# Service difficulty reports: N445MC

A list on [N445MC](https://openairdocs.org/aircraft/N445MC.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 2 · 73 reports

- [SDR UIEA2026053000371](https://openairdocs.org/sdr/UIEA2026053000371.md): Fmu · faulted · May 29, 2026 · N445MC · Boeing 7474B5F · Fuel Controlling System
  > ENG 2 DUE TO ABNORMAL INDICATIONS AND UNRESPONSIVE THRUST LEVER. (ENG 2 WAS SHUT DOWN IN FLIGHT) R & R NR 2 ENG FMU PER AMM 73-21-01-401 AND IPC 73-21-01-05. OPS CHECK GOOD. NO LEAK NOTED. FOLLOWED FIM 71-00-00-104B)
- [SDR UIEA2025091801240](https://openairdocs.org/sdr/UIEA2025091801240.md): Windshield · failed · Sep 18, 2025 · N445MC · Boeing 7474B5F · Flight Compartment Windows
  > RIGHT FORWARD OUTER WINDSHIELD BROKE. R & R RIGHT FORWARD WINDSHIELD ASSY IAW AMM 56-11-00. OPS CHK OK.
- [SDR UIEA2025071300946](https://openairdocs.org/sdr/UIEA2025071300946.md): B-Nut · loose · Jul 13, 2025 · N445MC · Boeing 7474B5F · Turbine Engine Oil System
  > DURING FLIGHT, #2 OIL QUANTITY FELL TO 0, NO OTHER ABNORMAL INDICATIONS WERE NOTED AT THE TIME. ABOUT 2 HRS LATER, OIL PRESS BEGAN TO DECREASE, #2 ENG SHUTDOWN DUE TO "ENG 2 OIL PRESS" EICAS MSG WHEN THROTTLES WENT TO IDLE AT DESCENT. OIL PRESS DROPPED TO NEAR
- [SDR UIEA2025070600836](https://openairdocs.org/sdr/UIEA2025070600836.md): Skin · delaminated · Jul 12, 2025 · N445MC · Boeing 7474B5F · Wing, Plate/Skin
  > RHW I/B FORE FLAP L/E MID AND O/B AREA FOUND DELAMINATED.(<P>PERFORMED PERMANENT COMPOSITE REPAIR AS PER SRM 51-70-07, PAR.5.A.(1). NO FURTHER DEFECTS NOTED.</P>)
- [SDR UIEA2025070600837](https://openairdocs.org/sdr/UIEA2025070600837.md): Skin · delaminated · Jul 12, 2025 · N445MC · Boeing 7474B5F · Wing, Plate/Skin
  > LHW I/B MID FLAP L/E MOST I/B AREA FOUND DELAMINATED.(<P>PERFORMED PERMANENT COMPOSITE REPAIR AS PER SRM 51-70-07, PAR.5.A.(1). NO FURTHER DEFECTS NOTED.</P>)
- [SDR UIEA2025070600838](https://openairdocs.org/sdr/UIEA2025070600838.md): Skin · delaminated · Jul 12, 2025 · N445MC · Boeing 7474B5F · Wing, Plate/Skin
  > LHW I/B FORE FLAP O/B OF MID FORE FLAP TRACK APPROX 9" L/E AREA FOUND DELAMINATED.(<P>PERFORMED PERMANENT COMPOSITE REPAIR AS PER SRM 51-70-07, PAR.5.A.(1). NO FURTHER DEFECTS NOTED.</P>)
- [SDR UIEA2025070600839](https://openairdocs.org/sdr/UIEA2025070600839.md): Skin · delaminated · Jul 12, 2025 · N445MC · Boeing 7474B5F · Wing, Plate/Skin
  > LHW I/B FORE FLAP L/E MOST I/B AREA FOUND DELAMINATED.(<P>PERFORMED PERMANENT COMPOSITE REPAIR AS PER SRM 51-70-07, PAR.5.A.(1). NO FURTHER DEFECTS NOTED.</P>)
- [SDR UIEA2025070600840](https://openairdocs.org/sdr/UIEA2025070600840.md): Skin · delaminated · Jul 12, 2025 · N445MC · Boeing 7474B5F · Wing, Plate/Skin
  > LHW I/B FORE FLAP I/B OF FORE FLAP TRACK CUTOUT FOUND DELAMINATED.(<P>PERFORMED PERMANENT COMPOSITE REPAIR AS PER SRM 51-70-07, PAR.5.A.(1). NO FURTHER DEFECTS NOTED.</P>)
