R/R BOGIE SUPPORT PINS IAW AMM 27-51-43 REV 116. NO FURTHER DEFECTS NOTED
) - [SDR UIEA2026031600092](https://openairdocs.org/sdr/UIEA2026031600092.md): Support · cracked · Mar 15, 2026 · N476MC · Boeing 74747UF · Leading Edge Devices > DURING INSPECTION OF RH T/E FOREFLAP #6, FOUND INBD AND OTBD BOGIE SUPPORT PINS CRACKED. PLEASE REPLACE(R/R BOGIE SUPPORT PINS IAW AMM 27-51-43 REV 116. NO FURTHER DEFECTS NOTED
) - [SDR UIEA2026031600093](https://openairdocs.org/sdr/UIEA2026031600093.md): Support · cracked · Mar 15, 2026 · N476MC · Boeing 74747UF · Leading Edge Devices > DURING INSPECTION OF RH INBD T/E FOREFLAP #5, FOUND CRACKS IN THE HEAD OF BOGIE SUPPORT PIN. PLEASE REPLACE PIN(R/R BOGIE SUPPORT PIN IAW AMM 27-51-43 REV 116. NO FURTHER DEFECTS NOTED. - [SDR UIEA2026010300003](https://openairdocs.org/sdr/UIEA2026010300003.md): Plug · leaking · Jan 3, 2026 · N476MC · Boeing 74747UF · Turbine Engine Oil System > DIVERSION 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 CHECK - [SDR UIEA2025122001355](https://openairdocs.org/sdr/UIEA2025122001355.md): Angle · cracked · Dec 20, 2025 · N476MC · Boeing 74747UF · Fuselage Miscellaneous Structure > FOUND 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)(
WHEN ACCOMPLISHED REPEAT INSPECTION PER EA 4453A258 PART 2, FOUND CRACK ON CLIP AND R - [SDR UIEA2025092401243](https://openairdocs.org/sdr/UIEA2025092401243.md): Support Fitting · cracked · Sep 24, 2025 · N476MC · Boeing 74747UF · Fuselage, Landing Gear Attach Fittings > R/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. - [SDR KRDY2025061714786](https://openairdocs.org/sdr/KRDY2025061714786.md): Engine · fire · Jun 13, 2025 · N476MC · Boeing 74747UF · Engine (Turbine/Turboprop) > N476MC FLT 5Y 8208 AFTER T/O ENGINE # 1 WAS FIRE, SO CREW TAKE THE DECISION TO DIVERT TO GYE. PLS SEE ALSO MSR-14785. - [SDR UIEA2025061200758](https://openairdocs.org/sdr/UIEA2025061200758.md): Engine · failed · Jun 12, 2025 · N476MC · Boeing 74747UF · Engine (Turbine/Turboprop) > ENGINE 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. - [SDR KRDY2025061714785](https://openairdocs.org/sdr/KRDY2025061714785.md): Engine · fire · Jun 12, 2025 · N476MC · Boeing 74747UF · Engine (Turbine/Turboprop) > ACFT 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 ASSI - [SDR UIEA2025041300456](https://openairdocs.org/sdr/UIEA2025041300456.md): Indication Sys · false indication · Apr 13, 2025 · N476MC · Boeing 74747UF · Fuel Indicating System > NO FUEL QTY INDICATION ON MAIN TANK #2.(
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.
) - [SDR UIEA2025040900447](https://openairdocs.org/sdr/UIEA2025040900447.md): Skin · cracked · Apr 11, 2025 · N476MC · Boeing 74747UF · Fuselage Main, Plate/Skin > FUSELAGE - SEC46 SKIN EXTERIOR SURFACE STA1733-1735 S-41R AREA FOUND SKIN CRACKED WITH CORROSION.(JOB ACCOMPLISHED AS PER EN #1023-25 REV.0. FIRST AND SECOND STAGE APPROVAL (APPROVAL FOR STATIC STRENGTH AND INSPECTION THRESHOLD) THE INSPECTION THRESHOLD FOR - [SDR UIEA2025040900451](https://openairdocs.org/sdr/UIEA2025040900451.md): Floor Support · cracked · Apr 11, 2025 · N476MC · Boeing 74747UF · Fuselage Miscellaneous Structure > MAIN DECK - MAIN DECK FLOOR PANEL SUPPORT MOST O/B AT ABOUT STA 1100-1140 FOUND 2 EA FASTENER HOLE CRACK.(
JOB ACCOMPLISHED AS PER EN #3003-25 REV.0. NO FURTHER DEFECTS NOTED.
