# N572UP: 2007 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: 35669
- Year built: 2007
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: November 28, 2007
- Certificate issued: December 4, 2025
- Expires: December 31, 2032
- Mode S code: A757A7
- 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=572UP
- Page: https://openairdocs.org/aircraft/N572UP

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 N572UP.

## FAA accident and incident reports

None matched to N572UP.

## 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 IPXA2026080575871](https://openairdocs.org/sdr/IPXA2026080575871), Aug 2, 2026: BATTERY. INOPERATIVE. FOUND THE UPPER DECK AISLE EMERGENCY LIGHT INOP. IAW SSM 33-51-01 REV.47 PERFORMED THE UPPER DECK AISLE EMERGENCY LIGHT SYSTEM CHECK , FOUND THE EMERGENCY LIGHT
- [SDR IPXA2026080575748](https://openairdocs.org/sdr/IPXA2026080575748), Aug 2, 2026: BATTERY. INOPERATIVE. FOUND THE UPPER DECK EMERGENCY EXIT SIGN LIGHT INOP. I.A.W SSM 33-51-01 REV.47 PERFORMED THE UPPER DECK EMERGENCY EXIT SIGN LIGHT SYSTEM CHECK , FOUND THE EMERG
- [SDR IPXA2026080375748](https://openairdocs.org/sdr/IPXA2026080375748), Aug 2, 2026: LIGHT. INOPERATIVE. FOUND THE UPPER DECK EMERGENCY EXIT SIGN LIGHT INOP. (REPLACE)
- [SDR IPXA2026080375871](https://openairdocs.org/sdr/IPXA2026080375871), Aug 2, 2026: LIGHT. INOPERATIVE. FOUND THE UPPER DECK AISLE EMERGENCY LIGHT INOPERATIVE. (REPLACE)
- [SDR IPXA2026070878270](https://openairdocs.org/sdr/IPXA2026070878270), Jul 3, 2026: FLAP. CRACKED. FOUND RT WING OUTBD AFT FLAP INBD SIDE BOTTOM SURFACE CRACK. PERFORMED NDT/UT FOR THE REWORKED AREA & PLUS 2 INCHES AROUND HEATED AREA ,PER 747 NDT MANUAL PART 
- [SDR IPXA2026071560216](https://openairdocs.org/sdr/IPXA2026071560216), Jul 2, 2026: SKIN. CRACKED. CRACKED SKIN, NR 4 PYLON R/H FAIRING DOOR L/E AREA. I.A.W.AMM 54-62-03-404-005 REV117 INSTALLED NO.4 PYLON R/H FAIRING DOOR.
- [SDR IPXA2026070759188](https://openairdocs.org/sdr/IPXA2026070759188), Jul 2, 2026: COWLING. DENTED. DENTED SKIN, NR 2 ENG NOSE COWL INLET AT 10 O'CLOCK POSITION. CUT OUT THE DAMAGE AND CLEAN, MEASURE THE CUT OUT ( DIA : 0.5", 12.8" FROM AFT EDGE, 51.7" FROM LW
- [SDR IPXA2026070724623](https://openairdocs.org/sdr/IPXA2026070724623), Jun 30, 2026: SEAL. BROKEN. BROKEN MOLDING SEAL, LT WING NR 11 KRUEGER FLAP INBD SIDE MOLDING. CHECKED OK.
- [SDR IPXA2026070921962](https://openairdocs.org/sdr/IPXA2026070921962), Jun 30, 2026: WEB. CORRODED. CORRODED UPPER DECK FLOOR PNL WEB AT BS 480 - 520, LBL 10 - RBL 40 CORRODED. INSTALLED A NEW WEB IAW SRM 51-40-02-0G, REV 107.