- [SDR UIEA2025070600843](https://openairdocs.org/sdr/UIEA2025070600843.md): Brace · chafed · Jul 12, 2025 · N445MC · Boeing 7474B5F · Nacelle/Pylon Miscellaneous Structure
  > NO.1 PYLON DIAGONAL BRACE RH BELOW HYD DEPRESSURIZATION MODULE FOUND CHAFING.(<P>#1 PYLON DIAGONAL BRACE CHAFING AREA SMOOTHED AS PER RI-54-50-17750 REV.A. (AFTER SMOOTH OUT AREA MEASURED: L=2", W=1.25" & D=0.125"). NO FURTHER DEFECTS NOTED.</P>)
- [SDR UIEA2025070700853](https://openairdocs.org/sdr/UIEA2025070700853.md): Fairing · delaminated · Jul 12, 2025 · N445MC · Boeing 7474B5F · Vertical Stabilizer
  > DORSAL FAIRING FOUND DELAMINATED.(<P>PERFORMED REPAIR AT DELAMINATION AREA IAW RI-55-30-17752 REV.A. NO FURTHER DEFECTS NOTED.</P>)
- [SDR UIEA2025070900876](https://openairdocs.org/sdr/UIEA2025070900876.md): Channel · cracked · Jul 12, 2025 · N445MC · Boeing 7474B5F · Horizontal Stabilizer Structure
  > LH HORIZONTAL STABILIZER TIP FAIRING AFT SUPPORT U CHANNEL FOUND CRACKED.(<P>LH HORIZONTAL STABILIZER TIP FAIRING T/E WEDGE U CHANNEL REPLACED AS PER RI-55-10-17767 REV A. NO FURTHER DEFECTS NOTED.</P>)
- [SDR UIEA2025070900877](https://openairdocs.org/sdr/UIEA2025070900877.md): Door · chafed · Jul 12, 2025 · N445MC · Boeing 7474B5F · Nacelle/Pylon, Main Frame
  > #2 PYLON LH AFT FAIRING DOOR FOUND CHAFFING.(<P>PERFORMED REPAIR AT CHAFFING AREA IAW <SPAN>RI-54-50-17761, REV. A. NO FURTHER DEFECTS NOTED.</SPAN></P>)
- [SDR UIEA2025070900882](https://openairdocs.org/sdr/UIEA2025070900882.md): Skin · dented · Jul 12, 2025 · N445MC · Boeing 7474B5F · Fuselage Main, Plate/Skin
  > FX STA 520-540 R/H S43R - S44R SKIN FOUND DENT.(<P>FX STA 520-540 R/H S43R-S44R SKIN DENT AREA REPAIRED AS PER SRM 53-00-01-2R-1 REQ 104. NO FURTHER DEFECTS NOTED.</P>)
- [SDR UIEA2025071000889](https://openairdocs.org/sdr/UIEA2025071000889.md): Stiffener · cracked · Jul 12, 2025 · N445MC · Boeing 7474B5F · Wing Main, Frame Structure
  > LHW L/E LOWER CENTER ZEE STIFFENER FOUND CRACKED.(<P>LHW L/E LOWER CENTER ZEE STIFFENER REPLACED AS PER RI-57-26-17755 REV A. NO FURTHER DEFECTS NOTED.</P>)
- [SDR UIEA2025071000890](https://openairdocs.org/sdr/UIEA2025071000890.md): Panel · cracked · Jul 12, 2025 · N445MC · Boeing 7474B5F · Nacelle/Pylon, Plate/Skin
  > NO.4 PYLON O/B #482KR PANEL FOUND CRACKED.(<P>NO.4 PYLON O/B #482KR PANEL REPLACED AS PER RI-54-50-17765 REV A. NO FURTHER DEFECTS NOTED.</P>)
- [SDR UIEA2025071000891](https://openairdocs.org/sdr/UIEA2025071000891.md): Beam · damaged · Jul 12, 2025 · N445MC · Boeing 7474B5F · Nacelle/Pylon, Main Frame
  > NO.4 PYLON AFT FAIRING AREA APPROX WAC STA 415 UPPER BEAM RH FASTENER HOLE FOUND ELONGATED(<P>OVERSIZE FASTENER HOLE AND INSTALL FREEZE PLUG PER RI-54-50-17760 REV A. NO FURTHER DEFECTS NOTED.</P>)
