# N127FE: 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: 43547
- Year built: 2015
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: September 28, 2015
- Certificate issued: October 19, 2015
- Expires: October 31, 2028
- Mode S code: A06E35
- 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=127FE
- Page: https://openairdocs.org/aircraft/N127FE

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 N127FE.

## FAA accident and incident reports

None matched to N127FE.

## Service difficulty reports (35)

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 FDEA202506261061](https://openairdocs.org/sdr/FDEA202506261061), Jun 26, 2025: WEB. CRACKED. MEC, LT TUNNEL, STA 246 - STA 266 FLOORBEAM WEB CRACKED, LBL APPROX 48 FABRICATED/REPLACED WEB P/N 141T5602-2, REF B767 SRM 51-40-02-0G & BOEING DRW 141T5602.TH
- [SDR FDEA202506251048](https://openairdocs.org/sdr/FDEA202506251048), Jun 25, 2025: FLOORBOARD. DAMAGED. NR# 0293: MAIN CARGO DECK, FLOOR PANEL 242JFF HAS DAMAGE. FABRICATED NEW FLOOR PANEL 242JFF, MPN:145T5876-102, RBL 33 - RBL 11, STA. 930 Ï¿½ 984.95 IN REF TO BO
- [SDR FDEA202506251046](https://openairdocs.org/sdr/FDEA202506251046), Jun 25, 2025: FLOORBOARD. DAMAGED. NR# 0297: MAIN CARGO COMPARTMENT, FLOOR PANEL 242SFF HAS DAMAGE FABRICATED NEW FLOOR PANEL 242SFF, MPN:145T5876-104, RBL 33- RBL 11, STATION 984.95 - 1114.82 IN
- [SDR FDEA202506241040](https://openairdocs.org/sdr/FDEA202506241040), Jun 24, 2025: FLOORBOARD. DAMAGED. NR# 0296: MAIN CARGO COMPARTMENT, FLOOR PANEL 241WFF HAS DAMAGE FABRICATED NEW FLOOR PANEL 241WFF, MPN:145T5876-51, RBL 11- LBL 11, STATION 984.95 - 1114.82 IN 
- [SDR FDEA202506241039](https://openairdocs.org/sdr/FDEA202506241039), Jun 24, 2025: FLOOR PANEL. DAMAGED. MAIN CARGO COMPARTMENT, FLOOR PANEL 242LFA HAS DAMAGE. FABRICATED MAIN COMPARTMENT, FLOOR PANEL 242LFA (MPN: 145T5876-110) AT STA 930 TO STA 984, RBL 54.75 TO R
- [SDR FDEA202506241037](https://openairdocs.org/sdr/FDEA202506241037), Jun 24, 2025: FLOOR PANEL. DENTED. MAIN CARGO COMPARTMENT, FLOOR PANEL 242VFF HAS DAMAGE : CORRECTION FLOOR PANEL 242UFF FABRICATED FLOORPANEL 242UFF MPN# 114T5876-112 STA: 980-1114.82 RBL: 54.75
- [SDR FDEA202506221025](https://openairdocs.org/sdr/FDEA202506221025), Jun 22, 2025: FLOOR PANEL. WORN. MAIN CARGO COMPARTMENT, FLOOR PANEL 241LFF HAS DAMAGE. FABRICATED NEW FLOOR PANEL 241LFF, MPN:145T5876-19, RBL 11 LBL 11, STATION 930-984.95 IN REF TO BOEING DW
