# N109FE: 2014 Boeing 767-3S2F

- Status: Valid registration
- Airframe: [Boeing 767-3S2F](https://openairdocs.org/model/boeing-767-3s2f) (registry code 138513F, 6 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: 42710
- Year built: 2014
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: November 14, 2014
- Certificate issued: December 2, 2014
- Expires: December 31, 2027
- Mode S code: A026A5
- Registered owner: [Federal Express Corp](https://openairdocs.org/faa-owner/FEDERAL%20EXPRESS%20CORP)
- Location: [Memphis, TN](https://openairdocs.org/faa-place/TN/Memphis)
- Owner type: Corporation
- Owner's area on the map: 35.0351° N, 89.9272° W: Placed by OpenAirDocs at the center of ZIP code 38118, within about 3 miles (OpenAirDocs). The owner's mailing address, not where the aircraft is based
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=109FE
- Page: https://openairdocs.org/aircraft/N109FE

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 767-3S2F)

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 N109FE.

## FAA accident and incident reports

None matched to N109FE.

## Service difficulty reports (26)

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 FDEA202607170944](https://openairdocs.org/sdr/FDEA202607170944), Jul 17, 2026: SKIN. DAMAGED. FUSELAGE SKIN EXTERNAL SURFACE FOUND 1EA LIGHTNING STRIKE AT STA1109 - STA1131 STR10L - STR11L. REPAIRED THE DAMAGED FUSELAGE SKIN AT STA1109-STA1131 STGR10L-ST
- [SDR FDEA202505100744](https://openairdocs.org/sdr/FDEA202505100744), May 10, 2025: SEAT TRACK. DAMAGED. REF TO WRI 25-50/1414, MAIN DECK SEAT TRACK BEAM RBL11 BROKEN AT STA610 - STA632 REPAIRED THE BROKEN SEAT TRACK BEAM RBL11 AT STA610 - STA632 PER B767 SRM53-00-
- [SDR FDEA202405030568](https://openairdocs.org/sdr/FDEA202405030568), May 3, 2024: FLOOR PANEL. DAMAGED. FLOOR PANEL DAMAGED STA.1197 13, BL-O HAS A 3.5 X 4.5 DENT IN UPPER SKIN NEAR EDGE OF PANEL. FABRICATED AND REPLACED FLOOR PANEL. FEDEX DRAWING SRZ-25-005 REV.R
- [SDR FDEA202403140290](https://openairdocs.org/sdr/FDEA202403140290), Mar 14, 2024: BATTERY PACK. NO TEST. ALL EMERGENCY LIGHTS WILL NOT ILLUMINATED. TEST FAILED. REMOVAL/INTALLATION OF BATTERY PACK ASSY ACCOMPLISHED IAW AMM 33-51-07-2, EMERGENCY LIGHTS TEST OK.
- [SDR FDEA202311161858](https://openairdocs.org/sdr/FDEA202311161858), Nov 16, 2023: RELAY. FAILED. ON APPROACH WITH LT AUTOPILOT ENGAGED. CLEARED ILS & ENGAGED APPROACH TILE. AUTOPILOT DISCONNECTED & CAPTAINS DISPLAY WENT BLANK. LOST STANDBY ATTITUDE INDICATO
- [SDR FDEA202209062208](https://openairdocs.org/sdr/FDEA202209062208), Sep 6, 2022: SKIN. DELAMINATED. LEFT WING OUTBOARD TRAILING EDGE FLAP (LOWER SURFACE) WITH DENT WS 825.2. LH WING OUTBOARD TRAILING EDGE FLAP LOWER SURFACE, WS 825.2 DENT WAS REPAIRED IAW SRM 
