# N346UP: 2011 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: 37868
- Year built: 2011
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: July 28, 2011
- Certificate issued: August 5, 2011
- Expires: August 31, 2027
- Mode S code: A3D568
- 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=346UP
- Page: https://openairdocs.org/aircraft/N346UP

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 N346UP.

## FAA accident and incident reports

None matched to N346UP.

## Service difficulty reports (23)

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 IPXA2026061094710](https://openairdocs.org/sdr/IPXA2026061094710), Jun 10, 2026: HANDLE. INOPERATIVE. MAIN ENTRY DOOR LOCK IS LOOSE WHEN LOCKING AND UNLOCKING FROM THE INSIDE. TIGHTEND SECONDARY CAPTURE HANDLE BOLT IAW AMM 52-12-25. PERFORMED OPERATIONAL CHECK O
- [SDR IPXA2026030497959](https://openairdocs.org/sdr/IPXA2026030497959), Mar 3, 2026: AOA. FAULTED. ATB, ON CLIMBOUT CAPT SIDE AIRSPEED WAS ABOVE CLEAN MAN BUT EICAS SHOWED AIRSPEED LOW F/O SIDE NORMAL. GOT STICK SHAKER WITH NORMAL AIRSPEED BOTH F/D VERTICAL G
- [SDR IPXA2025062521798](https://openairdocs.org/sdr/IPXA2025062521798), Jun 20, 2025: ANGLE. BROKEN. BROKEN - ANGLE, AFTER CARGO DOOR FORWARD LINK AREA (REPLACE) FORMED THE JOGGLES OF THE REPAIR ANGLE I.A.W. EGAT EI NO. F2025A52M-1318 SEQUENCE A STEP 1.C (FORME
- [SDR IPXA2025070304712](https://openairdocs.org/sdr/IPXA2025070304712), Jun 19, 2025: LEVER. DEFORMED. FOUND THE ENTRY DOOR DOORWAY ARMING LEVER HINGE ASSY WITH DEFORM DAMAGE (REPLACE) INSTALLED DOORWAY LINING I.A.W AMM 52-12-02-404-025 REV. 145.
- [SDR IPXA2025062601105](https://openairdocs.org/sdr/IPXA2025062601105), Jun 19, 2025: FILLER. CORRODED. FOUND THE PLATE WITH CORROSION DAMAGE AT STA 1601 LBL 59 IN BULK CARGO COMPARTMENT CEILING AREA. (REPLACE) 1. FABRICATE FILLER (P/N: 146T5609-67) PER BOEING DRA
- [SDR IPXA2025061904712](https://openairdocs.org/sdr/IPXA2025061904712), Jun 19, 2025: HINGE. DEFORMED. FOUND THE ENTRY DOOR DOORWAY ARMING LEVER HINGE ASSY WITH DEFORM DAMAGE (REPLACE)
- [SDR IPXA2025061901689](https://openairdocs.org/sdr/IPXA2025061901689), Jun 19, 2025: FLOOR PANEL. DENTED. FOUND MAIN DECK FLOOR PANEL WITH DENT DAMAGE, P/N : 146T5876-105 PANEL NO : 231AFF STA 412 ~ STA 530 RBL 11 ~ LBL 11 (REPAIR) I.A.W AMM 25-57-02-004-029, AMM 25
- [SDR IPXA2025061901603](https://openairdocs.org/sdr/IPXA2025061901603), Jun 19, 2025: FLOOR PANEL. CRACKED. FOUND MAIN DECK CARGO FLOOR PANEL WITH CRACK DAMAGE, P/N : 143T5864-89 PANEL NO : 251XFF (REPAIR) I.A.W AMM 25-57-02-004-029, AMM 25-57-05-004-001 AND AMM 25-58
- [SDR IPXA2025061901749](https://openairdocs.org/sdr/IPXA2025061901749), Jun 19, 2025: FLOOR PANEL. DENTED. FOUND MAIN DECK FLOOR PANEL WITH DENT DAMAGE, P/N : 146T5876-99 PANEL NO : 231FFF STA 530 ~ STA 654+22 LBL 11 ~ RBL 11 (REPAIR) I.A.W AMM 25-57-02-004-029, AMM 
- [SDR IPXA2025061901844](https://openairdocs.org/sdr/IPXA2025061901844), Jun 19, 2025: FLOOR PANEL. DENTED. FOUND MAIN DECK FLOOR PANEL WITH DENT DAMAGE, P/N : 146T5876-111 PANEL NO : 232FFF STA 530 ~ STA 654+22 RBL 11 ~ RBL 33 (REPAIR) I.A.W AMM 25-57-02-004-029, AMM