- [SDR FDEA202503050334](https://openairdocs.org/sdr/FDEA202503050334), Mar 5, 2025: WINDSHIELD. CRACKED. DURING CRUISE AT FL320, CAPTAIN S WINDSHIELD CRACKED IN A SPIDER WEB DESIGN. L FWD WINDSHIELD HEAT WENT INOP. WINDSHIELD REMOVED. WINDSHIELD HARDWARE IN FLIGHT 
- [SDR FDEA202412241829](https://openairdocs.org/sdr/FDEA202412241829), Dec 24, 2024: FORMER. CRACKED. RIGHT WING LEADING EDGE FORMER AT STA 433 CRACKED. REMOVED AND REPLACED RIGHT WING LEADING EDGE FORMER AT STA 433 REF 57-41-01-2R
- [SDR FDEA202410151502](https://openairdocs.org/sdr/FDEA202410151502), Oct 15, 2024: CONTROL UNIT. FAILED. MAIN CARGO DOOR LIGHT EICAS AND CARGO DOORS DISCREET LIGHT CAME ON DURING FLIGHT. 3 LIGHTS ON MAIN ENTRANCE DOOR PANEL WERE EXTINGUISHED. EXECUTED QRH PROCEDURE
- [SDR FDEA202409011212](https://openairdocs.org/sdr/FDEA202409011212), Sep 1, 2024: RETAINER. CRACKED. LOWER FORWARD CARGO DOOR SEAL RETAINER DAMAGED AT UPPER FORWARD AREA. LWR FWD CGO DOOR, UPPER SEAL RETAINER REPAIR PERFORMED IAW B767 SRM 52-30-02-2R REPAIR 5. 
- [SDR FDEA202306291126](https://openairdocs.org/sdr/FDEA202306291126), Jun 29, 2023: SLAT. DAMAGED. PERFORM MAJOR REPAIR TO SLAT #11 TRAILING EDGE WEDGE IN ACCORDANCE WITH 51-70-10-2R IN THE AREA OF SLAT #11 OSS 933.729. REF B767 SRM51-70-10-2R REPAIR4 & EA:H-
- [SDR FDEA202210222644](https://openairdocs.org/sdr/FDEA202210222644), Oct 22, 2022: FORMER. CRACKED. L/WING FLE OSS 499 HAS A CRACKED FORMER REPLACED FORMER B67-57-002-03 AT L/WING FLE OSS 499 USING EA H-5720-T0371261 AS REFERENCE.
- [SDR FDEA202206231539](https://openairdocs.org/sdr/FDEA202206231539), Jun 23, 2022: SLAT. CHAFED. RH WING LEADING EDGE SLAT #11 HAS A WEAR GROOVE ON THE UNDERSIDE(CONCAVE SIDE) SKIN. COMPLIED WITH E.A. H-5750-T0369144 P1.
- [SDR FDEA202009162253](https://openairdocs.org/sdr/FDEA202009162253), Sep 16, 2020: FLOOR PANEL. DELAMINATED. MAIN CARGO FLOOR PANEL 242TFA DELAMINATED AND HAS EDGE DAMAGE AT CORNER. REPAIRED AREAS OF DELAMINATION AND EDGE DAMAGE TO CARGO FLOOR PANEL 242TFA, IAW B767 SR
- [SDR FDEA202009162226](https://openairdocs.org/sdr/FDEA202009162226), Sep 16, 2020: ANGLE. CRACKED. NR 2 PYLON AFT BULKHEAD TO AFT FAIRING INBOARD ATTACH ANGLE CRACKED AT NAC STA 295 LT. REMOVED AND REPLACED ANGLE, PER B767 SRM 551-40-02 AND BOEING DWG 313T331
