# N579UP: 1994 Boeing 747-45E

- Status: Valid registration
- Airframe: [Boeing 747-45E](https://openairdocs.org/model/boeing-747-45e) (registry code 1384947, 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: 26062
- Year built: 1994
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: October 31, 2008
- Certificate issued: May 6, 2008
- Expires: May 31, 2027
- Mode S code: A771A8
- Registered owner: [United Parcel Service Co](https://openairdocs.org/faa-owner/UNITED%20PARCEL%20SERVICE%20CO)
- Location: [Louisville, KY](https://openairdocs.org/faa-place/KY/Louisville)
- Owner type: Corporation
- Owner's area on the map: 38.2585° N, 85.5398° W: Placed by OpenAirDocs at the center of ZIP code 40223, within about 2 miles (OpenAirDocs). The owner's mailing address, not where the aircraft is based
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=579UP
- Page: https://openairdocs.org/aircraft/N579UP

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 747-45E)

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 N579UP.

## FAA accident and incident reports

None matched to N579UP.

## Service difficulty reports (248, 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 IPXA2026083188098](https://openairdocs.org/sdr/IPXA2026083188098), Aug 29, 2026: TIRE TREAD. SEPARATED. NUMBER 6 TIRE LOST TREAD FROM ENTIRE CIRCUMFERENCE. CASING PLIES SHOWING. EMERGENCY DECLARED. REPLACED NR 6 MAIN WHEEL ASSY IAW MM 32-45-01-4.
- [SDR IPXA2026090287354](https://openairdocs.org/sdr/IPXA2026090287354), Aug 23, 2026: ACTUATOR. FAULTED. EICAS DOOR U/D FLT LK ON CLIMB OUT, NO PRESSURIZATION ISSUES. INSTALLED R/H UPPER DECK DOOR FLIGHT LOCK ACTUATOR REF MM 52-23-08. PLACED AIRCRAFT IN AIR MODE RE
- [SDR IPXA2026062322884](https://openairdocs.org/sdr/IPXA2026062322884), Jun 11, 2026: COVER. DAMAGED. NR 4 ENGINE INBOARD THRUST REVERSER HINGE COVER DAMAGED. INSTALLED THE NR 4 INBD T/R HINGE COVER PANEL IAW AMM 78-31-01-401.
- [SDR IPXA2026061222884](https://openairdocs.org/sdr/IPXA2026061222884), Jun 11, 2026: COVER. DAMAGED. NR 4 ENGINE INBOARD THRUST REVERSER HINGE COVER DAMAGED ENGINE #4 INBOARD T/R HINGE COVER DEFERRED PER EO-97744.
- [SDR IPXA2026040172052](https://openairdocs.org/sdr/IPXA2026040172052), Apr 1, 2026: NONE. NONE. ALL FOUR OVERWING EMERGENCY SLIDE LIGHTS ARE INOPERATIVE. LEFT AND RIGHT WINGS IAW ENGINEERING, LIGHTS WERE DEACTIVATED DURING P TO F CONVERSION IAW SB 747-00-2
- [SDR IPXA2026022742660](https://openairdocs.org/sdr/IPXA2026022742660), Feb 27, 2026: BRACKET. UNSECURE. AFTER CORNER OF RIGHT UPPER MAIN DECK DOOR EXIT LIGHT PANEL NOT SECURED. INSTALLED BRACKET AND SECURED PANEL USING STANDARD TORQUES REF AMM 20-51-01
- [SDR IPXA2026030242660](https://openairdocs.org/sdr/IPXA2026030242660), Feb 27, 2026: PANEL. UNSECURE. AFTER CORNER OF RIGHT UPPER MAIN DECK DOOR EXIT LIGHT PANEL NOT SECURED. ITEM DEFERRED WITH REFERENCE TO EO-96656-REQ 1. OPEN
- [SDR IPXA2025100973364](https://openairdocs.org/sdr/IPXA2025100973364), Oct 9, 2025: ANTI-ICE SYSTEM. WARNING MESSAGE. **ATB**ANTI-ICE NAC 1, ANTI-ICE NAC 2, ANTI-ICE NAC 3, ANTI-ICE NAC 4 STATUS MESSAGE PERFORMED OPS TEST IAW AMM:31-21-00/501 REV.114<BR>FOUND SATIS.<BR>ALL TOOL
