# Service difficulty reports: N408MC A list on [N408MC](https://openairdocs.org/aircraft/N408MC.md). Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first. Page 1 of 5 · 206 reports - [SDR UIEA2026100400944](https://openairdocs.org/sdr/UIEA2026100400944.md): Pcb · damaged · Oct 2, 2026 · N408MC · Boeing 74747UF · Air Conditioning System Wiring > EQUIPMENT 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 LONG - [SDR UIEA2026081200747](https://openairdocs.org/sdr/UIEA2026081200747.md): Engine · faulted · Aug 12, 2026 · N408MC · Boeing 74747UF · Engine (Turbine/Turboprop) > ENGINE 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 79-34-0 - [SDR UIEA2026080700685](https://openairdocs.org/sdr/UIEA2026080700685.md): Heat Exchanger · faulted · Aug 7, 2026 · N408MC · Boeing 74747UF · Engine Oil Cooler > ENG 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 NORMA - [SDR UIEA2026063000562](https://openairdocs.org/sdr/UIEA2026063000562.md): Flap · damaged · Jun 27, 2026 · N408MC · Boeing 74747UF · Trailing Edge Flaps > SUSPECTED 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.

) - [SDR UIEA2025112901330](https://openairdocs.org/sdr/UIEA2025112901330.md): Elec Connector · faulted · Nov 29, 2025 · N408MC · Boeing 74747UF · Hydraulic Power System Wiring > ON 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 NORM - [SDR UIEA2025083001150](https://openairdocs.org/sdr/UIEA2025083001150.md): Solenoid · faulted · Aug 30, 2025 · N408MC · Boeing 74747UF · Fuel Controlling System > ENG 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.(

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.

) - [SDR UIEA2025073001071](https://openairdocs.org/sdr/UIEA2025073001071.md): Software · faulted · Jul 30, 2025 · N408MC · Boeing 74747UF · Flight Management Computing Hardware System > L 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. - [SDR UIEA2025060700734](https://openairdocs.org/sdr/UIEA2025060700734.md): Starter · faulted · Jun 7, 2025 · N408MC · Boeing 74747UF · Engine Starter > ENG 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.(

FOUND PACKING ON STARTER SHAFT CUT. REPLACED PACKING. INSPECTED MCD, FOUND SMALL QTY METAL SHAVING C - [SDR UIEA2025052600695](https://openairdocs.org/sdr/UIEA2025052600695.md): Panel · damaged · May 26, 2025 · N408MC · Boeing 74747UF · Drag Control System > DURING 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.(

R/R #6 SPOILER IAW AMM 27-62-01 AND OPERATIONAL CHECKS NORMAL

) - [SDR UIEA2025020200111](https://openairdocs.org/sdr/UIEA2025020200111.md): Rib · cracked · Feb 6, 2025 · N408MC · Boeing 74747UF · Horizontal Stabilizer, Spar/Rib > EMP HORIZONTAL STABILIZER TIP MOST O/B CLOSURE RIB WEB P/N: 65B03520-60 FOUND CRACKED.(

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.

) - [SDR UIEA2025020200110](https://openairdocs.org/sdr/UIEA2025020200110.md): Rib · cracked · Feb 6, 2025 · N408MC · Boeing 74747UF · Horizontal Stabilizer, Spar/Rib > EMP HORIZONTAL STABILIZER TIP MOST O/B CLOSURE RIB LOWER CHORD P/N: 65B03520-54 FOUND CRACKED.(

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

) - [SDR UIEA2024052000396](https://openairdocs.org/sdr/UIEA2024052000396.md): Doubler · cracked · May 23, 2024 · N408MC · Boeing 74747UF · Fuselage Main, Structure > DOOR 1 EXTERIOR LOWER HINGE DOUBLER FOUND CRACK(

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

) - [SDR UIEA2024012500023](https://openairdocs.org/sdr/UIEA2024012500023.md): Skin · punctured · Feb 5, 2024 · N408MC · Boeing 74747UF · Leading Edge Devices > L/H I/B FLAP FORE FLAP UPPER SURFACE FOUND 1EA PUNCH HOLE DAMAGED AS MARK.(

