# N350UP: 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: 37873
- Year built: 2012
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: April 14, 2012
- Certificate issued: April 16, 2012
- Expires: April 30, 2028
- Mode S code: A3E69D
- 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=350UP
- Page: https://openairdocs.org/aircraft/N350UP

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 N350UP.

## FAA accident and incident reports

None matched to N350UP.

## 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 IPXA2026012633485](https://openairdocs.org/sdr/IPXA2026012633485), Jan 22, 2026: WINDOW. LEAKING. RIGHT (F.O.) #2 WINDOW SEAL MADE VERY LOUD "BARKING" SOUND DURING CLIMB OUT AND FOR ABOUT 45 MINUTES DURING CRUISE. REPLACED F/O'S #2 WINDOW SEAL PER AMM 56-11-
- [SDR IPXA2025072210407](https://openairdocs.org/sdr/IPXA2025072210407), Jul 13, 2025: WINDOW. WARNING MESSAGE. ETOPS, L WINDOW MSG QRH ACTIONED MSG REMAINS DISPLAYED REPLACED L2 WINDOW IAW MM 56-11-02-404-026 OPS CHECK NORMAL
- [SDR IPXA2025071410407](https://openairdocs.org/sdr/IPXA2025071410407), Jul 13, 2025: WARNING MESSAGE. ILLUMINATED. LEFT WINDOW MSG QRH ACTIONED MSG REMAINS DISPLAYED. DEFERRED THE L2 WINDOW AS PER MEL 30-41-1-2. DMP C/W AND PLACARD INSTALLED
- [SDR IPXA2025060660934](https://openairdocs.org/sdr/IPXA2025060660934), Jun 5, 2025: RADIO. INOPERATIVE. **ATB**RADIO FAILURE BOTH L/R VHF RADIOS HAVE LOUD SIDE TONE, UNABLE TO RECEIVE -TRANSMIT AND RECEIVE REGAINED CAPTAIN RADIO WHEN SWITCHES IN ALT. CREW REPORT. 
- [SDR IPXA2024041612970](https://openairdocs.org/sdr/IPXA2024041612970), Apr 15, 2024: BATTERY. DISCHARGED. EXIT LIGHT BATTERY FAIL R/R EMERGENCY EXIT LIGHT BATTERY W/R/T MM 33-51-07.
- [SDR IPXA2024011214437](https://openairdocs.org/sdr/IPXA2024011214437), Dec 30, 2023: FORMER. CRACKED. FORMER RH WING OUTBD FXD LE NOSE SKIN, OSS 499.60 (REPLACE) I.A.W AMM 27-81-31-024-001 REV.140 REMOVED CURTAIN OF RH WING L/E FORMER ASSY, OSS 499.60. I.A.W AMM
- [SDR IPXA2024011214418](https://openairdocs.org/sdr/IPXA2024011214418), Dec 30, 2023: SKIN. BENT. FORMER, RH WING OUTBD FXD LE NOSE SKIN, OSS 565.90 (REPLACE) I.A.W AMM 27-81-31-024-001 REV.140 REMOVED CURTAIN OF RH WING L/E FORMER ASSY, OSS 565.9. I.A.W AMM
- [SDR IPXA2024010314437](https://openairdocs.org/sdr/IPXA2024010314437), Dec 30, 2023: UNKNOWN. UNKNOWN. *SDR FILED OPEN* FAULT - CRACK - FORMER RH WING OUTBD FXD LE NOSE SKIN, OSS 499.60 (REPLACE) OK TO WORK
