# Service difficulty reports: N418MC

A list on [N418MC](https://openairdocs.org/aircraft/N418MC.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 4 · 152 reports

- [SDR UIEA2026072300640](https://openairdocs.org/sdr/UIEA2026072300640.md): Apu · odor · Jul 23, 2026 · N418MC · Boeing 74747UF · APU Oil System
  > BACK TO BLOCK DUE TO EICAS MESSAGE SMOKE CREW REST AND UNUSUAL SCENT DETECTED IN UPPER DECK. PERFORM FIRE TEST, NO SMOKE PRESENT IN CABIN. OIL SCENT COMING FROM APU. SUSPECT APU BEARING OIL LEAK ENTERING CABIN. REMOVED AND REPLACED APU IAW ATLAS WORK CARD 49-
- [SDR UIEA2026051400315](https://openairdocs.org/sdr/UIEA2026051400315.md): Rib · broken · May 14, 2026 · N418MC · Boeing 74747UF · Wing, Rib/Bulkhead
  > BROKEN ON THE RIB OF RH WING FIXED LE AT ILES 766.45. REPAIR THE RIB IAW EI T2026A57M-913, REV 2. JOB COMPLETED AND CONDITION CHECK NORMAL.
- [SDR UIEA2026051400316](https://openairdocs.org/sdr/UIEA2026051400316.md): Rib · cracked · May 14, 2026 · N418MC · Boeing 74747UF · Wing, Rib/Bulkhead
  > CRACKED DAMAGE ON THE RIB OF THE RT WING FIXED LE AT ILES 756.95. REPAIR THE RIB IAW EI T2026A57M-914, REV 1. JOB COMPLETED AND CONDIITON CHECK NORMAL.
- [SDR UIEA2026051400317](https://openairdocs.org/sdr/UIEA2026051400317.md): Support Angle · damaged · May 14, 2026 · N418MC · Boeing 74747UF · Aerodynamic Fairings
  > CORRODED ANGLE FWD WING TO BODY FAIRING PANEL SUPPORT BS 977, LBL 3.42. REMOVED DAMAGED ANGLE IAW SRM 51-40-02-0G-0, REV 106. INSTALLED NEW ANGLE IAW SRM 51-40-02-0G-0 REV 106 AND DWG 65B06976, SHEET 2, REV G. JOB COMPLETED AND CONDITION CHECKED NORMAL.
- [SDR UIEA2026051400318](https://openairdocs.org/sdr/UIEA2026051400318.md): Fitting · corroded · May 14, 2026 · N418MC · Boeing 74747UF · Fuselage, Equipment Attach Fittings
  > CORROSION- FND M/D FLOOR FITTING CORROSION AT BS 460 RBL 95. FABRICATED REPLACEMENT FITTING IAW EI T2026A25M-962 REV 1. JOB COMPLETED AND CORROSION CHECK NORMAL.
- [SDR UIEA2026051400319](https://openairdocs.org/sdr/UIEA2026051400319.md): Fitting · corroded · May 14, 2026 · N418MC · Boeing 74747UF · Fuselage Main, Attach Fittings
  > FND M/D FLOOR FITTING CORROSION AT STA 460 RBL 95. REPLACED MD FLOOR FITTING AT BS 460, RBL 95 IAW AMM 53-44-00-202-001 REV 116. JOB COMPLETED AND CONDITION CHKD NORMAL.
- [SDR UIEA2026051400320](https://openairdocs.org/sdr/UIEA2026051400320.md): Repair · not reported · May 14, 2026 · N418MC · Boeing 74747UF · Fuselage Main, Plate/Skin
  > EXISITNG REPAIR ON FUSELAGE SKIN BETWEEN STA 1787 AND STA 1800, NEAR S-34R. REMOVED EXISTING PARTS IAW SRM 57-40-02-0G-0 REV 106. ACCOMPLISHED REPAIR ON THE FUSELAGE SKIN IAW EI T2026A53M-976 REV 1. JOB ACCOMPLISHED AND CONDITION CHECK NORMAL.
