# N302UP: 1995 Boeing 767-34AF

- Status: Valid registration
- Airframe: [Boeing 767-34AF](https://openairdocs.org/model/boeing-767-34af) (registry code 1385212, 190 seats)
- Engine: [GE CF6-80 series](https://openairdocs.org/engine/ge-cf6-80-series) (registry code 30025)
- Data sheets: [TCDS E13NE](https://openairdocs.org/tcds/E13NE) (General Electric Company GE Aerospace) (OpenAirDocs)
- Serial number: 27240
- Year built: 1995
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: October 12, 1995
- Certificate issued: October 13, 1995
- Expires: August 31, 2028
- Mode S code: A32890
- 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=302UP
- Page: https://openairdocs.org/aircraft/N302UP

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. The registry lists only the engine series, so ADs for every GE CF6-80 model are included.

## ADs that may apply (OpenAirDocs): 61 in force

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

None in force.

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

- [AD 2024-24-03](https://openairdocs.org/ad/2024-24-03): Engine Exhaust · Boeing MD-11, MD-11F and CF6-80C2D1F. Effective Jan 13, 2025
- [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 2022-02-18](https://openairdocs.org/ad/2022-02-18): Engine Mount Section · General Electric CF6-80C2A1, CF6-80C2A2, CF6-80C2A3 and 3 more. Effective Feb 25, 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 2018-07-05](https://openairdocs.org/ad/2018-07-05): Turbine Section · General Electric CF6-80A, CF6-80A1, CF6-80A2 and 1 more. Effective May 11, 2018
- [AD 2017-11-15](https://openairdocs.org/ad/2017-11-15): Turbine/ Turboprop Engine--Turbine Section · General Electric CF6-80C2L1F. Effective Jul 13, 2017
- [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 2011-23-04](https://openairdocs.org/ad/2011-23-04): Forward engine mount assembly side links · General Electric CF6-45A, CF6-45A2, CF6-50A and 14 more. Effective Dec 12, 2011
- [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 2009-14-08](https://openairdocs.org/ad/2009-14-08): High-pressure compressor rotor (HPCR) stages 11-14 spool/ shafts · General Electric CF6-80C2B5F. Effective Aug 5, 2009
- [AD 2009-08-06](https://openairdocs.org/ad/2009-08-06): Stage 1 high-pressure turbine (HPT) rotor  
 disks · General Electric CF6-80A, CF6-80A1, CF6-80A2 and 1 more. Effective May 18, 2009
- [AD 2009-07-10](https://openairdocs.org/ad/2009-07-10): High-pressure turbine rotor (HPTR) · General Electric CF6-80A, CF6-80A1, CF6-80A2 and 1 more. Effective May 6, 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 2008-02-17](https://openairdocs.org/ad/2008-02-17): Thrust reverser actuation systems · General Electric CF6-50A, CF6-50C, CF6-50C1 and 16 more. Effective Feb 28, 2008
- [AD 2007-24-07](https://openairdocs.org/ad/2007-24-07): Thermal spray coating on certain stage 1 fan disks · General Electric CF6-80C2B1. Effective Jan 2, 2008
- [AD 2007-22-07](https://openairdocs.org/ad/2007-22-07): Electronic control unit (ECU) · General Electric CF6-80C2D1F. Effective Nov 28, 2007
- [AD 2007-21-06](https://openairdocs.org/ad/2007-21-06): Electronic control unit (ECU) · General Electric CF6-80C2A5F. Effective Nov 15, 2007
- [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 2006-06-08](https://openairdocs.org/ad/2006-06-08): Latching system of the fan reverser · General Electric CF6-80C2D1F. Effective Apr 25, 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 2005-06-07](https://openairdocs.org/ad/2005-06-07): Directional pilot valve (DPV) assembly · General Electric CF6-80A1, CF6-80A3, CF6-80C2A1 and 5 more. Effective Apr 25, 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 2004-07-13](https://openairdocs.org/ad/2004-07-13): High pressure turbine (HPT) stage 1 disks · General Electric CF6-80C2A5F, CF6-80C2B5F, CF6-80C2B7F and 1 more. Effective May 6, 2004
- [AD 2003-12-08](https://openairdocs.org/ad/2003-12-08): Directional pilot valve · General Electric CF6-80A1, CF6-80A3, CF6-80C2A1 and 5 more. Effective Jul 23, 2003
- [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 2001-06-09](https://openairdocs.org/ad/2001-06-09): Aft Engine Mount Link Assemblies · General Electric CF6-80A3. Effective May 1, 2001
- [AD 2000-12-08](https://openairdocs.org/ad/2000-12-08): Mount Link Assemblies · General Electric CF6-80C2A1, CF6-80C2A2, CF6-80C2A3 and 4 more. Effective Aug 28, 2000
- [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 95-17-16](https://openairdocs.org/ad/95-17-16): Compressor Rear Frame · General Electric CF6-80A, CF6-80A1, CF6-80A2 and 1 more. Effective Nov 7, 1995
- [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 94-07-04](https://openairdocs.org/ad/94-07-04): High Pressure Turbine Disk · General Electric CF6-80A, CF6-80A1, CF6-80A2 and 1 more. Effective May 23, 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

