# Service difficulty reports: N416MC

A list on [N416MC](https://openairdocs.org/aircraft/N416MC.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 · 173 reports

- [SDR UIEA2026092200907](https://openairdocs.org/sdr/UIEA2026092200907.md): Display · failed · Sep 22, 2026 · N416MC · Boeing 74747UF · Central Display
  > FO INBOARD IDU SHOWED GARBLED INFO. R & R FO NAV DISPLAY IAW AMM 31-61-02 AND IPC 31-61-01A. OPS CHECK GOOD.</P>)
- [SDR UIEA2026081000719](https://openairdocs.org/sdr/UIEA2026081000719.md): Fitting · cracked · Aug 8, 2026 · N416MC · Boeing 74747UF · Fuselage Main, Attach Fittings
  > FOUND LUG FITTING CRACK AT FWD CARGO, BS 1000, LBL 11.33. REMOVED DAMAGED PART IAW SRM 51-40-02-0G-0, REV 107. INSTALLED NEW PART IAW SRM 51-40-02-0G-0, REV 107 AND REF EO 4453C024, PART 3, REV 4. CONDITION CHKD NORMAL.
- [SDR UIEA2026081000721](https://openairdocs.org/sdr/UIEA2026081000721.md): Shear Tie · cracked · Aug 8, 2026 · N416MC · Boeing 74747UF · Fuselage Internal Mounting Structure
  > FOUND SHEAR TIE CRACK AT STA 1000 RBL 33, FWD CGO. REMOVED DAMAGED PART IAW SRM 51-40-02-0G-0 REV 107. PERFORMED EI T2026A53M-1419, REV 0, AND REF EO 4453C024, PART 8, REV 4. ACCOMPLISHED EI T2026A53M-1419, REV 1. CONDITION CHKD NORMAL.
- [SDR UIEA2026081000722](https://openairdocs.org/sdr/UIEA2026081000722.md): Seat Track · cracked · Aug 8, 2026 · N416MC · Boeing 74747UF · Fuselage, Seat/Cargo Attach Fittings
  > FOUND SUBSTITUTE SEAT TRACK SURFACE CRACKED AT M/D BS 1000, LBL 75.92. REMOVED DAMAGED TRACK IAW SRM 51-40-02-0G-0, REV 107. REPAIRED DAMAGED AREA IAW W/S 64525, SRM 53-00-52-2R-13, REV 107. INSTALLED FASTENERS IAW SRM 51-40-02-0G-0, REV 107, AND DWG 65B82
- [SDR UIEA2026081000723](https://openairdocs.org/sdr/UIEA2026081000723.md): Cargo Track · broken · Aug 8, 2026 · N416MC · Boeing 74747UF · Fuselage, Seat/Cargo Attach Fittings
  > FOUND FWD CARGO TRACK BROKEN BS 560, LBL 24.75. REMOVED DAMAGED IAW SRM 51-40-02-0G-0, REV 107. REPAIRED DAMAGED AREA IAW W/S 60524, SRM 53-00-52-2R-10 REV 107, & EI T2026A53M-1614, REV 0. INSTALL FASTENERS IAW SRM 51-40-02-0G-0, REV 107, AND DWG 65B12300
- [SDR UIEA2026081000724](https://openairdocs.org/sdr/UIEA2026081000724.md): Spar Web · none · Aug 8, 2026 · N416MC · Boeing 74747UF · Standard Practices/Structures
  > FOUND EXISTING REPAIR ON VERTICLE STAB REAR SPAR WEB BETWEEN VSS 205 - VSS 220. REMOVED EXISTING REPAIR DOUBLER IAW SRM 51-40-02-0G-0, REV 107. REPAIRED DAMAGED AREA IAW W/S 60564 SRM 55-30-10-2R-2 REV 107. CHKD NORMAL.
- [SDR UIEA2026081000734](https://openairdocs.org/sdr/UIEA2026081000734.md): Bulkhead · modification · Aug 8, 2026 · N416MC · Boeing 74747UF · Standard Practices/Structures
  > PERFORMED BS 2598 BULKHEAD MODIFICATION, FOUND DEVIATION AT DOUBLER. ACCOMPLISHED EI T2026A53M-1528, REV 1, AND EI T2026A53M-1439, REV 1. CHECKED NORMAL.
