# N418MC: 2002 Boeing 747-47UF

- Status: Valid registration
- Airframe: [Boeing 747-47UF](https://openairdocs.org/model/boeing-747-47uf) (registry code 1384812, 660 seats)
- Engine: [GE CF6-80 series](https://openairdocs.org/engine/ge-cf6-80-series) (registry code 30025)
- Data sheets: [TCDS E13NE](https://openairdocs.org/tcds/E13NE) (General Electric Company GE Aerospace) (OpenAirDocs)
- Serial number: 32840
- Year built: 2002
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: November 27, 2002
- Certificate issued: December 8, 2022
- Expires: December 31, 2029
- Mode S code: A4F2EE
- 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=418MC
- Page: https://openairdocs.org/aircraft/N418MC

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. The registry lists only the engine series, so ADs for every GE CF6-80 model are included.

## ADs that may apply (OpenAirDocs): 61 in force

### Matched by airframe (Boeing 747-47UF)

None in force.

### Matched by engine (GE CF6-80 series)

- [AD 2024-24-03](https://openairdocs.org/ad/2024-24-03): Engine Exhaust · Boeing MD-11, MD-11F and CF6-80C2D1F. Effective Jan 13, 2025
- [AD 2023-20-08](https://openairdocs.org/ad/2023-20-08): Engine (Turbine/Turboprop) · General Electric CF6-80C2B1F, CF6-80C2B2F, CF6-80C2B4F and 4 more. Effective Oct 19, 2023
- [AD 2021-26-22](https://openairdocs.org/ad/2021-26-22): Turbine Section · General Electric CF6-80A, CF6-80A1, CF6-80A2 and 21 more. Effective Mar 14, 2022
- [AD 2022-02-18](https://openairdocs.org/ad/2022-02-18): Engine Mount Section · General Electric CF6-80C2A1, CF6-80C2A2, CF6-80C2A3 and 3 more. Effective Feb 25, 2022
- [AD 2021-14-11](https://openairdocs.org/ad/2021-14-11): Turbine Section · General Electric CF6-80A, CF6-80A1, CF6-80A2 and 25 more. Effective Aug 27, 2021
- [AD 2021-03-02](https://openairdocs.org/ad/2021-03-02): Fuel Control/Turbine Engines · General Electric CF6-80C2A1, CF6-80C2A2, CF6-80C2A3 and 16 more. Effective Mar 31, 2021
- [AD 2020-22-02](https://openairdocs.org/ad/2020-22-02): Engine Fuel and Control · General Electric CF6-80C2A5F, CF6-80C2B1F, CF6-80C2B2F and 13 more. Effective Dec 3, 2020
- [AD 2018-07-05](https://openairdocs.org/ad/2018-07-05): Turbine Section · General Electric CF6-80A, CF6-80A1, CF6-80A2 and 1 more. Effective May 11, 2018
- [AD 2017-11-15](https://openairdocs.org/ad/2017-11-15): Turbine/ Turboprop Engine--Turbine Section · General Electric CF6-80C2L1F. Effective Jul 13, 2017
- [AD 2016-08-10](https://openairdocs.org/ad/2016-08-10): Accessory heat shield · General Electric CF6-80C2A1, CF6-80C2A2, CF6-80C2A3 and 26 more. Effective Jun 1, 2016
- [AD 2014-21-01](https://openairdocs.org/ad/2014-21-01): Fuel manifold · General Electric CF6-80C2A1, CF6-80C2A2, CF6-80C2A3 and 26 more. Effective Nov 28, 2014
- [AD 2013-08-20](https://openairdocs.org/ad/2013-08-20): Fuel tube · General Electric CF6-80C2A1, CF6-80C2A2, CF6-80C2A3 and 14 more. Effective May 31, 2013
- [AD 2012-03-12](https://openairdocs.org/ad/2012-03-12): No. 3 bearing packing · General Electric CF6-80C2A1, CF6-80C2A2, CF6-80C2A3 and 21 more. Effective Apr 5, 2012
