# N576UP: 2008 Boeing 747-44AF

- Status: Valid registration
- Airframe: [Boeing 747-44AF](https://openairdocs.org/model/boeing-747-44af) (registry code 13848B2, 2 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: 35665
- Year built: 2008
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: September 19, 2008
- Certificate issued: September 23, 2008
- Expires: May 31, 2028
- Mode S code: A76683
- 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=576UP
- Page: https://openairdocs.org/aircraft/N576UP

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 747-44AF)

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 N576UP.

## FAA accident and incident reports

None matched to N576UP.

## Service difficulty reports (74, 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 IPXA2026092146237](https://openairdocs.org/sdr/IPXA2026092146237), Sep 21, 2026: LAMP. INOPERATIVE. MAIN CARGO COMPARTMENT ENTRY, EMERGENCY LIGHTS INOP. RELAMPED AND OPS CHKD IAW AMM 33-51-00.
- [SDR IPXA2026082710827](https://openairdocs.org/sdr/IPXA2026082710827), Jul 5, 2026: DOUBLER. GROUND DAMAGE. UPON REMOVAL, TAILSTAND CONTACTED STANCHION DOUBLER. ACCOMPLISHED ALL REQUIRED AMT STEPS AND VERIFIED ALL OTHER STEPS HAVE BEEN ACCOMPLISHED PER EO-97949-REQ1. 
- [SDR IPXA2026063024905](https://openairdocs.org/sdr/IPXA2026063024905), Jun 30, 2026: CRASH AXE. DAMAGED. MAIN DECK CRASH AXE FOUND DAMAGED/CORRODED REINSTALLED CRASH AXE INTO HOLDER ON MAIN CARGO DECK IAW AMM 25-60-00.
- [SDR IPXA2025090523303](https://openairdocs.org/sdr/IPXA2025090523303), Sep 5, 2025: FIRE DETECTOR. FAULTED. ENG 3 FIRE INDICATION FOR 20-30 SEC, WENT OUT. DIVERTED TO HKG, REPLACED NR 3 ENG LOWER AFT FIRE LOOP ASSY (TS682) IAW AMM 26-11-02/401 AND PERFORMED FIRE SYSTE
- [SDR IPXA2025082526064](https://openairdocs.org/sdr/IPXA2025082526064), Aug 18, 2025: BATTERY. INOPERATIVE. FOUND THE UPPER DECK AISLE EMERGENCY LIGHT M4915 AND L5733 INOP. I.A.W AMM 33-51-04-902-001-001 REV.114 REPLACED EMERGENCY LIGHT BATTERY (M5169) AT UPPER DECK S
- [SDR IPXA2025081826064](https://openairdocs.org/sdr/IPXA2025081826064), Aug 18, 2025: LIGHT. INOPERATIVE. FOUND THE UPPER DECK AISLE EMERGENCY LIGHT M4915 AND L5733 INOPERATIVE.
- [SDR IPXA2025081616076](https://openairdocs.org/sdr/IPXA2025081616076), Jul 31, 2025: DOUBLER. CRACKED. DURING PERFORM EO-26856-JIC001 FOUND FASTENER HOLE CRACK AT STA 740 R/H SIDE. REPAIR DAMAGE AREA IAW UPS EO-94857-REQ1 REV.1 2.
- [SDR IPXA2025081691792](https://openairdocs.org/sdr/IPXA2025081691792), Jul 30, 2025: DOUBLER. CRACKED. DURING PERFORM EO-26856-JIC001 FOUND FASTENER HOLE CRACK AT STA 720 L/H SIDE. REPAIR DAMAGE AREA I.A.W. UPS EO-94856-REQ1 REV.1 2.
