# N347UP: 2012 Boeing 767-34AF

- Status: Valid registration
- Airframe: [Boeing 767-34AF](https://openairdocs.org/model/boeing-767-34af) (registry code 1385212, 190 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: 37871
- Year built: 2012
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: January 30, 2012
- Certificate issued: February 1, 2012
- Expires: February 29, 2028
- Mode S code: A3D91F
- Registered owner: [C C & E I LLC](https://openairdocs.org/faa-owner/C%20C%20%26%20E%20I%20LLC)
- Location: [Louisville, KY](https://openairdocs.org/faa-place/KY/Louisville)
- Owner type: LLC
- Owner's area on the map: 38.2585° N, 85.5398° W: Placed by OpenAirDocs at the center of ZIP code 40223, within about 2 miles (OpenAirDocs). The owner's mailing address, not where the aircraft is based
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=347UP
- Page: https://openairdocs.org/aircraft/N347UP

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 767-34AF)

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 N347UP.

## FAA accident and incident reports

None matched to N347UP.

## 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 IPXA2026050535451](https://openairdocs.org/sdr/IPXA2026050535451), May 5, 2026: LIGHT SYS. INTERMITTENT. EMER LIGHTS ON INTERMITTENTLY WITH TOGGLE SWITCH IN ARMED POSITION AND GUARD CLOSED FOUND GUARD FOR EMERGENCY LIGHT SWITCH NOT CORRECT INSTALLED. RE-INSTALLED G
- [SDR IPXA2026030381295](https://openairdocs.org/sdr/IPXA2026030381295), Mar 2, 2026: POWER SUPPLY. INOPERATIVE. EMERGENCY LIGHT WILL NOT COME ON. REMOVED & REPLACED THE EMERGENCY POWER SUPPLY IAW AMM 33-51-07/201. OPS TESTED GOOD.
- [SDR IPXA2025121553721](https://openairdocs.org/sdr/IPXA2025121553721), Dec 3, 2025: SKIN. PUNCTURED. MAJOR REPAIR. INSPECTED LEFT OTBD AILERON IAW SRM 57-60-02-1A-1 TABLE I NOTE A AND D. PERFORMED PERMANENT REPAIR PER EO-95924-REQ2.
- [SDR IPXA2025082300630](https://openairdocs.org/sdr/IPXA2025082300630), Aug 16, 2025: PLATE. CORRODED. CORRODED PLATE, AFT WING TO BODY LOWER KEELBEAM AFT SECTION. INSTALLED NEW PLATE IAW SRM 51-40-02-0G REV 93, & DWG 145T8610, SHT 9, REV D & 145T8610, SHT 13, RE
- [SDR IPXA2025082981252](https://openairdocs.org/sdr/IPXA2025082981252), Aug 15, 2025: SUPPORT BRACKET. CRACKED. CRACK-CLIP, NO.1 ENG IDG/OIL COOLER SENING TUBE SUPPORT CLIP.I.A.W. AMM 20-11-00-910-802 REV.145 REPLACED THE CLIP
- [SDR IPXA2025081500252](https://openairdocs.org/sdr/IPXA2025081500252), Aug 15, 2025: SUPPORT ANGLE. CRACKED. -CRACK-CLIP, NO.1 ENG IDG/OIL COOLER SENING TUBE SUPPORT CLIP OK TO WORK
- [SDR IPXA2025082965432](https://openairdocs.org/sdr/IPXA2025082965432), Aug 14, 2025: DUCT. CRACKED. NUMBER 1 ENG LPT ACC MANIFOLD 6:00 POS.I.A.W. AMM 75-24-03-004-050-H00 REV.145 AND AMM 75-24-03-404-037-H00 REV.145 REPLACED THE DUCT.
- [SDR IPXA2025081565432](https://openairdocs.org/sdr/IPXA2025081565432), Aug 14, 2025: DUCT. CRACKED. CRACK- DUCT, NR 1 ENG LPT ACC MANIFOLD 6:00 POS. OK TO WORK
