# Service difficulty reports: N650FE

A list on [N650FE](https://openairdocs.org/aircraft/N650FE.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 5 · 219 reports

- [SDR FDEA202512192263](https://openairdocs.org/sdr/FDEA202512192263.md): Wire · loose · Dec 19, 2025 · N650FE · Airbus A300F4605R · Door System Wiring
  > R1 DOOR WARNING HORN DOES NOT COME ON WHILE USING PRESS TO TEST SWITCH, DOOR WARNING LIGHT FLASHES DURING TEST. AWM: 52-73-01 ESPM: CH. 20 FOUND WIRE W5273-1085-22 PULLED LOOSE FROM TERMINAL ON R1 DOOR PUSH BUTTON TEST SWITCH (40WN). RETERMINATE SAME, SW
- [SDR FDEA202511142179](https://openairdocs.org/sdr/FDEA202511142179.md): Oxygen Bottle · low pressure · Nov 14, 2025 · N650FE · Airbus A300F4605R · Crew Oxygen System
  > NR 4 O2 BELOW 1500PSI, REQUIRES SERVICING. REPLENISHED CREW OXYGEN IAW AMM 12-14-35-00. NO LEAKS DETECTED AT THIS TIME. ACFT OK FOR SERVICE.
- [SDR FDEA202509221765](https://openairdocs.org/sdr/FDEA202509221765.md): Power Supply · no test · Sep 22, 2025 · N650FE · Airbus A300F4605R · Emergency Lighting
  > ENTRY AREA EMERGENCY EXIT LIGHTS WON'T TEST OR LIGHT UP DURING PREFLIGHT. SUSPECT ESPU BATTERY. FOUND EMERGENCY POWER SUPPLY UNIT WON'T BITE TEST. REPLACED POWER SUPPLY UNIT BATTERY REF A300 AMM 33-51-14-04. EMERGENCY LIGHTS AND POWER SUPPLY UNIT TESTS G
- [SDR FDEA202505020710](https://openairdocs.org/sdr/FDEA202505020710.md): Switch · failed · May 2, 2025 · N650FE · Airbus A300F4605R · Leading Edge Slat Control System
  > KRUGER NOT RETRACTED FAULT AT FL 350 AND.79 MACH. COMPLIED WITH QRH / ECAM DESCENDED TO 290/.65 MACH. AMM: 27-87-00-09 TSM: 27-80-00 AMM: 05-51-13-00 SFCC 1 AND 2 HAD FAULT BALL IN "L/H RETRACT SW". REACTIVATEED KRUEGER FLAP SYSTEM AND PERFORMED LEAK
- [SDR FDEA202503250496](https://openairdocs.org/sdr/FDEA202503250496.md): Arming Lever · out of adjust · Mar 25, 2025 · N650FE · Airbus A300F4605R · Passenger/Crew Doors
  > THE R1 MAIN ENTRANCE DOOR SLIDE WILL NOT ARM. RELEASED FOR SERVICE PER MEL: 52-XX-XX CAT: C EXP: 04APR25 "MEL 52-XX-XX4: ECAM SLIDE INDICATION SYSTEM FOR R1 DOOR - INOP. DOOR ESCAPE SLIDE ARMING SYSTEM IS TO BE VERIFIED AS FULLY ARMED PRIOR TO EACH
- [SDR FDEA202502200252](https://openairdocs.org/sdr/FDEA202502200252.md): Slide · inoperative · Feb 20, 2025 · N650FE · Airbus A300F4605R · Escape Slide
  > D31023-101 MSN: 423TH POS: L1 REMOVE AND REPLACE L1 DR SLIDE/RAFT. REPLACED THE SLIDE/RAFT OF L1 CREW DOOR PER AMM 25-61-22-04-01. MINOR REPAIR IAW FEDEX GMM 6-2-100.
