N476MC

Service difficulty reports · 227

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 = 'N476MC' 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 UIEA2026070200567Adc · faultedLOSS OF RT ADC, AND RT AOA IN FLIGHT WITH C/B TRIPPED. R & R RIGHT ADC IAW AMM 34-12-01-401, REV 116 & IPC 34-12-01-01B, REC 92. IAW FIM TASK 34-12 TASK 869 IAW CMC MSG 34653. PERFORMED GRD TEST OF RIGHT ADC IAW AMM 34-12-00/501. ALL TEST PASSED.Jul 2, 2026 · N476MC · Boeing 74747UF · Air Data ComputerSDR UIEA2026031600091Support · crackedDURING INSPECTION OF RH T/E FOREFLAP #6, FOUND INBD & OTBD BOGIE SUPPORT PINS CRACKED. PLEASE REPLACE(<P>R/R BOGIE SUPPORT PINS IAW AMM 27-51-43 REV 116. NO FURTHER DEFECTS NOTED</P>)Mar 15, 2026 · N476MC · Boeing 74747UF · Leading Edge DevicesSDR UIEA2026031600092Support · crackedDURING INSPECTION OF RH T/E FOREFLAP #6, FOUND INBD AND OTBD BOGIE SUPPORT PINS CRACKED. PLEASE REPLACE(<P>R/R BOGIE SUPPORT PINS IAW AMM 27-51-43 REV 116. NO FURTHER DEFECTS NOTED</P>)Mar 15, 2026 · N476MC · Boeing 74747UF · Leading Edge DevicesSDR UIEA2026031600093Support · crackedDURING INSPECTION OF RH INBD T/E FOREFLAP #5, FOUND CRACKS IN THE HEAD OF BOGIE SUPPORT PIN. PLEASE REPLACE PIN(<P>R/R BOGIE SUPPORT PIN IAW AMM 27-51-43 REV 116. NO FURTHER DEFECTS NOTED.Mar 15, 2026 · N476MC · Boeing 74747UF · Leading Edge DevicesSDR UIEA2026010300003Plug · leakingDIVERSION ENGINE 3 OIL QUANTITY LOSS. INSPECTED #3 ENG AND FOUND OIL LEAKING FROM #3 IDG. DEACTIVATION BLANKING PLATE, REMOVED BLANKING PLATE AND FOUND DRIVE SEAL PLUG MISSING & INSTALLED DRIVE SEAL PLUG PER MEL 24-11-01A. RAN ENG IAW AMM 71-00-00, LEAK CHECKJan 3, 2026 · N476MC · Boeing 74747UF · Turbine Engine Oil SystemSDR UIEA2025122001355Angle · crackedFOUND 1 INCH LENGTH CRACK ON RH LONGERON BOX FRAME (PN: 65B15001-80) REPAIRED PER EA 4453A258 PART 1, REQUIRE TO PERFORM REPEAT INSPECTION PER EA 4453A258 PART 2. (14340)(<P>WHEN ACCOMPLISHED REPEAT INSPECTION PER EA 4453A258 PART 2, FOUND CRACK ON CLIP AND RDec 20, 2025 · N476MC · Boeing 74747UF · Fuselage Miscellaneous StructureSDR UIEA2025092401243Support Fitting · crackedR/H BODY LANDING GEAR WHEEL WELL AREA SUPPORT FITTING CRACK (STA 1372). PERFORMED TIME LIMITED REPAIR PER EA-4453A258 PART 1. NO FURTHER DEFECTS NOTED.Sep 24, 2025 · N476MC · Boeing 74747UF · Fuselage, Landing Gear Attach FittingsSDR KRDY2025061714786Engine · fireN476MC FLT 5Y 8208 AFTER T/O ENGINE # 1 WAS FIRE, SO CREW TAKE