- [SDR IPXA2025022185975](https://openairdocs.org/sdr/IPXA2025022185975), Feb 21, 2025: LAMP. INOPERATIVE. L1 DOOR EMERGENCY LIGHT L1854 INOP RELAMPED L1854 REFERENCE AMM 33-51-05-962-031. OPS CEHCK GOOD
- [SDR IPXA2025052636411](https://openairdocs.org/sdr/IPXA2025052636411), Sep 11, 2024: SKIN. DENTED. LH INBOARD ELEVATOR DENTED ACCOMPLISHED PERMANENT REPAIR SEE TASK NUMBER FOR DETAILS T3F18E006RAL6. MAJOR REPAIR. COMPLETED PERMANENT REPAIR AND C/W STREPS 1-11
- [SDR IPXA2024071522094](https://openairdocs.org/sdr/IPXA2024071522094), Jul 15, 2024: BATTERY PACK. INOPERATIVE. DURING PS-1 FOUND SEVERAL EMERGENCY LIGHTS WITHOUT FUNCTION. PLEASE INVESTIGATE. FOUND LIGHTS L1853, L1854 AND L5735 WITHOUT FUNCTION. REPLACED AND TESTED EMERG
- [SDR IPXA2024022999856](https://openairdocs.org/sdr/IPXA2024022999856), Feb 28, 2024: DOOR. INOPERATIVE. FOUND L1 DOOR AFT SIDE NOT FLUSH WHEN CLOSED, DOOR JAMMED, EXCESSIVE FORCE TO OPEN, SUSPECT DOOR OUT OF RIG. PICTURES ATTACHED ADJUSTED LOWER L1 DOOR HINGE FITT
- [SDR IPXA2023091754668](https://openairdocs.org/sdr/IPXA2023091754668), Sep 6, 2023: RUB STRIP. WORN. *SUPPLEMENTAL SDR* FAULT - WORN - WEAR STRIP, NO.1 MAIN ENTRY DOOR LH CUTOUT MID HANDLE LATCH MECHANISM GUIDE (REPLACE). 1. REMOVED DAMAGE PARTS I.A.W SRM 51-40
- [SDR IPXA2023092655738](https://openairdocs.org/sdr/IPXA2023092655738), Sep 6, 2023: BEARING. WORN. FAULT- BEARING , NO.1 MAIN ENTRY FREIGHTER DOOR LATCH LH LOWER TORQUE TUBE , TOTAL:1EA.(REPLACE) I.A.W AMM 52-11-01-735-080 REV 108 REPLACED L1 ENTRY DOOR LATCH
- [SDR IPXA2023092655715](https://openairdocs.org/sdr/IPXA2023092655715), Sep 6, 2023: BEARING. WORN. FAULT- WORN - BEARING , NO.1 MAIN ENTRY FREIGHTER DOOR LATCH RH UPPER TORQUE TUBE , TOTAL:1EA.(REPLACE) I.A.W AMM 52-11-01-735-080 REV 108 REPLACED L1 ENTRY DOO
- [SDR IPXA2023090755738](https://openairdocs.org/sdr/IPXA2023090755738), Sep 6, 2023: UNKNOWN. UNKNOWN. FAULT- BEARING , NO.1 MAIN ENTRY FREIGHTER DOOR LATCH LH LOWER TORQUE TUBE , TOTAL:1EA.(REPLACE) OK TO WORK
- [SDR IPXA2023090755715](https://openairdocs.org/sdr/IPXA2023090755715), Sep 6, 2023: UNKNOWN. UNKNOWN. *** SDR FILED OPEN *** FAULT- WORN - BEARING , NO.1 MAIN ENTRY FREIGHTER DOOR LATCH RH UPPER TORQUE TUBE , TOTAL:1EA.(REPLACE) OK TO WORK
- [SDR IPXA2023090754668](https://openairdocs.org/sdr/IPXA2023090754668), Sep 6, 2023: UNKNOWN. UNKNOWN. *** SDR FILED OPEN *** FAULT - WORN - WEAR STRIP, NO.1 MAIN ENTRY DOOR LH CUTOUT MID HANDLE LATCH MECHANISM GUIDE (REPLACE) OK TO WORK
