# N582UP: 1997 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: 29053
- Year built: 1997
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: May 25, 2011
- Certificate issued: May 4, 2011
- Expires: May 31, 2027
- Mode S code: A77F26
- Registered owner: [C C & E I LLC](https://openairdocs.org/faa-owner/C%20C%20%26%20E%20I%20LLC)
- Location: [Louisville, KY](https://openairdocs.org/faa-place/KY/Louisville)
- Owner type: LLC
- 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=582UP
- Page: https://openairdocs.org/aircraft/N582UP

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 N582UP.

## FAA accident and incident reports

None matched to N582UP.

## Service difficulty reports (230, 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 IPXA2026081576499](https://openairdocs.org/sdr/IPXA2026081576499), Aug 13, 2026: SPAR CAP. DAMAGED. DURING LIGHTNING STRIKE INSPECTION FOUND RT WING FWD SPAR UPPER T CAP AT WING STATION 891-896 CORRODED WITH TWO PULLED FASTENERS. REMOVED DAMAGED PANEL AND CORR
- [SDR IPXA2026022551482](https://openairdocs.org/sdr/IPXA2026022551482), Feb 23, 2026: SUPPORT ANGLE. CRACKED. LEFT-HAND ELEVATOR, OUTBOARD, TRAILING EDGE WEDGE INTERNAL STRUCTURE CRACKED. REMOVED CRACKED/DAMAGED SUPPORT ANGLE IAW B747 SRM 51-40-02. INSTALLED NEW ANGLE I
- [SDR IPXA2025081263703](https://openairdocs.org/sdr/IPXA2025081263703), May 19, 2025: SKIN. DENTED. BIRD STRIKE OBSERVED ON L/H INBOARD FLAP. ALL STEPS OF EO-93777-REQ3. THIS REPAIR IS CONSIDERED PERMANENT, AND THIS DEFERRAL IS NOW CLOSED.
- [SDR IPXA2025041460385](https://openairdocs.org/sdr/IPXA2025041460385), Mar 26, 2025: TENSION TIE. CRACKED. CRACKED TENSION TIE STA 840 L/H AFT CHANNEL (REPAIR).PERFORMED THE HEAT TREATMENT FROM 2024-O-071 BARE TO T42 CONDITION. I.A.W. WORK SHEET NO. 50219 STEP I AND 
- [SDR IPXA2025041460411](https://openairdocs.org/sdr/IPXA2025041460411), Mar 26, 2025: TENSION TIE. CRACKED. TENSION TIE STA 880 CRACKED, R/H AFT CHANNEL (REPAIR).PERFORMED THE HEAT TREATMENT FROM 2024-O-071 BARE TO T42 CONDITION. I.A.W. WORK SHEET NO. 50219 STEP I AND
- [SDR IPXA2025040160385](https://openairdocs.org/sdr/IPXA2025040160385), Mar 26, 2025: CHANNEL. CRACKED. **SDR FILED OPEN** FAULT - CRACK - TENSION TIE STA 840 L/H AFT CHANNEL (REPAIR) PERFORM W/S 50220 (SRM 53-20-30-2R-2 REV 103)STEP 4.A. B. C.
- [SDR IPXA2025040160411](https://openairdocs.org/sdr/IPXA2025040160411), Mar 26, 2025: CHANNEL. CRACKED. **SDR FILED OPEN** CRACK - TENSION TIE STA 880 R/H AFT CHANNEL (REPAIR) PERFORM W/S 50219 (SRM 53-20-30-2R-2 REV 103)STEP 4.A. B. C.
- [SDR IPXA2025031442035](https://openairdocs.org/sdr/IPXA2025031442035), Mar 14, 2025: RADOME. DAMAGED. BIRD STRIKE ON RIGHT SIDE OF RADOME AT 3:00 POSITION REMOVED AND REPLACED NOSE RADOME WITH REF TO MM 53-52-01-201.