- [SDR UIEA2026081000735](https://openairdocs.org/sdr/UIEA2026081000735.md): Repair · none · Aug 8, 2026 · N416MC · Boeing 74747UF · Trailing Edge Flaps
  > EXISTING REPAIR ON RT WING OTBD MID FLAP LOWER SURFACE. PERFORMED PERMANENT REPAIR ON RT WING OTBD MID FLAP LOWER SURFACE, WBL 563 IAW SRM 57-53-01-2R-1 AND SRM 51-70-10-2R-0, REV 107. CONDITION CHECK IS SATISFACTORY. REPAIR PROCESS REFER TO J/C ATTACHING SH
- [SDR UIEA2026081000736](https://openairdocs.org/sdr/UIEA2026081000736.md): Splice Angle · cracked · Aug 8, 2026 · N416MC · Boeing 74747UF · Fuselage Main, Structure
  > CRACK, PERFORMED SB 4453B761, PART 1-2. FOUND A CRACK AT BS 2598, S11R, RT FWD LWR FITTING AREA. ACCOMPLISHED EI 2026A53M-1510, REV 2, AND DWG 65B02706, SH 24, REV A, AND DWG 65B02597, SH 2 REV H, AND DWG 65B02509, SHT 3, REV R. CHECKED NORMAL.
- [SDR UIEA2026081000737](https://openairdocs.org/sdr/UIEA2026081000737.md): Angle · corroded · Aug 8, 2026 · N416MC · Boeing 74747UF · Fuselage Main, Structure
  > FOUND CORROSION ON THE UPPER ANGLE BS 1030, LBL 11.33. ACCOMPLISHED W/S 60551 IAW SRM 53-40-52-2R-3, REV 107. & EI T2026A53M-1522, REV 1. CHECKED NORMAL.
- [SDR UIEA2026081000738](https://openairdocs.org/sdr/UIEA2026081000738.md): Repair · none · Aug 8, 2026 · N416MC · Boeing 74747UF · Standard Practices/Structures
  > PERFORMED UPGRADE TIME-LIMITED REPAIR ON SEC 48 FUSELAGE SKIN AT BS 2600, S51R. ACCOMPLISHED EI T2026A53M-1409, REV 1, AND DWG 65B02509, SH 9, REV C, AND DWG 65B02700, SH 2, REV G, SH 6, REV -. CHECKED NORMAL.
- [SDR UIEA2026050500295](https://openairdocs.org/sdr/UIEA2026050500295.md): Signal Cond Unit · faulted · May 4, 2026 · N416MC · Boeing 74747UF · Engine Ignition Analyzer System
  > HIGH SPEED RTO AT 140KTS INDICATED DUE TO ENG NR 1 NOT MAKING T/O THRUST. R & R N1 FAN SHAFT SPEED SENSOR & ENG IDLE RUN CHKD OK IAW AMM 77-12-01/401, AMM 71-00-00/501 & IPC 77-12-01-01. NEED THE ENG HIGH PWR CHK. R & R AVM SIGNAL CONDITIONER THEN OPS CHKD O
- [SDR UIEA2025061400773](https://openairdocs.org/sdr/UIEA2025061400773.md): Tire · failed · Jun 14, 2025 · N416MC · Boeing 74747UF · Tire
  > #10 MLG TIRE FAILURE ON LANDING. R/R #9 & #10 MLG WHEEL ASSY PER AMM 32-45-01/401 & AIPC 32-45-03-02. FOUND DAMAGE ON RIGHT BODY GEAR DOOR (OUTBOARD). REPLACED DOOR PER AMM 32-14-02. RIGHT BODY GEAR STRUT DOOR DAMAGED. REPLACED PER AMM 32-14-06. DAMAGE AT R/H
- [SDR UIEA2025052300679](https://openairdocs.org/sdr/UIEA2025052300679.md): Switch · inoperative · May 23, 2025 · N416MC · Boeing 74747UF · Engine Bleed Air System
