# Service difficulty reports: N683FE

A list on [N683FE](https://openairdocs.org/aircraft/N683FE.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 6 · 289 reports

- [SDR FDEA202411011628](https://openairdocs.org/sdr/FDEA202411011628.md): Floorboard · damaged · Nov 1, 2024 · N683FE · Airbus A300F4605R · Fuselage Floor Panel
  > AFT BULK CARGO COMPRT CATWALK FLOORBOARD (PNL# 262GF) (A539-80656-006-00) 2 INSERTS DAMMAGED AT STA. 3198 BTW FR70-FR76. REPAIRED DAMAGED INSERTS IN AFT BULK CARGO COMPARTMENT CATWALK FLOORBOARD AT STA. 3198 BTW FR. 70 AND FR 76 (MPN: A539-80656-006-00 / P
- [SDR FDEA202409111290](https://openairdocs.org/sdr/FDEA202409111290.md): Skid · pilot error · Sep 11, 2024 · N683FE · Airbus A300F4605R · Fuselage Main, Structure
  > BOUNCED LANDING LANDING TO GO AROUND. UPON BLOCK IN, FOUND TAIL SKID PAINT MISSING. SEE WRI 32-70/3582 FOR DETAILS. PERFORMED INSPECTION PER AMM 05-51-21-00 AND FOUND TO BE OUT OF LIMITS. INSPECTED PER E.A. 6-0550-T0380603, REV NR PS P1, NO FURTHER FINDING
- [SDR FDEA202404180470](https://openairdocs.org/sdr/FDEA202404180470.md): Bleed Valve · failed · Apr 18, 2024 · N683FE · Airbus A300F4605R · Compressor Bleed Valve
  > ON DEPARTURE PASSING 3000 FT RECEIVED ECAM ALERT BLEED HP VALVE FAULT NR 1. REFERENCED QRH BLEED VALVE FAULT. RESET OF HP BLEED VALVE UNSUCCESSFUL. RECEIVED BLEED HP VALVE STUCK OPEN. BLEED HP VALVE RESET. WITH MEL ON THE BLEED VALVE 2 RETURNED TO AFW.
- [SDR FDEA202403290407](https://openairdocs.org/sdr/FDEA202403290407.md): Seat Track · worn · Mar 29, 2024 · N683FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach Fittings
  > (WRI 25-50-3077) SEAT TRACK DAMAGE BETEEN FR65 & FR66, Y1456. PN A5327400500053 MINOR REPAIR REPLACED SEAT TRACK SECTION (FROM FR65 TO FR66 WITH) USING A300-600 SRM 53-10-16 PAGE 201, WITH A300-600 SRM 51-40-21 AS REFERENCE.
- [SDR FDEA202311051827](https://openairdocs.org/sdr/FDEA202311051827.md): Actuator · inoperative · Nov 5, 2023 · N683FE · Airbus A300* · Nose/Tail Landing Gear
  > PDIS 683 32-20 2696 03NOV23 CAN FACT U L/G DOOR NOT CLOSED ECAM AFTER GEAR RETRACTION. AMBER LIGHTS ILLUMINATED ON BOTH GEAR INDICATION PANELS. COMPLIED WITH QRH. DISCUSSED WITH GOC & MOC. WHEN GEAR WAS EXTENDED, THE AMBER DOOR LIGHTS REMAI
- [SDR FDEA202310201781](https://openairdocs.org/sdr/FDEA202310201781.md): Door · cracked · Oct 20, 2023 · N683FE · Airbus A300* · Cargo/Baggage Doors
  > FWD CARGO DOOR INNER SKIN FOUND 3EA CRACKS JUST AT BOTH SIDES OF ACTUATOR ATTACH FITTING AT FR22A BETWEEN BEAM1 AND BEAM2 COMPLIED WITH EA: 6-5230-T0376680 P1. TITLE: DOORS - CARGO DOOR/HYD SYS - FWD CARGO DOOR INNER SKIN CRACKED AT FR22A. REPAIRED THE FWD