- [SDR IPXA2026070724617](https://openairdocs.org/sdr/IPXA2026070724617), Jun 30, 2026: SEAL. BROKEN. BROKEN MOLDING SEAL, LT WING NR 6 VC FLAP INBD SIDE MOLDING. IAW SRM 57-43-02-2R-5 REV. 107 REFER TO SOPM 20-50-12 REV. 160 PERFORM REPAIR
- [SDR IPXA2026070624604](https://openairdocs.org/sdr/IPXA2026070624604), Jun 30, 2026: SEAL. BROKEN. BROKEN MOLDING SEAL, LT WING NR 3 VC FLAP INBD SIDE, IAW SRM 57-43-02-2R-5 REV. 107 REFER TO SOPM 20-50-12 REV. 160 PERFORM REPAIR.
- [SDR IPXA2026070624589](https://openairdocs.org/sdr/IPXA2026070624589), Jun 30, 2026: SEAL. BROKEN. BROKEN MOLDING SEAL, LT WING NR 2 VC FLAP INBD SIDE. REMOVED THE RAIN EROSION SHIELDS AND CLEANED. APPLY THE SEALANT TO REPAIR AREA.
- [SDR IPXA2026070324858](https://openairdocs.org/sdr/IPXA2026070324858), Jun 30, 2026: SKIN. DAMAGED. ABRADED SKIN, UPPER FACE OF LT WING INBD L/E REFUELING STATION LOWER DOOR, PANEL 521BB, IAW AMM 52-49-09-402-003, REV 116. INSTALLED REFUELING PANEL 521BB. COND
- [SDR IPXA2026070420634](https://openairdocs.org/sdr/IPXA2026070420634), Jun 30, 2026: FAIRING. DEBONDED. DEBONDED PANEL, AFT WING TO BODY FAIRING PANEL 193CL EXTERNAL SURFACE. IAW AMM 20-51-01-912-008 REV.116 INSTALL PANEL 193CL. CONDITION CHECK NORMAL.
- [SDR IPXA2026070524776](https://openairdocs.org/sdr/IPXA2026070524776), Jun 30, 2026: SKIN. CRACKED. CRACKED SKIN, RT WING T/E NEAR INBD AILERON PANEL 673AB. IAW SRM 57-51-01-2R-1 REFER TO SRM 51-70-07-0G-0 REV.107 PERFORM REPAIR AS BELOW STEP: REMOVE THE DAMAG
- [SDR IPXA2026070324807](https://openairdocs.org/sdr/IPXA2026070324807), Jun 30, 2026: SKIN. CRACKED. CRACKED SKIN, RT WING T/E NEAR INBD AILERON 673CB. IAW AMM 20-51-01-912-008 REV. 116 INSTALLED THE ACCESS PANEL 673CB. CONDITION CHECKED NORMAL.
- [SDR IPXA2026070624831](https://openairdocs.org/sdr/IPXA2026070624831), Jun 30, 2026: SKIN. CRACKED. CRACKED SKIN, LOWER FACE OF LT WING INBD L/E REFUELING STATION LOWER DOOR CUTOUT, ILES 845. IAW AMM 52-49-09-402-003, REV. 116. INSTALLED REFUELING PANEL NO. 52
- [SDR IPXA2026073009895](https://openairdocs.org/sdr/IPXA2026073009895), Jun 29, 2026: WEB. CRACKED. SURFACE & HOLE CRACK INDICATION , DURING PFM SB 747-57A2357 FND SURFACE & HOLE CRACK . ACCOMPLISHED REPAIR IAW EO-98227-REQ1, REV 1, & EGAT EI F2026A57M-1427, R
- [SDR IPXA2026072111084](https://openairdocs.org/sdr/IPXA2026072111084), Jun 29, 2026: PANEL. DEBONDED. DEBONDED PANEL, VERTICAL STABILIZER LOWER PANEL 322BL. REPAIR DISBOND ON PANEL ASSY OF VST FWD TORQUE BOX BETWEEN STA 2365 AND STA 2413 I.A.W. EGAT EI F2026A55M