- [SDR FDEA202012093078](https://openairdocs.org/sdr/FDEA202012093078), Dec 9, 2020: SLAT SYSTEM. MALFUNCTIONED. PDIS 109 27-80 5999 09DEC20 DUB OPEN U LOGPAGES:371455. LEADING EDGE SLAT ASYM EICAS MESSAGE LIGHT WITH LEADING EDGE LIGHT FLAP GAUGE INDICATIONG BETWEEN 1 AND 
- [SDR FDEA202011202933](https://openairdocs.org/sdr/FDEA202011202933), Nov 20, 2020: FLOOR PANEL. DAMAGED. MAIN CABIN FLOOR PANEL 241FFF HAS TWO SMALL AREAS OF DAMAGE. REPAIRED FLOOR PANEL 241FFF, IAW B767 SRM 53-00-50-2R, PARA 4C.
- [SDR FDEA202011202932](https://openairdocs.org/sdr/FDEA202011202932), Nov 20, 2020: FLOOR PANEL. DAMAGED. MAIN CABIN FLOOR PANEL 241LFF HAS TWO SMALL AREAS OF DAMAGE. REPAIRED FLOOR PANEL 241LFF, IAW B767 SRM 53-00-50-2R, PARA 4C.
- [SDR FDEA202011202931](https://openairdocs.org/sdr/FDEA202011202931), Nov 20, 2020: FLOOR PANEL. DAMAGED. MAIN CABIN FLOOR PANEL 241ZFF HAS ONE SMALL AREA OF DAMAGE. REPAIRED FLOOR PANEL 241ZFF, IAW B767 SRM 53-00-50-2R, PARA 4C.
- [SDR FDEA202011202930](https://openairdocs.org/sdr/FDEA202011202930), Nov 20, 2020: FLOOR PANEL. DAMAGED. MAIN CABIN FLOOR PANEL 241XFF HAS A SMALL HOLE. REPAIRED FLOOR PANEL 241XFF, IAW B767 SRM 53-00-50-2R, PARA 4C.
- [SDR FDEA202011202929](https://openairdocs.org/sdr/FDEA202011202929), Nov 20, 2020: FLOOR PANEL. DAMAGED. MAIN CABIN FLOOR PANEL 241AFF HAS DAMAGE 2 PLACES. REPAIRED FLOOR PANEL 241AFF, IAW B767 SRM 53-00-50-2R, PARA 4E.
- [SDR FDEA202011202928](https://openairdocs.org/sdr/FDEA202011202928), Nov 20, 2020: FLOOR PANEL. DAMAGED. MAIN CABIN FLOOR PANEL 241DFF HAS PUNCTURE DAMAGE. REPAIRED FLOOR PANEL 241DFF, IAW B767 SRM 53-00-50-2R, PARA 4C.
- [SDR FDEA202011202927](https://openairdocs.org/sdr/FDEA202011202927), Nov 20, 2020: FLOOR PANEL. DAMAGED. MAIN CABIN FLOOR PANEL 241DFF IS DAMAGED AT STA 759 AND LBL 61.5. REPAIRED FLOOR PANEL 241DFF, IAW B767 SRM 53-00-50-2R, PARA 4E.
- [SDR FDEA202011202926](https://openairdocs.org/sdr/FDEA202011202926), Nov 20, 2020: FLOOR PANEL. DAMAGED. MAIN CABIN FLOOR PANEL 241AFF IS DAMAGED AT STA 752 AND LBL 7. REPAIRED FLOOR PANEL 241AFF, IAW B767 SRM 53-00-50-2R, PARA 4C.
- [SDR FDEA202011192908](https://openairdocs.org/sdr/FDEA202011192908), Nov 19, 2020: FLOOR PANEL. DELAMINATED. MAIN CABIN FLOOR PANEL 242CFF HAS SEVERAL AREAS OF DAMAGE. REPAIRED MAIN CABIN FLOOR PANEL 242CFF, IAW B767 SRM 53-00-50-2R FIG 201 AND 51-30-10-0G. MAJOR REPAI
- [SDR FDEA202011192907](https://openairdocs.org/sdr/FDEA202011192907), Nov 19, 2020: FLOOR PANEL. DELAMINATED. MAIN CABIN FLOOR PANEL 242SFF HAS SEVERAL AREAS OF DAMAGE. REPAIRED MAIN CABIN FLOOR PANEL 242SFF, IAW B767 SRM: 53-00-50-2R FIG 201. MAJOR REPAIR.