  > BLEED 2 OVHT / PRV EICAS MSG. QRH PROCEDURE IND NO NAI AVAILABLE FOR ENG #2.(<P>REMOVED AND REPLACED BLEED 2 OVHT SWITCH REF AMM 36-22-01 & AIPC 36-22-01-01, OPS CHECK GOOD. NO LEAKS DETECTED. PERFORMED MPA RUN AS REQUESTED, NO FAULTS FOUND REF AMM 71-00-00-71
- [SDR UIEA2024092300930](https://openairdocs.org/sdr/UIEA2024092300930.md): Switch · no discrepancy · Sep 23, 2024 · N416MC · Boeing 74747UF · Overheat Detection
  > BLD 4 OVHT/PRV EICAS MSG. REPEAT ISSUE SEE LG PAGE 1858928.(<P>MSG 36044. PERFORMED WIRING CHECK BTWN ASCTU & OVERTEMP SW, RESULT GOOD. R/R ASCTU & GND TEST / OPS CHECK GOOD PER AMM 36-11-30 & IPC 36-11-30-01A. ENG RUN UP PERFORMED AND NO DEFECTS NOTED PER AMM
- [SDR UIEA2024092300915](https://openairdocs.org/sdr/UIEA2024092300915.md): Switch · faulted · Sep 22, 2024 · N416MC · Boeing 74747UF · Engine Bleed Air System
  > BLD 4 OVHT/PRV EICAS MSG. QRH C/W(<P>R/R OVERTEMP SW IAW AMM 36-22-01 & IPC 36-22-01-01. LEAK & OPS CHECK GOOD.</P>)
- [SDR UIEA2024081400827](https://openairdocs.org/sdr/UIEA2024081400827.md): Pin · corroded · Aug 13, 2024 · N416MC · Boeing 74747UF · Hydraulic Power System Wiring
  > ATB, HYD SYS 4 QTY INDICATION LOW #4. A/C ARRIVED WITH 0.75 ON THE #4 HYD SYS. PLACED LOAD ON SYS WITH NO VISUAL HYD LEAKS ANYWHERE AND A STEADY QTY IND SYS 1 & 2 ARE AT 1.20 AND 3 AT 0.97.(<P>R/R THE CORRODED PIN, CLEAN & RECONNECT. C/W FLUID TRANSFER PER AMM
- [SDR UIEA2024061400520](https://openairdocs.org/sdr/UIEA2024061400520.md): Stringer · cracked · Jun 24, 2024 · N416MC · Boeing 74747UF · Nacelle/Pylon, Longeron/Stringer
  > #3 PYLON - I/B LOWER STRINGER CRACK FOUND AT MOST AFT END AREA (APPROX NAC STA 374) AS MARKED(<P>3 PYLON - I/B LOWER STRINGER REPAIRED AS PER SRM 54-51-02-2R-2 REPAIR 2 REV 101 DATE 20 JUN 2024. NO FURTHER DEFECTS NOTED</P>)
- [SDR UIEA2024061400521](https://openairdocs.org/sdr/UIEA2024061400521.md): Structure · corroded · Jun 24, 2024 · N416MC · Boeing 74747UF · Fuselage Structure (General)
  > CENTER SECTION AFT FACE FOUND CORROSION ( NEAR LH O/J PUMP BONDING AREA)(<P>CENTER SECTION AFT FACE CORROSION REMOVED IAW SRM 51-10-02 AND REPROTECTED IAW SRM 51-20-01 AND MEASURED. REMAIN 0.783" ORG 0.806" WIDTH 1.4, LENGTH 2" WITHIN SRM 57-10-10-1A-2 ALLOWA
- [SDR UIEA2024061400522](https://openairdocs.org/sdr/UIEA2024061400522.md): Structure · corroded · Jun 24, 2024 · N416MC · Boeing 74747UF · Fuselage Main, Structure
  > CENTER SECTION AFT FACE CORROSION ( NEAR RH O/J PUMP BONDING AREA)(<P>CENTER SECTION AFT FACE CORROSION REMOVED IAW SRM 51-10-02 AND REPROTECTED IAW SRM 51-20-01 AND MEASURED: REMAIN 0.755" ORG 0806, WIDTH 1.4" LENGTH 2" WITHIN SRM 57-10-10-1A-2 ALLOWABLE DA
