# N578UP: 1993 Boeing 747-45E

- Status: Valid registration
- Airframe: [Boeing 747-45E](https://openairdocs.org/model/boeing-747-45e) (registry code 1384947, 495 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: 27154
- Year built: 1993
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: July 16, 2008
- Certificate issued: January 30, 2008
- Expires: May 31, 2029
- Mode S code: A76DF1
- 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=578UP
- Page: https://openairdocs.org/aircraft/N578UP

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 747-45E)

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 (1)

From the NTSB's public API. Aircraft are matched to registry aircraft by N-number and event date, checked against the reported serial number, make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model.

- [NTSB DCA19WA071](https://openairdocs.org/ntsb/DCA19WA071), Oct 16, 2018: Boeing 747 (N578UP), Kolkata, India, incident, no damage

## FAA accident and incident reports

None matched to N578UP.

## Service difficulty reports (288, 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 IPXA2026100851661](https://openairdocs.org/sdr/IPXA2026100851661), Oct 8, 2026: STRAP. BROKEN. MAJOR REPAIR, TRIM BACKING BROKEN STATION 7120. REPAIRED IAW EO-98860-REQ1
- [SDR IPXA2026101229819](https://openairdocs.org/sdr/IPXA2026101229819), Oct 1, 2026: WARNING MESSAGE. ILLUMINATED. L1 DOOR NOT SHOWING CLOSED AND LATCHED ON EXTERIOR DOOR SYNOPTIC WHEN L1 DOOR CLOSED FOUND L-1 DOOR CLOSE SWITCH NG.REPLACED L-1 DDOR CLOSE SWITCH PER AMM 52-71
- [SDR IPXA2026100129819](https://openairdocs.org/sdr/IPXA2026100129819), Oct 1, 2026: WARNING MESSAGE. INDICATION. L1 DOOR NOT SHOWING CLOSED AND LATCHED ON EXTERIOR DOOR SYNOPTIC WHEN L1 DOOR CLOSED DEFER PER MEL 52-73-1-0-1.
- [SDR IPXA2026090480472](https://openairdocs.org/sdr/IPXA2026090480472), Sep 4, 2026: LATCH. BROKEN. PED- LITHIUM FIRE CONTAINMENT CASE IS BROKEN SECURING LATCH PERFORMED SREO-90628-REQ2, PED FIRE CONTAINMENT CASE TAMPER SEAL DAMAGED, MISSING OR DAMAGED FILTER 
- [SDR IPXA2026082480215](https://openairdocs.org/sdr/IPXA2026082480215), Aug 23, 2026: FIRE WARNING. FALSE ACTIVATION. FIRE CARGO FWD EICAS MSG ON SHORT FINAL EXTINGUISH AFTER APPROX 15 SECONDS NO STATUS MSG ,CMC MSG SHOWS CARGO FWD. -4 LOOP -B FAIL ,FIM 26-16 TASK 891 FOLLOWED.
- [SDR IPXA2026022552524](https://openairdocs.org/sdr/IPXA2026022552524), Feb 23, 2026: POWER SUPPLY. INOPERATIVE. FOUND M5055 POWER SUPPLY MALFUNCTION. (REPLACE) IAW AMM 33-51-04-902-001-001 REV.115 REPLACED POWER SUPPLY (M5055) AT UPPER DECK LEFT SIDE AND PERFORMED POWER S
