# N335UP: 2009 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: 37856
- Year built: 2009
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: July 17, 2009
- Certificate issued: August 20, 2009
- Expires: February 29, 2028
- Mode S code: A3AA32
- 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=335UP
- Page: https://openairdocs.org/aircraft/N335UP

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 N335UP.

## FAA accident and incident reports

None matched to N335UP.

## Service difficulty reports (50)

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 IPXA2025020159321](https://openairdocs.org/sdr/IPXA2025020159321), Jan 24, 2025: FLOOR PANEL. DENTED. PANEL , MAIN DECK CARGO COMPARTMENT FLOOR PANEL DENT BETWEEN STA 1197+22 AND STA 1197+132 , LBL 75 ~ LBL 90 P/N : 146T5869-9 (REPAIR). FABRICATE A NEW FLOOR PAN
- [SDR IPXA2025020159637](https://openairdocs.org/sdr/IPXA2025020159637), Jan 24, 2025: FLOOR PANEL. DENTED. FLOOR PANEL , MAIN DECK CARGO COMPARTMENT FLOOR PANEL DENT BETWEEN STA 1197+110 AND STA 1197+22 , RBL 77.5 ~ RBL 88.5 P/N : 146T5869-10 (REPAIR). FABRICATE A NE
- [SDR IPXA2025020159212](https://openairdocs.org/sdr/IPXA2025020159212), Jan 24, 2025: FLOOR PANEL. DENTED. DENT - PANEL , MAIN DECK CARGO COMPARTMENT FLOOR PANEL DENT BETWEEN STA 1087 AND STA 1197+22 LBL 77.5 ~ LBL 88.5 P/N : 146T5869-1 (REPAIR). FABRICATE A NEW FLOO
- [SDR IPXA2025020159377](https://openairdocs.org/sdr/IPXA2025020159377), Jan 24, 2025: FLOOR PANEL. DENTED. *SUPPLEMENTAL SDR* FAULT - DENT - PANEL , MAIN DECK CARGO COMPARTMENT FLOOR PANEL DENT BETWEEN STA 731.11 AND STA 834 RBL11 ~ RBL33 P/N : 145T5876-67 (REPAIR). 
- [SDR IPXA2025020159234](https://openairdocs.org/sdr/IPXA2025020159234), Jan 24, 2025: FLOOR PANEL. DENTED. MAIN DECK CARGO COMPARTMENT FLOOR PANEL DAMAGE BETWEEN STA 764 AND STA 875 , RBL 77.5 ~ RBL 88.5 P/N : 145T5876-7 (REPAIR). FABRICATE A NEW FLOOR PANEL I.A.W. S
- [SDR IPXA2025020159328](https://openairdocs.org/sdr/IPXA2025020159328), Jan 24, 2025: FLOOR PANEL. DAMAGED. MAIN DECK CARGO COMPARTMENT FLOOR PANEL DAMAGE BETWEEN STA 1451 AND STA 1540 , LBL 75 ~ LBL 90 P/N : 146T5869-88 (REPAIR). FABRICATE A NEW FLOOR PANEL I.A.W. SR
- [SDR IPXA2025013136383](https://openairdocs.org/sdr/IPXA2025013136383), Jan 23, 2025: FLOOR PANEL. DAMAGED. MAIN DECK CARGO COMPARTMENT FLOOR PANEL DAMAGE BETWEEN STA 1451 AND STA 1540 LBL 75 ~ LBL 90 P/N : 146T5869-89 (REPAIR). FABRICATE A NEW FLOOR PANEL I.A.W. SREO
- [SDR IPXA2025012204020](https://openairdocs.org/sdr/IPXA2025012204020), Jan 21, 2025: FLOOR PANEL. DAMAGED. FOUND MAIN DECK FLOOR PANEL DAMAGE , P/N : 143T5876-83 PANEL NO : 231GFF (REPAIR). FABRICATE A NEW FLOOR PANEL I.A.W. SREO-9693-REQ001 REV.4. CONDITION CHECK IS
- [SDR IPXA2025020189621](https://openairdocs.org/sdr/IPXA2025020189621), Jan 20, 2025: FLOOR PANEL. DAMAGED. FOUND MAIN DECK FLOOR PANEL DAMAGE, P/N : 146T5869-90 PANEL NO : 252WFF (REPAIR). FABRICATE A NEW FLOOR PANEL I.A.W. SREO-9693-REQ001 REV.4. CONDITION CHECK IS 
- [SDR IPXA2025011978340](https://openairdocs.org/sdr/IPXA2025011978340), Jan 19, 2025: FLOOR PANEL. DAMAGED. FOUND MAIN DECK FLOOR PANEL DAMAGE, P/N: 143T5876-58 PANEL NO.231RFF (REPAIR). FABRICATE A NEW FLOOR PANEL I.A.W. SREO-9693-REQ001 REV.4. I.A.W AMM 25-57-05-404
- [SDR IPXA2025021279655](https://openairdocs.org/sdr/IPXA2025021279655), Jan 19, 2025: SEAL. DAMAGED. FOUND THE CREW ENTRY DOOR FORWARD DOORWAY SEAL WITH BROKEN DAMAGE (REPLACE). I.A.W AMM 52-12-02-004-001 REV.144 AND AMM 52-12-02-404-025 REV.144 REPLACED SEAL.