- [SDR UIEA2024052200401](https://openairdocs.org/sdr/UIEA2024052200401.md): Skin · delaminated · May 27, 2024 · N418MC · Boeing 74747UF · Trailing Edge Flaps
  > LHW I/B MID FLAP L/E FAIRING TO I/B EDGE 157" FOUND DELAMINATION(<P>PERFORMED PERMANENT COMPOSITE HOTBOND REPAIR SRM 51-70-07 PAR 5A REV.100 REV DATE:20 FEB 2024. NO FURTHER DEFECTS NOTED.</P>)
- [SDR UIEA2024052200402](https://openairdocs.org/sdr/UIEA2024052200402.md): Skin · delaminated · May 27, 2024 · N418MC · Boeing 74747UF · Trailing Edge Flaps
  > RHW O/B FORE FLAP L/E FAIRING I/B EDGE110" FOUND DELAMINATION(<P>PERFORMED PERMANENT COMPOSITE HOTBOND REPAIR SRM 51-70-07 PAR 5A REV.100 REV DATE:20 FEB 2024. NO FURTHER DEFECTS NOTED.</P>)
- [SDR UIEA2024052200403](https://openairdocs.org/sdr/UIEA2024052200403.md): Skin · delaminated · May 27, 2024 · N418MC · Boeing 74747UF · Trailing Edge Flaps
  > LHW I/B FORE FLAP L/E FAIRING I/B EDGE 230" FOUND DELAMINATION(<P>PERFORMED PERMANENT COMPOSITE HOTBOND REPAIR SRM 51-70-07 PAR 5A REV.100 REV DATE:20 FEB 2024. NO FURTHER DEFECTS NOTED.</P>)
- [SDR UIEA2024052200404](https://openairdocs.org/sdr/UIEA2024052200404.md): Skin · delaminated · May 27, 2024 · N418MC · Boeing 74747UF · Trailing Edge Flaps
  > RHW I/B AFT FLAP LOWER T/E I/B EDGE 172" FOUND DELAMINATION(<P>PERFORMED PERMANENT COMPOSITE HOTBOND REPAIR SRM 51-70-07 PAR 5A REV.100 REV DATE:20 FEB 2024. NO FURTHER DEFECTS NOTED.</P>)
- [SDR UIEA2024052200405](https://openairdocs.org/sdr/UIEA2024052200405.md): Skin · delaminated · May 27, 2024 · N418MC · Boeing 74747UF · Trailing Edge Flaps
  > RHW O/B MID FLAP L/E FAIRING I/B EDGE14" FOUND DELAMINATION(<P>PERFORMED PERMANENT COMPOSITE HOTBOND REPAIR SRM 51-70-07 PAR 5A REV.100 REV DATE:20 FEB 2024. NO FURTHER DEFECTS NOTED.</P>)
- [SDR UIEA2024052200406](https://openairdocs.org/sdr/UIEA2024052200406.md): Skin · delaminated · May 27, 2024 · N418MC · Boeing 74747UF · Trailing Edge Flaps
  > RHW O/B FORE FLAP L/E FAIRING 158" TO I/B EDGE FOUND DELAMINATION(<P>PERFORMED PERMANENT COMPOSITE HOTBOND REPAIR SRM 51-70-07 PAR 5A REV.100 REV DATE:20 FEB 2024. NO FURTHER DEFECTS NOTED.</P>)
- [SDR UIEA2024052200407](https://openairdocs.org/sdr/UIEA2024052200407.md): Skin · delaminated · May 27, 2024 · N418MC · Boeing 74747UF · Trailing Edge Flaps
  > LHW I/B AFT FLAP UPPER T/E FROM I/B EDGE 122" FOUND DELAMINATION(<P>PERFORMED PERMANENT COMPOSITE HOTBOND REPAIR SRM 51-70-07 PAR 5A REV.100 REV DATE:20 FEB 2024. NO FURTHER DEFECTS NOTED.</P>)