### 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 2006-12-24](https://openairdocs.org/ad/2006-12-24) (historical): Five-link forward mount assembly · General Electric CF6-45A, CF6-45A2, CF6-50A and 14 more. Effective Jul 21, 2006
- [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 2003-01-05](https://openairdocs.org/ad/2003-01-05) (historical): Dovetail slots · General Electric CF6-80A, CF6-80A1, CF6-80A2 and 1 more. Effective Jan 28, 2003
- [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 2000-08-12](https://openairdocs.org/ad/2000-08-12) (historical): Life-limited Parts · General Electric CF6-80A, CF6-80A1, CF6-80A2 and 10 more. Effective Oct 23, 2000
- [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 99-18-20](https://openairdocs.org/ad/99-18-20) (historical): Inadvertent In-flight Thrust Reverser · General Electric Aircraft Engines CF6-50 Series (all), CF6-80A1, CF6-80A3 and 6 more. Effective Nov 2, 1999
- [AD 99-18-19](https://openairdocs.org/ad/99-18-19) (historical): Inadvertent Thrust Reverser · General Electric CF6-80A, CF6-80A1, CF6-80A2 and 7 more. Effective Sep 24, 1999
- [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 98-15-17](https://openairdocs.org/ad/98-15-17) (historical): Link Assembly · General Electric CF6-80A3. Effective Aug 7, 1998
- [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

All 80: https://openairdocs.org/aircraft/N302UP/ads.md

## 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 N302UP.

## FAA accident and incident reports

None matched to N302UP.

