# N487MC: 2002 Boeing 747-45EF

- Status: Valid registration
- Airframe: [Boeing 747-45EF](https://openairdocs.org/model/boeing-747-45ef) (registry code 1384961, 495 seats)
- Engine: [GE CF6-80C2B1F](https://openairdocs.org/engine/ge-cf6-80c2b1f) (registry code 30106)
- Data sheets: [TCDS E13NE](https://openairdocs.org/tcds/E13NE) (General Electric Company GE Aerospace) (OpenAirDocs)
- Serial number: 30609
- Year built: 2002
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: September 5, 2018
- Certificate issued: August 23, 2018
- Expires: August 31, 2028
- Mode S code: A603B0
- Registered owner: [Umb Bank Na Trustee](https://openairdocs.org/faa-owner/UMB%20BANK%20NA%20TRUSTEE)
- Location: [Salt Lake City, UT](https://openairdocs.org/faa-place/UT/Salt%20Lake%20City)
- Owner type: Corporation
- Owner's area on the map: 40.6171° N, 111.6866° W: Placed by OpenAirDocs at the center of ZIP code 84121, within about 5 miles (OpenAirDocs). The owner's mailing address, not where the aircraft is based
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=487MC
- Page: https://openairdocs.org/aircraft/N487MC

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): 33 in force

### Matched by airframe (Boeing 747-45EF)

None in force.

### Matched by engine (GE CF6-80C2B1F)

- [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 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 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 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 2009-07-03](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 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 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 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 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 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 95-10-11](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 94-06-03](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
- [AD 93-14-18](https://openairdocs.org/ad/93-14-18): High pressure turbine (HPT) thermal shields · General Electric CF6-45A, CF6-45A2, CF6-50A and 40 more. Effective Oct 4, 1993
- [AD 91-15-25](https://openairdocs.org/ad/91-15-25): High Pressure Compressor Rotor · General Electric CF6-80A, CF6-80A1, CF6-80A2 and 16 more. Effective Sep 6, 1991
- [AD 91-11-05](https://openairdocs.org/ad/91-11-05): High Pressure Compressor Rotor · General Electric CF6-80A, CF6-80A1, CF6-80A2 and 16 more. Effective Jul 5, 1991

### 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 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 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 2000-16-12](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 99-08-13](https://openairdocs.org/ad/99-08-13) (historical): General Electric CF6-80A, CF6-80A1, CF6-80A2 and 26 more. Effective May 13, 1999
- [AD 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

## 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

None matched to N487MC.

## FAA accident and incident reports

None matched to N487MC.