- [SDR FDEA202009152221](https://openairdocs.org/sdr/FDEA202009152221), Sep 15, 2020: HOUSING. CRACKED. AFT CARGO DOOR UPPER AFT CARGO LIGHT GOUGED AND CRACKED. REPAIRED AFT CARGO DOOR UPPER AFT CARGO LIGHT, IAW B767-AMM 25-00-00-8.
- [SDR FDEA202009152220](https://openairdocs.org/sdr/FDEA202009152220), Sep 15, 2020: HOUSING. CRACKED. AFT CARGO DOOR UPPER FWD CARGO LIGHT GOUGED AND CRACKED. REPAIRED AFT CARGO DOOR UPPER FWD CARGO LIGHT, IAW B767-AMM 25-00-00-8.
- [SDR FDEA2020091432191](https://openairdocs.org/sdr/FDEA2020091432191), Sep 13, 2020: SKIN. CHAFED. RIGHT WING SLAT NR 11, T/E LOWER SURFACE CHAFE AT O/B TRACK. REPAIRED RT WING NR 11 SLAT T/E LOWER SURFACE CHAFE AT O/B TRACK WITH 250 DEG METAL BOND, IAW B767 
- [SDR FDEA2020091422186](https://openairdocs.org/sdr/FDEA2020091422186), Sep 12, 2020: BEAM. GOUGED. NR 2 PYLON AFT FAIRING INBOARD LONGITUDINAL BEAM GOUGED AT NUTPLATE LOCATION AT NAC STA 308 LT. REMOVED LATCH BEAM, IAW B767 SRM 51-40-02-0G. REPAIRED LATCH BEA
- [SDR FDEA202009112171](https://openairdocs.org/sdr/FDEA202009112171), Sep 11, 2020: FLOOR PANEL. DAMAGED. MAIN CABIN FLOOR PANEL 242GFF IS DAMAGED. REPAIRED MAIN CABIN FLOOR PANEL 242GFF, IAW B767 SRM 53-00-50-2R.
- [SDR FDEA202009112170](https://openairdocs.org/sdr/FDEA202009112170), Sep 11, 2020: FLOOR PANEL. DAMAGED. MAIN CABIN FLOOR PANEL 241ZFF IS DAMAGED. REPAIRED MAIN CABIN FLOOR PANEL 241ZFF, IAW B767 SRM 53-00-50-2R.
- [SDR FDEA2020090982147](https://openairdocs.org/sdr/FDEA2020090982147), Sep 8, 2020: FORMER. CRACKED. RT WING LEADING EDGE INTERNAL FORMER CRACKED ON OUTBOARD SIDE OF SLAT NR 8 OUTBOARD ACTUATOR. REMOVED AND REPLACED RT WING RIB FORMER AT W/S 480, PER FEDEX B767
- [SDR FDEA2020090972139](https://openairdocs.org/sdr/FDEA2020090972139), Sep 7, 2020: BRACKET. CRACKED. LT WING, LEADING EDGE CAVITY FWD FORMER BRACKET CRACKED, LEADING EDGE STA 430. REMOVED CRACKED FORMER BRACKET IAW B767 SRM 51-40-02, MATERIAL ID 2024T3 .040" IA
- [SDR FDEA2020090972138](https://openairdocs.org/sdr/FDEA2020090972138), Sep 7, 2020: SPLICE PLATE. CRACKED. RT WING LEADING EDGE INTERNAL SPLICE PLATE CRACKED APPROX 1' OUTBOARD OF SLAT #8 OUTBOARD ACTUATOR. REMOVED AND REPLACED SPLICE P/N 114T2800-165, PER BAC DWG 11
- [SDR FDEA2020090972137](https://openairdocs.org/sdr/FDEA2020090972137), Sep 7, 2020: BRACKET. CRACKED. LT WING, LEADING EDGE CAVITY FWD FORMER BRACKET CRACKED. LEADING EDGE STA 480 REMOVED AND REPLACED NOSE FORMER, IAW BOEING DWG 114T2511, REV D, B767 SRM 51-40-0
