# N445MC: 2003 Boeing 747-4B5F - Status: Valid registration - Airframe: [Boeing 747-4B5F](https://openairdocs.org/model/boeing-747-4b5f) (registry code 13848BH, 490 seats) - Engine: [Pratt & Whitney PW4062A](https://openairdocs.org/engine/pratt-whitney-pw4062a) (registry code 51675) - Data sheets: [TCDS E24NE](https://openairdocs.org/tcds/E24NE) (Pratt & Whitney Division) (OpenAirDocs) - Serial number: 33515 - Year built: 2003 - Type: Fixed wing multi engine - Engine type: Turbo-fan - Airworthiness: Standard, transport - Airworthiness date: September 28, 2017 - Certificate issued: August 2, 2021 - Expires: August 31, 2028 - Mode S code: A55E46 - Registered owner: [Atlas Air Inc](https://openairdocs.org/faa-owner/ATLAS%20AIR%20INC) - Location: [Purchase, NY](https://openairdocs.org/faa-place/NY/Purchase) - Owner type: Corporation - Owner's area on the map: 41.0382° N, 73.7107° W: Placed by OpenAirDocs at the center of ZIP code 10577, within about a mile (OpenAirDocs). The owner's mailing address, not where the aircraft is based - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=445MC - Page: https://openairdocs.org/aircraft/N445MC From the FAA registry file of October 24, 2026. ADs below are matched by the registry's airframe and engine model codes. They may apply; each AD's applicability can narrow it by serial number, part number or installed equipment. This is not a compliance determination. ## ADs that may apply (OpenAirDocs): 15 in force ### Matched by airframe (Boeing 747-4B5F) None in force. ### Matched by engine (Pratt & Whitney PW4062A) - [AD 2026-21-06](https://openairdocs.org/ad/2026-21-06): Engine Fuel and Control · Pratt & Whitney Division PW4052, PW4056, PW4060 and 10 more. Effective Nov 23, 2026 - [AD 2018-13-02](https://openairdocs.org/ad/2018-13-02): Turbine Engine Combustion Section · Pratt & Whitney Division PW4052, PW4056, PW4060 and 7 more. Effective Jul 20, 2018 - [AD 2016-08-09](https://openairdocs.org/ad/2016-08-09): HPC 10th stage disk · Pratt & Whitney Division PW4050, PW4052, PW4056 and 24 more. Effective Jun 1, 2016 - [AD 2015-22-03](https://openairdocs.org/ad/2015-22-03): LPT 4th stage IAS · Pratt & Whitney Division PW4050, PW4052, PW4056 and 24 more. Effective Dec 1, 2015 - [AD 2012-22-16](https://openairdocs.org/ad/2012-22-16): 3rd stage LPT duct segments · Pratt & Whitney Division PW4050, PW4052, PW4056 and 13 more. Effective Dec 19, 2012 - [AD 2012-14-09](https://openairdocs.org/ad/2012-14-09): 3rd and 4th stage vane fractures · Pratt & Whitney Division PW4050, PW4052, PW4056 and 24 more. Effective Nov 7, 2012 - [AD 2012-18-17](https://openairdocs.org/ad/2012-18-17): HPC drum rotor disk assembly · Pratt & Whitney Division PW4052, PW4056, PW4060 and 16 more. Effective Oct 22, 2012 - [AD 2012-18-03](https://openairdocs.org/ad/2012-18-03): 1st stage HPT air seal rings · Pratt & Whitney Division PW4050, PW4052, PW4056 and 18 more. Effective Oct 11, 2012 - [AD 