# N353UP: 2012 Boeing 767-34AF

- Status: Valid registration
- Airframe: [Boeing 767-34AF](https://openairdocs.org/model/boeing-767-34af) (registry code 1385212, 190 seats)
- Engine: [GE CF6-80C2B6F](https://openairdocs.org/engine/ge-cf6-80c2b6f) (registry code 30109)
- Data sheets: [TCDS E13NE](https://openairdocs.org/tcds/E13NE) (General Electric Company GE Aerospace) (OpenAirDocs)
- Serial number: 37877
- Year built: 2012
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: August 31, 2012
- Certificate issued: September 4, 2012
- Expires: September 30, 2028
- Mode S code: A3F1C2
- 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=353UP
- Page: https://openairdocs.org/aircraft/N353UP

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): 34 in force

### Matched by airframe (Boeing 767-34AF)

None in force.

### Matched by engine (GE CF6-80C2B6F)

- [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
- [AD 91-05-21](https://openairdocs.org/ad/91-05-21): High Pressure Turbine · General Electric CF6-80C2A5, CF6-80C2B6, CF6-80C2B6F and 1 more. Effective Mar 27, 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) (4 in force)

- [SAIB 2023-15](https://openairdocs.org/saib/2023-15): Falsified Forms from AOG Technics. Issued Dec 19, 2023
- [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 N353UP.

## FAA accident and incident reports

None matched to N353UP.

