N728FD

Service difficulty reports · 266

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 = 'N728FD' 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 FDEA202510192053Skin · crackedAFT CARGO COMPARTMENT DOOR UPPER INNER SKIN 2EA CRACKS WERE FOUND AT FR61 - FR62 COMPLIED WITH EA 6-5230-T0385399 P1. TITLE: DOORS - CARGO DOOR/HYD SYS - AFT CARGO DOOR INNER SKINS AND ACTUATOR FITTING AT FR61A - CRACKS, PERMANENT REPAIR. REPAIRED AFT CARGOct 19, 2025 · N728FD · Airbus A300B4622R · Cargo/Baggage DoorsSDR FDEA202510192052Fitting · crackedAFT CARGO COMPARTMENT DOOR ACTUATOR FITTING CRACKEDOct 19, 2025 · N728FD · Airbus A300B4622R · Cargo/Baggage DoorsSDR FDEA202510172038Floorbeam · corrodedFWD CARGO COMPARTMENT FLOOR SUPPORT BEAM CORRODED AT FR29 Y-1470 REPAIRED THE FWD CARGO COMPARTMENT CORRODED FLOOR SUPPORT BEAM AT FR29 Y-1470 PER A300-600 SRM53-10-15-201 FIGURE 207 AND EA: 6-5321-T0385349 P1. TITLE: FUSELAGE - CARGO COMP FLOOR - FWD CAROct 17, 2025 · N728FD · Airbus A300B4622R · Fuselage Main, Floor BeamSDR FDEA202510172037Roller Track · corrodedFWD CARGO COMPARTMENT LOADING SYS TRACK CORRODED AT FR38.1 - FR38.2 Y140 REPAIRED THE FWD CARGO COMPARTMENT CORRODED LOADING SYS TRACK AT FR38.1 - FR38.2 Y140 PER A300-600 SRM53-10-15-201 FIG.203. THIS IS CAT A REPAIR, MAJOR REPAIR IAW GMM6-2-100.Oct 17, 2025 · N728FD · Airbus A300B4622R · Cargo CompartmentsSDR FDEA202510152008Frame · crackedNDT INSPECTION, LT SIDE FUSELAGE FRAME FR73A ONE RIVET HOLE CRACKED AT S24L - S25L REPAIRED LH DOOR FRAME FR73A RIVET HOLE AT STGR24 - STGR25.THIS IS CATEGORY B REPAIR.MAJOR REPAIR IAW FEDEX GMM6-2-100.SEE WRI 53100887 FOR WORK DETAILS.Oct 15, 2025 · N728FD · Airbus A300B4622R · Fuselage Main, FrameSDR FDEA202510152007Frame · crackedNDT INSP - RH SIDE FUSELAGE FRAME FR73A 1EA RIVET HOLE CRACKED AT STGR24 - STGR25 COMPLIED WITH EA:6-5310-T0385324 P1,TITLE: FUSELAGE - MAINFRAME - EO 6-5310-E0327267 (SB A300-53-6175) INSPECTION - CRACK FOUND ON LH & RH DOOR FRAME FR73A - SPLICE REPAIR PEOct 15, 2025 · N728FD · Airbus A300B4622R · Fuselage Main, FrameSDR FDEA202510141980Hinge Arm · delaminatedRH WING - #4 SPOILER INBD HINGE ARM INBD SIDE AND OTBD HIINGE ARM OUTBD SIDE DELAMINATED. 