- [SDR UIEA2025071000892](https://openairdocs.org/sdr/UIEA2025071000892.md): Rib · cracked · Jul 12, 2025 · N445MC · Boeing 7474B5F · Wing, Rib/Bulkhead
  > LHW L/E #581HB PANEL RIB FOUND CRACKED.(<P>LHW L/E #581HB PANEL RIB REPLACED AS PER RI-57-51-17762 REV A. NO FURTHER DEFECTS NOTED.</P>)
- [SDR UIEA2025071000894](https://openairdocs.org/sdr/UIEA2025071000894.md): Rib · cracked · Jul 12, 2025 · N445MC · Boeing 7474B5F · Wing, Rib/Bulkhead
  > LHW L/E #581JB PANEL RIB FOUND CRACKED.(<P>LHW L/E #581JB PANEL RIB REPLACED AS PER RI-57-51-17769 REV A. NO FURTHER DEFECTS NOTED.</P>)
- [SDR UIEA2025071200937](https://openairdocs.org/sdr/UIEA2025071200937.md): Fuel Tank · corroded · Jul 12, 2025 · N445MC · Boeing 7474B5F · Fuel Storage
  > LWLG W/W CENTER TANK AFT B/H FUEL BONDING ATTACH AREA SURFACE CORROSION.(<P><SPAN>LWLG W/W CENTER TANK AFT B/H FUEL BONDING AREA </SPAN>CORROSION REMOVED AS PER SRM 51-10-02 AND REPROTECTED AS PER SRM 51-20-01. WITHIN ALLOWABLE DAMAGE LIMITS IAW SRM 57-10-10 A
- [SDR UIEA2025032500388](https://openairdocs.org/sdr/UIEA2025032500388.md): Wire · damaged · Mar 25, 2025 · N445MC · Boeing 7474B5F · Hydraulic Power System Wiring
  > HYD CONTROL 4 ADVISORY MSG IN FLIGHT. CHECKLIST C/W. AIR TURNBACK TO KMIA.(<P>REPLACED WIRE W4261-434-24R AND 24B PER WDM 29-30-11 AND SWPM 20-10-13. TEST GOOD PER AMM 29-31-00.</P>)
- [SDR UIEA2025021600149](https://openairdocs.org/sdr/UIEA2025021600149.md): Pcu · faulted · Feb 16, 2025 · N445MC · Boeing 7474B5F · Aileron Control System
  > RT INBOARD AILERON INDICATION MISSING. FLT CONTROL HYD POWER WING SHUTOFF SWITCHES SELECTED TO CLOSED ON P61 PANEL.(<P>1.PARTIALLY REMOVED INBD ALERON POWER CONT PACKAGE PER AMM 27-11-12-002-001 STEP F(1)(I). ACCOMPLISHED REMOVAL OF INBD AILERON AS PER AMM 2
- [SDR UIEA2024041000268](https://openairdocs.org/sdr/UIEA2024041000268.md): Roller Cam · unknown · Apr 10, 2024 · N445MC · Boeing 7474B5F · Passenger/Crew Doors
  > AFTER TAKE OFF AT 2500 FT, DOOR ENTRY L1 EICAS MESSAGE. ACFT PRESSURIZING NORMALLY. 2 VERY LOUD BANGS, SHOOK FLIGHT DECK DOOR. FOUND L1 DOOR UPPER FWD & AFT CRANK ROLLER CAM ASSY BROKEN. CRANK ROLLER CAM ASSY REPLACED. L1 DOOR FUNCTION CHK GOOD IAW AMM 52-1
- [SDR UIEA2023071000735](https://openairdocs.org/sdr/UIEA2023071000735.md): Unknown · unknown · Jul 5, 2023 · N445MC · Boeing 7474B5F · Fuselage Structure (General)
  > CRACK DAMAGE ON THE WEB OF STA 2231 FRAME AT S-21L AND S-22L(<P>1. REMOVED AFFECTED FASTENERS TO GET ACCESS IAW SRM 51-40-02-06-0. REV 97. 2. REPAIRED DAMAGE AREA IAW SRM 53-60-15-2R-3 REPAIR 3 FIG 203 PARAGRAPH 5 REV 97. 3. INSTALLED FASTENERS IAW SRM 57-40-0
- [SDR UIEA2023071000736](https://openairdocs.org/sdr/UIEA2023071000736.md): Unknown · unknown · Jul 5, 2023 · N445MC · Boeing 7474B5F · Fuselage Structure (General)
