# N359UP: 2013 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: 37870
- Year built: 2013
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: July 12, 2013
- Certificate issued: July 15, 2013
- Expires: July 31, 2029
- Mode S code: A4080C
- Registered owner: [C C & E I LLC](https://openairdocs.org/faa-owner/C%20C%20%26%20E%20I%20LLC)
- Location: [Louisville, KY](https://openairdocs.org/faa-place/KY/Louisville)
- Owner type: LLC
- 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=359UP
- Page: https://openairdocs.org/aircraft/N359UP

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 N359UP.

## FAA accident and incident reports

None matched to N359UP.

## Service difficulty reports (22)

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 IPXA2025081102208](https://openairdocs.org/sdr/IPXA2025081102208), Aug 11, 2025: PUMP. NO DISCREPANCY. AIR TURN BACK, CENTER TANK RIGHT FUEL PUMP PRESSURE IS LOW PERFORMED QRH PROCEDURE DID NOT RETURN A/C TO NORMAL OPERATION RESULTED IN AN ATB IAW AMM 28-31-01. R
- [SDR IPXA2025072256161](https://openairdocs.org/sdr/IPXA2025072256161), Jul 22, 2025: PUMP. INOPERATIVE. DURING CRUISE, RECEIVED CTR R FUEL PUMP (EICAS C). RAN CHECKLIST AND OPERATED REMAINDER OF FLIGHT WITH CTR R FUEL PUMP INOP. I.A.W. AMM 28-22-05-004-057-002 REV
- [SDR IPXA2024101525778](https://openairdocs.org/sdr/IPXA2024101525778), Oct 14, 2024: BATTERY PACK. INOPERATIVE. EMERGENCY LIGHT SYSTEM WAS INOP R&R BATTERY PACK IAW AMM 33-51-07/201. OPS CHECK GOOD. OK FOR SERVICE.
- [SDR IPXA2024032664195](https://openairdocs.org/sdr/IPXA2024032664195), Mar 25, 2024: DOOR. LEAKING. CREW ENTRY DOOR LEAKS. AT 6000€™ CLIMBING EXCESSIVE NOISE FROM ENTRY DOOR INSPECTED CREW ENTRY DOOR AND FOUND DOOR SEAL AT THE BOTTOM OUT OF SEAL RETAINER. SEA
- [SDR IPXA2024020222506](https://openairdocs.org/sdr/IPXA2024020222506), Jan 25, 2024: WINDOW. HAZE. DURING PRE-FLIGHT, FOUND FIRST OFFICERS FORWARD WINDOW TO BE HAZY AND OPAQUE. VISION OUT OF WINDOW IS IMPAIRED R/R #1 WINDOW ON FO SIDE IAW B767 AMM 56-11-01/40
- [SDR IPXA2024012622506](https://openairdocs.org/sdr/IPXA2024012622506), Jan 25, 2024: WINDOW. HAZE. *SDR FILED OPEN* DURING PRE-FLIGHT, FOUND FIRST OFFICERS FORWARD WINDOW TO BE HAZY AND OPAQUE. VISION OUT OF WINDOW IS IMPAIRED REMOVED AND REPLACED WINDOW HEAT
- [SDR IPXA2024012580764](https://openairdocs.org/sdr/IPXA2024012580764), Jan 22, 2024: WINDOW. CLOUDY. *SUPPLEMENTAL SDR* R1 WINDOW VERY CLOUDY. RR R1 WINDOW IAW AMM 55-11-01. OPS CHECK GOOD.
- [SDR IPXA2024012380764](https://openairdocs.org/sdr/IPXA2024012380764), Jan 22, 2024: WINDOW. DAMAGED. R1 WINDOW VERY CLOUDY. REMOVED R1 WINDOW IAW 767 AMM 56-11-01-004-039
- [SDR IPXA2023020690680](https://openairdocs.org/sdr/IPXA2023020690680), Feb 4, 2023: NOT REPORTED. INOPERATIVE. INSPECTION TYPE:NALOUD HISSING NOISE COMING FROM BOTTOM OF ENTRY DOOR PASSING 5000 FT. ON CLIMBOUT. SUBSIDED, BUT STILL LOUD, PASSING 17000'. MAINTAINED VOLUME 
- [SDR IPXA2022092486559](https://openairdocs.org/sdr/IPXA2022092486559), Sep 23, 2022: CHANNEL. LEAKING. FRM CODE 52-11-10-04 NOISE FROM AIR LOCK TOWARD THE BOTTOM OF THE FORWARD ENTRY DOORFOUND APPROX 8" OF CREW ENTRY DOOR BOTTOM SEAL OUT OF CHANNEL REINSTALLED PE