- [SDR IPXA2023022313190](https://openairdocs.org/sdr/IPXA2023022313190), Feb 22, 2023: LIGHT. FAILED. EMERGENCY LIGHTS WILL NOT TURN OFF WHEN SWITCH IN OFF POSITION, ARM AND ON NORMAL. REPLACED S7 SWITCH ON ASSY 285U0230-13 X1081 FLIGHT ATTENDANT PANEL IAW CMM 3
- [SDR IPXA2021102775381](https://openairdocs.org/sdr/IPXA2021102775381), Oct 26, 2021: NONE. NONE. INSPECTION TYPE:NADOOR F\D OVHDFOUND LOCK HANDLE SLIGHTLY OUT OF POSITION, CYCLED HATCH OPEN / CLOSED SEVERAL TIMES, MSG SE;F ERASED. OK PER AMM 52-21-00
- [SDR IPXA2021020165122](https://openairdocs.org/sdr/IPXA2021020165122), Feb 1, 2021: BATTERY PACK. INOPERATIVE. INSPECTION TYPE: 18FO FOUND U/D AISLE EMERGENCY LIGHT INOP. REPLACED THE U/D AISLE EMERGENCY LIGHT BATTERY ASSEMBLY M5168, AND PERFORMED EMERGENCY LIGHT OPERATI
- [SDR IPXA2020102761735](https://openairdocs.org/sdr/IPXA2020102761735), Oct 26, 2020: AOA. INOPERATIVE. INSPECTION TYPE: N/A ATB NO EMERGENCY DECLARED. LANDED WITHOUT INCIDENT. IAS DISAGREE ALT DISAGREE AND STELL WARNING PLI SHOWED IN CAPTAINS FD STICK SHAKER WAS 
- [SDR IPXA2020031653177](https://openairdocs.org/sdr/IPXA2020031653177), Feb 15, 2020: FLOOR PANEL. PUNCTURED. INSPECTION TYPE:N/AFLOOR PANEL PUNCTURED AT STA 1950LEFTREPAIRED DAMAGED PANEL PER SRM 53-00-50-2R-1
- [SDR IPXA2019102328158](https://openairdocs.org/sdr/IPXA2019102328158), Oct 20, 2019: SKIN. CRACKED. INSPECTION TYPE:C1CRACK WAS FOUND ON INNER SKIN OF FLAP PANEL(P/N:65B39205-72)OF #16 KRUGER FLAP T/E AREA,ILES 625.REPAIR I.A.W. 747-400F SRM 57-43-02 REPAIR 1 
- [SDR IPXA2019052142340](https://openairdocs.org/sdr/IPXA2019052142340), May 21, 2019: STICK SHAKER. INOPERATIVE. INSPECTION TYPE:NA**EMERGENCY DECLARED** ENCOUNTERED MODERATE INTERMITTENT SEVERE TURBULANCE FOR APPROX 60 SEC. FL 400 M. 83S A/C WT APPROX 497.0 LNAV DISENGAGE
- [SDR IPXA2019051342026](https://openairdocs.org/sdr/IPXA2019051342026), May 12, 2019: FLOORBOARD. DAMAGED. INSPECTION TYPE:N/A FACE SHEET MISSING 1"X.5" FROM FLOORBOARD STAT 1300 RBL 90. REPAIRED IAW SRM 53-00-50 2R-1. ALL WORK RECORDED ON NRC#167347. 5-11-19-1195530
- [SDR IPXA201805189494](https://openairdocs.org/sdr/IPXA201805189494), May 9, 2018: UPLOCK SENSOR. BROKEN. DURING REPLACEMENT OF THE RT BODY GEAR ALT UPLOCK SENSOR. FOUND PRI SENSOR HEAD BROKEN. TROUBLESHOT IAW FIM 32-61 TASK 898 & 878. RIGHT BODY GEAR PRI SENSOR FAU
- [SDR IPXA2018041428547](https://openairdocs.org/sdr/IPXA2018041428547), Apr 14, 2018: CRASH AXE. DAMAGED. CRASH AXE DAMAGED. REMOVED AND REPLACED THE CRASH AXE AND SHEATH IAW AMM 25-60-00.
- [SDR IPXA2018021326503](https://openairdocs.org/sdr/IPXA2018021326503), Feb 12, 2018: SMOKE BARRIER. TORN. CARGO SMOKE CURTAIN TORN. REPAIRED THE SMOKE CURTAIN IAW AMM 25-59-00-308-036.