1.80MM*40MM*1.55MM 2.90MM*40MM*1.45MM. COMPLIED WITH EA 6-5750-T0319441 P2. TITLE: WINGS - FLIGHT SURFACES - RH #4 SPOILER LOWER SKIN REPAIR - OUTSIDE CENTER HINGE AOct 14, 2025 · N728FD · Airbus A300B4622R · SpoilersSDR FDEA202510141979Hinge Arm · delaminatedRH WING - #3 SPOILER INBD HINGE ARM INBD SIDE AND OUTBD HINGE ARM OUTBD SIDE DELAMINATED .1.80MM*15MM*0.92MM 2.30MM*25MM*1.09MM 3.25MM*18MM*0.96MMOct 14, 2025 · N728FD · Airbus A300B4622R · SpoilersSDR FDEA202510141978Hinge Arm · delaminatedLH WING - NR 3 SPOILER OUTBD HINGE ARM OUTBD SIDE AND INBD HINGE ARM INBD SIDE DELAMINATED. 1.65MM, 820MM, 81.38MM, 2.100, MM, 20MM, 1.73MM. COMPLIED WITH EA 6-5750-T0385295 P1. REPAIRED THE LH WING #3 SPOILER OTBD HINGE ARM OTBD SIDE & INBD HINGE ARM OTBD Oct 14, 2025 · N728FD · Airbus A300B4622R · Leading Edge DevicesSDR FDEA202510141977Hinge Arm · delaminatedLEFT WNG - #5 SPOILER OUTBD HINGE ARM OUTBD SIDE DELAMINATED. 80MM*20MM*1.62MM COMPLIED WITH EA 6-5750-T0385306 P1. TITLE: WINGS - FLIGHT SURFACES - LH #5 SPOILER CENTER HINGE ARM OUTSIDE SURFACE DELAMINATION. REPAIRED THE LH WING #5 SPOILER OUTBD HINGE AOct 14, 2025 · N728FD · Airbus A300B4622R · SpoilersSDR FDEA202510131975Floorbeam · corrodedAFT CARGO COMPARTMENT FLOOR SUPPORT BEAM CORRODED AT FR58 Y-805 - Y-1470 REPAIRED THE AFT CARGO COMPARTMENT CORRODED FLOOR SUPPORT BEAM AT FR58 Y-805 - Y- 1470 PER A300-600 SRM53-10-15-201 FIGURE 207 AND EA: 6-5321-T0385357 P1. TITLE: FUSELAGE - CARGO COMPOct 13, 2025 · N728FD · Airbus A300B4622R · Fuselage Main, Floor BeamSDR FDEA202510091931Fitting · not reportedCOMPLY WITH: DOORS - CARGO DOOR/HYD SYS - DETAILED VISUAL INSPECTION OF THE MAIN DECK CARGO DOOR (MDCD) ACTUATOR BEARING FITTINGS AT FRAME 23 AND 24 - AOT A52W016- 24. COMPLIED WITH EO 6-5230-E0378588 B P5. TITLE: DOORS - CARGO DOOR/HYD SYS - DETAILED VISOct 9, 2025 · N728FD · Airbus A300B4622R · Cargo/Baggage DoorsSDR FDEA202510091930Skin · contaminatedLEFT ELEVATOR TOP SKIN AT ER13 FOUND WATER INJECTED. REPAIRED LH ELEVATOR TOP SKIN AT ER13 FOUND WATER INJECTED PER A300-600 SRM55-21-12-201 PARA.5.J & SRM51-77-12-201 & EA 6-5520-T0385455 P1. EA TITLE: STABILIZERS - ELEVATORS - LH ELEVATOR UPPER SKIN REPOct 9, 2025 · N728FD · Airbus A300B4622R · Elevator, Plate/SkinSDR FDEA202510091929Rib · crackedNDT INSP - LH WING CENTER FLAP INNER STRUCTURE RIB25/STGR2.8 - REAR SPAR,RIB26/STGR2.6-2.7,RIB26/STGR2.7-2.8,RIB27/STGR2.7-2.8,RIB27/STGR2.8-REAR SPAR TOTAL OF 5 CRACKS FOUND. REPAIRED THE CRACKED RIB UPR FLANGE AT LH WING CENTER FLAP RIB25/STGR2.8 - REAOct 9, 2025 · N728FD · Airbus A300B4622R · Trailing Edge FlapsSDR