# N415MC: 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: 32837 - Year built: 2002 - Type: Fixed wing multi engine - Engine type: Turbo-fan - Airworthiness: Standard, transport - Airworthiness date: May 1, 2002 - Certificate issued: June 28, 2002 - Expires: August 31, 2027 - Mode S code: A4E7C9 - Registered owner: [U S Bank Na Trustee](https://openairdocs.org/faa-owner/U%20S%20BANK%20NA%20TRUSTEE) - Location: [Seattle, WA](https://openairdocs.org/faa-place/WA/Seattle) - Owner type: Corporation - Owner's area on the map: 47.6109° N, 122.3364° W: Placed by OpenAirDocs at the center of ZIP code 98101, 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=415MC - Page: https://openairdocs.org/aircraft/N415MC 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/N415MC/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 DCA18WA287](https://openairdocs.org/ntsb/DCA18WA287), Aug 30, 2018: Boeing 747 (N415MC), Hong Kong, Hong Kong SAR China, incident, minor damage ## FAA accident and incident reports (1) From the FAA Accident/Incident Data System. Reports are matched to registry aircraft by N-number and event date, checked against the reported make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model. - [Incident 20180830018959I](https://openairdocs.org/incident/20180830018959I), Aug 30, 2018: Boeing 747-47UF (N415MC), Hong Kong, Minor damage. On August 30, 2018 an atlas air Boeing 747-47UF (freighter aircraft), registration number N415MC, operating as atlas air flight gti 8060 departed al maktoum… ## Service difficulty reports (147, 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 UIEA2026091700882](https://openairdocs.org/sdr/UIEA2026091700882), Sep 17, 2026: ENGINE. VIBRATION. MULTIPLE ALT VIBRATIONS FELT FIRST THEN INDICATIONS ON NR 1 ENG UP TO 5.0. ACCOMPLISHED VIBE SURVEY ENGINE SUCCESSFULLY BALANCED N1 AT 0.6 AT 99% N1 IAW AMM 71- - [SDR UIEA2026040600131](https://openairdocs.org/sdr/UIEA2026040600131), Apr 6, 2026: DOUBLER. DAMAGED. DEVIATION - DURING PERFORM SB 4453A749 PART 12 L/H DOUBLER HAVE 1 EA EXISTING HOLE SHORT E/M AND FIGURE 27 NOT SHOW FL 49. ACCOMPISHED EI T2026A53M-507 REV 1 AN - [SDR UIEA2026040600132](https://openairdocs.org/sdr/UIEA2026040600132), Apr 6, 2026: FITTING. DAMAGED. DEVIATION - DURING PERFORM SB 4453B761 PART 1-2, R/H UPPER SPLICE FITTING EXISTING HOLE IS 0.341". ACCOMPLISHED EI T2026A53M-528 REV 1 AND EI ATTACHED TO W/O 12 - [SDR UIEA2026040600133](https://openairdocs.org/sdr/UIEA2026040600133), Apr 6, 2026: FITTING. CRACKED. CRACKED DURING PERFORM SB 4453B761 PART 1-2, RT UPPER SPLICE FITTING HAVE 1 HOLE CRACK. ACCOMPLISHED EI T2026A53M-528 REV 1, AND DWG 65B02705, SH 4 REV D, SH 6 - [SDR UIEA2026040600134](https://openairdocs.org/sdr/UIEA2026040600134), Apr 6, 2026: SEAT TRACK. CRACKED. CRACKED M/D SUBSTITUTE SEAT TRACK AT BS 1480, LBL 75.92. REMOVED AFFECTED FASTENERS TO GET ACCESS IAW SRM 51-40-02-0G-0 REV 106. REPAIR DAMAGE AREA IAW W/S 6014 - [SDR