- [SDR FDEA202011192906](https://openairdocs.org/sdr/FDEA202011192906), Nov 19, 2020: FLOOR PANEL. DELAMINATED. MAIN CABIN FLOOR PANEL 241WFF HAS SEVERAL AREAS OF DAMAGE. REPAIRED MAIN CABIN FLOOR PANEL 241WFF, IAW B767 SRM 53-00-50-2R FIG 201. MAJOR REPAIR.
- [SDR FDEA202011192902](https://openairdocs.org/sdr/FDEA202011192902), Nov 19, 2020: SKIN. PUNCTURED. RT WING NR 7 SPOILER UPPER SURFACE IS PUNCTURED. REPAIRED RT WING NR 7 SPOILER UPPER SURFACE, IAW B767 SRM 57-70-01-2R FIG 201, SRM 51-70-017-0G PARA 4B FIG 24.
- [SDR FDEA202011172894](https://openairdocs.org/sdr/FDEA202011172894), Nov 17, 2020: CLOSEOUT PANEL. CRACKED. LEFT WING NR 5 SLAT LOWER COMPOSITE SEAL CRACKED REPAIRED LEFT WING NR 5 CLOSE OUT PANEL, IAW B767-SRM 57-43-01-2R DETAIL II FIG 201 TABLE 1 AND 51-70-07-0G PAR
- [SDR FDEA202011162880](https://openairdocs.org/sdr/FDEA202011162880), Nov 16, 2020: WEDGE. GOUGED. LT WING, NR 5 SLAT WEDGE, INNER SURFACE, GOUGE TOWARD OUTBOARD END OF SLAT. REPAIRED 2 AREAS ON LT WING NR 5 SLAT LOWER SURFACE AT OUTBOARD END, IAW B767 SRM 57
- [SDR FDEA202011142859](https://openairdocs.org/sdr/FDEA202011142859), Nov 14, 2020: FLOORBEAM. CRACKED. RIGHT AFT MAIN FLOOR BEAM SPLICE AT STA 1572, AT THE UPPER OUTBOARD FLOOR BEAM, IS CRACKED. REMOVED AND REPLACED SPLICE ANGLE, IAW BAC DWG 146T5650, REV C AND B
- [SDR FDEA202011142858](https://openairdocs.org/sdr/FDEA202011142858), Nov 14, 2020: FLOORBEAM. CRACKED. LEFT AFT MAIN FLOOR BEAM SPLICE AT STA 1572, AT THE UPPER OUTBOARD FLOOR BEAM, IS CRACKED. REMOVED AND REPLACED SPLICE ANGLE, IAW BAC DWG 146T5650, REV C AND B7
- [SDR FDEA202011142856](https://openairdocs.org/sdr/FDEA202011142856), Nov 14, 2020: FLOOR PANEL. DAMAGED. MAIN CARGO COMPARTMENT AT STA 1250 APPROXIMATELY AND LBL 59 FLOOR BOARD DAMAGED. REPAIRED MAIN CABIN FLOOR PANEL STA 1250 LBL 59, IAW B767 SRM 53-00-50-2R PARA 
- [SDR FDEA201902180445](https://openairdocs.org/sdr/FDEA201902180445), Feb 18, 2019: SKIN. DENTED. LEFT WING OTBD FLAP HAS DENT 11 INCHES FROM INBD EDGE. REPAIRED LEFT WING OUTBD FLAP LOWER SKIN BY REMOVING DAMAGED AREA AND POTTING DAMAGE AND FABRICATING AND 
- [SDR FDEA201601030011](https://openairdocs.org/sdr/FDEA201601030011), Jan 3, 2016: LIGHT. INOPERATIVE. AFTER LOWERING THE LG ON APPROACH, LT MAIN GEAR DID NOT ILLUMINATE. GO AROUND ACCOMPLISHED WITH GEAR DOWN. LIGHT TEST ACCOMPLISHED & BOTH BULBS WERE INOPERATIVE

## 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 767-3S2F aircraft: https://openairdocs.org/model/boeing-767-3s2f/aircraft.md
- The GE CF6-80C2B6F engine: https://openairdocs.org/engine/ge-cf6-80c2b6f.md

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