N408MC

Service difficulty reports · 206

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 = 'N408MC' 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 UIEA2026100400944Pcb · damagedEQUIPMENT COOLING EICAS CAUTION F270 ON CLIMB. CAPT ND BLANK FOR 30", FO PFD FLICKERED ON CLIMB. MESSAGE BLANKED THEN LOST CAPT ND AND FO ND WAS INTERMITTENT. R & R PRINTED CIRCUIT ASSY IAW AMM 21-58-05/401 & IPC 21-58-55-01B. OPS CHK OK; SCREENS ARE NO LONGOct 2, 2026 · N408MC · Boeing 74747UF · Air Conditioning System WiringSDR UIEA2026081200747Engine · faultedENGINE 2 OIL TEMP INFLIGHT. ENG 2 IFS. PERFORMED WINDMILLING INSPECTION & NO TROUBLE FOUND IAW AMM 72-00-00/601. PERFORMED ENG MAG CHIP INSPECTION & NO TROUBLE FOUND IAW AMM 79-00-00/601. R & R NR 2 ENG'S EEC & OPS CHECKED OK IAW AMM 73-21-15/401, AMM 79-34-0Aug 12, 2026 · N408MC · Boeing 74747UF · Engine (Turbine/Turboprop)SDR UIEA2026080700685Heat Exchanger · faultedENG 2 OIL TEMP EICAS MSG. FL 380 MAX OIL TEMP APPROX 194. ENG 2 SHUT DOWN. PERFORMED FIM 79-00, FT FIG 109. R & R FUEL/OIL HEAT EXCHANGER IAW AMM 79-21-01-404-014-J00, OPS CHECK & LEAK CHECKED GOOD. RUN ENG NR 2 AT DIFFERENT POWER SETTINGS AND OIL TEMP NORMAAug 7, 2026 · N408MC · Boeing 74747UF · Engine Oil CoolerSDR UIEA2026063000562Flap · damagedSUSPECTED HARD LANDING. PERFORMED PHASE 1A INSP PER AMM 05-51-05-222-081. DURING INSP, FOUND LH FLAP DAMAGE AT MIDDLE OF FOREFLAP LEVEL. SUBSEQUENT DAMAGE TO THE MID FLAP TRACK AND FUSELAGE OF LH TRAILING EDGE MIDFLAP.</P>)Jun 27, 2026 · N408MC · Boeing 74747UF · Trailing Edge FlapsSDR UIEA2025112901330Elec Connector · faultedON DEPARTURE AT 1000' AGL, HYD QTY LOW 4 EICAS ADVISORY MESSAGE, RAN NNC 13.29, SECURED NR 4 HYDRAULIC SYSTEM OFF. T/S PER WDM 29-33-12-2 TO PERFORM WIRING CHKS BTWN HYQUIM D7848CA TO #4 HYD SYS TRANSMITTER DT404, CHKS GOOD & INSULATION RESISTANCE CHCKS NORMNov 29, 2025 · N408MC · Boeing 74747UF · Hydraulic Power System WiringSDR UIEA2025083001150Solenoid · faultedENG 4 FUEL VALVE EICAS, ENG 4 FUEL VALVE STATUS, #4 ENG WOULD NOT SHUT DOWN UPON FUEL CONTROL SWITCHING OFF POSN. L13 CB FOUND IN OUT POSITION.(<P>R/R SOLENOID FUEL SOV PER AMM 73-21-20 & IPC 73-21-14-01 ITEM 67. PFM #4 ENG IDLE RUN CHK, NO LEAK FND.</P>)Aug 30, 2025 · N408MC · Boeing 74747UF · Fuel Controlling SystemSDR UIEA2025073001071Software · faultedL NAV WON'T ENGAGE. RELOADED ALL ASSOCIATED SOFTWARE INTO BOTH LT & RT FMC IAW AMM 34-61-00. ALL GROUND TEST PASSED. VERIFIED ALL SOFTWARE CORRECT CONFIG.Jul 30, 2025 · N408MC · Boeing 74747UF · Flight Management Computing Hardware SystemSDR UIEA2025060700734Starter · faultedENG 1 OIL PRESS EICAS MSG. ENG 1 OIL QTY DROPPED ON INITIAL CLIMB, PRESSURE DECREASED STEADILY UNTIL ENG 1 SHUT DOWN IN FLIGHT. ENG WINDMILL FOR 15 MINUTES.