N678FE

Service difficulty reports · 220

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.

Query with SQL
duckdb -csv -c "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"

Prints the whole list as CSV. It reads the release’s Parquet files over HTTPS, so there’s nothing to download first. Install DuckDB to run it.

SDR FDEA202607200951Pressure Deck · corrodedFWD 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 5310911Jul 20, 2026 · N678FE · Airbus A300F4605R · Fuselage Main, StructureSDR FDEA202607200950Pressure Deck · crackedFWD 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.Jul 20, 2026 · N678FE · Airbus A300F4605R · Fuselage Main, StructureSDR FDEA202607140936Repair · no discrepancyEXISTING 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 Jul 14, 2026 · N678FE · Airbus A300F4605R · Standard Practices/StructuresSDR FDEA202607140935Repair · no discrepancyEXISTING 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 Jul 14, 2026 · N678FE · Airbus A300F4605R · Standard Practices/StructuresSDR FDEA202607140934Repair · inaccurateEXISTING 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 MIJul 14, 2026 · N678FE · Airbus A300F4605R · Standard Practices/StructuresSDR FDEA202607140933Repair · inaccurateEXISTING 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 INJul 14, 2026 · N678FE · Airbus A300F4605R · Standard Practices/StructuresSDR FDEA202607140932Seat Track · misrepairedEXISTING 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 MISSINJul 14, 2026 · N678FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR FDEA202607140931Repair · no discrepancyEXISTING 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 Jul 14, 2026 · N678FE · Airbus A300F4605R · Cargo/Baggage DoorsSDR FDEA202607140920Hinge Arm · delaminatedLH 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 Jul 14, 2026 · N678FE · Airbus A300F4605R · SpoilersSDR FDEA202607130923Skin · misrepairedEXISTING 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 Jul 13, 2026 · N678FE · Airbus A300F4605R · Fuselage Main, Plate/SkinSDR FDEA202607100884Floorbeam · corrodedEXISTING 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-T03Jul 10, 2026 · N678FE · Airbus A300F4605R · Fuselage Main, Floor BeamSDR FDEA202607100883Floor Panel · crackedMDCC 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: 2400Jul 10, 2026 · N678FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA202607100882Web · crackedMDCC 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, Jul 10, 2026 · N678FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA202607050840Crossbeam · crackedMDCC 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.Jul 5, 2026 · N678FE · Airbus A300F4605R · Fuselage Main, StructureSDR FDEA202602280292Safety Wire · wrong partR1 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 WIREFeb 28, 2026 · N678FE · Airbus A300F4605R · Emergency EquipmentSDR FDEA202502160236Brake · faultedAIRCRAFT 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 #3Feb 16, 2025 · N678FE · Airbus A300F4605R · Landing Gear Brake SystemSDR FDEA202501180105Bottle · low pressureR1 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 AJan 18, 2025 · N678FE · Airbus A300F4605R · Emergency EquipmentSDR FDEA202404210484Rib · corrodedRH 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 Apr 21, 2024 · N678FE · Airbus A300F4605R · Fuselage, Landing Gear Attach FittingsSDR FDEA202402070209Floor Panel · delaminatedMAIN 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"Feb 7, 2024 · N678FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA202401300131Plate · deformedGROUND 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.Jan 30, 2024 · N678FE · Airbus A300F4605R · Fuselage Miscellaneous StructureSDR FDEA202401270177Skin · damagedFOUND 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.Jan 27, 2024 · N678FE · Airbus A300F4605R · Fuselage Main, Plate/SkinSDR FDEA202401250166Rib · corrodedRH #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.Jan 25, 2024 · N678FE · Airbus A300F4605R · Wing, Rib/BulkheadSDR FDEA202401170130Strap · crackedFUSELAGE 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-23Jan 17, 2024 · N678FE · Airbus A300F4605R · Fuselage Miscellaneous StructureSDR FDEA202401160129Floorbeam · crackedFOUND 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.Jan 16, 2024 · N678FE · Airbus A300F4605R · Fuselage Main, Floor