# N128FE: 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: 42719
- Year built: 2015
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: October 12, 2015
- Certificate issued: November 5, 2015
- Expires: November 30, 2028
- Mode S code: A071EC
- 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=128FE
- Page: https://openairdocs.org/aircraft/N128FE

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 N128FE.

## FAA accident and incident reports

None matched to N128FE.

## 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 FDEA202508051370](https://openairdocs.org/sdr/FDEA202508051370), Aug 5, 2025: SKIN. DENTED. DENT IN LOWER SURFACE AT OTEF STA 232.69 AND 9" OF LEADING EDGE ON LH OUTBOARD FLAP LEADING EDGE ON LH OUTBOARD FLAP WAS REPAIRED IAW B767 SRM 57-53-01-2R FIG 2
- [SDR FDEA202508041363](https://openairdocs.org/sdr/FDEA202508041363), Aug 4, 2025: FLOOR PANEL. CRACKED. PUNCTURE ON FLOOR PANEL 242TFA AT MDC. FLOOR PANEL 242TFA AT MDC WAS REPAIRED IAW B767 SRM 53-00-50-2R PAR 4B FIGURE 201 SHEET 2 REV. 92 APR 15, 2025
- [SDR FDEA202508021358](https://openairdocs.org/sdr/FDEA202508021358), Aug 2, 2025: SKIN. DENTED. DENT ON EXTERNAL SURFACE OF SLAT NO. 7 AT 3" FROM UPPER EDGE AND 49.5" FROM OUTBOARD EDGE, RIGHT WING RH WING, SLAT NO. 7 AT 3" FROM UPPER EDGE AND 49.5" FROM O
- [SDR FDEA202508011354](https://openairdocs.org/sdr/FDEA202508011354), Aug 1, 2025: ACCESS PANEL. PUNCTURED. FLOOR ACCESS PANEL 242 VFF WITH SEVERAL PUNCTURE ON MAIN DECK CARGO COMPARTMENT. FLOOR PANEL 242 VFF WAS REPAIRED IAW B767 SRM 53-00-50-2R PAR4-B FIG 201 SHEET 
- [SDR FDEA202508011353](https://openairdocs.org/sdr/FDEA202508011353), Aug 1, 2025: FLOOR PANEL. PUNCTURED. PUNCTURE ON FLOOR PANEL 241AGF AT MDC FLOOR PANEL 241AGF WAS REPAIRED IAW B767 SRM 53-00-50-2R PAR 4-B FIG. 201 SHEET 2 REV. 92 APR 15,2025
- [SDR FDEA202508011352](https://openairdocs.org/sdr/FDEA202508011352), Aug 1, 2025: FLOOR PANEL. CRACKED. CRACKS ON FLOOR PANEL 241WFF FLOOR PANEL 241WFF WAS REPAIRED IAW B767 SRM 53-00-50 2R PAR 4.B FIG 201 SHEET 2 REV.92 APR 15,2025
- [SDR FDEA202508011351](https://openairdocs.org/sdr/FDEA202508011351), Aug 1, 2025: FLOOR PANEL. PUNCTURED. PUNCTURE ON FLOOR PANEL 242GFF AT MDC FLOOR PANEL 242GFF AT MDC WAS REPAIRED IAW B767 SRM 53-00-50-2R PAR 4.B FIGURE 201 SHEET 2 REV.92 APR 15,2025
- [SDR FDEA202508011350](https://openairdocs.org/sdr/FDEA202508011350), Aug 1, 2025: FLOOR PANEL. PUNCTURED. PUNCTURE ON FLOOR PANEL 251FFF AT MDC FLOOR PANEL 251FFF AT MDC WAS REPAIRED IAW B767 SRM 53-00-50-2R PAR4.B FIGURE 201 SHEET 2 REV. 92 APR 15,2025