- [AD 2012-04-05](https://openairdocs.org/ad/2012-04-05): Electronic control unit (ECU) · General Electric CF6-80C2B1F, CF6-80C2B1F1, CF6-80C2B1F2 and 8 more. Effective Mar 30, 2012
- [AD 2011-23-04](https://openairdocs.org/ad/2011-23-04): Forward engine mount assembly side links · General Electric CF6-45A, CF6-45A2, CF6-50A and 14 more. Effective Dec 12, 2011
- [AD 2009-21-07](https://openairdocs.org/ad/2009-21-07): Thrust and thrust control · General Electric CF6-80C2A1, CF6-80C2A2, CF6-80C2A3 and 21 more. Effective Dec 1, 2009
- [AD 2009-14-08](https://openairdocs.org/ad/2009-14-08): High-pressure compressor rotor (HPCR) stages 11-14 spool/ shafts · General Electric CF6-80C2B5F. Effective Aug 5, 2009
- [AD 2009-08-06](https://openairdocs.org/ad/2009-08-06): Stage 1 high-pressure turbine (HPT) rotor  
 disks · General Electric CF6-80A, CF6-80A1, CF6-80A2 and 1 more. Effective May 18, 2009
- [AD 2009-07-10](https://openairdocs.org/ad/2009-07-10): High-pressure turbine rotor (HPTR) · General Electric CF6-80A, CF6-80A1, CF6-80A2 and 1 more. Effective May 6, 2009
- [AD 2009-07-03](https://openairdocs.org/ad/2009-07-03): Eddy current inspection (ECI) · General Electric CF6-80C2A1, CF6-80C2A2, CF6-80C2A3 and 26 more. Effective Apr 30, 2009
- [AD 2009-04-10](https://openairdocs.org/ad/2009-04-10): Critical life-limited parts · General Electric CF6-80A, CF6-80A1, CF6-80A2 and 30 more. Effective Mar 30, 2009
- [AD 2008-21-11](https://openairdocs.org/ad/2008-21-11): Low-pressure turbine (LPT) cases · General Electric CF6-80C2A1, CF6-80C2A2, CF6-80C2A3 and 25 more. Effective Nov 28, 2008
- [AD 2008-02-17](https://openairdocs.org/ad/2008-02-17): Thrust reverser actuation systems · General Electric CF6-50A, CF6-50C, CF6-50C1 and 16 more. Effective Feb 28, 2008
- [AD 2007-24-07](https://openairdocs.org/ad/2007-24-07): Thermal spray coating on certain stage 1 fan disks · General Electric CF6-80C2B1. Effective Jan 2, 2008
- [AD 2007-22-07](https://openairdocs.org/ad/2007-22-07): Electronic control unit (ECU) · General Electric CF6-80C2D1F. Effective Nov 28, 2007
- [AD 2007-21-06](https://openairdocs.org/ad/2007-21-06): Electronic control unit (ECU) · General Electric CF6-80C2A5F. Effective Nov 15, 2007
- [AD 2007-11-20](https://openairdocs.org/ad/2007-11-20): Fuel shroud retaining rings · General Electric CF6-80C2A1, CF6-80C2A2, CF6-80C2A3 and 22 more. Effective Jul 10, 2007
- [AD 2007-05-14](https://openairdocs.org/ad/2007-05-14): Cast titanium weld- repaired forward engine mount platforms · General Electric CF6-80C2A1, CF6-80C2A2, CF6-80C2A3 and 16 more. Effective Apr 9, 2007
- [AD 2006-16-06](https://openairdocs.org/ad/2006-16-06): Certain stage 1 high- pressure turbine (HPT) rotor disks · General Electric CF6-80A, CF6-80A1, CF6-80A2 and 21 more. Effective Sep 5, 2006
- [AD 2006-06-08](https://openairdocs.org/ad/2006-06-08): Latching system of the fan reverser · General Electric CF6-80C2D1F. Effective Apr 25, 2006
- [AD 2005-17-05](https://openairdocs.org/ad/2005-17-05): High pressure compressor rotor (HPCR) · General Electric CF6-80C2A1, CF6-80C2A2, CF6-80C2A3 and 25 more. Effective Sep 27, 2005
