# N121FE: 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: 43545
- Year built: 2015
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: May 31, 2015
- Certificate issued: June 1, 2015
- Expires: June 30, 2028
- Mode S code: A057EB
- 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=121FE
- Page: https://openairdocs.org/aircraft/N121FE

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 N121FE.

## FAA accident and incident reports

None matched to N121FE.

## Service difficulty reports (29)

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 FDEA202602250279](https://openairdocs.org/sdr/FDEA202602250279), Feb 25, 2026: INDICATOR. LEAKING. LOST HYDRAULIC SYSTEM NR 1 QTY IN CRUISE FL370. AMM: 29-11-17-4 JRH: CHAP 6 AMM: 12-12-01-3 CONFIRMED HYD LT EDP & LT ELECT PUMP SWITCHED IS IN OFF POSITION IAW
- [SDR FDEA202504080583](https://openairdocs.org/sdr/FDEA202504080583), Apr 8, 2025: STRINGER. DAMAGED. COMPLY WITH FEDEX EO:H-5310-E0365800 A P2, TITLE: FUSELAGE - MAINFRAME - INSTALLATION OF SPLICE FITTINGS ON STRINGERS S-20L AND S-20R AT STA 1506,STA 1530,AND S
- [SDR FDEA202504080582](https://openairdocs.org/sdr/FDEA202504080582), Apr 8, 2025: STRINGER. DAMAGED. COMPLY WITH FEDEX EO:H-5310-E0365800 A P1, TITLE:FUSELAGE - MAINFRAME - INSTALLATION OF SPLICE FITTINGS ON STRINGERS S-20L AND S-20R AT STA 1506,STA 1530,AND ST
- [SDR FDEA202503300538](https://openairdocs.org/sdr/FDEA202503300538), Mar 30, 2025: FLOORBEAM. DAMAGED. THE BULK CARGO COMPARTMENT FLOOR BEAM 1EA HOLE WAS FOUND AT RBL29.34 STA1480 - STA1502 REPLACED THE BULK CARGO COMPARTMENT STRINGER RBL29.34 AT STA1480 - STA150
- [SDR FDEA202503280529](https://openairdocs.org/sdr/FDEA202503280529), Mar 28, 2025: FLOORBEAM. CRACKED. BULK CARGO COMPARTMENT FLOOR BEAM LBL8.73 CRACKED AT STA1395 - STA1417 REPLACED THE CRACKED BULK CARGO COMPARTMENT FLOOR BEAM LBL8.73 AT STA1395 - STA1417 PER D
- [SDR FDEA202503280528](https://openairdocs.org/sdr/FDEA202503280528), Mar 28, 2025: FLOORBEAM. CRACKED. BULK CARGO COMPARTMENT FLOOR BEAM LBL15.48 CRACKED AT STA1395 - STA1417 REPLACED THE CRACKED BULK CARGO COMPARTMENT FLOOR BEAM LBL15.48 AT STA1395 - STA1417 PER
- [SDR FDEA202503280527](https://openairdocs.org/sdr/FDEA202503280527), Mar 28, 2025: FLOORBEAM. CRACKED. BULK CARGO COMPARTMENT FLOOR BEAM RBL15.48 CRACKED AT STA1439. REPLACED THE CRACKED BULK CARGO COMPARTMENT TRANSITION SUPPORT RBL15.48 AT STA1439 PER B767 SRM51
- [SDR FDEA202405080614](https://openairdocs.org/sdr/FDEA202405080614), May 8, 2024: TEE FITTING. CRACKED. CABIN FLOOR BOARD SUPPORT LOWER SUPPORT "T" SEVERED, STA 246-20, 6" RIGHT OF CENTER. MARKED WITH DOT. REPLACED "T" FITTING FABRICATED AND PROCESSED CABIN FLOORB