- [SDR FDEA2020090962134](https://openairdocs.org/sdr/FDEA2020090962134), Sep 6, 2020: BRACKET. CRACKED. LEFT WING PANEL 511KB AREA INBOARD BRACKET CRACKED. REMOVED AND REPLACED BRACKET P/N 256T2425-6, PER BOEING DWG 114T1240 REV D.
- [SDR FDEA2020090942107](https://openairdocs.org/sdr/FDEA2020090942107), Sep 4, 2020: BRACKET. CRACKED. RT WING PANEL 611KB AREA IB BRACKET CRACKED. REMOVED AND REPLACED BRACKET ON RT WING PANEL 611KB AREA, PER FEDEX B767 SRM 51-40-02 AND PER BOEING DWG 114T1240 R
- [SDR FDEA2020090922082](https://openairdocs.org/sdr/FDEA2020090922082), Sep 2, 2020: FORMER. CRACKED. LT WING LEADING EDGE CAVITY FWD FORMER STRAP CRACKED LEADING EDGE STA 505. REMOVED AND REPLACED LT WING LEADING EDGE CAVITY FWD FORMER STRAP LES 505 PN 114T2800
- [SDR FDEA202006261369](https://openairdocs.org/sdr/FDEA202006261369), Jun 26, 2020: UNKNOWN. ODOR. ON CLIMBOUT AND DESCENT PACKS SMELL LIKE DIRTY SOCKS. PERFORMED AIR CONDITIONING OIL/FUME CONTAMINATION REMOVAL AS PER MM 21-00-21-2. OIL SMELL WITH PACKS RUNIN
- [SDR FDEA202006261368](https://openairdocs.org/sdr/FDEA202006261368), Jun 26, 2020: MODULE. ODOR. ON CLIMBOUT AND DESCENT PACKS SMELL LIKE DIRTY SOCKS. REMOVED AND REPLACED YSM, PER AMM 27-09-00-2. CHECKS GOOD. UNIT CHANGED, YAW DAMPER/STAB TRIM MODULE.
- [SDR FDEA201909112212](https://openairdocs.org/sdr/FDEA201909112212), Sep 11, 2019: PRESSURE SWITCH. FAILED. UNSCHD STAB TRIM FOR APPROXIMATELY 2 SECONDS ON EICAS, PASSING 8000 FT DURING DESCENT SPEED 210 KTS FLAP 1. REPLD C HYD PRESS SWITCH S29. PRESSURE SWITCH LEAK C
- [SDR FDEA2018110213074](https://openairdocs.org/sdr/FDEA2018110213074), Nov 1, 2018: ESCAPE ROPE. UNSECURE. ON ARRIVAL AT THE ACFT, FOUND AN ESCAPE ROPE DROPPED DOWN AT THE FRONT OF DOOR. RESTORED THE L1 ENTRY DOOR ESCAPE ROPE IAW MM 25-61-04-2-1. AIRCRAFT OK SERVICE.
- [SDR FDEA201802110336](https://openairdocs.org/sdr/FDEA201802110336), Feb 11, 2018: TRANSMITTER. MALFUNCTIONED. RECEIVED RED STABLIZER WARNING ON INITIAL POWER APPLICATION DURING PREFLIGHT STAB TRIM SET TO 6.75. CONFIG T/O CHECK PERFORMED 3 TIMES. AFTER WARNING, STAB INDI
- [SDR FDEA201606152003](https://openairdocs.org/sdr/FDEA201606152003), Jun 15, 2016: ROTARY ACTUATOR. INOPERATIVE. AT 220 KTS RECEIVED L/E SLAT DISAGREE LIGHT. ACCOMPLISHED QRH CHECKLIST 9.1.10, L/E SLAT DISAGREE 0. L/E WOULD NOT DEPLOY BEYOND, BETWEEN UP AND 1, USING ALT FL