- [SDR IPXA2025021279447](https://openairdocs.org/sdr/IPXA2025021279447), Jan 19, 2025: BUFFER. FAILED. FOUND FLIGHT DECK LEFT RAFT AND STOWAGE GAS STRUT BUFFER FUNCTION FAIL (REPLACE). I.A.W AMM 20-11-00-912-802 REV.144 REPLACED STOWAGE GAS STRUT BUFFER.
- [SDR IPXA2025011978338](https://openairdocs.org/sdr/IPXA2025011978338), Jan 19, 2025: FLOOR PANEL. DAMAGED. FOUND MAIN DECK FLOOR PANEL DAMAGE, P/N: 146T5869-62 PANEL NO.252BFF (REPAIR). FABRICATE A NEW FLOOR PANEL I.A.W. SREO-9693-REQ001 REV.4. I.A.W AMM 25-57-05-404
- [SDR IPXA2025011978332](https://openairdocs.org/sdr/IPXA2025011978332), Jan 19, 2025: FLOOR PANEL. DAMAGED. FOUND MAIN DECK FLOOR PANEL DAMAGE, P/N:146T5869-68 PANEL NO:252GFF (REPAIR). FABRICATE A NEW FLOOR PANEL I.A.W. SREO-9693-REQ001 REV.4. I.A.W AMM 25-57-05-404-
- [SDR IPXA2025012179447](https://openairdocs.org/sdr/IPXA2025012179447), Jan 19, 2025: LIFE RAFT. NO TEST. FOUND FLIGHT DECK LEFT RAFT 4AND STOWAGE GAS STRUT BUFFER FUNCTION FAIL (REPLACE) OK TO WORK
- [SDR IPXA2025012179655](https://openairdocs.org/sdr/IPXA2025012179655), Jan 19, 2025: SEAL. BROKEN. FOUND THE CREW ENTRY DOOR FORWARD DOORWAY SEAL WITH BROKEN DAMAGE (REPLACE) OK TO WORK
- [SDR IPXA2025012198340](https://openairdocs.org/sdr/IPXA2025012198340), Jan 19, 2025: FLOOR PANEL. DAMAGED. FOUND MAIN DECK FLOOR PANEL DAMAGE, P/N: 143T5876-58 PANEL NO.231RFF (REPAIR) REQUEST UPS ENGINEERING DETERMINE MAJOR OR MINOR REPAIR. OPEN
- [SDR IPXA2025011969173](https://openairdocs.org/sdr/IPXA2025011969173), Jan 18, 2025: FLOOR PANEL. DAMAGED. FOUND MAIN DECK FLOOR PANEL DAMAGE, P/N: 143T5876-19 PANEL NO: 231QFF. (REPAIR). FABRICATE A NEW FLOOR PANEL I.A.W. SREO-9693-REQ001 REV.4. I.A.W AMM 25-57-05-4
- [SDR IPXA2023110224349](https://openairdocs.org/sdr/IPXA2023110224349), Oct 30, 2023: DOUBLER. DAMAGED. *** MAJOR REPAIR *** LAV. SERVICE DOOR LAND DOUBLER DAMAGED. REF. FAULT T3F18E00359LY. ASSIGNED EO-88577-REQ1 FOR PERMANENT REPAIR. ALL STEPS OF FINAL EO HAVE B
- [SDR IPXA2023100941831](https://openairdocs.org/sdr/IPXA2023100941831), Oct 6, 2023: ACTUATOR. CRACKED. *** SUPPLEMENT SDR *** #2 ENGINE, THE L/H UPPER SIDE T/R ACTUATOR BALLSCREW WAS CORRSION AND ACTUATOR END WAS CRACKED. DURING LUB T/R BALLSCREW NUT FOUND. ACCOM
- [SDR IPXA2023100641831](https://openairdocs.org/sdr/IPXA2023100641831), Oct 6, 2023: UNKNOWN. UNKNOWN. *SDR FILED OPEN* #2 ENGINE, THE L/H UPPER SIDE T/R ACTUATOR BALLSCREW WAS CORRSION AND ACTUATOR END WAS CRACKED. DURING LUB T/R BALLSCREW NUT FOUND. NO PARTS IN
