# N357UP: 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: 37876
- Year built: 2013
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: April 29, 2013
- Certificate issued: May 23, 2013
- Expires: May 31, 2029
- Mode S code: A4009E
- 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=357UP
- Page: https://openairdocs.org/aircraft/N357UP

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 N357UP.

## FAA accident and incident reports

None matched to N357UP.

## Service difficulty reports (25)

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 IPXA2026091418249](https://openairdocs.org/sdr/IPXA2026091418249), Sep 6, 2026: BLEED VALVE. FAULTED. ATB, LT ENG HPSOV EICAS MSG ON TAKEOFF ROLL. ACCOMPLISHED QRH PROCEDURE, BUT BLEED LIGHT REMAINED ILLUMINATE, UNABLE TO FLY IN FEINE CONDITION, RESULTED IN ATB 
- [SDR IPXA2026090618249](https://openairdocs.org/sdr/IPXA2026090618249), Sep 6, 2026: WARNING MESSAGE. ILLUMINATED. AIR TURN BACK, LT ENG HPSOV EICAS MSG ON TAKEOFF ROLL. ACCOMPLISHED QRH PROCEDURE, BUT BLEED LIGHT REMAINED ILLUMINATED. RESULTED IN ATB.
- [SDR IPXA2025031293400](https://openairdocs.org/sdr/IPXA2025031293400), Mar 12, 2025: FLOOR PANEL. DENTED. FAULT - FOUND MAIN DECK FLOOR PANEL WITH DENT DAMAGE, P/N: 143T5876-101 PANEL NO.232CFF. I.A.W AMM 25-57-02-004-029 AND AMM 25-57-05-004-001 AND AMM 25-57-06-00
- [SDR IPXA2025031293446](https://openairdocs.org/sdr/IPXA2025031293446), Mar 12, 2025: FLOOR PANEL. DENTED. FOUND MAIN DECK FLOOR PANEL WITH DENT DAMAGE, P/N: 143T5876-75 PANEL NO.231CFF.FABRICATED A NEW FLOOR PANEL I.A.W. SREO-9693-REQ001 REV.4.
- [SDR IPXA2025031293491](https://openairdocs.org/sdr/IPXA2025031293491), Mar 12, 2025: FLOOR PANEL. DENTED. FOUND MAIN DECK FLOOR PANEL WITH DENT DAMAGE, P/N: 143T5876-102 PANEL NO.231DFF.FABRICATED A NEW FLOOR PANEL I.A.W. SREO-9693-REQ001 REV.4.
- [SDR IPXA2025031293494](https://openairdocs.org/sdr/IPXA2025031293494), Mar 12, 2025: FLOOR PANEL. DENTED. FOUND MAIN DECK FLOOR PANEL WITH DENT DAMAGE, P/N: 143T5876-107 PANEL NO.232HFF.FABRICATED A NEW FLOOR PANEL I.A.W. SREO-9693-REQ001 REV.4.
- [SDR IPXA2025031293465](https://openairdocs.org/sdr/IPXA2025031293465), Mar 12, 2025: FLOOR PANEL. DENTED. FOUND MAIN DECK FLOOR PANEL WITH DENT DAMAGE, P/N: 143T5876-106 PANEL NO.231JFF.FABRICATED A NEW FLOOR PANEL I.A.W. SREO-9693-REQ001 REV.4.
- [SDR IPXA2025031293370](https://openairdocs.org/sdr/IPXA2025031293370), Mar 12, 2025: FLOOR PANEL. DENTED. FOUND MAIN DECK FLOOR PANEL WITH DENT DAMAGE, P/N: 143T5876-104 PANEL NO.231BFF.FABRICATED A NEW FLOOR PANEL I.A.W. SREO-9693-REQ001 REV.4.
- [SDR IPXA2025031296288](https://openairdocs.org/sdr/IPXA2025031296288), Mar 12, 2025: FLOOR PANEL. DENTED. FOUND MAIN DECK FLOOR PANEL WITH DENT DAMAGE, P/N: 143T5876-105 PANEL NO.231AFF (REPAIR). FABRICATE A NEW FLOOR PANEL I.A.W. SREO-9693-REQ001 REV.4. I.A.W AMM 5
- [SDR IPXA2025031293431](https://openairdocs.org/sdr/IPXA2025031293431), Mar 12, 2025: FLOOR PANEL. DENTED. FOUND MAIN DECK FLOOR PANEL WITH DENT DAMAGE, P/N: 143T5876-109 PANEL NO.232GFF.FABRICATED A NEW FLOOR PANEL I.A.W. SREO-9693-REQ001 REV.4.
- [SDR IPXA2025031293510](https://openairdocs.org/sdr/IPXA2025031293510), Mar 12, 2025: FLOOR PANEL. DENTED. FOUND MAIN DECK FLOOR PANEL WITH DENT DAMAGE, P/N: 143T5876-110 PANEL NO.231GFF.FABRICATED A NEW FLOOR PANEL I.A.W. SREO-9693-REQ001 REV.4.