- [AD 2005-06-07](https://openairdocs.org/ad/2005-06-07): Directional pilot valve (DPV) assembly · General Electric CF6-80A1, CF6-80A3, CF6-80C2A1 and 5 more. Effective Apr 25, 2005
- [AD 2004-22-07](https://openairdocs.org/ad/2004-22-07): Stage 2 nozzle guide vanes (HPT S2 NGVs) · General Electric CF6-80C2A1, CF6-80C2A2, CF6-80C2A3 and 16 more. Effective Dec 1, 2004
- [AD 2004-07-13](https://openairdocs.org/ad/2004-07-13): High pressure turbine (HPT) stage 1 disks · General Electric CF6-80C2A5F, CF6-80C2B5F, CF6-80C2B7F and 1 more. Effective May 6, 2004
- [AD 2003-12-08](https://openairdocs.org/ad/2003-12-08): Directional pilot valve · General Electric CF6-80A1, CF6-80A3, CF6-80C2A1 and 5 more. Effective Jul 23, 2003
- [AD 2003-02-07](https://openairdocs.org/ad/2003-02-07): Low pressure turbine (LPT) shrouds · General Electric CF6-50A, CF6-50C, CF6-50C1 and 30 more. Effective Mar 3, 2003
- [AD 2002-25-08](https://openairdocs.org/ad/2002-25-08): High pressure compressor rotor · General Electric CF6-45A, CF6-45A2, CF6-50A and 40 more. Effective Jan 23, 2003
- [AD 2002-22-12](https://openairdocs.org/ad/2002-22-12): Titeflex hoses · BAE Systems ATP, Avro 146-RJ100A, Avro 146-RJ70A and 122 more. Effective Dec 13, 2002
- [AD 2001-06-09](https://openairdocs.org/ad/2001-06-09): Aft Engine Mount Link Assemblies · General Electric CF6-80A3. Effective May 1, 2001
- [AD 2000-12-08](https://openairdocs.org/ad/2000-12-08): Mount Link Assemblies · General Electric CF6-80C2A1, CF6-80C2A2, CF6-80C2A3 and 4 more. Effective Aug 28, 2000
- [AD 2000-03-04](https://openairdocs.org/ad/2000-03-04): General Electric CF6-80C2A1, CF6-80C2A2, CF6-80C2A3 and 19 more. Effective Apr 10, 2000
- [AD 99-01-01](https://openairdocs.org/ad/99-01-01): Accessory Gearbox (AGB) idler adapters · General Electric CF6-80C2A1, CF6-80C2A2, CF6-80C2A3 and 19 more. Effective Jan 21, 1999
- [AD 98-22-06](https://openairdocs.org/ad/98-22-06): Fan Disks · General Electric CF6-45A, CF6-45A2, CF6-50A and 41 more. Effective Nov 23, 1998
- [AD 97-22-14](https://openairdocs.org/ad/97-22-14): (HPCR) 3-9 Spool · General Electric CF6-50A, CF6-50C, CF6-50C1 and 29 more. Effective Nov 17, 1997
- [AD 96-16-07](https://openairdocs.org/ad/96-16-07): Rear Right Hand Mount Link · General Electric CF6-80C2A1, CF6-80C2A2, CF6-80C2A3 and 17 more. Effective Aug 28, 1996
- [AD 95-17-16](https://openairdocs.org/ad/95-17-16): Compressor Rear Frame · General Electric CF6-80A, CF6-80A1, CF6-80A2 and 1 more. Effective Nov 7, 1995
- [AD 95-10-11](https://openairdocs.org/ad/95-10-11): Fan Reversers · General Electric CF6-80C2A1, CF6-80C2A2, CF6-80C2A3 and 17 more. Effective May 31, 1995
- [AD 94-20-06](https://openairdocs.org/ad/94-20-06): Oil System · General Electric CF6-80C2A1, CF6-80C2A2, CF6-80C2A3 and 16 more. Effective Dec 27, 1994
- [AD 94-07-04](https://openairdocs.org/ad/94-07-04): High Pressure Turbine Disk · General Electric CF6-80A, CF6-80A1, CF6-80A2 and 1 more. Effective May 23, 1994
- [AD 94-06-03](https://openairdocs.org/ad/94-06-03): High Pressure Turbine Disk · General Electric CF6-80C2A1, CF6-80C2A2, CF6-80C2A3 and 16 more. Effective Apr 29, 1994