- [SDR UIEA2024052300408](https://openairdocs.org/sdr/UIEA2024052300408.md): Skin · dented · May 27, 2024 · N418MC · Boeing 74747UF · Trailing Edge Flaps
  > RHW O/B AFT FLAP LOWER T/E 24" TO I/B PNL EDGE FOUND DENT(<P>PERFORMED PERMANENT METAL TO METAL HOTBOND REPAIR SRM 51-70-10 REPAIR 4 REV.100 REV DATE:20 FEB 2024. NO FURTHER DEFECTS NOTED.</P>)
- [SDR UIEA2024052300409](https://openairdocs.org/sdr/UIEA2024052300409.md): Skin · dented · May 27, 2024 · N418MC · Boeing 74747UF · Trailing Edge Flaps
  > LHW O/B AFT FLAP LOWER T/E 36" TO I/B PNL EDGE FOUND DENT(<P>PERFORMED PERMANENT METAL TO METAL HOTBOND REPAIR SRM 51-70-10 REPAIR 4 REV.100 REV DATE:20 FEB 2024. NO FURTHER DEFECTS NOTED.</P>)
- [SDR UIEA2024052300410](https://openairdocs.org/sdr/UIEA2024052300410.md): Structure · corroded · May 27, 2024 · N418MC · Boeing 74747UF · Fuselage Miscellaneous Structure
  > FX - LH AIRCON BAY STA 1220 - 1240 CENTER TANK LWR SURFACE O/B CHORD CRACK(<P>LH AIR COND BAY STA 1220-1240 CENTER TANK LWR SURFACE O/B CHORD REPAIR AS PER RI NO: RI-57-00-16879 REV A. NO FURTHER DEFECTS NOTED</P>)
- [SDR UIEA2024052300411](https://openairdocs.org/sdr/UIEA2024052300411.md): Fuel Tank · corroded · May 27, 2024 · N418MC · Boeing 74747UF · Fuel Storage
  > FX - LH AIRCON BAY STA 1240 CENTER TANK LOWER SURFACE CORR AT O/B AREA(<P>LH AIRCON BAY STA 1240 CENTER TANK LOWER SURFACE AT O/B AREA REPAIRED IAW RI NO: RI-57-10-16896 REV A. NO FURTHER DEFECTS NOTED.</P>)
- [SDR UIEA2024052300413](https://openairdocs.org/sdr/UIEA2024052300413.md): Structure · corroded · May 27, 2024 · N418MC · Boeing 74747UF · Fuselage Structure (General)
  > CENTER SECTION AFT FACE FOUND CORROSION ( RH O/J PUMP BONDING AREA)(<P>CORROSION REMOVED AND REPROTECTED IAW SRM 51-10-02 AND SRM 51-20-01 REV 100 DATE 20 FEB 2024. NO FURTHER DEFECTS NOTED.</P>)
- [SDR UIEA2024052300414](https://openairdocs.org/sdr/UIEA2024052300414.md): Stiffener · cracked · May 27, 2024 · N418MC · Boeing 74747UF · Nacelle/Pylon Miscellaneous Structure
  > NO.3 PYLON - I/B STIFFENER FOUND CRACK AT NAC STA 300(<P>NO.3 PYLON - I/B STIFFENER REPAIRED AS PER SRM 54-51-02-2R-2 REPAIR 2. NO FURTHER DEFECTS NOTED.</P>)
- [SDR UIEA2024052300431](https://openairdocs.org/sdr/UIEA2024052300431.md): Access Panel · chafed · May 27, 2024 · N418MC · Boeing 74747UF · Trailing Edge Flaps
  > LHW O/B T/E AFT FLAP O/B UPPER ACCESS PANEL 588IT EXTERIOR SURFACE SERVERAL AREA FOUND CHAFING(<P>PERMANENT METAL TO METAL HOTBOND REPAIR AS PER RI NO. RI-57-51-16892 REV.A. NO FURTHER DEFECTS NOTED.</P>)