- [SDR IPXA2025032415971](https://openairdocs.org/sdr/IPXA2025032415971), Mar 7, 2025: BEAM. CRACKED. LOWER CHORD CRACK OF R/H WING T/E BEAM ASSY AT NO. 7 SPOILER. AREA , WBL 296 AND WBL 303. (REPAIR). REPAIR DAMAGE AREA I.A.W. UPS EO-93195-REQ1 REV.1 JOB COMPLE
- [SDR IPXA2025032415924](https://openairdocs.org/sdr/IPXA2025032415924), Mar 7, 2025: BEAM. CRACKED. LOWER CHORD CRACK OF R/H WING T/E BEAM ASSY AT NO. 8 SPOILER. AREA , WBL 382 AND WBL 389. (REPAIR). REPAIR DAMAGE AREA I.A.W. UPS EO-93212-REQ1 REV.1
- [SDR IPXA2025032989763](https://openairdocs.org/sdr/IPXA2025032989763), Mar 6, 2025: SEAT TRACK. CORRODED. CORROSION - MAIN DECK SEAT TRACK CORROSION BETWEEN 480 AND STA 500 , LBL 33.99. (REPLACE). .FABRICATE P/N:65B11244-7 PER BOEING DWG NO.65B11244 SH3 REV."-"; PL 
- [SDR IPXA2025032569716](https://openairdocs.org/sdr/IPXA2025032569716), Mar 5, 2025: CHANNEL. CORRODED. RIGHT WING OUTBOARD LEADING EDGE CAVITY INSIDE, LOWER CHANNEL CORROSION, OLES 1350-1400.REPAIRED DAMAGE AREA I.A.W. UPS EO-93164-REQ1 REV.1
- [SDR IPXA2025032645221](https://openairdocs.org/sdr/IPXA2025032645221), Mar 4, 2025: SKIN. DAMAGED. FAULT - SINK - SCREWS, L/H WING OUTBOARD AFT FLAP INBOARD SIDE EDGE (AGING A/C INSPECTION) (REPLACE). REPAIR GOUGE DAMAGE ON INBD EDGE OF L/H OUTBD AFT FLAP UPP
- [SDR IPXA2025032748217](https://openairdocs.org/sdr/IPXA2025032748217), Mar 4, 2025: HINGE. CORRODED. CORROSION - HINGE, L/H AIR CONDITION ACCESS DOOR PNL NO.191ML MID SIDE. (REPLACE). I.A.W AMM 20-51-01-912-008 REV.113 INSTALL THE HINGE MIDDLE SIDE AT PNL NO.19
- [SDR IPXA2025032548217](https://openairdocs.org/sdr/IPXA2025032548217), Mar 4, 2025: HINGE. CORRODED. CORROSION - HINGE, L/H AIR CONDITION ACCESS DOOR PNL NO.191ML MID SIDE. (REPLACE) PAPER REVIEWED OK.
- [SDR IPXA2025032350590](https://openairdocs.org/sdr/IPXA2025032350590), Mar 4, 2025: STRUCTURE. CRACKED. CRACK - CHORD, L/H WING T/E CAVITY INBD AILERON OUTBD WEB UPPER CHORD, WBL 515. (REPLACE). COMPELTED EI NO.F2025A57M-475 SEQUENCE A STEP 9.
- [SDR IPXA2025032733616](https://openairdocs.org/sdr/IPXA2025032733616), Mar 3, 2025: SUPPORT FITTING. CRACKED. NO.8 SPOILER ACTUATOR FITTING, OUTBOARD LOWER CRACK (REPAIR). .I.A.W AMM 27-61-06-402-011 REV.113 CONNECT INPUT ROD AND AMM 27-61-13-404-014 REV.113 CONNECT HYD
- [SDR IPXA2025032329386](https://openairdocs.org/sdr/IPXA2025032329386), Mar 3, 2025: SKIN. DENTED. DENT - SKIN, R/H WING INBOARD AFT FLAP LOWER SKIN, 2 PLACE, (AGING A/C INSPECTION) (REPAIR). REPAIR DENTS WITH AN ESISTING REPAIR ON THE LOWER SURFACE OF THE RH
- [SDR IPXA2025032433593](https://openairdocs.org/sdr/IPXA2025032433593), Mar 3, 2025: FITTING. CRACKED. NO.8 SPOILER ACTUATOR FITTING, INBOARD LOWER CRACK (REPAIR). REPAIR DAMAGE AREA I.A.W. SRM 57-51-13-2R-1 REV.62 AND EGAT WORK SHEET NO.50147. ACCOMPLISH THE REP
- [SDR IPXA2025032433614](https://openairdocs.org/sdr/IPXA2025032433614), Mar 3, 2025: FITTING. CRACKED. NO.7 SPOILER ACTUATOR FITTING, OUTBOARD LOWER CRACK (REPAIR). .REPAIR DAMAGE AREA I.A.W. SRM 57-51-13-2R-1 REV.62 AND EGAT WORK SHEET NO.50146. .JOB COMPLETED. 