- [SDR FDEA202502140224](https://openairdocs.org/sdr/FDEA202502140224.md): Pressure Deck · corroded · Feb 14, 2025 · N650FE · Airbus A300F4605R · Fuselage Main, Structure
  > FWD CARGO HORIZONTAL PRESSURE DECK UPPER SURFACE CORRODED AT FR40 Y-953 - Y0. COMPLIED WITH EA: 6-5310-T0382182 P1. TITLE: FUSELAGE - MAINFRAME- EXFOLIATED CORROSION ON HORIZONTAL PRESSURE FLOOR PANEL BETWEEN FR39-FR40. REPAIRED THE CORRODED PANEL AT HORI
- [SDR FDEA202501290148](https://openairdocs.org/sdr/FDEA202501290148.md): Pressure Deck · corroded · Jan 29, 2025 · N650FE · Airbus A300F4605R · Fuselage Main, Structure
  > FWD CARGO HORIZONTAL PRESSURE DECK UPPER SURFACE CORRODED AT FR40 Y953 - Y1456. COMPLIED WITH EA: 6-5310-T0382182 P1. TITLE: FUSELAGE - MAINFRAME- EXFOLIATED CORROSION ON HORIZONTAL PRESSURE FLOOR PANEL BETWEEN FR39-FR40. REPAIRED THE CORRODED PANEL AT HO
- [SDR FDEA202501240129](https://openairdocs.org/sdr/FDEA202501240129.md): Hinge Arm · delaminated · Jan 24, 2025 · N650FE · Airbus A300F4605R · Spoilers
  > RH WING - #4 SPOILER CENTER O/B HINGE ARM OUTBD FOUND DELAMINATION. (AREA: 18MM*18MM, DEPTH:1.60MM) PERFORMED THE REPAIR ON RH WING #4 SPOILER CENTER O/B HINGE ARM OUTBD PER FEDEX EA:6-5750-T0382101 P1 & SB A300-57-6082 R03 FIGURE 2 SHEET 2 & 4 AND FIGURE
- [SDR FDEA202501240126](https://openairdocs.org/sdr/FDEA202501240126.md): Hinge Arm · delaminated · Jan 24, 2025 · N650FE · Airbus A300F4605R · Spoilers
  > LH WING - #3 SPOILER CENTER O/B HINGE ARM OUTBD DELAMINATION. (AREA: 25MM*12MM, DEPTH:1.25MM) PERFORMED THE REPAIR ON LH WING #3 SPOILER CENTER O/B HINGE ARM OUTBD PER FEDEX EA:6-5750-T0382100 P1 & SB A300-57-6082 R03 FIGURE 2 SHEET 2 & 4 AND FIGURE 5. EA
- [SDR FDEA202501240125](https://openairdocs.org/sdr/FDEA202501240125.md): Web · cracked · Jan 24, 2025 · N650FE · Airbus A300F4605R · Fuselage Miscellaneous Structure
  > MDCC UNDER FLOOR PANEL - FR47, Y953-Y1456 FOUND 1EA WEB CRACKED. REPAIRED THE CRACKED WEB AT MDCC UNDER FLOOR PANEL FR47, Y953-Y1456 PER A300-600F SRM53-15-15-201 FIG201. THIS IS CAT B REPAIR AND MUST BE INSPECTED AT DEFINED INTERVALS PER SRI53-15-15-2-002
- [SDR FDEA202501240124](https://openairdocs.org/sdr/FDEA202501240124.md): Frame · cracked · Jan 24, 2025 · N650FE · Airbus A300F4605R · Fuselage Main, Frame
  > NDT INSP - RH CENTER WING BOX REAR SPAR FR47 BOTTOM PANEL "C" HOLE FOUND CRACKED SINGAL. COMPLIED WITH EA: 6-5710-T0381607 P1. TITLE: WINGS - BASIC WING STRUCTURE - LH WING FR47 REAR SPAR HOLE G CRACK REPAIR - SB A300-57-6113. REPAIRED THE CENTER WING BOX
