N651FE

Service difficulty reports · 421

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 = 'N651FE' 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 FDEA202412101647Control Unit · failedDURING OPS CHECK OF 71WN FOUND THE AUTONOMOUS STANDBY UNIT FAILED OPS CHECK. REMOVED AND REPLACED AUTONOMOUS STANDBY UNIT. OPS CHECK GOOD.Oct 13, 2024 · N651FE · Airbus A300F4605R · Door Warning SystemSDR FDEA202408151129Connector · damagedR1 CEILING EMERGENCY LIGHT INOP. AMM: 33-51-00-05 WDM: 33-51-04 CLEANED AND RECECURED PLUG CONNETION 5824VC AND PERFORMED EMERGENCY LIGHT OPS TEST REF ABOVE REF, EMERGENCY LIGHTING NOW OPS CHECK NORMAL. PLACARD REMOVED. IDENTIFIED ITEM AS AN SDR, NAug 15, 2024 · N651FE · Airbus A300F4605R · Light System WiringSDR FDEA202408151128Power Supply · failedWHEN A/C WAS BOARDED, L1 AND R1 EMERGENCY EXIT SIGNS WERE ILLUMINATED WITH BOTH COCKPIT EMERGENCY SWITCH AND COURIER EMERGENCY SWITCH IN THE OFF POSITION. R/I 06JUL24 11:13 BWI REASON CODE : PREMATURE REMOVAL/INSTALLATION OFF MPN: 3214-41 POS: ONLAug 15, 2024 · N651FE · Airbus A300F4605R · Emergency LightingSDR FDEA202404300533Pitot Tube · blockedIN CRUISE AT FL340, .80M (279 IAS) ABOUT 40 MINUTES INTO THE FLIGHT, RECEIVED FO IAS DISCREPANCY ECAM. HIS STANDBY AIRSPEED INDICATOR REMAINED AT 279-280 BUT HIS PFD SPEED TAPE WENT TO 220 KTS AND VERY SLOWLY CREEPED BACK UP TO 279-280. TOOK ABOUT TWO MINApr 30, 2024 · N651FE · Airbus A300F4605R · Pitot/Static SystemSDR FDEA202404260534Indicator · malfunctionedAFTER TURBULENCE AND ICING ENCOUNTER, FL360 ADC 2 AIRSPEED INDICATION DROPPED TO 60KTS. FO STANDBY, CAPT STANDBY AND ADC 1 SHOWED CORRECT INDICATION. FOLLOWED QRH PROCEDURE. AMM: 34-10-00-05, AMM: 22-40-00-05 PERFORMED BITE CHECK ON #2 ADC, TEST OK, AIRSPEApr 26, 2024 · N651FE · Airbus A300F4605R · Airspeed/Mach IndicatorSDR FDEA202404230535Adc · failedAT FL350, .78 MACH, ABOUT 1 HOUR INTO FLIGHT, FO SPEED TAPE BEGAN ROLLING BACK FOLLOWED BY IAS DISCREPANCY ECAM ALERT. FOLLOWED ECAM AND QRH SWITCHING TO SYS 1 ADC ON FO SIDE. SUSPECT ADC2 FAILURE. R & R NO.2 ADC, PERFORMED SATISFACTORY ADS2 BITE TEST. COMPApr 23, 2024 · N651FE · Airbus A300F4605R · Altimeter, Barometric/EncoderSDR FDEA202403280390Seat Track · brokenSEAT TRACK LOBES BROKEN UNDER LOCK POSITION MG0828. NO FLOOR PANEL DAMAGE AND NO SEAT TRACK CRACKS. FABRICATED, LOCATED, AND MATCH-DRILLED NEW SEAT TRACK SECTION AND SPLICE FITTINGS IAW SRM FIG. 201. INSTALLED THE SEAT TRACK AND REPAIR IAW SRM 53-10-16.Mar 28, 2024 · N651FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR FDEA202312220068Fitting · corrodedLH RIB 5, MLG FWD PINTLE AIRFRAME ATTACH FITTING HAS CORROSION