- [SDR UIEA2024052400432](https://openairdocs.org/sdr/UIEA2024052400432.md): Skin · cracked · May 27, 2024 · N418MC · Boeing 74747UF · Leading Edge Devices
  > RHW L/E #24 VC FLAP FOLDING NOSE ASSY FOUND CRACKED AT THE /B EDGE(<P>DAMAGED AREA REPAIRED AS PER RI-57-43-16891 REV A. NO FURTHER DEFECTS NOTED.</P>)
- [SDR UIEA2024052400434](https://openairdocs.org/sdr/UIEA2024052400434.md): Fastener · loose · May 27, 2024 · N418MC · Boeing 74747UF · Nacelle/Pylon, Main Frame
  > NO.2 ENG R/H CORE COWL FOUND SEVERAL FASTENER LOOSE(<P>#2 ENG RH CORE COWL FASTENER REPLACED IAW EA -1971A101 REV 0 AND SRM 51-40-02 REV 100 DATE 20 FEB 2024. NO FURTHER DEFECTS NOTED. </P>)
- [SDR UIEA2024052500443](https://openairdocs.org/sdr/UIEA2024052500443.md): Skin · cracked · May 27, 2024 · N418MC · Boeing 74747UF · Nacelle/Pylon, Plate/Skin
  > NO.3 ENG - RH CORE COWL AFT EDGE EXTERNAL SKIN CRACK FOUND AT CENTER AREA AS MARKED(<P>NO.3 ENG - RH CORE COWL AFT EDGE SKIN REPAIRED IAW EA NO: EA-1971A099 REV 0. NO FURTHER DEFECTS NOTED.</P>)
- [SDR UIEA2024052500444](https://openairdocs.org/sdr/UIEA2024052500444.md): Structure · cracked · May 27, 2024 · N418MC · Boeing 74747UF · Nacelle/Pylon, Main Frame
  > #2 ENG R/H CORE COWL EXHAUST AREA FOUND SEVERAL FASTNER HOLE CRACKED(<P>REPAIRED IAW SRM 54-41-01-2R-3 REPAIR 3 AND EA-1971A104. NO FURTHER DEFECTS NOTED.</P>)
- [SDR UIEA2024052500445](https://openairdocs.org/sdr/UIEA2024052500445.md): Skin · cracked · May 27, 2024 · N418MC · Boeing 74747UF · Nacelle/Pylon, Plate/Skin
  > NO.3 ENG - RH CORE COWL EXTERNAL SKIN CRACK FOUND JUST BELOW THE EXHAUST LOUVER AS MARKED(<P>REPAIRED IAW SRM 54-45-01-2R-4 REPAIR 4. NO FURTHER DEFECTS NOTED.</P>)
- [SDR UIEA2024052500446](https://openairdocs.org/sdr/UIEA2024052500446.md): Panel · damaged · May 27, 2024 · N418MC · Boeing 74747UF · Nacelle/Pylon Structure
  > NO.4 PYLON 482EL SCREW HOLE FOUND ELONGATED.(<P>#4 PYLON PANEL 482EL FABRICATED IAW RI NO: RI-54-51-16889 REV A. HFEC INSPECTION C/W PER NTM PART 6 51-00-00 PROCEDURE 23 REV 176 ON BEND RAD11 AREA, NO CRACK FOUND</P>)
- [SDR UIEA2024052600447](https://openairdocs.org/sdr/UIEA2024052600447.md): Structure · cracked · May 27, 2024 · N418MC · Boeing 74747UF · Fuselage Structure (General)
  > 1EA CRACK WAS FOUND ON LH NOSE WHEEL WELL FORWARD CORNER FASTENER HOLE(<P>STA 240 LH SIDE PANEL CHORD P/N: 65B07942-609 CRACK AREA REPAIRED IAW RI-53-00-16890 REV A. NO FURTHER DEFECTS NOTED.</P>)
- [SDR UIEA2024052600448](https://openairdocs.org/sdr/UIEA2024052600448.md): Structure · cracked · May 27, 2024 · N418MC · Boeing 74747UF · Fuselage Structure (General)