- [SDR FDEA202403170303](https://openairdocs.org/sdr/FDEA202403170303), Mar 17, 2024: WINDOW. LEAKING. AT CRUISE FL 340, VERT AUDIBLE SQUEAL AROUND L1 WINDOW. PERFORMED THE EXCESSIVE PRESSURE LEAKAGE CHECK OF THE FUSELAGE, TOOK THE PRESSURIZATION UP TO 4.0 PSI AN
- [SDR FDEA202402290224](https://openairdocs.org/sdr/FDEA202402290224), Feb 29, 2024: UNKNOWN. ODOR. ON DESCENT FROM 10,000 FT TO TOUCHDOWN THERE WAS A STRONG ODOR OF DIRTY SOCKS THAT GRADUALLY TURNED INTO A SWEETER SMELL UPON LANDING. POSSIBLE FUME EVENT. AS S
- [SDR FDEA202308161451](https://openairdocs.org/sdr/FDEA202308161451), Aug 16, 2023: PANEL. CRACKED. PANEL PN 146T5869-152 CRACKED FABRICATE NEW PANEL 146T5869-152 (252YFF) REF FEDEX DWG SRZ-25-005 REV R.
- [SDR FDEA202304120627](https://openairdocs.org/sdr/FDEA202304120627), Apr 12, 2023: SEAL. CRACKED. RH WING LE SKIN INTERNAL SPLICE STRAP IS CRACKED AT APPROX WS 508 REMOVED AND REPLACED RIGHT WING SEAL STRIP IAW B767 SRM 51-40-02 AND BAC DWG 114T2800, SHEET 6
- [SDR FDEA202304110623](https://openairdocs.org/sdr/FDEA202304110623), Apr 11, 2023: SEAL. CRACKED. L/H WING L/E SKIN INTERNAL SPLICE STRAP IS CRACKED AT APPROX WS 508 REMOVED AND REPLACED LEADING EDGE SEAL STRIP IAW B767 SRM 51-40-02 AND BAC DWG 114T2800, SHE
- [SDR FDEA202304100607](https://openairdocs.org/sdr/FDEA202304100607), Apr 10, 2023: ANGLE. CRACKED. MAIN CABIN LOWER RH FLOOR SUPPORT IS CRACKED AT APPROX STA 1580, RBL 78 OTBD ATTACH ANGLE REMOVED & REPLACED FLOOR SUPPORT ATTACH ANGLE IAW B767 SRM 51-40-02 & 
- [SDR FDEA202304100606](https://openairdocs.org/sdr/FDEA202304100606), Apr 10, 2023: ANGLE. CRACKED. MAIN CABIN LOWER RH FLOOR SUPPORT IS CRACKED AT APPROX STA 1580, RBL 78 REMOVED & REPLACED FLOOR SUPPORT ATTACH ANGLE IAW B767 SRM 51-40-02 & BAC DWG 146T5650, 
- [SDR FDEA202304100605](https://openairdocs.org/sdr/FDEA202304100605), Apr 10, 2023: ANGLE. CRACKED. MAIN CABIN LOWER LH FLOOR SUPPORT IS CRACKED AT APPROX STA 1580, LBL 78 REMOVED & REPLACED FLOOR SUPPORT ATTACH ANGLE IAW B767 SRM 51-40-02 & BAC DWG 146T5650, 
- [SDR FDEA202304100604](https://openairdocs.org/sdr/FDEA202304100604), Apr 10, 2023: ANGLE. CRACKED. MAIN CABIN LOWER LH FLOOR SUPPORT IS CRACKED AT APPROX STA 1580, LBL 78, OTBD ATTACH ANGLE REMOVED & REPLACED FLOOR SUPPORT ATTACH ANGLE IAW B767 SRM 51-40-02 A
- [SDR FDEA202304070587](https://openairdocs.org/sdr/FDEA202304070587), Apr 7, 2023: FLAP. DELAMINATED. RH WING I/B FLAP AFT FLAP LOWER SKIN HAS A DENT WITH SUBSTRATE BREAK THROUGH. REPAIRED RH I/B AFT FLAP ON THE LOWER SKIN IAW B767 SRM 57-53-01-2R AND 51-70-10-2
- [SDR FDEA202304070586](https://openairdocs.org/sdr/FDEA202304070586), Apr 7, 2023: SPOILER. DELAMINATED. LH WING #6 SPOILER LOWER SURFACE IS PUNCTURED THROUGH BOTH THE UPPER AND LOWER SURFACES APPROX 12" O/B OF THE I/B EDGE. REPAIRED LH WING #6 SPOILER UPP AND LOWE