ON AFT SPOT FACE. REPAIRED PER AIRBUS INSTRUCTIONS R57240425Dec 22, 2023 · N651FE · Airbus A300F4605R · Main Landing Gear Attach SectionSDR FDEA202312220067Fitting · corrodedLH RIB 5, MLG FWD PINTLE AIRFRAME ATTACH FITTING HAS CORROSION ON FWD SPOT FACE. REPAIRED PER AIRBUS INSTRUCTIONS R57240425Dec 22, 2023 · N651FE · Airbus A300F4605R · Main Landing Gear Attach SectionSDR FDEA202312200066Fitting · corrodedL/H MLG AFT PINTLE FWD LUG HAS SIGN OF CORROSION. REPAIRED PER AIRBUS INSTRUCTIONS R57240425Dec 20, 2023 · N651FE · Airbus A300F4605R · Main Landing Gear Attach SectionSDR FDEA202303210563Skin · unknownAGING AIRCRAFT ASSESSMENT : EXISTING DOUBLER REPAIR FOUND ON RH I/B FLAP LWR SKIN BTW RIB 11~13 T/E-9". COMPLIED WITH ATTACHMENT B OF EO: E 6-5100-7-5000 D7 PT1, TITLE: STRUCTURES-REPAIR CATALOG-A300/A310 REPAIR IDENTIFICATION & TRACKING REQUIREMENTS 14 CMar 21, 2023 · N651FE · Airbus A300* · Wing, Control SurfacesSDR FDEA202303210562Skin · unknownAGING AIRCRAFT ASSESSMENT : EXISTING DOUBLER REPAIR FOUND ON RH I/B FLAP LWR SKIN BTW RIB 11~13 T/E-9". COMPLIED WITH ATTACHMENT B OF EO: E 6-5100-7-5000 D7 PT1, TITLE: STRUCTURES-REPAIR CATALOG-A300/A310 REPAIR IDENTIFICATION & TRACKING REQUIREMENTS 14 CMar 21, 2023 · N651FE · Airbus A300* · Wing, Control SurfacesSDR FDEA202303210561Skin · unknownAGING AIRCRAFT ASSESSMENT : EXISTING DOUBLER REPAIR FOUND ON RH I/B FLAP UPR SKIN BTW RIB 1C~5,STGR 2.1~2.2. COMPLIED WITH ATTACHMENT B OF EO: E 6-5100-7-5000 D7 PT1, TITLE: STRUCTURES-REPAIR CATALOG-A300/A310 REPAIR IDENTIFICATION & TRACKING REQUIREMENTS Mar 21, 2023 · N651FE · Airbus A300* · Wing, Control SurfacesSDR FDEA202303150622Skin · unknownEXISTING REPAIR ON RH WING #1 SLAT TAIL SECTION UPR SKIN, T/E-8.5" POSITION, BTW RIB 22~24, EVALUATE TO DETERMINE WHETHER IT IS ACCOMPLISHED BY APPROVED DATA DUE TO NO EXISTING DOCUMENTATION SUPPORTING THIS REPAIR, REMOVED THE EXISTING REPAIR AND PERFORMEDMar 15, 2023 · N651FE · Airbus A300* · Wing, Control SurfacesSDR FDEA202303150621Skin · unknownEXISTING REPAIR ON RH WING #1 SLAT TAIL SECTION UPR SKIN, T/E-11.5" POSITION, BTW RIB 8~9, EVALUATE TO DETERMINE WHETHER IT IS ACCOMPLISHED BY APPROVED DATA DUE TO NO EXISTING DOCUMENTATION SUPPORTING THIS REPAIR, REMOVED THE EXISTING REPAIR AND PERFORMED Mar 15, 2023 · N651FE · Airbus A300* · Wing, Control SurfacesSDR FDEA202303090400Seat Track · wornFR54/FR54.2 RH NO.2 DUMMY SEAT TRACK GAP OVER 1.0MM. I.A.W A300-600 SRM 53-15-16 PARA 5A FIG.201 P201-P210 PERFORM REPAIR ACCOMPLISHED.Mar 9, 2023 · N651FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR FDEA202303080646Spoiler · delaminatedLH WING #6 SPOILER L/E CTR SECTION