- [SDR FDEA202310051709](https://openairdocs.org/sdr/FDEA202310051709.md): Crossbeam · cracked · Oct 5, 2023 · N683FE · Airbus A300* · Fuselage Main, Structure
  > MAIN DECK CARGO COMPARTMENT FLOOR STRUCTURE - CROSSBEAM CRACKED, AT FR64, BETWEEN Y1456 AND Y1959 REPAIRED THE MAIN DECK CARGO COMPARTMENT FLOOR STRUCTURE CRACKED CROSSBEAM AT FR64 BETWEEN Y1456 AND Y1959 PER A300-600F SRM53-10-15-201 PARA.14. FIG.211. THI
- [SDR FDEA202310051708](https://openairdocs.org/sdr/FDEA202310051708.md): Crossbeam · cracked · Oct 5, 2023 · N683FE · Airbus A300* · Fuselage Miscellaneous Structure
  > MAIN DECK CARGO COMPARTMENT FLOOR STRUCTURE - CROSSBEAM CRACKED, AT FR58, BETWEEN Y1456 AND Y1959 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. THI
- [SDR FDEA202308231480](https://openairdocs.org/sdr/FDEA202308231480.md): Valve · unknown · Aug 23, 2023 · N683FE · Airbus A300* · Landing Gear Retraction/Extension System
  > GEAR WOULD NOT RETRACT. CREW REPORTED THE GEAR HANDLE MADE THE INTERLOCK AND WENT TO THE UP POSITION. MULTIPLE COMPONENTS CHANGED DIFFRENT WRI'S, FINAL GEAR OPERATIONAL CHECKS GOOD IAW AMM 32-31-00-05. REMOVE AND REPLACE LANDING GEAR FREE FALL CUTOUT VA
- [SDR FDEA202308101394](https://openairdocs.org/sdr/FDEA202308101394.md): Control Unit · unknown · Aug 10, 2023 · N683FE · Airbus A300* · Landing Gear Retraction/Extension System
  > ON APPROACH LOWERED GEAR HANDLE, GEAR DIDN T EXTEND. RECEIVED 3 RED UNLOCK LIGHTS AND ECAM WARNING. ON THE GO-AROUND AS WE STARTED THE CLIMB, GEAR DROPPED AND WE HAD 3 GREEN DOWN AND LOCK LIGHTS AFTER ABOUT 30 SECONDS. LANDING GEAR NORMAL CONTROL MICROS
- [SDR FDEA202204110917](https://openairdocs.org/sdr/FDEA202204110917.md): None · failed · Apr 11, 2022 · N683FE · Airbus A300* · Emergency Lighting
  > MDIS 683 33-50 0922 11APR22 MEM FACT U DURING SERVICE CHECK FOUND EMERG LIGHTS TEST SWITCH WOULD NOT ILLUMINATE R/I 11APR22 08:02 MEM U REASON CODE: PREMATURE REMOVAL/INSTALLATION OFF MPN: AD-3214-30 POS: 3 SRL:
- [SDR FDEA202106161567](https://openairdocs.org/sdr/FDEA202106161567.md): Stringer · corroded · Jun 16, 2021 · N683FE · Airbus A300F4605R · Fuselage Main, Longeron/Stringer
  > CORROSION ON STR 38R BTW FR42 TO FR46 ON AIR CONDITION BAY PERFORMED PERMANENT REPAIR ON STR 38R BTW FR45 TO FR46 ON AIR CONDITION BAY IAW EA # 6-5310-T0362286 EA TITLE: FUSELAGE MAINFRAME - CORROSION ON STRINGER S-38R BETWEEN FRAMES 45 AND 46 - BLEND REPA
- [SDR FDEA202105261493](https://openairdocs.org/sdr/FDEA202105261493.md): Floor Panel · cracked · May 26, 2021 · N683FE · Airbus A300F4605R · Fuselage Floor Panel
