# N573UP: 2008 Boeing 747-44AF

- Status: Valid registration
- Airframe: [Boeing 747-44AF](https://openairdocs.org/model/boeing-747-44af) (registry code 13848B2, 2 seats)
- Engine: [GE CF6-80C2B1F1](https://openairdocs.org/engine/ge-cf6-80c2b1f1) (registry code 30111)
- Data sheets: [TCDS E13NE](https://openairdocs.org/tcds/E13NE) (General Electric Company GE Aerospace) (OpenAirDocs)
- Serial number: 35662
- Year built: 2008
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: March 21, 2008
- Certificate issued: March 24, 2008
- Expires: November 30, 2029
- Mode S code: A75B5E
- 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=573UP
- Page: https://openairdocs.org/aircraft/N573UP

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): 24 in force

### Matched by airframe (Boeing 747-44AF)

None in force.

### Matched by engine (GE CF6-80C2B1F1)

- [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 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 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 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 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 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 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 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 DCA23WA064](https://openairdocs.org/ntsb/DCA23WA064), Nov 11, 2022: Boeing 747-44AF (N573UP), Almaty, Kazakhstan, occurrence

## FAA accident and incident reports

None matched to N573UP.

## Service difficulty reports (117, 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 IPXA2026102389310](https://openairdocs.org/sdr/IPXA2026102389310), Oct 23, 2026: LIFE VEST. TORN. SUPERNUMERARY LIFE VEST EXP TAG TORN. REMOVED AND REPLACED LT OTBD LIFE VEST IAW AMM 25-62-05
- [SDR IPXA2026101188731](https://openairdocs.org/sdr/IPXA2026101188731), Oct 10, 2026: BATTERY PACK. INOPERATIVE. FOUND UPPER DECK EMERGENCY LIGHT M4915, L1533, L5733,5767 INOPERATIVE. IAW AMM 33-51-04-002-009-001, 33-51-04-402-012-001, AND 33-51-04-902-001-001 REV.117 AND 
- [SDR IPXA2026093003820](https://openairdocs.org/sdr/IPXA2026093003820), Sep 30, 2026: HANDLE. BINDING. L1 DOOR IS DIFFICULT TO OPEN & CLOSE HANDLE SWINGS VIOLENTLY COULD CAUSE INSURY. LUB THE L1 DOOR HANDLE AS PER B747 AMM 12-21-04 P.301 AND PERFORMED L1 DOOR OPS
- [SDR IPXA2026081096634](https://openairdocs.org/sdr/IPXA2026081096634), Aug 9, 2026: LIGHT. INOPERATIVE. DOOR 1L, EMERGENCY EXIT SIGN LIGHT INOPERATIVE. C/W AMM33-51-05-962-031, REV. 137, OPC O.K.
- [SDR IPXA2026032784468](https://openairdocs.org/sdr/IPXA2026032784468), Mar 26, 2026: BALLAST. INOPERATIVE. ALL LIGHTS IN THE LAVATORY FOUND TO BE INOPERATIVE, NOT JUST THE CEILING LIGHT. BALLAST CONNECTION RESET AND LAMPS RESET C/OUT, FOUND OPS NORMAL.
- [SDR IPXA2025111479619](https://openairdocs.org/sdr/IPXA2025111479619), Nov 14, 2025: SPOILER SYS. INOPERATIVE. **ATB** HYD QUAN 2 LOW - EICAS. R&R SPOILER CONTROL PACKAGE ASSEMBLY PER AMM 27-61-05-402-012. LEAK AND OPS CHECK OK. NO FAULTS NOTED AT THIS TIME.
- [SDR IPXA2025100885263](https://openairdocs.org/sdr/IPXA2025100885263), Oct 4, 2025: FLOOR PANEL. CRACKED. CRACK- FLOOR PANEL, MAIN DECK COMPARTMENT FLOOR PNL (P/N: 144U5803-98). MAIN DECK COMPARTMENT FLOOR PNL (P/N: 144U5803-98).I.A.W AMM 25-59-01-004-175 REV.114 RE