### Historical (superseded or no longer in force)

- [AD 2020-20-13](https://openairdocs.org/ad/2020-20-13) (historical): Turbine Section · General Electric CF6-80A, CF6-80A1, CF6-80A2 and 21 more. Effective Nov 12, 2020
- [AD 2018-15-04](https://openairdocs.org/ad/2018-15-04) (historical): Turbine/Turboprop Engine--Turbine Section · General Electric CF6-80A, CF6-80A1, CF6-80A2 and 21 more. Effective Oct 2, 2018
- [AD 2009-05-02](https://openairdocs.org/ad/2009-05-02) (historical): Drainless fuel manifold assemblies · General Electric CF6-80C2A1, CF6-80C2A2, CF6-80C2A3 and 26 more. Effective Mar 31, 2009
- [AD 2007-12-07](https://openairdocs.org/ad/2007-12-07) (historical): Electronic control units (ECUs) · General Electric CF6-80C2B1F, CF6-80C2B2F, CF6-80C2B4F and 5 more. Effective Jul 11, 2007
- [AD 2006-12-24](https://openairdocs.org/ad/2006-12-24) (historical): Five-link forward mount assembly · General Electric CF6-45A, CF6-45A2, CF6-50A and 14 more. Effective Jul 21, 2006
- [AD 2004-04-07](https://openairdocs.org/ad/2004-04-07) (historical): Stage 1 HPT rotor disks · General Electric CF6-80A, CF6-80A1, CF6-80A2 and 21 more. Effective Mar 12, 2004
- [AD 2003-01-05](https://openairdocs.org/ad/2003-01-05) (historical): Dovetail slots · General Electric CF6-80A, CF6-80A1, CF6-80A2 and 1 more. Effective Jan 28, 2003
- [AD 2002-07-12](https://openairdocs.org/ad/2002-07-12) (historical): Life Limits Section of Continued Airworthiness (ICA) - Selected Critical Life-limited Parts · General Electric CF6-80A, CF6-80A1, CF6-80A2 and 27 more. Effective May 15, 2002
- [AD 2001-10-07](https://openairdocs.org/ad/2001-10-07) (historical): High Pressure Turbine Rotor Disks · General Electric CF6-80C2A1, CF6-80C2A2, CF6-80C2A3 and 19 more. Effective Jun 18, 2001
- [AD 2000-08-12](https://openairdocs.org/ad/2000-08-12) (historical): Life-limited Parts · General Electric CF6-80A, CF6-80A1, CF6-80A2 and 10 more. Effective Oct 23, 2000
- [AD 2000-16-12](https://openairdocs.org/ad/2000-16-12) (historical): High Pressure Compressor Rotor Stage 3-9 Spools · General Electric CF6-45A, CF6-45A2, CF6-50A and 39 more. Effective Sep 5, 2000
- [AD 2000-04-14](https://openairdocs.org/ad/2000-04-14) (historical): Fuel tube flange seating · General Electric CF6-80C2A1, CF6-80C2A2, CF6-80C2A3 and 12 more. Effective May 1, 2000
- [AD 99-24-15](https://openairdocs.org/ad/99-24-15) (historical): High Pressure Compressor Rotor (HPCR) Stage 3-9 Spools · General Electric CF6-45A, CF6-45A2, CF6-50A and 39 more. Effective Jan 28, 2000
- [AD 99-18-20](https://openairdocs.org/ad/99-18-20) (historical): Inadvertent In-flight Thrust Reverser · General Electric Aircraft Engines CF6-50 Series (all), CF6-80A1, CF6-80A3 and 6 more. Effective Nov 2, 1999
- [AD 99-18-19](https://openairdocs.org/ad/99-18-19) (historical): Inadvertent Thrust Reverser · General Electric CF6-80A, CF6-80A1, CF6-80A2 and 7 more. Effective Sep 24, 1999
- [AD 99-08-13](https://openairdocs.org/ad/99-08-13) (historical): General Electric CF6-80A, CF6-80A1, CF6-80A2 and 26 more. Effective May 13, 1999
- [AD 98-15-17](https://openairdocs.org/ad/98-15-17) (historical): Link Assembly · General Electric CF6-80A3. Effective Aug 7, 1998
- [AD 91-20-02](https://openairdocs.org/ad/91-20-02) (historical): Fuel Manifolds · General Electric CF6-80C2A1, CF6-80C2A2, CF6-80C2A3 and 12 more. Effective Nov 25, 1991
- [AD 90-26-01](https://openairdocs.org/ad/90-26-01) (historical): Fuel Manifold Systems · General Electric CF6-80C2A1, CF6-80C2A2, CF6-80C2A3 and 11 more. Effective Dec 20, 1990