  > 1EA CRACK WAS FOUND ON THE FASTENER HOLE AT RH STA 240 #3 RD LAYER ( SHIM)(<P>STA 240 RH #3 RD LAYER ( SHIM) FABRICATED AND INSTALLED IAW RI-53-00-16890 REV A. NO FURTHER DEFECTS NOTED. </P>)
- [SDR UIEA2024052600449](https://openairdocs.org/sdr/UIEA2024052600449.md): Doubler · none · May 27, 2024 · N418MC · Boeing 74747UF · Standard Practices/Structures
  > LH STA 240 NOSE WHEEL CORNER DOUBLER FOUND S.E.W AND FORWARD CORNER MOD DEVIATION(<P>LH STA 240 NOSE WHEEL CORNER DOUBLER FOUND S.E.W AND FORWARD CORNER MOD DEVIATION AREA REPAIRED IAW RI-53-00-16890 REV A. NO FURTHER DEFECTS NOTED.</P>)
- [SDR UIEA2024052600450](https://openairdocs.org/sdr/UIEA2024052600450.md): Doubler · none · May 27, 2024 · N418MC · Boeing 74747UF · Standard Practices/Structures
  > RH STA 240 NOSE WHEEL CORNER DOUBLER FOUND S.E.W AND FORWARD CORNER MOD DEVIATION(<P>RH STA 240 NOSE WHEEL CORNER DOUBLER FOUND S.E.M AND FORWARD CORNER MOD DEVIATION AREA REPAIRED IAW RI-53-00-16890 REV A. NO FURTHER DEFECTS NOTED.</P>)
- [SDR UIEA2024052600451](https://openairdocs.org/sdr/UIEA2024052600451.md): Support Rod · corroded · May 27, 2024 · N418MC · Boeing 74747UF · Wing Miscellaneous Structure
  > LHW T/E UPR FIXED PANEL RIB SUPPORT ROD LOWER FITTING P/N: 69B11633-13 FOUND CORROSION(<P>LHW T/E UPR FIXED PANEL RIB SUPPORT ROD LOWER FITTING P/N: 69B11633-13 AND BRACKET P/N: 65B81991-41 REPLACED AND INSTALLED IAW RI-57-00-16905 REV A. NO FURTHER DEFECTS N
- [SDR UIEA2024052210398](https://openairdocs.org/sdr/UIEA2024052210398.md): Bulb · failed · May 21, 2024 · N418MC · Boeing 74747UF · Emergency Lighting
  > 2EA EMERGENCY LIGHT FOUND INOP(<P>2EA EMERGENCY LIGHT BULB REPLACED IAW AMM 33-51-07 REV 110 15MAR2024 AND OPERATIONAL TEST NORMAL IAW AMM 33-51-07 REV 110 15MAR2024.</P>)
- [SDR UIEA2024011400013](https://openairdocs.org/sdr/UIEA2024011400013.md): Cdu · unknown · Jan 14, 2024 · N418MC · Boeing 74747UF · Central Display
  > 30 MINS INTO FLIGHT, FO CDU LOST POWER. THIS HAPPENED JUST AS THEY WERE COASTING OUT. REPEAT WRITE-UP(<P>FOUND 115 VAC AT PLUG (DM7440A) PIN 40 TO P41. VOLTAGE NORMAL DURING WIRE SHAKE. GND ALSO NORMAL DURING WIRE SHAKE. OPS CHECK NORMAL FOR RH CDU. FOR T/S PU
- [SDR UIEA2022053000558](https://openairdocs.org/sdr/UIEA2022053000558.md): Drive Assy · failed · May 30, 2022 · N418MC · Boeing 74747UF · Doppler System
  > BOTH L & R WEATHER RADARS FAILED AT CRUISE. REMOVED AND REPLACED WEATHER RADAR DRIVE MOUNT ASSEMBLY.