FDEA202510091928Rib · crackedNDT INSP - LH WING CENTER FLAP INNER STRUCTURE RIB18/STGR2.8 - REAR SPAR 1EA CRACK WAS FOUND. COMPLIED WITH EA: 6-5750-T0319244 P2, TITLE: WINGS - FLIGHT SURFACES - LHS CENTER FLAP RIB 18 CRACKED AT UPPER FLANGE BETWEEN STGR2.8 AND REAR SPAR. REPAIRED THEOct 9, 2025 · N728FD · Airbus A300B4622R · Trailing Edge FlapsSDR FDEA202510091927Rib · crackedNDT INSP - LT WING CENTER FLAP INNER STRUCTURE 1EA CRACK WAS FOUND RIB11/STGR2.7 - 2.8 COMPLIED WITH EA: 6-5750-T0337526 P2. TITLE: WINGS - FLIGHT SURFACES - LHW, CENTER FLAP, SKIN AND RIB REPAIRS PER SRM - RSC TRACKING. REPAIRED THE LH WING CENTER FLAP INNEROct 9, 2025 · N728FD · Airbus A300B4622R · Trailing Edge FlapsSDR FDEA202510091926Rib · crackedNDT INSP - RH WING CENTER FLAP RIBS UPR FLANGE FOUND 1EA CRACK AT RIB17 B/W STGR2.8 AND REAR SPAR. REPAIRED THE CRACKED RIB UPR FLANGE AT RH WING CENTER FLAP RIB17 BETWEEN STGR2.8 AND REAR SPAR. THIS IS CATEGORY A REPAIR. MAJOR REPAIR IAW FEDEX GMM6-2-Oct 9, 2025 · N728FD · Airbus A300B4622R · Trailing Edge FlapsSDR FDEA202510091925Rib · crackedNDT INSP - RH WING CENTER FLAP RIBS UPR FLANGE FOUND 1EA CRACK AT RIB11 & RIB12 & RIB13 & RIB15 B/W STGR2.8 AND REAR SPAR. REPAIRED THE CRACKED RIB UPR FLANGE AT RH WING CENTER FLAP RIB11 & RIB12 & RIB15 BETWEEN STGR2.8 AND REAR SPAR,RIB13 BETWEEN STGR2Oct 9, 2025 · N728FD · Airbus A300B4622R · Trailing Edge FlapsSDR FDEA202510091924Rib · crackedNDT INSP - RH WING CENTER FLAP RIBS UPR FLANGE FOUND 4EA CRACK AT RIB19 BETWEENSTGR2.6 AND REAR SPAR,RIB20 B/W STGR2.8 AND REAR SPAR. REPAIRED THE CRACKED RIB UPR FLANGE AT RT WING CENTER FLAP RIB19 BETWEEN STGR2.6 AND REAR SPAR,RIB20 BETWEEN STGR2.8 AND Oct 9, 2025 · N728FD · Airbus A300B4622R · Trailing Edge FlapsSDR FDEA202510091923Rib · crackedNDT INSP - RT WING CENTER FLAP RIBS UPR FLANGE FOUND 3EA CRACK AT RIB26 BETWEEN STGR2.6 AND REAR SPAR. REPAIRED THE CRACKED RIB UPR FLANGE AT RH WING CENTER FLAP RIB26 BETWEEN STGR2.6 AND REAR SPAR. THIS IS CATEGORY A REPAIR. MAJOR REPAIR IAW GMM6-2-100.Oct 9, 2025 · N728FD · Airbus A300B4622R · Trailing Edge FlapsSDR FDEA202306141129Bracket · crackedAFT CGO COMP'T FWD PRESSURE BULKHEAD SUPPORT BRACKET CRACK AT CENTERLINE FR54 POSITION. REPLACED THE NEW BRACKET. I.A.W A300-600 SRM 51-72-10-001,P2.Jun 14, 2023 · N728FD · Airbus A300* · Fuselage Miscellaneous StructureSDR FDEA202306131085Profile · crackedAFT MAIN DECK UTILITY