISHED THE RIB FLANGE REPAIR AND LOWER SKIN EXTERNAL DOUBLERS REPAIR (LOWER SKIN CUT OUT WAS FOR ACCESS REQUIREMENT) I.A.W FEDEX EA NO:T6-5750-T03283
- [SDR FDEA202308051522](https://openairdocs.org/sdr/FDEA202308051522.md): Flap · cracked · Aug 5, 2023 · N652FE · Airbus A300* · Trailing Edge Flaps
  > 2EA CRACKS (30MM & 7MM) WERE FOUND AT L/H WING CENTER FLAP RIB25 AFT AREA OF TOP SURFACE RIB FLANGE. ACCOMPLISHED THE RIB FLANGES AND LOWER SKIN CUT OUT, REPAIRED WITH REPAIR ANGLES AND DOUBLERS (LOWER SKIN CUT OUT WAS FOR ACCESS REQUIREMENT) I.A.W FEDEX E
- [SDR FDEA202308041390](https://openairdocs.org/sdr/FDEA202308041390.md): Elevator · unknown · Aug 4, 2023 · N652FE · Airbus A300* · Elevator Structure
  > AIRCRAFT REPAIR ASSESSMENT: EXISTING COMPOSITE REPAIR FOUND ON LH ELEVATOR UPR SKIN AT ER7-12", T/E-5" POSITION COMPLIED WITH ATTACHMENT B OF EO:E6-5100-7-5000 D7 PT1, TITLE:STRUCTURES-REPAIR CATALOG-A300/A310 REPAIR IDENTIFICATION & TRACKING REQUIREMENTS
- [SDR FDEA202308041389](https://openairdocs.org/sdr/FDEA202308041389.md): Elevator · unknown · Aug 4, 2023 · N652FE · Airbus A300* · Elevator Structure
  > AIRCRAFT REPAIR ASSESSMENT: EXISTING COMPOSITE REPAIR FOUND ON LH ELEVATOR UPR SKIN AT ER10-24", T/E-5" POSITION COMPLIED WITH ATTACHMENT B OF EO:E6-5100-7-5000 D7 PT1, TITLE:STRUCTURES-REPAIR CATALOG-A300/A310 REPAIR IDENTIFICATION & TRACKING REQUIREMEN
- [SDR FDEA202308041388](https://openairdocs.org/sdr/FDEA202308041388.md): Elevator · unknown · Aug 4, 2023 · N652FE · Airbus A300* · Elevator Structure
  > AIRCRAFT REPAIR ASSESSMENT: EXISTING COMPOSITE REPAIR FOUND ON LH ELEVATOR UPR SKIN AT ER10 6", T/E-5" POSITION COMPLIED WITH ATTACHMENT B OF EO:E6-5100-7-5000 D7 PT1, TITLE:STRUCTURES-REPAIR CATALOG-A300/A310 REPAIR IDENTIFICATION & TRACKING REQUIREMENTS
- [SDR FDEA202308041387](https://openairdocs.org/sdr/FDEA202308041387.md): Elevator · unknown · Aug 4, 2023 · N652FE · Airbus A300* · Elevator Structure
  > AIRCRAFT REPAIR ASSESSMENT: EXISTING COMPOSITE REPAIR FOUND ON LH ELEVATOR UPR SKIN AT ER16 18", T/E-5.5" POSITION COMPLIED WITH ATTACHMENT B OF EO:E6-5100-7-5000 D7 PT1, TITLE:STRUCTURES-REPAIR CATALOG-A300/A310 REPAIR IDENTIFICATION & TRACKING REQUIREME
- [SDR FDEA202308041386](https://openairdocs.org/sdr/FDEA202308041386.md): Seat Track · unknown · Aug 4, 2023 · N652FE · Airbus A300* · Fuselage, Seat/Cargo Attach Fittings
  > AIRCRAFT REPAIR ASSESSMENT: EXISTING SPLICE REPAIR FOUND ON M/D SEAT TRACK BTW FR57-57.2, Y1456 COMPLIED WITH ATTACHMENT B OF EO:E6-5100-7-5000 D7 PT1, TITLE:STRUCTURES-REPAIR CATALOG-A300/A310 REPAIR IDENTIFICATION & TRACKING REQUIREMENTS 14 CFR 121.707,
- [SDR FDEA202308041385](https://openairdocs.org/sdr/FDEA202308041385.md): Seat Track · unknown · Aug 4, 2023 · N652FE · Airbus A300* · Fuselage, Seat/Cargo Attach Fittings
  > AIRCRAFT REPAIR ASSESSMENT: EXISTING SPLICE REPAIR FOUND ON M/D SEAT TRACK BTW FR28-30, Y450 COMPLIED WITH ATTACHMENT B OF EO:E6-5100-7-5000 D7 PT1, TITLE:STRUCTURES-REPAIR CATALOG-A300/A310 REPAIR IDENTIFICATION & TRACKING REQUIREMENTS 14 CFR 121.707,