- [SDR FDEA202508011348](https://openairdocs.org/sdr/FDEA202508011348), Aug 1, 2025: FLOOR PANEL. CRACKED. CRACK ON FLOOR PANEL 251AFF FLOOR PANEL 251AFF WAS REPAIRED IAW B767 SRM 53-00-50-2R PAR 4-B FIG.201 (SHEET 2) REV. 92 APR 15,2025
- [SDR FDEA202508011347](https://openairdocs.org/sdr/FDEA202508011347), Aug 1, 2025: FLOOR PANEL. CRACKED. CRACKS ON FLOOR PANEL 251QFF FLOOR PANEL 251QFF WAS REPAIRED IAW B767 SRM 53-00-50-2R PAR. 4-B FIG.201 (SHEET 2) REV. 92 APR 15,2025
- [SDR FDEA202508011349](https://openairdocs.org/sdr/FDEA202508011349), Aug 1, 2025: FLOOR PANEL. DENTED. SEVERAL DENTS ON FLOOR PANEL 251PFF FLOOR PANEL 251PFF WAS REPAIRED IAW B767 SRM 53-00-50-2R PAR 4.B FIG.201 (SHEET 2) REV. 92 APR 15,2025
- [SDR FDEA202312231952](https://openairdocs.org/sdr/FDEA202312231952), Dec 23, 2023: BRAKE ASSY. MAKING METAL. ON WALK AROUND METAL SHAVINGS COMING FROM #5 BRAKE. AMM: 32-11-18-4 COMPLETED INSTALLATION OF LMLG BOGIE BEAM ASSY, IAW AMM 32-11-18-4. PLS SEE W/O 87633, SEQ. 
- [SDR FDEA202308251492](https://openairdocs.org/sdr/FDEA202308251492), Aug 25, 2023: FLOORBEAM. CRACKED. 1EA FLOORBEAM ATTACH ANGLE IS CRACKED, INSIDE E&E COMPARTMENT ON LH SIDE AT STA 246, APPROX LBL 44 ON AFT SIDE OF THE FLOORBEAM REMOVED AND REPLACED FLOORBEAM A
- [SDR FDEA202308241490](https://openairdocs.org/sdr/FDEA202308241490), Aug 24, 2023: WEDGE. WORN. RH WING #8 L/E SLAT, T/E WEDGE, LOWER SURFACE IS WORN JUST OUTBD OF THE INBD AUX TRACK REPAIRED DAMAGE ON THE RH WING #8 SLAT, T/E WEDGE, LOWER SURFACE IAW B767
- [SDR FDEA202308241489](https://openairdocs.org/sdr/FDEA202308241489), Aug 24, 2023: WEDGE. WORN. RH WING #8 L/E SLAT T/E WEDGE LOWER SURFACE IS WORN JUST OUTBD OF THE OUTBD ROTARY ACTUATOR CONTROL ROD REPAIRED RH WING #8 SLAT, T/E WEDGE IAW B767 SRM 57-43-0
- [SDR FDEA202308231481](https://openairdocs.org/sdr/FDEA202308231481), Aug 23, 2023: SLAT. WORN. RH WING #9 L/E SLAT WEDGE LOWER SURFACE IS WORN JUST INBD OF THE INBD ROTARY ACTUATOR TIE ROD. ACCOMPLISHED PERMANENT REPAIR OF RIGHT WING #9 L/E SLAT T/E WEDGE
- [SDR FDEA202207071694](https://openairdocs.org/sdr/FDEA202207071694), Jul 7, 2022: BRAKE. WORN. THE INBOARD SURFACE OF THE #4 WHEEL IS TOUCHING OUTBOARD SURFACE OF THE #4 BRAKE ASSEMBLY. EXCESSIVE GAP NOTED BETWEEN #4 BRAKE AND AXLE SLEEVE REMOVED AND REPL
- [SDR FDEA202109072235](https://openairdocs.org/sdr/FDEA202109072235), Sep 7, 2021: SKIN. DENTED. UPPER FUSELAGE SKIN STA212.5 - STA220.5 S2R-S3R FOUND 1EA DENT. PERFORMED THE REPAIR ON UPPER FUSELAGE SKIN STA212.5 - STA220.5, S2R-S3R PER FEDEX EA # : H-5330