## Service difficulty reports (181, 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 UIEA2026072400648](https://openairdocs.org/sdr/UIEA2026072400648), Jul 24, 2026: FLOORBEAM. DAMAGED. CORROSION DAMAGE ON FLOORBEAM UPPER TEE BS 2240 NEAR LBL 36. REPAIRED DAMAGE FLOORBEAM IAW EI T2026A53M-1294, REV 0, AND W/O 60480, SRM 53-00-51-1R-3, REV 107. 
- [SDR UIEA2026072400649](https://openairdocs.org/sdr/UIEA2026072400649), Jul 24, 2026: PIN. DAMAGED. FOUND NR 3 PYLON UPPER LINK FWD PIN AND BUSHING DAMAGE AND PYLON SIDE LUG BUSHING DAMAGE. IAW AMM 54-51-01-004-001 REV 116 AND AMM 54-51-02-004-001-005 REV 116,
- [SDR UIEA2026072400650](https://openairdocs.org/sdr/UIEA2026072400650), Jul 24, 2026: LINK. DAMAGED. FOUND NR 1 PYLON LINK AFT SIDE BOLT, WASHER, NUT DAMAGE, AND WING LUG BUSHING DAMAGE. IAW AMM 54-51-01-004-001 REV 116 AND AMM 54-51-02-004-001-005 REV 116, REM
- [SDR UIEA2026072400651](https://openairdocs.org/sdr/UIEA2026072400651), Jul 24, 2026: BUSHING. GOUGED. FOUND NR 2 PYLON UPPER LINK FWD AND AFT SIDE PIN AND BUSHING, BEARING GOUGE AND WING LUG, PYLON LUG BISHING GOUGE. IAW AMM 54-51-01-004-001 REV 116 AND AMM 54- 
- [SDR UIEA2026072400652](https://openairdocs.org/sdr/UIEA2026072400652), Jul 24, 2026: RETAINER. CORRODED. CORROSION RETAINER R/H WING L/G W/W FWD OUTBD SIDE LWR SUPPORT NEAR WBL 128.45. REMOVED DAMAGE PART IAW SRM 51-40-02-06-0 REV 107. INSTALLED NEW PART IAW SRM 51
- [SDR UIEA2026072400653](https://openairdocs.org/sdr/UIEA2026072400653), Jul 24, 2026: BATTERY. NO TEST. FOUND EMERGENCY LIGHT BATTERY M5170 FUNCTION FAIL(<P>1. IAW AMM 33-51-04-902-001-001 REV 107 REPLACED EMERGENCY LIGHT BATTERY PACK (M5170) AT UPPER DECK, CONDIT
- [SDR UIEA2026051300313](https://openairdocs.org/sdr/UIEA2026051300313), May 13, 2026: OXYGEN BOTTLE. LOW PRESSURE. CREW OXY LOW EICAS MESSAGE. OXY LEVEL SHOWS 250. TRANSFER TO DMI 252465 PER MEL 35-11-02 CAT C DUE DATE 23MAY26. DETERMINED IT WAS AN INDICATION PROBLEM.
- [SDR UIEA2026050500294](https://openairdocs.org/sdr/UIEA2026050500294), May 5, 2026: TRANSDUCER. FAULTED. CREW OXYGEN LOW IN FLIGHT. FOUND 2 EA CONNECTORS AT BOTTLE LOOSE, SECURED AND VERIFIED INDICATION WAS OPERATIONAL. DEFERRED O2 INDICATION SYSTEM AS PRECAUTION. 
- [SDR UIEA2026042900264](https://openairdocs.org/sdr/UIEA2026042900264), Apr 28, 2026: ENGINE. POWER LOSS. UPON SETTING TAKEOFF THRUST, ENGINE 4 DID NOT SPOOL UP. FOLLOWED FIM 71-00 TO BLOCK 43, ENGINE OPERATED NORMAL, NO DAMAGE FOUND TO ABRADABLE SHROUD OR FAN BLADE
- [SDR UIEA2025122401357](https://openairdocs.org/sdr/UIEA2025122401357), Dec 24, 2025: SKIN. PUNCTURED. LEFT WING INBD AFT FLAP LE ENGINE LOWER SURFACE HAS A PUNCTURE. 36" OUTBD OF ACCORDION SEAL. REPAIRED SMALL PUNCTURE 1/2" ON LH INBD AFT FLAP LEADING EDGE 501/2
