# N102FE: 2013 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: 42707 - Year built: 2013 - Type: Fixed wing multi engine - Engine type: Turbo-fan - Airworthiness: Standard, transport - Airworthiness date: October 3, 2013 - Certificate issued: October 18, 2013 - Expires: October 31, 2029 - Mode S code: A00CA4 - 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=102FE - Page: https://openairdocs.org/aircraft/N102FE 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 N102FE. ## FAA accident and incident reports None matched to N102FE. ## 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 FDEA202605130594](https://openairdocs.org/sdr/FDEA202605130594), May 13, 2026: CHARGER. INOPERATIVE. WHILE PERFORM EMERGENCY LIGHT TEST, FOUND EMERGENCY LIGHTS ARE NOT ILLUMINATED. PREMATURE REMOVAL/INSTALLATION AMM: 33-51-07-2 CHECK FOUND IT IS THE POWER SUPPL - [SDR FDEA202603060318](https://openairdocs.org/sdr/FDEA202603060318), Mar 6, 2026: SKIN. PUNCTURED. LH WING INBD T/E AFT FLAP LOWER SKIN FOUND 1EA PUNCTURE BTW IFS179.75 & IFS257.75. REPAIRED LH WING INBD TRAILING EDGE AFT FLAP LOWER SKIN 1EA PUNCTURE BTW IFS1 - [SDR FDEA202511042123](https://openairdocs.org/sdr/FDEA202511042123), Nov 4, 2025: FAIRING. DENTED. RT WING INBD FLAP O/B ACTUATOR AFT FAIRING DENTED. REPAIRED W/H WING I/B FLAP O/B ACTUATOR AFT FAIRING SKIN DENTED DAMGAGE (MPN:113T1770-56G CPN:5721384) IN REF - [SDR FDEA202503120390](https://openairdocs.org/sdr/FDEA202503120390), Mar 12, 2025: LIGHT. SPARKS. SPARKS ARE SEEN WHEN THE CAPTAIN S GRIMES LIGHT IS LIFTED OFF ITS BASE AND THEN THE LIGHT S POST TOUCHES THE FOOT HEATER SWITCH. UTILITY LIGHTS C/B P32 ON PANEL - [SDR FDEA202411161680](https://openairdocs.org/sdr/FDEA202411161680), Nov 16, 2024: SKIN. GOUGED. RIGHT ELEVATOR LOWER LEADING EDGE SKIN, BETWEEN HINGE FITTING AND ACTUATOR ATTACH FITTING, AT ELEVATOR STATION 167.24, COMPOSITE SKIN HAS 2EA WEAR MARKS IN THE - [SDR FDEA202411161679](https://openairdocs.org/sdr/FDEA202411161679), Nov 16, 2024: STIFFENER. CRACKED. RIGHT ELEVATOR LOWER LEADING EDGE VERTICAL STIFFENER, BETWEEN HINGE FITTING AND ACTUATOR ATTACH FITTING, AT ELEVATOR STATION 167.74, COMPOSITE STIFFENER IS BROK - [SDR FDEA202411131674](https://openairdocs.org/sdr/FDEA202411131674), Nov 13, 2024: SKIN. DELAMINATED. L/H WING, INBD AILERON, UPPER OUTBD SURFACE HAS A LARGE AREA OF DELAMINATION. MWT REPAIRED LH INBD AILERON TOP SKIN AT WS. 520 MPN: (113T6100-89G) IN REF. TO 76 - [SDR FDEA202411131673](https://openairdocs.org/sdr/FDEA202411131673), Nov 13, 2024: FLOORBOARD. DENTED. MAIN DECK CARGO COMPARTMENT, FLOORBOARD AT F.S.450 CENTERLINE HAS MULTIPLE DENTS. MWD REPAIRED FLOORBOARD MAIN CARGO COMPARTMENT PANEL #231AFF, AT STA 450 LEFT - [SDR FDEA202411131672](https://openairdocs.org/sdr/FDEA202411131672), Nov 13, 2024: FLOORBOARD. GOUGED. MAIN