- [SDR IPXA2023032692249](https://openairdocs.org/sdr/IPXA2023032692249), Mar 19, 2023: ANGLE. CRACKED. INSPECTION TYPE:C7CRACK ON THE ANGLE(P/N:146T5651-5)OF THE MAIN DECK FLOOR STRUCTURE NEAR STA 1577 AND LBL 79.INSTALL NEW PART I.A.W BOEING DWG NO.:146T5650 SH 
- [SDR IPXA2023032692248](https://openairdocs.org/sdr/IPXA2023032692248), Mar 19, 2023: ANGLE. CRACKED. INSPECTION TYPE:C7CRACK ON THE ANGLE(P/N:146T5651-6)OF THE MAIN DECK FLOOR STRUCTURE NEAR STA 1577 AN RBL 79.INSTALL NEW PART I.A.W BOEING DWG NO.:146T5650 SH 5
- [SDR IPXA2023032792279](https://openairdocs.org/sdr/IPXA2023032792279), Mar 18, 2023: UNKNOWN. CRACKED. INSPECTION TYPE:C7CRACK ON THE CLIP(P/N:140T0130-38)OF THE AFT CGO COMPT NEAR STA 1087 AND RBL 26.INSTALL NEW PART I.A.W 767-300F SRM 51-40-02-0G,REV 85.01 AND 
- [SDR IPXA2023032292117](https://openairdocs.org/sdr/IPXA2023032292117), Mar 17, 2023: SKIN. UNKNOWN. INSPECTION TYPE:C7*MAJOR REPAIR* FUSELAGE DRAIN HOLES ADDITION AND INSPECTION AFT OF STA 1725.5 BETWEEN S-36L AND S-36R.PERFORM UPS EO B767-2740-82173-C APPX B.
- [SDR IPXA2022071184033](https://openairdocs.org/sdr/IPXA2022071184033), Jul 10, 2022: DOOR SEAL. LEAKING. INSPECTION TYPE:N/ADURING CLIMB PHASE OF FLIGHT THERE WAS A LOAD HISSING NOISE COMING FROM THE MAINN CREW ENTRY DOORFOUND LWR BOTTOM DOOR SEAL OUT OF TRACK. REP
- [SDR IPXA2022040980995](https://openairdocs.org/sdr/IPXA2022040980995), Apr 9, 2022: FLOOR PANEL. CRACKED. INSPECTION TYPE:N/AMAIN DECK FLOOR PANEL POSITION 4 L DAMAGED IN MULTIPLE LOCATIONSFABRICATED NEW FLOOR PANEL IAW EO B767-5320-9693-I
- [SDR IPXA2021072171933](https://openairdocs.org/sdr/IPXA2021072171933), Jul 21, 2021: RETAINER. NOT SEATED. INSPECTION TYPE:NAL1 DR SEAL HAS MULTIPLE REPORTS OF HISSING /SQUEALING. SEAL WILL NOT SEAT PROPERLY IN LOWER FWD SEAL RETAINER OF L1 CREW ENTRY DOORR/R SEAL PE
- [SDR IPXA2021070871437](https://openairdocs.org/sdr/IPXA2021070871437), Jul 7, 2021: SEAL. OBSTRUCTED. AFTER TAKEOFF PASSING 5000 FEET WE HEARD VERY LOUD HISSING FROM LOWER SECTION OF ENTRY DOOR. CONTINUED ENTIRE FLIGHT. PRESSURAZITION IN CABIN WAS NORMALRESECURE
- [SDR IPXA2021042768695](https://openairdocs.org/sdr/IPXA2021042768695), Apr 27, 2021: SEAL. LEAKING. INSPECTION TYPE:N/AFAIRLY LOUD PRESSURE AIR LEAK BY COCKPIT DOOR AREA. APPEARS TO BE FROM LWR FWD AREA OF DOOR. STARTED AT 2.5 PSI AND CONTINUED AT HIGHER AP.RE
- [SDR IPXA2021030266282](https://openairdocs.org/sdr/IPXA2021030266282), Feb 21, 2021: STIFFENER. CRACKED. INSPECTION TYPE:C6CRACK ON CENTER WING TANK STIFFENER(P/N:111T2008-12) ON STA 785.9,RBL 33.REPAIR I.A.W 767-300F SRM 57-10-10-2R-2 REPAIR 2 REV.79.01 AND UPS EO