- [SDR IPXA2024010314418](https://openairdocs.org/sdr/IPXA2024010314418), Dec 30, 2023: UNKNOWN. UNKNOWN. *SDR FILED OPEN* FAULT - BEND - FORMER, RH WING OUTBD FXD LE NOSE SKIN, OSS 565.90 (REPLACE) OK TO WORK
- [SDR IPXA2024010314319](https://openairdocs.org/sdr/IPXA2024010314319), Dec 30, 2023: ANGLE. CRACKED. CRACK - ANGLE AFT CARGO COMPARTMENT FWD SIDE AT STA 1087 RBL 18" (REPLACE) OK TO WORK. REMOVED DAMAGE PART I.A.W SRM 51-40-02-0G REV. 88. INSTALLED NEW PART I.A
- [SDR IPXA2024010314307](https://openairdocs.org/sdr/IPXA2024010314307), Dec 30, 2023: ANGLE. CRACKED. AFT CARGO COMPARTMENT FWD SIDE AT STA 1087 LBL 18" ANGLE (REPLACE) OK TO WORK REMOVED DAMAGE PART I.A.W SRM 51-40-02-0G REV. 88. INSTALLED NEW PART I.A.W SRM 51
- [SDR IPXA2024011279972](https://openairdocs.org/sdr/IPXA2024011279972), Dec 28, 2023: PANEL. ERODED. EROSION PNL SKIN, RH WING UPPER SURFACE PNL NO.611PT (REPAIR) REMOVE THE DAMAGE MATERIALS AND CLEAN.MEASURE THE DAMAGE AREA (LENGTH:2", WIDTH:1",4" FROM INBOARD
- [SDR IPXA2024011278974](https://openairdocs.org/sdr/IPXA2024011278974), Dec 28, 2023: FRAME. CRACKED. FAULT - CRACK - CLIP, INTERNAL AFTER OUTBOARD SIDE FRAME OF NO.1 PYLON AFTER FAIRING, NAC STA 376.20 (REPLACE) REMOVED DAMAGE PART I.A.W SRM 51-40-02-0G REV. 88
- [SDR IPXA2024010378974](https://openairdocs.org/sdr/IPXA2024010378974), Dec 28, 2023: UNKNOWN. UNKNOWN. *SDR FILED OPEN* FAULT - CRACK - CLIP, INTERNAL AFTER OUTBOARD SIDE FRAME OF NO.1 PYLON AFTER FAIRING, NAC STA 376.20 (REPLACE) PAPER OK
- [SDR IPXA2023122879972](https://openairdocs.org/sdr/IPXA2023122879972), Dec 28, 2023: UNKNOWN. UNKNOWN. *SDR FILED OPEN* FAULT - EROSION PNL SKIN, RH WING UPPER SURFACE PNL NO.611PT (REPAIR)
- [SDR IPXA2022012278134](https://openairdocs.org/sdr/IPXA2022012278134), Jan 10, 2022: NONE. NONE. INSPECTION TYPE:C5DISBOND DAMAGE ON R/H VST TORQUE BOX PANEL (P/N:175T2001-4) AT UPR FWD SIDE.REPAIR I.A.W BOEING SRID:3-5253366378 AND UPS EO B767-5530-82629-A
- [SDR IPXA2022012078048](https://openairdocs.org/sdr/IPXA2022012078048), Jan 10, 2022: NONE. NONE. INSPECTION TYPE:C5DISBOND DAMAGE ON L/H VST TORQUE BOX PANEL(P/N:175T2001-1)REPAIR I.A.W 767-300F SRM 55-30-1, REPAIR 1 , 767-300F SRM 51-70-10, REPAIR GENERAL 
- [SDR IPXA2021060870314](https://openairdocs.org/sdr/IPXA2021060870314), Jun 8, 2021: ENGINE. UNRESPONSIVE. INSPECTION TYPE:NA**DIV-EMERG DECL'D-NO EQUIP USED-LANDED UNEVENTFUL** RT ENGINE NOT RESPONDING TO HIGHER COMMANDED N1 AT ALTITUDE(APPARENT MAX AVAIL 89.1 N1/W 
- [SDR IPXA2020050654994](https://openairdocs.org/sdr/IPXA2020050654994), May 4, 2020: UNKNOWN. ODOR. INSPECTION TYPE:N/ACHEMICAL SMELL AT FL 350 POSSIBLY OZONE - SUBTLE USED O2 UNTIL 17000 NO SMELL AT THIS ALT. CONTINUED W/O O2 THERE AFTER.C/W SMOKE ODOR IN COC
