N740FD

Service difficulty reports · 156

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 = 'N740FD' 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 FDEA202309221634Stringer Splice · crackedCOMPLY WITH EO 6-5310-7-5023 A PT2. REPLACED THE CRACKED SPLICE AT THE JUNCTION AT STGR18RH - FR47. TITLE: FUSELAGE - CENTER SECTION - INSPECTION OF STRINGER 18 LH/RH AT FRAME47, AIRBUS SB A300-53-6157 COMPLIED WITH EO 6-5310-7-5023 A PT2. TITLE: FUSELAGE Sep 22, 2023 · N740FD · Airbus A300* · Fuselage Main, Longeron/StringerSDR FDEA202309051547Skin · damagedEXISTING REPAIR ON FUSELAGE SKIN BETWEEN FR95 AND FR97, STGR3LH AND STGR5LH REQUIRES EVALUATION FOR CONFORMITY THE EXISTING REPAIR IN FUSELAGE SKIN BETWEEN FR95 AND FR97, STGR3LH AND STGR5LH WAS EVALUATED AND FOUND CONFORMITY WITH A300-600 SRM53-19-12 FIG.Sep 5, 2023 · N740FD · Airbus A300* · Fuselage Main, Plate/SkinSDR FDEA202309051546Skin · dentedEXISTING REPAIR ON FUSELAGE SKIN BETWEEN FR94 AND FR96, STGR4LH AND STGR6LH REQUIRES EVALUATION FOR CONFORMITY THE EXISTING REPAIR IN FUSELAGE SKIN BETWEEN FR94 AND FR96, STGR4LH AND STGR6LH WAS EVALUATED AND FOUND CONFORMITY WITH RAS/DATLS/0002239/2004 ISSep 5, 2023 · N740FD · Airbus A300* · Fuselage Main, Plate/SkinSDR FDEA202309011535Stringer · unknownEXISTING REPAIR ON FUSELAGE STRINGER AT STGR33 LH BETWEEN FR72 AND FR73 REQUIRES EVALUATION FOR CONFORMITY THE EXISTING REPAIR ON FUSELAGE STRINGER AT STGR33 LH BETWEEN FR72 AND FR73 WAS EVALUATED AND FOUND IN CONFORMITY WITH A300-600 SRM53-10-14 FIG.201. Sep 1, 2023 · N740FD · Airbus A300* · Fuselage Main, Longeron/StringerSDR FDEA202309011534Stringer · unknownEXISTING REPAIR ON FUSELAGE STRINGER AT STGR32 LH BETWEEN FR72 AND FR73 REQUIRES EVALUATION FOR CONFORMITY THE EXISTING REPAIR ON FUSELAGE STRINGER AT STGR32 LH BETWEEN FR72 AND FR73 WAS EVALUATED AND FOUND IN CONFORMITY WITH A300-600 SRM53-10-14 FIG.201. Sep 1, 2023 · N740FD · Airbus A300* · Fuselage Main, Longeron/StringerSDR FDEA202309011533Stringer · unknownEXISTING REPAIR ON FUSELAGE STRINGER AT STGR31 LH BETWEEN FR72 AND FR73 REQUIRES EVALUATION FOR CONFORMITY THE EXISTING REPAIR ON FUSELAGE STRINGER AT STGR31 LH BETWEEN FR72 AND FR73 WAS EVALUATED AND FOUND IN CONFORMITY WITH A300-600 SRM53-10-14 FIG.201. Sep 1, 2023 · N740FD · Airbus A300* · Fuselage Main, Longeron/StringerSDR FDEA202308271511Skin Panel · crackedLH WING - LEADING EDGE PANEL 523BB CUTOUT EDGE SKIN 1EA CRACK WAS FOUND COMPLIED WITH EA: 6-5710-T0375872 P1. TITLE: WINGS - BASIC WING STRUCTURE - LH WING BOTTOM SKIN PANEL NO.1 LEADING EDGE BETWEEN RIBS 8-9 - CRACK. REPAIRED THE LH WING LEADING EDGE PANEAug 27, 2023 · N740FD · Airbus A300* · Wing, Plate/SkinSDR FDEA202308271510Angle · crackedRIB8 INSPECTION OF CENTER SPAR SEALING ANGLE VERTICAL WEB ADJACENT TO PYLON REAR