# Service difficulty reports: N678FE

A list on [N678FE](https://openairdocs.org/aircraft/N678FE.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 · 220 reports

- [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 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 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 FDEA202602280292](https://openairdocs.org/sdr/FDEA202602280292.md): Safety Wire · wrong part · Feb 28, 2026 · N678FE · Airbus A300F4605R · Emergency Equipment
  > R1 SLIDE ASSY. REPLACE PACKBOARD RELEASE CABLE SAFETY WIRE WITH MS20995C15 STAINLESS STEEL WIRE. AMM: 25-61-20-05-01 CMM: 25-60-40 FEA: 6-2560-F0386375 A OTHER: SMIS 25-60/5160 R1 SLIDE ASSY. REMOVED AND REPLACED PACKBOARD RELEASE CABLE SAFETY WIRE
- [SDR FDEA202502160236](https://openairdocs.org/sdr/FDEA202502160236.md): Brake · faulted · Feb 16, 2025 · N678FE · Airbus A300F4605R · Landing Gear Brake System
  > AIRCRAFT ARRIVED AT GATE WITH # 4 MLG TIRE SHREDDED AMM: 32-41-11-04-02 R/R #4 TIRE PER ABOVE REF UP TO STEP D 12. WHILE PERFORMING TEST NUMBER 8, #4 TACH IS DRIVEN AT 1500 RPM AND THE RIGHT PEDAL DEPRESSED THE OPPOSITE BRAKE #3 IS ENGAGED. THE #3
- [SDR FDEA202501180105](https://openairdocs.org/sdr/FDEA202501180105.md): Bottle · low pressure · Jan 18, 2025 · N678FE · Airbus A300F4605R · Emergency Equipment
  > R1 DOOR ASSIT BOTTLE PRESSURE LOW FACT 18JAN25 19:09 LRD AMM: 52-10-14-03-02 SERVICED R1 ASSIST BOTTLE TO PROPER PRESSURE PER TEMPERATURE CHART, NO FURTHER DEFECTS, WORKED PER ABOVE REF FACT 18JAN25 19:09 LRD AMM: 52-10-14-03-02 SERVICED R1 A
- [SDR FDEA202404210484](https://openairdocs.org/sdr/FDEA202404210484.md): Rib · corroded · Apr 21, 2024 · N678FE · Airbus A300F4605R · Fuselage, Landing Gear Attach Fittings
  > RH MLG FWD PINTLE ATTACHMENT: HAS EVIDENCE OF CORROSION BETWEEN THE BUSHINGS IN RIB 5 FWD LUG. REWORKED R/H MLG RIB 5 FWD LUG PER AIRBUS R57240425 AND EA # 6-5710-T0378785 TITLE: WINGS - RH MAIN LANDING GEAR FITTING - REPAIR OF RIB 5 AFT PINTLE FWD LUG BORE
- [SDR FDEA202402070209](https://openairdocs.org/sdr/FDEA202402070209.md): Floor Panel · delaminated · Feb 7, 2024 · N678FE · Airbus A300F4605R · Fuselage Floor Panel
  > MAIN GEAR WELL AND HYDRAULICS COMPARTMENT FLOOR PANEL #143DF WAS FOUND DELAMINATION. FABRICATED THE NEW FLOOR PANEL I.A.W FEDEX DRAWING SRZ-25-005, AS PER GMM 6-2-100 "MAJOR REPAIR"
- [SDR FDEA202401300131](https://openairdocs.org/sdr/FDEA202401300131.md): Plate · deformed · Jan 30, 2024 · N678FE · Airbus A300F4605R · Fuselage Miscellaneous Structure
  > GROUND CHECK FOUND AFT CGO FR59A~FR61 STR28 A PLATE DEFORMED. REPLACED THE PLATE 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 FDEA202401270177](https://openairdocs.org/sdr/FDEA202401270177.md): Skin · damaged · Jan 27, 2024 · N678FE · Airbus A300F4605R · Fuselage Main, Plate/Skin
  > FOUND LIGHTNING STRIKE TRACE AT FR28 PLUS 7", S-46L ACCOMPLISHED THE DOUBLER REPAIR, THIS IS CAT.B REPAIR I.A.W A300-600F SRM 53-10-12-201, PARA.11, PAGE.279-288, FIG.208 (SHEET-2) & SRI:53-10-12-201, IIR:53-10-12-2-002-00, PARA.3B, TABLE.205. MAJOR REPAIR.