  > CRACK ON FLOOR PANEL 132LG OF FWD CARGO COMPARTMENT MANUFACTURED FLOOR PANEL 132LG OF FWD CARGO COMPARTMENT WITH NEW REPLACEMENT MATERIAL AND IDENTIFIED WITH P/N: SR30R5332B113200000 FDX MANUFACTURED DATE: 04-JUN-21 AS PER DWG: SRZ-25-005 REV. R AND GMM 07
- [SDR FDEA202105261490](https://openairdocs.org/sdr/FDEA202105261490.md): Floor Panel · cracked · May 26, 2021 · N683FE · Airbus A300F4605R · Fuselage Floor Panel
  > CRACK ON FLOOR PANEL 132PG OF FWD CARGO COMPARTMENT MANUFACTURED FLOOR PANEL 132PG OF FWD CARGO COMPARTMENT WITH NEW REPLACEMENT MATERIAL AND IDENTIFIED WITH P/N: SR30A5327997800200 FDX MANUFACTURED DATE 10-JUN-21 AS PER DWG SRZ-25-005 REV. R AND GMM 07-0-
- [SDR FDEA202105261488](https://openairdocs.org/sdr/FDEA202105261488.md): Floor Panel · cracked · May 26, 2021 · N683FE · Airbus A300F4605R · Fuselage Floor Panel
  > CRACK ON FLOOR PANEL 131QG OF FWD CARGO COMPARTMENT MANUFACTURED FLOOR PANEL 131QG OF FWD CARGO COMPARTMENT WITH NEW REPLACEMENT MATERIAL AND IDENTIFIED WITH P/N: SR30R532B113600000 FDX MANUFACTURED DATE 04-JUN-21 AS PER DWG SRZ-25-005 REV. R AND GMM 07-0-
- [SDR FDEA202105261479](https://openairdocs.org/sdr/FDEA202105261479.md): Floor Panel · cracked · May 26, 2021 · N683FE · Airbus A300F4605R · Fuselage Floor Panel
  > CRACK ON FLOOR PANEL 131LG OF FWD CARGO COMPARTMENT MANUFACTURED FLOOR PANEL 131LG OF FWD CARGO COMPARTMENT WITH NEW REPLACEMENT MATERIAL AND IDENTIFIED WITH P/N: SR30R532B113100000 FDX MANUFACTURED DATE 04-JUN-21 AS PER DWG SRZ-25-005 REV. R AND GMM 07-
- [SDR FDEA202105261466](https://openairdocs.org/sdr/FDEA202105261466.md): Floor Panel · damaged · May 26, 2021 · N683FE · Airbus A300F4605R · Fuselage Floor Panel
  > PERFORATION ON FLOOR PANEL 241WH IN MAIN DECK MANUFACTURED FLOOR PANEL 241WH IN MAIN DECK WITH NEW REPLACEMENT MATERIAL AND IDENTIFIED WITH P/N: SR30B5327060400200 FDX MANUFACTURED DATE 04-JUN-21 AS PER DWG SRZ-25-005 REV. R AND GMM 07-0-1000 FOR RAW MATER
- [SDR FDEA202105261465](https://openairdocs.org/sdr/FDEA202105261465.md): Floor Panel · damaged · May 26, 2021 · N683FE · Airbus A300F4605R · Fuselage Floor Panel
  > PERFORATION ON FLOOR PANEL 241SJ IN MAIN DECK MANUFACTURED FLOOR PANEL 241SJ IN MAIN DECK WITH NEW REPLACEMENT MATERIAL AND IDENTIFIED WITH P/N: SR30B5327062500000 FDX MANUFACTURED DATE 04-JUN-21 AS PER DWG SRZ-25-005 REV. R AND GMM 07-0-1000 FOR RAW MATER
- [SDR FDEA202105261464](https://openairdocs.org/sdr/FDEA202105261464.md): Floor Panel · damaged · May 26, 2021 · N683FE · Airbus A300F4605R · Fuselage Floor Panel