DELAMINATED. REMOVED L6 SPLR, REPAIRED THE DELAMINATION AREA, REINSTALLED, ADJUSTED, AND PFMED TEST OF L6 SPLR IAW A300-600 AMM 27-61-53-04 AND A300-600F SRM 57-72-11-201, PARA.12, PAGE.211-213, FIG.206. "MAJOR REPAIR"Mar 8, 2023 · N651FE · Airbus A300* · Wing StructureSDR FDEA202303080626Skin · delaminatedLH WING #6 SPOILER L/E CTR SECTION DELAMINATED REMOVED L6 SPLR, REPAIRED THE DELAMINATION AREA, REINSTALLED, ADJUSTED, AND PFMED TEST OF L6 SPLR IAW A300-600 AMM 27-61-53-04 AND A300-600F SRM 57-72-11-201, PARA.12, PAGE.211-213, FIG.206. "MAJOR REPAIR"Mar 8, 2023 · N651FE · Airbus A300* · Wing StructureSDR FDEA202303070645Slat · unknownAGING AIRCRAFT ASSESSMENT : EXISTING FLUSH DOUBLER REPAIR FOUND ON RH WING #3 SLAT NOSE SKIN O/B END. DUE TO NO APPROVED DOCUMENTATION TO SUPPORT THE REPAIR, REMOVED ALL REPAIR PARTS AND PERFORMED NEW REPAIR TO THE AREA I.A.W. EA# T6-5750-T0373565 P1, TITLMar 7, 2023 · N651FE · Airbus A300* · Wing, Control SurfacesSDR FDEA202303070644Spoiler · delaminated1EA DELAMINATION WAS FOUND (2" X 1") AT LH SPOILER NO.5 UPPER SKIN. REMOVED L5 SPLR, REPAIRED THE DELAMINATION AREA, REINSTALLED, ADJUSTED, AND PFMED TEST OF L5 SPLR IAW A300-600 AMM 27-61-53-04 AND A300-600F SRM 57-72-11-201, PARA.12, P.211~213, FIG.206. Mar 7, 2023 · N651FE · Airbus A300* · Wing StructureSDR FDEA202303070631Skin · noneEXISTING FLUSH DOUBLER REPAIR FOUND ON RH WING #3 SLAT NOSE SKIN O/B END. DUE TO NO APPROVED DOCUMENTATION TO SUPPORT THE REPAIR, REMOVED ALL REPAIR PARTS AND PERFORMED NEW REPAIR TO THE AREA I.A.W. EA# T6-5750-T0373565 P1, TITLE: WINGS- FLIGHT SURFACES-RMar 7, 2023 · N651FE · Airbus A300* · Wing, Control SurfacesSDR FDEA202303070625Skin · delaminated1EA DELAMINATION WAS FOUND (2" X 1") AT LH SPOILER NO.5 UPPER SKIN REMOVED L5 SPLR, REPAIRED THE DELAMINATION AREA, REINSTALLED, ADJUSTED, AND PFMED TEST OF L5 SPLR IAW A300-600 AMM 27-61-53-04 AND A300-600F SRM 57-72-11-201, PARA.12, P.211~213, FIG.206. Mar 7, 2023 · N651FE · Airbus A300* · Wing StructureSDR FDEA202303070544Seat Track · unknownN00119 AGING AIRCRAFT ASSESSMENT : EXISTING SPLICE REPAIR FOUND ON M/D SEAT TRACK, BTW FR 31~32, -Y1456 FOUND THE EXISTING SPLICE REPAIR UPPER FLANGE NOT COMPLIANCE WITH APPROVED DATA: A300-600F SRM 53-10-16-201, FIG.201, REMOVED HILOKS AND PERFORMED ROTOTMar 7, 2023 · N651FE · Airbus A300* · Fuselage Main, StructureSDR FDEA202303070493Seat Track · unknownN00125 AGING AIRCRAFT ASSESSMENT : EXISTING SPLICE REPAIR FOUND ON M/D SEAT TRACK, BTW FR 69~70, 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 121Mar 7, 2023 · N651FE · Airbus A300* · Fuselage Main, StructureSDR FDEA202303070492Seat Track · unknownN00124 