- [SDR IPXA2026022323848](https://openairdocs.org/sdr/IPXA2026022323848), Feb 4, 2026: SEAT TRACK. BROKEN. FOUND MAIN DECK FLOOR STRUCTURE BROKEN AT STA 2054 RBL 75 (REPAIR). CUT AND REMOVE THE DAMAGED SEAT TRACK. MAKE THE EDGES OF THE CUT SMOOTH TO 125 MICROINCHES R
- [SDR IPXA2026021021755](https://openairdocs.org/sdr/IPXA2026021021755), Jan 29, 2026: SKIN. CRACKED. MAJOR REPAIR. FUSELAGE SKIN CRACK AT BS 560 S-23L - S-24L. (REPAIR) . ACCOMPLISH THE REPAIR I.A.W SRM 53-00-01-2R-13 REV.64 AND EGAT WORK SHEET NO.60081 REVIEWE
- [SDR IPXA2026022021669](https://openairdocs.org/sdr/IPXA2026022021669), Jan 29, 2026: BRACKET. GOUGED. GOUGED BRACKET, BULK CGO APU PNEUMATIC DUCT SUPPORT UPPER BEAM LOWER SIDE AT STA 2280. REMOVED DAMAGE BRACKET IAW SRM 51-40-02-0G REV.64 2. INSTALLED NEW BRACKE
- [SDR IPXA2026013021723](https://openairdocs.org/sdr/IPXA2026013021723), Jan 29, 2026: FLOOR PANEL. DAMAGED. MAJOR REPAIR - FOUND MAIN DECK FLOOR PANEL DAMAGE AT STA 1460 RBL 15 P/N:144U5880-26 (REPAIR) REMOVE THE DAMAGED PANEL IN ACCORDANCE WITH AMM 53 21 02. I.A.W. S
- [SDR IPXA2026013021744](https://openairdocs.org/sdr/IPXA2026013021744), Jan 29, 2026: FLOOR PANEL. DELAMINATED. MAJOR REPAIR. FOUND MAIN DECK FLOOR PANEL DELAMINATED AT STA 1000 RBL 20 P/N:144U5882-14 (REPAIR) REVIEWED TASK PER GMM-MTX 09.05.01.09.
- [SDR IPXA2026020600994](https://openairdocs.org/sdr/IPXA2026020600994), Jan 28, 2026: ANGLE. CORRODED. FAULT- CRACK- BRACKET, FWD LOWER WING TO BODY INTERNAL ATTACH BRACKET OF THE CORROSION AT STA 986 LBL 4. (REPLACE) 1. REMOVE DAMAGE BRACKET I.A.W SRM 51-40-02-0
- [SDR IPXA2026020630367](https://openairdocs.org/sdr/IPXA2026020630367), Jan 16, 2026: CARGO TRACK. CRACKED. MAJOR REPAIR FWD CARGO COMPARTMENT SEAT TRACK CRACK AT STA 968 RBL45. (REPAIR) 1. ACCOMPLISH THE REPAIR I.A.W SRM 53-00-52-2R-10 REV. 64 AND EGAT WORK SHEET NO:
- [SDR IPXA2026022330508](https://openairdocs.org/sdr/IPXA2026022330508), Jan 16, 2026: SUPPORT FITTING. CRACKED. ***MAJOR REPAIR*** FAULT - FOUND #6 SPOILER ACTUATOR SUPPORT FITTING L/H LOWER CRACK. (REPAIR) CUT OUT THE DAMAGED AREA AS SHOWN IN FIGURE 202 INSTALL THE REPAI
- [SDR IPXA2025121778168](https://openairdocs.org/sdr/IPXA2025121778168), Dec 16, 2025: SLIDE. UNWANTED DEPLOY. RIGHT UPPER DECK ESCAPE DOOR/SLIDE DEPLOYED. REINSTALLED NEW RH UPPER DECK ESCAPE SLIDE IAW AMM 25-68-01 UP TO AND INCLUDING STEP G. 9. VERIFIED SAFETY PINS REM
- [SDR IPXA2025071825183](https://openairdocs.org/sdr/IPXA2025071825183), Jul 14, 2025: AILERON SYS. NO DISCREPANCY. DURING CLIMB OUT AILERON FORCE WERE A LITTLE HEAVIER THAN NORMAL AND RIGHT AILERON REQUIRED SIGNIFICANTLY MORE FORCE THEN LEFT AILERON. PERFORM ROTATIONAL TORQU
- [SDR IPXA2025040311394](https://openairdocs.org/sdr/IPXA2025040311394), Apr 3, 2025: SIGN. INOPERATIVE. FAULT - FOUND THE UPPER DECK EMERGENCY EXIT SIGN LIGHT INOP AT STA 620 AND STA 690 (REPLACE). I.A.W AMM 33-51-00-715-105 REV.113 CONTINUE TO SUPPLY POWER TO THE