FLOOR LEVEL AREA FOUND Z PROFILE CRACKED AT FR80 AND Y1470 REPLACED THE DAMAGE PART WITH NEW. I.A.W A300-600 SRM 51-72-10-001,PAGE.2Jun 13, 2023 · N728FD · Airbus A300* · Fuselage Miscellaneous StructureSDR FDEA202306131084Profile · crackedAFT MAIN DECK UTILITY FLOOR LEVEL AREA FOUND Z PROFILE CRACKED AT FR80 AND Y-1470 REPLACED THE DAMAGE PART WITH NEW. I.A.W A300-600 SRM 51-72-10-001,PAGE.2Jun 13, 2023 · N728FD · Airbus A300* · Fuselage Miscellaneous StructureSDR FDEA202306121107Elevator · unknownAGING AIRCRAFT ASSESSMENT : EXISTING COMPOSITE REPAIR FOUND ON LH ELEVATOR LWR SKIN AT ER10 12", T/E-5" POSITION COMPLIED WITH ATTACHMENT B OF EO:E6-5100-7-5000 D7 PT1, TITLE:STRUCTURES-REPAIR CATALOG-A300/A310 REPAIR IDENTIFICATION & TRACKING REQUIREMENTSJun 12, 2023 · N728FD · Airbus A300* · Elevator StructureSDR FDEA202306121106Elevator · unknownAGING AIRCRAFT ASSESSMENT : EXISTING COMPOSITE REPAIR FOUND ON LH ELEVATOR LWR SKIN AT ER7 23", T/E-5.5" POSITION COMPLIED WITH ATTACHMENT B OF EO:E6-5100-7-5000 D7 PT1, TITLE:STRUCTURES-REPAIR CATALOG-A300/A310 REPAIR IDENTIFICATION & TRACKING REQUIREMENTJun 12, 2023 · N728FD · Airbus A300* · Elevator StructureSDR FDEA202306121105Elevator · unknownAGING AIRCRAFT ASSESSMENT : EXISTING COMPOSITE REPAIR FOUND ON LH ELEVATOR LWR SKIN AT ER5, T/E-4" POSITION COMPLIED WITH ATTACHMENT B OF EO:E6-5100-7-5000 D7 PT1, TITLE:STRUCTURES-REPAIR CATALOG-A300/A310 REPAIR IDENTIFICATION & TRACKING REQUIREMENTS 14 CJun 12, 2023 · N728FD · Airbus A300* · Elevator StructureSDR FDEA202306121104Elevator · unknownAGING AIRCRAFT ASSESSMENT : EXISTING COMPOSITE REPAIR FOUND ON LH ELEVATOR LWR SKIN AT ER2 18", T/E-6" POSITION COMPLIED WITH ATTACHMENT B OF EO:E6-5100-7-5000 D7 PT1, TITLE:STRUCTURES-REPAIR CATALOG-A300/A310 REPAIR IDENTIFICATION & TRACKING REQUIREMENTS Jun 12, 2023 · N728FD · Airbus A300* · Elevator StructureSDR FDEA202306111108Stringer · unknownAIRCRAFT REPAIR ASSESSMENT : EXISTING COUPLING REPAIR FOUND ON STRINGER BTW FR 36~37, STGR 33L COMPLIED WITH ATTACHMENT B OF EO:E6-5100-7-5000 D7 PT1, TITLE:STRUCTURES-REPAIR CATALOG-A300/A310 REPAIR IDENTIFICATION & TRACKING REQUIREMENTS 14 CFR 121.707, Jun 11, 2023 · N728FD · Airbus A300* · Fuselage Main, StructureSDR FDEA202306101196Spoiler · damagedRH WING #2 SPOILER FRONT SPAR FITTING O/B SIDE GOT A PUNCTURED CUT OUT AND INSTALLED WITH REPAIR PARTS I.A.W FEDEX EA NO:T6-5750-T0374908 P1, SEQ NO:966, TITLE:WING-FLIGHT SURFACES-RH #2 SPOILER-WEAR DAMAGE AND MATERIAL TEAR-OUT AT OUTBD FACE OF FRONT SPARJun 10, 2023 · N728FD · Airbus A300* · SpoilersSDR FDEA202306101175Angle · corrodedTHE SHIELD SUPPORT PLATE OF FWD BULKHEAD WAS FOUND CORROSION JUST ABOVE THE RADAR MOUNT UPPER RH SIDE FABRICATED AND INSTALLED NEW PART I.A.W FEDEX EA NO:T6-5340-T0375002 P1, SEQ NO:962, TITLE:FUSELAGE-ATTACH FITTINGS-FWD PRESSURE BULKHEAD-RADAR ANTENNA UPJun 10, 2023 · N728FD · Airbus A300* · Fuselage Main, Attach FittingsSDR FDEA202306091179Splice · corrodedAVIONICS COMP'T BILGE STRUCTURE OF SPLICE GOT CORRODED AT FR19,STGR-52L POSITION REPLACED THE CORRODED SPLICE WITH NEW PART I.A.W A300-600 SRM 51-72-10-001, PAGE.2 & 51-40-21-001, PARA.6~7, PAGE.7B~23Jun 9, 2023 · N728FD · Airbus A300* · Fuselage Main, StructureSDR FDEA202306091125Angle · crackedAVIONICS COMP'T FLOOR BEAM ANGLE FITTING CRACK AT FR10,Y403 POSITION. REPLACED THE NEW ANGLE. I.A.W A300-600 SRM 51-72-10-001, P.2Jun 9, 2023 · N728FD · Airbus A300* · Fuselage Miscellaneous StructureSDR FDEA202306091086Seat Track · unknownAGING AIRCRAFT ASSESSMENT : EXISTING SPLICE REPAIR FOUND ON M/D SEAT TRACK, BTW FR 62~65, -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 121.707, Jun 9, 2023 · N728FD · Airbus A300* · Fuselage, Seat/Cargo Attach FittingsSDR FDEA202306081089Aileron · unknownAGING AIRCRAFT ASSESSMENT : EXISTING DOUBLER REPAIR FOUND ON RH WING AILERON LWR SKIN BTW RIB 8~9,T/E-4" COMPLIED WITH ATTACHMENT B OF EO:E6-5100-7-5000 D7 PT1, TITLE:STRUCTURES-REPAIR CATALOG-A300/A310 REPAIR IDENTIFICATION & TRACKING REQUIREMENTS 14 CFR Jun 8, 2023 · N728FD · Airbus A300* · Wing, Control SurfacesSDR FDEA202306081083Support Web · crackedAFT MAIN DECK UTILITY AREA FLOOR STRUCTURE 1EA SUPPORT WEB FOUND CRACK AT FR79 PLUS 6" , Y-1610 REPLACED THE DAMAGE PART WITH NEW. I.A.W A300-600 SRM 51-72-10-001,PAGE.2Jun 8, 2023 · N728FD · Airbus A300* · Fuselage Miscellaneous StructureSDR FDEA202306081082Support Web · crackedAFT MAIN DECK UTILITY AREA FLOOR STRUCTURE 1EA SUPPORT WEB FOUND CRACK AT FR79 PLUS 6" , Y1610 REPLACED THE DAMAGE PART WITH NEW. I.A.W A300-600 SRM 51-72-10-001,PAGE.2Jun 8, 2023 · N728FD · Airbus A300* · Fuselage Miscellaneous StructureSDR FDEA202306081054Slat · unknownAIRCRAFT REPAIR ASSESSMENT : EXISTING FLUSH DOUBLER REPAIR FOUND ON RH WING #1 SLAT NOSE SKIN BTW RIB 19~JACK RIB 2 COMPLIED WITH ATTACHMENT