# N583UP: 1993 Boeing 747-4R7F

- Status: Valid registration
- Airframe: [Boeing 747-4R7F](https://openairdocs.org/model/boeing-747-4r7f) (registry code 13848BP, 490 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: 25867
- Year built: 1993
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: March 24, 2011
- Certificate issued: January 21, 2011
- Expires: January 31, 2030
- Mode S code: A782DD
- 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=583UP
- Page: https://openairdocs.org/aircraft/N583UP

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 747-4R7F)

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 N583UP.

## FAA accident and incident reports

None matched to N583UP.

## Service difficulty reports (419, 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 IPXA2026073173712](https://openairdocs.org/sdr/IPXA2026073173712), Jul 9, 2026: HINGE. BROKEN. FOUND RT WING NR 24 V.C FLAP INBD SIDE FOLDING NOSE HINGE BROKEN. OK TO INSTALL, CONDITION CHECK SATISFIED. IAW AMM 27-81-02-404-010 REV.117 ASSEMBLY RT WING NR
- [SDR IPXA2026071539478](https://openairdocs.org/sdr/IPXA2026071539478), Jul 7, 2026: STRINGER. DAMAGED. FOUND LT WING NR 5 VC FLAP UPPER SIDE STRINGER DAMAGE. INSTALL NEW STRINGER IAW SRM 51-40-02-0G REV.107 AND DWG 65B15168, SH2, REV G.
- [SDR IPXA2026072984187](https://openairdocs.org/sdr/IPXA2026072984187), Jul 3, 2026: FITTING. CORRODED. FOUND THE CORROSION ON INBOARD LOWER FITTING CAP AT LT BODY GEAR. IAW AMM 32-13-01-404-022 REV. 117 AND EI NO. F2026A53M-1507 SEQUENCE A, PERFORMED INSTALL, LEA
- [SDR IPXA2026072984213](https://openairdocs.org/sdr/IPXA2026072984213), Jul 3, 2026: FITTING. CORRODED. FOUND THE CORROSION ON INBD LOWER FITTING CAP AT RT BODY GEAR. IAW AMM 32-13-01-404-022 REV. 117 AND EI F2026A53M-1506 SEQUENCE A, PERFORMED INSTALL, LEAK CHECK
- [SDR IPXA2026063066815](https://openairdocs.org/sdr/IPXA2026063066815), Jun 26, 2026: STRUT. WORN. FOUND RH WING OUTBD FLAP SUPPORT STRUT LOWER INSERT, COVE ATTACH WORN OUT, WBL 695. REVIEWED PER GMM-MTX 09.05.01.09. IAW CMM 57-52-55 601, REPAIR PARAGRAPH 1.F
- [SDR IPXA2026072970144](https://openairdocs.org/sdr/IPXA2026072970144), Jun 26, 2026: SPLICE PLATE. CRACKED. DURING PERFORM EO-76733-JIC2 STEP 247, FOUND NR 2 FASTENER HOLE CRACK. ACCOMPLISHED REPAIR IAW EO-98163-REQ1 REV.1 AND EGAT EI F2026A57M-1371 REV 3.
- [SDR IPXA2026072970341](https://openairdocs.org/sdr/IPXA2026072970341), Jun 26, 2026: SKIN. CRACKED. SKIN CRACKED AT BS 560, BELOW S26R. ACCOMPLISHED REPAIR I.A.W EO-98185-REQ1 REV.1 2
- [SDR IPXA2026072140524](https://openairdocs.org/sdr/IPXA2026072140524), Jun 25, 2026: SAFETY NET. FRAYED. FOUND MAIN DECK SIDE CARGO DOOR SAFETY NET FRAYED. IAW AMM 52-32-00-410-801 REV.116 AND AMM 52-32-00-010-801 REV.116 REPLACED MAIN DECK SIDE CARGO DOOR SAFETY N
- [SDR IPXA2026070540146](https://openairdocs.org/sdr/IPXA2026070540146), Jun 25, 2026: SEAL. BROKEN. BROKEN SEAL, NR 3 PYLON 472HR PANEL. REVIEWED TASK IAW GMM-MTX 09.05.01.09. INSTALLED A NEW SEAL IAW SRM 51-40-02-0G, REV.107, AND DWG 65B90466, SH 2, REV D.