- [SDR FDEA202308041384](https://openairdocs.org/sdr/FDEA202308041384.md): Seat Track · unknown · Aug 4, 2023 · N652FE · Airbus A300* · Fuselage, Seat/Cargo Attach Fittings
  > AIRCRAFT REPAIR ASSESSMENT: EXISTING SPLICE REPAIR FOUND ON M/D SEAT TRACK BTW FR28-30, Y0 COMPLIED WITH ATTACHMENT B OF EO:E6-5100-7-5000 D7 PT1, TITLE:STRUCTURES-REPAIR CATALOG-A300/A310 REPAIR IDENTIFICATION & TRACKING REQUIREMENTS 14 CFR 121.707, IN
- [SDR FDEA202308041377](https://openairdocs.org/sdr/FDEA202308041377.md): Angle · cracked · Aug 4, 2023 · N652FE · Airbus A300* · Fuselage Miscellaneous Structure
  > AFT CGO COMP'T CEILING PANEL SUPPORT ANGLE CRACK NEAR UPR FWD CORNER AREA BETWEEN FR60~61 POSITION. REMOVED CRACKED SUPPORT ANGLE AND INSTALLED NEW ONE. I.A.W A300-600F SRM 51-72-10- 001, PAGE.2 AND 51-40-21-001, PARA.6, PAGE.7B-23
- [SDR FDEA202308031383](https://openairdocs.org/sdr/FDEA202308031383.md): Flap · unknown · Aug 3, 2023 · N652FE · Airbus A300* · Trailing Edge Flaps
  > AIRCRAFT REPAIR ASSESSMENT: EXISTING DOUBLER REPAIR FOUND ON LH I/B FLAP LWR SKIN AT T/E RIB 14A,T/E-10" COMPLIED WITH ATTACHMENT B OF EO:E6-5100-7-5000 D7 PT1, TITLE:STRUCTURES-REPAIR CATALOG-A300/A310 REPAIR IDENTIFICATION & TRACKING REQUIREMENTS 14 CFR
- [SDR FDEA202308031382](https://openairdocs.org/sdr/FDEA202308031382.md): Aileron · unknown · Aug 3, 2023 · N652FE · Airbus A300* · Ailerons
  > AIRCRAFT REPAIR ASSESSMENT: EXISTING DOUBLER REPAIR FOUND ON RH WING AILERON LWR SKIN BTW RIB 2~3,T/E-7" COMPLIED WITH ATTACHMENT B OF EO:E6-5100-7-5000 D7 PT1, TITLE:STRUCTURES-REPAIR CATALOG-A300/A310 REPAIR IDENTIFICATION & TRACKING REQUIREMENTS 14 CFR
- [SDR FDEA202308031381](https://openairdocs.org/sdr/FDEA202308031381.md): Aileron · unknown · Aug 3, 2023 · N652FE · Airbus A300* · Ailerons
  > AIRCRAFT REPAIR ASSESSMENT: EXISTING DOUBLER REPAIR FOUND ON RH WING AILERON LWR SKIN BTW RIB 11~13,T/E-2.7" COMPLIED WITH ATTACHMENT B OF EO:E6-5100-7-5000 D7 PT1, TITLE:STRUCTURES-REPAIR CATALOG-A300/A310 REPAIR IDENTIFICATION & TRACKING REQUIREMENTS 14
- [SDR FDEA202308031380](https://openairdocs.org/sdr/FDEA202308031380.md): Flap · unknown · Aug 3, 2023 · N652FE · Airbus A300* · Trailing Edge Flaps
  > AIRCRAFT REPAIR ASSESSMENT: EXISTING DOUBLER REPAIR FOUND ON RH CENTER FLAP LWR SKIN BTW RIB 9~10,REAR SPAR DATUM 12" COMPLIED WITH ATTACHMENT B OF EO:E6-5100-7-5000 D7 PT1, TITLE:STRUCTURES-REPAIR CATALOG-A300/A310 REPAIR IDENTIFICATION & TRACKING REQUIR
- [SDR FDEA202308031378](https://openairdocs.org/sdr/FDEA202308031378.md): Support · damaged · Aug 3, 2023 · N652FE · Airbus A300* · Fuselage Miscellaneous Structure
  > AFT CGO CMPTR RH FR59A FOUND 1EA WIRE CONDUIT SUPPORT BROKEN REMOVED BROKEN WIRE CONDUIT SUPPORT, AND INSTALLED NEW ONE. I.A.W A300-600F SRM 51- 72-10-001, PAGE.2 AND 51-40-21-001, PARA.13, PAGE.149-156