THE DECISION TO DIVERT TO GYE. PLS SEE ALSO MSR-14785.Jun 13, 2025 · N476MC · Boeing 74747UF · Engine (Turbine/Turboprop)SDR UIEA2025061200758Engine · failedENGINE 1 DUAL FIRE LOOP INDICATION CONFIRMED BY VISUAL OF FLAME COMING FROM INTAKE AND SMOKE OUT EXHAUST AFTER DISCHARGING BOTH FIRE BOTTLES. C/W ENGINE CHANGE PER TASK CARD 71-099-02-01. NO FURTHER DEFECTS NOTED. ORIGINAL SUBMISSION DATE; 6/16/2025.Jun 12, 2025 · N476MC · Boeing 74747UF · Engine (Turbine/Turboprop)SDR KRDY2025061714785Engine · fireACFT N476MC FLT 5Y8208 B747C DEPARTED FROM UIO, AFTER DEPART ENG #1 WAS FIRED SO CREW TOOK THE DECISION TO DIVERT TO GYE. ACFT LAND ON GYE, TOWED TO POSITION 13. A RIDING MECHANIC FROM ATLAS IS IN CHARGE OF THE TECHNICAL RELEASE AND WE PROVIDE MECHANIC ASSIJun 12, 2025 · N476MC · Boeing 74747UF · Engine (Turbine/Turboprop)SDR UIEA2025041300456Indication Sys · false indicationNO FUEL QTY INDICATION ON MAIN TANK #2.(<P>CONFIRMED NO FUEL LEAKS, DRIP STICK READING ACCOMPLISHED, AND DDG 28-41-01 APPLIED. TRANSFER TO DMI 229181 PER MEL 28-41-01 CAT C DUE DATE 24APR25.</P>)Apr 13, 2025 · N476MC · Boeing 74747UF · Fuel Indicating SystemSDR UIEA2025040900447Skin · crackedFUSELAGE - SEC46 SKIN EXTERIOR SURFACE STA1733-1735 S-41R AREA FOUND SKIN CRACKED WITH CORROSION.(<P>JOB ACCOMPLISHED AS PER EN #1023-25 REV.0. FIRST AND SECOND STAGE APPROVAL (APPROVAL FOR STATIC STRENGTH AND INSPECTION THRESHOLD) THE INSPECTION THRESHOLD FORApr 11, 2025 · N476MC · Boeing 74747UF · Fuselage Main, Plate/SkinSDR UIEA2025040900451Floor Support · crackedMAIN DECK - MAIN DECK FLOOR PANEL SUPPORT MOST O/B AT ABOUT STA 1100-1140 FOUND 2 EA FASTENER HOLE CRACK.(<P>JOB ACCOMPLISHED AS PER EN #3003-25 REV.0. NO FURTHER DEFECTS NOTED.</P>)Apr 11, 2025 · N476MC · Boeing 74747UF · Fuselage Miscellaneous StructureSDR UIEA2024092000911Acm · odor1. DURING APPROACH, LOUD HOWL OR GROAN NOISE FROM BELOW COCKPIT. AFTER LANDING TURNED OFF PACK 2, NOISE STOPPED. 2. PACK 2 EICAS MSG, PACK WILL NOT RESET. 3. TURNING FINAL APPROACH APPROX 3000 FT, BURNING SMELL COMING THROUGH A/C SYSTEM, LESSENED THROUGH LANDISep 20, 2024 · N476MC · Boeing 74747UF · Cabin Cooling SystemSDR UIEA2024091100907Power Supply · inoperativeDIVERTED, MULTIPLE FLIGHT CONTROL EICAS STATUS MESSAGES(<P>R/R FCE POWER SUPPLY 1R (M7360) IAW AMM 27-09-00 & AIPC 27-09-04-01A. OPS CHECK GOOD. NIL EXISTING FAULT MSG NOTED. AC-1 DIST C/B STAYED IN SET POSITION.Sep 12, 2024 · N476MC · Boeing 74747UF · Engine Starting SystemSDR UIEA2024070600585Elec Connector · dirtyBLEED 3 EICAS MESSAGE(<P>FOUND #2 WIRE ON HPSOV WAS READING 12 MEGA OHMS. REMOVED CANNON PLUG AND CLEANED, RESEATED CANNON PLUG AND FOUND RESISTANCE CHECK TO BE .2 MEGA OHMS WHICH IS NORMAL PER FIM 36-11 TASK 803. NO FURTHER DEFECTS NOTED.