  > PERFORATION ON FLOOR PANEL 241YJ IN MAIN DECK MANUFACTURED FLOOR PANEL 241YJ IN MAIN DECK WITH NEW REPLACEMENT MATERIAL AND IDENTIFIED WITH P/N: SR30B5327062700000 FDX MANUFACTURED DATE 04-JUN-21 AS PER DWG SRZ-25-005 REV. R AND GMM 07-0-1000 FOR RAW MATER
- [SDR FDEA202105261463](https://openairdocs.org/sdr/FDEA202105261463.md): Floor Panel · damaged · May 26, 2021 · N683FE · Airbus A300F4605R · Fuselage Floor Panel
  > PERFORATION ON FLOOR PANEL 241TH IN MAIN DECK MANUFACTURED FLOOR PANEL 241TH IN MAIN DECK WITH NEW REPLACEMENT MATERIAL AND IDENTIFIED WITH P/N: SR30B5327060000200 FDX MANUFACTURED DATE 04-JUN-21 AS PER DWG SRZ-25-005 REV. R AND GMM 07-0-1000 FOR RAW MATER
- [SDR FDEA202105261462](https://openairdocs.org/sdr/FDEA202105261462.md): Floor Panel · damaged · May 26, 2021 · N683FE · Airbus A300F4605R · Fuselage Floor Panel
  > PERFORATION ON FLOOR PANEL 241QH IN MAIN DECK MANUFACTURED FLOOR PANEL 241QH IN MAIN DECK WITH NEW REPLACEMENT MATERIAL AND IDENTIFIED WITH P/N: SR30B5327061801400 FDX MANUFACTURED DATE 04-JUN-21 AS PER DWG SRZ-25-005 REV. R AND GMM 07-0-1000 FOR RAW MATER
- [SDR FDEA202105251501](https://openairdocs.org/sdr/FDEA202105251501.md): Rib · cracked · May 25, 2021 · N683FE · Airbus A300F4605R · Trailing Edge Flaps
  > CRACK INDICATION ON FLAP CENTER RIB 27 AFT ON LH WING PERFORMED PERMANENT REPAIR ON FLAP CENTER RIB 27 AFT AREA ON LH WING AS PER EA# 6-5750-T0361991 P1 TITLE: WING - FLIGHT SURFACES - LH CENTER FLAP CRACK IN UPPER FLANGE OF RIB 27 AT STRINGERS 2.7 AND 2
- [SDR FDEA202105211508](https://openairdocs.org/sdr/FDEA202105211508.md): Floor Panel · unknown · May 21, 2021 · N683FE · Airbus A300F4605R · Fuselage Floor Panel
  > FABRICATE ACCESS PANEL 121AF IN FWD AVIONIC COMPARTMENT MANUFACTURED FLOOR PANEL 121AF IN FWD AVIONIC COMPARTMENT WITH NEW REPLACEMENT MATERIAL AND IDENTIFIED WITH P/N: SR30A5321007600100 FDX MANUFACTURED DATE: 10-JUN-21.AS PER DWG SRZ-25-005 REV. R AND GM
- [SDR FDEA202105211491](https://openairdocs.org/sdr/FDEA202105211491.md): Floor Panel · cracked · May 21, 2021 · N683FE · Airbus A300F4605R · Fuselage Floor Panel
  > CRACK FLOOR PANEL 221HF AT FWD GALLEY AREA MANUFACTURED FLOOR PANEL 221HF AT FWD GALLEY AREA WITH NEW REPLACEMENT MATERIAL AND IDENTIFIED WITH P/N: SR30A5328538200200 FDX MANUFACTURED DATE 09-JUN- 21 AS PER DWG SRZ-25-005 REV. R AND GMM 07-0-1000 FOR RAW MA
- [SDR FDEA202105201436](https://openairdocs.org/sdr/FDEA202105201436.md): Seat Track · damaged · May 20, 2021 · N683FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach Fittings