BeamSDR FDEA202401150210Support Frame · crackedMAIN 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 REPLAJan 15, 2024 · N678FE · Airbus A300F4605R · Fuselage Main, StructureSDR FDEA202401150167Rib · gougedRH #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 HJan 15, 2024 · N678FE · Airbus A300F4605R · Wing, Rib/BulkheadSDR FDEA202206161437None · nonePDIS 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 : 26Jun 16, 2022 · N678FE · Airbus A300* · Wheel/Ski/FloatSDR FDEA202204130967None · damagedAIRCRAFT STRUCK LH WINGTIP WITH RH WINGTIP OF A/C 597 COMPLY WITH EA 6-0550-T0367981 COMPLIED WITH EA 6-0550-T0367981Apr 13, 2022 · N678FE · Airbus A300* · Fuselage Structure (General)SDR FDEA202109062295Floor Support · corrodedBULK 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.Sep 6, 2021 · N678FE · Airbus A300F4605R · Fuselage Miscellaneous StructureSDR FDEA202108292215Skin · dentedLH 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.Aug 29, 2021 · N678FE · Airbus A300F4605R · Wing, Plate/SkinSDR FDEA202108252216Spar · cracked1EA 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, Aug 25, 2021 · N678FE · Airbus A300F4605R · Trailing Edge FlapsSDR FDEA202108242176Stiffener · crackedRH 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.Aug 24, 2021 · N678FE · Airbus A300F4605R · Nacelle/Pylon Miscellaneous StructureSDR FDEA202108212240Floor Panel · damagedMAIN 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.Aug 21, 2021 · N678FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA202108212239Floor Panel · damagedMAIN 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.Aug 21, 2021 · N678FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA202108212238Floor Panel · damagedMAIN 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.Aug 21, 2021 · N678FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA202108132058Skin · damaged1EA 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(2Aug 13, 2021 · N678FE · Airbus A300F4605R · Elevator, Plate/SkinSDR FDEA202108132057Skin · damaged1EA 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 55Aug 13, 2021 · N678FE · Airbus A300F4605R · Elevator, Plate/SkinSDR FDEA202108132056Skin · damaged1EA 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 55-21-12-201Aug 13, 2021 · N678FE · Airbus A300F4605R · Elevator, Plate/SkinSDR FDEA202108112245Floor Panel · damagedTHE #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.Aug 11, 2021 · N678FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA202108112244Floor Panel · damagedTHE #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.Aug 11, 2021 · N678FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA202108112243Floor Panel · damagedTHE #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.Aug 11, 2021 · N678FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA202108112242Floor Panel · damagedTHE #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.Aug 11, 2021 · N678FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA202108112241Floor Panel · damagedTHE #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.Aug 11, 2021 · N678FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA202108042286Skin · damagedN00074: 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 55-41-12-2Aug 4, 2021 · N678FE · Airbus A300F4605R · Rudder, Plate/SkinSDR FDEA202108042284Rudder · damagedN00075: 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 Aug 4, 2021 · N678FE · Airbus A300F4605R · Rudder StructureSDR FDEA202108042283Rudder · damagedN00305: 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 55-41-12-201Aug 4, 2021 · N678FE · Airbus A300F4605R · Rudder StructureSDR FDEA202108042281Rudder · damagedN00306: 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 55-41-12-201Aug 4, 2021 · N678FE · Airbus A300F4605R · Rudder StructureSDR FDEA202108042288Skin · damagedN00302: 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 55-41-12-201Aug 4, 2021 · N678FE · Airbus A300F4605R · Rudder, Plate/SkinSDR FDEA202108042287Skin · damagedN00301: 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 55-41-12-201Aug 4, 2021 · N678FE · Airbus A300F4605R · Rudder, Plate/SkinSDR FDEA202108042285Skin · damagedN00303: 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 55-41-12-201Aug 4, 2021 · N678FE · Airbus A300F4605R · Rudder, Plate/Skin
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