AGING AIRCRAFT ASSESSMENT : EXISTING SPLICE REPAIR FOUND ON M/D SEAT TRACK, BTW FR 67~68, -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 12Mar 7, 2023 · N651FE · Airbus A300* · Fuselage Main, StructureSDR FDEA202303070491Seat Track · unknownN00123 AGING AIRCRAFT ASSESSMENT : EXISTING SPLICE REPAIR FOUND ON M/D SEAT TRACK, BTW FR 67~68, -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 1Mar 7, 2023 · N651FE · Airbus A300* · Fuselage Main, StructureSDR FDEA202303070490Seat Track · unknownN00122 AGING AIRCRAFT ASSESSMENT : EXISTING SPLICE REPAIR FOUND ON M/D SEAT TRACK, BTW FR 65~69, 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 121.7Mar 7, 2023 · N651FE · Airbus A300* · Fuselage Main, StructureSDR FDEA202303070489Seat Track · unknownN00121 AGING AIRCRAFT ASSESSMENT : EXISTING SPLICE REPAIR FOUND ON M/D SEAT TRACK, BTW FR 62~63, -Y953 COMPLIED WITH ATTACHMENT B OF EO:E6-5100-7-5000 D7 PT1, TITLE:STRUCTURES-REPAIR CATALOG-A300/A310 REPAIR IDENTIFICATION & TRACKING REQUIREMENTS 14 CFR 12Mar 7, 2023 · N651FE · Airbus A300* · Fuselage Main, StructureSDR FDEA202303070488Seat Track · unknownN00120 AGING AIRCRAFT ASSESSMENT : EXISTING SPLICE REPAIR FOUND ON M/D SEAT TRACK, BTW FR 55~56, -Y953 COMPLIED WITH ATTACHMENT B OF EO:E6-5100-7-5000 D7 PT1, TITLE:STRUCTURES-REPAIR CATALOG-A300/A310 REPAIR IDENTIFICATION & TRACKING REQUIREMENTS 14 CFR 12Mar 7, 2023 · N651FE · Airbus A300* · Fuselage Main, StructureSDR FDEA202303030483Aileron · damagedLH WING AILERON UPPER SKIN DEFORMED AT RIB1 & REAR SPAR-17" ACCOMPLISHED THE DOUBLER REPAIR, THIS IS CAT.A REPAIR I.A.W A300-600F SRM 57-61-11-201, PARA.4D, PAGE.213-PAGE.216, FIG.204 MAJOR REPAIRMar 3, 2023 · N651FE · Airbus A300* · Wing, Control SurfacesSDR FDEA202303020596Skin · damagedEVALUATE PREVIOUS DENT AT LHS FUSELAGE LWR SKIN FR10 6", 8 O'CLOCK. ACCOMPLISHED THECAT B DOUBLER REPAIR IAW A300-600F SRM 53-12-12-201, CONFIG 2, PAR. 5A, PAGE 203-208, FIG.201 & SRI 53-12-12-201, IR 53-12-12-2-006-00, PARA. 3F, TABLE 207 "MAJOR REPAIR".Mar 2, 2023 · N651FE · Airbus A300* · Fuselage Main, Plate/SkinSDR FDEA202204180988Control Module · unknownMDIS 651 26-10 5623 18APR22 IND OPEN U #1 ENGINE AGENT #2 SQUIB INOP SHGN 18APR22 15:25 IND U WHEN TESTING #1 ENG SQUIB, AGENT 2 SQUIB LIGHT IS NOT ILLUMINATING. SQUIB LIGHT ILLUMINATES W/ ANNUN LT TEST. PER A300-600 TSM 26-21-00, FIG 11Apr 18, 2022 · N651FE · Airbus A300* · Detection SystemSDR FDEA202203180745Light · inoperativeMDIS 651 33-50 5547 18MAR22 LRD FACT U LAVATORY AUXILIARY MIRROW EMERGENCY LIGHT OUT. FACT 18MAR22 14:45 LRD U RELAMPED LAV AUX MIRROW EMERGENCY, IAW AMM 33-51-21-04, OPS CKS NORMAL AT THIS