  > PERFORMED REPAIR ON SEAT TRACK RH NO.5 LOC. FR 54.2 AND Y1959 IN PASSENGER CABIN IAW SRM 53-15-16-201 PERFORMED PERMANENT REPAIR ON SEAT TRACK LH N5 LOC FR54.2 AND Y1959 IN PASSENGER CABIN IAW A300-600 SRM 53-15-16-201 AND A300-600 SRM 51-40-21 AND DWG #
- [SDR FDEA202105201473](https://openairdocs.org/sdr/FDEA202105201473.md): Fitting · cracked · May 20, 2021 · N683FE · Airbus A300F4605R · Fuselage Main, Attach Fittings
  > CRACK INDICATION FOUND ON HOLE X LOCATED ON FR 47 CENTER WING BOX CORNER VERTICAL FITTING AT REAR SPAR RH WING, CRACK DIRECTION: 07 OCLOCK (LOOKING AFT TO FWD) D1-D2:0.8005 INCH APPROX PERFORMED PERMANENT REPAIR ON HOLE X LOC. ON FR47 CENTER WING BOX CORN
- [SDR FDEA202105201439](https://openairdocs.org/sdr/FDEA202105201439.md): Seat Track · worn · May 20, 2021 · N683FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach Fittings
  > PERFORM REPAIR ON SEAT TRACK LH NO.4 LOCATED FR 38.2 AND Y1456 IN MAIN DECK IAW SRM 53-15-16-201 PERFORMED PERMANENT REPAIR ON SEAT TRACK LH N4 LOC FR 38.2 AND Y1456 IN MAIN DECK IAW A300-600 SRM 53-15-16-201, A300-600 SRM 51-40-21 AND DWG #A53813159 ISS
- [SDR FDEA202105201438](https://openairdocs.org/sdr/FDEA202105201438.md): Seat Track · damaged · May 20, 2021 · N683FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach Fittings
  > PERFORMED REPAIR ON SEAT TRACK RH NO.4 LOCATED FR 54.2 AND Y1456 IN PASSENGER CABIN IAW SRM 53-15-16-201 PERFORMED PERMANENT REPAIR ON SEAT TRACK LH N4 LOC FR54.2 AND Y1456 IN PASSENGER CABIN IAW A300-600 SRM 53-15-16-201 AND A300-600 SRM 51-40-21 AND DW
- [SDR FDEA202105201437](https://openairdocs.org/sdr/FDEA202105201437.md): Seat Track · damaged · May 20, 2021 · N683FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach Fittings
  > PERFORMED REPAIR ON SEAT TRACK RH NO.3 LOCATED FR 54.2 AND Y-953 IN PASSENGER CABIN IAW SRM 53-15-16-201 PERFORMED PERMANENT REPAIR ON SEAT TRACK RH N3 LOC FR54.2 AND Y-953 IN PASSENGER CABIN IAW A300-600 SRM 53-15-16-201 AND A300-600 SRM 51-40-21 AND DW
- [SDR FDEA202105161506](https://openairdocs.org/sdr/FDEA202105161506.md): Floor Panel · cracked · May 16, 2021 · N683FE · Airbus A300F4605R · Fuselage Floor Panel
  > CRACK FLOOR PANEL 262YF IN MAIN DECK MANUFACTURED FLOOR PANEL 262YF WITH NEW REPLACEMENT MATERIAL AND IDENTIFIED WITH P/N: SR30B5327032400600 FDX MANUFACTURED DATE 04-JUN-21 AS PER DWG SRZ-25- 005 REV. R AND GMM 07-0-1000 FOR RAW MATERIAL TRACEABILITY GILLF
- [SDR FDEA202105151519](https://openairdocs.org/sdr/FDEA202105151519.md): Fitting · cracked · May 15, 2021 · N683FE · Airbus A300F4605R · Fuselage Main, Attach Fittings