2012-16-01](https://openairdocs.org/ad/2012-16-01): High-pressure turbine (HPT) stage 1 front hubs · Pratt & Whitney Division PW4052, PW4056, PW4060 and 14 more. Effective Sep 28, 2012 - [AD 2012-06-18](https://openairdocs.org/ad/2012-06-18): Engine · Pratt & Whitney Division PW4050, PW4052, PW4056 and 13 more. Effective Apr 27, 2012 - [AD 2012-04-04](https://openairdocs.org/ad/2012-04-04): fuel metering units (FMUs) · Pratt & Whitney Division PW4050, PW4052, PW4056 and 13 more. Effective Apr 5, 2012 - [AD 2011-25-09](https://openairdocs.org/ad/2011-25-09): PW4000 turbofan engines · Pratt & Whitney Division PW4050, PW4052, PW4056 and 18 more. Effective Jan 10, 2012 - [AD 2010-24-14](https://openairdocs.org/ad/2010-24-14): HPC 10th stage disk · Pratt & Whitney Division PW4050, PW4052, PW4056 and 17 more. Effective Jan 21, 2011 - [AD 2010-24-09](https://openairdocs.org/ad/2010-24-09): No. 3 bearing oil pressure tubes · Pratt & Whitney Division PW4050, PW4052, PW4056 and 34 more. Effective Dec 28, 2010 - [AD 2005-25-09](https://openairdocs.org/ad/2005-25-09): Engine manufacturer's time limits section (TLS) · Pratt & Whitney Division PW4050, PW4052, PW4056 and 26 more. Effective Jun 12, 2006 ### Historical (superseded or no longer in force) - [AD 2010-18-13](https://openairdocs.org/ad/2010-18-13) (historical): Blade · Pratt & Whitney Division PW4052, PW4056, PW4060 and 16 more. Effective Oct 18, 2010 ## Information bulletins (advisory) (5 in force) - [SAIB 2025-06](https://openairdocs.org/saib/2025-06): High Pressure Turbines. Issued Jul 22, 2025 - [SAIB NE-19-02](https://openairdocs.org/saib/NE-19-02): Turbine Engine Compressor Section -- Low-pressure turbine uncontainment. Issued Feb 19, 2019 - [SAIB NE-16-01R1](https://openairdocs.org/saib/NE-16-01R1): Turbine Section. Issued Jan 14, 2016 - [SAIB NE-15-19](https://openairdocs.org/saib/NE-15-19): Turbine Section. Issued Jul 14, 2015 - [SAIB NE-13-31](https://openairdocs.org/saib/NE-13-31): Turbine Engine Oil System Scavenge Oil Tube Coking and Proper Cleaning at Overhaul. Issued May 9, 2013 - [SAIB NE-16-01](https://openairdocs.org/saib/NE-16-01) (historical): Turbine Section. Issued Oct 5, 2015 ## NTSB investigations None matched to N445MC. ## FAA accident and incident reports None matched to N445MC. ## Service difficulty reports (73, newest 50) As reported by operators and repair stations. Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR UIEA2026053000371](https://openairdocs.org/sdr/UIEA2026053000371), May 29, 2026: FMU. FAULTED. 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. OP - [SDR UIEA2025091801240](https://openairdocs.org/sdr/UIEA2025091801240), Sep 18, 2025: WINDSHIELD. FAILED. 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), Jul 13, 2025: B-NUT. LOOSE. 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 - [SDR UIEA2025070600836](https://openairdocs.org/sdr/UIEA2025070600836), Jul 12, 2025: SKIN. DELAMINATED. RHW I/B FORE FLAP L/E MID AND O/B AREA FOUND DELAMINATED.(