ATTACH FITTING, FASTENER HOLE 58 FOUND CRACK COMPLIED WITH EA: 6-5710-T0375850 P1. TITLE: WINGS - BASIC WING STRUCTURE - CRACK ON RH WING RIB 8 SEAL ANGLE - REPAIR. REPAIRED TAug 27, 2023 · N740FD · Airbus A300* · Wing SparSDR FDEA202308211471Spoiler · delaminatedLH WING #4 SPOILER CENTER I/B & O/B HINGE ARM OUTSIDE SURFACE AND CENTER I/B HINGE ARM LWR SURFACE FOUND DELAMINATION. SIZE: (1)44MM*25MM, DEPTH: 1.3MM (2)80MM*25MM, DEPTH: 1.14MM (3)25MM*20MM, DEPTH: 2.65MM COMPLIED WITH EA: 6-5750-T0359414 A P2. TITLE: WAug 21, 2023 · N740FD · Airbus A300* · SpoilersSDR FDEA202308211470Stringer · unknownEXISTING REPAIR ON FUSELAGE STRINGER AT STGR50 LH BETWEEN FR70 AND FR71 REQUIRES EVALUATION FOR CONFORMITY THE EXISTING REPAIR ON FUSELAGE STRINGER AT STGR50 LH BETWEEN FR70 AND FR71 WAS EVALUATED AND FOUND IN CONFORMITY WITH A300-600 SRM53-10-14 FIG.201. Aug 21, 2023 · N740FD · Airbus A300* · Fuselage Main, Longeron/StringerSDR FDEA202308211469Seat Track · unknownEXISTING REPAIR ON MAIN DECK COMPT SEAT TRACK AT FR66 - FR68, Y450 REQUIRES EVALUATION FOR CONFORMITY THE EXISTING REPAIR ON MAIN DECK COMPT SEAT TRACK AT FR66 - FR68, Y450 WAS EVALUATED AND FOUND IN CONFORMITY WITH A300-600 SRM53-10-16 FIG.208. EO: 6-510Aug 21, 2023 · N740FD · Airbus A300* · Fuselage, Seat/Cargo Attach FittingsSDR FDEA202308211468Seat Track · unknownEXISTING REPAIR ON MAIN DECK COMPT SEAT TRACK AT FR59 - FR60, Y1959 REQUIRES EVALUATION FOR CONFORMITY THE EXISTING REPAIR ON MAIN DECK COMPT SEAT TRACK AT FR59 - FR60, Y1959 WAS EVALUATED AND FOUND IN CONFORMITY WITH A300-600 SRM53-10-16 FIG.208. EO: 6-5Aug 21, 2023 · N740FD · Airbus A300* · Fuselage, Seat/Cargo Attach FittingsSDR FDEA202308151438Seat Track · unknownEXISTING REPAIR ON MAIN DECK COMPT SEAT TRACK AT FR54.3 - FR55, Y953 REQUIRES EVALUATION FOR CONFORMITY THE EXISTING REPAIR ON MAIN DECK COMPT SEAT TRACK AT FR54.3 - FR55, Y953 WAS EVALUATED AND FOUND IN CONFORMITY WITH A300-600 SRM53-10-16 FIG.208. EO: 6Aug 15, 2023 · N740FD · Airbus A300* · Fuselage, Seat/Cargo Attach FittingsSDR FDEA202308151437Seat Track · unknownEXISTING REPAIR ON MAIN DECK COMPT SEAT TRACK AT FR54.3 - FR55, Y450 REQUIRES EVALUATION FOR CONFORMITY THE EXISTING REPAIR ON MAIN DECK COMPT SEAT TRACK AT FR54.3 - FR55, Y450 WAS EVALUATED AND FOUND IN CONFORMITY WITH A300-600 SRM53-10-16 FIG.208. EO: 6Aug 15, 2023 · N740FD · Airbus A300* · Fuselage, Seat/Cargo Attach FittingsSDR FDEA202308151436Seat Track · unknownEXISTING REPAIR ON MAIN DECK COMPT SEAT TRACK AT FR61 - FR62, Y1456 REQUIRES EVALUATION FOR CONFORMITY THE EXISTING REPAIR ON MAIN DECK COMPT SEAT TRACK AT FR61 - FR62, Y1456 WAS EVALUATED AND FOUND IN CONFORMITY WITH A300-600 SRM53-10-16 FIG.208. EO: 6-5Aug 15, 2023 · N740FD · Airbus A300* · Fuselage, Seat/Cargo Attach FittingsSDR FDEA202308151435Seat