- [SDR IPXA2025031130046](https://openairdocs.org/sdr/IPXA2025031130046), Mar 3, 2025: SKIN. DENTED. DENT - SKIN, L/H WING OUTBOARD MID FLAP, PANEL #587MT (AGING A/C INSPECTION) (REPAIR). CLEAN, SEAL AND FINFISH AT REPAIR AREA I.A.W. 747-400SF SRM 51-70-10-2R-0
- [SDR IPXA2025031129315](https://openairdocs.org/sdr/IPXA2025031129315), Mar 3, 2025: SKIN. DENTED. DENT - SKIN, R/H WING INBOARD MID FLAP UPPER PANEL EXTERNAL SURFACE, PANEL NO.677JT (AGING A/C INSPECTION) (REPAIR). CLEAN, SEAL AND FINFISH REPAIR AREA I.A.W. 
- [SDR IPXA2025032821491](https://openairdocs.org/sdr/IPXA2025032821491), Mar 2, 2025: FITTING. CORRODED. CORROSION - FITTING, L/H WING L/E CAVITY FRONT SPAR FITTING OLES 1493.45 (REPAIR). EMOVE DAMAGE FITTING I.A.W. SRM 51-40-02-0G REV.62. PERFORM UPS EO-93174-REQ1
- [SDR IPXA2025032821541](https://openairdocs.org/sdr/IPXA2025032821541), Mar 2, 2025: WEB. CRACKED. CRACK - WEB, L/H WING INBD AILERON OUTBD WEB, WBL 515, TOTAL: 2 AREA (REPLACE). ACCOMPLISH THE REPAIR PER EO-93194-REQ1 (N579UP: LEFT WING FIXED TRAILING EDGE R
- [SDR IPXA2025032621567](https://openairdocs.org/sdr/IPXA2025032621567), Mar 2, 2025: ACCESS PANEL. CORRODED. CORROSION - BRACE, R/H AIR CONDITION ACCESS PNL NO.192ER STA 1059.9 RBL 57.7.FOUND CHAFE DAMAGE THRU CHAFE PLATE 100% MATERIAL LOSS, REMOVED CHAFE PLATE AS REQU
- [SDR IPXA2025032321569](https://openairdocs.org/sdr/IPXA2025032321569), Mar 2, 2025: SUPPORT FITTING. CRACKED. CRACK - FITTING, INBD LOWER SIDE OF L/H WING NO.6 SPOILER MID SUPPORT FITTING (REPAIR). .REPAIR DAMAGE AREA I.A.W. SRM 57-51-13-2R-1 REV.62 AND EGAT WORK SHEET 
- [SDR IPXA2025031321601](https://openairdocs.org/sdr/IPXA2025031321601), Mar 2, 2025: FITTING. CRACKED. CRACK - FITTING, INBD LOWER SIDE OF L/H WING NO.5 SPOILER MID SUPPORT FITTING (REPAIR). I.A.W AMM 27-61-06-402-011 REV.113 CONNECT THE INPUT ROD AND AMM 27-61-1
- [SDR IPXA2025031321427](https://openairdocs.org/sdr/IPXA2025031321427), Mar 2, 2025: STIFFENER. CORRODED. FAULT - CORROSION - STIFFENER, L/H AIR CONDITION ACCESS PNL NO.191LL FWD INBD SIDE (REPLACE). REMOVE DAMAGE PARTS I.A.W. SRM 51-40-02-0G REV.62. FABRICATE P/N:6
- [SDR IPXA2025032593531](https://openairdocs.org/sdr/IPXA2025032593531), Feb 28, 2025: SUPPORT BEAM. CORRODED. CORROSION - BEAM, L/H WING L/E LOWER PNL FWD SUPPORT BEAM INNER FACE, OLES 1530 ~ OLES 1535 (REPAIR). REPAIR DAMAGE AREA I.A.W. UPS EO-93163-REQ1 REV.1.