  > CRACK INDICATION ON FRAMEE 47 RH SIDE CORNER FITTING AT REAR SPAR AND BOTTOM PANEL JUNCTION WITH FUSELAGE AREA ON OPEN FASTENER HOLE C. AFFECTED LAYER IS REAR SPAR AND CRACK DIRECTIONS IS 12 OCLOCK IN CENTER FUEL TANK (1 EA) PERFORMED REPAIR INSTRUCTIONS O
- [SDR FDEA202105151496](https://openairdocs.org/sdr/FDEA202105151496.md): Stringer · corroded · May 15, 2021 · N683FE · Airbus A300F4605R · Fuselage Main, Longeron/Stringer
  > CORROSION ON STRINGER 37L BTW FR 46 TO FR 47 IN AIR CONDITIONING BAY PERFORMED PERMANENT REPAIR LOC ON STRINGER 37L BTW FR46 TO FR47 IN AIR CONDITIONING BAY IAW EA NO 6-5310-T0361926 EA TITLE FUSELAGE - MAINFRAME - CORROSION ON STRINGER 37LH BETWEEN FRAMES
- [SDR FDEA202105131507](https://openairdocs.org/sdr/FDEA202105131507.md): Floor Panel · cracked · May 13, 2021 · N683FE · Airbus A300F4605R · Fuselage Floor Panel
  > CRACK ON FLOOR PANELS 131NG OF FWD CARGO COMPARTMENT MANUFACTURED FLOOR PANEL 131NG OF FWD CARGO COMPARTMENT WITH NEW REPLACEMENT MATERIAL AND IDENTIFIED WITH P/N: SR30R53B113300000 FDX MANUFACTURED DATE 10-JUN-21 AS PER DWG SRZ-25-005 REV. R AND GMM 07-0
- [SDR FDEA202105131492](https://openairdocs.org/sdr/FDEA202105131492.md): Floor Panel · cracked · May 13, 2021 · N683FE · Airbus A300F4605R · Fuselage Floor Panel
  > CRACK FLOOR PANEL 151WF IN AFT CARGO COMPARTMENT (1EA) MANUFACTURED FLOOR PANEL 151GF IN AFT CARGO COMPARTMENT WITH NEW REPLACEMENT MATERIAL AND IDENTIFIED WITH P/N: SR30A5327991300200 FDX MANUFACTURED DATE 10-JUN- 21 AS PER DWG SRZ-25-005 REV. R AND GMM 07
- [SDR FDEA202105131481](https://openairdocs.org/sdr/FDEA202105131481.md): Floor Panel · damaged · May 13, 2021 · N683FE · Airbus A300F4605R · Fuselage Floor Panel
  > PERFORATION ON FLOOR PANEL 242LJ IN MAIN DECK MANUFACTURED FLOOR PANEL 242LJ IN MAIN DECK WITH NEW REPLACEMENT MATERIAL AND IDENTIFIED WITH P/N: SR30B5327080700000 FDX MANUFACTURED DATE 09-JUN-21 AS PER DWG SRZ-25-005 REV. R AND GMM 07-0-1000 FOR RAW MATER
- [SDR FDEA202105131330](https://openairdocs.org/sdr/FDEA202105131330.md): Access Panel · cracked · May 13, 2021 · N683FE · Airbus A300F4605R · Fuselage Miscellaneous Structure
  > CRACKS ON ACCESS PANEL 121LF ON AVIONICS COMPARTMENT REPAIRED ACCESS PANEL 121LF ON AVIONICS COMPARTMENT AS PER DRAWING SRZ-25-005 REV. R TOOL USED SCALE P/N SCA-301 S/N AE-412125 DUE DATE 24-FEB-22.
- [SDR FDEA202105131329](https://openairdocs.org/sdr/FDEA202105131329.md): Access Panel · damaged · May 13, 2021 · N683FE · Airbus A300F4605R · Fuselage Miscellaneous Structure
  > ELONGATE HOLE ON ACCESS PANEL 121SF OF AVIONICS COMPARTMENT REPAIRED ACCESS PANEL 121SF OF AVIONICS COMPARTMENT AS PER DRAWING SRZ-25-005 REV. R TOOL USED SCALE P/N SCA-301 S/N AE-412125 DUE DATE 24-FEB-22.