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

) - [SDR UIEA2024012500024](https://openairdocs.org/sdr/UIEA2024012500024.md): Skin · damaged · Feb 5, 2024 · N408MC · Boeing 74747UF · Trailing Edge Flaps > LHW I/B FORE FLAP LWR SURFACE FOUND DAMAGED AS MARK (156" FROM O/B TO I/B).(

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

) - [SDR UIEA2024012500025](https://openairdocs.org/sdr/UIEA2024012500025.md): Skin · delaminated · Feb 5, 2024 · N408MC · Boeing 74747UF · Trailing Edge Flaps > L/H I/B FLAP MID FLAP MOST O/B LWR SURFACE FOUND DELAMINATION AS MARK (15" TO O/B EDGE).(

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 DEFECT - [SDR UIEA2024012500026](https://openairdocs.org/sdr/UIEA2024012500026.md): Skin · delaminated · Feb 5, 2024 · N408MC · Boeing 74747UF · Trailing Edge Flaps > LHW T/E I/B AFT FLAP L/E 66" FOUND DELAMINATION AS MARKED (COUNT FROM O/B).(

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.

) - [SDR UIEA2024012500028](https://openairdocs.org/sdr/UIEA2024012500028.md): Skin · dented · Feb 5, 2024 · N408MC · Boeing 74747UF · Trailing Edge Flaps > LHW I/B AFT FLAP LWR T/E SURFACE AT MID AREA FOUND 1EA DENT AS MARK (155" FROM I/B TO O/B).(

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.

) - [SDR UIEA2024012500029](https://openairdocs.org/sdr/UIEA2024012500029.md): Skin · punctured · Feb 5, 2024 · N408MC · Boeing 74747UF · Trailing Edge Flaps > L/H I/B FLAP AFT FLAP T/E UPPER SURFACE FOUND 1EA PUNCH DAMAGED AS MARK.(

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.

) - [SDR UIEA2024012500030](https://openairdocs.org/sdr/UIEA2024012500030.md): Skin · dented · Feb 5, 2024 · N408MC · Boeing 74747UF · Trailing Edge Flaps > LHW I/B AFT FLAP O/B LWR SURFACE FOUND 1EA DENT AS MARK (146" FROM I/B TO O/B).(

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.

) - [SDR UIEA2024012500031](https://openairdocs.org/sdr/UIEA2024012500031.md): Skin · delaminated · Feb 5, 2024 · N408MC · Boeing 74747UF · Trailing Edge Flaps > LHW T/E I/B AFT FLAP LOWER SURFACE T/E 130" FOUND DELAMINATION AS MARK. (COUNT FROM I/B TO O/B)(

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. NO - [SDR UIEA2024012500032](https://openairdocs.org/sdr/UIEA2024012500032.md): Skin · delaminated · Feb 5, 2024 · N408MC · Boeing 74747UF · Trailing Edge Flaps > LHW T/E I/B FLAP FLAP LOWER SURFACE L/E 47" (COUNT FROM I/B) FOUND DELAMINATION AS MARKED.(

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 DEFECTS - [SDR UIEA2024012500033](https://openairdocs.org/sdr/UIEA2024012500033.md): Panel · delaminated · Feb 5, 2024 · N408MC · Boeing 74747UF · Trailing Edge Flaps > L/H O/B FLAP MID FLAP O/B CARRIAGE ASSY COVER PANEL FOUND DELAMINATION AS MARK.(

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.

) - [SDR UIEA2024012500034](https://openairdocs.org/sdr/UIEA2024012500034.md): Skin · delaminated · Feb 5, 2024 · N408MC · Boeing 74747UF · Trailing Edge Flaps > RHW T/E I/B AFT FLAP LOWER SURFACE T/E 100" FOUND DELAMINATION AS MARKED (COUNT FROM I/B).(

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.

) - [SDR UIEA2024012500035](https://openairdocs.org/sdr/UIEA2024012500035.md): Skin · delaminated · Feb 5, 2024 · N408MC · Boeing 74747UF · Trailing Edge Flaps > RHW T/E I/B AFT FLAP LOWER SURFACE T/E 122" FOUND DELAMINATION AS MARKED (COUNT FROM I/B).(

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.