- [SDR IPXA2025032593591](https://openairdocs.org/sdr/IPXA2025032593591), Feb 28, 2025: SUPPORT BEAM. CORRODED. CORROSION - BEAM, L/H WING L/E LOWER PNL FWD SUPPORT BEAM INNER FACE, OLES 1535 ~ OLES 1540 (REPAIR). REPAIR DAMAGE AREA I.A.W. UPS EO-93161-REQ1 REV.1. ALL PAP
- [SDR IPXA2025032593475](https://openairdocs.org/sdr/IPXA2025032593475), Feb 28, 2025: SUPPORT BEAM. CORRODED. CORROSION - BEAM, L/H WING L/E LOWER PNL FWD SUPPORT BEAM INNER FACE, OLES 1425 (REPAIR). .REPAIR DAMAGE AREA I.A.W. UPS EO-93160-REQ1 REV.1. ALL PAPERWORK REVI
- [SDR IPXA2025031093354](https://openairdocs.org/sdr/IPXA2025031093354), Feb 28, 2025: SPLICE PLATE. CORRODED. CORROSION - PLATE, UPPER FACE OF L/H WING L/E LOWER PNL, OLES 1545 (REPLACE). FABRICATE P/N:65B11862-36 PER BOEING DWG NO:65B11862 SH 2 REV. "F";PL REV."N";PSDL
- [SDR IPXA2025031252166](https://openairdocs.org/sdr/IPXA2025031252166), Feb 26, 2025: PANEL. DEBONDED. DISBOND, FOUND L/H VERTICAL STABILIZER LOWER FORWARD TORQUE BOX PANEL, P/N: 186U1006-3 (EXCEED SRM LIMITATION 200 SQUARE INCHES) (REPAIR). INSTALL L/H VERTICAL 
- [SDR IPXA2025031252215](https://openairdocs.org/sdr/IPXA2025031252215), Feb 26, 2025: PANEL. DEBONDED. DISBOND, FOUND L/H VERTICAL STABILIZER LOWER FORWARD TORQUE BOX PANEL, P/N:186U1002-2 (EXCEED SRM LIMITATION 200 SQUARE INCHES) (REPAIR). REPAIR DISBOND ON LH F
- [SDR IPXA2025031252237](https://openairdocs.org/sdr/IPXA2025031252237), Feb 26, 2025: PANEL. DEBONDED. DISBOND, FOUND L/H VERTICAL STABILIZER LOWER FORWARD TORQUE BOX PANEL, P/N: 186U1001-2 (EXCEED SRM LIMITATION 200 SQUARE INCHES) (REPAIR). REPAIR DISBOND DAMAGE
- [SDR IPXA2025011255732](https://openairdocs.org/sdr/IPXA2025011255732), Jan 12, 2025: RELAY. FAULTED. STATUS MESSAGE MD CGO MID LP B REPLACED SMOKE DETECTOR 6B1 AND 6B2 SEPERATLY AFTER EACH OTHER IAW AMM 26-14-01/401 REV. 112; NO HELP. TEST ALWAYS PASS, BUT STS 
- [SDR IPXA2025011347308](https://openairdocs.org/sdr/IPXA2025011347308), Jan 12, 2025: WARNING MESSAGE. ILLUMINATED. MD CGO MID LP B NO STS MSG PRESENT. FIRE/OVHT DETECTION SYSTEM OPS TEST ACC AMM 26-10-00-715-001 R112 PASS.
- [SDR IPXA2025010567156](https://openairdocs.org/sdr/IPXA2025010567156), Dec 31, 2024: SKIN. CONTAMINATED. CORROSION ON R/H WING LOWER SKIN UPPER SURFACE NEAR OLES 1455 AND 1462.(REPAIR). ACCOMPLISHED REPAIR I.A.W UPS EO-92447-REQ1 REV.1.
- [SDR IPXA2025010967139](https://openairdocs.org/sdr/IPXA2025010967139), Dec 31, 2024: SKIN. CORRODED. CORROSION ON R/H WING LOWER SKIN LOWER SURFACE NEAR OLES 1423.5. (REPAIR). ACCOMPLISHED REPAIR I.A.W UPS EO-92449-REQ1 REV.1.