  > REPAIR - SKIN MODIFICATION FOR STATION 1640 TO 1740 LEFT SIDE AT STRINGER 34 PER SB 747-53A2487(<P>1. ACCOMPLISHED JOB IAW EI T2023A53M-1374 REV 1. 2. ACCOMPLISHED EI 72023A53M-1374 REV 2. 3. JOB ACCOMPLISHED AND COND CHK NORMAL.</P>)
- [SDR UIEA2023071000737](https://openairdocs.org/sdr/UIEA2023071000737.md): Unknown · unknown · Jul 5, 2023 · N445MC · Boeing 7474B5F · Fuselage Structure (General)
  > CRACK ON FASTENER HOLE OF TENSION TIE AFT CHANNEL AT STA 740 RH SIDE(<P>1. REMOVED AFFECTED FASTENER TO GET ACCESS IAW 51-40-02-0G-0. REV 97. 2. PERFORM EI T2023A53M-1451 REV 0 SEQUENCE A. 3. REINSTALL FASTENERS IAW SRM 51-40-02-0G-0. REV 97 AND DWG 14241023 S
- [SDR UIEA2023071000738](https://openairdocs.org/sdr/UIEA2023071000738.md): Unknown · unknown · Jul 5, 2023 · N445MC · Boeing 7474B5F · Fuselage Structure (General)
  > CRACK ON FASTENER HOLE OF TENSION TIE AFT CHANNEL STA 760 RH SIDE(<P>1. REMOVED AFFECTED FASTENERS TO GET ACCESS IAW SRM 51-40-02-0G-0, REV 97. 2. PERFORM EI T2023A53M-1450, REV 0 SEQUENCE A. 3. REINSTALL FASTENERS IAW SRM 51-40-02-0G-0, REV 97 AND DWG 1424102
- [SDR UIEA2023071000739](https://openairdocs.org/sdr/UIEA2023071000739.md): Unknown · unknown · Jul 5, 2023 · N445MC · Boeing 7474B5F · Fuselage Structure (General)
  > FWD FLOOR STRUCTURE SUBSTITUTE TRACK CRACK AT M/D STA 980 LBL 75.92(<P>1. REMOVED FASTENERS IAW SRM 51-40-02-0G-0 REV97. 2. REPAIR SUBSTITUTE TRACK IAW SRM 53-00-52-2R-13. REPAIR 13 REV 97. 3. INSTALL REPAIR PARTS IAW SRM 53-00-52-2R-13. REPAIR 13 REV 97 AND D
- [SDR UIEA2023071000740](https://openairdocs.org/sdr/UIEA2023071000740.md): Unknown · unknown · Jul 5, 2023 · N445MC · Boeing 7474B5F · Fuselage Structure (General)
  > DUE TO EO INSP WASHERS WERE NOT FOUND UNDER EACH FASTENER HEAD. REQUEST ADD EO PART 2 AND PART 5. PERFORMED NOSE WW FWD CORNER DOUBLER MODIFICATION NEAR STA 240, S-39 TO S-45(<P>1. PERFORM EI T2023A53M-1504 SEQUENCE A REV 0. 2. ACCOMPLISHED REPAIR AREA IAW EI
- [SDR UIEA2023071000741](https://openairdocs.org/sdr/UIEA2023071000741.md): Unknown · unknown · Jul 5, 2023 · N445MC · Boeing 7474B5F · Fuselage Structure (General)
  > FOUND FLOOR STRUCTURE SUBSTITUTE TRACK CRACK AT M/D STA 1540 RBL 75.92(<P>1. REMOVED FASTENERS IAW SRM 51-40-02-0G-0 REV 98. 2. REPAIR TRACK IAW SRM 53-00-52-2R-13 REPAIR 13 REV 98. 3. INSTALL REPAIR PARTS IAW SRM 53-00-52-2R-13 REPAIR 13 REV 98 AND DWG 65B382
- [SDR UIEA2023071000742](https://openairdocs.org/sdr/UIEA2023071000742.md): Unknown · unknown · Jul 5, 2023 · N445MC · Boeing 7474B5F · Escape Slide
  > FOUND FLOOR STRUCTURE SUBSTITUTE TRACK CRACK AT M/D STA1641 LBL 75.92(<P>1. REMOVED FASTENERS IAW SRM 51-40-02-0G-0 REV 98. 2. REPAIR TRACK IAW SRM 53-00-52-2R-13 REPAIR 13 REV 98. 3. INSTALL REPAIR PARTS IAW SRM 53-00-52-2R-13 REPAIR 13 REV 98 AND DWG 65B3825