- [SDR FDEA202501220119](https://openairdocs.org/sdr/FDEA202501220119.md): Rib · cracked · Jan 22, 2025 · N650FE · Airbus A300F4605R · Trailing Edge Flaps
  > RH WING CENTER FLAP RIB UPR FLANGE FOUND CRACK AT RIB27 BETWEEN STGR2.6 AND STGR2.7. REPAIRED RH WING CENTER FLAP RIB UPR FLANGE CRACK AT RIB27 BETWEEN STGR2.6 AND STGR2.7 PER A300-600F SRM57-50-00-201 FIG201 & FIG205. THIS IS CAT A REPAIR. EA:6-5750- T0
- [SDR FDEA202501210109](https://openairdocs.org/sdr/FDEA202501210109.md): Crossbeam · cracked · Jan 21, 2025 · N650FE · Airbus A300F4605R · Fuselage Main, Structure
  > MDCC CROSSBEAM C31,-Y700 CRACKED. REPAIRED THE CROSSBEAM AT C31, -Y700 PER A300-600F SRM53-10-15-201 FIG212 & EA:6-5310- T0381895 P1. TITLE: FUSELAGE - MAINFRAME - CRACK ON FR31 CROSSBEAM, BETWEEN -Y450 AND -Y953. THIS IS A CAT A REPAIR. MAJOR REPAIR IAW FE
- [SDR FDEA202501210108](https://openairdocs.org/sdr/FDEA202501210108.md): Stringer · corroded · Jan 21, 2025 · N650FE · Airbus A300F4605R · Fuselage Main, Longeron/Stringer
  > FWD CARGO FR38.2 - FR39, S44R STRINGER CORRODED. REPAIRED THE CORRODED STRINGER AT FR38.2 - FR39, S44R PER A300-600F SRM53-10-14. THIS IS CAT B REPAIR AND MUST BE INSPECTED AT DEFINED INTERVALS PER A300-600F SRI53-10-14-2-008- 00. FIRST INSP AFTER REPAIR EM
- [SDR FDEA202312141938](https://openairdocs.org/sdr/FDEA202312141938.md): Power Supply · failed · Dec 14, 2023 · N650FE · Airbus A300* · Emergency Lighting
  > "EMERG TEST" P/BSW (25WL) DOES NOT ILLUMINATE & EMERGENCY LIGHTS REMAIN ILLUMINATED WHEN TEST CYCLE IS ENERGIZED. FACT 14DEC23 14:10 MSN U AMM: 33-51-14-04-0 RED LED FAULT LIGHT ILLUMINATED ON EPSU REMOVED AND REPLACED POWER SUPPLY UNIT (29WL) IAW
- [SDR FDEA202209242717](https://openairdocs.org/sdr/FDEA202209242717.md): None · none · Sep 24, 2022 · N650FE · Airbus A300F4605R · Standard Practices/Structures
  > AGING AIRCRAFT ASSESSMENT:EXISTING DOUBLER REPAIR FOUND ON RH WING #1 SPOILER UPR SKIN I/B EDGE MID SECTION. REMOVED THE UNDOCUMENTED EXISTING DOUBLER REPAIR ON RH #1 SPOILER UPR SKIN I/B EDGE AERA AND PERFORMED NEW REPAIR WITH PRE-CURED CFRP DOUBLER I.A.W
- [SDR FDEA202209242716](https://openairdocs.org/sdr/FDEA202209242716.md): None · none · Sep 24, 2022 · N650FE · Airbus A300F4605R · Standard Practices/Structures