- [SDR UIEA2022052400538](https://openairdocs.org/sdr/UIEA2022052400538.md): Rod End Bearing · elongated · May 25, 2022 · N418MC · Boeing 74747UF · Engine Thrust Reverser
  > NO.4 ENG LH C-DUCT OPEN ACTUATOR ROD END BOLT HOLE FOUND ELONGATED. NO.4 ENG L/H C-DUCT REPLACED IAW 78-31-01
- [SDR UIEA2022051600482](https://openairdocs.org/sdr/UIEA2022051600482.md): Fitting · cracked · May 25, 2022 · N418MC · Boeing 74747UF · Fuselage Structure (General)
  > FUSE - CENTER SECTION - STA 1000 FRONT SPAR SHEAR TIE AND INTERCOSTAL LUG FTG INSPECTION FOUND CRACKED AT STA 1000 RBL 33.99. FUSE - CENTER SECTION - STA 1000 RBL 33.99" FRONT SPAR SHEAR TIE LUG FTG P/N 69B14267U9 REPLACED AND INSTALLED IAW ATLAS EO: 4453C024
- [SDR UIEA2022051600483](https://openairdocs.org/sdr/UIEA2022051600483.md): Fitting · cracked · May 25, 2022 · N418MC · Boeing 74747UF · Fuselage Structure (General)
  > FUSE - CENTER SECTION - STA 1000 FRONT SPAR SHEAR TIE AND INTERCOSTAL LUG FTG INSPECTION FOUND CRACKED AT STA 1000 LBL 57.5. FUSE - CENTER SECTION - STA 1000 LBL 57.5" FRONT SPAR SHEAR TIE LUG FTG P/N: 69B14267U7 REPLACED AND INSTALLED IAW ATLAS EO: 4453C024 P
- [SDR UIEA2022051800487](https://openairdocs.org/sdr/UIEA2022051800487.md): Cargo Track · cracked · May 25, 2022 · N418MC · Boeing 74747UF · Fuselage Structure (General)
  > AFT CARGO STA 1860 AND STA 1880 LBL 24" CARGO TRACK FOUND CRACKED. AFT CARGO STA 1830.45 TO STA 1890.45 LBL 24.75 CARGO TRACK REPAIRED IAW RI-53-00-15595 REV.A
- [SDR UIEA2022051800488](https://openairdocs.org/sdr/UIEA2022051800488.md): Skin · cracked · May 25, 2022 · N418MC · Boeing 74747UF · Fuselage Structure (General)
  > EO 4453A516 PART 1 AND PART 2 - FUSE SKIN NOSE WHEEL WELL AFT CORNER SKIN PANEL INSPECTION FOUND LH SKIN CRACKED. FUSE - STA 400 L/H AND R/H SKIN NOSE WHEEL WELL AFT CORNER SKIN PANEL MOD ACCOMPLISHED IAW EO 4453A516 PART 3 AND PART 4 AND RI-53-10-15613 REV.A<
- [SDR UIEA2022052400539](https://openairdocs.org/sdr/UIEA2022052400539.md): Latch · elongated · May 25, 2022 · N418MC · Boeing 74747UF · Tail Cone Doors
  > APU DOOR RH NO.5 LATCH CUTOUT FOUND ELONGATED. APU DOOR ASSY RH P/N: 65B02771-204 S/N: TLS28220 REPLACED AND INSTALLED IAW AMM 52-48-02
- [SDR UIEA2022052600545](https://openairdocs.org/sdr/UIEA2022052600545.md): Latch · elongated · May 25, 2022 · N418MC · Boeing 74747UF · Tail Cone Doors
  > APU DOOR RH NO.5 LATCH CUTOUT FOUND ELONGATED. APU DOOR ASSY RH P/N: 65B02771-204 S/N TLS28220 REPLACED AND INSTALLED IAW AMM 52-48-02
- [SDR UIEA2022011860032](https://openairdocs.org/sdr/UIEA2022011860032.md): Valve · malfunctioned · Jan 15, 2022 · N418MC · Boeing 74747UF · Pneumatic Distribution System
  > ON TAKEOFF ROLL AT APPROXIMATELY 80 KNOTS BLEED 1 EICAS MESSAGE APPEARED AND A PRONOUNCED ACRID SMELL INFILTRATED THE FLIGHT DECK.(<P ><SPAN>PERFORMED TAKE OFF POWER RUNS PER AMM 71-00-00. NO DISCREPANCIES FOUND. SEE LOG PAGE ITEMS M5 AND M6 FOR CONDITIONAL IN