- [SDR UIEA2025122401358](https://openairdocs.org/sdr/UIEA2025122401358), Dec 24, 2025: SKIN. DAMAGED. LT WING OTBD FORE FLAP OTBD END LOWER SURFACE L/E DAMAGED ABOUT 6 INCHES INBD OF OTBD EDGE(<P>PERMANENT COMPOSITE REPAIR MADE TO LH WING OTBD FORE FLAP LOWER SU
- [SDR UIEA2025113001331](https://openairdocs.org/sdr/UIEA2025113001331), Nov 30, 2025: VALVE. FAULTED. BLEED 4 CAUTION MSG ON CLIMB OUT. MSG 36229. REPLACED NR 4 PRVC AND CHECKED NORMAL PER AMM 36-11-20/401 &AMP; IPC 36-11-19-01</P>)
- [SDR UIEA2025081401123](https://openairdocs.org/sdr/UIEA2025081401123), Aug 14, 2025: AUDIO PANEL. ODOR. STRONG SMELL OF BURNING WIRE IN COCKPIT DURING PREFLIGHT. PERFORMED SMOKE OR FUME IN CABIN INSPECTION IAW FIM 21-00TASK 810. FOUND F/O CONTROL AUDIO PANEL BAD W
- [SDR UIEA2025062600815](https://openairdocs.org/sdr/UIEA2025062600815), Jun 30, 2025: WEB. CRACKED. LEFT WING T/E CAVITY SUPPORT RIB WEB AT NR 5 SPOILER INBD LWR WBL 432.65 FOUND CRACKED. LT WING T/E CAVITY SUPPORT RIB WEB (P/N: 6565B10865-26) AT NR 5 SPOILER 
- [SDR UIEA2025011900089](https://openairdocs.org/sdr/UIEA2025011900089), Jan 19, 2025: PACKING. LEAKING. ENG 2 OIL QTY DROPPED FROM 20Q TO 9Q, FOLLOWED BY A DROP FROM 8 TO 7 TO 6 ABOUT EVERY HALF HOUR. FOUND ENG #2 LOW PRESSURE WARNING SWITCH PACKING INSTALLED IN W
- [SDR UIEA2024112501112](https://openairdocs.org/sdr/UIEA2024112501112), Nov 26, 2024: WINDOW. LEAKING. CLIMBING THROUGH 18,000' AND 6 PSI DIFFERENTIAL. A LOUD SQUEAL BEGAN FROM ONE OF THE CAPTAIN SIDE WINDOWS. DIFFICULT TO ASCERTAIN WHICH WINDOW BUT IT SEEMINGLY 
- [SDR UIEA2024072700756](https://openairdocs.org/sdr/UIEA2024072700756), Jul 27, 2024: SMOKE DETECTOR. FAULTED. DURING CRUISE FL310 EICAS CAUTION EQUIPMENT COOLING PERFORMED NNC, MESSAGE BLANKED, SMELLED ELECTRICAL BURNING, DIVERTED TO CTS.(<P>CMC REPORTED MX MSG 21422. R
- [SDR UIEA2024062000561](https://openairdocs.org/sdr/UIEA2024062000561), Jul 17, 2024: SKIN. DENTED. FUSELAGE SECTION 41 DENT/NICK DAMAGE FOUND ON FUSELAGE SKIN (PN 65B12874) AT STA 284 APPROXIMATELY NEAR STR 10R(<P>DAMAGE AREA REPAIRED AS PER RI-53-10-16982 RE
- [SDR UIEA2024062000562](https://openairdocs.org/sdr/UIEA2024062000562), Jul 17, 2024: FRAME. CRACKED. #2 ENG L/H CORE COWL #2 FRAME (COUNT FROM FWD) FOUND CHAFING MARK.(<P>#2 FRAME CHAFING MARK AREA REPAIRED AS PER SRM 54-45-02-2R-1 REPAIR 1 FIG 201. NO FURTHER 
- [SDR UIEA2024062000563](https://openairdocs.org/sdr/UIEA2024062000563), Jul 17, 2024: FRAME. CRACKED. #2 ENG L/H CORE COWL MOST AFT FRAME FOUND CRACK.(<P>FRAME CRACK AREA REPAIRED AS PER SRM 54-45-02-2R-2 REPAIR 2 FIG 201. NO FURTHER DEFECTS NOTED</P>)