## Service difficulty reports (189, 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 IPXA2026081088170](https://openairdocs.org/sdr/IPXA2026081088170), Aug 8, 2026: LIGHT. INOPERATIVE. EXIT LIGHT IS COMING OUT OF ITS SOCKET NEAR MAIN ENTERANCE DOOR CAREFULLY PUSHED THE LENS INTO ITS POSITION IAW AMM 33-51-01-402-030 4(B)(3)
- [SDR IPXA2026012494466](https://openairdocs.org/sdr/IPXA2026012494466), Jan 14, 2026: WASHER. MISSING. MAJOR REPAIR, FOUND AFT CARGO DOOR NOISE DURING OPERATION. (REPLACE) 23. REPLACED THE FORWARD ROTARY ACTUATOR OF AFT CARGO DOOR I.A.W AMM 52-37-04-004-001 REV.1
- [SDR IPXA2026011553100](https://openairdocs.org/sdr/IPXA2026011553100), Jan 5, 2026: BRACKET. CORRODED. RIGHT WING INBOARD TRAILING EDGE, LANDING GEAR SUPPORT BEAM ATTACH HYD TUBE BRACKET AND CHANNER CORROSION (REPLACE). INSTALL FABRICATE BRACKET I.A.W SRM 51-40-0
- [SDR IPXA2026011219182](https://openairdocs.org/sdr/IPXA2026011219182), Jan 2, 2026: SKIN. CRACKED. -CRACK, L1 ENTRY DOOR AFT LOWER CORNER OUTER SKIN CRACK (REPAIR) PERFORMED SRM 53-10-01-2R-1 REV.94 AND EGAT WORK SHEET NO.60004 STEP 26.
- [SDR IPXA2026010910971](https://openairdocs.org/sdr/IPXA2026010910971), Jan 1, 2026: TEE ANGLE. CRACKED. DURING PERFORM INSPECTION FOUND NOSE W/W CRACK OF ANGLE AT STA 287 RBL 25. (REPAIR). ACCOMPLISHED THE REPAIR I.A.W SRM 51-70-12-0G-0 REV. 94 AND EGAT WORK SHEET
- [SDR IPXA2026010910990](https://openairdocs.org/sdr/IPXA2026010910990), Jan 1, 2026: TEE ANGLE. CRACKED. DURING PERFORM INSPECTION FOUND NOSE W/W ANGLE CRACK AT STA 287 LBL 25. (REPAIR). ACCOMPLISHED THE REPAIR I.A.W SRM 51-70-12-0G-0 REV. 94 AND EGAT WORK SHEET NO
- [SDR IPXA2025111187420](https://openairdocs.org/sdr/IPXA2025111187420), Nov 3, 2025: DOOR. INOPERATIVE. COCKPIT LIFE RAFT STOWAGE COMPARTMENT DOOR WILL NOT STAY OPEN. FOUND BUSHING LOSE IN PFM BOX. INSTALLED SHOCK STRUT IN COCKPIT LIFE RAFT STOWAGE BOX COMPARTMENT
- [SDR IPXA2025110387420](https://openairdocs.org/sdr/IPXA2025110387420), Nov 3, 2025: DOOR. MALFUNCTIONED. COCKPIT LIFE RAFT STOWAGE COMPARTMENT DOOR WILL NOT STAY OPEN. DEFERRED PER SREO-52198.
- [SDR IPXA2025080476560](https://openairdocs.org/sdr/IPXA2025080476560), Aug 3, 2025: LEVER. MALFUNCTIONED. MAIN ENTRY DOOR - YELLOW PUSH TO, SECURE LEVER WILL NOT ENGAGE TO THE LOCK/SECURE POSITION WITH THE ENTRY DOOR CLOSED. PERFORMED ADJUSTMENT OPS CHECK OF ENTRY/S
- [SDR IPXA2024012439367](https://openairdocs.org/sdr/IPXA2024012439367), Jan 2, 2024: FAIRING. CRACKED. FAULT - CRACK FAIRING, LH WING NO.3 FLAP TRACK AFT FAIRING INBD LE (REPAIR) REVIEW COMPLETE
