# N360UP: 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: 37946
- Year built: 2013
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: July 29, 2013
- Certificate issued: July 30, 2013
- Expires: July 31, 2029
- Mode S code: A40E1C
- 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=360UP
- Page: https://openairdocs.org/aircraft/N360UP

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 N360UP.

## FAA accident and incident reports

None matched to N360UP.

## Service difficulty reports (21)

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 IPXA2025101589962](https://openairdocs.org/sdr/IPXA2025101589962), Oct 4, 2025: ELEC CONNECTOR. FAULTED. RIGHT SIDE WINDOW EICAS DID NOT RESET. REPLACED POWER PLUG TERMINALS FOR J8 PER SWPM 20-30-12. WINDOW HEAT OPS CHECK GOOD PER AMM 30-41-00. THIS CLEARS THIS MEL
- [SDR IPXA2025100489962](https://openairdocs.org/sdr/IPXA2025100489962), Oct 4, 2025: CONNECTOR. SHORTED. RIGHT SIDE WINDOW EICAS DID NOT RESET. REVERSED DMP.PER FIM 30-41 TREE 803,PERFORMED WHCU BIT/VERIFY TEST, FOUND WINDOW 2 AMBER LIGHT COME ON. PER TABLE 101 AND
- [SDR IPXA2025080237986](https://openairdocs.org/sdr/IPXA2025080237986), Aug 1, 2025: FLOOR PANEL. DAMAGED. FOUND MAIN DECK FLOOR PANEL DAMAGE, P/N : 143T5876-105 PANEL NO : 231AFF. I.A.W AMM 25-57-02-004-029 AND AMM 25-57-05-004-001 REV.145. FABRICATE A NEW FLOOR PAN
- [SDR IPXA2025080518981](https://openairdocs.org/sdr/IPXA2025080518981), Jul 31, 2025: ANGLE. CRACKED. FOUND CRACK - ANGLE, BULK CGO COMPT CEILING AREA, STA 1577 LBL 74 INBD SIDE. .I.A.W AMM 53-01-06-000-801 REV.145 REMOVE MAIN DECK CARGO FLOOR PANEL , G.V.I AND 
- [SDR IPXA2025080519135](https://openairdocs.org/sdr/IPXA2025080519135), Jul 31, 2025: ANGLE. CRACKED. FOUND CRACK - ANGLE, BULK CGO COMPT CEILING AREA, STA 1577 LBL 74 OUTBD SIDE. I.A.W AMM 25-59-01-004-001 REV.145. REMOVED DAMAGE ANGLE I.A.W SRM 51-40-02-0G REV
- [SDR IPXA2025070324235](https://openairdocs.org/sdr/IPXA2025070324235), Jun 26, 2025: SKIN. DAMAGED. LOWER FWD CARGO DOOR SKIN DAMAGE. FABRICATED AND DRILLED UP REPAIR DOUBLER FOR AFT REPAIR PER EO-94209-PRELIM3 FIG 2. REPLACED DAMAGED SEAL RETAINERS IAW SRM 51
- [SDR IPXA2025070336769](https://openairdocs.org/sdr/IPXA2025070336769), Jun 26, 2025: STRINGER. DAMAGED. STRINGER S25R DAMAGED BETWEEN F.S.478 AND F.S 456 REPAIRED STRINGER ON BARCODE [T3F18E006XUTC] IAW EO-94202. INSTALLED 1EA STR CLIP AT 25R STA 456 IAW SRM 51-40
- [SDR IPXA2025070315311](https://openairdocs.org/sdr/IPXA2025070315311), Jun 25, 2025: SKIN. GOUGED. GOUGE FWD OF LOWER FWD CARGO DOOR EO-94202-REQ1 C/W.REMOVED GOUGE COMMON TO LWR FWD CARGO DOOR BY BLENDING IAW SRM 51-10-02.CUT OUT DAMAGE TO FUSELAGE SKIN AT S
- [SDR IPXA2023111542226](https://openairdocs.org/sdr/IPXA2023111542226), Oct 31, 2023: COVER. STUCK. *SUPPLEMENTAL SDR* PUSH TO SECURE LEVER DOOR COVER IS STUCK IN THE UP ++ REPLACED LEVEL DOOR LATCH COVER SPRING ASSY PER IPC 52-11-02-10A. OPS CHK NML PER MM 52