- [SDR IPXA2024121865806](https://openairdocs.org/sdr/IPXA2024121865806), Dec 18, 2024: HANDLE. DAMAGED. MAIN DECK CREW ENTRY DOOR, OUTER HANDLE GUIDE ROLLER MISSING HARDWARE. ROLLER MECHANISM PREVENTING DOOR CLOSURE. DEFERRED PER EO-92323-REQ1 FOR MISSING HARDWARE
- [SDR IPXA2024121833593](https://openairdocs.org/sdr/IPXA2024121833593), Dec 16, 2024: HANDLE. DAMAGED. MAIN DECK CREW ENTRY DOOR, OUTER HANDLE GUIDE ROLLER MISSING HARDWARE. ROLLER MECHANISM PREVENTING DOOR CLOSURE. ACCOMPLISHED EO-92323-REQ1 FOR MISSING HARDWARE
- [SDR IPXA2024121633593](https://openairdocs.org/sdr/IPXA2024121633593), Dec 16, 2024: ROLLER. DAMAGED. MAIN DECK CREW ENTRY DOOR, OUTER HANDLE GUIDE ROLLER MISSING HARDWARE. ROLLER MECHANISM PREVENTING DOOR CLOSURE. ACCOMPLISHED EO-92323-REQ1 FOR MISSING HARDWARE
- [SDR IPXA2024112135030](https://openairdocs.org/sdr/IPXA2024112135030), Nov 17, 2024: FLOOR PANEL. DAMAGED. MCD 15L INBOARD FLOOR PANEL HAS DAMAGE AROUND EDGE. AND MULTIPLE SCREW HOLES DAMEGED. ROUTED TO SHEET METAL FOR REPAIR. INSTALLED FLOOR PANEL IN POSITION 15L RE
- [SDR IPXA2024110653108](https://openairdocs.org/sdr/IPXA2024110653108), Oct 30, 2024: FLOOR PANEL. DAMAGED. **SUPPLEMENTAL SDR** MAIN CARGO DECK, FLOOR PANEL P/N 65B23347-52,(POSITION 12R, STA. 1225-1265 R/H CENTER PANELS), HAS 3/4 INCH HOLE. MARKED. LABOR ROW ENTERED
- [SDR IPXA2024110453108](https://openairdocs.org/sdr/IPXA2024110453108), Oct 30, 2024: FLOOR PANEL. DAMAGED. MAIN CARGO DECK, FLOOR PANEL P/N 65B23347-52,(POSITION 12R, STA. 1225-1265 R/H CENTER PANELS), HAS 3/4 INCH HOLE. MARKED. LABOR ROW ENTERED IN ERROR
- [SDR IPXA2024103187749](https://openairdocs.org/sdr/IPXA2024103187749), Oct 27, 2024: FLOOR PANEL. BROKEN. PANEL 65B23347-50 AT POS 12R CORNER BROKEN AND DELAM ON END OF PANEL *MARKED INSTALLED MCD FLOOR PANEL 65B23347-50 AT POSITION 12R REF AMM 53-21-02.
- [SDR IPXA2024103184870](https://openairdocs.org/sdr/IPXA2024103184870), Oct 27, 2024: FLOOR PANEL. DAMAGED. MCD CENTER FLOOR PANEL P/N: 144U5876-6 @ 14R & 15R BROKEN. MARKED WITH ORANGE TAPE. REF IPC 53-21-02-12F ITEM 475. INSTALLED MCD CENTER FLOOR PANEL P/N: 144U587
- [SDR IPXA2024103187769](https://openairdocs.org/sdr/IPXA2024103187769), Oct 27, 2024: FLOOR PANEL. DAMAGED. PANEL 65B15769-10 AT POS 12R DAMAGED (CRUSH DAMAGE AT SCREW HOLE) *MARKED. C/W SREO-42648-REQ1.
- [SDR IPXA2024103187705](https://openairdocs.org/sdr/IPXA2024103187705), Oct 27, 2024: FLOOR PANEL. DAMAGED. PANEL 65B23345-28 AT POS 17R DAMAGED INSTALLED MCD FLOOR PANEL 65B23345-28 AT POSITION 17R REF AMM 53-21-02.
- [SDR IPXA2024103187720](https://openairdocs.org/sdr/IPXA2024103187720), Oct 27, 2024: FLOOR PANEL. CRUSHED. PANEL 65B23341-32 AT POS 15R CRUSHED AND MISSING FILLER AT 5 EDGE LOCATIONS *MARKED. C/W SREO-42648-REQ1.