- [SDR IPXA2024010339386](https://openairdocs.org/sdr/IPXA2024010339386), Jan 2, 2024: SKIN. UNKNOWN. *SDR FILED OPEN* FAULT - DENT, FUSELAGE EXTERNAL SKIN, STA 1654.5 ~ STA 1678, S-25R TO S-26R (EVALUATE) OK TO WORK
- [SDR IPXA2024010239367](https://openairdocs.org/sdr/IPXA2024010239367), Jan 2, 2024: UNKNOWN. UNKNOWN. CRACK FAIRING, LH WING NO.3 FLAP TRACK AFT FAIRING INBD LE (REPAIR) OK TO WORK. OPEN
- [SDR IPXA2024012933121](https://openairdocs.org/sdr/IPXA2024012933121), Jan 1, 2024: FLOOR PANEL. CRACKED. FAULT- FOUND AFT CARGO FLOOR PANEL CRACK, P/N:453T1996-20 (REPAIR) CUT OUT THE DAMAGE AND CLEAN. MEASURE THE CUTOUT (LENGTH: 1.4", WIDTH: 0.3", AT AFTER EDGE AN
- [SDR IPXA2024012434330](https://openairdocs.org/sdr/IPXA2024012434330), Jan 1, 2024: ACCESS PANEL. CRACKED. FAULT - CRACK PNL, RH WING LOWER OUTD MAIN FUEL PUMP ACCESS PNL(REPLACE) REVIEWED
- [SDR IPXA2024012433335](https://openairdocs.org/sdr/IPXA2024012433335), Jan 1, 2024: SKIN. DEBONDED. **SUPPLEMENTAL SDR**FAULT - DISBOND - SKIN, EXTERNAL LOWER SIDE SURFACE OF L/H AFTER WING TO BODY ACCESS PNL NO.197KL. (REPAIR) REVIEWED
- [SDR IPXA2024012433143](https://openairdocs.org/sdr/IPXA2024012433143), Jan 1, 2024: FLOOR PANEL. CRACKED. FAULT - FOUND AFT CARGO FLOOR PANEL CRACK, P/N:453T1996-12 (REPAIR) REVIEW COMPLETE
- [SDR IPXA2024010933056](https://openairdocs.org/sdr/IPXA2024010933056), Jan 1, 2024: SKIN PANEL. CRACKED. FAULT- CRACK - RIVET EDGE SKIN, NO.2 PYLON FWD TORQUE BOX ACCESS PANEL NO.442AL CUTOUT.(REPAIR) IAW AMM 78-31-01-404-026-H00, REV:141, STEP G. (28), PERF UPS EO
- [SDR IPXA2024010334304](https://openairdocs.org/sdr/IPXA2024010334304), Jan 1, 2024: UNKNOWN. UNKNOWN. *SDR FILED OPEN* FAULT - CRACK ANGLE, INTERNAL AFT INBOARD UPPER SLAT EDGE OF NO.1 PYLON AFT NACELLE STRUT FAIRING(REPLACE) OK TO WORK
- [SDR IPXA2024010333121](https://openairdocs.org/sdr/IPXA2024010333121), Jan 1, 2024: UNKNOWN. UNKNOWN. *SDR FILED OPEN* FAULT- FOUND AFT CARGO FLOOR PANEL CRACK, P/N:453T1996-20 (REPAIR) OK TO WORK
- [SDR IPXA2024010333335](https://openairdocs.org/sdr/IPXA2024010333335), Jan 1, 2024: UNKNOWN. UNKNOWN. *SDR FILED OPEN* FAULT - DISBOND - SKIN, EXTERNAL LOWER SIDE SURFACE OF L/H AFTER WING TO BODY ACCESS PNL NO.197KL. (REPAIR) OK TO WORK
- [SDR IPXA2024010334330](https://openairdocs.org/sdr/IPXA2024010334330), Jan 1, 2024: ACCESS PANEL. UNKNOWN. *SDR FILED OPEN* FAULT - CRACK PNL, RH WING LOWER OUTD MAIN FUEL PUMP ACCESS PNL(REPLACE) OK TO WORK