- [SDR FDEA202401250166](https://openairdocs.org/sdr/FDEA202401250166.md): Rib · corroded · Jan 25, 2024 · N678FE · Airbus A300F4605R · Wing, Rib/Bulkhead
  > RH #3 SPOILER JACK RIB I/B UPPER BORE FOUND CORROSION ACCOMPLISHED THE REINFORCEMENT REPAIR AT RH #3 SPOILER JACK RIB I.A.W FEDEX EA NO:T6-5740-T0377948 P1, SEQ NO:636, MAJOR REPAIR.
- [SDR FDEA202401170130](https://openairdocs.org/sdr/FDEA202401170130.md): Strap · cracked · Jan 17, 2024 · N678FE · Airbus A300F4605R · Fuselage Miscellaneous Structure
  > FUSELAGE S-33R WEB STRAP CRACK AT FR85 PLUS 6" AREA. CRACKED SECTION REPLACED NEW PART INSTALLED WITH RIVETS I.A.W A300-600F SRM 51-72-10- 001 PAGE2 AND 51-40-21-001 PARA6 PAGE 7B-23
- [SDR FDEA202401160129](https://openairdocs.org/sdr/FDEA202401160129.md): Floorbeam · cracked · Jan 16, 2024 · N678FE · Airbus A300F4605R · Fuselage Main, Floor Beam
  > FOUND FLOOR CROSS BEAM SUPPORT ANGLE CRACK AT RH FWD E/E COMPARTMENT, NEAR FR10,-990MM POS REPLACED THE ANGLE WITH NEW ONE I.A.W. A300-600F S.R.M 51-72-10-001 PAGE 2.
- [SDR FDEA202401150210](https://openairdocs.org/sdr/FDEA202401150210.md): Support Frame · cracked · Jan 15, 2024 · N678FE · Airbus A300F4605R · Fuselage Main, Structure
  > MAIN DECK CARGO DOOR SUPPORT YOKE DOOR FRAMES WERE FOUND CRACK. FABRICATED NEW SUPPORT FRAMES AND INSTALLED WITH FASTENERS I.A.W FEDEX EA NO:T6- 5230-T0377842A P1, SEQ NO:634, TITLE:DOORS - CARGO DOOR/HYD SYS - MAIN CARGO DOOR ACTUATOR BEARING FITTING REPLA
- [SDR FDEA202401150167](https://openairdocs.org/sdr/FDEA202401150167.md): Rib · gouged · Jan 15, 2024 · N678FE · Airbus A300F4605R · Wing, Rib/Bulkhead
  > RH #5 SPOILER JACK RIB O/B LOWER BORE FOUND GOUGE ACCOMPLISHED THE REINFORCEMENT REPAIR AT RH #5 SPOILER JACK RIB I.A.W FEDEX EA NO:T6-5740-T0377951 P1, SEQ NO:637, TITLE:WINGS-ATTACH FITTINGS-RH WING #5 SPOILER JACK RIB AT STA ABX184.625-BEAM ATTACHMENT H
- [SDR FDEA202206161437](https://openairdocs.org/sdr/FDEA202206161437.md): None · none · Jun 16, 2022 · N678FE · Airbus A300* · Wheel/Ski/Float
  > PDIS 678 32-46 2166 16JUN22 SHV OPEN U HOT BREAKS # 1 WHILE AIRBORNE BRAKE FAN DID NOT LWR THE TEMP, HIGHEST TEMP 385 LAND AT KSHV ***EMERGENCY DECLARED*** MEL 16JUN22 04:47 SHV U REL FOR SVC PER MEL: 32-47-02 CATEGORY: C EXPIRATION: 26
- [SDR FDEA202204130967](https://openairdocs.org/sdr/FDEA202204130967.md): None · damaged · Apr 13, 2022 · N678FE · Airbus A300* · Fuselage Structure (General)
  > AIRCRAFT STRUCK LH WINGTIP WITH RH WINGTIP OF A/C 597 COMPLY WITH EA 6-0550-T0367981 COMPLIED WITH EA 6-0550-T0367981
- [SDR FDEA202109062295](https://openairdocs.org/sdr/FDEA202109062295.md): Floor Support · corroded · Sep 6, 2021 · N678FE · Airbus A300F4605R · Fuselage Miscellaneous Structure
  > BULK CGO COMP'T FLOOR BEAM GOT CORROSION AT CENTERLINE BTW FR65 AND FR66 POSITION. ACCOMPLISHED THE CROSSBEAM REPAIR I.A.W. A300-600F SRM 53-10-15-201, PARA. 11, FIG. 208, P. 361-364.