- [SDR FDEA202105131327](https://openairdocs.org/sdr/FDEA202105131327.md): Access Panel · cracked · May 13, 2021 · N683FE · Airbus A300F4605R · Fuselage Miscellaneous Structure
  > CRACK ON ACCESS PANEL 121EF OF AVIONICS COMPARTMENT REPAIRED ACCESS PANEL 121EF OF AVIONICS COMPARTMENT AS PER DRAWING SRZ-25-005 REV. R TOOL USED SCALE P/N SCA-301 S/N AE-412125 DUE DATE 24-FEB-22.
- [SDR FDEA202105131326](https://openairdocs.org/sdr/FDEA202105131326.md): Floor Panel · broken · May 13, 2021 · N683FE · Airbus A300F4605R · Fuselage Floor Panel
  > BROKEN ACCESS PANEL 121YF ON AVIONICS COMPARTMENT REPAIRED ACCESS PANEL 121YF ON AVIONICS COMPARTMENT AS PER DRAWING SRZ-25-005 REV. R TOOL USED SCALE P/N SCA-301 S/N AE-412125 DUE DATE 24-FEB-22.
- [SDR FDEA202105131324](https://openairdocs.org/sdr/FDEA202105131324.md): Floor Panel · delaminated · May 13, 2021 · N683FE · Airbus A300F4605R · Fuselage Floor Panel
  > DELAMINATED FLOOR PANEL 152VF IN AFT CARGO COMPARTMENT (1EA) REPAIRED FLOOR PANEL 152VF IN AFT CARGO COMPARTMENT AS PER DRAWING SRZ-25-005 REV. R TOOL USED SCALE P/N SCA-301 S/N AE-412125 DUE DATE 24-FEB-22.
- [SDR FDEA202105121489](https://openairdocs.org/sdr/FDEA202105121489.md): Floor Panel · cracked · May 12, 2021 · N683FE · Airbus A300F4605R · Fuselage Floor Panel
  > CRACK FLOOR PANEL 152QF IN AFT CARGO COMPARTMENT (1EA) MANUFACTURED FLOOR PANEL 152GF IN AFT CARGO COMPARTMENT WITH NEW REPLACEMENT MATERIAL AND IDENTIFIED WITH P/N: SR30R5321B114200000 FDX MANUFACTURED DATE 04- JUN-21 AS PER DWG SRZ-25-005 REV. R AND GMM 0
- [SDR FDEA202105121328](https://openairdocs.org/sdr/FDEA202105121328.md): Floor Panel · delaminated · May 12, 2021 · N683FE · Airbus A300F4605R · Fuselage Floor Panel
  > DELAMINATED FLOOR PANEL 151VF IN AFT CARGO COMPARTMENT (1EA) REPAIRED FLOOR PANEL 151VF IN AFT CARGO COMPARTMENT AS PER DRAWING SRZ-25-005 REV. R TOOL USED SCALE P/N SCA-301 S/N AE-412125 DUE DATE 24-FEB-22.