- [SDR IPXA2026072111043](https://openairdocs.org/sdr/IPXA2026072111043), Jun 29, 2026: PANEL. DEBONDED. DISBONDED PANEL , VERTICAL STABILIZER LOWER PANEL 322CL. REPAIR DISBOND DAMAGE ON LH FWD LWR VST FORWARD TORQUE BOX PANEL BETWEEN STA 2285 AND 2365 AND BETWEEN 
- [SDR IPXA2026070697892](https://openairdocs.org/sdr/IPXA2026070697892), Jun 28, 2026: SEAL. BROKEN. BROKEN MOLDING SEAL, L/H WING NR 4 VC FLAP INBD SIDE MOLDING. IAW SRM 57-43-02-2R-5, REV 107, REFER TO SOPM 20-50-12 REV 160. PERFORMED A REPAIR, REMOVED THE RA
- [SDR IPXA2026070697902](https://openairdocs.org/sdr/IPXA2026070697902), Jun 28, 2026: SEAL. BROKEN. BROKEN MOLDING SEAL, LT WING NR 5 VC FLAP INBD SIDE. IAW SRM 57-43-02-2R-5, REV 107, REFER TO SOPM 20-50-12, REV 160. PERFORMED A REPAIR, REMOVED THE RAIN EROSI
- [SDR IPXA2026072186856](https://openairdocs.org/sdr/IPXA2026072186856), Jun 27, 2026: SEAL. DAMAGED. FOUND NR 1 ENTRY DOOR LOWER SEAL DAMAGED. IAW AMM 52-09-00-308-001, REV.116. REPLACED NR 1 ENTRY DOOR LOWER SEAL. CONDITION CHECK NORMAL.
- [SDR IPXA2026071085535](https://openairdocs.org/sdr/IPXA2026071085535), Jun 27, 2026: SKIN. BROKEN. CRACKED SKIN, RT WING L/E NR 23 V.C FLAP INBD LWR. ACCOMPLISHED JOB IAW EO-97981-REQ1, REV1 AND EGAT EI F2026A57M-1340. ACCOMPLISHED JOB I.A.W UPS EO-97981-REQ1
- [SDR IPXA2026062986856](https://openairdocs.org/sdr/IPXA2026062986856), Jun 27, 2026: SEAL. DAMAGED. FOUND NO.1 ENTRY DOOR LOWER SEAL DAMAGED
- [SDR IPXA2026073003261](https://openairdocs.org/sdr/IPXA2026073003261), May 28, 2026: STIFFENER. WORN. MAJOR REPAIR, SUPPORT ROD INSIDE FUELING PANEL STATION AFT ATTACH BOLT HOLE IS ELONGATED AND ATTACH ANGLE IS WORN. ACCOMPLISH THE REPAIR IAW EO-97627-REQ2 REV1 
- [SDR IPXA2026060120516](https://openairdocs.org/sdr/IPXA2026060120516), May 11, 2026: FUEL SYS. OUT OF BALANCE. AFTER LEVEL OFF ENG 3 FUEL INDICATED 2,000LBS LESS THAN ENG 2. WE BALANCED THE FUEL MANUALLY BUT HAD TO CONTINUE TO BALANCE THE FUEL THE ENTIRE FLIGHT. SUSPECT 
- [SDR IPXA2026051220516](https://openairdocs.org/sdr/IPXA2026051220516), May 11, 2026: TRANSFER SYS. MALFUNCTIONED. AFTER LEVEL OFF ENG 3 FUEL INDICATED 2,000LBS LESS THAN ENG 2. WE BALANCED THE FUEL MANUALLY BUT HAD TO CONTINUE TO BALANCE THE FUEL THE ENTIRE FLIGHT. SUSPECT 
- [SDR IPXA2026041322009](https://openairdocs.org/sdr/IPXA2026041322009), Apr 9, 2026: WINDOW. CRACKED. AT FL 370 FWD WINDOW LEFT CRACKED. R & R L1 WINDOW IAW AMM 56-11-01/401. REPLACED WINDOW HEAT CONTROL UNIT IAW AMM 30-41-01/401. OPS CHKD WINDSHIED HEATER SYS A