- [SDR UIEA2024061700526](https://openairdocs.org/sdr/UIEA2024061700526.md): Structure · cracked · Jun 24, 2024 · N416MC · Boeing 74747UF · Fuselage Main, Structure
  > BS 2598 LH LOWER INNER CHORD 1EA CRACK FOUND ON FASTENER HOLE 2ND LAYER ( COUNT FROM AFT) AT 2 O'CLOCK POSITION WITH THROUGH THICKNESS CRACK(<P>BS 2598 LH LOWER INNER CHORD 1EA CRACK ON FASTENER HOLE 2ND LAYER ( COUNT FROM AFT) REPAIRED IAW RI-53-00-16937 RE
- [SDR UIEA2024061800535](https://openairdocs.org/sdr/UIEA2024061800535.md): Fairing · delaminated · Jun 24, 2024 · N416MC · Boeing 74747UF · Trailing Edge Flaps
  > LHW O/B MID FLAP L/E FAIRING FOUND DELAMINATION(<P>PERFORMED PERMANENT REPAIR AS PER SRM 51-70-07 PAR 5A. NO FURTHER DEFECTS NOTED.</P>)
- [SDR UIEA2024061800536](https://openairdocs.org/sdr/UIEA2024061800536.md): Fairing · delaminated · Jun 24, 2024 · N416MC · Boeing 74747UF · Trailing Edge Flaps
  > LHW O/B MID FLAP L/E FAIRING FOUND DELAMINATION(<P>PERFORMED PERMANENT REPAIR AS PER SRM 51-70-07 PAR 5A. NO FURTHER DEFECTS NOTED.</P>)
- [SDR UIEA2024061800538](https://openairdocs.org/sdr/UIEA2024061800538.md): Fairing · delaminated · Jun 24, 2024 · N416MC · Boeing 74747UF · Trailing Edge Flaps
  > RHW O/B MID FLAP L/E FAIRING FOUND DELAMINATION(<P><SPAN>PERFORMED PERMANENT REPAIR AS PER SRM 51-70-07 PAR 5A. NO FURTHER DEFECTS NOTED.</SPAN></P>)
- [SDR UIEA2024061800548](https://openairdocs.org/sdr/UIEA2024061800548.md): Frame · unknown · Jun 24, 2024 · N416MC · Boeing 74747UF · Fuselage Main, Frame
  > MAIN DECK BS 2231 FRAME BETWEEN STRINGERS 15 TO 31 INSPECTION THE SCREW CANNOT BE INSTALLED AFTER MOVED DUE TO BRACKET BLOCKED(<P>MAIN DECK BS 2231 FRAME BETWEEN STRINGERS 15 TO 31 SCREW CANNOT BE INSTALLED. CASE REPAIRED IAW RI-53-60-16951 REV A AND SB 747-53
- [SDR UIEA2024061800549](https://openairdocs.org/sdr/UIEA2024061800549.md): Support Rod · damaged · Jun 24, 2024 · N416MC · Boeing 74747UF · Wing, Landing Gear Attach Fittings
  > LH LDG SUPPORT BEAM O/B UPR SUPPORT ROD ( WS 522 AREA) FOUND HOLE ELONGATED(<P>LH LDG SUPPORT BEAM O/B UPR SUPPORT ROD ( WS 522 AREA) ROD FITTING FABRICATED IAW RI-57-22-16946 REV A AND REPLACED IAW SRM 51-10-02 AND INSTALLED IAW SRM 51-40-02 REV 101 DATE 20
- [SDR UIEA2024061900556](https://openairdocs.org/sdr/UIEA2024061900556.md): Skin · chafed · Jun 24, 2024 · N416MC · Boeing 74747UF · Trailing Edge Flaps
  > LHW O/B AFT FLAP UPPER SURFACE O/B AREA FOUND SEVERAL CHAFING MARKS(<P>PERMANENT METAL TO METAL HOTBOND REPAIR AS PER RI NO. RI-57-51-16950 REV.A. NO FURTHER DEFECTS NOTED</P>)