PERFORMED PERMANENT COMPOSITE REPAIR AS PER SRM 51-70-07, PAR.5.A.(1). NO FURTHER DEFECTS NOTED.

PERFORMED PERMANENT COMPOSITE REPAIR AS PER SRM 51-70-07, PAR.5.A.(1). NO FURTHER DEFECTS NOTED.

) - [SDR UIEA2025070600838](https://openairdocs.org/sdr/UIEA2025070600838), Jul 12, 2025: SKIN. DELAMINATED. LHW I/B FORE FLAP O/B OF MID FORE FLAP TRACK APPROX 9" L/E AREA FOUND DELAMINATED.(

PERFORMED PERMANENT COMPOSITE REPAIR AS PER SRM 51-70-07, PAR.5.A.(1). NO - [SDR UIEA2025070600839](https://openairdocs.org/sdr/UIEA2025070600839), Jul 12, 2025: SKIN. DELAMINATED. LHW I/B FORE FLAP L/E MOST I/B AREA FOUND DELAMINATED.(

PERFORMED PERMANENT COMPOSITE REPAIR AS PER SRM 51-70-07, PAR.5.A.(1). NO FURTHER DEFECTS NOTED.

) - [SDR UIEA2025070600840](https://openairdocs.org/sdr/UIEA2025070600840), Jul 12, 2025: SKIN. DELAMINATED. LHW I/B FORE FLAP I/B OF FORE FLAP TRACK CUTOUT FOUND DELAMINATED.(

PERFORMED PERMANENT COMPOSITE REPAIR AS PER SRM 51-70-07, PAR.5.A.(1). NO FURTHER DEFECTS - [SDR UIEA2025070600843](https://openairdocs.org/sdr/UIEA2025070600843), Jul 12, 2025: BRACE. CHAFED. NO.1 PYLON DIAGONAL BRACE RH BELOW HYD DEPRESSURIZATION MODULE FOUND CHAFING.(

#1 PYLON DIAGONAL BRACE CHAFING AREA SMOOTHED AS PER RI-54-50-17750 REV.A. (AFT - [SDR UIEA2025070700853](https://openairdocs.org/sdr/UIEA2025070700853), Jul 12, 2025: FAIRING. DELAMINATED. DORSAL FAIRING FOUND DELAMINATED.(

PERFORMED REPAIR AT DELAMINATION AREA IAW RI-55-30-17752 REV.A. NO FURTHER DEFECTS NOTED.

) - [SDR UIEA2025070900876](https://openairdocs.org/sdr/UIEA2025070900876), Jul 12, 2025: CHANNEL. CRACKED. LH HORIZONTAL STABILIZER TIP FAIRING AFT SUPPORT U CHANNEL FOUND CRACKED.(

LH HORIZONTAL STABILIZER TIP FAIRING T/E WEDGE U CHANNEL REPLACED AS PER RI-55-10-1 - [SDR UIEA2025070900877](https://openairdocs.org/sdr/UIEA2025070900877), Jul 12, 2025: DOOR. CHAFED. #2 PYLON LH AFT FAIRING DOOR FOUND CHAFFING.(

PERFORMED REPAIR AT CHAFFING AREA IAW RI-54-50-17761, REV. A. NO FURTHER DEFECTS NOTED.

) - [SDR UIEA2025070900882](https://openairdocs.org/sdr/UIEA2025070900882), Jul 12, 2025: SKIN. DENTED. FX STA 520-540 R/H S43R - S44R SKIN FOUND DENT.(

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 NOT - [SDR UIEA2025071000889](https://openairdocs.org/sdr/UIEA2025071000889), Jul 12, 2025: STIFFENER. CRACKED. LHW L/E LOWER CENTER ZEE STIFFENER FOUND CRACKED.(

LHW L/E LOWER CENTER ZEE STIFFENER REPLACED AS PER RI-57-26-17755 REV A. NO FURTHER DEFECTS NOTED.

) - [SDR UIEA2025071000890](https://openairdocs.org/sdr/UIEA2025071000890), Jul 12, 2025: PANEL. CRACKED. NO.4 PYLON O/B #482KR PANEL FOUND CRACKED.(

NO.4 PYLON O/B #482KR PANEL REPLACED AS PER RI-54-50-17765 REV A. NO FURTHER DEFECTS NOTED.

) - [SDR UIEA2025071000891](https://openairdocs.org/sdr/UIEA2025071000891), Jul 12, 2025: BEAM. DAMAGED. NO.4 PYLON AFT FAIRING AREA APPROX WAC STA 415 UPPER BEAM RH FASTENER HOLE FOUND ELONGATED(

OVERSIZE FASTENER HOLE AND INSTALL FREEZE PLUG PER RI-54-50-17760 - [SDR UIEA2025071000892](https://openairdocs.org/sdr/UIEA2025071000892), Jul 12, 2025: RIB. CRACKED. LHW L/E #581HB PANEL RIB FOUND CRACKED.(

LHW L/E #581HB PANEL RIB REPLACED AS PER RI-57-51-17762 REV A. NO FURTHER DEFECTS NOTED.

) - [SDR UIEA2025071000894](https://openairdocs.org/sdr/UIEA2025071000894), Jul 12, 2025: RIB. CRACKED. LHW L/E #581JB PANEL RIB FOUND CRACKED.(

LHW L/E #581JB PANEL RIB REPLACED AS PER RI-57-51-17769 REV A. NO FURTHER DEFECTS NOTED.