- [SDR IPXA2026041022009](https://openairdocs.org/sdr/IPXA2026041022009), Apr 9, 2026: WINDOW. CRACKED. AT FL 370, FWD WINDOW LEFT CRACKED
- [SDR IPXA2026012682273](https://openairdocs.org/sdr/IPXA2026012682273), Jan 26, 2026: START VALVE. FAULTED. AIR TURN BACK, NR 3 STARTER CUTOUT EICAS MESSAGE IN CLIMB, CONTINUED THROUGH FLIGHT. QRH PROCEDURE FOLLOWED. R & R NR 3 ENG START VALVE IAW AMM 80-11-02/401 & O
- [SDR IPXA2025012496294](https://openairdocs.org/sdr/IPXA2025012496294), Jan 9, 2025: SKIN. DAMAGED. DAMAGE AFT OFF TAIL STAND MOUNT FOUND DURING WALK-AROUND FOR CORRECTIVE ACTION PLEASE SEE REF: EO-92470-REQ1 (SECTION 48 FUSELAGE SKIN PANEL DENT, GOUGE, AND CR
- [SDR IPXA202501096294](https://openairdocs.org/sdr/IPXA202501096294), Jan 9, 2025: STRUCTURE. DAMAGED. DAMAGE AFT OFF TAIL STAND MOUNT FOUND DURING WALK-AROUND DIRECT AFTER LANDING WE FOUND DAMAGE TO THE TAIL AREA OF THE AIRPLANE. BEFORE GROUND HANDLING TOUCHED T
- [SDR IPXA2024122341321](https://openairdocs.org/sdr/IPXA2024122341321), Dec 21, 2024: BULB. INOPERATIVE. EMERGENCY LIGHT IN CEILING PANEL ABOVE L-1 DOOR FWD BULB INOP. RE-LAMPED FWD BULB IN EMERGENCY CEILING LIGHT ABOVE L1 DOOR PER AMM 33-51-07. OPS CHECK GOOD PER 
- [SDR IPXA2024101703256](https://openairdocs.org/sdr/IPXA2024101703256), Oct 12, 2024: FLOOR PANEL. CRACKED. MAIN CARGO DECK FLOOR PANEL APPROX. STA 1140 L TO APPROX STA 1220L CRACKED ALONG ENTIRE OUTBID LENGTH MARKED WITH TAPE. INSTALLED NEW FLOOR PANEL IAW AMM 53-21-
- [SDR IPXA2024070771367](https://openairdocs.org/sdr/IPXA2024070771367), Jun 22, 2024: SKIN. DENTED. DENT -SKIN, LH WING OUTBD AFT FLAP OUTBD LOWER SIDE.REMOVED THE DAMAGED SKIN,MEASURE THE CUTOUT (DIA:0.8", 10.75" FROM OUTBD EDGE I.A.W. 747-400F SRM 57-53-01-2
- [SDR IPXA20240701367](https://openairdocs.org/sdr/IPXA20240701367), Jun 22, 2024: SKIN. DENTED. DENT -SKIN, LH WING OUTBD AFT FLAP OUTBD LOWER SIDE. (REPAIR) PERFORMED NDT/UT REWORKED AREA AND PLUS 8" AROUND HEATED AREA, I.A.W. 747 NDT MANUAL PART 1 51-01-
- [SDR IPXA2024070258057](https://openairdocs.org/sdr/IPXA2024070258057), Jun 21, 2024: SHEAR TIE. CRACKED. L/H FRONT SPAR THE SHEAR TIE AT LBL 75.92, STA 1000. REMOVED HARNESS FOR SM REWORK UNDER FLOOR PANEL IAW SWPM 20-10-12
- [SDR IPXA2024070258045](https://openairdocs.org/sdr/IPXA2024070258045), Jun 21, 2024: FITTING. CRACKED. R/H FRONT SPAR THE INERCOSTAL LUG FITTING AT RBL 11.33 STA 1000 REMOVED BOTS AT STA 1000. CKD NORMAL. REMOVED TUBE. CKD NORMAL IAW IPC 57-14-01-01A.
