# N570UP: 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: 35667
- Year built: 2007
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: June 27, 2007
- Certificate issued: July 25, 2025
- Expires: July 31, 2032
- Mode S code: A75039
- 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=570UP
- Page: https://openairdocs.org/aircraft/N570UP

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 N570UP.

## FAA accident and incident reports

None matched to N570UP.

## Service difficulty reports (150, 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 IPXA2026092951034](https://openairdocs.org/sdr/IPXA2026092951034), Sep 21, 2026: DOOR. DAMAGED. UNKNOWN NOISE & VIBRATION FROM AIRCRAFT ON CLIMBOUT RESULTED IN AIR TURN BACK. FOUND #2 AIR INLET DOOR DAMAGED. INSTALLED NEW INLET DOOR ASSY IAW AMM 21-62-02.
- [SDR IPXA2026092251034](https://openairdocs.org/sdr/IPXA2026092251034), Sep 21, 2026: UNKNOWN. VIBRATION. ATB, UNKNOWN NOISE & VIBRATION FROM AIRCRAFT DURING CLIMBOUT. RESULTED IN AIR TURN BACK.
- [SDR IPXA2026020652253](https://openairdocs.org/sdr/IPXA2026020652253), Jan 30, 2026: ANTENNA. FAULTED. AIR TURN BACK, TCAS SYSTEM ADVISORY MESSAGE CHECK CMC PRESENT LEG FAULT.FND TCAS LOWER ANTENNA FAIL. REPLACED LOWER TACAS ANTENNA .PFM GOUND TEST PASS.PER AMM34
- [SDR IPXA2025111341703](https://openairdocs.org/sdr/IPXA2025111341703), Nov 12, 2025: ENGINE. OIL CONSUMPTION. INFLIGHT SHUTDOWN, EMERGENCY DECLARED. DURING CRUISE AT APPROX 3.5 HRS INTO FLT. ENG 4 OIL QTY BEGAN TO DROP FROM 5 QT TO ZERO IN 25 MINS. OIL PRESS WAS NORMAL 
- [SDR IPXA2025042900346](https://openairdocs.org/sdr/IPXA2025042900346), Apr 23, 2025: LIGHT. INOPERATIVE. INTERIOR EMERGENCY LIGHT ON MAIN DECK L1 DOOR AREA INOP. RE-LAMPED INTERIOR EMERGENCY LIGHT ON MAIN DECK L1 DOOR AREA IAW AMM 33-51-07. OPS CHECK GOOD AT THIS T
- [SDR IPXA2025042300346](https://openairdocs.org/sdr/IPXA2025042300346), Apr 23, 2025: LIGHT. INOPERATIVE. INTERIOR EMERGENCY LIGHT ON MAIN DECK L1 DOOR AREA INOP DEFERRED IAW MEL 33-51-1-0-2. PLACARD INSTALLED
- [SDR IPXA2025021997634](https://openairdocs.org/sdr/IPXA2025021997634), Feb 17, 2025: SEAT TRACK. DAMAGED. UPON REMOVAL OF CAPTAINS SEAT INSPECTED OUTBOARD FWD TRACK(PRECAUTIONARY) AND FOUND THAT TRACK TO BE CRACKED AT THE FORWARD STOP AREA AS WELL. REPLACED CAPTAINS
- [SDR IPXA2025021897634](https://openairdocs.org/sdr/IPXA2025021897634), Feb 17, 2025: SEAT TRACK. CRACKED. UPON REMOVAL OF CAPTAINS SEAT INSPECTED OUTBOARD FWD TRACK(PRECAUTIONARY) AND FOUND THAT TRACK TO BE CRACKED AT THE FORWARD STOP AREA AS WELL. OPEN