- [SDR UIEA2023071000743](https://openairdocs.org/sdr/UIEA2023071000743.md): Unknown · unknown · Jul 5, 2023 · N445MC · Boeing 7474B5F · Wing Structure
  > GOUGE DAMAGE ON RH WING LOWER SKIN PANEL NO.2 BETWEEN STRINGER L-8 AND L-9 AT WBL 743.828(<P>1. ACCOMPLISHED EI T2023A57M-1479. SEQUENCE B REV 1. 2. ACCOMPLISHED EI T2023A57M-1479, REV 2. 3. JOB COMPLETED AND COND CHK NORMAL.</P>)
- [SDR UIEA2023071000744](https://openairdocs.org/sdr/UIEA2023071000744.md): Shear Tie · unknown · Jul 5, 2023 · N445MC · Boeing 7474B5F · Fuselage Structure (General)
  > CRACK ON THE SHEAR TIE AT 1000 LBL 33.99 SB 747-53A2904(<P>1. REMOVED DAMAGE PART IAW SRM 51-40-02-0G-0 REV 97. 2. ACCOMPLISHED EI T2023A53M-1550 REV 0 AND SB 747-53A2904 FIG 8 & 9 REV 0 AND IAW EO 4453C024 PART 4 REV 3. 3. ACCOMPLISHED EI NO T2023A53M.1550 RE
- [SDR UIEA2023071000745](https://openairdocs.org/sdr/UIEA2023071000745.md): Shear Tie · unknown · Jul 5, 2023 · N445MC · Boeing 7474B5F · Fuselage Structure (General)
  > CRACK ON THE SHEAR TIE AT STA 1000 RBL 33.99 SB 747 53A2904(<P>1. REMOVED DAMAGE PART IAW SRM 51.40.02.0G.0 REV 97. ACCOMPLISHED EI T2023A53M-1550 REV 0, SB 747-53A2924 FIG 21, 22 REV0 AND EI ATTACHED TO W/O 8402500 (319) AND IAW EO 4453C024 PART 8 REV 3. 3. J
- [SDR UIEA2023071000746](https://openairdocs.org/sdr/UIEA2023071000746.md): Fitting · unknown · Jul 5, 2023 · N445MC · Boeing 7474B5F · Fuselage Structure (General)
  > CRACK ON THE INTERCOSTAL LUG FITTING AT STA 1000 RBL 11.33, SB 747-53A2904(<P>1. REMOVED DAMAGE PART IAW SRM 51-40-02-0G-0 REV 97. 2. ACCOMPLISHED EI NO T2023A53M-1550 REV 0 AND SB 747-53A2904 FIG 17 & 18 REV 0 AND EI ATTACHED TO W/O 8402504 (319) AND EO 4453C
- [SDR UIEA2023071000747](https://openairdocs.org/sdr/UIEA2023071000747.md): Cap · unknown · Jul 5, 2023 · N445MC · Boeing 7474B5F · Fuselage Structure (General)
  > CORROSION - FOUND MAIN DECK CGO FLOOR BEAM CAP CORROSION STA 2360 RBL 3.(<P>1. REMOVED DAMAGE PARTS IAW 51-40-02-0G-0 REV98. 2. INSTALL NEW PARTS IAW SRM 51-40-02-0G-0 REV98 AND BOEING DWG NO. 65B02634 SH 22 REV 4 AND DNG NO 65B06161 SH2 REV E, DWG NO. 65B3875
- [SDR UIEA2023071000748](https://openairdocs.org/sdr/UIEA2023071000748.md): Fitting · unknown · Jul 5, 2023 · N445MC · Boeing 7474B5F · Fuselage Structure (General)
  > CORROSION - 2EA CGO TRACK CORROSION AT R/H STA 2360 MAIN DECK FLOOR(<P>1. IAW AMM SUBTASK 53-44-00-212-001, REV107 REMOVE CGO TRACK 2. IAW AMM SUBTASK 53-44-00-020-001 REV 107 AND REFRENCE EI T2023A53M-1566, REV 0. INSTALL CGO TRACK. 3. JOB COMPLETED AND COND
- [SDR UIEA2023071000749](https://openairdocs.org/sdr/UIEA2023071000749.md): Unknown · unknown · Jul 5, 2023 · N445MC · Boeing 7474B5F · Trailing Edge Flaps