## Service difficulty reports (52, 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 IPXA2026100560445](https://openairdocs.org/sdr/IPXA2026100560445), Oct 2, 2026: LENS. MISSING. COCKPIT EMERGENCY LIGHT PANEL -LIGHT INDICATION MISSING LENS, REPLACED LENS IN REF WITH AMM 33-16-02 OPS CK NORMAL
- [SDR IPXA2026091898870](https://openairdocs.org/sdr/IPXA2026091898870), Sep 17, 2026: SMOKE GOGGLES. DAMAGED. CENTER SUPERNUMERARY SEAT SMOKE GOGGLES CRAZED AND BUBBLED REMOVED AND REPLACED CENTER SUPERNUMERARY SEAT SMOKE GOGGLES IAW MM 25-64-00
- [SDR IPXA2026071295408](https://openairdocs.org/sdr/IPXA2026071295408), Jul 10, 2026: ENGINE. STALLED. DIVERTED, LEFT ENG COMPRESSOR STALL AND VIBRATION. REF. T3F18E0095NNN. NR 1 ENG WAS REPLACED IAW MXP-6002-INST-JIC.
- [SDR IPXA2026071095408](https://openairdocs.org/sdr/IPXA2026071095408), Jul 10, 2026: COMPRESSOR. STALLED. EMERGENCY DECLARED, LEFT ENG COMPRESSOR STALLED AND VIBRATION.
- [SDR IPXA2026061846827](https://openairdocs.org/sdr/IPXA2026061846827), Jun 13, 2026: BEARING. WORN. WORN BEARING, NR 2 PYLON R/H AFT FAIRING DOOR NR 4 HINGE FITTING. (REPLACE). INSTALL LOCK FASTENERS ON NEW HINGE IAW SRM 51-40-02-0G REV. 95 AND DWG 313T3340 SH
- [SDR IPXA2026061746847](https://openairdocs.org/sdr/IPXA2026061746847), Jun 13, 2026: HINGE. WORN. WORN OUT, BEARING, NR 1 PYLON LT FAIRING DOOR NO.4 HINGE. IAW BAC5117-18 REV. D PERFORMED BONDING RESISTANCE TEST BETWEEN THE FASTEREN HEAD AND THE STRUCTURE, T
- [SDR IPXA2026061648693](https://openairdocs.org/sdr/IPXA2026061648693), Jun 13, 2026: SEAL. BROKEN. BROKEN SPRING SEAL, NR 1 PYLON 436CL PANEL. REMOVED DAMAGE SEAL IAW SRM 51-40-02-0G, REV. 95. INSTALLED NEW SEAL IAW SRM 51-40-02-0G REV. 95, AND DWG 311T2570 S
- [SDR IPXA2026061646606](https://openairdocs.org/sdr/IPXA2026061646606), Jun 13, 2026: SEAL. BROKEN. BROKEN SEAL, NR 2 PYLON FAIRING PNL 446CL. REMOVED DAMAGE SEAL IAW SRM 51-40-02-0G REV. 95. INSTALLED NEW SEAL IAW SRM 51-40-02-0G REV. 95 AND DWG 311T2570 SH. 
- [SDR IPXA2026061549269](https://openairdocs.org/sdr/IPXA2026061549269), Jun 13, 2026: RUB STRIP. CHAFED. CHAFED WEARSTRIP, NR 1 ENG RT CORE COWL OUTER L/E 1:00 TO 4:00 AREA. INSTALLED NEW WEARSTRIP I.A.W SRM 51-40-02-0G REV.95 AND GOODRICH AEROSTRUCTURES CMM IPL 71
- [SDR IPXA2026061546619](https://openairdocs.org/sdr/IPXA2026061546619), Jun 13, 2026: BRACKET. CHAFED. CHAFED BRACKET ASSY, NO.1 ENG L/H CORE COWL HOLD OPEN ROD STOWAGE. INSTALLED NEW BRACKET I.A.W SRM 51-40-02-0G REV. 95 AND GOODRICH CMM IPL 71-13-23 REV. 47.
- [SDR IPXA2026061648540](https://openairdocs.org/sdr/IPXA2026061648540), Jun 13, 2026: RIVET. SHEARED. SHEARED RIVET, RT WING OTBD L/E UPPER SURFACE AT OSS 439.50, ADJACENT NO.8 SLAT INBD AUX TRACK. REMOVED DAMAGE FORMER IAW SRM 51-40-02-0G, REV 95. INSTALLED NEW
- [SDR IPXA2026061548246](https://openairdocs.org/sdr/IPXA2026061548246), Jun 13, 2026: BRACKET. CRACKED. CRACKED BRACKET, LT WING INBD L/E NO.6 SLAT DRIVE TORQUE TUBE SUPPORT, LES 285. INSTALLED NEW BRACKET I.A.W SRM 51-40-02-0G REV. 95 AND DWG NO.114T1240 SH.6 REV
- [SDR IPXA2026061548249](https://openairdocs.org/sdr/IPXA2026061548249), Jun 13, 2026: BRACKET. CRACKED. CRACKED BRACKET, RT WING INBD SLAT TORQUE TUBE SUPPORT AT INBD L/E CAVITY, ISS 285.233. INSTALLED NEW BRACKET IAW SRM 51-40-02-0G REV. 95 AND DWG NO. 114T1240 S