- [SDR FDEA202108292215](https://openairdocs.org/sdr/FDEA202108292215.md): Skin · dented · Aug 29, 2021 · N678FE · Airbus A300F4605R · Wing, Plate/Skin
  > LH WING O/B FLAP L/E GOT 2EA DENTS AT RIB16 ACCOMPLISHED THE O/B FLAP CAT.B REPAIR I.A.W A300-600F SRM 57-50-00-201 PARA. 4H, FIG208 SHEET 2, P.231-234 AND SRI 57-50-00-201, IIR 57-50-00-2-002 PARA 3B, P205-208.
- [SDR FDEA202108252216](https://openairdocs.org/sdr/FDEA202108252216.md): Spar · cracked · Aug 25, 2021 · N678FE · Airbus A300F4605R · Trailing Edge Flaps
  > 1EA CRACK INDICATION WAS FOUND AT RIB26 REAR SPAR WEB FLANGE AREA OF LH CENTER FLAP. ACCOMPLISHED THE WORK: LH CENTER FLAP, CRACK IN UPPER FLANGE OF RIB 26 AT STRINGERS 2.8 - ALI 575306-01 (FAA AD 2019-21-01) I.A.W. A300-600 EA NO: T6-5750-T0363500 P1,
- [SDR FDEA202108242176](https://openairdocs.org/sdr/FDEA202108242176.md): Stiffener · cracked · Aug 24, 2021 · N678FE · Airbus A300F4605R · Nacelle/Pylon Miscellaneous Structure
  > RH PYLON FORWARD FAIRING STIFFENERS CRACKED AT THE RIB J08 FWD AREA. ACCOMPLISHED THE CANTILEVER BEAM REPAIR I.A.W A300-600F SRM 54-52-11-201 CONFIG-2, FIG201 SHEET1, P201-207, PARA5.
- [SDR FDEA202108212240](https://openairdocs.org/sdr/FDEA202108212240.md): Floor Panel · damaged · Aug 21, 2021 · N678FE · Airbus A300F4605R · Fuselage Floor Panel
  > MAIN DECK COMPT #241TG FLOOR PANEL WAS FOUND EDGE DAMAGED. ACCOMPLISHED THE FLOOR PANEL REPAIR I.A.W A300-600F SRM 53-10-20-201 PARA 8A, P201-205, FIG201.
- [SDR FDEA202108212239](https://openairdocs.org/sdr/FDEA202108212239.md): Floor Panel · damaged · Aug 21, 2021 · N678FE · Airbus A300F4605R · Fuselage Floor Panel
  > MAIN DECK COMPT Z231LG FLOOR PANEL WAS FOUND EDGE DAMAGED. ACCOMPLISHED THE FLOOR PANEL REPAIR I.A.W A300-600F SRM 53-10-20-201 PARA 8A, P201-205, FIG201.
- [SDR FDEA202108212238](https://openairdocs.org/sdr/FDEA202108212238.md): Floor Panel · damaged · Aug 21, 2021 · N678FE · Airbus A300F4605R · Fuselage Floor Panel
  > MAIN DECK COMPT #241QH FLOOR PANEL WAS FOUND EDGE DAMAGED. ACCOMPLISHE THE FLOOR PANEL REPAIR I.A.W. A300-600F SRM 53-10-20-201, PARA. 8A, P.201-205, FIG. 201.