  > FOUND #1 FLAP TRACK INBD SIDE LOAD FITTING CONTACT SURFACE CORROSION AND BUSHING MIGRATION(<P>1. IAW AMM 20-51-01-912-008, REV 107 R/R #1 FLAP TRACK INBD SIDE LOAD FIG. 2. REFRENCE EI NO. T2023A57M-1497 REV 1 SEQUENCE A REPAIR #1 FLAP TRACK. 3. CONDITION CHECK
- [SDR UIEA2023071000750](https://openairdocs.org/sdr/UIEA2023071000750.md): Unknown · unknown · Jul 5, 2023 · N445MC · Boeing 7474B5F · Trailing Edge Flaps
  > FOUND #8 FLAP TRACK INBD SIDE LOAD FITTING CONTACT SURFACE CORROSION AND BUSHING MIGRATION(<P>1. IAW AMM 20-51-01-912-008 REV107 R/R #8 FLAP TRACK INBD SIDE LOAD PLATE. 2. REFRENCE EI. NO: T2023A57M-1501 REV1 SEQUENCE A REPAIR #8 FLAP TRACK. 3. CONDITION CHECK
- [SDR UIEA2023071000751](https://openairdocs.org/sdr/UIEA2023071000751.md): Unknown · unknown · Jul 5, 2023 · N445MC · Boeing 7474B5F · Trailing Edge Flaps
  > FOUND #3Â FLAP TRACK INBD SIDE LOAD FIG CONTACT SURFACE CORROSION AND BUSHING MIGRATION(<P>1. IAW AMM 20-51-01-912-008 REV107 R/R #3 FLAP TRACK INBD SIDE LOAD PLATE. 2. REFRENCE EI NO. T2023A57M-1498 REV1 SEQUENCE A REPAIR #3 FLAP TRACK. 3. CONDITION CHK NORM
- [SDR UIEA2023071000752](https://openairdocs.org/sdr/UIEA2023071000752.md): Unknown · unknown · Jul 5, 2023 · N445MC · Boeing 7474B5F · Trailing Edge Flaps
  > FOUND #6 FLAP TRACK INBD SIDE LOAD FIG CONTACT SURFACE CORROSION AND BUSHING MIGRATION(<P>1. IAW AMM 20-51-01-912-008, REV107 R/R #6 FLAP TRACK INBD SIDE LOAD PLATE. 2. REFERENCE EI NO. T2023A57M-1499 REV1 SEQUENCE A REPAIR #6 FLAP TRACK. 3. CONDITION CHECK NO
- [SDR UIEA2023071000753](https://openairdocs.org/sdr/UIEA2023071000753.md): Unknown · unknown · Jul 5, 2023 · N445MC · Boeing 7474B5F · Trailing Edge Flaps
  > FOUND #7 FLAP TRACK INBD SIDE LOAD FITTING CONTACT SURFACE CORROSION AND BUSHING MIGRATION(<P>1. IAW AMM 20-51-01-912-008 REV107 R/R #7 FLAP TRACK INBD SIDE LOAD PLATE. 2. REFERENCE EI NO. T2023A57M-1500 REV1 SEQUENCE A REPAIR NO.7 FLAP TRACK. 3. CONDITION CHE
- [SDR UIEA2023071000754](https://openairdocs.org/sdr/UIEA2023071000754.md): Charger · unknown · Jul 5, 2023 · N445MC · Boeing 7474B5F · Emergency Lighting
  > FOUND EMERGENCY LIGHT BATTERY PACK (MJ120) FUNCTION FAIL.(<P>1. IAW AMM 33-51-04-002-009-001 & 33-51-04-402-012-001 REV.107. REPLACED POWER SUPPLY (MJ170). 2. IAW AMM 33-51-04-402-012-001 REV 107. PERFORMED EMERGENCY LIGHT POWER. SUPPLY INSTALLATION TEST AND T
- [SDR UIEA2023081500777](https://openairdocs.org/sdr/UIEA2023081500777.md): Window · unknown · Jun 14, 2023 · N445MC · Boeing 7474B5 · Flight Compartment Windows
  > CAPT SIDE REAR MOST WINDOW SQUEALING AND VIBRATING(<P>R/R WINDOW PER AMM 56-11-02. OPS CHK GOOD.</P>)
- [SDR UIEA2022053000559](https://openairdocs.org/sdr/UIEA2022053000559.md): Fmu · failed · May 30, 2022 · N445MC · Boeing 7474B5F · Fuel Control/Turbine Engines
  > REJECTED TAKEOFF. AIRCRAFT DID NOT MAKE TAKEOFF POWER. REMOVED AND REPLACED FMU, FUEL BOOST PUMP AND VSV ACTUATOR.