- [SDR IPXA2025100965035](https://openairdocs.org/sdr/IPXA2025100965035), Oct 3, 2025: SKIN. GOUGED. GOUGE - SKIN, RT WING OUTBOARD AFT FLAP AT WS900 - WS920. REPAIRED GOUGE DAMAGE RT WING OUTBD T/E FLAP AFT FLAP UPPER PANEL BETWEEN WBL 747.7 AND WBL 822.0 IAW 
- [SDR IPXA2025101564861](https://openairdocs.org/sdr/IPXA2025101564861), Oct 3, 2025: SKIN. GOUGED. GOUGE - SKIN - RT WING OUTBOARD FLAP AFT FLAP AT WS 880 - 890. REFER TO 747 NDT MANUAL, PART 6,51-00-00, FIGURE 1,11OR 16 FOR HFEC PROCEDURE. IAW EGAT EI F 2025
- [SDR IPXA2025101564889](https://openairdocs.org/sdr/IPXA2025101564889), Oct 3, 2025: SKIN. GOUGED. GOUGE - SKIN - RT WING OUTBOARD FLAP AFT FLAP AT STA WS 862-870. RT WING OUTBD AFT FLAP T. REFER TO 747 NDT MANUAL, PART 6,51-00-00, FIGURE 1,11OR 16 FOR HFEC P
- [SDR IPXA2025101443697](https://openairdocs.org/sdr/IPXA2025101443697), Oct 2, 2025: CHANNEL. CRACKED. MAJOR REPAIR, DURING PERFORM EO-26856-JIC001 FOUND CHANNEL CRACK AT STA 740 L/H AFT SIDE. PERFORMED THE HEAT TREATMENT FROM 2024-O-071 CLAD TO T42 CONDITION I.A
- [SDR IPXA2025091257708](https://openairdocs.org/sdr/IPXA2025091257708), Sep 11, 2025: DOOR. OUT OF ADJUST. NO ENTRY DOOR INDICATION ADJUSTED THE DOOR PER AMM 52-11-01-735-080, IND BACK NML
- [SDR IPXA2025062519505](https://openairdocs.org/sdr/IPXA2025062519505), Jun 20, 2025: VHF COMM. INOPERATIVE. DURING CRUISE EICAS ALERT THEN STATUS MESSAGE EQUIPMENT SMOKE ALONG WITH VHF DATA OFF RESULTED IN ATB. REPLACED C VHF TRANSCEIVER PER AMM 23-12-01-404-027, GROU
- [SDR IPXA2025062019505](https://openairdocs.org/sdr/IPXA2025062019505), Jun 20, 2025: TRANSCEIVER. FAULTED. ATB, DURING CRUISE EICAS ALERT THEN STATUS MESSAGE EQUIPMENT SMOKE ALONG WITH VHF DATA OFF RESULTED IN ATB. REPLACED C VHF TRANSCEIVER PER AMM 23-12-01-404-027,
- [SDR IPXA2025012703089](https://openairdocs.org/sdr/IPXA2025012703089), Jan 27, 2025: BULB. INOPERATIVE. ENERG LIGHT BULB OUT AT L1 DOOR SILL AFT SIDE. R&R BULB LIGHT CK OK IAW AMM 33-51-00. CERTIFY
- [SDR IPXA2025012791068](https://openairdocs.org/sdr/IPXA2025012791068), Jan 26, 2025: WINDOW. ARCED. F/O (R2) WINDOW OUTER PANE CRACK. R & R R1 WINDOW PER AMM REF 56-11-01/401 AND IPC REF 56-11-11-02B #30. A/C OK FOR SERVICE.
- [SDR IPXA2024030725989](https://openairdocs.org/sdr/IPXA2024030725989), Mar 6, 2024: PANEL. DELAMINATED. *SDR FILED OPEN* FOUND DELAMINATION ON VERTICAL STABILIZER PANEL
- [SDR IPXA2023120633589](https://openairdocs.org/sdr/IPXA2023120633589), Dec 6, 2023: HMU. FAULTED. ENG 3 FUEL VLV EICAS WITH ASSOC ENG 3 FAIL/ ENG 3 AUTOSTART 2X, ENG 3 RE-LIT INFLT BOTH TIMES, DIVERT REPLACE ENG 3 HMU REF MTR ID T3F18E003FW0V AND PFM WINDMIL
- [SDR IPXA2023111858806](https://openairdocs.org/sdr/IPXA2023111858806), Nov 18, 2023: BATTERY. INOPERATIVE. DURING PS-1 CHECK FOUND SEVERAL EMERGENCY LIGHTS WITHOUT FUNCTION FOUND ALL FAULTY LIGHTS CONNECTED TO BATTERY PACK M5168. REPLACED AND TESTED BATTERY PACK IAW 
- [SDR IPXA2023111310526](https://openairdocs.org/sdr/IPXA2023111310526), Nov 9, 2023: SWITCH. FAILED. FOUND L1 ENTRY DOOR WARNING SWITCH FAIL LOC: DOOR AFT-LOWER SIDE(REPLACE) I.A.W AMM 52-71-01-004-024 AND 52-71-01-404-047 REV.108 REPLACED THE L1 ENTRY DOOR WAR
- [SDR IPXA2023110910526](https://openairdocs.org/sdr/IPXA2023110910526), Nov 9, 2023: UNKNOWN. UNKNOWN. FOUND L1 ENTRY DOOR WARNING SWITCH FAIL LOC: DOOR AFT-LOWER SIDE(REPLACE)
- [SDR IPXA2023110271851](https://openairdocs.org/sdr/IPXA2023110271851), Nov 2, 2023: LIGHT. INOPERATIVE. FOUND UPPER DECK DOORWAY EMERGENCY LIGHT INOP EQUIP L5734(REPLACE) I.A.W AMM 33-51-00-032-001 AND 33-51-00-432-006 REV 108 AND WDM 33-51-72 REV 43 REPLACED EMER