- [SDR IPXA2018021326502](https://openairdocs.org/sdr/IPXA2018021326502), Feb 12, 2018: SMOKE BARRIER. TORN. SMOKE CURTAIN AT BS 700 TORN AND MISSING FASTENERS. REPAIRED SMOKE CURTAIN IAW AMM 25-59-00-308-036.
- [SDR IPXA2018012125720](https://openairdocs.org/sdr/IPXA2018012125720), Jan 21, 2018: ACTUATOR. RUPTURED. AIR TURNBACK, LOSS OF HYDRAULIC SYSTEM NR 4. CHECKED THE NR 4 ENG CASE DRAIN DPI NOT POPPED, AND REPLACED EDP AND ADP CASE DRAIN FILTER, NO METAL CHIP IAW AMM 2
- [SDR IPXA2017080620174](https://openairdocs.org/sdr/IPXA2017080620174), Aug 6, 2017: HOOK AND LOOP. WORN. SUPERNUMERARY AREA EMERGENCY DECENT CONTAINER WILL NOT STAY CLOSED. REPLACED WORN HOOK AND LOOP IAW AMM 25-61-00.
- [SDR IPXA2017080120019](https://openairdocs.org/sdr/IPXA2017080120019), Jul 31, 2017: WARNING MESSAGE. FALSE ACTIVATION. NR 2 ENGINE FAN VIBRATION, AUTO DISPLAYED. OCCURRED AFTER TAKE OFF, STABLE CRUISE THRUST SETTING. TROUBLESHOT IAW FIM 71-00-00-101, FIG 118, NOTE 1, WITHIN LIMI
- [SDR IPXA2017060117759](https://openairdocs.org/sdr/IPXA2017060117759), Jun 1, 2017: BATTERY. INOPERATIVE. INSPECTION TYPE: 18FO, UPPER DECK EMERGENCY LIGHTS L1533, L5733 , L5767 AND M4915 INOPERATIVE. REPLACED EMERGENCY LIGHT BATTERY (M5169) IAW AMM 33-51-04-902-001
- [SDR IPXA2017042816600](https://openairdocs.org/sdr/IPXA2017042816600), Apr 28, 2017: BULB. INOPERATIVE. EMERGENCY LIGHTS AT THE L1 DOOR ARE INOPERATIVE. REPLACED THE BULBS. OPS CHECKED GOOD IAW AMM 31-51-05-962-031.
- [SDR IPXA2017040415792](https://openairdocs.org/sdr/IPXA2017040415792), Apr 3, 2017: MODULE. DAMAGED. PERFORMED THE FIRE, OVERHEAT TEST. THE TEST FAILED. ALL MN DECK DETECTORS FAILED. TROUBLESHOT AND FOUND ON FIRE TEST SWITCH ON THE OVERHEAD PANEL M7317 HAD ONE 
- [SDR IPXA2016112110894](https://openairdocs.org/sdr/IPXA2016112110894), Nov 21, 2016: FLOOR PANEL. CRACKED. MCD NR 11 FWD THIRD ROW FROM THE LEFT FLOOR PANEL CRACKED AND DELAMINATED. FABRICATED NEW PANEL IAW EO B747-5320-42648-A.
- [SDR IPXA2016050803045](https://openairdocs.org/sdr/IPXA2016050803045), May 8, 2016: LANYARD. LOOSE. LIFE RAFT UNPACKED. R & R LIFE RAFT IAW AMM 25-62-01.
- [SDR IPXA2016012898565](https://openairdocs.org/sdr/IPXA2016012898565), Jan 15, 2016: INTERCOSTAL. DENTED. DENT WAS FOUND ON THE INTERCOSTAL, AT BS 2108, LBL 7.625. REPAIR IAW SRID 4-3124562467, AND EO B747-5310-59635-A.