(<P>FOUND PACKING ON STARTER SHAFT CUT. REPLACED PACKING. INSPECTED MCD, FOUND SMALL QTY METAL SHAVING CJun 7, 2025 · N408MC · Boeing 74747UF · Engine StarterSDR UIEA2025052600695Panel · damagedDURING DESCENT, A/C EXPERIENCED HIGH FREQUENCY VIBRATIONS DURING SPEED BRAKE APPLICATIONS. ONCE LANDED IN HKG, STATION NOTICED THE #6 SPEED BRAKE PANEL ASSY DAMAGED / SEPERATED IN FLIGHT.(<P>R/R #6 SPOILER IAW AMM 27-62-01 AND OPERATIONAL CHECKS NORMAL</P>)May 26, 2025 · N408MC · Boeing 74747UF · Drag Control SystemSDR UIEA2025020200111Rib · crackedEMP HORIZONTAL STABILIZER TIP MOST O/B CLOSURE RIB WEB P/N: 65B03520-60 FOUND CRACKED.(<P>EMP HORIZONTAL STABILIZER TIP MOST O/B CLOSURE RIB WEB P/N: 65B03520-60 REPAIRED IAW SRM 55-10-09-2R-13 REPAIR 13 DETAIL III. NO FURTHER DEFECTS NOTED.</P>)Feb 6, 2025 · N408MC · Boeing 74747UF · Horizontal Stabilizer, Spar/RibSDR UIEA2025020200110Rib · crackedEMP HORIZONTAL STABILIZER TIP MOST O/B CLOSURE RIB LOWER CHORD P/N: 65B03520-54 FOUND CRACKED.(<P>EMP HORIZONTAL STABILIZER TIP MOST O/B CLOSURE RIB LOWER CHORD P/N: 65B03520-54 REPAIRED IAW SRM 55-10-09-2R-13 REPAIR 13 DETAIL V. NO FURTHER DEFECTS NOTED</P>)Feb 6, 2025 · N408MC · Boeing 74747UF · Horizontal Stabilizer, Spar/RibSDR UIEA2024052000396Doubler · crackedDOOR 1 EXTERIOR LOWER HINGE DOUBLER FOUND CRACK(<P>DOOR 1 LH EXTERIOR LOWER HINGE AREA DOUBLER P/N: 65B22350-7 REPLACED AND INSTALLED IAW SRM 51-40-02 AND BOEING 65B01836 SHEET 23 REV E. NO FURTHER DEFECTS NOTED</P>)May 23, 2024 · N408MC · Boeing 74747UF · Fuselage Main, StructureSDR UIEA2024012500023Skin · puncturedL/H I/B FLAP FORE FLAP UPPER SURFACE FOUND 1EA PUNCH HOLE DAMAGED AS MARK.(<P>L/H I/B FLAP FORE FLAP UPPER SURFACE PUNCH HOLE DAMAGE AREA. PERFORMED HOT BOND REPAIR AS PER SRM 51-70-07 PAR 5.A.(1) AND FIG 5. NO FURTHER DEFECTS NOTED</P>)Feb 5, 2024 · N408MC · Boeing 74747UF · Leading Edge DevicesSDR UIEA2024012500024Skin · damagedLHW I/B FORE FLAP LWR SURFACE FOUND DAMAGED AS MARK (156" FROM O/B TO I/B).(<P>LHW I/B FORE FLAP LWR SURFACE 156" FROM O/B TO I/B DAMAGED AREA. PERFORMED HOT BOND REPAIR AS PER SRM 51-70-07 PAR 5.A.(1) AND FIG 5. NO FURTHER DEFECTS NOTED</P>)Feb 5, 2024 · N408MC · Boeing 74747UF · Trailing Edge FlapsSDR UIEA2024012500025Skin · delaminatedL/H I/B FLAP MID FLAP MOST O/B LWR SURFACE FOUND DELAMINATION AS MARK (15" TO O/B EDGE).(<P>L/H I/B FLAP MID FLAP MOST O/B LOWER SURFACE (15" TO O/B EDGE) DELAMINATION AREA. PERFORMED HOT BOND REPAIR AS PER SRM 51-70-07 PAR 5.A.(1) AND FIG 5. NO FURTHER DEFECTFeb 5, 2024 · N408MC · Boeing 74747UF · Trailing Edge FlapsSDR UIEA2024012500026Skin · delaminatedLHW T/E I/B AFT FLAP L/E 66" FOUND DELAMINATION AS MARKED (COUNT FROM O/B).