- [SDR IPXA2024122013341](https://openairdocs.org/sdr/IPXA2024122013341), Dec 20, 2024: CIRCUIT CARD. FAULTED. DURING PRE-DEPARTURE CHECK FOUND CARGO FIRE MD ZONE 6 LOOP-A FAIL NO CURENT FAULT FOUND. C/O FIRE TEST IAW AMM 26-11-00-715-001 REV 112. CHECKED SATIS. THIS CLO
- [SDR IPXA2024082676285](https://openairdocs.org/sdr/IPXA2024082676285), Aug 21, 2024: STRUCTURE. BROKEN. LOAD CREW FOUND CENTERLINE GUIDE AND AIRCRAFT STRUCTURE BROKEN AT STATION 1820-1840 (POSITION 9 AFT LOWER PIT) INSTALLED 2(EA) BALL MAT PANELS IN LWR AFT PIT AT
- [SDR IPXA2024082176285](https://openairdocs.org/sdr/IPXA2024082176285), Aug 21, 2024: STRUCTURE. BROKEN. LOAD CREW FOUND CENTERLINE GUIDE AND AIRCRAFT STRUCTURE BROKEN AT STATION 1820-1840 (POSITION 9 AFT LOWER PIT) OPEN
- [SDR IPXA2024080588574](https://openairdocs.org/sdr/IPXA2024080588574), Aug 4, 2024: WINDOW. DELAMINATED. CAPT€™S #1 (FRONT) WINDSHIELD DELAMINATING ON TOP SECTION OF WINDOW COMPLETED WINDOW INSLALL WITH REF TO B747 MM 56-11-01. PERFORMED WIPER OPS CHECK WITH REF T
- [SDR IPXA2024071862660](https://openairdocs.org/sdr/IPXA2024071862660), Jul 17, 2024: HMU. INOPERATIVE. ON DECENT GOT #3 GEN ELECT FAIL. THEN ENG 3 FAILED APPEARED. N1 WAS AROUND 28%. ENGINE RETURNED TO NORMAL IDLE. ENG FAIL MESSAGE LASTED ABOUT 20 SECONDS NO OTHE
- [SDR IPXA2024062744323](https://openairdocs.org/sdr/IPXA2024062744323), Jun 27, 2024: LIGHT. FAULTED. EMER LIGHTS EICAS. RESET EMERGENCY LIGHT SWITCH. PERFORMED OPS CHECK OF THE EMERGENCY LIGHTS IAW AMM 33-51-00-715-001. OPS CHECK GOOD.
- [SDR IPXA2024021728160](https://openairdocs.org/sdr/IPXA2024021728160), Feb 12, 2024: BATTERY. INOPERATIVE. FOUND THE UPPER DECK DOOR RIGHT SIDE EXIT EMERGENCY LIGHT INOP (REPLACE) C/W I.A.W AMM 33-51-04-902-001-001 REV.109 REPLACED THE EMERGENCY LIGHT BATTERY (M5056)
- [SDR IPXA2024021228160](https://openairdocs.org/sdr/IPXA2024021228160), Feb 12, 2024: LIGHT. INOPERATIVE. SDR FILED OPEN. FOUND THE UPPER DECK DOOR RIGHT SIDE EXIT EMERGENCY LIGHT INOP (REPLACE)
- [SDR IPXA2024013125856](https://openairdocs.org/sdr/IPXA2024013125856), Jan 31, 2024: SNUBBER. OUT OF LIMITS. FOUND L4 ENTRY DOOR SNUBBER INDICATOR OUT OF LIMIT. (REPLACE) C/W 1. I.A.W AMM 52-11-10-004-001 REV. 109 AND AMM 52-11-10-404-005 REV. 109 REPLACE SNUBBER. 2. I
- [SDR IPXA2024021230568](https://openairdocs.org/sdr/IPXA2024021230568), Jan 19, 2024: TENSION TIE. CRACKED. *MAJOR REPAIR* FAULT - CRACK - FND TENSION TIE CHANNEL FWD SIDE CRACK AT STA 1120 L/H (REPAIR) ACCOMPLISH REINFORCING REPAIR I/A/W B747-400SF (REV. 58) SRM 53-4