) - [SDR UIEA2024012500036](https://openairdocs.org/sdr/UIEA2024012500036.md): Skin · delaminated · Feb 5, 2024 · N408MC · Boeing 74747UF · Trailing Edge Flaps > RHW T/E I/B MID FLAP LOWER SURFACE L/E 124" FOUND DELAMINATION AS MARKED (COUNT FROM TO I/B).(

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.

) - [SDR UIEA2024012500037](https://openairdocs.org/sdr/UIEA2024012500037.md): Frame · cracked · Feb 5, 2024 · N408MC · Boeing 74747UF · Fuselage Main, Bulkhead > FX STA 1480 RH BULKHEAD FRAME WEB FOUND CRACK(

FRAME WEB REPAIRED AS PER SRM 53-40-08-2R-1 REPAIR 1 FIG 201. NO FURTHER DEFECTS NOTED.

) - [SDR UIEA2024012500038](https://openairdocs.org/sdr/UIEA2024012500038.md): Skin · delaminated · Feb 5, 2024 · N408MC · Boeing 74747UF · Trailing Edge Flaps > RHW T/E I/B AFT FLAP LOWER SURFACE T/E 48" FOUND DELAMINATION AS MARKED (COUNT FROM I/B).(

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

) - [SDR UIEA2024012500039](https://openairdocs.org/sdr/UIEA2024012500039.md): Skin · delaminated · Feb 5, 2024 · N408MC · Boeing 74747UF · Trailing Edge Flaps > RHW T/E I/B MID FLAP L/E 2" (COUNT FROM I/B) FOUND DELAMINATION AS MARK.(

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.

) - [SDR UIEA2024012500040](https://openairdocs.org/sdr/UIEA2024012500040.md): Panel · delaminated · Feb 5, 2024 · N408MC · Boeing 74747UF · Trailing Edge Flaps > R/H I/B T/E FLAP MID FLAP O/B CARRIAGE ASSY UPPER COVER APNEL FOUND DELAMINATION AS MARK.(

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.

) - [SDR UIEA2024012500041](https://openairdocs.org/sdr/UIEA2024012500041.md): Skin · delaminated · Feb 5, 2024 · N408MC · Boeing 74747UF · Trailing Edge Flaps > RHW T/E I/B AFT FLAP LOWER SURFACE T/E 155" FOUND DELAMINATION AS MARKED (COUNT FROM I/B).(

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.

) - [SDR UIEA2024012500042](https://openairdocs.org/sdr/UIEA2024012500042.md): Fairing · delaminated · Feb 5, 2024 · N408MC · Boeing 74747UF · Trailing Edge Flaps > RHW O/B FWD FLAP FWD FAIRING 48" FOUND DELAMINATION AS MARKED (COUNT FROM O/B).(

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.

) - [SDR UIEA2024012800046](https://openairdocs.org/sdr/UIEA2024012800046.md): Seat Track · damaged · Feb 5, 2024 · N408MC · Boeing 74747UF · Fuselage, Seat/Cargo Attach Fittings > M/D STA 1890 RBL 11 SEAT TRACK CTR GUIDE STOP HOLE FOUND ELONGATED(

SEAT TRACK REPAIRED AS PER SRM 53-00-52-2R-12 REPAIR 12. NO FURTHER DEFECTS NOTED.

) - [SDR UIEA2024012800047](https://openairdocs.org/sdr/UIEA2024012800047.md): Tension Tie · cracked · Feb 5, 2024 · N408MC · Boeing 74747UF · Fuselage Miscellaneous Structure > LH BS 840 UPPER DECK TENSION TIE 1EA CRACK FOUND AT AFT CHANNEL(

TENSION TIE REPAIRED AS PER SRM 53-20-30-2R-1 REPAIR. NO FURTHER DEFECTS NOTED.