(<P>LHW T/E I/B AFT FLAP L/E 66" (COUNT FROM O/B) DELAMINATION AREA. PERFORMED HOT BOND REPAIR AS PER SRM 51-70-07 PAR 5.A.(1) AND FIG 5. NO FURTHER DEFECTS NOTED.</P>)Feb 5, 2024 · N408MC · Boeing 74747UF · Trailing Edge FlapsSDR UIEA2024012500028Skin · dentedLHW I/B AFT FLAP LWR T/E SURFACE AT MID AREA FOUND 1EA DENT AS MARK (155" FROM I/B TO O/B).(<P>LHW I/B AFT FLAP LWR T/E SURFACE 155" FROM I/B DENT AREA. PERFORMED HOT BOND REPAIR AS PER SRM 51-70-07 PAR 5.A.(1) AND FIG 5. NO FURTHER DEFECTS NOTED.</P>)Feb 5, 2024 · N408MC · Boeing 74747UF · Trailing Edge FlapsSDR UIEA2024012500029Skin · puncturedL/H I/B FLAP AFT FLAP T/E UPPER SURFACE FOUND 1EA PUNCH DAMAGED AS MARK.(<P>LH I/B FLAP AFT FLAP T/E UPPER SURFACE PUNCH DAMAGED AREA. PERFORMED HOT BOND REPAIR AS PER SRM 51-70-07 PAR 5.A.(1) AND FIG 5. NO FURTHER DEFECTS NOTED.</P>)Feb 5, 2024 · N408MC · Boeing 74747UF · Trailing Edge FlapsSDR UIEA2024012500030Skin · dentedLHW I/B AFT FLAP O/B LWR SURFACE FOUND 1EA DENT AS MARK (146" FROM I/B TO O/B).(<P>LHW I/B AFT FLAP O/B LWR SURFACE (146" FROM I/B TO O/B) DENT AREA. PERFORMED HOT BOND REPAIR AS PER SRM 51-70-07 PAR 5.A.(1) AND FIG 5. NO FURTHER DEFECTS NOTED.</P>)Feb 5, 2024 · N408MC · Boeing 74747UF · Trailing Edge FlapsSDR UIEA2024012500031Skin · delaminatedLHW T/E I/B AFT FLAP LOWER SURFACE T/E 130" FOUND DELAMINATION AS MARK. (COUNT FROM I/B TO O/B)(<P>LHW T/E I/B AFT FLAP LOWER SURFACE T/E 130" (COUNT FROM I/B TO O/B) DELAMINATION AREA. PERFORMED HOT BOND REPAIR AS PER SRM 51-70-07 PAR 5.A.(1) AND FIGURE 5. NOFeb 5, 2024 · N408MC · Boeing 74747UF · Trailing Edge FlapsSDR UIEA2024012500032Skin · delaminatedLHW T/E I/B FLAP FLAP LOWER SURFACE L/E 47" (COUNT FROM I/B) FOUND DELAMINATION AS MARKED.(<P>LHW T/E I/B AFT FLAP LOWER SURFACE L/E 47" (COUNT FROM I/B) DELAMINATION AREA. PERFORMED HOT BOND REPAIR AS PER SRM 51-70-07 PAR 5.A.(1) AND FIG 5. NO FURTHER DEFECTSFeb 5, 2024 · N408MC · Boeing 74747UF · Trailing Edge FlapsSDR UIEA2024012500033Panel · delaminatedL/H O/B FLAP MID FLAP O/B CARRIAGE ASSY COVER PANEL FOUND DELAMINATION AS MARK.(<P>L/H O/B FLAP MID O/B CARRIAGE ASSY COVER PANEL DELAMINATION AREA. PERFORMED HOT BOND REPAIR AS PER SRM 51-70-07 PAR 5.A.(1) AND FIG 5. NO FURTHER DEFECTS NOTED.</P>)Feb 5, 2024 · N408MC · Boeing 74747UF · Trailing Edge FlapsSDR UIEA2024012500034Skin · delaminatedRHW T/E I/B AFT FLAP LOWER SURFACE T/E 100" FOUND DELAMINATION AS MARKED (COUNT FROM I/B).(<P>RHW T/E I/B AFT FLAP LOWER SURFACE T/E 100" (COUNT FROM I/B) DELAMINATION AREA. PERFORMED REPAIR AS PER SRM 51-70-07 PAR 5.A. NO FURTHER DEFECTS NOTED.