- [SDR IPXA2025021897613](https://openairdocs.org/sdr/IPXA2025021897613), Feb 17, 2025: SEAT TRACK. CRACKED. WHILE STOWING CAPTAINS SEAT FOUND INBOARD FORWARD SEAT TRACK BROKEN AT FORWARD STOP AREA. RR'D CAPTAINS SEAT INBOARD, FORWARD TRACK ASSY PER AMM REF 25-11-01-82
- [SDR IPXA2024112247889](https://openairdocs.org/sdr/IPXA2024112247889), Nov 22, 2024: LAMP. BROKEN. L1 DOOR FWD EMERGENCY LIGHT INOP REMOVED AND REPLACED L1 DOOR FWD EMERGENCY LIGHT LAMP IAW B747-400 AMM 33-51-05. OPS CHECKED GOOD, NO DEFECTS NOTED AT THIS TIM
- [SDR IPXA2024012299859](https://openairdocs.org/sdr/IPXA2024012299859), Jan 12, 2024: ACCESS PANEL. DAMAGED. **SUPPLEMENTAL SDR**FAULT - RIGHT OUTBD ELEVATOR ACCESS PANEL 344LBR, PANEL SKIN ONE HOLE (REPAIR) REVIEWED
- [SDR IPXA2024011299859](https://openairdocs.org/sdr/IPXA2024011299859), Jan 12, 2024: UNKNOWN. UNKNOWN. *SDR FILED OPEN* FAULT - RIGHT OUTBD ELEVATOR ACCESS PANEL 344LBR, PANEL SKIN ONE HOLE (REPAIR) OK TO WORK
- [SDR IPXA2024012239172](https://openairdocs.org/sdr/IPXA2024012239172), Jan 9, 2024: SEAL DEPRESSOR. DAMAGED. FAULT - FWD CARGO DOOR FWD UPPER CORNER SEAL DEPRESSOR DAMAGE. (REPLACE). I.A.W AMM 20-51-01-912-008 REV.109 INSTALL SEAL DEPRESSOR. I.A.W AMM 53-21-02-004-001 
- [SDR IPXA2024012239192](https://openairdocs.org/sdr/IPXA2024012239192), Jan 9, 2024: SEAL DEPRESSOR. DAMAGED. FAULT - FWD CARGO DOOR AFT UPPER CORNER SEAL DEPRESSOR DAMAGE. (REPLACE). I.A.W AMM 20-51-01-912-008 REV.109 INSTALL SEAL DEPRESSOR. I.A.W AMM 53-21-02-004-001 
- [SDR IPXA2024012239212](https://openairdocs.org/sdr/IPXA2024012239212), Jan 9, 2024: BEAM. CRACKED. **SUPPLEMENTAL SDR**FAULT - CRACK WEB L/H WING CTR FXD LE CAVITY NOSE BEAM , ILES 692. (REPAIR) C/W REVIEW
- [SDR IPXA2024010939212](https://openairdocs.org/sdr/IPXA2024010939212), Jan 9, 2024: UNKNOWN. UNKNOWN. CRACKED WEB L/H WING CTR FXD LE CAVITY NOSE BEAM , ILES 692. (REPAIR)
- [SDR IPXA2024021902794](https://openairdocs.org/sdr/IPXA2024021902794), Jan 6, 2024: SKIN. DENTED. *SUPPLEMENTAL SDR* FAULT- SECTION 46 FUSELAGE SKIN REPAIR DOUBLE ONE DENT , STA1920-1940, S-31~S32R.(EVALUATE) 1.MEASURE DENT DIMENSION LENGTH:2.4", WIDTH:1.35"
- [SDR IPXA2024012204223](https://openairdocs.org/sdr/IPXA2024012204223), Jan 6, 2024: SKIN PANEL. CRACKED. **SUPPLEMENTAL SDR**FAULT - CRACK - SKIN PNL, LH WING INBD TE UPPER FIXED PNL WBL 235 (REPAIR) REVIEWED