Track · unknownEXISTING REPAIR ON MAIN DECK COMPT SEAT TRACK AT FR65 - FR68, -Y450 REQUIRES EVALUATION FOR CONFORMITY THE EXISTING REPAIR ON MAIN DECK COMPT SEAT TRACK AT FR65 - FR68, -Y450 WAS EVALUATED AND FOUND IN CONFORMITY WITH A300-600 SRM53-10-16 FIG.208. EO: 6-5Aug 15, 2023 · N740FD · Airbus A300* · Fuselage Main, StructureSDR FDEA202308151434Seat Track · unknownEXISTING REPAIR ON MAIN DECK COMPT SEAT TRACK AT FR61 - FR62, Y953 REQUIRES EVALUATION FOR CONFORMITY THE EXISTING REPAIR ON MAIN DECK COMPT SEAT TRACK AT FR61 - FR62, Y953 WAS EVALUATED AND FOUND IN CONFORMITY WITH A300-600 SRM53-10-16 FIG.208. EO: 6-510Aug 15, 2023 · N740FD · Airbus A300* · Fuselage Main, StructureSDR FDEA202308151432Stringer · unknownEXISTING REPAIR ON FUSELAGE STRINGER AT STGR27 LH BETWEEN FR77 AND FR78 REQUIRES EVALUATION FOR CONFORMITY THE EXISTING REPAIR ON FUSELAGE STRINGER AT STGR27 LH BETWEEN FR77 AND FR78 WAS EVALUATED AND FOUND IN CONFORMITY WITH A300-600 SRM53-10-14 FIG.201. Aug 15, 2023 · N740FD · Airbus A300* · Fuselage Main, StructureSDR FDEA202308151431Stringer · unknownEXISTING REPAIR ON FUSELAGE STRINGER AT STGR28 LH BETWEEN FR77 AND FR78 REQUIRES EVALUATION FOR CONFORMITY THE EXISTING REPAIR ON FUSELAGE STRINGER AT STGR28 LH BETWEEN FR77 AND FR78 WAS EVALUATED AND FOUND IN CONFORMITY WITH A300-600 SRM53-10-14 FIG.201. Aug 15, 2023 · N740FD · Airbus A300* · Fuselage Main, StructureSDR FDEA202308151430Stringer · unknownEXISTING REPAIR ON FUSELAGE STRINGER AT STGR43 RH BETWEEN FR71 AND FR72 REQUIRES EVALUATION FOR CONFORMITY THE EXISTING REPAIR ON FUSELAGE STRINGER AT STGR43 RH BETWEEN FR71 AND FR72 WAS EVALUATED AND FOUND IN CONFORMITY WITH A300-600 SRM53-10-14 FIG.201. Aug 15, 2023 · N740FD · Airbus A300* · Fuselage Main, StructureSDR FDEA202308151429Stringer · unknownEXISTING REPAIR ON FUSELAGE STRINGER AT STGR42 RH BETWEEN FR71 AND FR72 REQUIRES EVALUATION FOR CONFORMITY THE EXISTING REPAIR ON FUSELAGE STRINGER AT STGR42 RH BETWEEN FR71 AND FR72 WAS EVALUATED AND FOUND IN CONFORMITY WITH A300-600 SRM53-10-14 FIG.201. Aug 15, 2023 · N740FD · Airbus A300* · Fuselage Main, StructureSDR FDEA202308151428Stringer · unknownEXISTING REPAIR ON FUSELAGE STRINGER AT STGR41 RH BETWEEN FR71 AND FR72 REQUIRES EVALUATION FOR CONFORMITY THE EXISTING REPAIR ON FUSELAGE STRINGER AT STGR41 RH BETWEEN FR71 AND FR72 WAS EVALUATED AND FOUND IN CONFORMITY WITH A300-600 SRM53-10-14 FIG.201. Aug 15, 2023 · N740FD · Airbus A300* · Fuselage Main, StructureSDR FDEA202308151424Seat Track · unknownEXISTING REPAIR ON MAIN DECK COMPT SEAT TRACK AT FR65 - FR66, Y1456 REQUIRES EVALUATION FOR CONFORMITY THE EXISTING REPAIR ON MAIN DECK COMPT SEAT TRACK AT FR65 - FR66, Y1456 WAS EVALUATED AND FOUND IN CONFORMITY WITH A300-600 SRM53-10-16 FIG.208. EO: 6-5Aug 15, 2023 · N740FD · Airbus A300* · Fuselage Main, StructureSDR FDEA202207241792None · damagedMDIS 740 25-50 5864 24AUG21 IND FACT U REF WRI 25-50/5863 SEAT TRACK DAMAGED AT LOCK POSITION M1654 SHGN 24AUG21 09:41 IND U FOUND ADAPTER SEAT TRACK LOBES MISSING OIL 24AUG21 09:56 IND U NO RESTRICTION REF : SR30-53-003 SEAT TRAug 24, 2021 · N740FD · Airbus A300* · Fuselage Main, StructureSDR FDEA202103010519Pump · failedPDIS 740 29-11 5444 01MAR21 ANC OPEN U LOGPAGES:3142187 UPON TAKEOFF YELLOW HYD PRESSURE DROPPED TO 0 PSI FOR APPROX 30 SEC WITH CORRESPONDING LOW HYD PRESS ECAM, PRESSURE THEN RETURNED TO 3050 PSI. THIS HAPPENED 3 SEPERATE TIMES WITHIN A 2 MMar 1, 2021 · N740FD · Airbus A300B4622R · Hydraulic System, MainSDR FDEA202102110329Skin · damagedLH ELEVATOR UPR SKIN PANEL RIB4-RIB5 FOUND IMPACT DAMAGE REPAIRED THE LH ELEVATOR UPR SKIN PANEL RIB4-RIB5 IMPACT DAMAGE PER A300-600 SRM55-21-12-201-2 PARA.5.J . THIS IS CAT B REPAIR. TRACKING EA: 6-5520-T0359677 P1 RAISED AND COMPLETED. TITLE: STABILIZEFeb 11, 2021 · N740FD · Airbus A300B4622R · Elevator, Plate/SkinSDR FDEA202102050293Hinge Arm · delaminatedRH WING #3 SPOILER CENTER I/B HINGE ARM O/B SURFACE AND CENTER I/B & O/B HINGE ARM LWR SURFACE FOUND DELAMINATION. SIZE: (1)20MM*10MM, DEPTH: 1.6MM (2)20MM*15MM, DEPTH: 2.1MM (3)20MM*15MM, DEPTH: 2.4MM COMPLIED WITH EA: 6-5750-T0359409 P1. TITLE: WINGFeb 5, 2021 · N740FD · Airbus A300B4622R · SpoilersSDR FDEA202102020263Stringer · corrodedAFT CARGO STRINGER 46RH FOUND CORROSION BETWEEN FR61 AND FR62A COMPLIED WITH EA: 6-5310-150949 A P3. TITLE: FUSELAGE - MAINFRAME - CORROSION DAMAGE ON STRINGER 46R - REPAIR. REPAIRED THE AFT CARGO STRINGER 46RH CORROSION BETWEEN FR61 AND FR62A. THIS IS CATFeb 2, 2021 · N740FD · Airbus A300B4622R · Fuselage Main, Longeron/StringerSDR FDEA202101290230Skin · crackedRH WING - RIB8~RIB9, SUSPECTED CRACK ACROSS FASTENER HOLE ON LWR SKIN FWD EDGE APPROX 1.0 INCH IN LENGTH COMPLIED WITH EA: 6-5710-T0359505 P1. TITLE: WINGS - BASIC WING STRUCTURE - RH WING BOTTOM SKIN PANEL NO.1 LEADING EDGE BETWEEN RIBS8-9 - CRACK. REPAIJan 29, 2021 · N740FD · Airbus A300B4622R · Wing, Plate/SkinSDR FDEA2020081211857Hydraulic System · lowDURIG CRUISE OBSERVED GREE HYDRAULICS ON OVERHEAD AT RED DOT, COMFIRMED BY ECAM. SHORTY THERE AFTER RECEIVED GRN LO LEVEL WARNIING. RAN QRH INCLUDING MANUAL GEAR EXTENETION CREW REQUESTED TOW TO GATE. ONCE PARKED, INSPECTED A/C FUSEAGE AND FLIGHT SURFACESAug 11, 2020 · N740FD · Airbus A300B4622R · Hydraulic System, MainSDR FDEA202001170160Selector Valve · failedL/G RETRACTION FAILURE SYSTEM 1, DOORS OPENED BUT GEAR DIDNT MOVE. IF WIRING CHECKS ARE OK OK FROM 2GA TO 3GA, THE WIRING SHOULD ALSO BE MEGGED. COMPLETE IF MEG CHECKS ARE OK, R/R 2GA AND 3GA. COMPLETE IF REQUIRED R/R 2GAA AND 3GAA C/P'S . COMPLETE R&R