- [SDR IPXA2026062940524](https://openairdocs.org/sdr/IPXA2026062940524), Jun 25, 2026: CARGO NET. FRAYED. FOUND MAIN DECK SIDE CARGO DOOR SAFETY NET FRAYED. (REPLACE)
- [SDR IPXA2026070301653](https://openairdocs.org/sdr/IPXA2026070301653), Jun 23, 2026: SNUBBER. OUT OF LIMITS. FOUND NR 1 MAIN ENTRY DOOR ROTARY SNUBBER OUT OF LIMITS. IAW AMM 52-11-10-004-001 REV.116 AND AMM 52-11-10-404-005 REV.116 REPLACED THE SNUBBER.
- [SDR IPXA2026062401653](https://openairdocs.org/sdr/IPXA2026062401653), Jun 23, 2026: SNUBBER. OUT OF LIMITS. FOUND NR 1 MAIN ENTRY DOOR ROTARY SNUBBER OUT OF LIMITS.
- [SDR IPXA2026070183406](https://openairdocs.org/sdr/IPXA2026070183406), Jun 22, 2026: SKIN. DEBONDED. DEBONDED SKIN, LOWER FACE OF LT WING NR 3 FLAP TRACK AFT FAIRING. IAW SRM 57-53-70-2R-1 REFER TO SRM 51-70-07-0G-0 REV. 107
- [SDR IPXA2026070183670](https://openairdocs.org/sdr/IPXA2026070183670), Jun 22, 2026: DOOR. CHAFED. CHAFING- EDGE, NR 2 ENG RT T/R LOWER FORWARD DOOR AFT SIDE. INSTALLED NEW PARTS IAW SRM 51-40-02-0G REV.107 AND IPC 78-32-22 REV.96.
- [SDR IPXA2026062381206](https://openairdocs.org/sdr/IPXA2026062381206), Jun 22, 2026: BRACKET. CHAFED. CHAFING - BRACKET , NR 1 ENG LT CORE COWL SUPPORT ROD SUPPORT FITTING. (REPLACE). INSTALLED NEW BRACKET I.A.W SRM 51-40-02-0G REV.107 AND GOODRICH CMM IPL 71-13
- [SDR IPXA2026071772387](https://openairdocs.org/sdr/IPXA2026071772387), Jun 21, 2026: DUCT. CRACKED. CRACKED DUCT , NR 1 ENG RT CORE COWL PRECOOLER EXHAUST DUCT. IAW AMM 71-11-06-004-001-J00, REV 117, AND AMM 71-11-06-404-006-J00, REV 117, REPLACED THE CORE COW
- [SDR IPXA2026063061139](https://openairdocs.org/sdr/IPXA2026063061139), Jun 20, 2026: PANEL. ERODED. EROSION, L/E, NR 3 PYLON 471B PANEL. REMOVE THE ERODED MATERIALS AND CLEAN. MEASURE THE DAMAGE AREA ( L : 3.5", W : 0.2", D : 1 PLY, AT L/E, 22" FROM INBD EDGE 
- [SDR IPXA2026071961031](https://openairdocs.org/sdr/IPXA2026071961031), Jun 20, 2026: BRACKET. CRACKED. CRACKED CLIP, RT BLG W/W FUILD TRANSFER ALT BRAKE SUPPORT ADJACENT KEEL BEAM AT STA 1394. (REPLACE) 1.REMOVED DAMAGE BRACKET I.A.W SRM 51-40-02-0G REV.107 2.FAB
- [SDR IPXA2026063061135](https://openairdocs.org/sdr/IPXA2026063061135), Jun 20, 2026: PANEL. ERODED. EROSION, L/E, NR 4 PYLON 481B PANEL. IAW SRM 54-51-70-1A-1 REV. 107 REFER TO SOPM 20-50-12 REV. 159 PERFORM REPAIR AS BELOW STEP: REMOVE THE ERODED MATERIALS AN
- [SDR IPXA2026062957241](https://openairdocs.org/sdr/IPXA2026062957241), Jun 20, 2026: SEAL. DAMAGED. NR 26 V.C FLAP, OUTBOARD MOLDING SEAL DAMAGE. INSTALLED NEW BRACKET IAW SRM 51-40-02-0G REV.107 & CMM IPL 71-13-24 REV.50.