  > AGING AIRCRAFT ASSESSMENT:EXISTING DOUBLER REPAIR FOUND ON RH WING #1 SPOILER UPR SKIN O/B EDGE MID SECTION. REMOVED THE UNDOCUMENTED EXISTING DOUBLER REPAIR ON RH #1 SPOILER UPR SKIN O/B EDGE AERA AND PERFORMED NEW REPAIR WITH PRE-CURED CFRP DOUBLER I.A.W
- [SDR FDEA202209212710](https://openairdocs.org/sdr/FDEA202209212710.md): Spar · damaged · Sep 21, 2022 · N650FE · Airbus A300F4605R · Spoilers
  > LH WING #2 SPOILER FRONT SPAR O/B FACE GOT ABRASION. ACCOMPLISHED THE REPAIR WITH DOUBLER, FILLER AND SHIM. THIS IS CAT.A REPAIR I.A.W EA NO:6-5750-T0370876P1, SEQ NO:000654, TITLE:WING-FLIGHT SURFACES-LH #2 SPOILER OUTBOARD FACE OF THE FRONT SPAR AT RI
- [SDR FDEA202209152325](https://openairdocs.org/sdr/FDEA202209152325.md): None · worn · Sep 15, 2022 · N650FE · Airbus A300* · Fuselage Main, Structure
  > FR54/FR54.2 LH NO.5 DUMMY SEAT TRACK SLOT GAP OVER GAP VALUE(A) 0.0393 INCHES(1.0MM) BUT LESS THAN 0.0846 INCHES(2.15MM) SLOT GAP ACTUAL VALUE 1.21MM. I.A.W A300-600 SRM 53-15-16-201 PARA 5A FIG.201 PAGE 201-210 PERFORM RAIL HOLE REPAIR ACCOMPLISHED.
- [SDR FDEA202209092795](https://openairdocs.org/sdr/FDEA202209092795.md): Fitting · damaged · Sep 9, 2022 · N650FE · Airbus A300F4605R · Cargo/Baggage Doors
  > MAIN DECK CARGO DOOR ACTUATING MECHANISM SUPPORT YOKE ASSY DOOR FRAME WAS FOUND FWD AND AFT BROKEN ACCOMPLISHED THE MDC DOOR ACTUATOR FITTING (FWD & AFT) REPLACEMENT &SKIN INNER REPAIRE, THIS IS CAT.C MAJOR REPAIR I.A.W EA NO:6-5230-T0370856A P1, SEQ NO:00
- [SDR FDEA2020073011395](https://openairdocs.org/sdr/FDEA2020073011395.md): Wire Harness · damaged · Jul 1, 2020 · N650FE · Airbus A300F4605R · Engine Exhaust System Wiring
  > NR 2 ENGINE REVERSER PRESSURIZED. REMOVED AND INSTALLED A NEW DPV IAW AMM 78-31-06-2 UP TO PART F (1) SUB. C. R & R THE NR 2 PRSOV IAW MM 78-31-05-04, INSTALLED NR 2 ENG.LT THRUST REVERSER CDU SWITCH ASSEMBLY IAW AMM 78-31-04-04. REPLACED THE RIGHT THRUS
- [SDR FDEA2020070211395](https://openairdocs.org/sdr/FDEA2020070211395.md): Thrust Reverser · unknown · Jul 1, 2020 · N650FE · Airbus A300F4605R · Engine Thrust Reverser
  > NR 2 ENG REV PRESSURIZED.
- [SDR FDEA2020052961051](https://openairdocs.org/sdr/FDEA2020052961051.md): Window Frame · gouged · May 26, 2020 · N650FE · Airbus A300F4605R · Fuselage Main, Structure
  > CAPTAIN'S WINDSHIELD FRAME WORK AT LOWER INBD SIDE, FASTENER HOLE GOUGED. ACCOMPLISHED REPAIR IAW EA 6-5310-T0353313. MAJOR REPAIR CAT C REPAIR. FUSELAGE, MAIN FRAME AND WINDSHIELD CENTER POST HOLE DOUBLE DRILLED CRACK INDICATION INTERIM REPAIR.