- [SDR UIEA2024070600586](https://openairdocs.org/sdr/UIEA2024070600586), Jul 17, 2024: SKIN. DELAMINATED. LHW I/B FORE FLAP FOUND DELAMINATION(<P>PERFORMED REPAIR AT DELAMINATION AREA PER SRM 51-70-07 PAR 5.A (1). NO FURTHER DEFECTS NOTED.</P>)
- [SDR UIEA2024070600587](https://openairdocs.org/sdr/UIEA2024070600587), Jul 17, 2024: SKIN. DELAMINATED. LHW I/B FORE FLAP FOUND DELAMINATION(<P>PERFORMED REPAIR AT DELAMINATION AREA PER SRM 51-70-07 PAR 5.A (1). NO FURTHER DEFECTS NOTED.</P>)
- [SDR UIEA2024070600588](https://openairdocs.org/sdr/UIEA2024070600588), Jul 17, 2024: SKIN. DELAMINATED. LHW I/B FORE FLAP FOUND DELAMINATION(<P>PERFORMED REPAIR AT DELAMINATION AREA PER SRM 51-70-07 PAR 5.A (1). NO FURTHER DEFECTS NOTED.</P>)
- [SDR UIEA2024070600589](https://openairdocs.org/sdr/UIEA2024070600589), Jul 17, 2024: SKIN. DELAMINATED. LHW I/B FORE FLAP FOUND DELAMINATION(<P>PERFORMED REPAIR AT DELAMINATION AREA PER SRM 51-70-07 PAR 5.A (1). NO FURTHER DEFECTS NOTED.</P>)
- [SDR UIEA2024070600590](https://openairdocs.org/sdr/UIEA2024070600590), Jul 17, 2024: SKIN. DELAMINATED. LHW I/B FORE FLAP FOUND DELAMINATION. PERFORMED REPAIR AT DELAMINATION AREA PER SRM 51-70-07 PAR 5.A (1). NO FURTHER DEFECTS NOTED.
- [SDR UIEA2024070600591](https://openairdocs.org/sdr/UIEA2024070600591), Jul 17, 2024: SKIN. DELAMINATED. LHW I/B MID FLAP FOUND DELAMINATION(<P>PERFORMED REPAIR AT DELAMINATION AREA PER SRM 51-70-07 PAR 5.A (1). NO FURTHER DEFECTS NOTED.</P>)
- [SDR UIEA2024070600592](https://openairdocs.org/sdr/UIEA2024070600592), Jul 17, 2024: SKIN. DELAMINATED. LHW I/B MID FLAP FOUND DELAMINATION(<P>PERFORMED REPAIR AT DELAMINATION AREA PER SRM 51-70-07 PAR 5.A (1). NO FURTHER DEFECTS NOTED.</P>)
- [SDR UIEA2024070600593](https://openairdocs.org/sdr/UIEA2024070600593), Jul 17, 2024: SKIN. DELAMINATED. LHW I/B MID FLAP FOUND DELAMINATION(<P>PERFORMED REPAIR AT DELAMINATION AREA PER SRM 51-70-07 PAR 5.A (1). NO FURTHER DEFECTS NOTED.</P>)
- [SDR UIEA2024070600594](https://openairdocs.org/sdr/UIEA2024070600594), Jul 17, 2024: SKIN. DELAMINATED. LHW I/B MID FLAP FOUND DELAMINATION(<P>PERFORMED REPAIR AT DELAMINATION AREA PER SRM 51-70-07 PAR 5.A (1). NO FURTHER DEFECTS NOTED.</P>)
- [SDR UIEA2024070600595](https://openairdocs.org/sdr/UIEA2024070600595), Jul 17, 2024: SKIN. DELAMINATED. LHW I/B MID FLAP FOUND DELAMINATION(<P>PERFORMED REPAIR AT DELAMINATION AREA PER SRM 51-70-07 PAR 5.A (1). NO FURTHER DEFECTS NOTED.</P>)
- [SDR UIEA2024070600596](https://openairdocs.org/sdr/UIEA2024070600596), Jul 17, 2024: SKIN. DELAMINATED. LHW I/B MID FLAP FOUND DELAMINATION(<P>PERFORMED REPAIR AT DELAMINATION AREA PER SRM 51-70-07 PAR 5.A (1). NO FURTHER DEFECTS NOTED.</P>)