) - [SDR UIEA2024012800048](https://openairdocs.org/sdr/UIEA2024012800048.md): Tension Tie · cracked · Feb 5, 2024 · N408MC · Boeing 74747UF · Fuselage Miscellaneous Structure > LH BS 880 UPPER DECK TENSION TIE 1EA CRACK FOUND AT AFT CHANNEL(

TENSION TIE REPAIRED AS PER SRM 53-20-30-2R-1 REPAIR 1. NO FURTHER DEFECTS NOTED.

) - [SDR UIEA2024012800049](https://openairdocs.org/sdr/UIEA2024012800049.md): Tension Tie · cracked · Feb 5, 2024 · N408MC · Boeing 74747UF · Fuselage Miscellaneous Structure > RH BS 840 UPPER DECK TENSION TIE 1EA CRACK FOUND AT 1 O/C POSITION OF THE AFT CHANNEL(

TENSION TIE REPAIRED AS PER SRM 53-20-30-2R-1 REPAIR 1. NO FURTHER DEFECTS NOTED.

) - [SDR UIEA2024012800050](https://openairdocs.org/sdr/UIEA2024012800050.md): Channel · cracked · Feb 5, 2024 · N408MC · Boeing 74747UF · Fuselage Miscellaneous Structure > LH BS 900 UPPER DECK TENSION TIE AFT CHANNEL 1EA HOLE FOUND CRACK(

TENSION TIE REPAIRED AS PER SRM 53-20-30-2R-1 REPAIR 1. NO FURTHER DEFECTS NOTED.

) - [SDR UIEA2024012800051](https://openairdocs.org/sdr/UIEA2024012800051.md): Skin · corroded · Feb 5, 2024 · N408MC · Boeing 74747UF · Fuselage Main, Plate/Skin > FUSELAGE SKIN AT LOWER LOBE CIRCUMFERENTIAL SPLICE LOCATION STA 1715 S45R FOUND CORROSION APPROX 1" X 1"(

SKIN REPAIRED AS PER SRM 53-00-01-2R-1 REPAIR 1 FIG 201 DETAIL I. NO FURTHER DEFECTS NOTED

) - [SDR UIEA2024012900052](https://openairdocs.org/sdr/UIEA2024012900052.md): Skin · corroded · Feb 5, 2024 · N408MC · Boeing 74747UF · Trailing Edge Flaps > LHW I/B AFT FLAP FOUNDÂ BULGE UP(

PERFORMED REPAIR AT BULGE UP AREA IAW RI-57-53-16705. NO FURTHER DEFECTS NOTED.

) - [SDR UIEA2024013000053](https://openairdocs.org/sdr/UIEA2024013000053.md): Skin · dented · Feb 5, 2024 · N408MC · Boeing 74747UF · Trailing Edge Flaps > LHW O/B T/E AFT FLAP O/B PANEL UPPER SURFACE FOUND SEVERAL AREA DENT MARK AS MARKED.(

METAL HOT BOND REPAIR CARRIED OUT AS PER RI-57-51-16699 REV.A. NO FURTHER DEFECTS NOTED.

) - [SDR UIEA2024013000054](https://openairdocs.org/sdr/UIEA2024013000054.md): Skin · dented · Feb 5, 2024 · N408MC · Boeing 74747UF · Trailing Edge Flaps > RHW O/B T/E AFT FLAP O/B PANEL UPPER SURFACE FOUND SEVERAL AREA DENT MARK AS MARKED.(

METAL HOT BOND REPAIR CARRIED OUT AS PER RI-57-51-16700 REV.A. NO FURTHER DEFECTS NOTED.

) - [SDR UIEA2024013100055](https://openairdocs.org/sdr/UIEA2024013100055.md): Frame · cracked · Feb 5, 2024 · N408MC · Boeing 74747UF · Fuselage Main, Bulkhead > LH 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(

INNER CHORD CRACK AREA REPAIRED AS PER RI-53-73-16683 REV.A. NO FURTHER DEFECTS NOTED

) - [SDR UIEA2024013100057](https://openairdocs.org/sdr/UIEA2024013100057.md): Longeron · cracked · Feb 5, 2024 · N408MC · Boeing 74747UF · Fuselage Main, Structure > FUS - 2EA CRACKS WERE FOUND ON RH BS 1480-1540 STR 32-33 LONGERON EXTENSION FITTING(