- [SDR IPXA2023110919447](https://openairdocs.org/sdr/IPXA2023110919447), Oct 29, 2023: ESCAPE REEL. DAMAGED. *** SUPPLEMENTAL SDR *** FAULT - FOUND COCKPIT EMERGENCY ESCAPE DESCENT DEVICE SEAL BROKEN LOC: NO.6, NO.7, NO.8 TOTAL: 3 EA I.A.W AMM 25-61-01-002-001 REV 108 
- [SDR IPXA2023103019447](https://openairdocs.org/sdr/IPXA2023103019447), Oct 29, 2023: UNKNOWN. UNKNOWN. *** SDR FILED OPEN *** FAULT - FOUND COCKPIT EMERGENCY ESCAPE DESCENT DEVICE SEAL BROKEN LOC: NO.6, NO.7, NO.8 TOTAL: 3 EA OK TO WORK
- [SDR IPXA2025022699591](https://openairdocs.org/sdr/IPXA2025022699591), Oct 16, 2023: HOSE. DEFORMED. *** SUPPLEMENTAL SDR *** FAULT - FOUND MAIN DECK AIR HOSE DEFORM AT STA 1210 RIGHT SIDE (REPLACE) REPLACED THE MAIN DECK AIR HOSE AT STA 1210 R/H SIDE. SUPPLY A
- [SDR IPXA2023101699591](https://openairdocs.org/sdr/IPXA2023101699591), Oct 16, 2023: UNKNOWN. UNKNOWN. *SDR FILED OPEN* FAULT - FOUND MAIN DECK AIR HOUSE DEFORM AT STA 1210 RIGHT SIDE (REPLACE) OKAY TO WORK
- [SDR IPXA2023030746362](https://openairdocs.org/sdr/IPXA2023030746362), Mar 5, 2023: FLAP. INOPERATIVE. *EMERGENCY DECLARED* ON SHORT FINAL GOT €ŒFLAPS DRIVE€?, DID GOAROUND, RAN CHECKLIST AND MADE NORMAL LANDING LEFT FLAPS DOWN. FOR PRECAUTIONAL, PERFORMED LUBR
- [SDR IPXA2022111456334](https://openairdocs.org/sdr/IPXA2022111456334), Nov 11, 2022: FIRE WARNING. FALSE ACTIVATION. DIVERSION, DECLARED A MAYDAY, PAN PAN. APU FIRE MESSAGE DURING CRUISE AFTER BOTTLE DISCHARGE OF APU FIRE BOTTLE. APU FIRE INDICATION WAS STILL ON INTERMITTENT. 
- [SDR IPXA2022121954390](https://openairdocs.org/sdr/IPXA2022121954390), Nov 10, 2022: CONTROL CARD. FAULTED. MOMENTARY "FIRE APU" EICAS WITH MOMENTARY FIRE LIGHT IN APU FIRE SWITCH HANDLE IN CRUISE FLIGHT APU COMPARTMENT OPENED AND INSPECTED WITH NO FINDINGS.<BR>T/S C/
- [SDR IPXA2022121922222](https://openairdocs.org/sdr/IPXA2022121922222), Oct 29, 2022: CIRCUIT CARD. FAULTED. EICAS MSG APU FIRE LINKED TO T3F18E000L8ZJ. REPLACED AFOLTS CARD PER 747 AMM 26-10-01.
- [SDR IPXA2022103119573](https://openairdocs.org/sdr/IPXA2022103119573), Oct 28, 2022: FIRE WARNING. ILLUMINATED. APU FIRE SWITCH LIGHT IN SWITCH BEGAN FLICKERING EN ROUTE SHORTLY AFTER EICAS MSSG APU FIRE BEGAN APPEARING ON & OFF RAPIDLY THEN APU FIRE BELL WENT OFF. LINKED
- [SDR IPXA2022072703486](https://openairdocs.org/sdr/IPXA2022072703486), Jul 24, 2022: DISPLAY. FAULTED. R MCDU WENT BLACK IN FLIGHT.JETTISON OF 100KLBS OF FUEL AND RETURNED TO SZX.AFTER LANDING AND POWER TRANSFER TO APU MCDU CAME BACK DEFER C MCDU PER MEL 34-61-2-
- [SDR IPXA2022062413841](https://openairdocs.org/sdr/IPXA2022062413841), Jun 23, 2022: BATTERY. INOPERATIVE. ONE HOUR AFTER LEVEL-OFF, FL390 "BATT CHARGER APU" STATUS MESSAGE "APU BATTERY CHARGER FAIL (BCU-2)"<BR>MSG: 24099<BR>REF FIM 24-34-00-812-803
- [SDR IPXA2022021679082](https://openairdocs.org/sdr/IPXA2022021679082), Feb 16, 2022: RADAR. FAILED. INSPECTION TYPE:NA**ATB SDR FILED** **NO EMERGENCY DECLARED** DURING CLIMBOUT LEFT AND RIGHT WXR SYS FAILED. AIR TURN BACKCOMPLETED GROUND TEST REF AMM 34-43-00
- [SDR IPXA2022010977673](https://openairdocs.org/sdr/IPXA2022010977673), Jan 9, 2022: BATTERY. NONE. INSPECTION TYPE:C3FOUND L1 DOOR EMERGENCY LIGHT INOPI.A.W AMM 33-51-04-902-001-001 REV.103.00 REPLACED THE L1 DOOR EMERGENCY LIGHT BATTERY AND PERFORMED EMERGEN