- [SDR IPXA2024092436192](https://openairdocs.org/sdr/IPXA2024092436192), Sep 17, 2024: DOOR. INOPERATIVE. L1 DOOR WILL NOT LATCH CLOSED FROM OUTSIDE. DOOR OPERATION NORMAL FROM INSIDE HANDLE OPENED AND CLOSED THE L1 ENTRY DOOR SEVERAL TIMES FROM THE OUTSIDE AS PER A
- [SDR IPXA2024091736192](https://openairdocs.org/sdr/IPXA2024091736192), Sep 17, 2024: LATCH. FAILED. L1 DOOR WILL NOT LATCH CLOSED FROM OUTSIDE. DOOR OPERATION NORMAL FROM INSIDE HANDLE DEFERRED L1 DOOR IAW MEL 52-11-1-1, PLACARDS ADHERED.
- [SDR IPXA2024051099060](https://openairdocs.org/sdr/IPXA2024051099060), May 10, 2024: MOTOR. FAILED. **ATB** THE FOLLOWING ECAS MSG POPULATED CLIMBING OUT OF SDF CABIN ALT AUTO FOUND FAULT CODE 21227 IN TELEMETRY. LEFT OUT FLOW VALVE A/C MOTOR FAIL.<BR>REMOVED 
- [SDR IPXA2024100743228](https://openairdocs.org/sdr/IPXA2024100743228), Apr 11, 2024: FLOOR PANEL. DAMAGED. MAIN CARGO FLOOR PANEL STA. 1150 DAMAGED P/N 65B15769-5 INSTALLED FLOOR PNL IAW AMM 53-21-02-404-006. INSTALLED ROLLER TRAYS IAW AMM 25-57-04 AND INSTALLED TRAY
- [SDR IPXA2024041274677](https://openairdocs.org/sdr/IPXA2024041274677), Apr 6, 2024: LIGHT. INOPERATIVE. EMERGENCY EXIT LIGHT AFT OF L1 DOOR DOES NOT ILLUMINATE RELAMPED OPERATIONAL CHECKED NORMAL IAW AMM 33-51-00.
- [SDR IPXA2024040874677](https://openairdocs.org/sdr/IPXA2024040874677), Apr 6, 2024: LIGHT. INOPERATIVE. **SDR FILED OPEN**EMERGENCY EXIT LIGHT AFT OF L1 DOOR DOES NOT ILLUMINATE
- [SDR IPXA2023090885145](https://openairdocs.org/sdr/IPXA2023090885145), Sep 8, 2023: DOOR. LEAKING. FLIGHT OVERHEAD DOOR INSP PFMD IAW 52-21-00-206-001. ISSUE DATE 15 NOV 2015. NIL FINDINGS. NIL WATER TRACES OBSERVED.
- [SDR IPXA2023052132850](https://openairdocs.org/sdr/IPXA2023052132850), May 13, 2023: LIGHT. INOPERATIVE. **SUPPLEMENTAL SDR**FAULT - FOUND UPPER DECK EMERGENCY LIGHTS NOT ILLUMINATE AT L1382,L5731,L5734 (REPLACE) ALL PAPERWORK C/W IAW AMM 33-51-72
- [SDR IPXA2023051532850](https://openairdocs.org/sdr/IPXA2023051532850), May 13, 2023: UNKNOWN. UNKNOWN. **SDR FILED OPEN**FAULT - FOUND UPPER DECK EMERGENCY LIGHTS NOT ILLUMINATE AT L1382,L5731,L5734 (REPLACE) OK TO WORK
- [SDR IPXA2023051875529](https://openairdocs.org/sdr/IPXA2023051875529), Apr 23, 2023: ANGLE. UNKNOWN. FAULT - DEVIATION, DURING PERFORM EO-26835-JIC004 SB747-53A2562 (REPAIR) ALL PAPERWORK C/W
- [SDR IPXA2023051358369](https://openairdocs.org/sdr/IPXA2023051358369), Apr 21, 2023: ANGLE. CRACKED. DURING PERFORM NOSE WHEEL WELL MODIFICATION FOUND ANGLE CRACK AT STA 260 - 340 LBL 30. ACCOMPLISHED UPS EO-87000-REQ1.