- [SDR FDEA202005261047](https://openairdocs.org/sdr/FDEA202005261047.md): Bulkhead · damaged · May 26, 2020 · N650FE · Airbus A300F4605R · Fuselage Main, Bulkhead
  > PUNCTURED SECTION OF AFT BULKHEAD AFT OF FWD CARGO COMPT LT SIDE ALONG ELECTIRCAL WIRES ATTACHMENT BRACKET 4EA. REPAIR IS ACCOMPLISHED IAW EA 6-5310-T0353322. MAJOR REPAIR CAT "A" REPAIR. FUSELAGE - MAINFRAME - FR39 - PRESSURE BULKHEAD - GOUGES / PUNCTURES - B
- [SDR FDEA2020052621034](https://openairdocs.org/sdr/FDEA2020052621034.md): Window Frame · gouged · May 22, 2020 · N650FE · Airbus A300F4605R · Fuselage Main, Structure
  > CAPT'S WINDSHIELD FRAMEWORK AT LOWER INBD SIDE, FASTENER HOLE GOUGED. ACCOMPLISHED REPAIR PER EA 6-5310-T0353313. MAJOR REPAIR CAT "C" REPAIR. FUSELAGE - MAINFRAME - WINDSHIELD CENTER POST HOLE DOUBLE DRILLED / CRACK INDICATION. INTERIM REPAIR.
- [SDR FDEA2020052660963](https://openairdocs.org/sdr/FDEA2020052660963.md): Fitting · corroded · May 16, 2020 · N650FE · Airbus A300F4605R · Nacelle/Pylon Miscellaneous Structure
  > PITTING CORROSION AT NR 2 ENG FWD MOUNT PYRAMID FITTING O/B AFT HOLE UPPER FLANGE. ACCOMPLISHED EA 6-5450-T0353224 REPAIR. NACELLES / PYLON WING PYLON / STRUT. RIGHT HAND PYLON, FWD ENG MOUNT AFT OUTBD HOLE CORROSION REPAIR CAT "A" REPAIR MAJOR REPAIR.
- [SDR FDEA2020052660962](https://openairdocs.org/sdr/FDEA2020052660962.md): Fitting · corroded · May 16, 2020 · N650FE · Airbus A300F4605R · Nacelle/Pylon Miscellaneous Structure
  > NR 1 PYLON SPIGOT RECEPTACLE FITTING SPHERICAL BEARING/BUSHING CONTACT INSIDE SURFACE HAS RUST/CORROSION. ACCOMPLISHED REPAIR IAW EA 6-5410-T0353242. NACELLES / PYLONS - TAIL AUX NAC STRUCTURE - NR 1 PYLON SPIGOT RECEPTACLE CORROSION REPAIR, FITTING REPLACEMEN
- [SDR FDEA2020052260962](https://openairdocs.org/sdr/FDEA2020052260962.md): Fitting · corroded · May 16, 2020 · N650FE · Airbus A300F4605R · Nacelle/Pylon Miscellaneous Structure
  > #1 PYLON SPIGOT RECEPTACLE FITTING SPHERICAL BEARING/BUSHING CONTACT INSIDE SURFACE HAS RUST/CORROSION. ACCOMPLISHED REPAIR IAW EA # 6-5410-T0353242. MAJOR REPAIR CAT"A" REPAIR
- [SDR FDEA2020051860963](https://openairdocs.org/sdr/FDEA2020051860963.md): Fitting · corroded · May 16, 2020 · N650FE · Airbus A300F4605R · Nacelle/Pylon Miscellaneous Structure
  > PITTING CORROSION AT NO. 2 ENG FWD MOUNT PYRAMID FITTING O/B AFT HOLE UPPER FLANGE. ACCOMPLISHED EA # 6-5450-T0353224 REPAIR. CAT "A" REPAIR MAJOR REPAIR
- [SDR FDEA2020051860962](https://openairdocs.org/sdr/FDEA2020051860962.md): Fitting · corroded · May 16, 2020 · N650FE · Airbus A300F4605R · Nacelle/Pylon Miscellaneous Structure
  > #1 PYLON SPIGOT RECEPTACLE FITTING SPHERICAL BEARING/BUSHING CONTACT INSIDE SURFACE HAS RUST/CORROSION. ACCOMPLISHED REPAIR IAW EA # 6-5410-T0353242. MAJOR REPAIR CAT"A" REPAIR
- [SDR FDEA2020052670910](https://openairdocs.org/sdr/FDEA2020052670910.md): Fitting · corroded · May 7, 2020 · N650FE · Airbus A300F4605R · Nacelle/Pylon Miscellaneous Structure
  > NR 2 ENG PYLON SPIGOT FITTING RECEPTACLE HAS CORROSION. ACCOMPLISHED FINAL EA 6-5450-T0353280. NACELLES / PYLONS - WING PYLON / STRUT - RT WING TO PYLON SPIGOT RECEPTACLE CORROSION REPAIR, FITTING REPLACEMENT PER SB A300-54-6017 CAT "A" MAJOR REPAIR.