## Service difficulty reports on N127FE not matched to an aircraft (28)

They name N127FE, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft.

- [SDR 02FDEA00617](https://openairdocs.org/sdr/02FDEA00617), Aug 30, 2002: STRINGER. CRACKED. FOUND STR 27 RT CRACKED IN INBOARD RADIUS AT BS 1111-1116. REMOVED AND REPLACED STRINGER PER SRM 51-40-4.
- [SDR 02FDEA00620](https://openairdocs.org/sdr/02FDEA00620), Aug 30, 2002: SKIN. CRACKED. CRACKS NOTED IN FASTENER HOLE AT BS 488, STR 3L, AFT HOLE OF FILLER IN ALL LAYERS INCLUDING FILLER, EXCEPT INNERMOST SKIN CRACKS ENDS MARKED. REMOVED AND REPLAC
- [SDR 02FDEA00619](https://openairdocs.org/sdr/02FDEA00619), Aug 30, 2002: SKIN. CRACKED. CRACKS NOTED IN FASTENER HOLES 5 EA AT BS 610-614, STR 3L IN ALL LAYERS EXCEPT INNERMOST AND FILTER. REMOVED AND REPLACED FASTENER HOLES PER EA 7-5330-65875.
- [SDR 02FDEA00618](https://openairdocs.org/sdr/02FDEA00618), Aug 30, 2002: STRUCTURE. CRACKED. CRACK AT AFT CARGO AFT LWR CORNER 4TH FASTENER FROM CORNER OF DOOR CUTOUT. REMOVED AND REPLACED CARGO DOOR PER SRM 51-10-7.
- [SDR 02FDEA00607](https://openairdocs.org/sdr/02FDEA00607), Aug 27, 2002: RIB. CHAFED. LEFT HORIZONTAL STAB T/E RIB AT ELEVATOR BS 209, I/B SIDE HAS CHAFING DAMAGE. REMOVED AND REPLACED RIB PER SRM 51-30-2.
- [SDR 02FDEA00600](https://openairdocs.org/sdr/02FDEA00600), Aug 21, 2002: WEB. CORRODED. CORROSION ON BOTTOM SIDE OF SHEAR WEB AT BS 1136, RBL 64, WL 208.
- [SDR 02FDEA00589](https://openairdocs.org/sdr/02FDEA00589), Aug 13, 2002: SKIN. LIGHTNING STRIKE. LIGHTNING STRIKE ON OUTER SKIN AT BS 401, STR 10R. REMOVED AND REPLACED SKIN PER SRM 53-30-3.
- [SDR 02FDEA00576](https://openairdocs.org/sdr/02FDEA00576), Aug 12, 2002: SKIN. LIGHTNING STRIKE. LIGHTNING STRIKE LWR FUSELAGE AT BS 181, STR 19R.
- [SDR 02FDEA00561](https://openairdocs.org/sdr/02FDEA00561), Aug 12, 2002: STRINGER CLIP. CRACKED. STRINGER CLIP CRACKED AT BS 1050, STR 8 LT. REMOVED AND REPLACED CLIP PER SRM 51-30-2.
- [SDR 02FDEA00579](https://openairdocs.org/sdr/02FDEA00579), Aug 10, 2002: STRINGER. CRACKED. STRINGER 8R CRACKED AT BS 600. REMOVED AND REPLACED STRINGER PER SRM 53-10-01, 51-40-4.
- [SDR 02FDEA00578](https://openairdocs.org/sdr/02FDEA00578), Aug 10, 2002: WEB. CRACKED. CRACKED WEB BS 600 BETWEEN STR 1 & 2 LT. REMOVED AND REPLACED WEB PER SRM 51-30-2, 51- 30-5, 51-20-1.
- [SDR 02FDEA00577](https://openairdocs.org/sdr/02FDEA00577), Aug 10, 2002: WEB. CRACKED. CRACKED WEB BS 613 BETWEEN STR 1 & 2 LT.
- [SDR 02FDEA00565](https://openairdocs.org/sdr/02FDEA00565), Aug 7, 2002: DOOR FRAME. CRACKED. AFT FRAME OF FWD CARGO DOOR CUT OUT CRACK AT THE TIP DOOR STOP FITTING BETWEEN STR 19R - 20R. REMOVED AND REPLACED ANGLE & FILLER ON AFT FRAME PER EA 7-5310-658
- [SDR 02FDEA00567](https://openairdocs.org/sdr/02FDEA00567), Aug 6, 2002: SKIN. DAMAGED. NUMEROUS NICKS IN LWR EXTERNAL FUSELAGE SKIN BETWEEN BS 580 & 600, STR 23R TO STR 26R.