- [SDR IPXA2026061548351](https://openairdocs.org/sdr/IPXA2026061548351), Jun 13, 2026: PLATE. CRACKED. CRACKED PLATE, LT WING INBD T/E CAVITY LOWER RIB SUPPORT, WS 293. INSTALLED NEW PLATE I.A.W SRM 51-40-02-0G REV. 95 AND BOEING DWG NO.113T1639 SH. 1 REV. G.
- [SDR IPXA2026061646643](https://openairdocs.org/sdr/IPXA2026061646643), Jun 13, 2026: ANGLE. CRACKED. CRACKED ANGLE, NR 1 PYLON LOWER FAIRING NAC STA 376 FRAME AFT OUTBOARD. REMOVED DAMAGE CLIP I.A.W SRM 51-40-02-0G REV. 95. INSTALLED NEW CLIP IAW SRM 51-40-02-0
- [SDR IPXA2026061729318](https://openairdocs.org/sdr/IPXA2026061729318), Jun 12, 2026: SEAL DEPRESSOR. DEFORMED. DEFORMED DEPRESSOR, MAIN DECK CGO DOOR CUTOUT UPPER AREA AFT SIDE STA 632. INSTALLED MAIN DECK SIDE CARGO DOOR AFT-UPPER SIDE DEPRESSOR SEAL I.A.W AMM 20-11-00-
- [SDR IPXA2026061731672](https://openairdocs.org/sdr/IPXA2026061731672), Jun 12, 2026: FORMER. CRACKED. CRACKED FORMER, FWD SIDE OF LT WING OUTBD L/E NOSE BEAM, OSS 441.6. REMOVED DAMAGE FORMER IAW SRM 51-40-02-0G REV.95. INSTALL NEW FORMER I.A.W SRM 51-40-02-0G R
- [SDR IPXA2026061733397](https://openairdocs.org/sdr/IPXA2026061733397), Jun 12, 2026: RUB STRIP. CHAFED. CHAFING - WEARSTRIP, NO.1 ENG L/H CORE COWL INNER FACE T/E UPPER SIDE. (REPLACE) IAW AMM 71-11-06-714-013-H00 REV.148. CORE COWL INSTALLED NEW WEAR STRIP IAW SR
- [SDR IPXA2026061733279](https://openairdocs.org/sdr/IPXA2026061733279), Jun 12, 2026: ANGLE. CRACKED. MEC COMPARTMENT, MAIN DECK FLOOR ANGLE CRACK STA 246, LBL 49. INSTALLED FABRICATED BRACKET I.A.W SRM 51-40-02-0G REV. 95 AND BOEING DWG NO:141T5600 SHEET 4 REV 
- [SDR IPXA2026061532808](https://openairdocs.org/sdr/IPXA2026061532808), Jun 12, 2026: BRACKET. CHAFED. CHAFED BRACKET ASSY, NR 1 ENG R/H CORE COWL HOLD OPEN ROD STOWAGE. INSTALL NEW BRACKET I.A.W SRM 51-40-02-0G REV.95 AND CMM IPL 71-13-24 REV.50.
- [SDR IPXA2026061628887](https://openairdocs.org/sdr/IPXA2026061628887), Jun 12, 2026: SUPPORT ANGLE. CRACKED. FOUND AFT CARGO DOORWAY CEILING PANEL SUPPORT ANGLE CRACK BETWEEN BS 1329 TO BS 1338 RBL 90. ACCOMPLISHED REPAIR I.A.W SRM 51-40-02-0G REV. 95, UPS SREO-12357-R
- [SDR IPXA2026061633263](https://openairdocs.org/sdr/IPXA2026061633263), Jun 12, 2026: PLATE. MISSING. MISSING PLATE, NR 1 PYLON LT FAIRING DOOR HOLD OPEN ROD BRACKET. FABRICATED IAW DWG 69B90733, SHT 1, REV.A. PL REV A; PSDL REV- AND ORIGINAL PART AS A SAMPLE IA
- [SDR IPXA2026061631589](https://openairdocs.org/sdr/IPXA2026061631589), Jun 12, 2026: CHANNEL. CRACKED. CRACKED CHANNEL, NR 1 PYLON FAIRING DOOR HOLD OPEN ROD BRACKET INSIDE. REMOVED DAMAGE BRACKET I.A.W SRM 51-40-02-0G REV. 95. INSTALLED NEW BRACKET I.A.W SRM 51-
- [SDR IPXA2026061816181](https://openairdocs.org/sdr/IPXA2026061816181), Jun 11, 2026: FLOOR PANEL. DELAMINATED. THE FLOOR PANEL P/N: 453T1996-116 IN THE AFT CARGO COMPARTMENT IS DELAMINATED. I.A.W. 767-300F SRM 53-00-50-2R-0 REV. 95 PERFORM REPAIR AS BELOW STEP :1.1 REMOV
- [SDR IPXA2026061611571](https://openairdocs.org/sdr/IPXA2026061611571), Jun 11, 2026: ANTENNA. ERODED. FOUND V.S.T HF ANTENNA (321E) EROSION.
- [SDR IPXA2026061612251](https://openairdocs.org/sdr/IPXA2026061612251), Jun 11, 2026: SKIN. DENTED. DENTED SKIN, LOWER FACE OF LT WING T/E OUTBD FLAP T/E LOWER SKIN, WBL 373. IAW AMM 51-21-10-307-020 REV.148, REPAINT REWORK AREA.. JOB COMPLETED AND CONDITION C