LANDIJan 17, 2020 · N740FD · Airbus A300B4622R · Landing Gear SelectorSDR FDEA2019040860769Line · leakingAFTER 30 MINUTES OF FLIGHT AT FL 290 GOT ECAM WARNING FOR GREEN HYSD PRESS LOW. VERIFIED ON OVERHEAD PANEL AND RT ECAM PAGE THAT GREEN HYDRAULIC WAS Apr 6, 2019 · N740FD · Airbus A300B4622R · Hydraulic System, MainSDR FDEA2018081412013Switch · out of adjustAT APPROXIMATELY 10,000 FT DURING DEPARTURE, RECIEVED AN ECAM CAUTION FOR THE MAIN DECK DOOR NOT CLOSED. COMPLIED WITH RED TABS AND RETURNED FOR LANDING. NO ABNORMAL CABIN RATE OBSERVED. FOUND THE SWITCH 48WS NOT MAKING CONTACT. ADJUSTED THE SWITCH IAW AMAug 11, 2018 · N740FD · Airbus A300B4622R · Door Warning SystemSDR FDEA201807171770Seat Track · damagedSEAT TRACK SCALLOP BROKEN IN MAIN DECK CARGO BETWEEN FR66 AND FR67 Y1456 CUT OUT SEAT TRACK SECTION Y1456 FR66 TO FR67 IAW SRM 53-10-16 FIG 201. FABRICATED NEW SEAT TRACK SECTION, MATERIAL P/N A53274005-SFS-DAP. INSTALLED NEW SEAT TRACK SECTION FR66 TO FR67 Jul 17, 2018 · N740FD · Airbus A300B4622R · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201807171766Seat Track · gougedGOUGES ON SEAT TRACK SCALLOP IN MAIN DECK CARGO AT FR60 Y1456. BLENDED AREA IAW SRM 51-73-10. CHECKED LIMITS, MINIMUM MATERIAL REMOVED IS .260 AFTER REWORK .190 FOUND OUT OF LIMITS IAW SRM 53-10-16 FIG 101. FABRICATED NEW SEAT TRACK MATERIAL P/N# A53274005-Jul 17, 2018 · N740FD · Airbus A300B4622R · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201807161723Floor Panel · damagedCOURIER FLOOR PANEL 221LF GOUGED AND PUNCTURED. FABRICATED COURIER FLOOR PANEL 221LF ON T18/1354016 IAW SRZ-25-005 MAJOR REPAIR.Jul 16, 2018 · N740FD · Airbus A300B4622R · Fuselage Floor PanelSDR FDEA201807161721Floor Panel · damagedCOURIER FLOOR PANEL 222F GOUGED. FABRICATED COURIER FLOOR PANEL 222F ON T18/1354014 IAW SRZ-25-005 MAJOR REPAIR.Jul 16, 2018 · N740FD · Airbus A300B4622R · Fuselage Floor PanelSDR FDEA201807161720Floor Panel · damagedCOURIER FLOOR PANEL 222QF GOUGED AND PUNCTURED. FABRICATED COURIER FLOOR PANEL 222QF ON T18/1354018 IAW SRZ-25-005 MAJOR REPAIR.Jul 16, 2018 · N740FD · Airbus A300B4622R · Fuselage Floor PanelSDR FDEA2018071641714Floor Panel · crackedCRACK ON FLOOR PANEL 251WH IN MDC FABRICATED 251WH FLOOR PANEL ON T18/1354253IAW DWG SRZ 25-006 REV M. CLASSIFIED AS A CAT "A" MAJOR REPAIR.Jul 14, 2018 · N740FD · Airbus A300B4622R · Fuselage Floor PanelSDR FDEA201807131705Floor Panel · brokenMAIN DECK CARGO COMPT 242EK FLOOR PANEL BROKEN. FABRICATED 242EK FLOOR PANEL ON T18/1353526 IAW DWG SRZ-25-005 REV M. MAJOR REPAIR.Jul 13, 2018 · N740FD · Airbus A300B4622R · Fuselage Floor PanelSDR FDEA201807131704Floor Panel · brokenMAIN DECK CARGO COMPT 242LK FLOOR PANEL BROKEN. FABRICATED 242LK FLOOR PANEL ON T18/1353615 IAW DWG SRZ-25-005 REV M. MAJOR REPAIR.Jul 13, 2018 · N740FD · Airbus A300B4622R · Fuselage Floor PanelSDR FDEA201807131703Floor Panel · brokenMAIN DECK CARGO COMPT 231TG FLOOR PANEL BROKEN. FABRICATED 231TG FLOOR PANEL ON T18/1353527 IAW DWG SRZ-25-005 REV M. MAJOR REPAIR.Jul 13, 2018 · N740FD · Airbus A300B4622R · Fuselage Floor PanelSDR FDEA201807131702Floor Panel · brokenMAIN DECK CARGO COMPT 232HG FLOOR PANEL BROKEN. FABRICATED 232HG FLOOR PANEL ON T18/1353529 IAW DWG SRZ-25-005 REV M. MAJOR REPAIR.Jul 13, 2018 · N740FD · Airbus A300B4622R · Fuselage Floor PanelSDR FDEA201807131700Floor Panel · brokenMAIN DECK CARGO COMPT 231HG FLOOR PANEL BROKEN. FABRICATE 231HG FLOOR PANEL ON T18/1353530 IAW DWG SRZ-25-005 REV M. MAJOR REPAIR.Jul 13, 2018 · N740FD · Airbus A300B4622R · Fuselage Floor PanelSDR FDEA201806011373B-Nut · looseDURING CRUISE AT 310 FT, THE APU AUTO SHUTDOWN. FOLLOWED QRH, TRIED TO RESTART, AND THE APU WOULD NOT RESTART. FOUND APU OIL LOW AT BLOCK IN. APU ECB SHOWED LOW OIL PRESSURE FAULT. CLEARED FAULT, SERVICED THE APU OIL SYSTEM. FOUND SCAVANGE LINE B-NUT LJun 1, 2018 · N740FD · Airbus A300B4622R · APU Oil SystemSDR FDEA201609273373Indication Sys · faultyFUEL SYSTEM HAS MEL 28-42-02-02-A. AFTER T/O TRIM FUEL DASHES CAME AND WENT CAUSING FMMS ISSUES. FUEL LOW LEVEL LIGHTS THEN CAME ON AND OFF. REF MEL 28-42-02-02-A, STEP 5 DELETES FUEL QTY. INPUTS TO FMS, REF AMM 28-42-41-04, RT FUEL LOW LEVEL LIGHTS CHECK Sep 27, 2016 · N740FD · Airbus A300B4622R · Fuel Indicating SystemSDR FDEA201603170939Seat Track · corrodedMDCC, FRAME 15A, Y953, SEAT TRACK WITH INNER - GRANULAR CORROSION. REPLACED THE SERIOUS CORRODED SEAT TRACK IAW SRM 51-40-21. MAJOR REPAIR IAW GMM6-6-100.Mar 17, 2016 · N740FD · Airbus A300B4622R · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201603140920Web · crackedMDCC FRAME 47, Y953~ 1456, FLOOR WEB, CRACKED APPROX 0.5 INCH IN LENGTH. DRILL CRACK STOP HOLE & REMOVED CRACK BY CUT OUT OF WEB IAW SRM 53-15-15 FIG 201 SHT 2. MADE REPAIR DOUBLER IAW SRM 53-15-15 FIG 201 SHT 2. WET INSTALLED REPAIR DOUBLER IAW SRM 53-15-1Mar 14, 2016 · N740FD · Airbus A300B4622R · Fuselage Miscellaneous StructureSDR FDEA201603140919Web · crackedMDCC FRAME 47, -Y953~-Y1456, FLOOR WEB CRACKED, APPROX 0.5 INCH IN LENGTH. DRILL CRACK STOP HOLE & REMOVED CRACK BY CUT OUT OF WEB IAW SRM53-15-15 FIG 201 SHT 2. MADE REPAIR DOUBLER IAW SRM53-15-15 FIG 201 SHT 2. WET INSTALLED REPAIR DOUBLER IAW SRM53-15-15Mar 14, 2016 · N740FD · Airbus A300B4622R · Fuselage Miscellaneous StructureSDR FDEA201603120909Web · crackedMDCC FRAME 47, Y0~ Y450, FLOOR WEB CRACKED, APPROX 1.0 INCH IN LENGTH. FABRICATE NEW WEB IAW DWG A53832100. INSTALL NEW WEB IAW SRM 51-40-21. MAJOR REPAIR.Mar 12, 2016 · N740FD · Airbus A300B4622R · Fuselage Miscellaneous Structure
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