All 80: https://openairdocs.org/aircraft/N418MC/ads.md

## Information bulletins (advisory) (5 in force)

- [SAIB 2023-15](https://openairdocs.org/saib/2023-15): Falsified Forms from AOG Technics. Issued Dec 19, 2023
- [SAIB NE-11-27](https://openairdocs.org/saib/NE-11-27): Fuel Injector Nozzle - CF6-80 Improperly Welded Fuel Nozzles. Issued Apr 5, 2011
- [SAIB NE-10-37](https://openairdocs.org/saib/NE-10-37): Engine Fuel and Control: FADEC Fuel Metering Valve Resolver Feedback Faults. Issued Jul 12, 2010
- [SAIB NE-08-44](https://openairdocs.org/saib/NE-08-44): Engine Thrust Reverser  Transcowl Clevis Pin. Issued Sep 3, 2008
- [SAIB NE-07-01](https://openairdocs.org/saib/NE-07-01): Dual engine flameouts on twin engine airplanes. Issued Oct 12, 2006

## NTSB investigations (1)

From the NTSB's public API. Aircraft are matched to registry aircraft by N-number and event date, checked against the reported serial number, make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model.

- [NTSB OPS06IA008](https://openairdocs.org/ntsb/OPS06IA008), Jul 24, 2006: Boeing 747 (N418MC), Chicago, IL, incident, no damage. Probable cause: The failure of the ORD tower south local controller to monitor Atlas Air flight 6972 on arrival to runway 14R and subsequently clearing United Airlines flight 1015 for takeoff on intersecting runway…

## FAA accident and incident reports

None matched to N418MC.