- [SDR FDEA202308011488](https://openairdocs.org/sdr/FDEA202308011488.md): Skin · none · Aug 1, 2023 · N652FE · Airbus A300* · Fuselage Main, Plate/Skin
  > AIRCRAFT REPAIR ASSESSMENT: EXISTING DOUBLER REPAIR FOUND ON FUSELAGE SKIN BTW FR 19~20, STGR 52~54L COMPLIED WITH ATTACHMENT B OF EO:E6-5100-7-5000 D7 PT1, TITLE:STRUCTURES - REPAIR CATALOG - A300/A310 REPAIR IDENTIFICATION & TRACKING REQUIREMENTS 14 CFR
- [SDR FDEA202308011379](https://openairdocs.org/sdr/FDEA202308011379.md): Skin · unknown · Aug 1, 2023 · N652FE · Airbus A300* · Fuselage Main, Plate/Skin
  > AGING AIRCRAFT ASSESSMENT: EXISTING DOUBLER REPAIR FOUND ON FUSELAGE SKIN AT FR 27, BTW STGR 32~34R COMPLIED WITH ATTACHMENT B OF EO:E6-5100-7-5000 D7 PT1, TITLE:STRUCTURES-REPAIR CATALOG-A300/A310 REPAIR IDENTIFICATION & TRACKING REQUIREMENTS 14 CFR 121.
- [SDR FDEA202307301575](https://openairdocs.org/sdr/FDEA202307301575.md): Fitting · cracked · Jul 30, 2023 · N652FE · Airbus A300* · Cargo/Baggage Doors
  > THE MDC DOOR ACTUATOR YOKE BOTH SUPPORT FRAME WERE FOUND CRACK & BROKEN FABRICATED NEW SUPPORT FRAMES AND INSTALLED WITH FASTENERS I.A.W FEDEX EA NO:T6- 5230-T0375508 P1, SEQ NO:857, TITLE:DOORS - CARGO DOOR/HYD SYS - MAIN CARGO DOOR ACTUATOR BEARING FITTIN
- [SDR FDEA202307301414](https://openairdocs.org/sdr/FDEA202307301414.md): Fitting · cracked · Jul 30, 2023 · N652FE · Airbus A300* · Fuselage Miscellaneous Structure
  > AVIONICS COMP'T ACCESS DOOR STOP OMEGA FITTING CRACK. REPLACED FITTING WITH NEW ONE I.A.W A300-600F SRM 51-72-10-001, PAGE.2 AND 51-40-21-001, PARA.6, PAGE.7B-PAGE.23
- [SDR FDEA202303210479](https://openairdocs.org/sdr/FDEA202303210479.md): Fitting · cracked · Mar 21, 2023 · N652FE · Airbus A300* · Fuselage Main, Structure
  > (EA # 6-5315-T0328356 D P2) UPON OPEN-HOLE HFEC OF FR44RL FOOT, FOUND HOLE # H1 CRACKED WITHIN THE FWD FRAME LAYER AT THE 4:00 CLOCK POSITION, AS VIEWED LOOKING AFT: MARKED IN RED. COMPLIED WITH EA T-6-5315-T0328356 E P3 FUSELAGE-FRAME FOOT CRACK,FRAME FEE
- [SDR FDEA202207311831](https://openairdocs.org/sdr/FDEA202207311831.md): Pump · failed · Jul 31, 2022 · N652FE · Airbus A300F4605R · Hydraulic Pump (Electric/Engine), Main
  > AT GEAR RETRACTION, HYDRAULIC GREEN PUMP #2 LOW PRESSURE ANNUNCIATOR ON ECAM. GEAR RETRACTED SLOWER THAN NORMAL. AFTER GEAR FULLY UP AND RETRACTED THE LOW PRESSURE CAUTION WENT AWAY. REPEAT SQUAK. REPLACED #2 GREEN HYD. EDP IAW A300-600 AMM CH. 29-11-3
- [SDR FDEA202201070022](https://openairdocs.org/sdr/FDEA202201070022.md): Bulkhead · damaged · Jan 7, 2022 · N652FE · Airbus A300* · Fuselage Main, Structure
  > MDIS 652 53-10 4930 05JAN22 FNT OPEN U AFT PRESSURE BULKHEAD PUNCTURED AT LEFT SIDE, MAIN DECK FLOOR LEVEL, BY GUIDE BAR LEFT ABOARD FROM ONLOADING COMMANDER. SHGN 05JAN22 18:14 FNT U REMOVED MDC AFT LEFT BULKHEAD PARTITION TO ACCESS AND
- [SDR FDEA202201060149](https://openairdocs.org/sdr/FDEA202201060149.md): None · unknown · Jan 6, 2022 · N652FE · Airbus A300* · Door Warning System