- [SDR IPXA2022010977672](https://openairdocs.org/sdr/IPXA2022010977672), Jan 9, 2022: BATTERY. NONE. INSPECTION TYPE:C3FOUND U/D EMERGENCY LIGHT M4914 INOPI.A.W AMM 33-51-04-902-001-001 REV.103.00 REPLACED THE U/D EMERGENCY LIGHT BATTERY (M5168) AND PERFORMED E
- [SDR IPXA2022011177765](https://openairdocs.org/sdr/IPXA2022011177765), Dec 27, 2021: NONE. NONE. INSPECTION TYPE:C3GOUGE ON EXISTING REPAIR DOUBLER OF TOP PANEL ON R/H OUTBD AFT FLAPREPAIR I.A.W BOEING SRID : 3-5236994806 AND UPS EO 747-5750-64795-C
- [SDR IPXA2020041054069](https://openairdocs.org/sdr/IPXA2020041054069), Apr 8, 2020: CIRCUIT CARD. FAULTY. INSPECTION TYPE:N/A** ATB ** EICAS MESSAGE DET FIRE/OHT 3 ALONG WITH STATUS MESSAGES ENG 3 FIRE LP B ENG 3 FIRE 3 FIRE LP A RESULTED IN AN ATB 0004Z.R&R CIRCUIT
- [SDR IPXA2020011350846](https://openairdocs.org/sdr/IPXA2020011350846), Dec 28, 2019: SKIN. GOUGED. INSPECTION TYPE:C2GOUGE ON EXISTING REPAIR OF TOP PANEL OF RH OUTBD AFT FLAPREPAIR I.A.W BOEING SRID : 3-4592189605 AND UPS EO B747-5750-64795-B
- [SDR IPXA2019100647574](https://openairdocs.org/sdr/IPXA2019100647574), Oct 6, 2019: FLOOR PANEL. DAMAGED. HOLE IN THE MAIN DECK FLOOR UNDER CENTERLINE RESTRAINT ASSY AT BS 1700. MANUFACTURED A NEW FLOOR PANEL IAW EO B747-5320-42648A.
- [SDR IPXA2019020138561](https://openairdocs.org/sdr/IPXA2019020138561), Jan 30, 2019: ENGINE. FLAMED OUT. ON LANDING #4 ENGINE FLAMED OUT WHEN ENTERING REVERSE AT APPROX 130 KTS.PERFORMED INSPECTION PER FIM 71 03 150 812 810 500, FOUND NO FOD DAMAGE. FOUND SPINNER F
- [SDR IPXA2018102985426](https://openairdocs.org/sdr/IPXA2018102985426), Oct 28, 2018: SKIN. DENTED. RIGHT OTBD AFT FLAP LOWER SURFACE WAS DENTED. REPAIRED IAW EO B747-5750-69080-B.
- [SDR IPXA2018081322692](https://openairdocs.org/sdr/IPXA2018081322692), Aug 11, 2018: CRASH AXE. DAMAGED. MCD CRASH AX BLADE DAMAGED. R & R THE CRASH AX IAW AMM 25-60-00-216-005.
- [SDR IPXA2018052730055](https://openairdocs.org/sdr/IPXA2018052730055), May 27, 2018: FLOOR PANEL. DAMAGED. MCD FLOOR PANEL P/N 141U5876-94 SEC 41 STA 460-480 TWO DAMAGES AFT EDGE 5"X2" OTBD EDGE 5"X1". FABRICATED NEW FLOOR PANEL IAW B747-5320-51172-A
- [SDR IPXA2018011525474](https://openairdocs.org/sdr/IPXA2018011525474), Jan 14, 2018: CRASH AXE. DAMAGED. MAIN CARGO CRASH AXE DAMAGED. REPLACED THE CRASH AXE IAW MM 25-60-00-216-005.
- [SDR IPXA2017112223804](https://openairdocs.org/sdr/IPXA2017112223804), Nov 21, 2017: SKIN. DAMAGED. FUSELAGE SKIN DAMAGE AT STA 1770 BETWEEN STR 35R & 36R. REPAIRED PER EO B747-5330-66492A AND SRM 53-00-01-2R REPAIR 1.
- [SDR IPXA2017101222530](https://openairdocs.org/sdr/IPXA2017101222530), Oct 11, 2017: BATTERY PACK. DISCHARGED. FOUND THE EXIT SIGN AFT OF COCKPIT NOT ILLUMINATED. REPLACED THE BATTERY PACK M5169 IAW AMM 33-51-04-902-001-001, REV 90.02.
- [SDR IPXA2017070518937](https://openairdocs.org/sdr/IPXA2017070518937), Jul 5, 2017: BATTERY. INOPERATIVE. UPPER DECK EMERGENCY LIGHTS L1533, L5733, L5767, AND M4915 INOPERATIVE. REPLACED THE EMERGENCY LIGHT BATTERY (M5169 )IAW AMM 33-51-04-902-001-001, REV 89.01, AN
- [SDR IPXA2017070518938](https://openairdocs.org/sdr/IPXA2017070518938), Jun 27, 2017: SKIN. DAMAGED. INSPECTION TYPE: 18FO, DEEP NOTCH DAMAGE ON THE RT WING OTBD AFT FLAP TOP PANEL.
- [SDR IPXA2017060517903](https://openairdocs.org/sdr/IPXA2017060517903), Jun 5, 2017: SKIN. DENTED. DENT IN THE LOWER MID SKIN OTBD OF THE INBD CANOE FAIRING. REPAIRED IAW SRM 57-53-01-2R-1, & 51-70-10-2R-4.