- [SDR IPXA2026070240523](https://openairdocs.org/sdr/IPXA2026070240523), Jun 19, 2026: SUPPORT BRACKET. CRACKED. CRACKED ANGLE, RT BLG W/W HYD TUBE SUPPORT BRACKET AT BS 1480 UNDER BLG HYD TRUCK POSITIONER SHUTOFF FUSE. REVIEWED TASK IAW GMM-MTX 09.05.01.09. INSTALLED NEW 
- [SDR IPXA2026071124310](https://openairdocs.org/sdr/IPXA2026071124310), Jun 18, 2026: SKIN. DELAMINATED. DELAMINATED SKIN, LOWER FACE OF LT WING INBD T/E CAVITY LOWER FIXED PANEL, WBL 294. I.A.W. AMM 20-51-01-912-008 REV.117 INSTALLED P-SEAL. CONDITION CHECK NORMAL
- [SDR IPXA2026063024575](https://openairdocs.org/sdr/IPXA2026063024575), Jun 18, 2026: TAIL CONE. DEBONDED. NR 7 FLAP TRACK AFT TAIL CONE, LOWER SKIN FOUND TAPE APPLY. PERFORMED NDT/UT FOR THE REWORKED AREA & PLUS 2" AROUND HEATED AREA , IAW NDT MANUAL PART 1 51-01-01
- [SDR IPXA2026070124788](https://openairdocs.org/sdr/IPXA2026070124788), Jun 18, 2026: RUB STRIP. CHAFED. CHAFED RUB STRIP, NR 3 ENG LT CORE COWL T/E INNER UPPER SIDE. INSTALLED NEW STRIP IAW SRM 51-40-02-0G REV.107 AND CMM IPL 71-13-23 REV.47
- [SDR IPXA2026070124731](https://openairdocs.org/sdr/IPXA2026070124731), Jun 18, 2026: RUB STRIP. CHAFED. CHAFED RUB STRIP, NR 3 ENG RT CORE COWL INNER FACE AFT UPPER EDGE. INSTALLED NEW STRIP IAW SRM 51-40-02-0G REV.107 AND CMM IPL 71-13-24 REV.50.
- [SDR IPXA2026070124595](https://openairdocs.org/sdr/IPXA2026070124595), Jun 18, 2026: FAIRING. DEBONDED. DEBONDED SKIN, LOWER FACE OF LT WING NR 4 FLAP TRACK AFT FAIRING. IAW SRM 57-53-70-2R-1 REFER TO SRM 51-70-17-0G-0 REV. 107 CONDITION CHECK IS SATISFACTORY.
- [SDR IPXA2026070124777](https://openairdocs.org/sdr/IPXA2026070124777), Jun 18, 2026: RUB STRIP. CHAFED. CHAFED RUB STRIP, NR 3 ENG RT CORE COWL T/E INNER UPPER SIDE. INSTALLED NEW STRIP IAW SRM 51-40-02-0G, REV 107, AND CMM IPL 71-13-24, REV 50.
- [SDR IPXA2026063024753](https://openairdocs.org/sdr/IPXA2026063024753), Jun 18, 2026: BRACKET. CHAFED. CHAFED BRACKET ASSY, NR 3 ENG RT CORE COWL HOLD OPEN ROD STOWAGE. REMOVED DAMAGE BRACKET I.A.W SRM 51-40-02-0G REV.107 2. INSTALLED NEW BRACKET I.A.W SRM 51-40-
- [SDR IPXA2026062525030](https://openairdocs.org/sdr/IPXA2026062525030), Jun 18, 2026: BRACKET. CHAFED. FAULT- CHAFING- BRACKET ASSY, NO.3 ENG L/H CORE COWL HOLD OPEN ROD STOWAGE. (REPLACE). INSTALL NEW BRACKET I.A.W SRM 51-40-02-0G REV.107 AND GOODRICH CMM IPL 71
- [SDR IPXA2026062923795](https://openairdocs.org/sdr/IPXA2026062923795), Jun 18, 2026: SEAL. BROKEN. BROKEN MOLDING SEAL, LT WING NR 3 V.C FLAP INBD SIDE CORD MOLDING. IAW SRM 57-43-02-2R-5 REV. 107 REFER TO SOPM 20-50-12 REV. 159 PERFORM REPAIR.