TIME.Mar 18, 2022 · N651FE · Airbus A300F4605R · Emergency LightingSDR FDEA202203150527Power Supply · unknownSLIDE DID NOT DISPLAY ON ECAM WHEN ARMING RIGHT CABIN DOOR. RELEASED FOR SERVICE PER MEL : 52- XX-XX CATEGORY : C EXP: 25MAR22 - (R1) DOOR - INOP. DOOR ESCAPE SLIDE ARMING SYSTEM IS TO BE VERIFIED AS FULLY ARMED PRIOR TO EACH DEPARTURE." AUTONOMOUS STANDBMar 15, 2022 · N651FE · Airbus A300* · Cargo/Baggage DoorsSDR FDEA202109232384Controller · inoperativeAFTER T/O ON SLAT RETRACTION HAD KRUEGER FAULT. RAN APPROPRIATE CHECKLISTS AND RTB. PERFORMED BITE DISPLAY OF BOTH SFCC'S AND FOUND ALL OF THE FAULT BALLS FOR THE NR 1 UNIT LIGHT. THAT FAULT CODE CORRESPONDS WITH BAD SFCC REF AMM 27-80-00. IND INSPECTEDSep 23, 2021 · N651FE · Airbus A300F4605R · Leading Edge Slat Control SystemSDR FDEA202010032403Actuator · failedCREW REPORT: DURING MANUAL GEAR EXTENSION GOT LOUD NOISE AND EXCESSIVE VIBRATION ABOVE NORMAL LEVELS. WOULD NOT RECYCLE, REMOVED AND REPLACED NLG DOOR ACTUATOR LT SIDE. REMOVED AND REPLACED NOSE GEAR SEQUENCE VALVE. REMOVED AND REPLACED NON RETURN VALVE. Oct 3, 2020 · N651FE · Airbus A300F4605R · Landing Gear Door Retract SectionSDR FDEA202008272047Pin · missingMISSING PASSENGER CREW DOOR 831 INFLATE RESERVOIR SAFETY PIN ESCAPE SLIDE RAFT AT FWD GALLEY AREA (1EA). REPLACED PASSENGER CREW DOOR 831 ESCAPE SLIDE RAFT IAW AMM 25-61-21-04 AT FWD GALLEY AREA.Aug 27, 2020 · N651FE · Airbus A300F4605R · Escape SlideSDR FDEA202008171959Bolt · corrodedCORROSION BOLT ATTACHMENT SLAT TRACK 7 UPPER POSITION ON LH WING (1 EA) REPLACED BOLT ATTACHMENT SLAT TRACK 7 UPPER POSITION ON LH WING IAW AMM 27-80-14- 04.Aug 17, 2020 · N651FE · Airbus A300F4605R · Leading Edge DevicesSDR FDEA2020081871927Bolt · corrodedONE CORRODED BOLT ATTACHMENT ON SLAT TRACK NR 7 LOWER POSITION OF THE LT WING. REPLACED THE BOLT IAW AMM 27-80-14-04.Aug 17, 2020 · N651FE · Airbus A300F4605R · Leading Edge DevicesSDR FDEA2020009091896Floor Panel · crackedCRACK FLOOR PANEL 232VH. THIS NON ROUTINE CARD IS FOR PURPOSE RDR GENERATION IN PASSENGER CABIN (1 EA). MANUFACTURED FLOOR PANEL 232VH, AS PER DWG SRZ-25-005 REV. R AUG-22-2019. FLOOR PANEL MARKED WITH P/N FX B5327048401400 FDX AUG-11-2020, AS PER GMM 7-0-1Aug 15, 2020 · N651FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA2020082851896Floor Panel · crackedCRACK FLOOR PANEL 232VH THIS NON ROUTINE CARD IS FOR PURPOSE RDR GENERATION IN PASSENGER CABIN (1 EA) MANUFACTURED FLOOR PANEL 232VH AS PER DWG SRZ-25-005 REV.R AUG-22-2019 AND FLOOR PANEL MARKED WITH P/N: FX B5327048401400 FDX AUG-11-2020 AS PER GMM 7-0-1001,Aug 15, 2020 · N651FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA2020082051941Floor