- [SDR IPXA2024021610259](https://openairdocs.org/sdr/IPXA2024021610259), Jan 18, 2024: SKIN. DENTED. DENT - SKIN SURFACE AT 7 O'CLOCK, NO.1 ENG LH FAN COWL EXTERNAL AREAS (REPAIR) 1.REMOVE THE DAMAGE MATERIALS AND CLEAN.MEASURE THE DAMAGE AREA (DIAMETER:1",DEPT
- [SDR IPXA2024021610224](https://openairdocs.org/sdr/IPXA2024021610224), Jan 18, 2024: SKIN. DENTED. DENT - SKIN SURFACE AT 10 O'CLOCK, NR 1 ENG LH FAN COWL EXTERNAL AREAS (REPAIR) REMOVE THE DAMAGE MATERIALS AND CLEAN.MEASURE THE DAMAGE AREA (LENGTH:0.8",WIDTH
- [SDR IPXA2024011810224](https://openairdocs.org/sdr/IPXA2024011810224), Jan 18, 2024: SKIN. DENTED. *** SDR FILED OPEN *** FAULT - DENT - SKIN SURFACE AT 10 O'CLOCK, NO.1 ENG LH FAN COWL EXTERNAL AREAS (REPAIR) OK TO WORK
- [SDR IPXA2024011810259](https://openairdocs.org/sdr/IPXA2024011810259), Jan 18, 2024: SKIN. DENTED. *** SDR FILED OPEN *** FAULT - DENT - SKIN SURFACE AT 7 O'CLOCK, NO.1 ENG LH FAN COWL EXTERNAL AREAS (REPAIR) OK TO WORK
- [SDR IPXA2024022347664](https://openairdocs.org/sdr/IPXA2024022347664), Jan 16, 2024: SKIN. CRACKED. CRACKED SKIN, LH WING NO.1E VC FLAP PANEL OUTER SURFACE (REPAIR) INSTALLED NEW PART I.A.W. SRM 51-40-02-0G REV.58 AND BOEING DWG NO:65B15168 SH.2 REV.G AND AIPC
- [SDR IPXA2024022347710](https://openairdocs.org/sdr/IPXA2024022347710), Jan 16, 2024: SKIN. BROKEN. BROKEN SKIN, LH WING LE LWR SURFACE PANEL (REPAIR) C/W 1. OK TO INSTALL PANEL NO: 521EB. 2. I.A.W AMM 20-51-01-912-008 REV.109 INSTALL PANEL NO: 521EB. 3. CONDI
- [SDR IPXA2024021647771](https://openairdocs.org/sdr/IPXA2024021647771), Jan 16, 2024: PANEL. DEBONDED. LEFT WING INBOARD LEADING EDGE UPPER FIXED PANEL DISBOND, 46" FROM LEADING, EDGE, 157" FROM INBOARD EDGE (REPAIR) 1.I.A.W AMM 51-24-11-477-083 REV.109,CLEANING 
- [SDR IPXA2024021645990](https://openairdocs.org/sdr/IPXA2024021645990), Jan 16, 2024: FAIRING. DAMAGED. NR 8 MOVABLE FAIRING OUTBD SIDE AND AFT SIDE SURFACE DAMAGE (REPAIR) REMOVE THE DAMAGE MATERIALS AND CLEAN.MEASURE THE DAMAGE AREA (LENGTH:0.8",WIDTH:0.5",AT UP
- [SDR IPXA2024021645522](https://openairdocs.org/sdr/IPXA2024021645522), Jan 16, 2024: STIFFENER. CRACKED. *** SUPPLEMENTAL SDR *** FAULT - RIGHT INBOARD ELEVATOR, INBOARD, LEADING EDGE RIB ANDSTIFFENER CRACK (REPLACE) I.A.W AMM 27-31-01-404-015 REV.109 STEP 3.H(14) 
- [SDR IPXA2024011747664](https://openairdocs.org/sdr/IPXA2024011747664), Jan 16, 2024: SKIN. CRACKED. *** SDR FILED OPEN *** FAULT - CRACK - SKIN, LH WING NO.1E VC FLAP PANEL OUTER SURFACE (REPAIR) I.A.W AMM 27-81-02-004-001 REV 109 REMOVE #1E V.C FLAP
- [SDR IPXA2024011745990](https://openairdocs.org/sdr/IPXA2024011745990), Jan 16, 2024: FAIRING. UNKNOWN. *** SDR FILED OPEN *** FAULT - NO.8 MOVABLE FAIRING OUTBD SIDE AND AFT SIDE SURFACE DAMAGE (REPAIR) OK TO WORK