) - [SDR UIEA2025071200937](https://openairdocs.org/sdr/UIEA2025071200937), Jul 12, 2025: FUEL TANK. CORRODED. LWLG W/W CENTER TANK AFT B/H FUEL BONDING ATTACH AREA SURFACE CORROSION.(

LWLG W/W CENTER TANK AFT B/H FUEL BONDING AREA CORROSION REMOVED AS PER - [SDR UIEA2025032500388](https://openairdocs.org/sdr/UIEA2025032500388), Mar 25, 2025: WIRE. DAMAGED. HYD CONTROL 4 ADVISORY MSG IN FLIGHT. CHECKLIST C/W. AIR TURNBACK TO KMIA.(

REPLACED WIRE W4261-434-24R AND 24B PER WDM 29-30-11 AND SWPM 20-10-13. TEST GOOD - [SDR UIEA2025021600149](https://openairdocs.org/sdr/UIEA2025021600149), Feb 16, 2025: PCU. FAULTED. RT INBOARD AILERON INDICATION MISSING. FLT CONTROL HYD POWER WING SHUTOFF SWITCHES SELECTED TO CLOSED ON P61 PANEL.(

1.PARTIALLY REMOVED INBD ALERON POWER CON - [SDR UIEA2024041000268](https://openairdocs.org/sdr/UIEA2024041000268), Apr 10, 2024: ROLLER CAM. UNKNOWN. 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 CRA - [SDR UIEA2023071000735](https://openairdocs.org/sdr/UIEA2023071000735), Jul 5, 2023: UNKNOWN. UNKNOWN. CRACK DAMAGE ON THE WEB OF STA 2231 FRAME AT S-21L AND S-22L(

1. REMOVED AFFECTED FASTENERS TO GET ACCESS IAW SRM 51-40-02-06-0. REV 97. 2. REPAIRED DAMAGE AR - [SDR UIEA2023071000736](https://openairdocs.org/sdr/UIEA2023071000736), Jul 5, 2023: UNKNOWN. UNKNOWN. REPAIR - SKIN MODIFICATION FOR STATION 1640 TO 1740 LEFT SIDE AT STRINGER 34 PER SB 747-53A2487(

1. ACCOMPLISHED JOB IAW EI T2023A53M-1374 REV 1. 2. ACCOMPLIS - [SDR UIEA2023071000737](https://openairdocs.org/sdr/UIEA2023071000737), Jul 5, 2023: UNKNOWN. UNKNOWN. CRACK ON FASTENER HOLE OF TENSION TIE AFT CHANNEL AT STA 740 RH SIDE(

1. REMOVED AFFECTED FASTENER TO GET ACCESS IAW 51-40-02-0G-0. REV 97. 2. PERFORM EI T202 - [SDR UIEA2023071000738](https://openairdocs.org/sdr/UIEA2023071000738), Jul 5, 2023: UNKNOWN. UNKNOWN. CRACK ON FASTENER HOLE OF TENSION TIE AFT CHANNEL STA 760 RH SIDE(

1. REMOVED AFFECTED FASTENERS TO GET ACCESS IAW SRM 51-40-02-0G-0, REV 97. 2. PERFORM EI T2 - [SDR UIEA2023071000739](https://openairdocs.org/sdr/UIEA2023071000739), Jul 5, 2023: UNKNOWN. UNKNOWN. FWD FLOOR STRUCTURE SUBSTITUTE TRACK CRACK AT M/D STA 980 LBL 75.92(

1. REMOVED FASTENERS IAW SRM 51-40-02-0G-0 REV97. 2. REPAIR SUBSTITUTE TRACK IAW SRM 53-0 - [SDR UIEA2023071000740](https://openairdocs.org/sdr/UIEA2023071000740), Jul 5, 2023: UNKNOWN. UNKNOWN. 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 - [SDR UIEA2023071000741](https://openairdocs.org/sdr/UIEA2023071000741), Jul 5, 2023: UNKNOWN. UNKNOWN. FOUND FLOOR STRUCTURE SUBSTITUTE TRACK CRACK AT M/D STA 1540 RBL 75.92(

1. REMOVED FASTENERS IAW SRM 51-40-02-0G-0 REV 98. 2. REPAIR TRACK IAW SRM 53-00-52-2R - [SDR UIEA2023071000742](https://openairdocs.org/sdr/UIEA2023071000742), Jul 5, 2023: UNKNOWN. UNKNOWN. FOUND FLOOR STRUCTURE SUBSTITUTE TRACK CRACK AT M/D STA1641 LBL 75.92(