- [SDR UIEA2022041700309](https://openairdocs.org/sdr/UIEA2022041700309.md): None · none · Apr 17, 2022 · N445MC · Boeing 747 · Ice/Rain Protection System
  > ON DESCENT, LOUD ELECTRICAL BUZZ BEHIND CAPTAIN LEFT SIDE FOLLOWED BY STRONG ELECTRICAL SMELL. POWER 2L WINDOW HEAT CIRCUIT BREAKER POPPED.(<P ><SPAN>REMOVED #2L WINDOW LINING. NO BURNING WIRES FOUND. FOUND MAINTENANCE MESSAGE 30120. FOLLOWED FIM 30-41 T818. R
- [SDR UIEA2022040700264](https://openairdocs.org/sdr/UIEA2022040700264.md): Skin · damaged · Apr 7, 2022 · N445MC · Boeing 7474B5F · Fuselage Structure (General)
  > R/H UPPER AFT FUSELAGE ABOVE RH ELEVATOR SECTION 48 APROXIMATE B.S. 258/ HAS HOLE IN SKIN WITH CRACKS.(<P><SPAN>REMOVED DAMAGED SKIN SECTION FROM STRINGER 11 RIGHT FROM FWD END AT STA 2638 FROM AFT END AT STA 2658 AND CUT SKIN BETWEEN STRING
- [SDR UIEA2022021700146](https://openairdocs.org/sdr/UIEA2022021700146.md): Module · none · Feb 17, 2022 · N445MC · Boeing 7474B5F · Landing Gear System
  > AIRCRAFT COMPLETED AIR TURN BACK AND RETURNED TO THE FIELD DUE TO GEAR MONITOR WARNING(<P ><SPAN>REPLACED PSEU MODULE IAW AMM 32-09-03. OPS CHECK GOOD.</SPAN></P> / <P> </P>)
- [SDR UIEA2021082301835](https://openairdocs.org/sdr/UIEA2021082301835.md): Access Door · punctured · Aug 26, 2021 · N445MC · Boeing 7474B5F · Fuselage Main, Plate/Skin
  > FUS - ACCESS DOOR 192AR INT. SURFACE FOUND PUNCTURE(<P>CARRIED OUT PERMANENT COMPOSITE HOTBOND REPAIR AS PER SRM 51-70-08 PAR 5A </P>)
- [SDR UIEA2021082301836](https://openairdocs.org/sdr/UIEA2021082301836.md): Access Door · delaminated · Aug 26, 2021 · N445MC · Boeing 7474B5F · Fuselage Main, Plate/Skin
  > FUS - ACCESS DOOR 191EL EXT SURFACE DELAM(<P><SPAN>CARRIED OUT PERMANENT COMPOSITE HOTBOND REPAIR AS PER SRM 51-70-08 PAR 5A </SPAN></P>)
- [SDR UIEA2021082301837](https://openairdocs.org/sdr/UIEA2021082301837.md): Access Door · delaminated · Aug 26, 2021 · N445MC · Boeing 7474B5F · Fuselage Main, Plate/Skin
  > FUS - ACCESS DOOR 192ER EXT SURFACE DELAM(<P><SPAN>CARRIED OUT PERMANENT COMPOSITE HOTBOND REPAIR AS PER SRM 51-70-08 PAR 5A </SPAN></P>)

Next page: https://openairdocs.org/aircraft/N445MC/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 = 'N445MC' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N445MC/reports

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