- [SDR FDEA2020050870910](https://openairdocs.org/sdr/FDEA2020050870910.md): Fitting · corroded · May 7, 2020 · N650FE · Airbus A300F4605R · Nacelle/Pylon Miscellaneous Structure
  > #2 ENG PYLON SPIGOT FITTING RECEPTACLE HAS CORROSION. ACCOMPLISHED FINAL E.A. 6-5450-T0353280. CAT "A" MAJOR REPAIR
- [SDR FDEA202004200760](https://openairdocs.org/sdr/FDEA202004200760.md): Fitting · cracked · Apr 20, 2020 · N650FE · Airbus A300F4605R · Fuselage Miscellaneous Structure
  > BULK CARGO FLOOR AT STA. Y140, FRAME 66 HAS ANCHOR PLATE FITTING CRACKED AND ELONGATED HOLE. REMOVED AND REPLACED ANCHOR PLATE FITTING IAW SRM 51-40-21. RECEIVED NEW FITTING ON TRAVELER # T20/1487312. P/N FX-A53974325213. LOCATED AND DRILLED IAW SRM 51-4
- [SDR FDEA202004200759](https://openairdocs.org/sdr/FDEA202004200759.md): Seat Track · corroded · Apr 20, 2020 · N650FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach Fittings
  > MAIN DECK FLR STRUCTURE BETWEEN FR26 & FR27 ON SEAT TRACK AT Y450 IS CORRODED. REMOVED & REPLACED SEAT TRACK IAW SRM 51-40-21 AND AIRBUS DWG A538781975. CORROSION FOUND OUT OF LIMITS IAW SRM 53-10-16 FIG 102. CAT "A" REPAIR MAJOR REPAIR
- [SDR FDEA2020042070757](https://openairdocs.org/sdr/FDEA2020042070757.md): Floorbeam · corroded · Apr 17, 2020 · N650FE · Airbus A300F4605R · Fuselage Main, Floor Beam
  > FUSE INTR STRUCTURE FR 69, ABOVE STGR RH 51 FLOOR BEAM HAS INTERGRANULAR CORROSION. REMOVED CORR. FOUND OUT OF LIMITS. CUT OUT DAMAGE IAW SRM 51-73-10 & 53-10-15. RECEIVED REPAIR ANGLE ON TRAVELER # T20/1486890 & REPAIR SPLICE ON TRAVELER # T20/1486887.