## Service difficulty reports (152, 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 UIEA2026072300640](https://openairdocs.org/sdr/UIEA2026072300640), Jul 23, 2026: APU. ODOR. 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
- [SDR UIEA2026051400315](https://openairdocs.org/sdr/UIEA2026051400315), May 14, 2026: RIB. BROKEN. 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), May 14, 2026: RIB. CRACKED. 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), May 14, 2026: SUPPORT ANGLE. DAMAGED. 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-
- [SDR UIEA2026051400318](https://openairdocs.org/sdr/UIEA2026051400318), May 14, 2026: FITTING. CORRODED. 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), May 14, 2026: FITTING. CORRODED. 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 CHK
- [SDR UIEA2026051400320](https://openairdocs.org/sdr/UIEA2026051400320), May 14, 2026: REPAIR. NOT REPORTED. 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 FUS
- [SDR UIEA2024052200401](https://openairdocs.org/sdr/UIEA2024052200401), May 27, 2024: SKIN. DELAMINATED. 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 202
- [SDR UIEA2024052200402](https://openairdocs.org/sdr/UIEA2024052200402), May 27, 2024: SKIN. DELAMINATED. 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. 
- [SDR UIEA2024052200403](https://openairdocs.org/sdr/UIEA2024052200403), May 27, 2024: SKIN. DELAMINATED. 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.
- [SDR UIEA2024052200404](https://openairdocs.org/sdr/UIEA2024052200404), May 27, 2024: SKIN. DELAMINATED. 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
- [SDR UIEA2024052200405](https://openairdocs.org/sdr/UIEA2024052200405), May 27, 2024: SKIN. DELAMINATED. 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
- [SDR UIEA2024052200406](https://openairdocs.org/sdr/UIEA2024052200406), May 27, 2024: SKIN. DELAMINATED. 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 20
- [SDR UIEA2024052200407](https://openairdocs.org/sdr/UIEA2024052200407), May 27, 2024: SKIN. DELAMINATED. 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 202
- [SDR UIEA2024052300408](https://openairdocs.org/sdr/UIEA2024052300408), May 27, 2024: SKIN. DENTED. 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 202
- [SDR UIEA2024052300409](https://openairdocs.org/sdr/UIEA2024052300409), May 27, 2024: SKIN. DENTED. 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 202
- [SDR UIEA2024052300410](https://openairdocs.org/sdr/UIEA2024052300410), May 27, 2024: STRUCTURE. CORRODED. 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 N
- [SDR UIEA2024052300411](https://openairdocs.org/sdr/UIEA2024052300411), May 27, 2024: FUEL TANK. CORRODED. 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-5
- [SDR UIEA2024052300413](https://openairdocs.org/sdr/UIEA2024052300413), May 27, 2024: STRUCTURE. CORRODED. 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 
- [SDR UIEA2024052300414](https://openairdocs.org/sdr/UIEA2024052300414), May 27, 2024: STIFFENER. CRACKED. 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), May 27, 2024: ACCESS PANEL. CHAFED. 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
- [SDR UIEA2024052400432](https://openairdocs.org/sdr/UIEA2024052400432), May 27, 2024: SKIN. CRACKED. 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), May 27, 2024: FASTENER. LOOSE. 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. N
- [SDR UIEA2024052500443](https://openairdocs.org/sdr/UIEA2024052500443), May 27, 2024: SKIN. CRACKED. 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 RE
- [SDR UIEA2024052500444](https://openairdocs.org/sdr/UIEA2024052500444), May 27, 2024: STRUCTURE. CRACKED. #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), May 27, 2024: SKIN. CRACKED. 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.<
- [SDR UIEA2024052500446](https://openairdocs.org/sdr/UIEA2024052500446), May 27, 2024: PANEL. DAMAGED. 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 PR
- [SDR UIEA2024052600447](https://openairdocs.org/sdr/UIEA2024052600447), May 27, 2024: STRUCTURE. CRACKED. 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 R
- [SDR UIEA2024052600448](https://openairdocs.org/sdr/UIEA2024052600448), May 27, 2024: STRUCTURE. CRACKED. 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
- [SDR UIEA2024052600449](https://openairdocs.org/sdr/UIEA2024052600449), May 27, 2024: DOUBLER. NONE. 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 DEV
- [SDR UIEA2024052600450](https://openairdocs.org/sdr/UIEA2024052600450), May 27, 2024: DOUBLER. NONE. 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 DEV
- [SDR UIEA2024052600451](https://openairdocs.org/sdr/UIEA2024052600451), May 27, 2024: SUPPORT ROD. CORRODED. 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: 69B11633-1
- [SDR UIEA2024052210398](https://openairdocs.org/sdr/UIEA2024052210398), May 21, 2024: BULB. FAILED. 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 15MA
- [SDR UIEA2024011400013](https://openairdocs.org/sdr/UIEA2024011400013), Jan 14, 2024: CDU. UNKNOWN. 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 
- [SDR UIEA2022053000558](https://openairdocs.org/sdr/UIEA2022053000558), May 30, 2022: DRIVE ASSY. FAILED. BOTH L & R WEATHER RADARS FAILED AT CRUISE. REMOVED AND REPLACED WEATHER RADAR DRIVE MOUNT ASSEMBLY.
- [SDR UIEA2022052400538](https://openairdocs.org/sdr/UIEA2022052400538), May 25, 2022: ROD END BEARING. ELONGATED. 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), May 25, 2022: FITTING. CRACKED. 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 R
- [SDR UIEA2022051600483](https://openairdocs.org/sdr/UIEA2022051600483), May 25, 2022: FITTING. CRACKED. 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 LB
- [SDR UIEA2022051800487](https://openairdocs.org/sdr/UIEA2022051800487), May 25, 2022: CARGO TRACK. CRACKED. 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), May 25, 2022: SKIN. CRACKED. 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 WEL
- [SDR UIEA2022052400539](https://openairdocs.org/sdr/UIEA2022052400539), May 25, 2022: LATCH. ELONGATED. 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), May 25, 2022: LATCH. ELONGATED. 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), Jan 15, 2022: VALVE. MALFUNCTIONED. 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 
- [SDR UIEA2021122802490](https://openairdocs.org/sdr/UIEA2021122802490), Dec 28, 2021: NONE. NONE. 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
- [SDR UIEA2021100702202](https://openairdocs.org/sdr/UIEA2021100702202), Oct 3, 2021: NONE. NONE. 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), Sep 12, 2021: PRESSURE SWITCH. FAILED. (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 
- [SDR UIEA2021081201767](https://openairdocs.org/sdr/UIEA2021081201767), Aug 12, 2021: SEQUENCE VALVE. FAILED. 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, C
- [SDR UIEA2020061901319](https://openairdocs.org/sdr/UIEA2020061901319), Jun 17, 2020: ENGINE. FIRE. 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 
- [SDR UIEA2020051200769](https://openairdocs.org/sdr/UIEA2020051200769), May 8, 2020: SUPPORT. CORRODED. 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 REPA
- [SDR UIEA2020051200770](https://openairdocs.org/sdr/UIEA2020051200770), May 8, 2020: SUPPORT. CORRODED. 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 REPAI