- [SDR IPXA2025061901724](https://openairdocs.org/sdr/IPXA2025061901724), Jun 19, 2025: FLOOR PANEL. DENTED. FOUND MAIN DECK FLOOR PANEL WITH DENT DAMAGE, P/N : 146T5876-103 PANEL NO : 232AFF STA 412 ~ STA 530 RBL 11 ~ RBL 33 (REPAIR) I.A.W AMM 25-57-02-004-029, AMM 25
- [SDR IPXA2024070873240](https://openairdocs.org/sdr/IPXA2024070873240), Jul 5, 2024: LAMP. INOPERATIVE. DURING PDC, FOUND EXTERIOR EMERGENCY LIGHT INOP RELAMPED EXTERIOR EMERGENCY LIGHT IAW AMM 33-51-16. OPS CHECK GOOD.
- [SDR IPXA2023052877635](https://openairdocs.org/sdr/IPXA2023052877635), May 22, 2023: BATTERY. NO TEST. *** SUPPLEMENTAL SDR *** FAULT - FOUND EMERGENCY LIGHT BATTERY PACK CAPACITY TEST FAIL (REPLACE) 1. I.A.W AMM 33-51-07-022-001 & 33-51-07-422-012 REV.139.01 REP
- [SDR IPXA2023052277635](https://openairdocs.org/sdr/IPXA2023052277635), May 22, 2023: UNKNOWN. UNKNOWN. *SDR FILED OPEN* FAULT - FOUND EMERGENCY LIGHT BATTERY PACK CAPACITY TEST FAIL (REPLACE)
- [SDR IPXA2022100486839](https://openairdocs.org/sdr/IPXA2022100486839), Oct 4, 2022: FAN. ODOR. FWD EQ EXH FAN STATUS FAUL ODOR IN COCKPIT. DEFERRED IAW MEL # 21 58 4 2 1 DMP C/W.R/R FWD EQUIP COOLING EXIT FAN PER AMM 21-58-06-004-133 & 21-58-404-146. LEAK
- [SDR IPXA2018062030876](https://openairdocs.org/sdr/IPXA2018062030876), Jun 17, 2018: FMC. LOCKED. BOTH FMC'S LOCKED UP. AIR TURNBACK. ACCOMPLISHED FIM PROCEDURE 815-854. FAULT CORRECTED.
- [SDR IPXA2016040101497](https://openairdocs.org/sdr/IPXA2016040101497), Apr 1, 2016: EEC. INOPERATIVE. EGT INDICATES BLANK OR ABNORMAL OTHER ENGINE INDICATIONS NORMAL. R & R NR 2 ELECTRONIC ENGINE CONTROL IAW AMM 73-21-15-401. OPS CHECKS GOOD IAW AMM 71-00-00-725
- [SDR IPXA2016031100633](https://openairdocs.org/sdr/IPXA2016031100633), Mar 11, 2016: SEAL. LEAKING. I.T. ISS BY L1 DOOR STARTED AT 8000FT DIFFICULTY IN YELLOW .87 CABIN ALT 6200, DIFFICULTY ALT 6200 DIFF AT FL 210 NOISE STOPPED, DIFFICULTY ALT 4KFOUND PRESSURE
- [SDR IPXA2016030800493](https://openairdocs.org/sdr/IPXA2016030800493), Mar 7, 2016: SKIN. DAMAGED. LEFT INBD AFT FLAP LOWER SKIN DAMAGED, REPAIRED IAW EP B767-5750-59435-C.
- [SDR IPXA2016020598932](https://openairdocs.org/sdr/IPXA2016020598932), Feb 4, 2016: SEAL. LEAKING. CREW ENTRY DOOR: CREW ENTRY DOOR HAS NOISE FROM AIRLEAK. LEAK SEEMS TO BE IN THE AREA NEAR THE BOTTOM OF THE DOOR. INSTALLED LOOSE SEAL AT BOTTOM OF CREW ENTRY 
- [SDR IPXA2014092984467](https://openairdocs.org/sdr/IPXA2014092984467), Sep 28, 2014: WEDGE. DAMAGED. NR 9 SLAT T/E WEDGE DAMAGED AT APPROXIMATELY OSS 682.74. REPAIRED IAW EO 5750-55602-A.
- [SDR IPXA2014092984466](https://openairdocs.org/sdr/IPXA2014092984466), Sep 28, 2014: SKIN. DAMAGED. NR 10 SLAT T/E WEDGE, UPPER SKIN DAMAGED AT INBD AFT CORNER. REPAIRED IAW EO B767-5750-55629-A.
- [SDR IPXA12671000](https://openairdocs.org/sdr/IPXA12671000), Jan 9, 2012: WARNING LIGHT. FALSE ACTIVATION. INSPECTION TYPE:ETOP ATB FORWARD EQUIPMENT OVERHEAT EICAS MESSAGE DISPLAYED AND OVERHEAT LIGHT ILLUMINATED. COMPLETED FIM 21-58-00, FIG 116. NO FAULTS FOUND.

## 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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