- [SDR IPXA2024012204170](https://openairdocs.org/sdr/IPXA2024012204170), Jan 6, 2024: SKIN. DEBONDED. **SUPPLEMENTAL SDR**FAULT - DISBOND - SKIN, EXTERNAL FORWARD UPPER SIDE PNL OF NO.1 PYLON TO WING (REPAIR) REVIEWED
- [SDR IPXA2024012204105](https://openairdocs.org/sdr/IPXA2024012204105), Jan 6, 2024: SKIN. GOUGED. **SUPPLEMENTAL SDR**FAULT - GOUGE - SKIN, RH WING INBD MID FLAP COVE PANEL LWR SURFACE (REPAIR) REVIEWED
- [SDR IPXA2024012202767](https://openairdocs.org/sdr/IPXA2024012202767), Jan 6, 2024: RIB. CRACKED. **SUPPLEMENTAL SDR**FAULT- CRACK - WEB, RH WING BL 255.692 FXD TE RIB. (REPAIR) C/W REVIEW
- [SDR IPXA2024010804223](https://openairdocs.org/sdr/IPXA2024010804223), Jan 6, 2024: UNKNOWN. UNKNOWN. CRACK - SKIN PNL, LH WING INBD TE UPPER FIXED PNL WBL 235 (REPAIR)
- [SDR IPXA2024010802767](https://openairdocs.org/sdr/IPXA2024010802767), Jan 6, 2024: UNKNOWN. UNKNOWN. *SDR FILED OPEN* FAULT- CRACK - WEB, RH WING BL 255.692 FXD TE RIB. (REPLACE) OK TO WORK
- [SDR IPXA2024010802794](https://openairdocs.org/sdr/IPXA2024010802794), Jan 6, 2024: UNKNOWN. UNKNOWN. SECTION 46 FUSELAGE SKIN REPAIR DOUBLE ONE DENT , STA1920-1940, S-31~S32R.(EVALUATE) PERFORMED NDT/ET FOR DENT AREA, I.A.W.747 NDT MANUAL PART 6, 51-00-00 PROCE
- [SDR IPXA2024010804170](https://openairdocs.org/sdr/IPXA2024010804170), Jan 6, 2024: UNKNOWN. UNKNOWN. DISBOND - SKIN, EXTERNAL FORWARD UPPER SIDE PNL OF NO.1 PYLON TO WING (REPAIR)
- [SDR IPXA2024010804105](https://openairdocs.org/sdr/IPXA2024010804105), Jan 6, 2024: UNKNOWN. UNKNOWN. GOUGED SKIN, RH WING INBD MID FLAP TE UPR FXD PNL LWR SURFACE, WBL 443 (REPAIR)
- [SDR IPXA2024012287760](https://openairdocs.org/sdr/IPXA2024012287760), Jan 5, 2024: SUPPORT BEAM. CRACKED. **SUPPLEMENTAL SDR**FAULT - CRACK - CHORD, LH WING INBD TE SUPPORT BEAM OUTBD END CHORD UPPER SIDE. (REPLACE) REVIEWED
- [SDR IPXA2024012287687](https://openairdocs.org/sdr/IPXA2024012287687), Jan 5, 2024: ANGLE. CRACKED. **SUPPLEMENTAL SDR**FAULT - CRACK - CLIP, RH WING WBL 322.636 TO 303.33 TE LWR RIB. (REPLACE) REVIEWED
- [SDR IPXA2024012287659](https://openairdocs.org/sdr/IPXA2024012287659), Jan 5, 2024: SKIN. CRACKED. **SUPPLEMENTAL SDR**FAULT - CRACK - SKIN, RH WING NO.18 VC FLAP FOLDING NOSE INBD END. (REPAIR) REVIEWED
- [SDR IPXA2024012285873](https://openairdocs.org/sdr/IPXA2024012285873), Jan 5, 2024: SKIN. DEBONDED. **SUPPLEMENTAL SDR**FAULT - DISBOND - SKIN PNL, LH WING INBD FORE FLAP NOSE SKIN PNL (REPAIR) REVIEWED