- [SDR IPXA2025010967137](https://openairdocs.org/sdr/IPXA2025010967137), Dec 31, 2024: SKIN. CORRODED. CORROSION ON R/H WING LOWER SKIN UPPER SURFACE NEAR OLES 1390.75. (REPAIR). ACCOMPLISHED REAPIE I.A.W UPS EO-92448-REQ1 REV.1. JOB COMPLETED AND ATTACHMENT ARE 
- [SDR IPXA2025010649808](https://openairdocs.org/sdr/IPXA2025010649808), Dec 22, 2024: PLATE. CORRODED. CORROSION FOUND UNDER NUTPLATES FOR LAV SERVICE AREA. 1.REMOVED DAMAGE PARTS I.A.W SRM 51-40-02-0G REV.61 2.FABRICATE P/N(146U8023-2) PER BOEING DWG NO.146U8023
- [SDR IPXA2024120643306](https://openairdocs.org/sdr/IPXA2024120643306), Dec 5, 2024: SWITCH. DIRTY. DOOR U/D FLT LK ADVISORY AND SUBSEQUENT STATES MESSAGE ON CLB OUT. RAN QRH PROCESSED NORMALLY. OPENED LEFT UPPER DECK DOOR. CLEANED SWITCHES AND CYCLED SEVERAL 
- [SDR IPXA2024121096511](https://openairdocs.org/sdr/IPXA2024121096511), Dec 3, 2024: FIRE LOOP. WARNING MESSAGE. *** SUPPLEMENTAL SDR *** MD CGO AFT LP A STATUS MESSAGE IN CRUISE. REFERENCE BARCODE T3F18E005PVTB FOR CORRECTIVE ACTION FOR R&R OF MD CARGO DETECTORS A111 AND 
- [SDR IPXA2024120396511](https://openairdocs.org/sdr/IPXA2024120396511), Dec 3, 2024: WARNING MESSAGE. ILLUMINATED. MD CGO AFT LP A STATUS MESSAGE IN CRUISE. ACCOMPLISHED DMP WITH REFERENCE TO MEL/DMP 26-14-1-2-3-1. PLACARD INSTALLED. OPEN
- [SDR IPXA2024120493434](https://openairdocs.org/sdr/IPXA2024120493434), Dec 3, 2024: FIRE DETECTOR. FALSE ACTIVATION. MD CARGO AFT LP A STATUS MSG PERFORMED FIRE TEST IAW AMM 26-14-00-710-801. OPS CHECK NORMAL. MESSAGE CLEARED.
- [SDR IPXA2025011324042](https://openairdocs.org/sdr/IPXA2025011324042), Oct 24, 2024: HINGE. CRACKED. LAVATORY SERVICE DOOR LATCH BROKEN AND PIANO HINGE CRACKED. PLEASE DEFER PER CDL 52-49-3 REMOVED DAMAGE PARTS I.A.W SRM 51-40-02-0G REV.61. FABRICATE P/N(146U80
- [SDR IPXA2024102523568](https://openairdocs.org/sdr/IPXA2024102523568), Oct 24, 2024: HANDLE. LOOSE. MAIN ENTRY DOOR HANDLE LOOSE RETIGHTENED MAIN ENTRY DOOR EXTERNAL HANDLE IAW AMM 52-11-13. OPS OK
- [SDR IPXA2025022609589](https://openairdocs.org/sdr/IPXA2025022609589), Nov 29, 2023: SKIN. DENTED. LT WING OUTBOARD LEADING EDGE HAS DENT. INSTALLED NEW SECTION LEFT WING LEADING EDGE IAW SRM 57-41-01-2R-6. THIS CLEARS DEF.
- [SDR IPXA2023112909589](https://openairdocs.org/sdr/IPXA2023112909589), Nov 29, 2023: UNKNOWN. UNKNOWN. *SDR FILED OPEN* LT WING OUTBOARD LEADING EDGE HAS DENT.***SM EVAL REQ*** DEFERRING DENT MEASURING 2.30 X4.00 AND .150 DEEP. IAW EO-88836-REQ1.
- [SDR IPXA2023112388846](https://openairdocs.org/sdr/IPXA2023112388846), Nov 21, 2023: SKIN. PUNCTURED. *SUPPLEMENTAL SDR* *MAJOR REPAIR* LOAD REPORTS DAMAGE TO AIRCRAFT STRUCTURE FWD OF LOWER FWD CARGO PIT. C/W EO-88772-REQ1

All 248: https://openairdocs.org/aircraft/N579UP/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 747-45E aircraft: https://openairdocs.org/model/boeing-747-45e/aircraft.md
- The GE CF6-80C2B1F engine: https://openairdocs.org/engine/ge-cf6-80c2b1f.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.