Panel · delaminatedDELAMINATED FLOOR PANEL 242LK. REPAIRED THE FLOOR PANEL IAW DWG SRZ 25-005 REV. R.Aug 15, 2020 · N651FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA2020081851896Floor Panel · crackedCRACK FLOOR PANEL 232VH THIS NON ROUTINE CARD IS FOR PURPOSE RDR GENERATION IN PASSENGER CABIN (1 EA) MANUFACTURED FLOOR PANEL 232VH AS PER DWG SRZ-25-005 REV. R AUG-22-2019. THIS NON ROUTINE CARD IS FOR PURPOSE RDR, SDR GENERATION. THIS JOB IS DOCUMENTED Aug 15, 2020 · N651FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA202008071957Floor Panel · delaminatedDELAMINATED FLOOR PANEL 231UG ON MAIN DECK AFT CARGO COMPARTMENT THIS TASK CARD IS GENERATED FOR RDR PURPOSE IN PASSENGER CABIN (1 EA) THE REPAIR IS DOCUMENTED ON NON ROUTINE CARD N00343,Aug 7, 2020 · N651FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA202008071960Floor Panel · delaminatedDELAMINATED FLOOR PANEL 231ZG ON MAIN DECK AFT CARGO COMPARTMENT THIS TASK CARD IS GENERATED FOR RDR PURPOSE IN PASSENGER CABIN (1 EA) THE REPAIR IS DOCUMENTED ON NON ROUTINE CARD N00343, THIS SNRM, (N00653) IS GENERATED RDR PURPOSEAug 7, 2020 · N651FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA202008071958Floor Panel · delaminatedDELAMINATED FLOOR PANEL 231NG ON MAIN DECK AFT CARGO COMPARTMENT THIS TASK CARD IS GENERATED FPR RDR PURPOSE IN PASSENGER CABIN (1 EA) THE REPAIR IS DOCUMENTED ON NON ROUTINE CARD N00543,Aug 7, 2020 · N651FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA2020082071956Floor Panel · delaminatedDELAMINATED TOP LAYER FLOOR PANEL (MAIN DECK) 241EF IN PASSENGER CABIN (1 EA) REPAIRED FLOOR PANEL 241EF ON MAIN DECK ASPER A300 SRM 53-10-20 PAGEBLOCK 201 PARA B TOOL USED CALIPER PN 500-197-30 S/N A18135089 DUE DATE JUL-11-2021 SCALE PN CL5000 S/N AE-398Aug 7, 2020 · N651FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA2020082641977Bolt · corrodedCORROSION BOLT ATTACHMENT SLAT TRACK 8 ECCENTRIC BOLT ON RT WING. REPLACED BOLT ATTACHMENT SLAT TRACK 8 ECCENTRIC BOLT ON RY WING IAW AMM 27-80-14-04.Aug 4, 2020 · N651FE · Airbus A300F4605R · Wing Miscellaneous StructureSDR FDEA2020082141961Bolt · corrodedCORROSION SLAT 2 SCREWJACK 4 BOLT ON LH WING REPLACED SLAT 2 SCREWJACK BOLT ON LH WING IAW AMM 27-84-22-04 STEP 2.D(5)(A)Aug 4, 2020 · N651FE · Airbus A300F4605R · Leading Edge DevicesSDR FDEA2020082041955Bolt · corrodedCORROSION BOLT ATTACHMENT SLAT TRACK 11 FWD LOWER POSITION ON RH WING REPLACED BOLT ATTACHMENT SLAT TRACK 11 FWD LOWER POSITION ON RH WING IAW AMM 27- 80-12-04Aug 4, 2020 · N651FE · Airbus A300F4605R · Leading Edge Devices
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