UIEA2026040600135](https://openairdocs.org/sdr/UIEA2026040600135), Apr 6, 2026: SEAT TRACK. CRACKED. CRACKED M/D SEAT TRACK AT BS 1500, LBL 98.58. REMOVED DAMAGED PARTS IAW SRM 51-40-02-0G-0 REV 106. ACCOMPLISHED WORK SHEET 60150 AND EI T2026A53M-562 REV 1 AND - [SDR UIEA2026040600136](https://openairdocs.org/sdr/UIEA2026040600136), Apr 6, 2026: SKIN. CORRODED. CORRODED SKIN, LT MLG FWD BULKHEAD AT CENTER WING TANK JETTISON PUMP, LEFT M224, BONDING JUMPER ATTACHED. ACCOMPLISHED THE EI T2026A57M-398 REV 5. CONDITION CHE - [SDR UIEA2026040600137](https://openairdocs.org/sdr/UIEA2026040600137), Apr 6, 2026: SKIN. CORRODED. CORRODED SKIN, RT MLG FWD BULKHEAD AT CENTER WING TANK JETTISON PUMP, LEFT M225, BONDING JUMPER ATTACHED. REPAIR THE CORROSION AREA IAW EI T2026A57M-397 REV 3 S - [SDR UIEA2026040600139](https://openairdocs.org/sdr/UIEA2026040600139), Apr 6, 2026: CHANNEL. CRACKED. CRACKED CHANNEL, FOUND MAIN ENTRY DOOR 1 UPPER MAIN SILL NEAR STA 460 S16L. REMOVED DAMAGED PARTS IAW SRM 51-40-02-0G-0 REV 106. FABRICATED NEW PARTS IAW EI T20 - [SDR UIEA2026040600140](https://openairdocs.org/sdr/UIEA2026040600140), Apr 6, 2026: FRAME. CRACKED. CRACKED FRAME AND CHANNEL, BS 820 S9-10R. REMOVED AFFECTED FASTENERS IAW SRM 51-40-02-0G-0 REV 106. REPAIRED DAMAGE AREA IAW W/S 60165 AND SRM 53-20-07-2R-2 REV - [SDR UIEA2026040600141](https://openairdocs.org/sdr/UIEA2026040600141), Apr 6, 2026: TENSION TIE. CRACKED. CRACKED TENSION TIE, STA 820 S9-10R. REMOVED AFFECTED FASTENERS TO GET ACCESS IAW SRM 51-40-02-0G-0 REV 106. REPAIRED DAMAGE AREA IAW W/S 60174 AND W/S 60169 AN - [SDR UIEA2026040600142](https://openairdocs.org/sdr/UIEA2026040600142), Apr 6, 2026: FRAME. CRACKED. CRACKED FRAME, BS 840 S-9-10R. REMOVED AFFECTED FASTENERS TO GET ACCESS IAW SRM 51-40-02-0G-0 REV 106. PERFORMED EI T2026A53M-586 REV 0. INSTALLED FASTENERS IAW - [SDR UIEA2026040700145](https://openairdocs.org/sdr/UIEA2026040700145), Apr 6, 2026: FRAME. CRACKED. CRACKED FRAME, BS 860, S9 -10R. REMOVED AFFECTED FASTENERS TO GET ACCESS IAW SRM 51-40-02-0G-0 REV 106. PERFORMED EI T2026A53M-590 REV 0. INSTALLED FASTENERS IA - [SDR UIEA2026040700147](https://openairdocs.org/sdr/UIEA2026040700147), Apr 6, 2026: RETAINER. CORRODED. CORRODED RETAINER, RT WLG W/W UNDERWING REAR SPAR FAIRING AND VAPOR BARRIER CORNER AREA SEAL. REMOVE DAMAGED PART IAW SRM 51-40-02-0G-0 REV 106. INSTALL NEW PAR - [SDR UIEA2026040700148](https://openairdocs.org/sdr/UIEA2026040700148), Apr 6, 2026: BRACKET. CORRODED. FOUND NR 1 PACK BRACKET CORROSION AT #1 COMPRESSOR BYPASS VALVE OUTBD SIDE AT STA 1028.86 LBL 57.7. REMOVED DAMAGED PARTS IAW SRM 51-40-02-0G-0 REV 106. 2. INST - [SDR UIEA2025052800702](https://openairdocs.org/sdr/UIEA2025052800702), May 29, 2025: ACTUATOR. FAULTED. GEAR CONFIG WARNING ON TAKEOFF. R & R BODY L/H ACTUATOR AND OPS CHECK GOOD IAW AMM 32-53-11 & IPC 32-53-11-05A ITEM 65. - [SDR UIEA2025010400002](https://openairdocs.org/sdr/UIEA2025010400002), Jan 4, 2025: VALVE. FAULTED. ENG 4 T/R EICAS CAUTION MESSAGE(