- [SDR IPXA2026062924546](https://openairdocs.org/sdr/IPXA2026062924546), Jun 18, 2026: SEAL. DAMAGED. NR 22 V.C FLAP INBOARD MOLDING SEAL DAMAGE. IAW SRM 57-43-02-2R-5 REV. 107 REFER TO SOPM 20-50-12 REV. 159 PERFORM REPAIR.
- [SDR IPXA2026062924655](https://openairdocs.org/sdr/IPXA2026062924655), Jun 18, 2026: SEAL. BROKEN. BROKEN- MOLDING SEAL, L/H WING NO.1E V.C FLAP INBD SIDE MOLDING. IAW SRM 57-43-02-2R-5 REV. 107 REFER TO SOPM 20-50-12 REV. 159 PERFORM REPAIR
- [SDR IPXA2026062924669](https://openairdocs.org/sdr/IPXA2026062924669), Jun 18, 2026: SEAL. BROKEN. BROKEN- MOLDING SEAL, L/H WING NO.9 V.C FLAP INBD SIDE MOLDING. IAW. SRM 57-43-02-2R-5 REV. 107 REFER TO SOPM 20-50-12 REV. 159 PERFORM REPAIR AS BELOW. REMOVE 
- [SDR IPXA2026072705515](https://openairdocs.org/sdr/IPXA2026072705515), Jun 17, 2026: RUB STRIP. MISSING. FOUND FORWARD CARGO ACTUATOR ARM RUB STRIP MISSING AT FORWARD AND AFTER SIDE I.A.W UPS SREO NO: SREO-69479-REQ2 REV3 TO INSTALL RUB STRIP. REVIEWED PER GMM-MTX 
- [SDR IPXA2026072010384](https://openairdocs.org/sdr/IPXA2026072010384), Jun 17, 2026: BRACKET. BROKEN. BROKEN - BRACKET , LT WING INBD L/E CAVITY AIR DUCT LINK SUPPORT , ILES 1098 (REPLACE). IAW AMM 20-51-01-912-008 REV.117 INSTALLED LT WING L/E DUCT LINK ROD. CO
- [SDR IPXA2026071706780](https://openairdocs.org/sdr/IPXA2026071706780), Jun 17, 2026: BRACKET. CRACKED. CRACKED DISCONNECT PANEL , NR 4 ENG R/H T/R FWD UPPER AREA. REMOVED DAMAGE BRACKET IAW SRM 51-40-02-0G REV.107 2. INSTALLED NEW BRACKET IAW SRM 51-40-02-0G REV.
- [SDR IPXA2026071106966](https://openairdocs.org/sdr/IPXA2026071106966), Jun 17, 2026: SKIN. DEBONDED. DEBONDED SKIN, LT AFT WING TO BODY FAIRING 193 BL. IAW SRM 53-60-70-2R-0 REFER TO SRM 53-00-70-2R-1 AND SRM 51-70-07-0G-0 REV.107. CONDITION CHECK IS SATISFACTO
- [SDR IPXA2026071007466](https://openairdocs.org/sdr/IPXA2026071007466), Jun 17, 2026: STIFFENER. CRACKED. CRACKED BRACKET, NR. 4 ENG LT THRUST REVERSER TORQUE BOX AFT 10:00 POSITION. REMOVED DAMAGE BRACKET IAW SRM 51-40-02-0G REV.107. INSTALLED NEW BRACKET IAW SRM 5
- [SDR IPXA2026070110500](https://openairdocs.org/sdr/IPXA2026070110500), Jun 17, 2026: RUB STRIP. CHAFED. CHAFED RUB STRIP, NR 3 ENG LT CORE COWL INNER FACE AFT UPPER EDGE. INSTALLED NEW STRIP I.A.W SRM 51-40-02-0G REV.107 AND GOODRICH CMM IPL 71-13-23 REV.47
- [SDR IPXA2026072386960](https://openairdocs.org/sdr/IPXA2026072386960), Jun 16, 2026: SKIN PANEL. CRACKED. FUSELAGE SKIN CRACK NEAR STA 1810 S-26R. ACCOMPLISH THE REPAIR I.A.W SRM 53-60-01-02-3 REV.107 AND EGAT WORK SHEET NO.60486 AND EGAT EI NO.F2026A53M-1385 REV.3 
- [SDR IPXA2026072348181](https://openairdocs.org/sdr/IPXA2026072348181), Jun 13, 2026: WEB. CORRODED. CORROSION , WEB OF CENTER WING TANK REAR SPAR NEAR JETTSION PUMP AT STA 1240 RBBL 93. (REPAIR) 1.PERFORMED EO-98103-REQ1 REV.1 AND EGAT EI NO.F2026A57M-1365 REV