</P>)Feb 5, 2024 · N408MC · Boeing 74747UF · Trailing Edge FlapsSDR UIEA2024012500035Skin · delaminatedRHW T/E I/B AFT FLAP LOWER SURFACE T/E 122" FOUND DELAMINATION AS MARKED (COUNT FROM I/B).(<P>RHW T/E I/B AFT FLAP LOWER SURFACE T/E 122" (COUNT FROM I/B) DELAMINATION AREA. PERFORMED REPAIR AS PER SRM 51-70-07 PAR 5.A. NO FURTHER DEFECTS NOTED.</P>)Feb 5, 2024 · N408MC · Boeing 74747UF · Trailing Edge FlapsSDR UIEA2024012500036Skin · delaminatedRHW T/E I/B MID FLAP LOWER SURFACE L/E 124" FOUND DELAMINATION AS MARKED (COUNT FROM TO I/B).(<P>RHW T/E I/B MID FLAP LOWER SURFACE L/E 124" (COUNT FROM TO I/B) DELAMINATION AREA. PERFORMED REPAIR AS PER SRM 51-70-07 PAR 5.A. NO FURTHER DEFECTS NOTED.</P>)Feb 5, 2024 · N408MC · Boeing 74747UF · Trailing Edge FlapsSDR UIEA2024012500037Frame · crackedFX STA 1480 RH BULKHEAD FRAME WEB FOUND CRACK(<P>FRAME WEB REPAIRED AS PER SRM 53-40-08-2R-1 REPAIR 1 FIG 201. NO FURTHER DEFECTS NOTED.</P>)Feb 5, 2024 · N408MC · Boeing 74747UF · Fuselage Main, BulkheadSDR UIEA2024012500038Skin · delaminatedRHW T/E I/B AFT FLAP LOWER SURFACE T/E 48" FOUND DELAMINATION AS MARKED (COUNT FROM I/B).(<P>RHW T/E I/B AFT FLAP LOWER SURFACE T/E 48" (COUNT FROM I/B) DELAMINATION AREA. PERFORMED REPAIR AS PER SRM 51-70-07 PAR 5.A. NO FURTHER DEFECTS NOTED</P>)Feb 5, 2024 · N408MC · Boeing 74747UF · Trailing Edge FlapsSDR UIEA2024012500039Skin · delaminatedRHW T/E I/B MID FLAP L/E 2" (COUNT FROM I/B) FOUND DELAMINATION AS MARK.(<P>RHW T/E I/B MID FLAP L/E 2" (COUNT FROM I/B) DELAMINATION AREA PERFORMED REPAIR AS PER SRM 51-70-07 PAR 5.A. NO FURTHER DEFECTS NOTED.</P>)Feb 5, 2024 · N408MC · Boeing 74747UF · Trailing Edge FlapsSDR UIEA2024012500040Panel · delaminatedR/H I/B T/E FLAP MID FLAP O/B CARRIAGE ASSY UPPER COVER APNEL FOUND DELAMINATION AS MARK.(<P>R/H I/B T/E FLAP MID FLAP O/B CARRIAGE ASSY UPPER COVER PANEL DELAMINATION AREA. PERFORMED REPAIR AS PER SRM 51-70-07 PAR 5.A. NO FURTHER DEFECTS NOTED.</P>)Feb 5, 2024 · N408MC · Boeing 74747UF · Trailing Edge FlapsSDR UIEA2024012500041Skin · delaminatedRHW T/E I/B AFT FLAP LOWER SURFACE T/E 155" FOUND DELAMINATION AS MARKED (COUNT FROM I/B).(<P>RHW T/E I/B AFT FLAP LOWER SURFACE T/E 155" (COUNT FROM I/B) DELAMINATION AREA. PERFORMED REPAIR AS PER SRM 51-70-07 PAR 5.A. NO FURTHER DEFECTS NOTED.</P>)Feb 5, 2024 · N408MC · Boeing 74747UF · Trailing Edge FlapsSDR UIEA2024012500042Fairing · delaminatedRHW O/B FWD FLAP FWD FAIRING 48" FOUND DELAMINATION AS MARKED (COUNT FROM O/B).(<P>RHW O/B FWD FLAP FWD FAIRING 48" (COUNT FROM O/B) DELAMINATION AREA. PERFORMED REPAIR AS PER SRM 51-70-07 PAR 5.A. NO FURTHER DEFECTS NOTED.