- [SDR UIEA2024062000558](https://openairdocs.org/sdr/UIEA2024062000558.md): Panel · corroded · Jun 24, 2024 · N416MC · Boeing 74747UF · Fuselage Structure (General)
  > M/D BELOW FSK STOWAGE PNL FOUND CORROSION(<P>M/D - BELOW FSK STOWAGE PNL REPAIR IAW FVCI EO - 24090-1, 2A, 3. NO FURTHER DEFECTS NOTED.</P>)
- [SDR UIEA2024022400126](https://openairdocs.org/sdr/UIEA2024022400126.md): Socket · shorted · Feb 24, 2024 · N416MC · Boeing 74747UF · Passenger Compartment Lighting
  > VIA SATCOM, CREW REPORTED INFLIGHT ELECTRICAL ODOR CORRESPONDING TO AN UN-COMMANED ILLUMINATION OF CEILING LIGHT IN THE GALLEY / LAV AREA. CREW REPORTED STRONG ODOR, BUT NOTED NO C/B OPENED.(<P>REMOVED UPPER DECK CEILING LIGHT COVER IAW AMM 33-28-01 AND FOUND
- [SDR UIEA2024012100020](https://openairdocs.org/sdr/UIEA2024012100020.md): Floor Panel · damaged · Jan 24, 2024 · N416MC · Boeing 74747UF · Fuselage Floor Panel
  > M/D STA 1850-1920 LBL 78-99 BALL MAT FLOOR PNL FOUND DAMAGE(<P>THE DAMAGED CASTER PANEL TOP SKIN REPAIR HAS BEEN CARRIED OUT PER EO.4425A500 REV.1</P>)
- [SDR UIEA2023061600647](https://openairdocs.org/sdr/UIEA2023061600647.md): Shutoff Valve · unknown · Jun 16, 2023 · N416MC · Boeing 74747UF · Air Conditioning System
  > ITEM 1: AIR TURNBACK DUE TO COCKPIT AND UPPER DECK TEMPERATURES CONTINUALLY DROPPING. FLT DECK SET AT 29C, FWD DECK SET AT 15C, UPPER DECK 8C & CREW REST AT 3C.(<P>REMOVED AND REPLACED FWD TRIM AIR SHUTOFF VALVE PER AMM 21-28-04, TEST PASSED.</P>)
- [SDR UIEA2022120701206](https://openairdocs.org/sdr/UIEA2022120701206.md): Engine · stalled · Dec 7, 2022 · N416MC · Boeing 74747UF · Turbine Engine Compressor Section
  > NR 2 ENGINE N2 VIBRATION 5.0 AND NR 2 COMPRESSOR STALLED ON CLIMB OUT. R & R NR 2 ENGINE IAW WORD CARD 71-099-02-01. OPS CHECK GOOD</P>)
- [SDR UIEA2022060200568](https://openairdocs.org/sdr/UIEA2022060200568.md): Indicator · fault message · Jun 2, 2022 · N416MC · Boeing 74747UF · Engine (Turbine/Turboprop)
  > ENGINE #2 OIL QUANTITY INDICATED 19 PRIOR TO START, 14 AFTER START, 10 AT THE TOP OF THE CLIMB, AND DECREASED TO 7 BY LANDING AFTER 2:51 FLIGHT TIME. RETURNED TO RKSI WITH ENGINE #2 AT IDLE POWER. REMOVED AND REPLACED WITH NO.2 ENG AND THEN LEAK CHECK NORMAL
- [SDR UIEA2022051700486](https://openairdocs.org/sdr/UIEA2022051700486.md): Plate · migrated · Jun 2, 2022 · N416MC · Boeing 74747UF · Wing Structure
  > R/H W/W STA 1350 WING LANDING GEAR SUPPORT BEAM SPLICE LOWER PLATE AFT I/B CORNER SHIM MIGRATED. SHIM MIGRATION INSPECTION PER SRM 51-20-08, MOUNT BOLT TORQUE CHECK PERFORMED PER SRM 51-40-04-0G-0, EDGE SEALEANT APPLIED PER AMM 51-31-01.