REMOVED AND REPLACED #4 ENGINE DIRECTIONAL PILOT VALVE IAW AMM 78-34-01/401. OPS CHECK NORMAL. DMI 223578 CLOSED

) - [SDR UIEA2024042400313](https://openairdocs.org/sdr/UIEA2024042400313), Apr 24, 2024: ENGINE. MAKING METAL. CAUTION MESSAGE (EICAS) ENG 4 OIL FILTER IN FLIGHT. TIME 0910Z. FIRE HANDLE NOT PULLED. ENG SHUTDOWN.(

C/W OIL SYS CONTAMINATION EXAMINATION IAW AMM 79-00-00, - [SDR UIEA2024012600044](https://openairdocs.org/sdr/UIEA2024012600044), Jan 26, 2024: ROTOR. UNKNOWN. ENG 3 CONTROL STS MSG. SUSPECT EEC FAILURE(

R/R #3 EEC & ROTOR OF CONTROL ALTERNATOR. OPS CHECK GOOD IAW AMM 73-21-08 & AMM 73-21-15. DMI 201757 CLOSE - [SDR UIEA2023040300304](https://openairdocs.org/sdr/UIEA2023040300304), Apr 2, 2023: SWITCH. UNKNOWN. ON TAKE-OFF, N1 ON #1 ENGINE ONLY PRODUCED 42% THRUST(

FOUND #1 THRUST REVERSER POSITION FEEDBACK SENSOR OUT OF ADJUSTMENT READING 28.0. ADJUSTED IAW B747-700 - [SDR UIEA2022051900492](https://openairdocs.org/sdr/UIEA2022051900492), May 19, 2022: STRAP. DISPLACED. FLAPPING AND RUSHING AIR SOUND COMING FROM UPPER DECK SERVICE DOOR AT 10,500 FT(

FOUND DOOR STRAP INHIBITING DOOR SEAL, REMOVED DOOR STRAP, DOOR CLOSED PROPER - [SDR UIEA2022021500135](https://openairdocs.org/sdr/UIEA2022021500135), Mar 1, 2022: SKIN. CRACKED. #3 ENG RH CORE COWL EXHAUST LWR RIVETS HOLES FOUND CRACKED(

#3 ENG RH CORE COWL PRECOOLER LOWER SKIN CRACK AREA EXTERNAL DOUBLER REPAIRED

) - [SDR UIEA2022021600139](https://openairdocs.org/sdr/UIEA2022021600139), Mar 1, 2022: DOUBLER. CRACKED. M/D LH #5 DOOR FWD CUTOUT STA 2231 DOOR REVEAL DOUBLER BETWEEN STR 21L AND STR 22L FOUND CRACKED(

M/D LH #5 DOOR FWD CUTOUT STA 2231 DOOR REVEAL DOUBLER BETWE - [SDR UIEA2022021700144](https://openairdocs.org/sdr/UIEA2022021700144), Mar 1, 2022: FRAME. CHAFED. #1 ENG L/H CORE COWL INNER NO.4 FRAME MID AREA FOUND CHAFING DAMAGE(

#1 ENG LH CORE COWL INNER NO.4 FRAME MID CHAFING DAMAGE AREA EXTERNAL PATCH REPAIRED

) - [SDR UIEA2022021700145](https://openairdocs.org/sdr/UIEA2022021700145), Mar 1, 2022: SKIN. DENTED. RHW #18 VC-FLAP BALLNOSE SKIN LWR MID AREA FOUND DENT(

RHW #18 VC-FLAP BALLNOSE SKIN LWR MID OUT OF LIMITS DENT AREA EXTERNAL DOUBLER REPAIRED

) - [SDR UIEA2022022100151](https://openairdocs.org/sdr/UIEA2022022100151), Mar 1, 2022: BATTERY. FAILED. EMERGENCY LIGHT TEST FOUND POWER SUPPLY BATT M5169 FAILED(

REPLACED POWER SUPPLY BATT M5169 IAW AMM 33-51-04 AND TEST PASS

) - [SDR UIEA2022022100152](https://openairdocs.org/sdr/UIEA2022022100152), Mar 1, 2022: BATTERY. FAILED. EMERGENCY LIGHT TEST FOUND POWER SUPPLY BATT M5170 FAILED(