</P>)Jul 6, 2024 · N476MC · Boeing 74747UF · Instrument System WiringSDR UIEA2024032400211Access Door · damagedON POST FLT, FOUND #4 ENG INBD PYLON DAMAGED (SAIL BOAT DOOR)(<P>TEMP REPAIR TO #4 ENG PYLON PANEL COMPLETED PEREA 4454A0080 & SRM 51-70-19-0G-0. SCHEDULED PERMANENT REPAIR UPON AIRCRAFT RETURN TO MIA FROM SCL PRIOR TO THE ACCUMULATION OF 2 F/C AFTER TIME LIMIMar 23, 2024 · N476MC · Boeing 74747UF · Nacelle/Pylon, Main FrameSDR UIEA2024020900074Indicator · false indicationAIR TURNBACK DUE TO CREW O2 QUANTITY LOW (SUSPECT LEAK)(<P>PERFORMED LEAK CHECK FOR OXY BOTTLES / LINES / ALL MASKS, NO LEAK FOUND. R/R CREW OXYGEN VOLTAGE AVERAGING UNIT AND OPS / IND CHECK GOOD PER AMM 35-41-12.</P>)Feb 10, 2024 · N476MC · Boeing 74747UF · Crew Oxygen SystemSDR UIEA2023031000242None · noneDEVIATION - PERFORM STA 2598 BULKHEAD MODIFICATION FOUND DEVIATION AT DOUBLER(<P>1. PERFORMED EI T2023A53M-310 REV 0 SEQUENCE A. 2. PERFORMED EI T2023A53M-310 REV 1 SEQUENCE B. 3. PERFORMED EI T2023A53M-384 REV 0 SEQUENCE A. 4. ACCOMPLISHED EI T2023A53M-310 REMar 8, 2023 · N476MC · Boeing 74747UF · Fuselage Structure (General)SDR UIEA2023031000241None · noneGOUGE - SKIN, RH WING INBD AILERON NOSE LE, WBL 502.5 - 514.25(<P>1. PERFORM REPAIR OF GOUGE DAMAGE FOUND ON RH WING INBD AILERON NOSE LE, WBL 502.5 - 514.25. PLEASE REFER TO THE JOB CARD ATTACHING SHEETS FOR DETAILED REWORKING INFORMATION. 2. CONDITION CHECK Mar 8, 2023 · N476MC · Boeing 74747UF · Wing StructureSDR UIEA2023031000240None · noneDISBOND - SKIN, #5 SPOILER UPPER SURFACE T/E FOUND DISBOND(<P>1. CUT OUT THE DISBOND AND CLEAN MEASURE THE CUTOUT (L = 5.5", W = 3", 32.5" FROM OUTBD EDGE AT T/E) INSTALL THE REPAIR CORE WITH COMPOUND, CURED AT 250 DEGREE FAHRENHEIT FOR 90 MINUTES WITH MINIMUMMar 8, 2023 · N476MC · Boeing 74747UF · Wing StructureSDR UIEA2023031000239None · noneFOUND EXISTING REPAIR DOUBLER ON OUTER SIDE SKIN OF FUSELAGE AT STA 2658 BETWEEN S-11L AND 13L(<P>1. REMOVE THE EXISTING DOUBLER IAW SRM 51-40-02-0G-0 REV 96. 2. PERFORM EI T2023A53M-272 REV 0 SEQUENCE A. 3. ACCOMPLISHED EI T2023A53M-272 REV 1. 