All 152: https://openairdocs.org/aircraft/N418MC/reports.md

## STCs that may be installed (OpenAirDocs) (6)

Approved for this aircraft's airframe or engine model, in force first, then newest. The registry doesn't record which STCs an aircraft has; its records do.

### Approved for the engine (GE CF6-80 series)

- [STC SE01543CH](https://openairdocs.org/stc/SE01543CH): Replace Hamilton Sundstrand P/N 778839-13, 778839-14, 778839-19, 778839-20, 778839-37, 778839-38, 816682-1, 840618-2, 880724 carbon bushings with Cook Airtomic P/N AIR22947 Slotted Entry Busing in the High Pressure Shutoff Valve. Cook Airtomic. Lists CF6-80A
- [STC SE01478CH](https://openairdocs.org/stc/SE01478CH): Installation of Cook Airtomic alignment joint p/n AIR 22912. Cook Airtomic. Lists CF6-80C2 Series
- [STC SE00969CH](https://openairdocs.org/stc/SE00969CH): Install AeroControlex P/N 2605290-001 variable stator feedback control cable. AeroControlex Group TransDigm Inc. Lists CF6-80A
- [STC SE01471AT](https://openairdocs.org/stc/SE01471AT): Replace right and left side Rohr, Inc. fire detection harness on GE CF6-80C2 engine. Unison Industries. Lists CF6-80C2 Series
- [STC SE00463LA](https://openairdocs.org/stc/SE00463LA): Install fireproof blankets on the engine fan reverser intermediate fireseal, in lieu of fireproof intumescent coating. This STC is jointly by owned by Hi Temp Insulation and MRA Systems acting through Middle River Aircraft Systems, 103 Chesapeake Park Plaza, Baltimore, MD 21220. Hi Temp Insulation Inc. Lists CF6-80C2A1
- [STC SA2227SO](https://openairdocs.org/stc/SA2227SO): Installation of wiring and associated components for utilization of the Rolls Royce, Inc., ARINC, interface/readers UT1317 or UT1317/1, for the purpose of acquisition, recording, and analysis in real time of engine/aircraft/ systems. (767 SERIES POWERED BY RR RB-11-524 SERIES. Rolls Royce, Inc

## Related

- Other Boeing 747-47UF aircraft: https://openairdocs.org/model/boeing-747-47uf/aircraft.md
- The GE CF6-80 series engine: https://openairdocs.org/engine/ge-cf6-80-series.md

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