- [SDR UIEA2022052200493](https://openairdocs.org/sdr/UIEA2022052200493.md): Attach Plate · corroded · Jun 2, 2022 · N416MC · Boeing 74747UF · Wing Main, Frame Structure
  > R/H WLG W/W STA 1241 R/H CTR OJ PUMP BONDING ATT SURFACE FOUND CORRODED. CORROSION AREA REMOVED AS PER SRM 51-10-02 AND REPROTECTED AS PER SRM 51-20-01, BLENDED OUT AREA WITHIN SRM 57-10-10-1A-2 ALLOWABLE DAMAGE 2 FIG 101 LIMITS
- [SDR UIEA2022052200494](https://openairdocs.org/sdr/UIEA2022052200494.md): Attach Plate · corroded · Jun 2, 2022 · N416MC · Boeing 74747UF · Wing Structure
  > L/H WLG W/W STA 1241 L/H CTR OJ PUMP BONDING ATT SURFACE FOUND CORRODED. CORROSION AREA REMOVED AS PER SRM 51-10-02 AND REPROTECTED AS PER SRM 51-20-01, BLENDED OUT AREA WITHIN SRM 57-10-10-1A-2 ALLOWABLE DAMAGE 2 FIG 101 LIMITS.
- [SDR UIEA2022052200495](https://openairdocs.org/sdr/UIEA2022052200495.md): Attach Angle · cracked · Jun 2, 2022 · N416MC · Boeing 74747UF · Fuselage Structure (General)
  > M/D RHS STA 960 S-7 FRAME FWD / CREASE BEAM LWR ATT ANGLE CRACKED. LOCAL FABRICATED ANGLE P/N: 65B38488-159 AS PER BOEING DWG: 65B38488 PL AND INSTALLED AS PER SRM 51-40-02 REV 94 DATE 20FEB2022</P>)
- [SDR UIEA2022052200496](https://openairdocs.org/sdr/UIEA2022052200496.md): Skin · cracked · Jun 2, 2022 · N416MC · Boeing 74747UF · Engine Cowling System
  > #4 ENG R/H CORE COWL LWR AREA OF AIR EXHAUST FOUND 2EA BOLT HOLE CRACKED SKIN 2EA BOLT HOLE CRACK AREA REPAIRED AS PER SRM 54-45-01-2R-4 REPAIR 4 FIG 201</P>)
- [SDR UIEA2022052200497](https://openairdocs.org/sdr/UIEA2022052200497.md): Skin · cracked · Jun 2, 2022 · N416MC · Boeing 74747UF · Doors
  > L/H BLG I/B STRUT DOOR SKIN FOUND CRACK. SKIN CRACK AREA REPAIRED AS PER SRM 52-80-01-2R-1 REPAIR 1 FIG 201 REV 94 DATE 20FEB 2022
- [SDR UIEA2022052200498](https://openairdocs.org/sdr/UIEA2022052200498.md): Attach Angle · cracked · Jun 2, 2022 · N416MC · Boeing 74747UF · Fuselage Structure (General)
  > M/D LHS STA 960 S-7 FRAME FWD/ CREASE BEAM LWR ATT ANGLE CRACKED. LOCAL FABRICATED AND P/N NO.65B38488-159 AS PER BOEING DWG: 65B38488 PL AND INSTALLED AS PER SRM 51-40-02</P>)
- [SDR UIEA2022052300499](https://openairdocs.org/sdr/UIEA2022052300499.md): Beam · elongated · Jun 2, 2022 · N416MC · Boeing 74747UF · Fuselage Structure (General)
  > AFT CGO STA 1820-1840 MOST RH HORIZ TORQUE TUBE R/H SUPPORT BEARING ATTACHED BEAM FOUND HOLE ELONGATED. HOLE ELONGATED INTERCOSTAL LOCAL FABRICATED AS PER BOEING DWG: 65B06061 & RPL AND INSTALLED AS PER SRM 51-40-02
- [SDR UIEA2022052300500](https://openairdocs.org/sdr/UIEA2022052300500.md): Panel · cracked · Jun 2, 2022 · N416MC · Boeing 74747UF · Wing Structure
  > LHW TE CAVITY LWR FIXED PANEL CHORD FOUND CRACKED AT WS 1470 CHORD LOCAL FABRICATED AS PER BOEING DWG: 65B08175 AND PART LIST AND CHORD INSTALLED AS PER SRM 51-40-02