- [SDR FDEA202108132058](https://openairdocs.org/sdr/FDEA202108132058.md): Skin · damaged · Aug 13, 2021 · N678FE · Airbus A300F4605R · Elevator, Plate/Skin
  > 1EA WATER TRAPPED AREA1(80MM X 90MM)WAS FOUND AT R/H ELEVATOR UPPER SKIN PANEL T/E NO.3 SCREW AREA. ACCOMPLISHED THE WATER TRAPPED AREA 1 (80MMX90MM) REPAIR I.A.W A300-600 SRM 55-21- 12- 21, PARA.5J, P268-270, FIG.212 SHEET3 AND 51-77-12-201, PARA.2A(2
- [SDR FDEA202108132057](https://openairdocs.org/sdr/FDEA202108132057.md): Skin · damaged · Aug 13, 2021 · N678FE · Airbus A300F4605R · Elevator, Plate/Skin
  > 1EA WATER TRAPPED AREA2(200MM X 90MM)WAS FOUND AT R/H ELEVATOR UPPER SKIN PANEL T/E BETWEEN NO.20 & NO.21 SCREW AREA. ACCOMPLISHED THE WATER TRAPPED AREA 2 (200MMX90MM) CAT.B REPAIR I.A.W A300-600 SRM 51-21-12-201 PARA5F, FIG209, P.241-256 AND SRI 55
- [SDR FDEA202108132056](https://openairdocs.org/sdr/FDEA202108132056.md): Skin · damaged · Aug 13, 2021 · N678FE · Airbus A300F4605R · Elevator, Plate/Skin
  > 1EA WATER TRAPPED AREA3(200MM X 90MM)WAS FOUND AT R/H ELEVATOR UPPER SKIN PANEL L/E BETWEEN NEAR ER18 AREA. ACCOMPLISHED THE WATER TRAPPED AREA 3 (200MMX90MM) CAT.B REPAIR I.A.W A300-600 SRM 51-21-12-201 PARA5D, FIG204, P.221-226 AND SRI 55-21-12-201
- [SDR FDEA202108112245](https://openairdocs.org/sdr/FDEA202108112245.md): Floor Panel · damaged · Aug 11, 2021 · N678FE · Airbus A300F4605R · Fuselage Floor Panel
  > THE #151WF FLOOR PANEL WAS FOUND EDGE DAMAGED WITH MARK ACCOMPLISHED THE FLOOR PANEL REPAIR I.A.W A300-600F SRM 53-10-20-201 PARA 8B, FIG203 SHEET 1, P209-211.
- [SDR FDEA202108112244](https://openairdocs.org/sdr/FDEA202108112244.md): Floor Panel · damaged · Aug 11, 2021 · N678FE · Airbus A300F4605R · Fuselage Floor Panel
  > THE #152SF FLOOR PANEL WAS FOUND DAMAGED ON EDGE WITH MARK ACCOMPLISHED THE FLOOR PANEL REPAIR I.A.W A300-600F SRM 53-10-20-201 PARA 8B, FIG203 SHEET 1, P209-211.
- [SDR FDEA202108112243](https://openairdocs.org/sdr/FDEA202108112243.md): Floor Panel · damaged · Aug 11, 2021 · N678FE · Airbus A300F4605R · Fuselage Floor Panel
  > THE #151QF FLOOR PANEL WAS FOUND EDGE DAMAGED WITH MARK ACCOMPLISHED THE FLOOR PANEL REPAIR I.A.W A300-600F SRM 53-10-20-201 PARA 8B, FIG203 SHEET 1, P209-211.
- [SDR FDEA202108112242](https://openairdocs.org/sdr/FDEA202108112242.md): Floor Panel · damaged · Aug 11, 2021 · N678FE · Airbus A300F4605R · Fuselage Floor Panel
  > THE #132RG FLOOR PANEL WAS FOUND EDGE DAMAGED WITH MARK ACCOMPLISHED THE FLOOR PANEL REPAIR I.A.W A300-600F SRM 53-10-20-201 PARA 8B, FIG203 SHEET 1, P209-211.
- [SDR FDEA202108112241](https://openairdocs.org/sdr/FDEA202108112241.md): Floor Panel · damaged · Aug 11, 2021 · N678FE · Airbus A300F4605R · Fuselage Floor Panel
  > THE #132SG FLOOR PANEL WAS FOUND EDGE DAMAGED WITH MARK ACCOMPLISHED THE FLOOR PANEL REPAIR I.A.W A300-600F SRM 53-10-20-201 PARA 8B, FIG203 SHEET 1, P209-211.