- [SDR IPXA2026061312271](https://openairdocs.org/sdr/IPXA2026061312271), Jun 11, 2026: ANGLE. CRACKED. THE BULK CARGO OUTBOARD ANGLE AT STA 1578 RBL 80 IS CRACKED. REMOVED DAMAGE ANGLE I.A.W SRM 51-40-02-0G REV.95. INSTALL NEW ANGLE I.A.W SRM 51-40-02-0G REV.95 A
- [SDR IPXA2026061312281](https://openairdocs.org/sdr/IPXA2026061312281), Jun 11, 2026: ANGLE. CRACKED. THE BULK CARGO OUTBOARD ANGLE AT BS 1578 LBL 80 IS CRACKED. REMOVED DAMAGE ANGLE I.A.W SRM 51-40-02-0G REV. 95. INSTALLED NEW ANGLE I.A.W SRM 51-40-02-0G REV. 9
- [SDR IPXA2026061312429](https://openairdocs.org/sdr/IPXA2026061312429), Jun 11, 2026: ANGLE. CRACKED. THE BULK CARGO INBOARD ANGLE AT STA 1578 LBL 80 IS CRACKED. INSTALLED NEW ANGLE I.A.W SRM 51-40-02-0G REV. 95 AND BOEING DWG NO. 146T5650 SH. 5 REV. C.
- [SDR IPXA2026061312492](https://openairdocs.org/sdr/IPXA2026061312492), Jun 11, 2026: ANGLE. CRACKED. THE BULK CARGO INBOARD ANGLE AT STA 1578 RBL 80 IS CRACKED. INSTALL NEW ANGLE I.A.W SRM 51-40-02-0G REV.95 AND BOEING DWG NO:146T5650 SH 5 REV.C.
- [SDR IPXA2026061311987](https://openairdocs.org/sdr/IPXA2026061311987), Jun 11, 2026: FLOOR PANEL. CRACKED. MAJOR REPAIR, FOUND MAIN DECK FLOOR PANEL WITH CRACK DAMAGE. REMOVED MAIN DECK CARGO FLOOR PANEL AND REMOVED SEALANT. PANEL 251XFF. INSTALLED FLOOR PANEL I.A.W 
- [SDR IPXA2026061312018](https://openairdocs.org/sdr/IPXA2026061312018), Jun 11, 2026: FLOOR PANEL. CRACKED. MAJOR REPAIR, FOUND MAIN DECK FLOOR PANEL WITH CRACK DAMAGE, REMOVED MAIN DECK CARGO FLOOR PANEL AND REMOVED SEALANT. PANEL NO:252UFF. INSTALLED FLOOR PANEL IAW
- [SDR IPXA2028080700149](https://openairdocs.org/sdr/IPXA2028080700149), Aug 6, 2025: STRUT. CORRODED. SUSPECTED CORROSION RH MLG UPPER STRUT BODY - APPROX 14€? X 0.75€? TOTAL AREA BLENDED CORROSION AREAS IAW CMM 20-10-01 STEP 2.F AND 2.H. PITTING STILL REMAINS
- [SDR IPXA2024062589422](https://openairdocs.org/sdr/IPXA2024062589422), Jun 11, 2024: STRAP. CRACKED. STRAP, NR 1 ENGINE LT HPT COOLING DUCT REAR FRAME FLANGE SUPPORT BRACKET RETAINING. IAW AMM 70-50-00-912-001-H00, REV.142, REPLACED THE STRAP WITH NEW & TORQUED
- [SDR IPXA2024061191168](https://openairdocs.org/sdr/IPXA2024061191168), Jun 11, 2024: NONE. NONE. FUSELAGE DRAIN HOLES INSPECTION AND INSTALLATION AFT OF BS 1725.5 BETWEEN S-36L AND S-36R. PERFORMED MODIFICATION PER UPS E.O.82173-JIC001. CONDITION CHECK OK.
- [SDR IPXA2024061189422](https://openairdocs.org/sdr/IPXA2024061189422), Jun 11, 2024: BRACKET. CRACKED. CRACK - STRAP, NO.1 ENGINE LH HPT COOLING DUCT REAR FRAME FLANGE SUPPORT BRACKET RETAINING (REPLACE) OK TO WORK
- [SDR IPXA2024040866276](https://openairdocs.org/sdr/IPXA2024040866276), Apr 1, 2024: SKIN. GOUGED. SKIN GOUGE RH FUSELAGE APPROX 26€? FORWARD OF LOWER FWD CARGO DOOR. (APPROX. FUSELAGE STATION 453 BETWEEN STRINGER 26R & 25R). MARKED WITH TAPE. REINSTALLED SA
- [SDR IPXA2024040166276](https://openairdocs.org/sdr/IPXA2024040166276), Apr 1, 2024: SKIN. GOUGED. SKIN GOUGE RH FUSELAGE APPROX 26€? FORWARD OF LOWER FWD CARGO DOOR. (APPROX. FUSELAGE STATION 453 BETWEEN STRINGER 26R & 25R). MARKED WITH TAPE. MATERIAL ID & 