DECK CARGO COMPARTMENT, FLOORBOARD HAS DEEP GOUGE AT 5L POSITION. MWD REPAIRED FLOORBOARD MAIN CARGO COMPARTMENT PANEL # 231PFF, AT STA 640- STA 648 LEFT O - [SDR FDEA202411121667](https://openairdocs.org/sdr/FDEA202411121667), Nov 12, 2024: SKIN. DELAMINATED. RT WING INBOARD FORE FLAP, OUTBOARD END LEADING EDGE IS DELAMINATED. MWT REPAIRED RH LEADING EDGE SKIN MAIN FLAP, INBD T/E FLAP (PNL# 655DB) (MPN: 113T2211-22) - [SDR FDEA202411111664](https://openairdocs.org/sdr/FDEA202411111664), Nov 11, 2024: WEB. CRACKED. MEC LT TUNNEL, BETWEEN FLOORBEAMS @ STA 246 & 266.5, LBL 50 CRACKED WEB. MEC LT TUNNEL BERWEEN FLOORBEAMS @ STA 246 AND 266 LBL 50 CRACKED WEB PART# 141T5602-6 - [SDR FDEA202407301066](https://openairdocs.org/sdr/FDEA202407301066), Jul 30, 2024: TRANSPONDER. FAULTED. ENROUTE GOT AN ATC FAULT EICAS MESSAGE. CREW REPORT SYSTEM RECOVERED DURING FLIGHT.TESTING IN PROGRESS. FIM: 34-53 FAULT TREE 803, BOTH ATC TRANSPONDERS TESTED - [SDR FDEA202305030802](https://openairdocs.org/sdr/FDEA202305030802), May 3, 2023: BRACKET. DAMAGED. ON CLIMBOUT LE FLAPS ASYM EICAS WHEN RETRACTING FLAPS FROM 1 TO UP, QRH COMPLIED, PAN PAN DECLARED. RETURN TO CRK RUNWAY 20, FLAPS 20 APPROACH. EMERGENCY DECLAR - [SDR FDEA202304210733](https://openairdocs.org/sdr/FDEA202304210733), Apr 21, 2023: STRINGER. DAMAGED. COMPLY WITH EO H-5310-EO365800 P2, FUSELAGE - MAINFRAME - INSTALLATION OF SPLICE FITTINGS ON STRINGERS S-20L AND S-20R AT STA 1506, STA1530, AND STA 1552 - BOEI - [SDR FDEA202304210732](https://openairdocs.org/sdr/FDEA202304210732), Apr 21, 2023: STRINGER. DAMAGED. COMPLY WITH EO H-5310-EO365800 P1, FUSELAGE - MAINFRAME - INSTALLATION OF SPLICE FITTINGS ON STRINGERS S-20L AND S-20R AT STA 1506, STA1530, AND STA 1552 - BOEI - [SDR FDEA202301170126](https://openairdocs.org/sdr/FDEA202301170126), Jan 17, 2023: TRANSMITTER. FAILED. RT SYS PRESS EICAS ON DEPARTURE. UNABLE TO RESTORE SYSTEM PRESSURE VIA QRH. DECLARED EMERGENCY AND RTB TO CAN. EMERGENCY DECLARED. CONSULTED WITH FLIGHT CREW JU - [SDR FDEA202203270703](https://openairdocs.org/sdr/FDEA202203270703), Mar 27, 2022: NONE. NONE. DURING EMER LT TEST, FOUND DID NOT ILLUMINATE ALL EMER LIGHTS EVEN WHEN EMER SW ON. R & R'ED EMER LT BATTERY PACK AND FUNCTION CHECKED NORMAL PER AMM 33-51-07-2 - [SDR FDEA201810293038](https://openairdocs.org/sdr/FDEA201810293038), Oct 29, 2018: CARABINER. MISSING. MDIS 102 25-60 5247 29OCT18 MNL OPEN U ON SERVICE CHECK STEPS 17 ITEM D(1) FOUND TOTAL OF SIX EA CARABINER OF HARNESS MISSING. CARABINER'S PROVIDED AS PER AMM 2 - [SDR FDEA201810132868](https://openairdocs.org/sdr/FDEA201810132868), Oct 13, 2018: CARABINER. MISSING. MDIS 102 25-60 5172 13OCT18 MNL OPEN U ON SVC CHK FOUND RIGHT JUMP/SUPERNUMERARY SEAT MISSING CARABINER/D- RING 2EA. MEL 13OCT18 00:21 MNL U RELEASED FOR SERVIC - [SDR