- [SDR IPXA2024010333266](https://openairdocs.org/sdr/IPXA2024010333266), Jan 1, 2024: SKIN. UNKNOWN. MAJOR REPAIR* FAULT- CRACK, FUSELAGE EXTERNAL SKIN, STA1654 STA1678 S-13AR (REPAIR) ACCOMPLISHED REPAIR I.A.W SRM 53-80-01-2R-7 REV.88 REVIEW COMPLETE
- [SDR IPXA2024010333056](https://openairdocs.org/sdr/IPXA2024010333056), Jan 1, 2024: UNKNOWN. UNKNOWN. *SDR FILED OPEN* FAULT- CRACK - RIVET EDGE SKIN, NO.2 PYLON FWD TORQUE BOX ACCESS PANEL NO.442AL CUTOUT.(REPAIR) OK TO WORK
- [SDR IPXA2024010333143](https://openairdocs.org/sdr/IPXA2024010333143), Jan 1, 2024: UNKNOWN. UNKNOWN. *SDR FILED OPEN* FAULT - FOUND AFT CARGO FLOOR PANEL CRACK, P/N:453T1996-12 (REPAIR) OK TO WORK
- [SDR IPXA2024012426549](https://openairdocs.org/sdr/IPXA2024012426549), Dec 31, 2023: CHANNEL. CRACKED. FAULT - CRACK - CHANNEL, NO.1 ENG PANEL NO.437DB TRIANGLE SUPPORT (REPAIR) REVIEW COMPLETE
- [SDR IPXA2024012425988](https://openairdocs.org/sdr/IPXA2024012425988), Dec 31, 2023: ANGLE. CRACKED. FAULT - CRACK - CLIP NO.2 PYLON AFTER LOWER FAIRING AFTER INNER SIDE, LH FAIRING PNL SUPPORT BRACKET(REPLACE) REVIEW COMPLETE
- [SDR IPXA2024012425948](https://openairdocs.org/sdr/IPXA2024012425948), Dec 31, 2023: SPLICE. CRACKED. FAULT - CRACK SPLICE, RH WING LE FIXED STRUCTURE NOSE AREA AT LES 691(REPLACE) REVIEW COMPLETE
- [SDR IPXA2024012425690](https://openairdocs.org/sdr/IPXA2024012425690), Dec 31, 2023: WEB. CRACKED. **SUPPLEMENTAL SDR**FAULT - CRACK - WEB, INTERNAL AFTER LOWER SIDE OF NO.2 PYLON AFTER FAIRING PNL NO.447DB (REPLACE) REVIEW COMPLETE
- [SDR IPXA2024012425651](https://openairdocs.org/sdr/IPXA2024012425651), Dec 31, 2023: BEAM. CRACKED. **SUPPLEMENTAL SDR**FAULT - CRACK FORMER, LH WING OUTBD FIXED LE NOSE BEAM OSS 437 (REPLACE) REVIEW COMPLETE
- [SDR IPXA2024012425639](https://openairdocs.org/sdr/IPXA2024012425639), Dec 31, 2023: BEAM. CRACKED. **SUPPLEMENTAL SDR**FAULT - CRACK FORMER, LH WING OUTBD FIXED LE NOSE BEAM OSS 441 (REPLACE) REVIEW COMPLETE.
- [SDR IPXA2024012425536](https://openairdocs.org/sdr/IPXA2024012425536), Dec 31, 2023: SKIN PANEL. CRACKED. FAULT- CRACK SKIN PNL, LH WING NO.2 FLAP TRACK AFT FAIRING(REPAIR) REVIEW COMPLETE
- [SDR IPXA2024012424970](https://openairdocs.org/sdr/IPXA2024012424970), Dec 31, 2023: WEB. CRACKED. FAULT - CRACK - WEB MAIN EQUIPMENT CENTER AT STA 246 LBL 50" (REPLACE) REVIEWED
- [SDR IPXA2024010326549](https://openairdocs.org/sdr/IPXA2024010326549), Dec 31, 2023: UNKNOWN. UNKNOWN. *SDR FILED OPEN* FAULT - CRACK - CHANNEL, NO.1 ENG PANEL NO.437DB TRIANGLE SUPPORT (REPAIR) OK TO WORK