- [SDR IPXA2023112854981](https://openairdocs.org/sdr/IPXA2023112854981), Nov 26, 2023: FLOOR PANEL. DAMAGED. FLOOR PANEL POSITION 4 CENTER HAS A HOLE IN IT (REMOVED FOR SHEET METAL) HOLE IS MARKED VERIFIED COMPLETION OF FLOORBOARD REPAIR PER SRM 53-00-50-2R. OK TO INST
- [SDR IPXA2023111733479](https://openairdocs.org/sdr/IPXA2023111733479), Nov 17, 2023: COVER. INOPERATIVE. L-1 DOOR ARMING LEVER HINGED COVER INOP. DEFERRED THE L-1 DOOR ARMING LEVER HINGED COVER IAW MEL 52-11-2. INSTALLED ARMING LEVER HINGE COVER AND INSTALLED L1 DO
- [SDR IPXA2023021891100](https://openairdocs.org/sdr/IPXA2023021891100), Feb 18, 2023: LIGHT. NONE. INSPECTION TYPE:N/ACOCKPIT AFT LFT EMERGENCY LIGHT INOP.R & R'D COCKPIT AFT LFT EMERGENCY LIGHT IAW MM 33-51-11-201.
- [SDR IPXA2022041681217](https://openairdocs.org/sdr/IPXA2022041681217), Apr 16, 2022: FLOOR PANEL. NONE. INSPECTION TYPE:N/AMAIN CARGO COMPARTMENT FLOOR PANEL REPAIR POSITION 4 CENTERMANUFACTURED NEW PANEL IAW UPS EO B767-5320-9693-1
- [SDR IPXA2021041968342](https://openairdocs.org/sdr/IPXA2021041968342), Apr 18, 2021: ACTUATOR. MALFUNCTIONED. ATB - NO EMERG DECLARED. NO EQUIP USED . AFTER T/O AND AFTER RAISING THE LANDING GEAR EICAS MESSAGE GEAR DISAGREE MSG DISPLAYED RAN APPROPIATE CHECK LIST, LANDI
- [SDR IPXA2021021565681](https://openairdocs.org/sdr/IPXA2021021565681), Feb 12, 2021: WARNING MESSAGE. FALSE INDICATION. -RAPID DECOMPRESSION -NO EMERG DECLARED-O2 MASKS USED-NO OTHER EMERG EQUIP USED** CABIN ALTTITUDE WARNING AT FL 360 WITH BOTH PACKS ON. RECOVERED CABIN IN AUTO 
- [SDR IPXA2019072945044](https://openairdocs.org/sdr/IPXA2019072945044), Jul 27, 2019: TRU. INOPERATIVE. INSPECTION TYPE:CK TRU (35 AMP) CIRCUIT BREAKER TRIPPED. FOUND DURING PS CHECK.REMOVED AND REPLACED APU TRU. SYSTEM OPS CHECK GOOD. REF AMM 24-32-04.
- [SDR IPXA2019052842568](https://openairdocs.org/sdr/IPXA2019052842568), May 28, 2019: UNKNOWN. MALFUNCTIONED. INSPECTION TYPE:N/A LEFT THRUST REVERSER UNLOCKED BUT DID NOT DEPLOY ON LANDING REV REMAINED AMBER BOTH THRUST REVERSERS STOWED CORRECTLY HAS HIST LPG 110584 5/
- [SDR IPXA2018021426536](https://openairdocs.org/sdr/IPXA2018021426536), Feb 13, 2018: OXYGEN MASK. INOPERATIVE. FIRST OFFICER`S OXYGEN MASK INFLATION HARNESS SEPERATED. DOES NOT INFLATE. REPLACED THE OXYGEN MASK. OPS CHECKED GOOD IAW MM 35-11-51-401.
- [SDR IPXA2017080720237](https://openairdocs.org/sdr/IPXA2017080720237), Aug 5, 2017: LAMP. INOPERATIVE. EXTERIOR EMERGENCY LIGHT INOPERATIVE. REPLACED THE LAMP AND OPS CHECKED GOOD IAW AMM 33-51-16.
- [SDR IPXA2016081707135](https://openairdocs.org/sdr/IPXA2016081707135), Aug 17, 2016: SHUTOFF VALVE. INOPERATIVE. EICAS FOR RT ENGINE HPSOV, LIGHT ON STEADY DURING CLIMBOUT. RT ENG BLEED LIGHT ILLUMINATED, AND DUCT PRESSURE FLUCTUATED.
- [SDR IPXA2016070805557](https://openairdocs.org/sdr/IPXA2016070805557), Jul 8, 2016: LAMP. INOPERATIVE. EXTERNAL EMERGENCY LIGHT INOPERATIVE. REPLACED THE LAMP, OPS TESTED GOOD IAW AMM 33-50-00.

All 52: https://openairdocs.org/aircraft/N353UP/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 CF6-80C2B6F)

- [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 767-34AF aircraft: https://openairdocs.org/model/boeing-767-34af/aircraft.md
- The GE CF6-80C2B6F engine: https://openairdocs.org/engine/ge-cf6-80c2b6f.md

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