- [SDR IPXA2023103142226](https://openairdocs.org/sdr/IPXA2023103142226), Oct 31, 2023: UNKNOWN. UNKNOWN. PUSH TO SECURE LEVER DOOR COVER IS STUCK IN THE UP DEFERRED PER MEL 52-11-2 OPEN
- [SDR IPXA2023072614817](https://openairdocs.org/sdr/IPXA2023072614817), Jul 21, 2023: PANEL. DEFORMED. *MAJOR REPAIR* FAULT - FOUND MAIN DECK CARGO FLOOR PANEL DEFORM PANEL NO.252UFF, P/N: 146T5869-134 (REPAIR) FABRICATE A NEW FLOOR PANEL I.A.W. SREO-9693-REQ001 
- [SDR IPXA2022121088853](https://openairdocs.org/sdr/IPXA2022121088853), Dec 10, 2022: ENGINE. PILOT ERROR. RIGHT ENGINE FLAMED OUT AT FL 330, RAN CHECK LIST, DESCENDED TO FL 300, WAS ABLE TO RESTART AND CONTINUE NORMAL, OPS TO BOG. ENGINE FLAMES OUT BECAUSE OF IMPROP
- [SDR IPXA2021041968410](https://openairdocs.org/sdr/IPXA2021041968410), Apr 16, 2021: COVER. INOPERATIVE. CREW ENTRY DOOR CAPTURE LEVER COVER WILL NOT STAY FLUSH WITH SIDE PANELS. DEFERRED IAW MEL 52-11-2, COVER REMOVED PLACARD INSTALLED.R/R'D CREW ENTRY DOOR ACCESS
- [SDR IPXA2019081445600](https://openairdocs.org/sdr/IPXA2019081445600), Aug 3, 2019: SKIN SPLICE. CRACKED. INSPECTION TYPE:C3, CRACKED SKIN OF THE NR 6 SLAT NEAR ISS 300. REPAIRED IAW SRID: 3-4498800622 AND EO B767-5750-73621-A.
- [SDR IPXA2018071831738](https://openairdocs.org/sdr/IPXA2018071831738), Jul 13, 2018: INDICATOR. DEFECTIVE. INSPECTION TYPE:MX, FLIGHT DECK TRIM AIR VALVE POSITION INDICATOR INOP, TEMP CONTROL NORMAL. R&R FLIGHT DECK TRIM AIR VLV INDICATOR ASSY IAW AMM 21-64-01.
- [SDR IPXA2018010225061](https://openairdocs.org/sdr/IPXA2018010225061), Jan 2, 2018: LAMP. INOPERATIVE. INSPECTION TYPE: ASE, ENTRY CEILING EMERGENCY LIGHT INOPERATIVE. REPLACED THE LAMPS.
- [SDR IPXA2017092521993](https://openairdocs.org/sdr/IPXA2017092521993), Sep 24, 2017: FLOOR PANEL. DAMAGED. FLOOR PANEL DAMAGED. FABRICATED A NEW FLOOR PANEL IAW EO B767-56320-9693-I.
- [SDR IPXA2017080420136](https://openairdocs.org/sdr/IPXA2017080420136), Aug 4, 2017: ANTI-ICE SYSTEM. WARNING MESSAGE. WHILE USING EAI DURING CRUISE, AN EICAS DISPLAYED FOR RT ENGINE ANTI-ICE. QRH PROCEDURE WAS COMPLIED WITH, CORRECTING THE PROBLEM. EAI OPERATED NORMALLY. NO CUR
- [SDR IPXA2017071719355](https://openairdocs.org/sdr/IPXA2017071719355), Jul 16, 2017: FLOOR PANEL. DAMAGED. MAIIN DECK CARGO FLOOR PANEL HAS HOLE DAMAGE. FABRICATED A NEW FLOOR PANEL IAW EO B767-5320-9693-I.
- [SDR IPXA2015072191351](https://openairdocs.org/sdr/IPXA2015072191351), Jul 17, 2015: SKIN. DAMAGED. INSPECTION TYPE:C1, HOLE DAMAGE ON LT WING NR 6 SLAT T/E WEDGE AT ISS 332. REPAIR IAW SRM 57-43-02-2R-1, REPAIR 1 AND SRM 51-70-10-2R-3, REPAIR 3, REV 62.00.
- [SDR IPXA2014082084027](https://openairdocs.org/sdr/IPXA2014082084027), Aug 16, 2014: POWER SUPPLY. INOPERATIVE. EMERGENCY LIGHT TEST FAILED DURING FLIGHT CREW PREFLIGHT CHECK. R & R EMERGENCY LIGHT POWER PACK IAW AMM 33-51-01. AMM REV 80.00. OPS CHECKED SATISFACTORY.

## 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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