All 117: https://openairdocs.org/aircraft/N573UP/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 CF6-80C2B1F1)

- [STC SE01543CH](https://openairdocs.org/stc/SE01543CH): Replace Hamilton Sundstrand P/N 778839-13, 778839-14, 778839-19, 778839-20, 778839-37, 778839-38, 816682-1, 840618-2, 880724 carbon bushings with Cook Airtomic P/N AIR22947 Slotted Entry Busing in the High Pressure Shutoff Valve. Cook Airtomic
- [STC SE01478CH](https://openairdocs.org/stc/SE01478CH): Installation of Cook Airtomic alignment joint p/n AIR 22912. Cook Airtomic
- [STC SE01471AT](https://openairdocs.org/stc/SE01471AT): Replace right and left side Rohr, Inc. fire detection harness on GE CF6-80C2 engine. Unison Industries. Lists CF6-80C2 Series
- [STC SE00463LA](https://openairdocs.org/stc/SE00463LA): Install fireproof blankets on the engine fan reverser intermediate fireseal, in lieu of fireproof intumescent coating. This STC is jointly by owned by Hi Temp Insulation and MRA Systems acting through Middle River Aircraft Systems, 103 Chesapeake Park Plaza, Baltimore, MD 21220. Hi Temp Insulation Inc
- [STC SA2227SO](https://openairdocs.org/stc/SA2227SO): Installation of wiring and associated components for utilization of the Rolls Royce, Inc., ARINC, interface/readers UT1317 or UT1317/1, for the purpose of acquisition, recording, and analysis in real time of engine/aircraft/ systems. (767 SERIES POWERED BY RR RB-11-524 SERIES. Rolls Royce, Inc. Lists CF6-80 Series

## Related

- Other Boeing 747-44AF aircraft: https://openairdocs.org/model/boeing-747-44af/aircraft.md
- The GE CF6-80C2B1F1 engine: https://openairdocs.org/engine/ge-cf6-80c2b1f1.md

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