- [SDR FDEA202108042286](https://openairdocs.org/sdr/FDEA202108042286.md): Skin · damaged · Aug 4, 2021 · N678FE · Airbus A300F4605R · Rudder, Plate/Skin
  > N00074: 1EA WATER TRAPPED AREA(50MM X 50MM) WAS FOUND AT L/H RUDDER T/E SCREW LINE NO.10 FASTENER. ACCOMPLISHED THE WORK: LH RUDDER SHELL MULTIPLE SCREW HOLES WATER INGRESS REPAIR I.A.W A300-600 EA NO:T6-5540-T0363520 P1, SEQ NO:1122 AND SRM 55-41-12-2
- [SDR FDEA202108042284](https://openairdocs.org/sdr/FDEA202108042284.md): Rudder · damaged · Aug 4, 2021 · N678FE · Airbus A300F4605R · Rudder Structure
  > N00075: 1EA WATER TRAPPED AREA(40MMX50MM) WAS FOUND AT R/H RUDDER T/E SCREW LINE NO.9 FASTENER. ACCOMPLISHED THE WORK: RH RUDDER SHELL MULTIPLE SCREW HOLES WATER INGRESS REPAIR I.A.W A300-600 EA NO:T6-5540-T0363521 P1, SEQ NO:1123 AND SRM 55-41-12-201
- [SDR FDEA202108042283](https://openairdocs.org/sdr/FDEA202108042283.md): Rudder · damaged · Aug 4, 2021 · N678FE · Airbus A300F4605R · Rudder Structure
  > N00305: 1EA WATER TRAPPED AREA(35MMX50MM) WAS FOUND AT R/H RUDDER T/E SCREW LINE NO.10 FASTENER. ACCOMPLISHED THE WORK: RH RUDDER SHELL MULTIPLE SCREW HOLES WATER INGRESS REPAIR I.A.W A300-600 EA NO:T6-5540-T0363521 P1, SEQ NO:1123 AND SRM 55-41-12-201
- [SDR FDEA202108042281](https://openairdocs.org/sdr/FDEA202108042281.md): Rudder · damaged · Aug 4, 2021 · N678FE · Airbus A300F4605R · Rudder Structure
  > N00306: 1EA WATER TRAPPED AREA(35MMX50MM) WAS FOUND AT R/H RUDDER T/E SCREW LINE NO.12 FASTENER. ACCOMPLISHED THE WORK: RH RUDDER SHELL MULTIPLE SCREW HOLES WATER INGRESS REPAIR I.A.W A300-600 EA NO:T6-5540-T0363521 P1, SEQ NO:1123 AND SRM 55-41-12-201
- [SDR FDEA202108042288](https://openairdocs.org/sdr/FDEA202108042288.md): Skin · damaged · Aug 4, 2021 · N678FE · Airbus A300F4605R · Rudder, Plate/Skin
  > N00302: 1EA WATER TRAPPED AREA(70MMX45MM) WAS FOUND AT L/H RUDDER T/E SCREW LINE NO.12 FASTENER. ACCOMPLISHED THE WORK: LH RUDDER SHELL MULTIPLE SCREW HOLES WATER INGRESS REPAIR I.A.W A300-600 EA NO:T6-5540-T0363520 P1, SEQ NO:1122 AND SRM 55-41-12-201
- [SDR FDEA202108042287](https://openairdocs.org/sdr/FDEA202108042287.md): Skin · damaged · Aug 4, 2021 · N678FE · Airbus A300F4605R · Rudder, Plate/Skin
  > N00301: 1EA WATER TRAPPED AREA(50MMX40MM) WAS FOUND AT L/H RUDDER T/E SCREW LINE NO.11 FASTENER. ACCOMPLISHED THE WORK: LH RUDDER SHELL MULTIPLE SCREW HOLES WATER INGRESS REPAIR I.A.W A300-600 EA NO:T6-5540-T0363520 P1, SEQ NO:1122 AND SRM 55-41-12-201
- [SDR FDEA202108042285](https://openairdocs.org/sdr/FDEA202108042285.md): Skin · damaged · Aug 4, 2021 · N678FE · Airbus A300F4605R · Rudder, Plate/Skin
  > N00303: 1EA WATER TRAPPED AREA(50MMX40MM) WAS FOUND AT L/H RUDDER T/E SCREW LINE NO.13 FASTENER. ACCOMPLISHED THE WORK: LH RUDDER SHELL MULTIPLE SCREW HOLES WATER INGRESS REPAIR I.A.W A300-600 EA NO:T6-5540-T0363520 P1, SEQ NO:1122 AND SRM 55-41-12-201

Next page: https://openairdocs.org/aircraft/N678FE/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 = 'N678FE' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N678FE/reports

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