4. JOB COMPLETEMar 8, 2023 · N476MC · Boeing 74747UF · Fuselage Structure (General)SDR UIEA2023031000238Fitting · noneCRACK ON FRONT SPAR INTERCOSTAL LUG FITTING AT STA 1000 LBL 11.33(<P>1. REMOVED DAMAGE PARTS IAW SRM 51-40-02-0G-0 REV 96. 2. INSTALL NEW PARTS IAW SRM 51-40-02-0G-0 REV 96 AND EO 4453C024 REV 3 AND EI T2023A53M-134 SEQUENCE B. 3. ACCOMPLISHED EI T2023A53M-134Mar 8, 2023 · N476MC · Boeing 74747UF · Fuselage Structure (General)SDR UIEA2023031000237None · noneWORN OUT - FOUND MAIN DECK SEAT TRACK WORN OUT AT STA 1100, LBL 11.33(<P>REMOVED THE AFFECTED FASTENER IAW SRM 57-00-02-0G-0 REV 96. 2. PERFORM REPAIR IAW EO T2023A53M-191 SEQUENCE A AND SEQUENCE B REV 1. 3 INSTALLED FASTENERS IAW SRM 51-44-02-0G-0 REV 96 AND Mar 8, 2023 · N476MC · Boeing 74747UF · Fuselage Structure (General)SDR UIEA2023030900235Battery · noneFOUND EMERGENCY BATTERY (M5169) FUNCTION FAIL(<P>1. IAW AMM 33-51-04-902-001-001 REV107 REPLACED EMEREGENCY LIGHT POWER SUPPLY (M5169) BATTERY 2. IAW AMM 33-51-04-902-001-001 REV 107 PERFORMED POWER SUPPLY BATTERY INSTALLATION TEST AND THE RESULT WAS SATISFACTMar 8, 2023 · N476MC · Boeing 74747UF · Lighting SystemSDR UIEA2023030900234Tube · noneFOUND FUEL TUBE CHAFING WITH STRUCTURE IN NO.4 FUEL TANK PANEL 646AB(<P>1. IAW AMM 28-22-07-004-072-001 REV106 AND AMM 28-22-07-404-080-001 REV106 RPL TUBE IN NO.4 FUEL TANK AND PFM LEAK TEST RESULT WAS NO LEAK FOUND. 2. COORDINATE WITH THE CLOSE PNL CARD 8017Mar 8, 2023 · N476MC · Boeing 74747UF · Fuel Boost PumpSDR UIEA2023030900233None · noneFOUND CVR BEACON BATTERY NEAR DUE AT N6 TIL:1EA(<P>1. IAW AMM 23-71-003-002-001 & 23-71-03-402-015 REV106 REPLACED CVR UNDERWATER LOCATOR BEACON 2. IAW AMM 23-71-03-712-114 REV106 PERFORMED CVR UNDERWATER LOCATOR BEACON INSTALLATION TEST AND THE RESULT WAS SATMar 8, 2023 · N476MC · Boeing 74747UF · Communications SystemSDR UIEA2023030900232None · noneEXISTING UNDOCUMENTED REPAIR ON OUTER SKIN OF AFT CARGO DOOR AT FWD LOWER CORNER BETWEEN STA 1810 AND STA 1823(<P>1. REMOVE EXISTING DOUBLER IAW SRM 51-40-02 RV 96 2. INSTALL REPAIR DOUBLER IAW SRM 51-40-02 REV96 AND EI NO. T2023A52M-121 REV1 3. CONDITION CHECMar 8, 2023 · N476MC · Boeing 74747UF · DoorsSDR UIEA2023030900231None · noneFOUND AN EXISTING RPR DOUBLER AT FWD CGO DOOR AFT LOWER CORNER NEAR STA 662 S-38R(<P>1. REMOVE EXISTING DOUBLER IAW SRM 51-40-02 REV96 2. INSTALL REPAIR DOUBLER IAW SRM 51-40-02 REV96 AND EI NO: T2023A52M-122 REV1 3. CONDITION CHECK NORMAL AND JOB COMPLETED</PMar 