- [SDR IPXA2019112759406](https://openairdocs.org/sdr/IPXA2019112759406), Nov 25, 2019: OIL SYSTEM. LOW. INSPECTION TYPE:ETOPAPU FAULT LIGHT IS ON & ECIAS MSG, MAKE TWO ATTEMPTS TO START THE APU DURING TAXI IN BOTH TIMES RECIEVED APU FAULTAPU LOW OIL LEVEL, SERVICE
- [SDR IPXA2019071944625](https://openairdocs.org/sdr/IPXA2019071944625), Jul 18, 2019: WARNING SYSTEM. FALSE ACTIVATION. INSPECTION TYPE:N/A DURING TAXI AFTER LANDING EICAS MSG INTERMITTENT "L FWD ENT DOOR" WITH ACARS INITIALIZE PAGE CAME ON. DOOR WARNING SENSOR TEST ACCOMPLISHED 
- [SDR IPXA2017072419691](https://openairdocs.org/sdr/IPXA2017072419691), Jul 21, 2017: TARGET. UNSECURE. LT FWD ENTRY DOOR EICAS ON GROUND WITH DOOR CLOSED. SECURED DOOR CLOSE SENSOR TARGET PLATE. CHECKED OK IAW AMM 52-71-00-825-141.
- [SDR IPXA2017053017725](https://openairdocs.org/sdr/IPXA2017053017725), May 30, 2017: CONTROL PANEL. SMOKE. ENROUTE, NOTICED ELECTRICAL FIRE ODOR BRIEFLY. ODOR OF SMOKE FROM TRANSPONDER. SMOKE STOPPED AND ODOR DISRUPTED. NO ISSUES WITH EQUIPMENT OR PLANE, ALL FUNCTION
- [SDR IPXA2016080806763](https://openairdocs.org/sdr/IPXA2016080806763), Aug 7, 2016: DOOR. UNKNOWN. CREW ENTRY DOOR HARD TO SLIDE OPEN OR CLOSED. R & R L1 ENTRY CEILING COVER PANEL IAW AMM 52-12.
- [SDR IPXA2016033101425](https://openairdocs.org/sdr/IPXA2016033101425), Mar 30, 2016: FLOOR PANEL. DAMAGED. INSPECTION TYPE: C2, FOUND DAMAGE ON M/D CARGO FLOOR PANEL 252WF AT BS 1598. FABRICATED THE REPLACEMENT FLOOR PANEL IAW EO NR B767-5320-9693-I.
- [SDR IPXA2015101994914](https://openairdocs.org/sdr/IPXA2015101994914), Oct 18, 2015: ROD. OUT OF ADJUST. LIFE RAFT CONTAINER TOP WILL NOT CLOSE PROPERTY. ADJUSTED ROD IAW AMM 25-60-00, OPS CHECK GOOD.
- [SDR IPXA2015020985629](https://openairdocs.org/sdr/IPXA2015020985629), Feb 5, 2015: DOOR. BINDING. MAIN ENTRY DOOR JAMMED ON CLOSING CHECKED ADJUSTMENT OF CREW ENTRY DOOR IAW AMM 52-12-00-715-110. CHECKED GOOD.
- [SDR IPXA2015012185390](https://openairdocs.org/sdr/IPXA2015012185390), Jan 18, 2015: HARNESS. DAMAGED. CRABINER MISSING AT EMERGENCY ESCAPE DESCENT HARNESS CENTER SUPERNUMERARY SEAT. REPLACED HARNESS ASSY IAW MM 25-61-03-4, CHECKS OK.
- [SDR IPXA3676938](https://openairdocs.org/sdr/IPXA3676938), Feb 3, 2013: SKIN. CRACKED. RT OTBD FLAP, OTBD END L/E SKIN PANEL CRACKED AND DEFLECTED. REPAIRED IAW EO B767-5750-49506-B.

## 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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