- [SDR IPXA2024010325536](https://openairdocs.org/sdr/IPXA2024010325536), Dec 31, 2023: UNKNOWN. UNKNOWN. *SDR FILED OPEN* FAULT- CRACK SKIN PNL, LH WING NO.2 FLAP TRACK AFT FAIRING(REPAIR) REMOVED FITTING I.A.W SRM 51-40-02-0G REV.88
- [SDR IPXA2024010324970](https://openairdocs.org/sdr/IPXA2024010324970), Dec 31, 2023: UNKNOWN. UNKNOWN. *SDR FILED OPEN* FAULT - CRACK - WEB MAIN EQUIPMENT CENTER AT STA 246 LBL 50" (REPLACE) 1.REMOVED DAMAGE PART I.A.W. SRM 51-40-02-0G REV.88
- [SDR IPXA2024010325651](https://openairdocs.org/sdr/IPXA2024010325651), Dec 31, 2023: UNKNOWN. UNKNOWN. *SDR FILED OPEN* FAULT - CRACK FORMER, LH WING OUTBD FIXED LE NOSE BEAM OSS 437 (REPLACE) ASSIGNED EO-89074-REQ1 TO FAULT.
- [SDR IPXA2024010325690](https://openairdocs.org/sdr/IPXA2024010325690), Dec 31, 2023: UNKNOWN. UNKNOWN. *SDR FILED OPEN* FAULT - CRACK - WEB, INTERNAL AFTER LOWER SIDE OF NO.2 PYLON AFTER FAIRING PNL NO.447DB (REPLACE) OK TO WORK
- [SDR IPXA2024010325988](https://openairdocs.org/sdr/IPXA2024010325988), Dec 31, 2023: UNKNOWN. UNKNOWN. *SDR FILED OPEN* FAULT - CRACK - CLIP NO.2 PYLON AFTER LOWER FAIRING AFTER INNER SIDE, LH FAIRING PNL SUPPORT BRACKET(REPLACE) OK TO WORK
- [SDR IPXA2024010325639](https://openairdocs.org/sdr/IPXA2024010325639), Dec 31, 2023: UNKNOWN. UNKNOWN. *SDR FILED OPEN* FAULT - CRACK FORMER, LH WING OUTBD FIXED LE NOSE BEAM OSS 441 (REPLACE) REMOVED DAMAGE PARTS I.A.W SRM 51-40-02-0G REV.88
- [SDR IPXA2024010325948](https://openairdocs.org/sdr/IPXA2024010325948), Dec 31, 2023: UNKNOWN. UNKNOWN. *SDR FILED OPEN* FAULT - CRACK SPLICE, RH WING LE FIXED STRUCTURE NOSE AREA AT LES 691(REPLACE) OK TO WORK
- [SDR IPXA2024012901641](https://openairdocs.org/sdr/IPXA2024012901641), Dec 29, 2023: HINGE. CRACKED. FAULT - CRACK - ANGLE, NO. 1 ENG R/H AFT FAIRING DOOR HINGE BEAM ANGLE AT #4.(REPLACE) I.A.W AMM 54-53-02-404-006 REV.141 INSTALLED HINGE BOLT FOR ACCESS NO.1 P
- [SDR IPXA2024012901341](https://openairdocs.org/sdr/IPXA2024012901341), Dec 29, 2023: LEVER. DEFORMED. FAULT - FOUND MAIN ENTRY DOOR DOORWAY ARMING LEVER HINGE ASSY DEFORM (REPLACE) I.A.W AMM 20-11-00-910-802 REV.141 REPLACE HINGE ASSY. I.A.W AMM 52-12-02-404-025
- [SDR IPXA2024011201605](https://openairdocs.org/sdr/IPXA2024011201605), Dec 29, 2023: FILLER. CRACKED. FAULT - CRACK - FLOOR STRUCTURE BULK CARGO COMPARTMENT RIGHT AREA STA 1600 RBL 60(REPLACE) I.A.W AMM 25-59-01-404-019 REV.140 INSTALL SLOPING SIDEWALL , SIDEWAL
- [SDR IPXA2024011201574](https://openairdocs.org/sdr/IPXA2024011201574), Dec 29, 2023: FILLER. CRACKED. CRACK - FLOOR STRUCTURE BULK CARGO COMPARTMENT LEFT AERA STA 1590 LBL60(REPLACE) I.A.W AMM 25-59-01-404-019 REV.140 INSTALL SLOPING SIDEWALL , SIDEWALL AND BULK