- [SDR UIEA2024071000622](https://openairdocs.org/sdr/UIEA2024071000622), Jul 17, 2024: SKIN. DELAMINATED. LHW O/B FORE FLAP FOUND DELAMINATION(<P>PERFORMED REPAIR AT DELAMINATION AREA PER SRM 51-70-07 PAR 5.A (1). NO FURTHER DEFECTS NOTED.</P>)
- [SDR UIEA2024071000623](https://openairdocs.org/sdr/UIEA2024071000623), Jul 17, 2024: SKIN. DELAMINATED. LHW O/B FORE FLAP FOUND DELAMINATION(<P>PERFORMED REPAIR AT DELAMINATION AREA PER SRM 51-70-07 PAR 5.A (1). NO FURTHER DEFECTS NOTED.</P>)
- [SDR UIEA2024071000624](https://openairdocs.org/sdr/UIEA2024071000624), Jul 17, 2024: SKIN. DELAMINATED. LHW O/B FORE FLAP FOUND DELAMINATION(<P>PERFORMED REPAIR AT DELAMINATION AREA PER SRM 51-70-07 PAR 5.A (1). NO FURTHER DEFECTS NOTED</P>)
- [SDR UIEA2024071000625](https://openairdocs.org/sdr/UIEA2024071000625), Jul 17, 2024: SKIN. DELAMINATED. LHW O/B FORE FLAP FOUND DELAMINATION(<P>PERFORMED REPAIR AT DELAMINATION AREA PER SRM 51-70-07 PAR 5.A (1). NO FURTHER DEFECTS NOTED</P>)
- [SDR UIEA2024071000626](https://openairdocs.org/sdr/UIEA2024071000626), Jul 17, 2024: SKIN. DELAMINATED. RHW O/B FORE FLAP FOUND DELAMINATION(<P>PERFORMED REPAIR AT DELAMINATION AREA PER SRM 51-70-07 PAR 5.A (1). NO FURTHER DEFECTS NOTED.</P>)
- [SDR UIEA2024071000627](https://openairdocs.org/sdr/UIEA2024071000627), Jul 17, 2024: SKIN. DELAMINATED. RHW O/B FORE FLAP FOUND DELAMINATION(<P>PERFORMED REPAIR AT DELAMINATION AREA PER SRM 51-70-07 PAR 5.A (1). NO FURTHER DEFECTS NOTED</P>)
- [SDR UIEA2024071000628](https://openairdocs.org/sdr/UIEA2024071000628), Jul 17, 2024: SKIN. DELAMINATED. RHW O/B FORE FLAP FOUND DELAMINATION(<P>PERFORMED REPAIR AT DELAMINATION AREA PER SRM 51-70-07 PAR 5.A (1). NO FURTHER DEFECTS NOTED.</P>)
- [SDR UIEA2024071000629](https://openairdocs.org/sdr/UIEA2024071000629), Jul 17, 2024: SKIN. DELAMINATED. RHW O/B FORE FLAP FOUND DELAMINATION(<P>PERFORMED REPAIR AT DELAMINATION AREA PER SRM 51-70-07 PAR 5.A (1). NO FURTHER DEFECTS NOTED</P>)
- [SDR UIEA2024071000630](https://openairdocs.org/sdr/UIEA2024071000630), Jul 17, 2024: SKIN. DELAMINATED. RHW O/B MID FLAP FOUND DELAMINATION(<P>PERFORMED REPAIR AT DELAMINATION AREA PER SRM 51-70-07 PAR 5.A (1). NO FURTHER DEFECTS NOTED</P>)
- [SDR UIEA2024071000631](https://openairdocs.org/sdr/UIEA2024071000631), Jul 17, 2024: SKIN. DELAMINATED. RHW O/B MID FLAP FOUND DELAMINATION(<P>PERFORMED REPAIR AT DELAMINATION AREA PER SRM 51-70-07 PAR 5.A (1). NO FURTHER DEFECTS NOTED</P>)
- [SDR UIEA2024071000632](https://openairdocs.org/sdr/UIEA2024071000632), Jul 17, 2024: SKIN. DELAMINATED. RHW O/B MID FLAP FOUND DELAMINATION(<P>PERFORMED REPAIR AT DELAMINATION AREA PER SRM 51-70-07 PAR 5.A (1). NO FURTHER DEFECTS NOTED</P>)