- [SDR IPXA2025082141090](https://openairdocs.org/sdr/IPXA2025082141090), Aug 13, 2025: STIFFENER. CRACKED. CRACK - ANGLE, FWD MEC AT STA 246 LBL 40 FLOOR STRUCTURE. .ACCOMPLISHED REPAIR I.A.W SRM 53-10-51-2R-4 REV.92 AND EGAT WORK SHEET NO.50647
- [SDR IPXA2025081621930](https://openairdocs.org/sdr/IPXA2025081621930), Aug 12, 2025: WEB. CRACKED. CRACKED WEB, AFT LOWER CARGO COMPT ENTRYWAY AT STA 1329 LBL 2.2. .I.A.W AMM 20-11-00-910-802 REV.145 REMOVED BALL PANEL SUPPORT FITTING.FABRICATE P/N: 451T2603-
- [SDR IPXA2025081107546](https://openairdocs.org/sdr/IPXA2025081107546), Aug 11, 2025: SEAL. BROKEN. FOUND THE CREW ENTRY DOOR AFT DOORWAY LINING SEAL BROKEN. OK TO WORK. OPEN
- [SDR IPXA2024011037383](https://openairdocs.org/sdr/IPXA2024011037383), Jan 9, 2024: DOOR. OFF TRACK. UPPER PORTION OF ENTRY DOOR SEAL, FWD SIDE IS OUT OF RETAINING TRACK RE-INSTALLED CREW ENTRY DOOR LINING TRIM SEAL IAW AMM 52-12-02.
- [SDR IPXA2024010884970](https://openairdocs.org/sdr/IPXA2024010884970), Jan 5, 2024: SKIN. GOUGED. FOUND A 1" LONG GOUGE NEAR FWD LOWER CARGO DOOR BETWEEN STA 500 AND 456. 24" FWD OF FWD LOWER CARGO DOOR. MEASUREMENTS - LENGTH 1" / DEPTH 0.01** RESTORED FINIS
- [SDR IPXA2023113003785](https://openairdocs.org/sdr/IPXA2023113003785), Nov 22, 2023: DOOR. INOPERATIVE. MAIN ENTRY DOOR ARM HANDLE COVER NOT FLUSH. INSTALLED NEW HINGE ASSY IAW AMM 52-11-00, OPS CK GD, MEL CLOSED AND PLACARED REMOVED
- [SDR IPXA2023112203785](https://openairdocs.org/sdr/IPXA2023112203785), Nov 22, 2023: UNKNOWN. UNKNOWN. *SDR FILED OPEN* MAIN ENTRY DOOR ARM HANDLE COVER NOT FLUSH. DEFERED IAW MEL 52-11-2, NO DMP REQUIRED.
- [SDR IPXA2023091152654](https://openairdocs.org/sdr/IPXA2023091152654), Sep 6, 2023: SPAR. CRACKED. *MAJOR REPAIR* FAULT - CRACK - STIFFENER WING CENTER FRONT SPAR CRACK IS STIFFENERS AT STA 789.5 RBL 55 (REPAIR) ACCOMPLISHED REPAIR I.A.W SRM 57-10-10-2R-2 REP
- [SDR IPXA2023032392189](https://openairdocs.org/sdr/IPXA2023032392189), Mar 23, 2023: LIGHT. INOPERATIVE. INSPECTION TYPE:NAGUARD COVER ON EMERGENCY EXIT LIGHTS SPRING BROKEN AND CAUSES EMERGENCY LIGHTS TO ILLUMINATE INTERMITTENTLYREPAIR EMER LIGHT COVER, CHK NORMAL
- [SDR IPXA2022040180726](https://openairdocs.org/sdr/IPXA2022040180726), Apr 1, 2022: FIRE WARNING. FALSE ACTIVATION. L ENG FIRE LOOP STATUS MESSAGE. C/W AFOLTS TEST PER 26 11 00 715 001 NO FAULTS NOTED DISCONNECTED D4200P AND D4230P AND CHECKED RESISTANCE OF ALL WIRE SEGMENTS 
- [SDR IPXA2021031967007](https://openairdocs.org/sdr/IPXA2021031967007), Mar 18, 2021: ESCAPE REEL. BROKEN. EMERGENCY ESCAPE DESCENT DEVICE FELL FROM CONTAINERREMOVED AND REPLACED EMERGENCY ESCAPE DESCENT DEVICE REF AMM 25-61-03-201 SN ON 26164 SN OFF 21927
- [SDR IPXA2020082659510](https://openairdocs.org/sdr/IPXA2020082659510), Aug 25, 2020: FLIGHT DIR. INOPERATIVE. AIR TURNBACK AFTER TAKE OFF FO,S FLT DIR DISAPPEARED. ALSO NO LAND 3 DISPLAYED. IN CLIMB RPDF DISPLAYED VNAV. LPDF DISPLAYED VNAV PATH. RT SIDE PDF ALT. WINDOW 
