# N132FE: 2016 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: 42721
- Year built: 2016
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: April 18, 2016
- Certificate issued: June 3, 2016
- Expires: June 30, 2029
- Mode S code: A08321
- 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=132FE
- Page: https://openairdocs.org/aircraft/N132FE

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 N132FE.

## FAA accident and incident reports

None matched to N132FE.

## Service difficulty reports (31)

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 FDEA202610031473](https://openairdocs.org/sdr/FDEA202610031473), Oct 3, 2026: UNKNOWN. ODOR. OIL SMELL IN COCKPIT FROM TAKEOFF AT VTBS. DID NOT NOTICE ANY SMELL AT ALTITUDE IN CRUISE. DESCENDING INTO WMKP AT ABOUT 14000 SMELL RETURNED. COMPLIED WITH MTS
- [SDR FDEA202609121330](https://openairdocs.org/sdr/FDEA202609121330), Sep 12, 2026: UNKNOWN. ODOR. ACRID FUMES IN COCKPIT DURING CLIMB OUT AND DESCENDING THROUGH 14,000 . PERFORMED AIR CONDITIONING SYSTEM OIL SMOKE/FUME CONTAMINATION REMOVAL PER AMM 21-00-21-
- [SDR FDEA202509191747](https://openairdocs.org/sdr/FDEA202509191747), Sep 19, 2025: FLOOR PANEL. CRACKED. PERFORATED FLOOR PANEL 241KFF IN MDC SECTION 45 FLOOR PANEL 241KFF IN MDC SECTION 45 WAS REPAIRED IAW 53-00-50-2R PAR 4-B FIG .201 SHEET 2 REV.92 APR 15,2025
- [SDR FDEA202509191746](https://openairdocs.org/sdr/FDEA202509191746), Sep 19, 2025: FLOOR PANEL. CRACKED. BROKEN FIBERS ON FLOOR PANEL 251HFF IN MDC FLOOR PANEL 251HFF IN MDC WAS REPAIRED IAW SRM 53-00-50-2R PAR 4-B FIG.201 SHEET 2 REV. 92 APR15,2025
- [SDR FDEA202509191745](https://openairdocs.org/sdr/FDEA202509191745), Sep 19, 2025: FLOOR PANEL. CRACKED. BROKEN FIBERS ON FLOOR PANEL 251SFF IN MDC FLOOR PANEL 251SFF IN MDC WAS REPAIRED IAW SRM 53.00.50.2R PAR 4.B FIG. 201 SHEET 2 REV 92 APR 15,2025
- [SDR FDEA202509191744](https://openairdocs.org/sdr/FDEA202509191744), Sep 19, 2025: FLOOR PANEL. CRACKED. PERFORATED FLOOR PANEL 251QFF IN MDC FLOOR PANEL 251QFF IN MDC WAS REPAIRED IAW SRM 53-00-50-2R PAR4.B FIG 201 SHEET 2 REV 92 APR 15,2025
- [SDR FDEA202509191743](https://openairdocs.org/sdr/FDEA202509191743), Sep 19, 2025: FLOOR PANEL. CRACKED. PERFORATED FLOOR PANEL 251KFF IN MDC FLOOR PANEL 251KFF IN MDC WAS REPAIRED IAW SRM 53.00.50.2R PAR 4.B FIG 201 SHEET 2 REV. 92 APR 15,2025
- [SDR FDEA202509191742](https://openairdocs.org/sdr/FDEA202509191742), Sep 19, 2025: FLOOR PANEL. CRACKED. PERFORATED FLOOR PANEL 241EFF IN MDC SECTION 45 FLOOR PANEL 241EFF IN MDC SECTION 45 WAS REPAIRED IAW SRM 53.00.50.2R PAR. 4.B FIG.201 SHEET 2 REV 92 APR 15,202
- [SDR FDEA202412241830](https://openairdocs.org/sdr/FDEA202412241830), Dec 24, 2024: SENSOR. FAULTED. SHORTLY AFTER REACHING TOP OF CLIMB, FL360, MAIN CARGO DOOR EICAS MESSAGE ILLUMINATED ALONG WITH ASSOCIATED CARGO DOOR DISCRETE LIGHT. WE ACCOMPLISHED THE CHECK