B OF EO:E6-5100-7-5000 D7 PT1, TITLE:STRUCTURES-REPAIR CATALOG-A300/A310 REPAIR IDENTIFICATION & TRACKING REQUIREMEJun 8, 2023 · N728FD · Airbus A300* · Leading Edge DevicesSDR FDEA202306081053Flap · unknownAGING AIRCRAFT ASSESSMENT : EXISTING DOUBLER REPAIR FOUND ON RH I/B FLAP LWR SKIN BTW STGR 2.8~2.9,RIB 10~11 COMPLIED WITH ATTACHMENT B OF EO:E6-5100-7-5000 D7 PT1, TITLE:STRUCTURES-REPAIR CATALOG-A300/A310 REPAIR IDENTIFICATION & TRACKING REQUIREMENTS 14 Jun 8, 2023 · N728FD · Airbus A300* · Trailing Edge FlapsSDR FDEA202306081052Flap · unknownAIRCRAFT REPAIR ASSESSMENT : EXISTING DOUBLER REPAIR FOUND ON RH I/B FLAP UPR SKIN BTW STGR 2.1~2.2,RIB 5~9 COMPLIED WITH ATTACHMENT B OF EO:E6-5100-7-5000 D7 PT1, TITLE:STRUCTURES-REPAIR CATALOG-A300/A310 REPAIR IDENTIFICATION & TRACKING REQUIREMENTS 14 CJun 8, 2023 · N728FD · Airbus A300* · Trailing Edge FlapsSDR FDEA202306081051Flap · unknownAIRCRAFT REPAIR ASSESSMENT : EXISTING DOUBLER REPAIR FOUND ON RH I/B FLAP LWR SKIN BTW RIB 19~19A,T/E-12" COMPLIED WITH ATTACHMENT B OF EO:E6-5100-7-5000 D7 PT1, TITLE:STRUCTURES-REPAIR CATALOG-A300/A310 REPAIR IDENTIFICATION & TRACKING REQUIREMENTS 14 CFRJun 8, 2023 · N728FD · Airbus A300* · Trailing Edge FlapsSDR FDEA202306071046Rudder · corrodedRUDDER T/E APEX STRIP CORROSION AT STA.470 AREA PFM APEX STRIP REPAIR BY APEX STRIP WITH CONNECTION PLATE AND RIVETS I.A.W A300-600 SRM 55-41-12-201, PARA.16, P.237-239, FIG.208C, THIS IS CAT.B REPAIR I.A.W A300-600 SRI:55-41-12- 201, IIR:55-41-12-2-003-00,Jun 7, 2023 · N728FD · Airbus A300* · Rudder StructureSDR FDEA202306041191Rudder · damaged1EA WATER TRAPPED AREA(120MM*140MM) WAS FOUND AT RUDDER L/H T/E SCREW LINE NO.37 FASTENER AREA. ACCOMPLISHED THE CAT.B COMPOSITE REPAIR I.A.W FEDEX EA NO:T6-5540-T0374745 P1, SEQ NO:965, TITLE:STABILIZERS-RUDDER-LH RUDDER SHELL SCREW HOLE #37 WATER INGREJun 4, 2023 · N728FD · Airbus A300* · Rudder StructureSDR FDEA202306041079Rudder · damaged1EA WATER TRAPPED AREA(130MMX120MM) WAS FOUND AT RUDDER R/H T/E SCREW LINE NO.39 FASTENER AREA ACCOMPLISHED THE COMPOSITE REPAIR, THIS IS CAT.B REPAIR I.A.W A300-600 SRM 55-41-12-201, PARA.31, PAGE.313-319, FIG.222 & SRI:55-41-12-201, IIR:55-41-12-2-006-00Jun 4, 2023 · N728FD · Airbus A300* · Rudder StructureSDR FDEA202211222827Warning System · intermittentMDIS 728 52-70 7660 22NOV22 SAN OPEN U DURING PREFLIGHT L1 AND R 1 DOORS SLIDE RELEASE WARNING LIGHTS