- [SDR UIEA2022052300501](https://openairdocs.org/sdr/UIEA2022052300501.md): Curtain · torn · Jun 2, 2022 · N416MC · Boeing 74747UF · Cargo Compartments
  > BULK CARGO STA 2160 CURTAIN FOUND LWR AREA TORN. PERMANENT REPAIR CARRIED OUT AS PER RI-25-54-15628 REV.A</P>)
- [SDR UIEA2022052300502](https://openairdocs.org/sdr/UIEA2022052300502.md): Frame · chipped · Jun 2, 2022 · N416MC · Boeing 74747UF · Powerplant System
  > #3 ENG R/H CORE COWL NO.5 FRAME (COUNT FROM FWD) MID LOW SECTION FOUND CHIPPED. FRAME REPAIRED AS PER SRM 54-45-02-2R-1 REPAIR 1 FIG. 201 REV 94, DATE: 20 FEB 2022</P>)
- [SDR UIEA2022052300503](https://openairdocs.org/sdr/UIEA2022052300503.md): Cowling · gouged · Jun 2, 2022 · N416MC · Boeing 74747UF · Powerplant System
  > #3 ENG R/H CORE COWL MOST AFT FRAME MID LOW SECTION FOUND GOUGE MARK(FRAME REPAIRED AS PER SRM 54-45-02-2R-2 REPAIR 2 FIG.201 REV.94 DATE: 20 FEB 2022</P>)
- [SDR UIEA2022052300504](https://openairdocs.org/sdr/UIEA2022052300504.md): Frame · chipped · Jun 2, 2022 · N416MC · Boeing 74747UF · Powerplant System
  > #4 ENG L/H CORE COWL #2 FRAME (COUNT FROM FWD) MID LOW SECTION FOUND CHIPPED (UNDER AREA OF HOLD OPEN ROD) FRAME REPAIRED AS PER SRM 54-45-02-2R-1 REPAIR 1 FIG.201 REV 94, DATE 20 FEB 2022
- [SDR UIEA2022052300528](https://openairdocs.org/sdr/UIEA2022052300528.md): Flap · chafed · Jun 2, 2022 · N416MC · Boeing 74747UF · Wing Structure
  > LHW O/B FORE FLAP T/E UPR SURFACE O/B AREA FOUND CHAFING AS MARKED (3" TO O/B). PERFORMED COMPOSITE HOTBOND REPAIR AS PER SRM 51-70-07 PAR.5.A REV94,FEB 20/2022</P>)
- [SDR UIEA2022052400529](https://openairdocs.org/sdr/UIEA2022052400529.md): Flap · delaminated · Jun 2, 2022 · N416MC · Boeing 74747UF · Wing Structure
  > LHW O/B FORE FLAP L/E FOUND DELAMINATION (125" TO I/B)(<P>PERFORMED COMPOSITE HOTBOND REPAIR AS PER SRM 51-70-07 PAR.5.A REV94,FEB20/2022</P>)
- [SDR UIEA2022052400530](https://openairdocs.org/sdr/UIEA2022052400530.md): Flap · delaminated · Jun 2, 2022 · N416MC · Boeing 74747UF · Wing Structure
  > LHW O/B FORE FLAP L/E FOUND DELAMINATION (22" TO O/B). PERFORMED COMPOSITE HOTBOND REPAIR AS PER SRM 51-70-07 PAR.5.A REV94,FEB20/2022</P>)
- [SDR UIEA2022052400531](https://openairdocs.org/sdr/UIEA2022052400531.md): Flap · delaminated · Jun 2, 2022 · N416MC · Boeing 74747UF · Wing Structure
  > LHW O/B FORE FLAP L/E FOUND DELAMINATION (145" TO I/B). PERFORMED COMPOSITE HOTBOND REPAIR AS PER SRM 51-70-07 PAR.5.A REV94,FEB20/2022</P>)

Next page: https://openairdocs.org/aircraft/N416MC/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 = 'N416MC' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N416MC/reports

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