- [SDR IPXA2025031293559](https://openairdocs.org/sdr/IPXA2025031293559), Mar 12, 2025: FLOOR PANEL. DENTED. FOUND MAIN DECK FLOOR PANEL WITH DENT DAMAGE, P/N: 143T5876-111 PANEL NO.232FFF.FABRICATED A NEW FLOOR PANEL I.A.W. SREO-9693-REQ001 REV.4.
- [SDR IPXA2025031293523](https://openairdocs.org/sdr/IPXA2025031293523), Mar 12, 2025: FLOOR PANEL. DENTED. FOUND MAIN DECK FLOOR PANEL WITH DENT DAMAGE, P/N: 143T5876-108 PANEL NO.231HFF.FABRICATED A NEW FLOOR PANEL I.A.W. SREO-9693-REQ001 REV.4.
- [SDR IPXA2023041192811](https://openairdocs.org/sdr/IPXA2023041192811), Apr 3, 2023: UNKNOWN. CRACKED. INSPECTION TYPE:C5CRACK ON CLIP (P/N:141T5146-16) OF M/D CGO FLOOR BEAM SUPPORT AT STA 246, LBL 49.INSTALL NEW PARTS I.A.W 767-300F SRM 51-40-02-0G REV. 85.01 A
- [SDR IPXA2023040992735](https://openairdocs.org/sdr/IPXA2023040992735), Apr 1, 2023: SKIN. UNKNOWN. INSPECTION TYPE:C5FUSELAGE DRAIN HOLES ADDITION AND INSPECTION AFT OF STA 1725.5 BETWEEN S-36L AND S-36R.PERFORM UPS EO B767-2740-82173-C APPX B.
- [SDR IPXA2022101987267](https://openairdocs.org/sdr/IPXA2022101987267), Oct 18, 2022: FLAP. NONE. INSPECTION TYPE:N/A**EMERGENCY DECLARED** WHEN CONFIGURING FOR LANDING GOT TE FLAP ASSYMETRY EICAS FOLLOWED CHECKLIST WITH FLAPS 20 FOR LANDINGNO HISTORY FOUND.
- [SDR IPXA2020082459445](https://openairdocs.org/sdr/IPXA2020082459445), Aug 23, 2020: WARNING LIGHT. FALSE INDICATION. ATB. FWD CARGO DOOR LIGHT ON IN FLIGHT. C/W FIM 52-71-00-815-807 PARA1, 11, & 22 IAW MM 52-33-00 / 501.
- [SDR IPXA2019041764186](https://openairdocs.org/sdr/IPXA2019041764186), Apr 6, 2019: FLOOR PANEL. DAMAGED. INSPECTION TYPE:C3DAMAGE ON M/D CARGO FLOOR PANEL AT STA 834 - STA 930, RBL 33 - RBL 55, PNL NO. 242FFF.FABRICATE THE REPLACEMENT FLOOR PANEL PER EO NO. B767-53
- [SDR IPXA2018020626260](https://openairdocs.org/sdr/IPXA2018020626260), Feb 5, 2018: FAN. FAILED. DURING FLIGHT, A SLIGHT ELECTRICAL SMOKE ODOR ACCOMPANIED BY FAN NOISE UNDER FWD INSTRUMENT PANEL. STATUS MESSAGE APPEARED. STAYED ON ALL WAY TO BLOCK. FWD EQUI
- [SDR IPXA2017050116650](https://openairdocs.org/sdr/IPXA2017050116650), Apr 30, 2017: BUSHING. DAMAGED. NR 2 ENGINE LT SIDE TURBINE CASE COOLING AIR TUBE HAS A SUPPORT LINK WITH DAMAGED BUSHING. REPLACED THE BUSHINGS IAW MM 75-24-03.
- [SDR IPXA2017042216351](https://openairdocs.org/sdr/IPXA2017042216351), Apr 16, 2017: FLOOR PANEL. DENTED. INSPECTION TYPE: C2, DENT ON MAIN DECK CARGO FLOOR PANEL BS 1300. FABRICATE A REPLACEMENT FLOOR PANEL IAW EO B767-5320-9693-I.
- [SDR IPXA2017032715582](https://openairdocs.org/sdr/IPXA2017032715582), Mar 25, 2017: BULB. BURNED OUT. FLT DECK EMERGENCY LIGHT SWITCH HAS A BURNED OUT BULB. REPLACED THE BULB, OPS CHECKED GOOD IAW AMM 33-13-00.
- [SDR IPXA2017022614432](https://openairdocs.org/sdr/IPXA2017022614432), Feb 26, 2017: FLOOR PANEL. DAMAGED. MAIN CARGO FLOOR PANEL DAMAGED. REPAIRED THE FLOOR PANEL IAW SRM 53-00-50-2R.
- [SDR IPXA2015070490823](https://openairdocs.org/sdr/IPXA2015070490823), Jul 4, 2015: FLOOR PANEL. DAMAGED. MAIN CARGO FLOOR PANEL DAMAGED. FABRICATED A NEW FLOOR PANEL IAW EO B767-5320-57907-A.
- [SDR IPXA2015052989519](https://openairdocs.org/sdr/IPXA2015052989519), May 24, 2015: SKIN. CRACKED. INSPECTION TYPE: C1, CRACK INDICATION WAS FOUND ON RT WING LOWER SKIN FASTENER HOLE AT STRINGER L9.5R REPAIRED IAW SRM 3-3290197682 AND EO B767-5730-57609-A.

## 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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