- [SDR IPXA2024070257995](https://openairdocs.org/sdr/IPXA2024070257995), Jun 21, 2024: FITTING. CRACKED. L/H FRONT SPAR THE INTERCOSTAL LUG FITTING AT LBL 11.30, STA 1000.REMOVED AND REINSTALLED THE BOLTS AND TUBE AT STA 1000. CONDITIONS WERE NORMAL IAW AMM 20-11-2
- [SDR IPXA2024070518937](https://openairdocs.org/sdr/IPXA2024070518937), Jun 19, 2024: STRINGER. CRACKED. STRINGER, L/H WING NO.7 V/C FLAP (REPLACE) INSTALL NEW PART IAW SRM 51-40-02-0G REV.101 AND BOEING DWG NO: 65B15170 SH 2 REV:H. IAW AMM 27-81-02-404-010, REV110
- [SDR IPXA2024041455734](https://openairdocs.org/sdr/IPXA2024041455734), Feb 25, 2024: SKIN. DENTED. NUMBER 14 INBOARD MOST RIGHT WING KRUGER FLAP HAS 2 DENTS VERIFIED CORRECT CLEARANCES AND OPS CHECK OF THE #14 KRUEGER FLAP IAW AMM 27-81-01. ALL CHECKS GOOD AT
- [SDR IPXA2024081812684](https://openairdocs.org/sdr/IPXA2024081812684), Jun 26, 2023: SKIN. CRACKED. HFEC REINSPECT REVEALED CRACK INDICATION AND NEW DAMAGED IDENTIFIED VISUALLY (T3F18E001Y856 CLOSED IN ERROR) FABRICATED REPAIR DOUBLER AND FILLER IAW SRM 53-00-
- [SDR IPXA2023062831080](https://openairdocs.org/sdr/IPXA2023062831080), May 27, 2023: STRUCTURE. PUNCTURED. LH I/B AFT FLAP HAS A PUNCTURE APPROX 26.75€? FROM TRAILING EDGE & 63€? FROM I/B EDGE. MARKED WITH TAPE.***SM36/LMX4/HGR*** ACCOMPLISHED STEPS 1-14 OF EO-8718
- [SDR IPXA2022122046355](https://openairdocs.org/sdr/IPXA2022122046355), Dec 18, 2022: GUST LOCK. BROKEN. L1 CREW ENTRANCE DOOR LATCH TO HOLD OPEN IS BROKEN CLEANED AND CHECKED HOLD OPEN MECHANISM IAW AMM 52-11-00-201 REV. 106.01. FOUND SATIS
- [SDR IPXA2022081179940](https://openairdocs.org/sdr/IPXA2022081179940), Jul 17, 2022: LIGHT. INOPERATIVE. **SUPPLEMENTAL SDR**FAULT FOUND THE MAIN DECK L1 DOOR AREA EMERGENCY LIGHT INOP (REPLACE) TASK COMPLETED IAW AMM 33-51-01 REV39.00
- [SDR IPXA2022080419083](https://openairdocs.org/sdr/IPXA2022080419083), Jun 26, 2022: PANEL. BROKEN. FAULT - BROKEN - LEFT WING OUTBOARD FORE FLAP ACCESS PANEL WBL 754 (REPAIR) TASK COMPLETED
- [SDR IPXA2022080100360](https://openairdocs.org/sdr/IPXA2022080100360), Jun 20, 2022: PANEL. CORRODED. FAULT - CORROSION - SUPPORT, RH AIR CONDITION COMPARTMENT ACCESS DOOR, MIDDLE SUPPORT. (REPLACE) TASK COMPLETED
- [SDR IPXA2022032580472](https://openairdocs.org/sdr/IPXA2022032580472), Mar 25, 2022: FLOOR PANEL. DAMAGED. INSPECTION TYPE:N/AMAIN DECK FLOOR PANEL POS 9L HAS DAMAED UPEPR FACE SHEETFABRICATE REPLACEMENT FLOOR PANEL PER EO B747-5320-42648-A
- [SDR IPXA2022032580471](https://openairdocs.org/sdr/IPXA2022032580471), Mar 25, 2022: FLOOR PANEL. DELAMINATED. INSPECTION TYPE:N/AUPPER FACE SHEET OF FLOOR PANEL POS 9L DELAMINATEDFABRICATE NEW FLOOR PANEL PER EO B747-5320-42648-A

All 181: https://openairdocs.org/aircraft/N572UP/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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