- [SDR IPXA2026062586867](https://openairdocs.org/sdr/IPXA2026062586867), May 28, 2026: FAIRING. CRACKED. DURING PHASE 1A HARD LANDING INSPECTION NOTED POSSIBLE ISSUE -FORWARD LOWER CARGO DOOR TOP AFT CORNER REQUIRES -SHEET METAL EVALUATION. IAW AMM 52-34-01-004-001
- [SDR IPXA2026070254508](https://openairdocs.org/sdr/IPXA2026070254508), May 12, 2026: SEAL DEPRESSOR. BROKEN. LOWER FORWARD CRG DOOR SEAL DEPRESSOR WITH MINOR DAMAGE. REVIEWED TASK PER GMM-MTX 09.05.01.09. INSTALLED NEW SEAL I.A.W SRM 51-40-02-0G REV.107 AND BOEING DWG 
- [SDR IPXA2026041766467](https://openairdocs.org/sdr/IPXA2026041766467), Apr 12, 2026: INLET. CRACKED. NR 2 ENGINE INLET COWL 12 O CLOCK POS . CRACK MEASURES 11IN DRILLED 4 EA. COUNTERSINK HOLES FOR HOIST SLING ATTACHMENT POINT PLUGS (BOLTS) I/A/W SRM 51-40-02. I
- [SDR IPXA2026041366467](https://openairdocs.org/sdr/IPXA2026041366467), Apr 12, 2026: COWLING. CRACKED. NR 2 ENGINE INLET COWL 12 O CLOCK POS . CRACK MEASURES 11IN PART IS ON TABLE IN S/M SHOP. BEGAN REMOVAL OF INLET LIP SKIN SECTION. ALL RIVETS REMOVED. SOME TOPS
- [SDR IPXA2026011254239](https://openairdocs.org/sdr/IPXA2026011254239), Jan 5, 2026: FLOOR PANEL. DAMAGED. DURING WALKAROUND FOUND FLOOR PANEL NEAR 15L SPONGY. INSTALLED FLOOR PANEL REF AMM 53-21-02. REF GMM 04-02. PERFORMED A FINAL GVI FOR THE REPLACEMENT OF FLOOR P
- [SDR IPXA2025102314177](https://openairdocs.org/sdr/IPXA2025102314177), Oct 17, 2025: SKIN. CRACKED. FOUND CRACK AT FORWARD LOWER CARGO DOOR CUTOUT AFT LOWER CORNER. C/W EO 95458-REQ1.
- [SDR IPXA2024123042606](https://openairdocs.org/sdr/IPXA2024123042606), Dec 28, 2024: FLOOR PANEL. DAMAGED. FOUND FLOORBOARD ABOVE AFT EQUIPMENT COOLING FANS DAMAGED, APPROX STA 2270, LEFT OF CENTER, ROUTED TO SHEETMETAL. OKAY TO INSTALL FABRICATED FLOORBOARD LOCATED 
- [SDR IPXA2024082414905](https://openairdocs.org/sdr/IPXA2024082414905), Aug 23, 2024: OIL SYSTEM. LOW PRESSURE. DURING CRUISE FLIGHT #4 ENG. OIL QUANITY DROPPED TO ZERO. OVER THE NEXT 20 MINUTES THE OIL PRESSURE DROPPED STEADILY REACHIMG 10 PSI(RED ZONE) THEN IT FLUCTUATE
- [SDR IPXA2024082314905](https://openairdocs.org/sdr/IPXA2024082314905), Aug 23, 2024: INDICATION SYS. FALSE INDICATION. OPEN, DURING CRUISE FLIGHT #4 ENG. OIL QUANITY DROPPED TO ZERO. OVER THE NEXT 20 MINUTES THE OIL PRESSURE DROPPED STEADILY REACHIMG 10 PSI(RED ZONE) THEN IT FLU

All 419: https://openairdocs.org/aircraft/N583UP/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 747-4R7F aircraft: https://openairdocs.org/model/boeing-747-4r7f/aircraft.md
- The GE CF6-80C2B1F engine: https://openairdocs.org/engine/ge-cf6-80c2b1f.md

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