REPLACED POWER SUPPLY BATT M5170 IAW AMM 33-51-04 AND TEST PASS

) - [SDR UIEA2022022200153](https://openairdocs.org/sdr/UIEA2022022200153), Mar 1, 2022: FLAP. DELAMINATED. RHW O/B MID FLAP L/E FOUND DELAMINATION(

PERFORMED REPAIR AS PER SRM 51-70-07 PAR.5A

) - [SDR UIEA2022022200154](https://openairdocs.org/sdr/UIEA2022022200154), Mar 1, 2022: FLAP. DELAMINATED. RHW I/B MID FLAP L/E FOUND DELAMINATION(

PERFORMED REPAIR AS PER SRM 51-70-07 PAR.5A

) - [SDR UIEA2022022200155](https://openairdocs.org/sdr/UIEA2022022200155), Mar 1, 2022: FLAP. DELAMINATED. LHW I/B MID FLAP L/E FOUND DELAMINATION(

PERFORMED REPAIR AS PER SRM 51-70-07 PAR.5A

) - [SDR UIEA2022022200156](https://openairdocs.org/sdr/UIEA2022022200156), Mar 1, 2022: FLAP. DELAMINATED. LHW O/B MID FLAP L/E FOUND DELAMINATION(

PERFORMED REPAIR AS PER SRM 51-70-07 PAR.5A

) - [SDR UIEA2022022200157](https://openairdocs.org/sdr/UIEA2022022200157), Mar 1, 2022: FLAP. DELAMINATED. LHW O/B FORE FLAP L/E FOUND DELAMINATION(

PERFORMED REPAIR AS PER SRM 51-70-07 PAR.5A

) - [SDR UIEA2022022200158](https://openairdocs.org/sdr/UIEA2022022200158), Mar 1, 2022: FLAP. DELAMINATED. RHW O/B AFT FLAP AFT O/B CORNER FOUND DELAMINATION(

PERFORMED REPAIR AS PER SRM 51-70-07 PAR.5G

) - [SDR UIEA2022022200159](https://openairdocs.org/sdr/UIEA2022022200159), Mar 1, 2022: FLAP. DELAMINATED. LHW O/B FORE FLAP L/E FOUND DELAMINATION(

PERFORMED REPAIR AS PER SRM 51-70-07 PAR.5A

) - [SDR UIEA2022022200160](https://openairdocs.org/sdr/UIEA2022022200160), Mar 1, 2022: FLAP. DELAMINATED. RHW O/B FORE FLAP L/E FOUND DELAMINATION(

PERFORMED REPAIR AS PER SRM 51-70-07 PAR.5A

) - [SDR UIEA2022022200161](https://openairdocs.org/sdr/UIEA2022022200161), Mar 1, 2022: FLAP. DELAMINATED. LHW O/B AFT FLAP L/E FOUND DELAMINATION(

PERFORMED REPAIR AS PER SRM 51-70-07 PAR.5A

) - [SDR UIEA2022022200162](https://openairdocs.org/sdr/UIEA2022022200162), Mar 1, 2022: FLAP. DELAMINATED. RHW O/B FORE FLAP L/E FOUND DELAMINATION(

PERFORMED REPAIR AS PER SRM 51-70-07 PAR.5A

) - [SDR UIEA2022022200163](https://openairdocs.org/sdr/UIEA2022022200163), Mar 1, 2022: RIB. CRACKED. RHW I/B MID FLAP O/B RIB AFT ANGLE (CLIP) FOUND CRACKED(

FABRICATE THE REPLACEMENT ANGLE (CLIP) FROM 70757651 BARD PLATE. AND REPLACED AND INSTALLED.

) - [SDR UIEA2022022300164](https://openairdocs.org/sdr/UIEA2022022300164), Mar 1, 2022: SHEAR TIE. CRACKED. STA 1000 FRONT SPAR UPPER RBL 33.99" ATTACH SHEAR TIE FOUND CRACKED(

USING 69B14267U11 SHEAR TIP IN LIEU OF 69B14267U9 SHEAR TIE REPLACED AND INSTALLED

) - [SDR UIEA2022022300165](https://openairdocs.org/sdr/UIEA2022022300165), Mar 1, 2022: ACCESS PANEL. ELONGATED. #2 PYLON VALVE ACCESS PNL #462EL 1EA BOLT HOLE ELONGATED(