) - [SDR UIEA2024092000911](https://openairdocs.org/sdr/UIEA2024092000911.md): Acm · odor · Sep 20, 2024 · N476MC · Boeing 74747UF · Cabin Cooling System > 1. 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 LANDI - [SDR UIEA2024091100907](https://openairdocs.org/sdr/UIEA2024091100907.md): Power Supply · inoperative · Sep 12, 2024 · N476MC · Boeing 74747UF · Engine Starting System > DIVERTED, MULTIPLE FLIGHT CONTROL EICAS STATUS MESSAGES(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. - [SDR UIEA2024070600585](https://openairdocs.org/sdr/UIEA2024070600585.md): Elec Connector · dirty · Jul 6, 2024 · N476MC · Boeing 74747UF · Instrument System Wiring > BLEED 3 EICAS MESSAGE(
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.
) - [SDR UIEA2024032400211](https://openairdocs.org/sdr/UIEA2024032400211.md): Access Door · damaged · Mar 23, 2024 · N476MC · Boeing 74747UF · Nacelle/Pylon, Main Frame > ON POST FLT, FOUND #4 ENG INBD PYLON DAMAGED (SAIL BOAT DOOR)(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 LIMI - [SDR UIEA2024020900074](https://openairdocs.org/sdr/UIEA2024020900074.md): Indicator · false indication · Feb 10, 2024 · N476MC · Boeing 74747UF · Crew Oxygen System > AIR TURNBACK DUE TO CREW O2 QUANTITY LOW (SUSPECT LEAK)(
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.
) - [SDR UIEA2023031000242](https://openairdocs.org/sdr/UIEA2023031000242.md): None · none · Mar 8, 2023 · N476MC · Boeing 74747UF · Fuselage Structure (General) > DEVIATION - PERFORM STA 2598 BULKHEAD MODIFICATION FOUND DEVIATION AT DOUBLER(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 RE - [SDR UIEA2023031000241](https://openairdocs.org/sdr/UIEA2023031000241.md): None · none · Mar 8, 2023 · N476MC · Boeing 74747UF · Wing Structure > GOUGE - SKIN, RH WING INBD AILERON NOSE LE, WBL 502.5 - 514.25(
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 - [SDR UIEA2023031000240](https://openairdocs.org/sdr/UIEA2023031000240.md): None · none · Mar 8, 2023 · N476MC · Boeing 74747UF · Wing Structure > DISBOND - SKIN, #5 SPOILER UPPER SURFACE T/E FOUND DISBOND(
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 MINIMUM - [SDR UIEA2023031000239](https://openairdocs.org/sdr/UIEA2023031000239.md): None · none · Mar 8, 2023 · N476MC · Boeing 74747UF · Fuselage Structure (General) > FOUND EXISTING REPAIR DOUBLER ON OUTER SIDE SKIN OF FUSELAGE AT STA 2658 BETWEEN S-11L AND 13L(
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 COMPLETE - [SDR UIEA2023031000238](https://openairdocs.org/sdr/UIEA2023031000238.md): Fitting · none · Mar 8, 2023 · N476MC · Boeing 74747UF · Fuselage Structure (General) > CRACK ON FRONT SPAR INTERCOSTAL LUG FITTING AT STA 1000 LBL 11.33(
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-134 - [SDR UIEA2023031000237](https://openairdocs.org/sdr/UIEA2023031000237.md): None · none · Mar 8, 2023 · N476MC · Boeing 74747UF · Fuselage Structure (General) > WORN OUT - FOUND MAIN DECK SEAT TRACK WORN OUT AT STA 1100, LBL 11.33(
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 - [SDR UIEA2023030900235](https://openairdocs.org/sdr/UIEA2023030900235.md): Battery · none · Mar 8, 2023 · N476MC · Boeing 74747UF · Lighting System > FOUND EMERGENCY BATTERY (M5169) FUNCTION FAIL(
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 SATISFACT - [SDR UIEA2023030900234](https://openairdocs.org/sdr/UIEA2023030900234.md): Tube · none · Mar 8, 2023 · N476MC · Boeing 74747UF · Fuel Boost Pump > FOUND FUEL TUBE CHAFING WITH STRUCTURE IN NO.4 FUEL TANK PANEL 646AB(