- [SDR IPXA2024011745522](https://openairdocs.org/sdr/IPXA2024011745522), Jan 16, 2024: STIFFENER. CRACKED. *** SDR FILED OPEN *** FAULT - RIGHT INBOARD ELEVATOR, INBOARD, LEADING EDGE RIB ANDSTIFFENER CRACK (REPLACE) I.A.W. AMM 27-31-01-004-001 REV.109 REMOVED R/H IN
- [SDR IPXA2024011747771](https://openairdocs.org/sdr/IPXA2024011747771), Jan 16, 2024: SKIN. DEBONDED. *** SDR FILED OPEN *** FAULT - LEFT WING INBOARD LEADING EDGE UPPER FIXED PANEL DISBOND, 46" FROM LEADING, EDGE, 157" FROM INBOARD EDGE (REPAIR) OK TO WORK
- [SDR IPXA2024011747710](https://openairdocs.org/sdr/IPXA2024011747710), Jan 16, 2024: SKIN. DAMAGED. *** SDR FILED OPEN *** FAULT - BROKEN - SKIN, LH WING LE LWR SURFACE PANEL (REPAIR) OK TO WORK
- [SDR IPXA2024010359777](https://openairdocs.org/sdr/IPXA2024010359777), Dec 27, 2023: DOOR. BINDING. *** SUPPLEMENTAL SDR *** MAIN ENTRY DOOR DIFFICULT TO OPEN AND CLOSE REPLACED ROD END ASSY. ON LOWER HINGE GUIDE ARM REF AMM 52-11-01-401. OPS NORMAL AT THIS TI
- [SDR IPXA2023122759777](https://openairdocs.org/sdr/IPXA2023122759777), Dec 27, 2023: UNKNOWN. UNKNOWN. MAIN ENTRY DOOR DIFFICULT TO OPEN AND CLOSE, OPEN
- [SDR IPXA2023110891070](https://openairdocs.org/sdr/IPXA2023110891070), Sep 27, 2023: TRUNNION. CRACKED. RIGHT AFT TRUNNION, CRACKS
- [SDR IPXA202309281070](https://openairdocs.org/sdr/IPXA202309281070), Sep 27, 2023: UNKNOWN. UNKNOWN. OPEN, RIGHT AFT TRUNNION, CRACKS
- [SDR IPXA2023092551464](https://openairdocs.org/sdr/IPXA2023092551464), Jul 25, 2023: CARGO TRACK. DAMAGED. *** MAJOR REPAIR *** DURING CARGO LOADING OPERATIONS, FOUND FWD LWR CARGO DOUBLE PALLET LOCK ASSY. SECURING RAIL BROKEN, WL-118 ST-560, RH FWD BALL-MAT.***SM26/
- [SDR IPXA2023052052755](https://openairdocs.org/sdr/IPXA2023052052755), May 16, 2023: LAMP. INOPERATIVE. *** SUPPLEMENTAL SDR *** FAULT - THE EMERGENCY SLIDE LIGHT (L2930) INOP AT RIGHT UPPER DECK DOOR. (REPLACE) ALL PAPERWORK C/W
- [SDR IPXA52755](https://openairdocs.org/sdr/IPXA52755), May 16, 2023: UNKNOWN. UNKNOWN. THE EMERGENCY SLIDE LIGHT (L2930) INOP AT RIGHT UPPER DECK DOOR. (REPLACE) OK TO WORK. OPEN
- [SDR IPXA2024021763758](https://openairdocs.org/sdr/IPXA2024021763758), Feb 3, 2023: SKIN. CORRODED. *MAJOR REPAIR* FASTENERS PULLED THROUGH SKIN, LH WING***SM40/LMX6***HGR*** 1.REPAIR PER UPS EO-89517-REQ1 REV.1. 2.JOB COMPLETED. REVIEWED
- [SDR 2022FA0000519](https://openairdocs.org/sdr/2022FA0000519), Sep 12, 2022: ACCESS PANEL. MISSING. OUTBD PYLON NO.4 FOUND PANEL 484DR MISSING

All 288: https://openairdocs.org/aircraft/N578UP/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 747-45E aircraft: https://openairdocs.org/model/boeing-747-45e/aircraft.md
- The GE CF6-80C2B1F engine: https://openairdocs.org/engine/ge-cf6-80c2b1f.md

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