- [SDR IPXA2024012285716](https://openairdocs.org/sdr/IPXA2024012285716), Jan 5, 2024: PANEL. CRACKED. **SUPPLEMENTAL SDR**FAULT - CRACK - SKIN PNL, LH WING CENTER LE LOWER SKIN PNL ILES 848 (REPAIR) REVIEWED
- [SDR IPXA2024012285961](https://openairdocs.org/sdr/IPXA2024012285961), Jan 5, 2024: LENS. CRACKED. **SUPPLEMENTAL SDR**FAULT - CRACK - LENS, RH WING EXTENSION NAV LT FWD FAIRING. (REPLACE) REVIEWED
- [SDR IPXA2024010885873](https://openairdocs.org/sdr/IPXA2024010885873), Jan 5, 2024: UNKNOWN. UNKNOWN. DISBOND - SKIN PNL, LH WING INBD FORE FLAP NOSE SKIN PNL WS 614. (REPAIR) OK TO WORK
- [SDR IPXA2024010887687](https://openairdocs.org/sdr/IPXA2024010887687), Jan 5, 2024: UNKNOWN. UNKNOWN. CRACK - CLIP, RH WING WBL 322.636 TO 303.33 TE LWR RIB. (REPLACE) OK TO WORK
- [SDR IPXA2024010587760](https://openairdocs.org/sdr/IPXA2024010587760), Jan 5, 2024: UNKNOWN. UNKNOWN. *** SDR FILED OPEN *** FAULT - CRACK - CHORD, LH WING INBD TE SUPPORT BEAM OUTBD END CHORD UPPER SIDE. (REPLACE)
- [SDR IPXA2024010585961](https://openairdocs.org/sdr/IPXA2024010585961), Jan 5, 2024: UNKNOWN. UNKNOWN. *** SDR FILED OPEN *** FAULT - CRACK - LENS, RH WING EXTENSION NAV LT FWD FAIRING. (REPLACE) OK TO WORK
- [SDR IPXA2024010585716](https://openairdocs.org/sdr/IPXA2024010585716), Jan 5, 2024: UNKNOWN. UNKNOWN. *** SDR FILED OPEN *** FAULT - CRACK - SKIN PNL, LH WING CENTER LE LOWER SKIN PNL ILES 848 (REPAIR) OK TO WORK
- [SDR IPXA2024010587659](https://openairdocs.org/sdr/IPXA2024010587659), Jan 5, 2024: UNKNOWN. UNKNOWN. *** SDR FILED OPEN *** FAULT - CRACK - SKIN, RH WING NO.18 VC FLAP FOLDING NOSE INBD END. (REPAIR)
- [SDR IPXA2024012252351](https://openairdocs.org/sdr/IPXA2024012252351), Jan 3, 2024: BEAM. CRACKED. **SUPPLEMENTAL SDR**FAULT - WEB CRACK - L/H WING L/E NOSE BEAM AT ILES 693 (REPAIR) ALL PAPERWORK C/W
- [SDR IPXA2024012252333](https://openairdocs.org/sdr/IPXA2024012252333), Jan 3, 2024: BEAM. CRACKED. **SUPPLEMENTAL SDR**FAULT - UPPER CHORD CRACK - R/H WING L/E NOSE BEAM AT ILES 693 (REPAIR) ALL PAPERWORK C/W
- [SDR IPXA2024011852388](https://openairdocs.org/sdr/IPXA2024011852388), Jan 3, 2024: SPAR. CORRODED. **SUPPLEMENTAL SDR**FAULT - CENTER TANK REAR SPAR WEB CORROSION ON GROUND POINT AREA OF JETTSION PUMP AT STA 1241 LBL 91 (REPAIR) ALL PAPERWORK C/W
- [SDR IPXA2024010452351](https://openairdocs.org/sdr/IPXA2024010452351), Jan 3, 2024: UNKNOWN. UNKNOWN. WEB CRACK - L/H WING L/E NOSE BEAM AT ILES 693 (REPAIR) OK TO WORK
- [SDR IPXA2024010452388](https://openairdocs.org/sdr/IPXA2024010452388), Jan 3, 2024: UNKNOWN. UNKNOWN. CENTER TANK REAR SPAR WEB CORROSION ON GROUND POINT AREA OF JETTSION PUMP AT STA 1241 LBL 91 (REPAIR) OK TO WORK