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 8017 - [SDR UIEA2023030900233](https://openairdocs.org/sdr/UIEA2023030900233.md): None · none · Mar 8, 2023 · N476MC · Boeing 74747UF · Communications System > FOUND CVR BEACON BATTERY NEAR DUE AT N6 TIL:1EA(
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 SAT - [SDR UIEA2023030900232](https://openairdocs.org/sdr/UIEA2023030900232.md): None · none · Mar 8, 2023 · N476MC · Boeing 74747UF · Doors > EXISTING UNDOCUMENTED REPAIR ON OUTER SKIN OF AFT CARGO DOOR AT FWD LOWER CORNER BETWEEN STA 1810 AND STA 1823(
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 CHEC - [SDR UIEA2023030900231](https://openairdocs.org/sdr/UIEA2023030900231.md): None · none · Mar 8, 2023 · N476MC · Boeing 74747UF · Doors > FOUND AN EXISTING RPR DOUBLER AT FWD CGO DOOR AFT LOWER CORNER NEAR STA 662 S-38R(
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
CORROSION ON LWR FUSELAGE KEEL BEAM STIFFENER AT STA 1000 WL 90 LBL9(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 CON - [SDR UIEA2023030900229](https://openairdocs.org/sdr/UIEA2023030900229.md): None · none · Mar 8, 2023 · N476MC · Boeing 74747UF · Fuselage Structure (General) > M/D CGO FLOOR STRUCTURE CORROSION AT STA 1860 RBL 117(
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. CORROSION - FOUND CORROSION ON SKIN INNER SURFACE TOTAL 26EA WHEN PERFORM SB 747-53A2898(
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- - [SDR UIEA2023030900227](https://openairdocs.org/sdr/UIEA2023030900227.md): None · none · Mar 8, 2023 · N476MC · Boeing 74747UF · Fuselage Structure (General) > EXISTING UNDOCUMENTED REPAIR DOUBLER ON OUTER SKIN OF FUSELAGE AT STA 2598 AFT SIDE BETWEEN S-26R AND S-49R(
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. CON - [SDR UIEA2023030900226](https://openairdocs.org/sdr/UIEA2023030900226.md): None · none · Mar 8, 2023 · N476MC · Boeing 74747UF · Fuselage Structure (General) > EXISTING UNDOCUMENTED REPAIR DOUBLER ON SKIN OF FUSELAGE AT STA 2598 FWD SIDE BETWEEN S-26R AND S-42R(
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. CO - [SDR UIEA2023030900225](https://openairdocs.org/sdr/UIEA2023030900225.md): None · none · Mar 8, 2023 · N476MC · Boeing 74747UF · Fuselage Structure (General) > EXISTING UNDOCUMENTED REPAIR DOUBLER ON FUSELAGE SKIN AT STAÂ 1880 BETWEEN S-43L AND S-46L(
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 R - [SDR UIEA2023030900224](https://openairdocs.org/sdr/UIEA2023030900224.md): Shear Tie · none · Mar 8, 2023 · N476MC · Boeing 74747UF · Fuselage Structure (General) > CRACK ON FRONT SPAR SHEAR TIE AT STA 1000 RBL 57.50(
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. - [SDR UIEA2023030900223](https://openairdocs.org/sdr/UIEA2023030900223.md): Shear Tie · none · Mar 8, 2023 · N476MC · Boeing 74747UF · Fuselage Structure (General) > CRACK ON FRONT SPAR SHEAR TIE AT STA 1000 RBL 75.92(
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
) - [SDR UIEA2023030900222](https://openairdocs.org/sdr/UIEA2023030900222.md): Shear Tie · none · Mar 8, 2023 · N476MC · Boeing 74747UF · Fuselage Structure (General) > CRACK ON FRONT SPAR SHEAR TIE AT STA 1000 RBL 33.99(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. ORIG - [SDR UIEA2023030900221](https://openairdocs.org/sdr/UIEA2023030900221.md): None · none · Mar 8, 2023 · N476MC · Boeing 74747UF · Fuselage Internal Mounting Structure > CRACK DAMAGE ON FUSELAGE FRAME WEB AT STA 670 BETWEEN S-34R AND S-35R(
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