8, 2023 · N476MC · Boeing 74747UF · DoorsSDR UIEA2023030900230Stiffener · noneCORROSION ON LWR FUSELAGE KEEL BEAM STIFFENER AT STA 1000 WL 90 LBL9(<P>1. REMOVE DAMAGE PARTS IAW SRM 51-40-02-OG-0 REV96 2. INSTALL NEW PARTS IAW SRM 51-40-02-0G-0 REV96 AND DWG NO: 65B01828 SH34 REV-A AND DWG NO: 65B01828 SH44 REV-C 3. JOB COMPLETED AND CONMar 8, 2023 · N476MC · Boeing 74747UF · Fuselage Structure (General)SDR UIEA2023030900229None · noneM/D CGO FLOOR STRUCTURE CORROSION AT STA 1860 RBL 117(<P>1. BLENDED OUT THE DAMAGE AREA IAW SRM 51-10-02-0G-0 REV96 2. PREFORM NDT INSPECT REFER JOB CARD ATTACHING SHEET NO: 0373340 3. ACCOMPLISHED EI NO: T2023A53M-328 REV1 4. JOB COMPLETED AND COND CHK NML.</Mar 8, 2023 · N476MC · Boeing 74747UF · Fuselage Structure (General)SDR UIEA2023030900228None · noneCORROSION - FOUND CORROSION ON SKIN INNER SURFACE TOTAL 26EA WHEN PERFORM SB 747-53A2898(<P>1. REMOVED THE AFFECTED FASTENERS IAW SRM 51-40-02-0G-0 REV96 2. PERFORMED EI NO T2023A53-135 REV0 3. PERFORMED EI NO T2023A53M-135 REV 1 4. PERFORMED EI NO. T2023A53M-Mar 8, 2023 · N476MC · Boeing 74747UF · Fuselage, Wing Attach FittingsSDR UIEA2023030900227None · noneEXISTING UNDOCUMENTED REPAIR DOUBLER ON OUTER SKIN OF FUSELAGE AT STA 2598 AFT SIDE BETWEEN S-26R AND S-49R(<P>1. REMOVED EXISTING DOUBLER IAW SRM 51-40-02-0G-0 REV96 2. REPAIR THE SKIN DOUBLER IAW EI NO. T2023A53M-436 REV1 AND DWG NO. 65B02707 SH2 REV1 3. CONMar 8, 2023 · N476MC · Boeing 74747UF · Fuselage Structure (General)SDR UIEA2023030900226None · noneEXISTING UNDOCUMENTED REPAIR DOUBLER ON SKIN OF FUSELAGE AT STA 2598 FWD SIDE BETWEEN S-26R AND S-42R(<P>1. REMOVED EXISTING DOUBLER IAW SRM 51-40-02-0G-0 REV96 2. ACCOMPLISHED THE SKIN REPAIR IAW EI NO. T2023A53M-433 REV1 AND DWG NO. 65B02698 SH13 REV A 3. COMar 8, 2023 · N476MC · Boeing 74747UF · Fuselage Structure (General)SDR UIEA2023030900225None · noneEXISTING UNDOCUMENTED REPAIR DOUBLER ON FUSELAGE SKIN AT STA  1880 BETWEEN S-43L AND S-46L(<P>1. REMOVE EXISTING REPAIR DOUBLER IAW SRM 51-40-02-0G-0 REV96 2. REPAIR SKIN IAW EI NO: T2023A53M-494 REV1 3. ACCOMPLISHED THE REPAIR AREA IAW EI NO: T2023A53M-494 RMar 8, 2023 · N476MC · Boeing 74747UF · Fuselage Structure (General)SDR UIEA2023030900224Shear Tie · noneCRACK ON FRONT SPAR SHEAR TIE AT STA 1000 RBL 57.50(<P>1. REMOVE DAMAGE PARTS IAW SRM 51-40-02-0G-0 REV96 2. INSTALL NEW PARTS IAW SRM 51-40-02-0G-0 REV96 AND EO NO. 4453C024 REV3 AND EI NO: T2023A53M-134 SEQUENCE B 3. ACCOMPLISHED EI NO: T2023A53M-134 REV2 4.Mar 8, 2023 · N476MC · Boeing 74747UF · Fuselage Structure (General)SDR UIEA2023030900223Shear Tie · noneCRACK ON FRONT SPAR SHEAR TIE AT STA 1000 RBL 75.92(<P>1. REMOVED DAMAGED PARTS IAW SRM 51-40-02-OG-0 REV96 2. INSTALL NEW PARTS IAW SRM 51-40-02-0G-0 REV96 AND EO NO: 4453C024 REV3 3. JOB COMPLETED</P>)Mar 8, 2023 · N476MC · Boeing 74747UF · Fuselage Structure (General)SDR UIEA2023030900222Shear Tie · noneCRACK ON FRONT SPAR SHEAR TIE AT STA 1000 RBL 33.99(<P>1. REMOVED DAMAGE PARTS IAW SRM 51-40-02-0G-0 REV96 2. INSTALL NEW PARTS IAW SRM 51-40-02-0G-0 AND EO NO: 4453C024 REV3 AND EI NO: T2023A53M-134 SEQUENCE B 3. ACCOMPLISHED EI NO: T2023A53M-134 REV2 4. ORIGMar 8, 2023 · N476MC · Boeing 74747UF · Fuselage Structure (General)SDR UIEA2023030900221None · noneCRACK DAMAGE ON FUSELAGE FRAME WEB AT STA 670 BETWEEN S-34R AND S-35R(<P>1.ACCOMPLISED REPAIR IAW SRM 51-40-02-0G-0 REV 96 AND EI NO T2023A53M-103 REV0 SEQUENCE A 2. ACCOMPLISHED EI NO: T2023A53M-103 REV1 3. JOB COMPLETED AND COND CHK NML</P>)Mar 8, 2023 · N476MC · Boeing 74747UF · Fuselage Internal Mounting StructureSDR UIEA2023030900220None · noneDEVIATION- DURING PERFORM SB 747-53A2443 REV2 HAVE SHORT EDGE MARGIN(<P>1. ACCOMPLISHED EI NO: T2023A53M-132 REV1 AND 2. JOB COMPLETED AND CONDITION CHECK NORMAL</P>)Mar 8, 2023 · N476MC · Boeing 74747UF · Fuselage Structure (General)SDR UIEA2023030900219None · noneCRACK ON SIDE ANGLE OF NOSE WHEEL WELL TOP PANEL ASSY NEAR STA 300, LBL 30 WL 190(<P>1. ACCOMPLISHED EI NO. T2023A53M-157 REV1 2. JOB COMPLETED AND CONDITION CHECK NORMAL</P>)Mar 8, 2023 · N476MC · Boeing 74747UF · Fuselage Structure (General)SDR UIEA2023030900218None · noneWORN OUT- FOUND MAIN DECK SEAT TRACK WORN OUT STA 1110 RBL 11.33(<P>1. REMOVED THE AFFECTED FASTENER IAW SRM 51-40-02-0G-0 REV96 2. REPAIRED DAMAGE AREA IAW EI T2023A53M-130 SEQUENCE A AND SEQUENCE B REV 1 3. INSTALLED FASTENERS IAW SRM 51-40-02-0G-0 REV96 ANDMar 8, 2023 · N476MC · Boeing 74747UF · Fuselage Structure (General)SDR UIEA2023030900217None · noneCHAFING DAMAGE ON LH FUSELAGE SKIN EXTERNAL SURFACE AT STA 980 S-39L(<P>1. REMOVE THE AFFECTED FASTENERS IAW SRM 51-40-02-0G-0 REV 96 2. ACCOMPLISHED EI NO. T2023A53M-109 REV2 AND INSTALL FASTENERS IAW SRM 51-40-02-0G-0 REV96 AND DWG NO. 140U0999 SH 28 REV- 3/Mar 8, 2023 · N476MC · Boeing 74747UF · Fuselage Floor PanelSDR UIEA2023030900216None · nonePUCH HOLE ON RH FUSELAGE SKIN BETWEEN STA 700 TO STA 720. 