- [SDR FDEA202004100730](https://openairdocs.org/sdr/FDEA202004100730.md): Floor Support · corroded · Apr 10, 2020 · N650FE · Airbus A300F4605R · Fuselage Miscellaneous Structure
  > AFT CARGO PIT FR58 R/H SIDE JUST INBOARD OF -Y1456 FLOOR SUPPORT UPPER FLANGE HAS CORROSION. REMOVED DAMAGED SECTION OF FLOOR SUPPORT IAW A300-600 SRM 53-10-15. FABRICATED 1EA REPAIR ANGLE AND FILLER USING P/N AND10136-2407 IAW A300-600 SRM 53-10-15. LOC
- [SDR FDEA202004100731](https://openairdocs.org/sdr/FDEA202004100731.md): Seat Track · corroded · Apr 10, 2020 · N650FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach Fittings
  > MAIN DECK FLOOR STRUCTURE BETWEEN FR27 AND FR28, SEAT TRACK AT Y1959 IS CORRODED. REMOVED CORROSION IAW SRM 51-74-10. FOUND TO BE OUT OF LIMITS IAW SRM 53-10-16 FIG 102. REMOVED AND REPLACED Y1959 SEAT TRACK SECTION BETWEEN FR26.5 TO FR32 IAW SRM 53-10-1
- [SDR FDEA2020040630679](https://openairdocs.org/sdr/FDEA2020040630679.md): Floor Panel · damaged · Apr 3, 2020 · N650FE · Airbus A300F4605R · Fuselage Floor Panel
  > AFT CARGO FLOOR PANEL 152PF HAS EDGE DAMAGE. FABRICATED FLOOR PANEL 152PF ON TRAVELER T20/1483878 PER DWG SRZ 25-005. P/N FX- A5327990200000 PART MARKED ON PANEL PER CMM 07-0-1001.
- [SDR FDEA2020040630677](https://openairdocs.org/sdr/FDEA2020040630677.md): Floor Panel · cracked · Apr 3, 2020 · N650FE · Airbus A300F4605R · Fuselage Floor Panel
  > AFT CARGO FLOOR PANEL 152QF HAS A CRACK. FABRICATED FLOOR PANEL 152QF ON TRAVELER T20/1483817 PER DWG SRZ 25-005. P/N FX- R532B114200000 PARTMARKED ON PANEL PER GMM 07-0-1001. (MAJOR REPAIR)
- [SDR FDEA2020040630683](https://openairdocs.org/sdr/FDEA2020040630683.md): Floor Panel · damaged · Apr 3, 2020 · N650FE · Airbus A300F4605R · Fuselage Floor Panel
  > AFT CARGO FLOOR PANEL 161CF HAS EDGE DAMAGE. FABRICATED FLOOR PANEL 161CF ON TRAVELER T20/1483402 PER DWG SRZ 25-005. P/N FX- A5327996400200 PART MARKED ON FLOOR PANEL PER GMM 07-0-1001. (MAJOR REPAIR)
- [SDR FDEA2020040630682](https://openairdocs.org/sdr/FDEA2020040630682.md): Floor Panel · delaminated · Apr 3, 2020 · N650FE · Airbus A300F4605R · Fuselage Floor Panel
  > AFT CARGO FLOOR PANEL 161HF HAS EDGE DELAMINATION. FABRICATED FLOOR PANEL 161HF ON TRAVELER T20/1483403 PER DWG SRZ 25-005. P/N FX- A531799100200 PART MARKED ON PANEL PER GMM 07-0-1001. (MAJOR REPAIR)
- [SDR FDEA2020040630681](https://openairdocs.org/sdr/FDEA2020040630681.md): Floor Panel · damaged · Apr 3, 2020 · N650FE · Airbus A300F4605R · Fuselage Floor Panel
  > AFT CARGO FLOOR PANEL 152WF HAS EDGE DAMAGE. FABRICATED FLOOR PANEL 152WF ON TRAVELER T20/1483871 PER DWG SRZ 25-005. P/N FX- R532B114800000 PART MARKED ON FLOOR PANEL PER GMM 07-0-1001. (MAJOR REPAIR)