- [SDR FDEA202007230038](https://openairdocs.org/sdr/FDEA202007230038.md): Warning System · malfunctioned · Jan 7, 2020 · N683FE · Airbus A300F4605R · Door Warning System
  > AFTER CLOSING CABIN DOORS, THERE WAS NO INDICATION FOR THE RT CABIN DOOR SLIDE. DISARMED AND REARMED DOORS. RT SLIDE INDICATOR APPEARED MOMENTARILY BUT LT SLIDE DISAPPERED MOMENTARILY ON ECAM. PERFORMED AN OPS CHECK OF LT AND RT CABIN DOOR SLIDE ARM/DISAR
- [SDR FDEA2020010970038](https://openairdocs.org/sdr/FDEA2020010970038.md): Indication Sys · malfunctioned · Jan 7, 2020 · N683FE · Airbus A300F4605R · Door Warning System
  > AFTER CLOSING CABIN DOORS THERE WAS NO INDICATION FOR RH CABIN DOOR SLIDE. DISARMED AND REARMED DOORS. R/H SLIDE INDICATOR APPEARED MOMENTARILY BUT LH SLIDE DISAPPERED MOMENTARILY ( ON ECAM). RELEASED FOR SERVICE PER MEL CAT: C EXP: 17JAN20, ECAM SLIDE
- [SDR FDEA201908071817](https://openairdocs.org/sdr/FDEA201908071817.md): Relay · malfunctioned · Aug 7, 2019 · N683FE · Airbus A300F4605R · Elevator Control System
  > ELEVATOR EXTREMLY STIFF ON LANDING RUNWAY 36L KMEM. GW 238.4 LBS. STAB TRIM 3.8 NOSE UP. NR 2 FLC FAULT LIGHT ON PITCH FEEL POWER LOOP. REPLACED RELAY 308CY2 IAW TSM 27-33-01 FIGURE 103. PERFORMED OPS TEST IAW AMM. OPERATIONAL TEST GOOD. OK FOR SERVICE.
- [SDR FDEA201811193305](https://openairdocs.org/sdr/FDEA201811193305.md): Repair · torn · Nov 19, 2018 · N683FE · Airbus A300F4605R · Fuselage Main, Plate/Skin
  > AFT TAIL COMPARTMENT, RIGHT HAND SIDE, UPPER, FRAME 95, BETWEEN STR 2 & 3, SKIN IS TORN. REMOVED DAMAGED SKIN, CUTOUT IAW SRM 53-19-12 FIG. 202. FABRICATED AND INSTALLED DOUBLER REPAIRES IAW A300 SRM 53-19-12, FIG 202, CAT 'A' AND MAJOR REPAIR.
- [SDR FDEA201811033101](https://openairdocs.org/sdr/FDEA201811033101.md): Floor Panel · broken · Nov 3, 2018 · N683FE · Airbus A300F4605R · Fuselage Floor Panel
  > MCDD 241BK FLOOR PANEL BROKEN. FABRICATED FLOOR PANEL 241BK ON T18/1375758 IAW DWG SRZ 25-005. CLASSIFIED AS A CAT "A" MAJOR REPAIR.
- [SDR FDEA201811033100](https://openairdocs.org/sdr/FDEA201811033100.md): Floor Panel · broken · Nov 3, 2018 · N683FE · Airbus A300F4605R · Fuselage Floor Panel
  > MDCC 242LH FLOOR PANEL BROKEN. FABRICATED FLOOR PANEL 242LH ON T18/1375789 IAW DWG SRZ 25-005. CLASSIFIED AS A CAT "A" MAJOR REPAIR.
- [SDR FDEA201811033099](https://openairdocs.org/sdr/FDEA201811033099.md): Floor Panel · broken · Nov 3, 2018 · N683FE · Airbus A300F4605R · Fuselage Floor Panel
  > MDCC 242BJ FLOOR PANEL BROKEN. FABRICATED FLOOR PANEL 242BJ ON T18/1375785 IAW DWG SRZ 25-005. CLASSIFIED AS A CAT "A" MAJOR REPAIR.
- [SDR FDEA201811033098](https://openairdocs.org/sdr/FDEA201811033098.md): Floor Panel · broken · Nov 3, 2018 · N683FE · Airbus A300F4605R · Fuselage Floor Panel
  > MDCC 242VG FLOOR PANEL BROKEN. FABRICATED FLOOR PANEL 242VG ON T18/1375762 IAW DWG SRZ 25-005. CLASSIFIED AS A CAT "A" MAJOR REPAIR.

Next page: https://openairdocs.org/aircraft/N683FE/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 = 'N683FE' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N683FE/reports

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