- [SDR FDEA2020082642008](https://openairdocs.org/sdr/FDEA2020082642008), Aug 24, 2020: ATTACH ANGLE. CRACKED. NR 2 PYLON LT FWD SKIRT BEAM ATTACH ANGLE CRACKED. REMOVED AND REPLACED ATTACH ANGLE PER B767 SRM 51-40-02 AND BAC DWG 313T3310 REV.
- [SDR FDEA2020082631996](https://openairdocs.org/sdr/FDEA2020082631996), Aug 23, 2020: SKIN. CHAFED. LT WING NR 5 SLAT LOWER TRAILING EDGE WEDGE SKIN CHAFED NUMEROUS SPOTS. REMOVED FINISH AT AREA AS MARKED OF NR 5 SLAT TRAILING EDGE WEDGE. LOWER SKIN, FOUND 1EA
- [SDR FDEA2020082091936](https://openairdocs.org/sdr/FDEA2020082091936), Aug 19, 2020: SKIN. GOUGED. RIGHT WING LE NR 8 SLAT LOWER SURFACE TE HAS GOUGED. REPAIRED THE NR 8 SLAT LOWER SURFACE IAW SRM: 57-42-02-2R, AND 51-70-10-2R, REPAIR 4. MAJOR REPAIR. 
- [SDR FDEA2020081871909](https://openairdocs.org/sdr/FDEA2020081871909), Aug 17, 2020: STRAP. CRACKED. RIGHT WING L/E CAVITY UPPER SKIN JOINT PLATE CRACKED AT L/E STA. 505. REMOVED AND REPLACED CRACKED SEAL STRAP PER B767 SRM 51-40-02 AND BAC DWG 114T2800 REV. C.
- [SDR FDEA202008141881](https://openairdocs.org/sdr/FDEA202008141881), Aug 14, 2020: DEPRESSOR. CRACKED. MAIN CARGO DOOR CUTOUT, FWD UPPER SEAL DEPRESSOR DENTED AND GOUGED. AFTER FURTHER EVALUATION FOUND CRACK IN DENT. CHECKED LIMITS FOR DENT AND GOUGE ON SEAL DEPR
- [SDR FDEA202001210181](https://openairdocs.org/sdr/FDEA202001210181), Jan 21, 2020: WARNING LIGHT. FALSE ACTIVATION. MAIN CARGO DOOR LIGHT ILLUMINATED ON THE EICAS, APPROACHING 370, LIGHT WENT OUT 20-40 MINUTES LATER.
- [SDR FDEA201602070487](https://openairdocs.org/sdr/FDEA201602070487), Feb 7, 2016: PSEU. FAULTY. AT FL340, HAS EICAS MSG, MAIN CARGO DOOR. COMPLIED WITH QRH. DESCENT TO 10,000 FT RTB KIND. MAIN DECK CARGO DOOR INDICATION SYS INOPERATIVE. VERIFY & RECORD IN 
- [SDR FDEA201601300403](https://openairdocs.org/sdr/FDEA201601300403), Jan 30, 2016: INDICATION SYS. MALFUNCTIONED. EICAS MSG MAIN CARGO DOOR AT FL 340, EXTINGUISHED AT 12000 MSL CABIN ALT OF 9500. RELEASED FOR SERVICE IAW MEL 52-71-01-02 CATEGORY C EXPIRATION 09FEB16. MAIN D

## 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

## Earlier aircraft with N128FE

The FAA can reassign an N-number once a registration is cancelled. These aircraft carried N128FE before.

- [Cancelled 2002-10-15](https://openairdocs.org/deregistered/N128FE-2002-10-15): Boeing 727-25C, S/N 19720, built 1967. Triennial form not returned. Owner: [Federal Express Corp](https://openairdocs.org/faa-owner/FEDERAL%20EXPRESS%20CORP), [Memphis, TN](https://openairdocs.org/faa-place/TN/Memphis)

## 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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