- [SDR UIEA2024071000633](https://openairdocs.org/sdr/UIEA2024071000633), Jul 17, 2024: SKIN. DELAMINATED. RHW O/B MID FLAP FOUND DELAMINATION(<P>PERFORMED REPAIR AT DELAMINATION AREA PER SRM 51-70-07 PAR 5.A (1). NO FURTHER DEFECTS NOTED</P>)
- [SDR UIEA2024071000634](https://openairdocs.org/sdr/UIEA2024071000634), Jul 17, 2024: SKIN. DELAMINATED. RHW O/B MID FLAP FOUND DELAMINATION(<P>PERFORMED REPAIR AT DELAMINATION AREA PER SRM 51-70-07 PAR 5.A (1). NO FURTHER DEFECTS NOTED</P>)
- [SDR UIEA2024071000635](https://openairdocs.org/sdr/UIEA2024071000635), Jul 17, 2024: SKIN. DELAMINATED. RHW O/B MID FLAP FOUND DELAMINATION(<P>PERFORMED REPAIR AT DELAMINATION AREA PER SRM 51-70-07 PAR 5.A (1). NO FURTHER DEFECTS NOTED</P>)
- [SDR UIEA2024071000636](https://openairdocs.org/sdr/UIEA2024071000636), Jul 17, 2024: SKIN. DELAMINATED. LHW OB MID FLAP FOUND DELAMINATION(<P>PERFORMED REPAIR AT DELAMINATION AREA PER SRM 51-70-07 PAR 5.A (1). NO FURTHER DEFECTS NOTED</P>)
- [SDR UIEA2024071000637](https://openairdocs.org/sdr/UIEA2024071000637), Jul 17, 2024: SKIN. DELAMINATED. LHW OB MID FLAP FOUND DELAMINATION(<P>PERFORMED REAPAIR AT DELAMINATION AREA PER SRM 51-70-07 PAR 5.A (1). NO FURTHER DEFECTS NOTED</P>)
- [SDR UIEA2024071000638](https://openairdocs.org/sdr/UIEA2024071000638), Jul 17, 2024: SKIN. DELAMINATED. LHW OB MID FLAP FOUND DELAMINATION(<P>PERFORMED REPAIR AT DELAMINATION AREA PER SRM 51-70-07 PAR 5.A (1). NO FURTHER DEFECTS NOTED</P>)
- [SDR UIEA2024071000639](https://openairdocs.org/sdr/UIEA2024071000639), Jul 17, 2024: SKIN. DELAMINATED. LHW OB MID FLAP FOUND DELAMINATION(<P>PERFORMED REPAIR AT DELAMINATION AREA PER SRM 51-70-07 PAR 5.A (1). NO FURTHER DEFECTS NOTED</P>)
- [SDR UIEA2024071000640](https://openairdocs.org/sdr/UIEA2024071000640), Jul 17, 2024: SKIN. DELAMINATED. LHW OB MID FLAP FOUND DELAMINATION(<P>PERFORMED REPAIR AT DELAMINATION AREA PER SRM 51-70-07 PAR 5.A (1). NO FURTHER DEFECTS NOTED</P>)

All 181: https://openairdocs.org/aircraft/N487MC/reports.md

## STCs that may be installed (OpenAirDocs) (5)

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 CF6-80C2B1F)

- [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
- [STC SE01478CH](https://openairdocs.org/stc/SE01478CH): Installation of Cook Airtomic alignment joint p/n AIR 22912. Cook Airtomic
- [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
- [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. Lists CF6-80 Series

## Related

- Other Boeing 747-45EF aircraft: https://openairdocs.org/model/boeing-747-45ef/aircraft.md
- The GE CF6-80C2B1F engine: https://openairdocs.org/engine/ge-cf6-80c2b1f.md

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