</P>)Feb 5, 2024 · N408MC · Boeing 74747UF · Trailing Edge FlapsSDR UIEA2024012800046Seat Track · damagedM/D STA 1890 RBL 11 SEAT TRACK CTR GUIDE STOP HOLE FOUND ELONGATED(<P>SEAT TRACK REPAIRED AS PER SRM 53-00-52-2R-12 REPAIR 12. NO FURTHER DEFECTS NOTED.</P>)Feb 5, 2024 · N408MC · Boeing 74747UF · Fuselage, Seat/Cargo Attach FittingsSDR UIEA2024012800047Tension Tie · crackedLH BS 840 UPPER DECK TENSION TIE 1EA CRACK FOUND AT AFT CHANNEL(<P>TENSION TIE REPAIRED AS PER SRM 53-20-30-2R-1 REPAIR. NO FURTHER DEFECTS NOTED.</P>)Feb 5, 2024 · N408MC · Boeing 74747UF · Fuselage Miscellaneous StructureSDR UIEA2024012800048Tension Tie · crackedLH BS 880 UPPER DECK TENSION TIE 1EA CRACK FOUND AT AFT CHANNEL(<P>TENSION TIE REPAIRED AS PER SRM 53-20-30-2R-1 REPAIR 1. NO FURTHER DEFECTS NOTED.</P>)Feb 5, 2024 · N408MC · Boeing 74747UF · Fuselage Miscellaneous StructureSDR UIEA2024012800049Tension Tie · crackedRH BS 840 UPPER DECK TENSION TIE 1EA CRACK FOUND AT 1 O/C POSITION OF THE AFT CHANNEL(<P>TENSION TIE REPAIRED AS PER SRM 53-20-30-2R-1 REPAIR 1. NO FURTHER DEFECTS NOTED.</P>)Feb 5, 2024 · N408MC · Boeing 74747UF · Fuselage Miscellaneous StructureSDR UIEA2024012800050Channel · crackedLH BS 900 UPPER DECK TENSION TIE AFT CHANNEL 1EA HOLE FOUND CRACK(<P>TENSION TIE REPAIRED AS PER SRM 53-20-30-2R-1 REPAIR 1. NO FURTHER DEFECTS NOTED.</P>)Feb 5, 2024 · N408MC · Boeing 74747UF · Fuselage Miscellaneous StructureSDR UIEA2024012800051Skin · corrodedFUSELAGE SKIN AT LOWER LOBE CIRCUMFERENTIAL SPLICE LOCATION STA 1715 S45R FOUND CORROSION APPROX 1" X 1"(<P>SKIN REPAIRED AS PER SRM 53-00-01-2R-1 REPAIR 1 FIG 201 DETAIL I. NO FURTHER DEFECTS NOTED</P>)Feb 5, 2024 · N408MC · Boeing 74747UF · Fuselage Main, Plate/SkinSDR UIEA2024012900052Skin · corrodedLHW I/B AFT FLAP FOUND BULGE UP(<P>PERFORMED REPAIR AT BULGE UP AREA IAW RI-57-53-16705. NO FURTHER DEFECTS NOTED.</P>)Feb 5, 2024 · N408MC · Boeing 74747UF · Trailing Edge FlapsSDR UIEA2024013000053Skin · dentedLHW O/B T/E AFT FLAP O/B PANEL UPPER SURFACE FOUND SEVERAL AREA DENT MARK AS MARKED.(<P>METAL HOT BOND REPAIR CARRIED OUT AS PER RI-57-51-16699 REV.A. NO FURTHER DEFECTS NOTED.</P>)Feb 5, 2024 · N408MC · Boeing 74747UF · Trailing Edge FlapsSDR UIEA2024013000054Skin · dentedRHW O/B T/E AFT FLAP O/B PANEL UPPER SURFACE FOUND SEVERAL AREA DENT MARK AS MARKED.(<P>METAL HOT BOND REPAIR CARRIED OUT AS PER RI-57-51-16700 REV.A. NO FURTHER DEFECTS NOTED.