- [SDR IPXA2019082876063](https://openairdocs.org/sdr/IPXA2019082876063), Aug 15, 2019: FLOOR PANEL. DAMAGED. INSPECTION TYPE:C4DAMAGE ON M/D CARGO FLOOR PANEL AT STA 685- STA 730, LBL 11- RBL 11, PNL NO. 231RFF.FABRICATE THE REPLACEMENT FLOOR PANEL PER EO NO. B767-5320
- [SDR IPXA2019082876062](https://openairdocs.org/sdr/IPXA2019082876062), Aug 15, 2019: FLOOR PANEL. DAMAGED. INSPECTION TYPE:C4, DAMAGE ON M/D CARGO FLOOR PANEL AT STA 412- STA 535, RBL 55 -RBL 77, PNL NO. 232CFF.FABRICATE THE REPLACEMENT FLOOR PANEL PER EO NO. B767-53
- [SDR IPXA2019072844958](https://openairdocs.org/sdr/IPXA2019072844958), Jul 28, 2019: FLOOR PANEL. PUNCTURED. INSPECTION TYPE:N/A MCD FLOOR PANEL 10R PUNCTURE .5"X.125" 8"FROM RT SIDE, 42" FROM FWD EDGE. REPAIRED IAW SRM 53-00-50.
- [SDR IPXA2019072844957](https://openairdocs.org/sdr/IPXA2019072844957), Jul 28, 2019: FLOOR PANEL. DAMAGED. INSPECTION TYPE:N/A MCD FLOOR PANEL 12L DAMAGED 1.5"X.25" HOLE 3" FROM RT SIDE 5" FROM FWD EDGEREPAIRED IAW SRM 53-00-50.
- [SDR IPXA2018111425902](https://openairdocs.org/sdr/IPXA2018111425902), Nov 9, 2018: COVER. DAMAGED. MAIN ENTRY DOOR HINGE COVER WAS INOPERATIVE. REMOVED, REPAIRED AND INSTALLED THE COVER IAW AMM 52-12-02.
- [SDR IPXA2018070231279](https://openairdocs.org/sdr/IPXA2018070231279), Jul 2, 2018: SKIN. DAMAGED. BULK CARGO DOOR OUTER SKIN DENTED AND GOUGED. REPAIR DOUBLER INSTALLED IAW EO 767-5230-67878-D.
- [SDR IPXA2017100322282](https://openairdocs.org/sdr/IPXA2017100322282), Oct 2, 2017: SPRING. DAMAGED. ENTRY DOOR ARMING LEVER COVER HAS A DAMAGED HINGE SPRING. ADJUSTED AND ALIGNED IAW AMM 20-00-00. OPS CHECKED GOOD.
- [SDR IPXA2017062118480](https://openairdocs.org/sdr/IPXA2017062118480), Jun 20, 2017: CARBON SEAL. LEAKING. DURING GENERATOR CHANGE ON THE RT ENGINE, FOUND THE CARBON SEAL LEAKING. REMOVED AND REPLACED THE CARBON SEAL IAW AMM 72-64-02-404-028-H00. LEAK CHECKED GOOD.
- [SDR IPXA2015022486375](https://openairdocs.org/sdr/IPXA2015022486375), Feb 23, 2015: SEAL. LOOSE. CREW ENTRY DOOR HAS EXCESSIVE NOISE LEVEL FROM AIR LEAKAGE, FOUND DOOR SEAL/ LWR CTR SECTION PULLED LOOSE APPROXIMATELY 4". REINSTALLED SEAL IAW AMM 52-09-01, P
- [SDR IPXA2014043082810](https://openairdocs.org/sdr/IPXA2014043082810), Apr 27, 2014: DIODE. INOPERATIVE. AIR TURNBACK, IN FLIGHT, THE LT MLG DOWN AND LOCKED LIGHT WOULD NOT GO OUT. R & R THE MAIN GEAR DIODE CARD NO HELP. SYSTEM FAILED THE GEAR POSITION TEST IN AMM.
- [SDR IPXA12671783](https://openairdocs.org/sdr/IPXA12671783), Feb 16, 2012: BUSS. INOPERATIVE. INSPECTION TYPE: E TOP, DURING APPROACH WITH FLAPS & GEAR UP, AUOPILOT AUTO THROTTLE ENGAGED, PASSING THRU HEAVY RAIN, MULTIPLE SIMULTANEOUS EICAS MESSAGES OCCU

## 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 767-34AF aircraft: https://openairdocs.org/model/boeing-767-34af/aircraft.md
- The GE CF6-80C2B6F engine: https://openairdocs.org/engine/ge-cf6-80c2b6f.md

---
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