- [SDR IPXA2023051833582](https://openairdocs.org/sdr/IPXA2023051833582), Apr 13, 2023: WEB. UNKNOWN. STA 1220 L/H OVERWING INTERCOSTALS EXIST REPAIR NEED UPGRADE BY SRM 53-40-51-2R REPAIR 5 (REPAIR) REPAIR INTERCOSTAL DAMAGE AREA I.A.W UPS EO-86941-REQ1 ALL PAP
- [SDR IPXA2023051833466](https://openairdocs.org/sdr/IPXA2023051833466), Apr 13, 2023: WEB. UNKNOWN. STA 1180 LH OVERWING INTERCOSTALS EXIST REPAIR NEED UPGRADE BY SRM 53-40-51-2R REPAIR 8 (REPAIR) ACCOMPLISHED UPS EO-86997-REQ1 ALL PAPERWORK C/W
- [SDR IPXA2023050633551](https://openairdocs.org/sdr/IPXA2023050633551), Apr 13, 2023: WEB. UNKNOWN. STA 1220 R/H OVERWING INTERCOSTALS FAST REPAIR NEED UPGRADE BY SRM 53-40-51-2R REPAIR 5 (REPAIR) ALL PAPERWORK C/W
- [SDR IPXA2023051832614](https://openairdocs.org/sdr/IPXA2023051832614), Apr 6, 2023: SEAT TRACK. CORRODED. A/C OOS* FAULT - MAIN DECK SEAT TRACK SKIN CORROSION, STA 1080 RBL 97. ACCOMPLISHED EO-87099-REQ1 ALL PAPERWORK C/W.
- [SDR IPXA2023051132657](https://openairdocs.org/sdr/IPXA2023051132657), Apr 6, 2023: CAP. CORRODED. CORROSION - UPPER CAP, MAIN DECK CARGO COMPARTMENT FLOOR AREA, STA 2374, RBL 15 (REPLACE) ALL PAPERWORK C/W
- [SDR IPXA2021112076177](https://openairdocs.org/sdr/IPXA2021112076177), Nov 20, 2021: NONE. DAMAGED. INSPECTION TYPE:N/AL1 DOOR SEAL IS DAMAGED.SECURED L1 DOOR SEAL & DOOR OPS CHECK OK AS PER AMM 52-11-00-601.
- [SDR IPXA2021111976134](https://openairdocs.org/sdr/IPXA2021111976134), Nov 18, 2021: NONE. INOPERATIVE. INSPECTION TYPE:PSMCABIN EMERGENCY LIGHT INOPEMERGENCY CEILING LIGHT LAMP REPLACEMENT PER AMM 33-51-07 OPS CK GD
- [SDR IPXA2021090873733](https://openairdocs.org/sdr/IPXA2021090873733), Sep 8, 2021: WARNING MESSAGE. FALSE ACTIVATION. INSPECTION TYPE:N/AEICAS MESSAGE DOES F/D OVHD RAN QRH PROCEDURE PRESSURIZATION NORMAL CONT'D FLIGHT.PERFORMED OPERATIONAL CHECK OF F/D OVHD DOOR IAW AMM 52 21 
- [SDR IPXA2021082773212](https://openairdocs.org/sdr/IPXA2021082773212), Aug 26, 2021: WARNING MESSAGE. FALSE ACTIVATION. DOOR F/D OVHD EICAS MESSAGE ON CLIMBOUT. PRESSURIZATION NORMAL.FOUND F/D OVHD HATCH DOOR HANDLE NOT ON LOCKED POSITION IAW AMM 52-21-00 PB 001 REV 102.00. HANDL
- [SDR IPXA2021052769902](https://openairdocs.org/sdr/IPXA2021052769902), May 25, 2021: DOOR. UNSECURE. INSPECTION TYPE:N/A** ATB **LANDED WITHOUT INCIDENT** DOOR F/D OVHD AFTER T/OFF CABIN PRESSURE RISING! PERFORMED FIM 52-71-00-812-828. FOUND F/D OVERHEAD DOOR S
- [SDR IPXA2021042068426](https://openairdocs.org/sdr/IPXA2021042068426), Apr 13, 2021: SKIN. DAMAGED. INSPECTION TYPE:C3DENT DAMAGE WAS FOUND ON OUTER SKIN (P/N: 65B08540-511) OF UPPER PANEL OF L/H WING OUTBD MID FLAP AT WBL 521.REPAIR I.A.W. B747-400F SRM 57-53