</P>)Feb 5, 2024 · N408MC · Boeing 74747UF · Trailing Edge FlapsSDR UIEA2024013100055Frame · crackedLH BS 2598 B/HEAD INNER CHORD 1EA HOLE FOUND CRACK AT 3ND LAYER (COUNTING FROM AFT) AT 5 O'CLOCK POSITION APPROX 0.050" IN DEPTH(<P>INNER CHORD CRACK AREA REPAIRED AS PER RI-53-73-16683 REV.A. NO FURTHER DEFECTS NOTED</P>)Feb 5, 2024 · N408MC · Boeing 74747UF · Fuselage Main, BulkheadSDR UIEA2024013100057Longeron · crackedFUS - 2EA CRACKS WERE FOUND ON RH BS 1480-1540 STR 32-33 LONGERON EXTENSION FITTING(<P>LONGERON EXTENSION FITTING REPLACEMENT CARRIED OUT AS PER ATLAS AIR EO 4453A818 R19 PART 4. NO FURTHER DEFECTS NOTED</P>)Feb 5, 2024 · N408MC · Boeing 74747UF · Fuselage Main, StructureSDR UIEA2024013100058Panel · crackedM/D STA 1720 L/H DADO PNL FOUND CRACK(<P>DADO PNL CRACK AREA REPAIRED AS PER RI-25-21-16675 REV.A. NO FURTHER DEFECTS NOTED.</P>)Feb 5, 2024 · N408MC · Boeing 74747UF · Fuselage Miscellaneous StructureSDR UIEA2024020100059Ladder · crackedM/D CREW LADDER I/B SIDE #7 & 10 STEP FOUND CRACK(<P>#7 AND #10 STEP CRACK AREA REPAIRED AS PER RI-25-50-16667 REV.A. NO FURTHER DEFECTS NOTED.</P>)Feb 5, 2024 · N408MC · Boeing 74747UF · Fuselage Main, StructureSDR UIEA2024020100060Skin · corrodedFX R/H AIRCON BAY STA 1000-1003 CENTER SECTION LOWER SURFACE CORR. AT RBL 15" - RBL 29"(<P>SKIN CORROSION AREA REPAIRED AS PER RI-57-10-16703 REV.A. NO FURTHER DEFECTS NOTED.</P>)Feb 5, 2024 · N408MC · Boeing 74747UF · Fuselage Main, Plate/SkinSDR UIEA2024020100061Bracket · damagedAPU COMPT L/H FRAME STA 2674 WIRE BRACKET AND ATT FRAME RIVET HOLES FOUND ELONGATED(<P>WIRE BRACKET REPLACED AS PER SRM 51-10-02, NEW BRACKET HOLES TRANSFERRED AS PER SRM 51-40-05, NEW BRACKET INSTALLED AS PER SRM 51-40-02 AND FRAME REPAIRED AS PER SRM 53-80-0Feb 5, 2024 · N408MC · Boeing 74747UF · Fuselage Miscellaneous StructureSDR UIEA2024020100062Skin · crackedFX - FUSELAGE SKIN STA 1680 STR 41R FOUND CORR CRACK(<P>SKIN REPAIRED AS PER RI-53-61-16685 REV.A. NO FURTHER DEFECTS NOTED.</P>)Feb 5, 2024 · N408MC · Boeing 74747UF · Fuselage Main, Plate/SkinSDR UIEA2024020100063Support · crackedLHW L/E CAVITY HOLES 1300 FIXED PNL SUPPORT CRACK (AFT OF #4 V/C FLAP)(<P>SUPPORT BEAM REPAIRED AS PER RI-57-41-16684 REV.A. NO FURTHER DEFECTS NOTED</P>)Feb 5, 2024 · N408MC · Boeing 74747UF · Wing Miscellaneous StructureSDR UIEA2024020100064Closeout Panel · crackedM/D STA 1241 LBL 77-99 CLOSURE PNL FOUND CRACK.(<P>CLOSURE PNL REPLACED AS PER SRM 51-10-02, NEW PNL HOLES TRANSFERRED AS PER SRM 51-40-05 AND NEW PNL INSTALLED AS PER SRM 51-40-02. NO FURTHER DEFECTS NOTED.</P>)Feb 5, 2024 · N408MC · Boeing 74747UF · Fuselage Main, StructureSDR UIEA2024020100065None · noneACCOMPLISHMENT OF EO 4453A301 REV.11, WE FOUND ONE EACH FREEZE PLUG INSTALLED ON UPPER DECK R/H STA 880 FRAME AREA.(<P>FRAME REPAIRED AS PER RI NO. RI-53-20-16702 REV.A. NO FURTHER DEFECTS NOTED.</P>)Feb 5, 2024 · N408MC · Boeing 74747UF · Standard Practices/Structures
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