# N125FE: 2015 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: 42717
- Year built: 2015
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: August 11, 2015
- Certificate issued: August 28, 2015
- Expires: August 31, 2028
- Mode S code: A066C7
- 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=125FE
- Page: https://openairdocs.org/aircraft/N125FE

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 N125FE.

## FAA accident and incident reports

None matched to N125FE.

## 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 FDEA202608211212](https://openairdocs.org/sdr/FDEA202608211212), Aug 21, 2026: SKIN. DENTED. DURING INSPECTION FOUND EVIDENCE OF STRIKE AT BS 368, STRINGER 5R, DOOR STA 108 3/4" INBD OF STR 5R, REPAIRED SKIN USING COMPLING WITH EA.H-5330-T0388341P1 (PAR
- [SDR FDEA202608201196](https://openairdocs.org/sdr/FDEA202608201196), Aug 20, 2026: PANEL. DELAMINATED. RIGHT WING UPPER L/E PANEL ABOVE PYLON AT ISS 337.60 HAS EROSION ACROSS L/E, WITH NUMEROUS FASTENER HEADS PULLING THROUGH SKIN. ALSO FOUND SEVERAL DOUBLE DRILLE
- [SDR FDEA202608061090](https://openairdocs.org/sdr/FDEA202608061090), Aug 6, 2026: SKIN. DENTED. #4 SLAT T/E WEDGE UPPER SURFACE, 22" FROM THE OUTBD END AND 7" FROM THE AFT EDGE HAS SMALL DENT.MWT, REPAIRED DENT ON # 4 SLAT ON UPPER SURFACE 22" FROM OB EDGE
- [SDR FDEA202608041083](https://openairdocs.org/sdr/FDEA202608041083), Aug 4, 2026: SKIN. DENTED. RIGHT WING NR 8 SLAT TOP SIDE APPROX IN THE MIDDLE HAS A DENT. REPAIRED RT WING NR 8 SLAT TRAILING EDGE WEDGE TOP SKIN SURFACE AT WS.465.65 IAW SRM: 57-43-02-2R
- [SDR FDEA202608011075](https://openairdocs.org/sdr/FDEA202608011075), Aug 1, 2026: SKIN. DENTED. RIGHT WING, NR 7 SLAT, UPPER SURFACE T/E WEDGE HAS 2EA DENTS APPROX 28" FROM OUTBD EDGE. REPAIRED DENTS ON RT WING, NR 7 SLAT, UPPER SURFACE T/E WEDGE AT ISS 31
- [SDR FDEA202509141704](https://openairdocs.org/sdr/FDEA202509141704), Sep 14, 2025: WARNING MESSAGE. ILLUMINATED. ENROUTE MAIN CARGO DOOR LIGHT ILLUMINATED. ON DESCENT PASSING 22K, LIGHT WENT OUT. RELEASED FOR SERVICE PER MEL : 52-71-01-02 CATEGORY : C. MAIN DECK CARGO DOOR
- [SDR FDEA202508171491](https://openairdocs.org/sdr/FDEA202508171491), Aug 17, 2025: ESCAPE ROPE. DISLODGED. ESCAPE ROPE FROM MAIN ENTRY DOOR DISLODGED FROM FRAME AMM 25 61-02-2 ESCAPE ROPE REPOSITIONED IN YOUR PLACE A/C OK FOR SVC.
- [SDR FDEA202507031111](https://openairdocs.org/sdr/FDEA202507031111), Jul 3, 2025: SLAT SYSTEM. MALFUNCTIONED. LE SLAT DISAG ON RAISING FLAPS FROM 1 TO UP. RAN QRH. DECLARED EMERGENCY, UPON ARRIVAL. RECONFIGURED SLAT/FLAP SYS TO NORMAL OPS IAW MM 27-81-00-5. PERFORMED FS
- [SDR FDEA202408131120](https://openairdocs.org/sdr/FDEA202408131120), Aug 13, 2024: FITTING. CRACKED. MAIN CARGO COMPARTMENT BETWEEN STA 977/999 AND RBL 11/33 FLOOR FITTING BROKEN. MAIN CARGO COMPARTMENT BTWN STA 977/999 AND RBL 11/33 FLOOR FITTING WAS REPLACED 
- [SDR FDEA202408101108](https://openairdocs.org/sdr/FDEA202408101108), Aug 10, 2024: SKIN. BURNED. RH WING, OUTBOARD AILERON BETWEEN WBL 910 AND WBL 890 WITH TWO LIGHTNING STRIKE. RH WING, OUTBOARD AILERON BTW WBL 910 AND WBL 890 WAS REPAIRED IAW B767 SRM 57-
- [SDR FDEA202408051086](https://openairdocs.org/sdr/FDEA202408051086), Aug 5, 2024: FLOOR PANEL. DENTED. MAIN DECK CARGO COMPARTMENT, FLOOR PANEL 251KFF WITH SEVERAL DENTS. MAIN DECK CARGO, FLOOR PANEL 251KFF WAS REPAIRED I.A.W. B767 SRM 53-00-50-2R PAR. 4.B FIG. 2
- [SDR FDEA202408051085](https://openairdocs.org/sdr/FDEA202408051085), Aug 5, 2024: FLOOR PANEL. CRACKED. MAIN DECK CARGO COMPARTMENT, FLOOR PANEL 241WFF WITH A PUNCTURE. MAIN DECK CARGO, FLOOR PANEL 241WFF WAS REPAIRED I.A.W. B767 SRM 53-00-50-2R PAR 4.B FIG. 201 S