#2 PYLON VALVE ACCESS PNL #462EL 1EA ELONGATED BOLT HOLE AREA DOUBLER REPAIRED AS PER RI-54-50-15404 - [SDR UIEA2022022300166](https://openairdocs.org/sdr/UIEA2022022300166), Mar 1, 2022: ACCESS PANEL. ELONGATED. #3 PYLON VALVE ACCESS PNL #472EL 2EA BOLT HOLES ELONGATED(

#3 PYLON VALVE ACCESS PNL #472EL 2EA ELONGATED BOLT HOLES AREA DOUBLER REPAIRED AS PER RI-54-50-154 - [SDR UIEA2022022300167](https://openairdocs.org/sdr/UIEA2022022300167), Mar 1, 2022: ACCESS PANEL. ELONGATED. #1 PYLON VALVE ACCESS PNL #452EL 1EA BOLT HOLE ELONGATED(

#1 PYLON VALVE ACCESS PNL #452EL 1EA ELONGATED BOLT HOLE AREA DOUBLER REPAIRED AS PER RI-54-50-15405 - [SDR UIEA2021102202275](https://openairdocs.org/sdr/UIEA2021102202275), Oct 22, 2021: NONE. NONE. ENG #1 WOULD NOT ACCELERATE OVER 50% N1 DURING TAKEOFF(

PERFORMED RIGGING OF ENG 1 RH TR FEED BACK ACTUATOR CDU. OPERATIONAL CHECK OKAY REF AMM 78-31-00/501 A - [SDR UIEA2021042300986](https://openairdocs.org/sdr/UIEA2021042300986), Apr 23, 2021: PDU. FAULTED. FLAPS DRIVE MSG(

REMOVED AND REPLACED R4 FLAP PDU. OPS OK IN BOTH MODE PER AMM 27-81-03.

) - [SDR UIEA2021031700609](https://openairdocs.org/sdr/UIEA2021031700609), Mar 17, 2021: EICAS. WARNING MESSAGE. ATB #4 ENGINE SHUTDOWN IN FLIGHT DUE TO LOW OIL PRESSURE, ENG 4 OIL PRESS EICAS MESSAGE. #4 OIL QTY 0 - OIL PRESS 4 WHILE WINDMILLING.(

REMOVED AND REP - [SDR UIEA2021011700068](https://openairdocs.org/sdr/UIEA2021011700068), Jan 17, 2021: ESCAPE REEL. DAMAGED. COCKPIT DESCENT DEVICE "C" SEAL DAMAGE CABLE OVEREXTENDED. REMOVED AND REPLACED DESCENT DEVICE POSITION "C", IAW AMM 25-61-01, NO DISCREPANCIES FOUND. - [SDR UIEA2021011700069](https://openairdocs.org/sdr/UIEA2021011700069), Jan 17, 2021: ESCAPE REEL. DAMAGED. COCKPIT DESCENT DEVICE "B" SEAL DAMAGE CABLE OVEREXTENDED. REMOVED AND REPLACED DESCENT DEVICE POSITION "B", IAW AMM 25-61-05. NO DISCREPANCIES FOUND. - [SDR UIEA2021011700070](https://openairdocs.org/sdr/UIEA2021011700070), Jan 17, 2021: ESCAPE REEL. DAMAGED. COCKPIT DESCENT DEVICE "A" SEAL DAMAGE CABLE OVEREXTENDED. REMOVED AND REPLACED DESCENT DEVICE POSITION "A", IAW AMM 25-61-01. NO DISCREPANCIES NOTED. - [SDR UIEA2020031700473](https://openairdocs.org/sdr/UIEA2020031700473), Mar 14, 2020: SKIN. DEBONDED. DISBOND - SKIN, OUTBD SIDE OF R/H WING INBD AILERON T/E SKIN, WBL 515.(

REMOVE THE DAMAGE MATERIAL AND CLEAN. MEASURE THE DAMAGED AREA (L = 2", W = 0.1", 1" F - [SDR UIEA2020031700476](https://openairdocs.org/sdr/UIEA2020031700476), Mar 14, 2020: SEAT TRACK. CORRODED. CORROSION ON THE MAIN DECK SEAT TRACK AT STA 2175, RBL 11.33.(

REPAIR DAMAGED SEAT TRACK IAW SRM 53-00-52-2R-12 REPAIR 12 REV. 88 AND EI NO T2020-A53M-662 REV All 147: https://openairdocs.org/aircraft/N415MC/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 --- 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.