  > L1 AND R1 ESCAPE SLIDE INDICATOR WARNING LIGHTS WILL NOT TEST REPLACED ASPSU IAW AMM 52-73-18-04-0, OPS CKS GOOD, MEL REMOVED
- [SDR FDEA202112073042](https://openairdocs.org/sdr/FDEA202112073042.md): Battery · failed · Dec 7, 2021 · N652FE · Airbus A300* · Passenger/Crew Doors
  > R1 DOOR SLIDE WILL NOT ARM.. RELEASED FOR SERVICE PER MEL: 52-XX-XX CATEGORY: C EXPIRATION: 15DEC21 "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 DEPARTUR
- [SDR FDEA202105201319](https://openairdocs.org/sdr/FDEA202105201319.md): Elevator · damaged · May 20, 2021 · N652FE · Airbus A300F4605R · Elevator, Plate/Skin
  > 1. 2 EA WATER TRAPPED AREAS (50MM X 50MM)(50MM X 50MM) WERE FOUND AT NO.22 & NO.28 FASTENER OF LH ELEVATOR UPPER SKIN PANEL. 2. 2 EA WATER TRAPPED AREAS WERE FOUND AT NO.2 & NO.7 FASTENER OF LH ELEVATOR LWR SKIN PANEL. THE MAX WATER TRAPPED AREA IS 50MM X
- [SDR FDEA202105201314](https://openairdocs.org/sdr/FDEA202105201314.md): Elevator · damaged · May 20, 2021 · N652FE · Airbus A300F4605R · Elevator Structure
  > 1.1EA WATER TRAPPED AREA(120MM*75MM) WAS FOUND AT NO.22 FASTENER OF LH ELEVATOR LWR SKIN PANEL. 2.2EA WATER TRAPPED AREA WERE FOUND AT NO.27 & NO.38 FASTENER OF LH ELEVATOR UPR SKIN PANEL. THE MAX WATER TRAPPED AREA IS 70MM*65MM. THE FASTENER NO COUNTI
- [SDR FDEA202105191297](https://openairdocs.org/sdr/FDEA202105191297.md): Skin · cracked · May 19, 2021 · N652FE · Airbus A300F4605R · Ailerons
  > RH WING ALL SPEED AILERON UPR SURFACE GOT A NICK AT T/E O/B SECTION AS MARK I.A.W. EA #6-5750-155229A PART:2 (P2) TITLE: WINGS - FLIGHT SURFACES - ALL SPEED AILERON UPPER AND LOWER SKIN REPAIRS ACCOMPLISHED THE WORK.
- [SDR FDEA202105191295](https://openairdocs.org/sdr/FDEA202105191295.md): Floor Panel · dented · May 19, 2021 · N652FE · Airbus A300F4605R · Fuselage Floor Panel
  > THE #132PG FLOOR PANEL OF LOWER FWD CARGO COMPPARTMENT WAS FOUND LOWER SURFACE SEVERAL DENT WITH MARK REPAIRED THE DAMAGED AREA WITH RESIN AND FIBERGLASS I.A.W A300-600F SRM 53-10-20- 201 PARA8B FIG203 SHEET1
- [SDR FDEA202105181263](https://openairdocs.org/sdr/FDEA202105181263.md): Floor Panel · broken · May 18, 2021 · N652FE · Airbus A300F4605R · Fuselage Floor Panel
  > THE #131PG FLOOR PANEL OF LOWER FWD CARGO COMPPARTMENT WAS FOUND BROKEN REPAIRED THE DAMAGED AREA WITH RESIN AND FIBERGLASS I.A.W A300-600F SRM 53-10-20- 201 PARA.8B FIG.203 SHEET1.
- [SDR FDEA202105181283](https://openairdocs.org/sdr/FDEA202105181283.md): Floor Panel · damaged · May 18, 2021 · N652FE · Airbus A300F4605R · Fuselage Floor Panel
  > THE #241PF FLOOR PANEL OF MAIN DECK COMPARTMENT WAS FOUND EDGE DAMAGED WITH MARK REPAIRED THE FLOOR PANEL I.A.W A300-600F SRM 53-10-20-201 P201~205 & P208 & FIG201

Next page: https://openairdocs.org/aircraft/N652FE/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 = 'N652FE' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N652FE/reports

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