- [SDR IPXA2021042668605](https://openairdocs.org/sdr/IPXA2021042668605), Apr 8, 2021: STRUCTURE. CORRODED. INSPECTION TYPE:C3CORROSION WAS BLENDED OUT ON RH WING TRAILING EDGE UPPER CHORD (P/N:65B11614-24) NEAR WBL 235.2.REPAIR I.A.W. BOEING SR:4-5032548637 AND UPS E
- [SDR IPXA2021042068425](https://openairdocs.org/sdr/IPXA2021042068425), Apr 8, 2021: SKIN. PUNCTURED. INSPECTION TYPE:C3PUNCTURE DAMAGE WAS FOUND ON INNER SKIN (P/N: 65B08426-22) OF LOWER PANEL OF R/H WING INBD MID FLAP AT WBL 235.REPAIR I.A.W. B747-400F SRM 57-
- [SDR IPXA2021042068424](https://openairdocs.org/sdr/IPXA2021042068424), Apr 8, 2021: SKIN. DAMAGED. INSPECTION TYPE:C32EA PUNCTURE DAMAGES WERE FOUND ON INNER SKIN (P/N: 65B08427-19) OF LOWER PANEL OF R/H WING INBD MID FLAP AT WBL 353.REPAIR I.A.W. B747-400F S
- [SDR IPXA2021022766156](https://openairdocs.org/sdr/IPXA2021022766156), Feb 27, 2021: SKIN. DAMAGED. INSPECTION TYPE:N/ART FUSELAGE SKIN REPAIR AT STA 2598 & BELOW STR 26RREPAIRED IAW UPS E.O. B747-5330-79437-A, ITEM IS TIME LIMITED PER THE E.O. AND WILL BE DEF
- [SDR IPXA2020011500935](https://openairdocs.org/sdr/IPXA2020011500935), Jan 13, 2020: LINE. RUPTURED. RUPTURE IN SINK WATER SUPPLY LINE, DURING CRUISE WATER TANK EMPTIED ONTO FLOOR. DIVERTED IAW AMC REQUEST. R & R THE LAV BASIN FAUCET ASSY. OP & LEAK CHECKED GOO
- [SDR IPXA2019102048072](https://openairdocs.org/sdr/IPXA2019102048072), Oct 20, 2019: SPAR. CORRODED. RIGHT WING AUX SPAR UPPER T-CHORD WBL 235.2 CORRODED AT INBOARD END. ACCOMPLISHED INSPECTION/REPAIR, IAW EO B747-5710-74368-A.
- [SDR IPXA2019102308072](https://openairdocs.org/sdr/IPXA2019102308072), Oct 20, 2019: TEE FITTING. CORRODED. INSPECTION TYPE:N/A**SDR FILED OPEN** RIGHT WING AUX SPAR UPPER T-CHORD WBL 235.2 CORRODED AT INBD END. REPAIRED IAW EO B747-5710-74368-A. DEFERRED DUE TO PERMA
- [SDR IPXA2019060322723](https://openairdocs.org/sdr/IPXA2019060322723), May 24, 2019: TENSION TIE. CRACKED. INSPECTION TYPE:C1 CRACK WAS FOUND ON TENSION TIE (P/N: 142U1023-104) AT RBL 90, STA 740.REPAIR I.A.W. 747-400F SRM 53-20-30 REPAIR 2 REV. 85.00.
- [SDR IPXA2019030639786](https://openairdocs.org/sdr/IPXA2019030639786), Mar 6, 2019: WARNING SYSTEM. FALSE ACTIVATION. INSPECTION TYPE:NA DOOR F/O OVHD EICAS MESSAGE. OPERATIONAL TEST OF THE DOOR WARNING SYSTEM ON THE OVERHEAD HATCH PERFORMED IAW AMM TASK 52-71-00-705-070 REV 94

All 230: https://openairdocs.org/aircraft/N582UP/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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