- [SDR FDEA202408051084](https://openairdocs.org/sdr/FDEA202408051084), Aug 5, 2024: SKIN. DENTED. SLAT 11, EXTERNAL SURFACE, UPPER WEDGE WITH DENT NEXT TO INB FRAME. SLAT 11, EXTERNAL SURFACE, UPPER WEDGE WITH DENT NEXT TO INB FRAME WAS REPAIRED IAW B767 SRM
- [SDR FDEA202307081186](https://openairdocs.org/sdr/FDEA202307081186), Jul 8, 2023: FORMER. FAILED. NOSE FORMER ANGLE CRACKED AT RIGHT WING OSS 565. VISUALLY INSPECTED FORMER AT FLE OSS 565 AND REPLACED FOMRER WITH ANGLE USING FEDEX DRW B67-57-002 / AND -003 R
- [SDR FDEA202307081185](https://openairdocs.org/sdr/FDEA202307081185), Jul 8, 2023: FORMER. FAILED. NOSE FORMER ANGLE CRACKED AT THE RIGHT WING OSS 499.6. PER EA H-5720-T0367172 REV A VISUALLY INSPECTED FORMER AT FLE OSS 499.603 AND REPLACED FOMRER WITH ANGLE 
- [SDR FDEA202211172811](https://openairdocs.org/sdr/FDEA202211172811), Nov 17, 2022: SKIN. WORN. RH WING SLAT #8 INNER SKIN WEDGE AREA TWO PREVIUS REPAIR WITH WEAR. RH WING SLAT #8 T/E WEDGE INNER SKIN, ONE PREVIOUS REPAIR WAS REPLACED AND ONE FILLER WAS RE
- [SDR FDEA202211172810](https://openairdocs.org/sdr/FDEA202211172810), Nov 17, 2022: SKIN. WORN. LEFT WING OUTBOARD SLAT NO 5 TRAILING EDGE WITH WEAR (LOWER SURFACE). LEFT WING OUTBOARD SLAT NO 5 TRAILING EDGE WEDGE WAS REPAIRED IAW SRM 51-70-10-2R REPAIR 4
- [SDR FDEA202007011419](https://openairdocs.org/sdr/FDEA202007011419), Jul 1, 2020: SLAT. CHAFED. RW #8 SLAT TE GOUGED TWO PLACES REPAIRED #8 SLAT TRAILING EDGE WEDGE AT TWO EACH LOCATIONS BY BONDING REPAIR IAW B767 SRM 57-43-02-0I, 57-43-02-2R REPAIR 1 AND 
- [SDR FDEA2020070811419](https://openairdocs.org/sdr/FDEA2020070811419), Jul 1, 2020: WEDGE. CHAFED. RW #8 SLAT TE GOUGED TWO PLACES REPAIRED #8 SLAT TRAILING EDGE WEDGE AT TWO EACH LOCATIONS BY BONDING REPAIR IAW B767 SRM 57-43-02-0I, 57-43-02-2R REPAIR 1 AND 
- [SDR FDEA2020070211419](https://openairdocs.org/sdr/FDEA2020070211419), Jul 1, 2020: WEDGE. GOUGED. RT WING NR 8 SLAT TE GOUGED TWO PLACES. REPAIRED NR 8 SLAT TRAILING EDGE WEDGE AT TWO EACH LOCATIONS BY BONDING REPAIR IAW SRM 57-43-02-0I, 57-43-02-2R REPAIR 1
- [SDR FDEA2019111522939](https://openairdocs.org/sdr/FDEA2019111522939), Nov 12, 2019: BRAKE. DAMAGED. PDIS 125 32-43 4006 12NOV19 CDG OPEN U LOGPAGES:2841209 ON LANDING ROLLOUT APPLIED BRAKES MANUALLY FELT VIBRATION. ON SHUTDOWN BRAKE TEMP LIGHT IS ON BRAKE TEMP
- [SDR FDEA2018081752047](https://openairdocs.org/sdr/FDEA2018081752047), Aug 15, 2018: SENSOR. FOD. 1.25 HOURS INTO FLIGHT, RECEIVED A MAIN CARGO EICAS. COMPLIED WITH QRH. INDICATOR WENT OUT. DECENDING THRU FL220. PRESSURIZATION NORMAL THOUGHOUT. FOUND DEBRIS 
- [SDR FDEA201806191544](https://openairdocs.org/sdr/FDEA201806191544), Jun 19, 2018: SMOKE BARRIER. DAMAGED. CREW REST SMOKE CURTAIN HAS HOLE IN IN LEFT PLASTIC WINDOW. INSTALLED NEW CURTAIN PER IPC 26-29-01-01.
- [SDR FDEA201607312683](https://openairdocs.org/sdr/FDEA201607312683), Jul 31, 2016: UNKNOWN. MALFUNCTIONED. FLAPS STOPPED BETWEEN 20 AND 25 FLAPS ON INITIAL CONFIGURATION FOR LANDING WITH T/E FLAP DISAGREE. COMPLIED WITH QRH FOR REF FLAP 20 LANDING. VERIFIED OVERLOAD 
- [SDR FDEA201509132855](https://openairdocs.org/sdr/FDEA201509132855), Sep 13, 2015: CONTROLLER. MALFUNCTIONED. AT FL 360 GOT A CABIN ALTITUDE MASTER WARNING. CABIN WAS SHOWING JUST OVER 10,000 FT WITH A 200 FT PER MIN CLIMB. WE WENT TO AUTO 2 BUT CABIN CONTINUED TO CLIMB

## 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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