- [SDR IPXA2016012998610](https://openairdocs.org/sdr/IPXA2016012998610), Jan 15, 2016: SKIN. DAMAGED. INSPECTION TYPE:D1, DURING D1, PLUS C1 CHECK OF DATUM ACFT, BROKEN AND DENT WERE FOUND ON THE SKIN BS 2595, BETWEEN STRINGERS 38 - 42R. REPAIRED IAW SRID 4-3117
- [SDR IPXA2015080892158](https://openairdocs.org/sdr/IPXA2015080892158), Aug 8, 2015: SMOKE GOGGLES. DAMAGED. FOUR SUPERNUMERARY GOGGLES ELASTIC BANDS STRETCHED, UNUSEABLE. REPLACED THE SMOKE GOGGLES IAW MM 25-00-00 .
- [SDR IPXA2015080892157](https://openairdocs.org/sdr/IPXA2015080892157), Aug 8, 2015: CONTAINER. TORN. NR 1 EA, RT SUPERNUMERARY LIFE VEST STORAGE BAG TORN. REPLACED RT SUPERNUMERARY LIFE VEST AS NEEDED, REF MM 25-60-00, EFF SOURCE REF IPC 25-62-51-010.
- [SDR IPXA2014111284829](https://openairdocs.org/sdr/IPXA2014111284829), Nov 11, 2014: TRANSMITTER. INOPERATIVE. HYD INDICATION .69 ON HYD SYS NR 4 AT THE DIRECTION OF THE COMPANY. R & R QTY TRANSMITTER IAW AMM 29-33-01-401. OPS TEST PASSED.
- [SDR IPXA2014071683625](https://openairdocs.org/sdr/IPXA2014071683625), Jul 14, 2014: BULB. INOPERATIVE. FWD BULB IN EMERGENCY EXIT LIGHT ON MAIN CARGO DECK CEILING INOPERATIVE, JUST INSIDE MAIN ENTRY DOOR, FWD OF CREW STAIRS. REPLACED THE BULB IAW AMM 33-51-02.
- [SDR IPXA2014051482955](https://openairdocs.org/sdr/IPXA2014051482955), May 11, 2014: FASTENER. MISSING. IN FLIGHT DECK, EMERGENCY DESCENT DEVICE COMPARTMENT IS MISSING SCREWS TO SECURE IT. INSTALLED REQUIRED FASTENERS. OK FOR SERVICE.
- [SDR IPXA2014030382118](https://openairdocs.org/sdr/IPXA2014030382118), Mar 1, 2014: SKIN. PUNCTURED. RT INBD AFT FLAP T/E WEDGE HAS A PUNCTURE IN INNER SKIN APPROX 10 FT FROM INBD EDGE. REPAIRED IAW EO B747-5750-53442-A.
- [SDR IPXA2014030382113](https://openairdocs.org/sdr/IPXA2014030382113), Mar 1, 2014: SKIN. DENTED. LEFT INBD AFT FLAP HAS 2.5 INCH DENT IN LOWER SKIN 11 INCHES FROM OTBD EDGE. REPAIRED IAW EO B747-5750-53443-A.
- [SDR IPXA201307229430](https://openairdocs.org/sdr/IPXA201307229430), Jul 21, 2013: FLOOR PANEL. DAMAGED. MAIN DECK CTR FLOOR PANEL AT BS 1440, DAMAGED. REPAIRED IAW SRM 51-00-50-2R1.
- [SDR IPXA3B79303](https://openairdocs.org/sdr/IPXA3B79303), Jul 14, 2013: FLOOR PANEL. PUNCTURED. FLOOR PANEL, BS 2200, POS 18R PUNCTURED. FABRICATED NEW FLOOR PANEL IAW EO B747-5320-51432-A.
- [SDR IPXA3B79302](https://openairdocs.org/sdr/IPXA3B79302), Jul 14, 2013: FLOOR PANEL. DAMAGED. FLOOR PANEL, BS 1740-1840, LBL12-33 HAS TWO AREAS OF DAMAGE, FABRICATED NEW FLOOR PANEL IAW EO B747-5320-51434-A.

All 74: https://openairdocs.org/aircraft/N576UP/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 747-44AF aircraft: https://openairdocs.org/model/boeing-747-44af/aircraft.md
- The GE CF6-80C2B1F engine: https://openairdocs.org/engine/ge-cf6-80c2b1f.md

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