- [SDR FDEA2020040630680](https://openairdocs.org/sdr/FDEA2020040630680.md): Floor Panel · damaged · Apr 3, 2020 · N650FE · Airbus A300F4605R · Fuselage Floor Panel
  > AFT CARGO FLOOR PANEL 152MF HAS DAMAGE. FABRICATED FLOOR PANEL 152MF ON TRAVELER T20/1483853 PER DWG SRZ 25-005. P/N FX- A53279900200200 PART MARKED ON PANEL PER GMM 07-0-1001. (MAJOR REPAIR)
- [SDR FDEA2020040630678](https://openairdocs.org/sdr/FDEA2020040630678.md): Floor Panel · damaged · Apr 3, 2020 · N650FE · Airbus A300F4605R · Fuselage Floor Panel
  > AFT CARGO FLOOR PANEL 151QF HAS EDGE DAMAGE. FABRICATED FLOOR PANEL 151QF ON TRAVELER T20/1483838 PER DGW SRZ 25-005. PANEL PART # FZ-R532B114300000 PART MARKED ON PANEL PER GMM 07-0-1001. (MAJOR REPAIR)
- [SDR FDEA202004030675](https://openairdocs.org/sdr/FDEA202004030675.md): Floor Panel · cracked · Apr 3, 2020 · N650FE · Airbus A300F4605R · Fuselage Floor Panel
  > FWD CARGO FLOOR PANEL 132KG HAS A CRACK. FABRICATED FLOOR PANEL 132KG ON TRAVELER T20/1483240 PER DWG SRZ 25-005. P/N FX- A53279977002 PART MARKED ON PANEL PER GMM 07-0-1001. (MAJOR REPAIR)
- [SDR FDEA202004030673](https://openairdocs.org/sdr/FDEA202004030673.md): Floor Panel · cracked · Apr 3, 2020 · N650FE · Airbus A300F4605R · Fuselage Floor Panel
  > FWD CARGO FLOOR PANEL 131QG HAS A CRACK. FABRICATED FLOOR PANEL 131QG ON TRAVELER T20/1483090 PER DWG SRZ 25-005. P/N FX- R532B113500000 PART MARKED ON PANEL PER GMM 07-0-1001. MAJOR REPAIR
- [SDR FDEA202004030672](https://openairdocs.org/sdr/FDEA202004030672.md): Floor Panel · cracked · Apr 3, 2020 · N650FE · Airbus A300F4605R · Fuselage Floor Panel
  > FWD CARGO FLOOR PANEL 131MG HAS A CRACK. FABRICATED FLOOR PANEL 131MG ON TRAVELER T20/1283234 PER DWG SRZ-25-005. P/N FX- A53279978002 PART MARKED ON FLOOR PANEL PER GMM 07-0-1001. MAJOR REPAIR
- [SDR FDEA202004030664](https://openairdocs.org/sdr/FDEA202004030664.md): Floor Panel · cracked · Apr 3, 2020 · N650FE · Airbus A300F4605R · Fuselage Floor Panel
  > FWD CARGO 131KG FLOOR PANEL HAS CRACK FABRICATED FLOOR PANEL 131KG ON TRAVELER T20/1483401 FROM DWG SRZ-25-005. FX - A53279977002. P/N PART MARKED ON FLOOR PANEL PER GMM 07-0-1001 CAT "A" MAJOR REPAIR
- [SDR FDEA202004030663](https://openairdocs.org/sdr/FDEA202004030663.md): Floor Panel · cracked · Apr 3, 2020 · N650FE · Airbus A300F4605R · Fuselage Floor Panel
  > FWD CARGO 131LG FLOOR PANEL HAS CRACK FABRICATED FLOOR PANEL 131LG ON TRAVELER T20/1483404 FROM DWG SRZ-25-005. FX - R532B113100000 P/N PART MARKED ON FLOOR PANEL PER GMM 07-0-1001 CAT "A" MAJOR REPAIR

Next page: https://openairdocs.org/aircraft/N650FE/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 = 'N650FE' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N650FE/reports

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