- [SDR IPXA2022072584540](https://openairdocs.org/sdr/IPXA2022072584540), Jul 23, 2022: EICAS. FAULT MESSAGE. INSPECTION TYPE:ETOPAFTER LANDING FWD EQPT VALVE EICAS EXECUTED QRH PROCEDURE VALVE LIGHT STAYED ILLUMINATEDC/W FIM TASK 21 58 00 815 828 001 MSG CLEARED C/W AM
- [SDR IPXA2021082373015](https://openairdocs.org/sdr/IPXA2021082373015), Aug 20, 2021: FLOOR PANEL. DAMAGED. INSPECTION TYPE:C4, DAMAGE ON M/D FLOOR PANEL AT STA 1480,AND BETWEEN RBL 54.75 AND 77.50.FABRICATE THE REPLACEMENT FLOOR PANEL PER EO NO.B767-5320-9693-I.
- [SDR IPXA2020111662459](https://openairdocs.org/sdr/IPXA2020111662459), Nov 16, 2020: SKIN. DENTED. INSPECTION TYPE: N/A LT WING OUTBOARD TRAILING EDGE FLAP LOWER SKIN DENTED. REPAIRED PER EO B767-5750-78220-B REPAIRED ON N/R'S 662344 AND 662346.
- [SDR IPXA2020071097551](https://openairdocs.org/sdr/IPXA2020071097551), Jul 9, 2020: WARNING MESSAGE. ACTIVATED. VIBRATION AND SLOW EXCELLARATION ABOVE V1. SUSPECT TIRE ON NOSE OR MAIN. WHEN GEAR LEVER PLACED TO OFF, GEAR DISAGREE AND TAIL SKID EICAS. GEAR UP POSITION CLEA
- [SDR IPXA2020032353392](https://openairdocs.org/sdr/IPXA2020032353392), Mar 20, 2020: LIGHT. INOPERATIVE. INSPECTION TYPE:N/AEXTERIOR EMERGENCY LIGHT INOPRELAMPED SAME & OPS OK PER AMM 33-51-16-201
- [SDR IPXA2019030439651](https://openairdocs.org/sdr/IPXA2019030439651), Mar 3, 2019: SKIN. DENTED. INSPECTION TYPE:N/A RIGHT WING NR 8 SLAT LEADING EDGE DENT. REPAIRED IAW SRM 57-43-01-2R-1 AND EO B767-5750-70968-B.
- [SDR IPXA2018111215869](https://openairdocs.org/sdr/IPXA2018111215869), Nov 11, 2018: FLOORBOARD. DAMAGED. MCD CENTER ISLE POSITION 8, FLOORBOARD WAS DAMAGED. FABRICATED A NEW FLOORBOARD IAW EO-B767-5320-9693-I.
- [SDR IPXA2017110723362](https://openairdocs.org/sdr/IPXA2017110723362), Nov 2, 2017: SIGN. OUT OF ADJUST. CREW ENTRY DOOR CLOSED SENSOR SIGN OUT OF ADJUSTMENT. SUSPECT DOOR RIG. FOUND CREW ENTRY DOOR CLOSED SENSOR SIGN WITHIN ADJ LIMITS IAW 52-71-00-735-072. NO DOOR
- [SDR IPXA2017082721003](https://openairdocs.org/sdr/IPXA2017082721003), Aug 24, 2017: ENGINE. OVERHEATED. RT ENGINE OVERHEAT MESSAGE, RAN QRH, PULLED ENGINE BACK 1 KNOB AND THE LIGHT WENT OUT. REMOVED AND REPLACED THE NR 2 ENGINE.
- [SDR IPXA2016080506674](https://openairdocs.org/sdr/IPXA2016080506674), Aug 2, 2016: STATIC PORT. DAMAGED. INSPECTION TYPE: ATB, LIGHTNING STRIKE TO RADOME, TWICE, RETURNED TO DEPARTURE. R & R LT ALT STATIC PORT IAW AMM 34-11-03-004-035 AND 34-11-03-404-010. SYS OK I
- [SDR IPXA2015080792095](https://openairdocs.org/sdr/IPXA2015080792095), Aug 7, 2015: SKIN. CRACKED. INSPECTION TYPE: C1, CRACK INDICATION WAS FOUND ON RT WING LOWER SKIN FASTENER HOLE AT STR 9.5, NEAR BS 995. REPAIR IAW SR 3-3313325038 .
- [SDR IPXA3679543](https://openairdocs.org/sdr/IPXA3679543), Jul 26, 2013: TRANSMITTER. FAILED. T/E FLAP ASYM EICAS MESSAGE EMERGENCY DECLARED. R & R NR 8 FLAP POSITION TRANSMITTER IAW AMM 27-51-45-022-160.

## 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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