- [SDR IPXA2024012401671](https://openairdocs.org/sdr/IPXA2024012401671), Dec 29, 2023: ANGLE. CRACKED. FAULT - CRACK - ANGLE, NO. 1 ENG L/H AFT FAIRING DOOR HINGE BEAM ANGLE AT #4(REPLACE) REVIEW COMPLETE
- [SDR IPXA2024010301605](https://openairdocs.org/sdr/IPXA2024010301605), Dec 29, 2023: UNKNOWN. UNKNOWN. *SDR FILED OPEN* FAULT - CORROSION - FLOOR STRUCTURE BULK CARGO COMPARTMENT RIGHT AREA STA 1600 RBL 60(REPLACE) 1. REMOVED DAMAGE PARTS I.A.W SRM 51-40-02-0G RE
- [SDR IPXA2024010301574](https://openairdocs.org/sdr/IPXA2024010301574), Dec 29, 2023: UNKNOWN. UNKNOWN. *SDR FILED OPEN* FAULT- CORROSION - FLOOR STRUCTURE BULK CARGO COMPARTMENT LEFT AERA STA 1590 LBL60(REPLACE) 1. REMOVED DAMAGE PARTS I.A.W SRM 51-40-02-0G REV. 
- [SDR IPXA2024010301341](https://openairdocs.org/sdr/IPXA2024010301341), Dec 29, 2023: UNKNOWN. UNKNOWN. *SDR FILED OPEN* FAULT - FOUND MAIN ENTRY DOOR DOORWAY ARMING LEVER HINGE ASSY DEFORM (REPLACE) OK TO WORK
- [SDR IPXA2024010301671](https://openairdocs.org/sdr/IPXA2024010301671), Dec 29, 2023: UNKNOWN. UNKNOWN. *SDR FILED OPEN* FAULT - CRACK - ANGLE, NO. 1 ENG L/H AFT FAIRING DOOR HINGE BEAM ANGLE AT #4(REPLACE) I.A.W. AMM 54-53-02-004-002, REV.140, REMOVED NO.4 L/H HI
- [SDR IPXA2024010301641](https://openairdocs.org/sdr/IPXA2024010301641), Dec 29, 2023: UNKNOWN. UNKNOWN. *SDR FILED OPEN* FAULT - CRACK - ANGLE, NO. 1 ENG R/H AFT FAIRING DOOR HINGE BEAM ANGLE AT #4.(REPLACE) I.A.W. AMM 54-53-02-004-002, REV.140, REMOVED NO.4 R/H H

All 189: https://openairdocs.org/aircraft/N302UP/reports.md

## STCs that may be installed (OpenAirDocs) (6)

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 CF6-80 series)

- [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. Lists CF6-80A
- [STC SE01478CH](https://openairdocs.org/stc/SE01478CH): Installation of Cook Airtomic alignment joint p/n AIR 22912. Cook Airtomic. Lists CF6-80C2 Series
- [STC SE00969CH](https://openairdocs.org/stc/SE00969CH): Install AeroControlex P/N 2605290-001 variable stator feedback control cable. AeroControlex Group TransDigm Inc. Lists CF6-80A
- [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. Lists CF6-80C2A1
- [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

## Related

- Other Boeing 767-34AF aircraft: https://openairdocs.org/model/boeing-767-34af/aircraft.md
- The GE CF6-80 series engine: https://openairdocs.org/engine/ge-cf6-80-series.md

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