1. REMOVED FASTENERS IAW SRM 51-40-02-0G-0 REV 98. 2. REPAIR TRACK IAW SRM 53-00-52-2R- - [SDR UIEA2023071000743](https://openairdocs.org/sdr/UIEA2023071000743), Jul 5, 2023: UNKNOWN. UNKNOWN. GOUGE DAMAGE ON RH WING LOWER SKIN PANEL NO.2 BETWEEN STRINGER L-8 AND L-9 AT WBL 743.828(

1. ACCOMPLISHED EI T2023A57M-1479. SEQUENCE B REV 1. 2. ACCOMPLISHE - [SDR UIEA2023071000744](https://openairdocs.org/sdr/UIEA2023071000744), Jul 5, 2023: SHEAR TIE. UNKNOWN. CRACK ON THE SHEAR TIE AT 1000 LBL 33.99 SB 747-53A2904(

1. REMOVED DAMAGE PART IAW SRM 51-40-02-0G-0 REV 97. 2. ACCOMPLISHED EI T2023A53M-1550 REV 0 AND SB 7 - [SDR UIEA2023071000745](https://openairdocs.org/sdr/UIEA2023071000745), Jul 5, 2023: SHEAR TIE. UNKNOWN. CRACK ON THE SHEAR TIE AT STA 1000 RBL 33.99 SB 747 53A2904(

1. REMOVED DAMAGE PART IAW SRM 51.40.02.0G.0 REV 97. ACCOMPLISHED EI T2023A53M-1550 REV 0, SB 747 - [SDR UIEA2023071000746](https://openairdocs.org/sdr/UIEA2023071000746), Jul 5, 2023: FITTING. UNKNOWN. CRACK ON THE INTERCOSTAL LUG FITTING AT STA 1000 RBL 11.33, SB 747-53A2904(

1. REMOVED DAMAGE PART IAW SRM 51-40-02-0G-0 REV 97. 2. ACCOMPLISHED EI NO T2023A5 - [SDR UIEA2023071000747](https://openairdocs.org/sdr/UIEA2023071000747), Jul 5, 2023: CAP. UNKNOWN. CORROSION - FOUND MAIN DECK CGO FLOOR BEAM CAP CORROSION STA 2360 RBL 3.(

1. REMOVED DAMAGE PARTS IAW 51-40-02-0G-0 REV98. 2. INSTALL NEW PARTS IAW SRM 51-40- - [SDR UIEA2023071000748](https://openairdocs.org/sdr/UIEA2023071000748), Jul 5, 2023: FITTING. UNKNOWN. CORROSION - 2EA CGO TRACK CORROSION AT R/H STA 2360 MAIN DECK FLOOR(

1. IAW AMM SUBTASK 53-44-00-212-001, REV107 REMOVE CGO TRACK 2. IAW AMM SUBTASK 53-44-00- - [SDR UIEA2023071000749](https://openairdocs.org/sdr/UIEA2023071000749), Jul 5, 2023: UNKNOWN. UNKNOWN. FOUND #1 FLAP TRACK INBD SIDE LOAD FITTING CONTACT SURFACE CORROSION AND BUSHING MIGRATION(

1. IAW AMM 20-51-01-912-008, REV 107 R/R #1 FLAP TRACK INBD SIDE L - [SDR UIEA2023071000750](https://openairdocs.org/sdr/UIEA2023071000750), Jul 5, 2023: UNKNOWN. UNKNOWN. FOUND #8 FLAP TRACK INBD SIDE LOAD FITTING CONTACT SURFACE CORROSION AND BUSHING MIGRATION(

1. IAW AMM 20-51-01-912-008 REV107 R/R #8 FLAP TRACK INBD SIDE LOA - [SDR UIEA2023071000751](https://openairdocs.org/sdr/UIEA2023071000751), Jul 5, 2023: UNKNOWN. UNKNOWN. FOUND #3Â FLAP TRACK INBD SIDE LOAD FIG CONTACT SURFACE CORROSION AND BUSHING MIGRATION(