- [SDR IPXA2024010452333](https://openairdocs.org/sdr/IPXA2024010452333), Jan 3, 2024: UNKNOWN. UNKNOWN. UPPER CHORD CRACK - R/H WING L/E NOSE BEAM AT ILES 693 (REPAIR) OK TO WORK
- [SDR IPXA2023121481575](https://openairdocs.org/sdr/IPXA2023121481575), Dec 14, 2023: LIGHT. INOPERATIVE. CREW REST EMERGENCY LIGHT INOP REMOVED AND REPLACED CREW REST EMERGENCY LIGHT LAMP IAW B747-400 AMM 33-51-07-962-001. OPS CHECK GOOD. NO DEFECTS NOTED AT THIS T
- [SDR IPXA2023120481904](https://openairdocs.org/sdr/IPXA2023120481904), Dec 3, 2023: FIRE DETECTOR. FALSE ACTIVATION. *** ATB *** IMMEDIATELY AFTER TAKEOFF €Œ DET FIRE/OHT 4€? ANNUNCIATION ON EICAS. CHECKLIST ACTIONED. FUEL JETTISON CHECKLIST ACTIONED. 26,000 LB DUMPED REMOVE
- [SDR IPXA2023060145039](https://openairdocs.org/sdr/IPXA2023060145039), May 15, 2023: A/C PACK. WARNING MESSAGE. *** SUPPLEMENTAL SDR - FILED IN ERROR *** PACK 2 STATUS MESSAGE (LINKED ALERT T3F18E001DMGH) PERFORMED PACK #2 SYSTEM A AND B GROUND TEST IAW AMM 21-51-00, TEST
- [SDR IPXA2023051545039](https://openairdocs.org/sdr/IPXA2023051545039), May 15, 2023: UNKNOWN. UNKNOWN. PACK 2 STATUS MESSAGE (LINKED ALERT T3F18E001DMGH) PERFORMED PACK #2 SYSTEM A AND B GROUND TEST IAW AMM 21-51-00, TEST FAILING PACK SYSTEM B CONTROLLER. SYSTEM 
- [SDR IPXA2024011592332](https://openairdocs.org/sdr/IPXA2024011592332), Jan 8, 2023: PANEL. DENTED. NO. 13 KRUEGER FLAP PANEL DENT/DELAMINATION***SM26/LMX6*** ALL JOB DONE
- [SDR IPXA2022030779796](https://openairdocs.org/sdr/IPXA2022030779796), Mar 7, 2022: DOOR. NONE. INSPECTION TYPE:N/A**SDR FILED OPEN** L1 ENTRY DOOR OPEN ,SYNOPTI C SHOW DOOR CLOSED ,ALSO NO ASSOCIATED EICAS MSG SAYING DOOR OPEN. 1.PER MEL 52-73-1-0-1 RLS A

All 150: https://openairdocs.org/aircraft/N570UP/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

## Earlier aircraft with N570UP

The FAA can reassign an N-number once a registration is cancelled. These aircraft carried N570UP before.

- [Cancelled 1997-03-17](https://openairdocs.org/deregistered/N570UP-1997-03-17): Swearingen SA227-AT, S/N AT570. Exported to Australia. Owner: [Wilmington Trust Company Owner Trustee](https://openairdocs.org/faa-owner/WILMINGTON%20TRUST%20COMPANY%20OWNER%20TRUSTEE), [Wilmington, DE](https://openairdocs.org/faa-place/DE/Wilmington)

## 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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