- [SDR 02FDEA00558](https://openairdocs.org/sdr/02FDEA00558), Aug 6, 2002: SKIN. DAMAGED. NUMEROUS NICKS IN LWR EXTERNAL FUSELAGE SKIN BETWEEN BS 368, STR 19L TO 20L. REMOVED AND REPLACED SKIN PER SRM 53-30-3 FIG 1.
- [SDR 02FDEA00560](https://openairdocs.org/sdr/02FDEA00560), Aug 6, 2002: STRINGER CLIP. CRACKED. CRACKED STR CLIP AT BS 1050, STR 6 LT. REMOVED AND REPLACED CLIP PER SRM 51-30-2.
- [SDR 02FDEA00559](https://openairdocs.org/sdr/02FDEA00559), Aug 6, 2002: STRINGER CLIP. CRACKED. CRACKED STR CLIP BS 1070, STR 7R.
- [SDR 02FDEA00564](https://openairdocs.org/sdr/02FDEA00564), Aug 6, 2002: FITTING. CORRODED. STRINGER END FITTING CORRODED AT BS 740, STR 9L. REMOVED AND REPLACED FITTING PER SRM 51-30-2.
- [SDR 02FDEA00563](https://openairdocs.org/sdr/02FDEA00563), Aug 6, 2002: STRINGER CLIP. CRACKED. CRACKED STRINGER CLIP AT BS 1030, STR 8 LT. REMOVED AND REPLACED CLIP PER SRM 51-30-2.
- [SDR 02FDEA00562](https://openairdocs.org/sdr/02FDEA00562), Aug 6, 2002: STRINGER CLIP. CRACKED. CRACKED STRINGER CLIP AT BS 1030, STR 4 RT.
- [SDR 02FDEA00554](https://openairdocs.org/sdr/02FDEA00554), Aug 5, 2002: SKIN. BULGED. LWR EXT FUSELAGE HAS BULGING SKIN AND SHEARED RIVET BETWEEN STR 28R AND 29R AT BS 352 AND 358. REMOVED AND REPLACED SKIN PER SRM 51-30-2, 51-30-5, 51-30-8, 51-1
- [SDR 02FDEA00555](https://openairdocs.org/sdr/02FDEA00555), Aug 5, 2002: FRAME. CORRODED. CORROSION CIRCUMFERENTIAL CHORD CORRODED AT BS 351 BETWEEN STR 26L AND 26R.
- [SDR 02FDEA00568](https://openairdocs.org/sdr/02FDEA00568), Aug 4, 2002: STRINGER CLIP. CRACKED. CRACK STRINGER CLIP AT BS 700, STR 2 L. *S/D* REMOVED AND REPLACED STRINGER CLIP PER SRM 51-30-2.
- [SDR 02FDEA00638](https://openairdocs.org/sdr/02FDEA00638), Aug 3, 2002: SPAR. CRACKED. RIGHT REAR SPAR CHORD CRACKED APPROX BS 200.
- [SDR 02FDEA00571](https://openairdocs.org/sdr/02FDEA00571), Aug 3, 2002: STRINGER CLIP. CRACKED. CRACKED STRINGER CLIP AT BS 1000, STR 9 LT. REMOVED AND REPLACED CLIP PER SRM 51-30-2, 51-30-5.
- [SDR 02FDEA00572](https://openairdocs.org/sdr/02FDEA00572), Aug 3, 2002: STRINGER CLIP. CRACKED. CRACKED STRINGER CLIP AT BS 1030, STR 9 LT. REMOVED AND REPLACED CLIP PER SRM 51-30-2, 51-30-5.
- [SDR 02FDEA00573](https://openairdocs.org/sdr/02FDEA00573), Aug 3, 2002: STRINGER CLIP. CRACKED. CRACKED STRINGER CLIP AT BS 1030, STR 7 LT. REMOVED AND REPLACED CLIP PER SRM 51-30-2, 51-30-5.
- [SDR 02FDEA00570](https://openairdocs.org/sdr/02FDEA00570), Aug 2, 2002: BULKHEAD. CRACKED. CRACK ON WEB AT BS 178, RBL 10, WL 235. REMOVED AND REPLACED WEB PER SRM 53-10-9.

## 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 N127FE

The FAA can reassign an N-number once a registration is cancelled. These aircraft carried N127FE before.

- [Cancelled 2001-06-11](https://openairdocs.org/deregistered/N127FE-2001-06-11): Boeing 727-25C, S/N 19719. Exported to Canada. 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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