1. IAW AMM 20-51-01-912-008 REV107 R/R #3 FLAP TRACK INBD SIDE LOAD P - [SDR UIEA2023071000752](https://openairdocs.org/sdr/UIEA2023071000752), Jul 5, 2023: UNKNOWN. UNKNOWN. FOUND #6 FLAP TRACK INBD SIDE LOAD FIG CONTACT SURFACE CORROSION AND BUSHING MIGRATION(

1. IAW AMM 20-51-01-912-008, REV107 R/R #6 FLAP TRACK INBD SIDE LOAD P - [SDR UIEA2023071000753](https://openairdocs.org/sdr/UIEA2023071000753), Jul 5, 2023: UNKNOWN. UNKNOWN. FOUND #7 FLAP TRACK INBD SIDE LOAD FITTING CONTACT SURFACE CORROSION AND BUSHING MIGRATION(

1. IAW AMM 20-51-01-912-008 REV107 R/R #7 FLAP TRACK INBD SIDE LOA - [SDR UIEA2023071000754](https://openairdocs.org/sdr/UIEA2023071000754), Jul 5, 2023: CHARGER. UNKNOWN. FOUND EMERGENCY LIGHT BATTERY PACK (MJ120) FUNCTION FAIL.(

1. IAW AMM 33-51-04-002-009-001 & 33-51-04-402-012-001 REV.107. REPLACED POWER SUPPLY (MJ170). - [SDR UIEA2023081500777](https://openairdocs.org/sdr/UIEA2023081500777), Jun 14, 2023: WINDOW. UNKNOWN. CAPT SIDE REAR MOST WINDOW SQUEALING AND VIBRATING(

R/R WINDOW PER AMM 56-11-02. OPS CHK GOOD.

) - [SDR UIEA2022053000559](https://openairdocs.org/sdr/UIEA2022053000559), May 30, 2022: FMU. FAILED. 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), Apr 17, 2022: NONE. NONE. ON DESCENT, LOUD ELECTRICAL BUZZ BEHIND CAPTAIN LEFT SIDE FOLLOWED BY STRONG ELECTRICAL SMELL. POWER 2L WINDOW HEAT CIRCUIT BREAKER POPPED.(

REMOVED #2 - [SDR UIEA2022040700264](https://openairdocs.org/sdr/UIEA2022040700264), Apr 7, 2022: SKIN. DAMAGED. R/H UPPER AFT FUSELAGE ABOVE RH ELEVATOR SECTION 48 APROXIMATE B.S. 258/ HAS HOLE IN SKIN WITH CRACKS.(

REMOVED DAMAGED SKIN SECTION FROM  STRINGER - [SDR UIEA2022021700146](https://openairdocs.org/sdr/UIEA2022021700146), Feb 17, 2022: MODULE. NONE. AIRCRAFT COMPLETED AIR TURN BACK AND RETURNED TO THE FIELD DUE TO GEAR MONITOR WARNING(

REPLACED PSEU MODULE IAW AMM 32-09-03. OPS CHECK GOOD.CARRIED OUT PERMANENT COMPOSITE HOTBOND REPAIR AS PER SRM 51-70-08 PAR 5A 

) - [SDR UIEA2021082301836](https://openairdocs.org/sdr/UIEA2021082301836), Aug 26, 2021: ACCESS DOOR. DELAMINATED. FUS - ACCESS DOOR 191EL EXT SURFACE DELAM(

CARRIED OUT PERMANENT COMPOSITE HOTBOND REPAIR AS PER SRM 51-70-08 PAR 5A 

) - [SDR UIEA2021082301837](https://openairdocs.org/sdr/UIEA2021082301837), Aug 26, 2021: ACCESS DOOR. DELAMINATED. FUS - ACCESS DOOR 192ER EXT SURFACE DELAM(

CARRIED OUT PERMANENT COMPOSITE HOTBOND REPAIR AS PER SRM 51-70-08 PAR 5A 

) All 73: https://openairdocs.org/aircraft/N445MC/reports.md ## STCs that may be installed (OpenAirDocs) None matched to this aircraft's models. ## Related - Other Boeing 747-4B5F aircraft: https://openairdocs.org/model/boeing-747-4b5f/aircraft.md - The Pratt & Whitney PW4062A engine: https://openairdocs.org/engine/pratt-whitney-pw4062a.md --- 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.