) - [SDR UIEA2023030900220](https://openairdocs.org/sdr/UIEA2023030900220.md): None · none · Mar 8, 2023 · N476MC · Boeing 74747UF · Fuselage Structure (General) > DEVIATION- DURING PERFORM SB 747-53A2443 REV2 HAVE SHORT EDGE MARGIN(1. ACCOMPLISHED EI NO: T2023A53M-132 REV1 AND 2. JOB COMPLETED AND CONDITION CHECK NORMAL
) - [SDR UIEA2023030900219](https://openairdocs.org/sdr/UIEA2023030900219.md): None · none · Mar 8, 2023 · N476MC · Boeing 74747UF · Fuselage Structure (General) > CRACK ON SIDE ANGLE OF NOSE WHEEL WELL TOP PANEL ASSY NEAR STA 300, LBL 30 WL 190(1. ACCOMPLISHED EI NO. T2023A53M-157 REV1 2. JOB COMPLETED AND CONDITION CHECK NORMAL
) - [SDR UIEA2023030900218](https://openairdocs.org/sdr/UIEA2023030900218.md): None · none · Mar 8, 2023 · N476MC · Boeing 74747UF · Fuselage Structure (General) > WORN OUT- FOUND MAIN DECK SEAT TRACK WORN OUT STA 1110 RBL 11.33(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 AND - [SDR UIEA2023030900217](https://openairdocs.org/sdr/UIEA2023030900217.md): None · none · Mar 8, 2023 · N476MC · Boeing 74747UF · Fuselage Floor Panel > CHAFING DAMAGE ON LH FUSELAGE SKIN EXTERNAL SURFACE AT STA 980 S-39L(
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/ - [SDR UIEA2023030900216](https://openairdocs.org/sdr/UIEA2023030900216.md): None · none · Mar 8, 2023 · N476MC · Boeing 74747UF · Fuselage Floor Panel > PUCH HOLE ON RH FUSELAGE SKIN BETWEEN STA 700 TO STA 720. 5-4R ~ 5-5R(
1. REPAIR FUSALAGE SKIN IAW SRM 53-00-01-2R-9 REPAIR 9 FIG 201 REV96 2. COND CHK NML AND JOB COMPLETED
) - [SDR UIEA2023030900215](https://openairdocs.org/sdr/UIEA2023030900215.md): None · none · Mar 8, 2023 · N476MC · Boeing 74747UF · Fuselage Structure (General) > CORROSION ON M/D FLOOR BEAM UPPER CAP NEAR STA 1580 LBL 77 ~ LBL 99(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
) - [SDR UIEA2023030900214](https://openairdocs.org/sdr/UIEA2023030900214.md): None · none · Mar 8, 2023 · N476MC · Boeing 74747UF · Fuselage Structure (General) > WORN OUT - FOUND MAIN DECK SEAT TRACK WORN OUT STA 1840 LBL 11.33(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. 65B3 - [SDR UIEA2023030900213](https://openairdocs.org/sdr/UIEA2023030900213.md): None · none · Mar 8, 2023 · N476MC · Boeing 74747UF · Fuselage Structure (General) > FOUND MAIN DECK SEAT TRACK WORN OUT STA 1600 LBL 11.33(
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. ACC - [SDR UIEA2023030900212](https://openairdocs.org/sdr/UIEA2023030900212.md): None · none · Mar 8, 2023 · N476MC · Boeing 74747UF · Fuselage Structure (General) > FOUND MAIN DECK SEAT TRACK WORN OUT STA 1746 RBL 11.33(
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. 65B382 - [SDR UIEA2023030900211](https://openairdocs.org/sdr/UIEA2023030900211.md): None · none · Mar 8, 2023 · N476MC · Boeing 74747UF · Fuselage Structure (General) > CORROSION - FOUND MAIN DECK SEAT TRACK CORROSION AT STA 1928 RBL 98.58(
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 65 - [SDR UIEA2023030900210](https://openairdocs.org/sdr/UIEA2023030900210.md): None · none · Mar 8, 2023 · N476MC · Boeing 74747UF · Fuselage Structure (General) > FND M/D CGO FLOOR SEAT TRACK CRACK AT STA 2238 RBL 75.92(
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: 65B Next page: https://openairdocs.org/aircraft/N476MC/reports.md?page=2 ## The whole list in SQL Runs in DuckDB 1.2 or later on the release's Parquet files over HTTPS: ```sql 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 ``` This list as a web page: https://openairdocs.org/aircraft/N476MC/reports --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.