5-4R ~ 5-5R(<P>1. REPAIR FUSALAGE SKIN IAW SRM 53-00-01-2R-9 REPAIR 9 FIG 201 REV96 2. COND CHK NML AND JOB COMPLETED</P>)Mar 8, 2023 · N476MC · Boeing 74747UF · Fuselage Floor PanelSDR UIEA2023030900215None · noneCORROSION ON M/D FLOOR BEAM UPPER CAP NEAR STA 1580 LBL 77 ~ LBL 99(<P>1. ACCOMPLISHED JOB IAW EI NO T2023A53N-170 SEQUENCE A REV0 AND DWG 65B338079 SH9 REV- 2. ACCOMPLISHED FINAL EI NO. T2023A53M-170 REV1 3. CONDITION CHECK NORMAL AND JOB COMPLETED</P>)Mar 8, 2023 · N476MC · Boeing 74747UF · Fuselage Structure (General)SDR UIEA2023030900214None · noneWORN OUT - FOUND MAIN DECK SEAT TRACK WORN OUT STA 1840 LBL 11.33(<P>1. REMOVED THE AFFECTED FASTENER IAW SRM 51-40-02-0G-0 REV96 2. REPAIR DAMAGE AREA IAW EI NO. T2023A53M-270 SEQUENCE A REV0 3. INSTALLED FASTENERS IAW SRM 51-40-02-0G-0 REV96 AND DWG NO. 65B3Mar 8, 2023 · N476MC · Boeing 74747UF · Fuselage Structure (General)SDR UIEA2023030900213None · noneFOUND MAIN DECK SEAT TRACK WORN OUT STA 1600 LBL 11.33(<P>1. REMOVED THE AFFECTED FASTENER IAW SRM 51-40-02 REV96 2. REPAIR DAMAGE AREA IAW EI NO. T2023A53M-269 SEQUENCE A REV 0 3. FASTENER INSTALLED IAW SRM 51-40-02 REV96 AND DWG NO. 65B38253 SH48 REV- 4. ACCMar 8, 2023 · N476MC · Boeing 74747UF · Fuselage Structure (General)SDR UIEA2023030900212None · noneFOUND MAIN DECK SEAT TRACK WORN OUT STA 1746 RBL 11.33(<P>1. REMOVED THE AFFECTED FASTENER I.A.W SRM 51-40-02 REV 96 2. REPAIRED DAMAGE AREA I.A.W SRM 53-00-52-2R-12 REPAIR 12 FIG 201 REV96 3. INSTALLED NEW FASTENER I.A.W SRM 51-40-02 REV 96 AND DWG NO. 65B382Mar 8, 2023 · N476MC · Boeing 74747UF · Fuselage Structure (General)SDR UIEA2023030900211None · noneCORROSION - FOUND MAIN DECK SEAT TRACK CORROSION AT STA 1928 RBL 98.58(<P>1. REMOVED THE AFFECTED FASTERNER I.A.W SRM 51-40-02 REV-96 2. REPAIRED DAMAGE AREA I.A.W EI NO. T2023A53M-147 SEQUENCE A REV 0. 3. INSTALLED FASTENERS I.A.W SRM 51-40-02 REV9 AND DWG 65Mar 8, 2023 · N476MC · Boeing 74747UF · Fuselage Structure (General)SDR UIEA2023030900210None · noneFND M/D CGO FLOOR SEAT TRACK CRACK AT STA 2238 RBL 75.92(<P>1. REMOVED AFFECTED FASTENER IAW SRM 51-40-02-0G-0 REV96 2. REPAIRED DAMAGE AREA IAW SRM 53-00-52-2R-13 REPAIR 13 FIG 201 REV 96 3. INSTALLED NEW FASTENERS IAW SRM 51-40-02-0G-0 REV 96 AND DWG NO: 65BMar 8, 2023 · N476MC · Boeing 74747UF · Fuselage Structure (General)
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