- [SDR FDEA202310041706](https://openairdocs.org/sdr/FDEA202310041706), Oct 4, 2023: FLOOR PANEL. DENTED. MDC FLOOR PANEL 221DFF WITH SEVERAL DENTS. MDC FLOOR PANEL 221DFF WAS REPAIRED IAW B767 SRM 53-00-50-2R PAR 4B FIG 201 REV 87 AUG 15 2023
- [SDR FDEA202310041705](https://openairdocs.org/sdr/FDEA202310041705), Oct 4, 2023: FLOOR PANEL. DENTED. MDC FLOOR PANEL 222CFF WITH SEVERAL DENTS. MDC FLOOR PANEL 222CFF WAS REPAIRED IAW B767 SRM 53-00-50-2R PAR 4B FIG 201 REV 87 AUG 15 2023
- [SDR FDEA202310041704](https://openairdocs.org/sdr/FDEA202310041704), Oct 4, 2023: FLOOR PANEL. DENTED. MDC FLOOR PANEL 222BFF WITH SEVERAL DENTS. MDC FLOOR PANEL 222BFF WAS REPAIRED IAW B767 SRM 53-00-50-2R PAR 4B FIG 201 REV 87 AUG 15 2023
- [SDR FDEA202310041703](https://openairdocs.org/sdr/FDEA202310041703), Oct 4, 2023: FLOOR PANEL. DENTED. MDC FLOOR PANEL 221CFF WITH SEVERAL DENTS MDC FLOOR PANEL 221CFF WAS REPAIRED IAW B767 SRM 53-00-50-2R PAR 4B FIG 201. REV 87 AUG 15 2023
- [SDR FDEA202310041701](https://openairdocs.org/sdr/FDEA202310041701), Oct 4, 2023: FLOOR PANEL. DENTED. MDC FLOOR PANEL 222AFF SEVERAL DENTS MDC FLOOR PANEL 222AFF WAS REPAIRED IAW B767 SRM 53-00-50-2R PAR 4B FIG 201. REV 87 AUG 15 2023
- [SDR FDEA202310041700](https://openairdocs.org/sdr/FDEA202310041700), Oct 4, 2023: FLAP. DELAMINATED. RH WING INBOARD FLAP, MAIN FLAP, LEADING EDGE OUTBOARD SIDE WITH DISBONDED RH WING INBOARD MAIN FLAP LEADING EDGE OUTBOARD SIDE WAS REPAIRED IAW B767 SRM 57- 53
- [SDR FDEA202305010793](https://openairdocs.org/sdr/FDEA202305010793), May 1, 2023: FUEL NOZZLE. FAILED. AFTER TAKEOFF, HAD R ENG OVHT EICAS WITH ASSOCIATED R ENG OVHT CAUTION LIGHT COMPLIED WITH QRH RETURNED TO MEMPHIS MOMENTARY STATUS MESSAGE R ENG OVHT LP2 WE NE
- [SDR FDEA202304290780](https://openairdocs.org/sdr/FDEA202304290780), Apr 29, 2023: UNKNOWN. UNKNOWN. PDIS 132 26-10 7156 28APR23 MEM OPEN U RIGHT ENG OVERHEAT INDICATION. ON CLIMB OUT. NO EXCEEDANCE NOTED. NO FIRE ALERT. ECAM MESSAGE OF RIGHT ENGINE OVERHEAT. R
- [SDR FDEA202304220745](https://openairdocs.org/sdr/FDEA202304220745), Apr 22, 2023: SKIN. DENTED. RIGHT WING #11 SLAT UPPER SURFACE HAS A LARGE SMOOTH DENT 3" FORWARD OF TRAILING EDGE AND 50" FROM OUTBOARD EDGE AS MARKED. 0000493008 : CRAIL, ROGER L - 23-APR
- [SDR FDEA202210012442](https://openairdocs.org/sdr/FDEA202210012442), Oct 1, 2022: CASE. DAMAGED. #1 ENGINE FWD FAN CASE, FWD OUTER LINER AT 1-2 O'CLOCK POSITION IS DAMAGED AROUND INBD INLET TEMP SENSOR. REF CF6-80C2 BOEING MM 72-22-02. IPC REF 72-33-01-05 I
- [SDR FDEA202210012441](https://openairdocs.org/sdr/FDEA202210012441), Oct 1, 2022: FORMER. CRACKED. RIGHT WING LEADING EDGE FORMER AT #5 SLAT WING STATION OSS 441 HAS EVIDENCE OF DAMAGE. REPLACE PART WITH NEW FORMER B67-57-002-02 ALONG WITH ANGLE B67-57-003-02