LONGERON EXTENSION FITTING REPLACEMENT CARRIED OUT AS PER ATLAS AIR EO 4453A818 R19 PART 4. NO FURTHER DEFECTS NOTED

) - [SDR UIEA2024013100058](https://openairdocs.org/sdr/UIEA2024013100058.md): Panel · cracked · Feb 5, 2024 · N408MC · Boeing 74747UF · Fuselage Miscellaneous Structure > M/D STA 1720 L/H DADO PNL FOUND CRACK(

DADO PNL CRACK AREA REPAIRED AS PER RI-25-21-16675 REV.A. NO FURTHER DEFECTS NOTED.

) - [SDR UIEA2024020100059](https://openairdocs.org/sdr/UIEA2024020100059.md): Ladder · cracked · Feb 5, 2024 · N408MC · Boeing 74747UF · Fuselage Main, Structure > M/D CREW LADDER I/B SIDE #7 & 10 STEP FOUND CRACK(

#7 AND #10 STEP CRACK AREA REPAIRED AS PER RI-25-50-16667 REV.A. NO FURTHER DEFECTS NOTED.

) - [SDR UIEA2024020100060](https://openairdocs.org/sdr/UIEA2024020100060.md): Skin · corroded · Feb 5, 2024 · N408MC · Boeing 74747UF · Fuselage Main, Plate/Skin > FX R/H AIRCON BAY STA 1000-1003 CENTER SECTION LOWER SURFACE CORR. AT RBL 15" - RBL 29"(

SKIN CORROSION AREA REPAIRED AS PER RI-57-10-16703 REV.A. NO FURTHER DEFECTS NOTED.

) - [SDR UIEA2024020100061](https://openairdocs.org/sdr/UIEA2024020100061.md): Bracket · damaged · Feb 5, 2024 · N408MC · Boeing 74747UF · Fuselage Miscellaneous Structure > APU COMPT L/H FRAME STA 2674 WIRE BRACKET AND ATT FRAME RIVET HOLES FOUND ELONGATED(

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 53-80-0 - [SDR UIEA2024020100062](https://openairdocs.org/sdr/UIEA2024020100062.md): Skin · cracked · Feb 5, 2024 · N408MC · Boeing 74747UF · Fuselage Main, Plate/Skin > FX - FUSELAGE SKIN STA 1680 STR 41R FOUND CORR CRACK(

SKIN REPAIRED AS PER RI-53-61-16685 REV.A. NO FURTHER DEFECTS NOTED.

) - [SDR UIEA2024020100063](https://openairdocs.org/sdr/UIEA2024020100063.md): Support · cracked · Feb 5, 2024 · N408MC · Boeing 74747UF · Wing Miscellaneous Structure > LHW L/E CAVITY HOLES 1300 FIXED PNL SUPPORT CRACK (AFT OF #4 V/C FLAP)(

SUPPORT BEAM REPAIRED AS PER RI-57-41-16684 REV.A. NO FURTHER DEFECTS NOTED

) - [SDR UIEA2024020100064](https://openairdocs.org/sdr/UIEA2024020100064.md): Closeout Panel · cracked · Feb 5, 2024 · N408MC · Boeing 74747UF · Fuselage Main, Structure > M/D STA 1241 LBL 77-99 CLOSURE PNL FOUND CRACK.(

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.

) - [SDR UIEA2024020100065](https://openairdocs.org/sdr/UIEA2024020100065.md): None · none · Feb 5, 2024 · N408MC · Boeing 74747UF · Standard Practices/Structures > ACCOMPLISHMENT OF EO 4453A301 REV.11, WE FOUND ONE EACH FREEZE PLUG INSTALLED ON UPPER DECK R/H STA 880 FRAME AREA.(

FRAME REPAIRED AS PER RI NO. RI-53-20-16702 REV.A. NO FURTHER DEFECTS NOTED.

) Next page: https://openairdocs.org/aircraft/N408MC/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 = 'N408MC' AND registry_match = 'registration' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/aircraft/N408MC/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.