- [SDR UIEA2021122802490](https://openairdocs.org/sdr/UIEA2021122802490.md): None · none · Dec 28, 2021 · N418MC · Boeing 74747UF · Landing Gear System
  > CAPTAIN REPORTED SEVERE SHIMMY IN AFT OF AIRCRAFT DURING TAKEOFF ROLL BEGINNING AT 50 KTS TO 80 KTS RESULTING IN REJECTED TAKE OFF(<P>REMOVED AND REPLACED WHEEL ASSEMBLY IAW AMM 32-45-02.</P>)
- [SDR UIEA2021100702202](https://openairdocs.org/sdr/UIEA2021100702202.md): None · none · Oct 3, 2021 · N418MC · Boeing 74747UF · Wing Structure
  > RH LWR WING SKIN PANEL CORROSION FOUND ON THE FRONT SPAR AT OLES 1493.45.(<P>PERFORMED CUT OUT CORROSION AREA AND DOUBLER REPAIR IAW EO 4457A757.</P>)
- [SDR UIEA2021091302013](https://openairdocs.org/sdr/UIEA2021091302013.md): Pressure Switch · failed · Sep 12, 2021 · N418MC · Boeing 74747UF · Engine Thrust Reverser
  > (70KTS) LOW SPEED REJECTED T/O DUE TO " ENG 3 T/R EICAS PLUS STATUS MSG. BRAKE TEMS MAX WAS 2 IN(<P>PLF SHOWS MSG 78403. PRESSIRE SWITCH FAIL TRF TO DMI 153434 PER MEL 78-31-01A CAC DUE 22SEP21. BRAKE TEMP ALL NORMAL. T/R #3 DEACTIVATED PER MEL 78-31-01A MCC;
- [SDR UIEA2021081201767](https://openairdocs.org/sdr/UIEA2021081201767.md): Sequence Valve · failed · Aug 12, 2021 · N418MC · Boeing 74747UF · Landing Gear Retraction/Extension System
  > NOSE GEAR FAILED TO EXTEND ON FINAL APPROACH. ABORTED APPROACH EXTENDED SUCCESSFULLY PER QRH PROCEDURES.(<P><SPAN>TRANSFERRED TO MDDR 151711 IAW MEL 32-30-01, CAT C.</SPAN></P> / <P><SPAN>COMPLIED WITH ACTION PLAN 20516 AND 20526. PER ACTION PLAN REMOVED AND
- [SDR UIEA2020061901319](https://openairdocs.org/sdr/UIEA2020061901319.md): Engine · fire · Jun 17, 2020 · N418MC · Boeing 74747UF · Engine (Turbine/Turboprop)
  > DURING NR 2 ENGINE START, TAIL PIPE FLASH FIRE REPORTED BY GROUND CREW, FOLLOWED BY RED EGT INDICATION ON EICAS. SHUT DOWN THE ENGINE AND COMPLIED WITH QRH AND RETURNED TO GATE. NR 2 ENGINE CHANGED IAW WO 67179, W/C 71-099-02-01. ENGINE RUN UP SATISFACTORY.
- [SDR UIEA2020051200769](https://openairdocs.org/sdr/UIEA2020051200769.md): Support · corroded · May 8, 2020 · N418MC · Boeing 74747UF · Aerodynamic Fairings
  > FX KEEL BEAM L/H BODY FAIRING ( 191JJ) ACCESS PANEL SUPPORT FOUND CORROSION.(<P>FX KEEL BEAM LH BODY FAIRING ( 191JJ) ACCESS PANEL SUPPORT CORROSION AREA REPAIRED AS PER SRM 53-00-71 FIG 101.</P>)
- [SDR UIEA2020051200770](https://openairdocs.org/sdr/UIEA2020051200770.md): Support · corroded · May 8, 2020 · N418MC · Boeing 74747UF · Aerodynamic Fairings
  > FX KEEL BEAM RH BODY FAIRING ( 191JJ) ACCESS PANEL SUPPORT FOUND CORROSION.(<P>FX KEEL BEAM RH BODY FAIRING ( 191JJ) ACCESS PANEL SUPPORT CORROSION AREA REPAIRED AS PER SRM 53-00-71 FIG 101.</P>)

Next page: https://openairdocs.org/aircraft/N418MC/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 = 'N418MC' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N418MC/reports

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