- [SDR FDEA202210012440](https://openairdocs.org/sdr/FDEA202210012440), Oct 1, 2022: FORMER. CRACKED. RIGHT WING LEADING EDGE FORMER AT #5 SLAT WING STATION OSS 441 HAS EVIDENCE OF DAMAGE. MWT REPLACE PART WITH NEW FORMER B67-57-002-02 ALONG WITH ANGLE B67-57-00
- [SDR FDEA202206221510](https://openairdocs.org/sdr/FDEA202206221510), Jun 22, 2022: WIRE. SPARKS. FO SEAT POWER CORD CRIMPED/SPARKED & TRIPPED CIRCUIT BREAKER. ADJUSTMENT SYSTEMS - INOP." FOUND CIRCUIT BREAKER IN. MOVED POWER CORD TO SEAT. SEAT REMAINED INOP
- [SDR FDEA202101220180](https://openairdocs.org/sdr/FDEA202101220180), Jan 22, 2021: PSEU. FALSE ACTIVATION. MAIN CARGO DOOR CAUTION AT FL320 COMPLIED WITH QRH RELEASED FOR SERVICE PER MEL: 52-71-01-02. CATEGORY: C EXPIRATION: 01FEB21 "MEL 52-71-01-02: MAIN DECK CARGO 
- [SDR FDEA202003060498](https://openairdocs.org/sdr/FDEA202003060498), Mar 6, 2020: SKIN. GOUGED. EXTERIOR FUSELAGE SKIN HAS 2EA DENT/GOUGES APPROX. 12" AFT OF THE MAIN E&E DOOR CUTOUT AT APPROX. LBL12. REPAIRED FUSELAGE SKIN AT STA 337 IAW FEDEX EA H-5310-T
- [SDR FDEA202002270396](https://openairdocs.org/sdr/FDEA202002270396), Feb 27, 2020: FORMER. CRACKED. RIGHT WING FIXED LE BEHIND SLAT 7 NOSE FORMER IS CRACKED AT FASTENER HOLE. REMOVED, FABRICATED, AND REPLACED RT WING FIXED LE NOSE FORMER IAW DWG 114T2170, DWG 
- [SDR FDEA2020022870396](https://openairdocs.org/sdr/FDEA2020022870396), Feb 27, 2020: FORMER. CRACKED. RW FIXED LE BEHIND SLAT #7 NOSE FORMER IS CRACKED AT FASTENER HOLE-DOT & STREAMER ATTACHED REMOVED, FABRICATED, AND REPLACED RW FIXED LE NOSE FORMER PER BAC DWG
- [SDR FDEA201802270512](https://openairdocs.org/sdr/FDEA201802270512), Feb 27, 2018: RELAY. INOPERATIVE. TE FLAP DISAGREE MSG ON EICAS, WHEN MOVING FLAP LEVER FROM 5 TO 15, COMPLIED WITH QRH AND USED TE ALTN FLAP EXTENSION FOR FLAPS 20 LANDING. ASSOCIATED STATUS MS
- [SDR FDEA201708202288](https://openairdocs.org/sdr/FDEA201708202288), Aug 20, 2017: D-RING. MISSING. ONE ESCAPE HARNESS UNDER THE LT SIDE JUMPSEAT IN COCKPIT MISSING A D-RING. THE D-RING WAS FOUND AND INSTALLED.
- [SDR FDEA201702220626](https://openairdocs.org/sdr/FDEA201702220626), Feb 22, 2017: SWITCH. FAILED. AFT CARGO DOOR ECIAS MSG DURING CRUISE. REPLACED THE SWITCH IAW AMM 52-71-03-2 AND OPS CHECKED GOOD IAW 52-71-00-5. OK FOR SERVICE.
- [SDR FDEA201701190227](https://openairdocs.org/sdr/FDEA201701190227), Jan 19, 2017: DISPLAY. FAILED. STATUS MESSAGE FOR THE LANDING GEAR MONITOR. NO NOSE GEAR GREEN DOWN AND LOCKED LIGHT. FOLLOWED QRH ALT. EXTENDED GEAR STILL NO GREEN NOSE GEAR LIGHT. TROUBLESH
- [SDR FDEA201607062297](https://openairdocs.org/sdr/FDEA201607062297), Jul 6, 2016: WARNING SYSTEM. ACTIVATED. TAKEOFF CONFIG WARNING ACTIVATED AT 85KTS FOR 1/2, FOLLOWED BY A FLAP RED EICAS FOR 2 SECONDS. ABORTED TAKEOFF AT APPROX 100KTS. WARNING LIGHT WENT OUT IMMEDIAT

## 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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