INOP - BUZZERS TEST O.K. MEL 22NOV22 04:52 SAN U RELEASED FOR SERVICE PER MEL : 52-73-01-01 CATEGORY : C EXPIRATION : 02DEC22 "MEL 52-73Nov 22, 2022 · N728FD · Airbus A300B4622R · Door Warning SystemSDR FDEA202211172803Floorboard · damagedRAMP REPORTED 2 HOLES IN MAIN DECK FLOOR BS 882 & 903,JUST INBD OF CA'S SIDE LONGITUDINAL RAIL. REMOVED FLOORBOARD AT 13L ON MAIN DECK. IAW SRM 53-10-20 REMOVED DAMAGE TO FLOORBOARD, FABRICATED A REPAIR AND PREPPED FLOORBOARD & REPAIR IAW SRM 53-10-20, PARNov 17, 2022 · N728FD · Airbus A300B4622R · Fuselage Floor PanelSDR FDEA202206151434Selector Valve · noneLANDING GEAR WOULD NOT EXTEND. 3 RED GEAR UNSAFE ON SYSTEM 1 AND 2. LANDING GEAR WAS GRAVITY EXTENDED. T/S IAW TSM 32-30, FIGURE 113. FOUND LANDING GEAR SELECTOR VALVE 3GA INOP. REMOVED AND REPLACED 3GA REF AMM 32-31-12-04. DURING T/S'ING FOUND LANDING Jun 15, 2022 · N728FD · Airbus A300* · Landing Gear Retraction/Extension SystemSDR FDEA202205261307Seat · unknownPDIS 728 25-10 7156 26MAY22 MEM OPEN U ON TAKEOFF ROLL, FO S SEAT CAME UNLOCKED AND SLID ALL THE WAY BACK AND OUTBOARD. ENROUTE DETERMINED THAT THE SEAT HAS A FORE/AFT LOCK POSITION THAT IS WEAK AND DOESN T FULLY LOCK WHICH ALLOWS SEAT TO MOMay 26, 2022 · N728FD · Airbus A300* · Flight Compartment EquipmentSDR FDEA202011202913Spar · crackedRT WING, BASIC WING STRUCTURE FRONT AND REAR SPAR BOTTOM BOOM INBOARD AND OUTBOARD OF RIB 9 INSPECTION, FOUND W HOLE WITH CRACK SIGNAL. COMPLIED WITH EA: 6-5710-T0358209 P1. TITLE: WINGS-BASIC WING STRUCTURE-RT WING REAR SPAR BOTTOM BOOM HOLE W/558 AT RIB 9 CNov 20, 2020 · N728FD · Airbus A300B4622R · Wing SparSDR FDEA202011182897Structure · crackedCENTER WING BOX, INSPECTION OF REAR SPAR AND BOTTOM PANEL AT JUNCTION OF FUSELAGE, LT SIDE, HOLE "C" FOUND CRACK SIGNAL. COMPLIED WITH EA: 6-5710-T0357880 P1. TITLE: WINGS-BASIC WING STRUCTURE-CRACK HOLE C AT FR 47 LT SIDE DURING SB57-6086 EMBODIMENT. REPNov 18, 2020 · N728FD · Airbus A300B4622R · Fuselage Main, StructureSDR FDEA202011182896Fitting · crackedLT WING ROOT FWD FACE FRAME 40 FWD FITTING STGR 32-33LT FOUND CRACK COMPLIED WITH EA: 6-5710-T0358132 P1. TITLE: WINGS-BASIC WING STRUCTURE-CRACK ON LT FR 40 FWD FITTING LOWER OUTBOARD RADIUS. REPAIRED THE LT WING ROOT FWD FACE- FRAME 40 FWD FITTING STGR 32Nov 18, 2020 · N728FD · Airbus A300B4622R · Fuselage, Wing Attach Fittings
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