- [SDR FDEA202304060577](https://openairdocs.org/sdr/FDEA202304060577), Apr 6, 2023: WEB. CRACKED. R/H WING L/E SUBSTRUCTRE BULLNOSE WEB IS CRACKED IN THE LOWER BEND RADIUS JUST FWD OF THE FUELING SVC PANEL. REPAIRED R/H WING L/E SUBSTRUCTURE BULLNOSE WEB IAW
- [SDR FDEA202304060576](https://openairdocs.org/sdr/FDEA202304060576), Apr 6, 2023: ATTACH ANGLE. CRACKED. #1 PYLON AFT FAIRING, 2EA FRAME ATTACH CLIPS ARE CRACKED ON INBD AND OUTBD SIDES AT NAC STA 376 REMOVED AND REPLACED CLIPS IAW B767 SRM 51-40-02 AND BAC DWG 313
- [SDR FDEA202304060574](https://openairdocs.org/sdr/FDEA202304060574), Apr 6, 2023: WEB. CRACKED. L/H WING L/E BULLNOSE INTERNAL WEB IS CRACKED IN THE LOWER RADIUS JUST FWD OF THE FUELING SVC PANEL
- [SDR FDEA202304030555](https://openairdocs.org/sdr/FDEA202304030555), Apr 3, 2023: UNKNOWN. UNKNOWN. #1 PYLON AFT FAIRING MID-FRAME IS CRACKED IN UPPER INBD CORNER AT APPROX NAC STA 330. REPAIRED #1 PYLON AFT FAIRING MID FRAME IAW B767-300 SRM 54-52-71-2R & BAC
- [SDR FDEA202304030554](https://openairdocs.org/sdr/FDEA202304030554), Apr 3, 2023: UNKNOWN. CRACKED. #2 PYLON, OB SIDE, FRAME JUST AFT OF HYDRO BAY DOOR HAS A CRACKED ANGLE REMOVED AND REPLACED CLIP IAW B767 SRM 51-40-02 & BAC DWG 313T2303, SHEET 146, REV-
- [SDR FDEA202101200158](https://openairdocs.org/sdr/FDEA202101200158), Jan 20, 2021: ACTUATOR. MALFUNCTIONED. GEAR DISAGREE / GEAR DOORS AFTER HANDLE RAISED. FOUND RIGHT GEAR FORWARD DRAG STRUT ACTUATOR ROD END PULLED OUT OF SHAFT. INSPECTED AREA SURROUNDING ACT. FOR DA
- [SDR FDEA202011132837](https://openairdocs.org/sdr/FDEA202011132837), Nov 13, 2020: WARNING MESSAGE. FALSE ACTIVATION. PDIS 121 27-80 5016 13NOV20 BKK FACT U. LEADING EDGE SLAT MESSAGE WHEN FLAP 25 SELECTED PRIOR TO LANDING GO AROUND EXECUTED EMERGENCY DECLARED. QRH COMPLIED WIT
- [SDR FDEA201910172682](https://openairdocs.org/sdr/FDEA201910172682), Oct 17, 2019: SKIN. DENTED. LEFT WING O/B FLAP LOWER SKIN HAS NUMEROUS DENTS. REPAIRED LEFT WING O/B FLAP LOWER SKIN DENTS IAW B767 SRM: 57-53-01-01A, 51-70-00-2R, 51-70-07-2R-G, 51-70-07-
- [SDR FDEA201910142641](https://openairdocs.org/sdr/FDEA201910142641), Oct 14, 2019: SLEEVE. CORRODED. NR 2 ENGINE, OUTBOARD THRUST REVERSER OUTER SHELL, INNER SURFACE, LOWER AREA CORRODED. REMOVED AND REPLACED THE NR 2 ENGINE OUTBOARD THRUST REVERSER SLEEVE IAW 
- [SDR FDEA201601240311](https://openairdocs.org/sdr/FDEA201601240311), Jan 24, 2016: SKIN. DENTED. LEFT FUSELAGE, APPROX STATION 766.5, HAS A DENT OUT OF LIMITS. REPAIRED IAW SRM 53-00-01 REPAIR 12 EA H-5330-T0321872 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 767-3S2F 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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