FDEA201706301882](https://openairdocs.org/sdr/FDEA201706301882), Jun 30, 2017: D-RING. MISSING. DURING FLIGHT, FOUND THE SUPERNUMENARY SEAT NEAREST TO THE LAVATORY, FOUND THE ESCAPE HARNESS D-RING MISSING. INSTALLED A NEW ESCAPE HARNESS D-RING. ACFT OK FOR - [SDR FDEA201703160920](https://openairdocs.org/sdr/FDEA201703160920), Mar 16, 2017: D-RING. MISSING. RT JUMPSEAT ONE CREW ESCAPE SAFETY HARNESS MISSING CARABINER. INSTALLED NEW CARABINER AND REPACK SAFETY HARNESS PER AMM 25-61-03-2-0. A/C OK FOR SERVICE. - [SDR FDEA201610063477](https://openairdocs.org/sdr/FDEA201610063477), Oct 6, 2016: FAN. INOPERATIVE. STRONG ELECTRICAL ODOR IN MAIN CARGO COMPARTMENT. ISOLATED ODOR TO THE NR 1 AFT EQUIPMENT EXHAUST FAN. REPLACED THE NR 1 AFT E & E COOLING SYS EXHAUST FAN IAW 2 - [SDR FDEA201607212592](https://openairdocs.org/sdr/FDEA201607212592), Jul 21, 2016: ACCESS DOOR. CRACKED. NR 11 SLAT OUTBOARD ACTUATOR DOOR CRACKED. REMOVED AND REPLACED THE DOOR IAW SRM 51-40-02. - [SDR FDEA201607212591](https://openairdocs.org/sdr/FDEA201607212591), Jul 21, 2016: ACCESS DOOR. CRACKED. NR 10 SLAT INBOARD SLAT ACTUATOR DOOR CRACKED. REMOVED AND REPLACED THE ACCESS DOOR IAW SRM 51-40-02. - [SDR FDEA201607212590](https://openairdocs.org/sdr/FDEA201607212590), Jul 21, 2016: ACCESS DOOR. CRACKED. NR 10 SLAT OUTBOARD SLAT ACTUATOR DOOR POSSIBLE CRACK. REMOVED AND REPLACED THE ACCESS DOOR IAW SRM 51-40-02. - [SDR FDEA201607212589](https://openairdocs.org/sdr/FDEA201607212589), Jul 21, 2016: SKIN. CRACKED. NR 9 SLAT OUTBOARD SLAT ACTUATOR DOOR CRACKED AT UPPER SCREW HOLES. REMOVED AND REPLACED THE NR 9 SLAT O/B ACTUATOR DOOR SKIN IAW SRM 51-40-02. - [SDR FDEA201606121973](https://openairdocs.org/sdr/FDEA201606121973), Jun 12, 2016: UNKNOWN. MALFUNCTIONED. MAIN CARGO DOOR FAILED TO OPEN. OPENED MANUALY. NOW MAIN CARGO DOOR FAILED TO CLOSE. IN THE PROCESS OF PREP TO R & R LIFT DRIVE ACTUATOR FOUND AFT RATCHET ARM C - [SDR FDEA201503120885](https://openairdocs.org/sdr/FDEA201503120885), Mar 12, 2015: ESCAPE ROPE. MISROUTED. FORWARD ENTRY ESCAPE ROPE NOT ROUTED CORRECTLY. ROUTED FWD ENTRY DOOR ESCAPE ROPE THRU CHANNELS IAW SMP. ROPE IN PROPER POSITION FOR USE. OK FOR SERVICE. - [SDR FDEA201411153711](https://openairdocs.org/sdr/FDEA201411153711), Nov 15, 2014: MODULE. FAULTY. AT LEVEL OFF AT CRUISE, NO NORMAL ALTITUDE ALERTING OCCURRED. NOTIFIED ATC, LEFT RVSM AIRSPACE. INSTALLED SERVICEABLE ALT ALERT MODULE M617 IAW AMM 34-16-01-4. ## 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 N102FE The FAA can reassign an N-number once a registration is cancelled. These aircraft carried N102FE before. - [Cancelled 2004-08-26](https://openairdocs.org/deregistered/N102FE-2004-08-26): Boeing 727-22C, S/N 19193, 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 --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.