- [SDR IPXA2021021065535](https://openairdocs.org/sdr/IPXA2021021065535), Feb 9, 2021: SEAL. LEAKING. INSPECTION TYPE:N/ACREW ENTRY DOOR HAS NOISE FROM AIR LEAK. DIFFICULT TO DETERMINE EXACT AREA, SEEMS TO BE LOWER AFTCLEANED ENTRANCE DOOR LOWER SEANL AND REPOST
- [SDR IPXA2020080128740](https://openairdocs.org/sdr/IPXA2020080128740), Aug 6, 2020: INDICATOR. INOPERATIVE. DIVERSION - EMERGENCY DECLARED**AFTER LEVELOFF R FUEL GAUGE STARTED TO DECREASE EXCESSIVELY -APPROX 5000 IMBAL- WITH FUEL CONFIG LIGHT - ACCOMPLISHED CHECKLIST 
- [SDR IPXA2020012205103](https://openairdocs.org/sdr/IPXA2020012205103), Jan 19, 2020: SEAL. LEAKING. PASSING 8000 FT DURING CLIMBOUT WE HEARD AIR ESCAPING FROM CREW ENTRY DOOR. IRO DISCOVERED LEAK WAS AT THE BOTTOM OF DOOR. CABIN PRESSURIZATION WAS NORMAL DURIN
- [SDR IPXA2019122085173](https://openairdocs.org/sdr/IPXA2019122085173), Dec 18, 2019: BATTERY. INOPERATIVE. INSPECTION TYPE:N/AFLT DEL EMERGENCY LIGHTS INOPR&R'D FLT DECK EMERGENCY LIGHTS BATTERY PACK REF AMM 33-51-07 OPS CHKS NORMAL PER SAME IPC 33-51-07-032-020
- [SDR IPXA2019080245243](https://openairdocs.org/sdr/IPXA2019080245243), Aug 1, 2019: LAMP. INOPERATIVE. EXTERIOR EMERGENCY LIGHT INOPERATIVE. REPLACED THE LAMP IAW AMM 33-51-169-62-001. OPS CHECKED GOOD.
- [SDR IPXA2019052842566](https://openairdocs.org/sdr/IPXA2019052842566), May 28, 2019: TARGET. DEFECTIVE. INSPECTION TYPE:N/A ATB - FLAPS EICAS MESSAGE AFTER T/O. CONFIG LT AND HORN ALSO CAME ON AND WAS UNABLE TO CANCEL EITHER. REMOVED AND REPLACED RT SIDE (SYS 2) N
- [SDR IPXA2019052842564](https://openairdocs.org/sdr/IPXA2019052842564), May 25, 2019: TRANSDUCER. FAULTY. INSPECTION TYPE:N/A ATB - ANTISKID MESSAGE ON EICAS INTERMITTANT. ACCOMPLISHED FIM 32-42-00-815-803, FOUND #4 XDCR FAULTY. NOTE: ALSO REF ITEM 2 AND 3 THIS LOGP
- [SDR IPXA2019022739500](https://openairdocs.org/sdr/IPXA2019022739500), Feb 17, 2019: FLOOR PANEL. DAMAGED. INSPECTION TYPE:C5DAMAGE ON M/D CARGO FLOOR PANEL AT STA 972 -STA 1112 , RBL 11 - RBL 33, PNL NO.242SFF.FABRICATE THE REPLACEMENT FLOOR PANEL PER EO NO.B767-532
- [SDR IPXA2018071831731](https://openairdocs.org/sdr/IPXA2018071831731), Jul 14, 2018: LIGHT. INOPERATIVE. EMERGENCY LIGHTS INOP. T/S PER FIM 33-51-00-815-803. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACK REF AMM 33-51-07-022-001 AND AMM 33-51-07-422-012. OPS CK
- [SDR IPXA2018071631659](https://openairdocs.org/sdr/IPXA2018071631659), Jul 14, 2018: BATTERY PACK. DISCHARGED. INSPECTION TYPE:PS1, EMERGENCY LIGHT INOP. T/S PER FIM 33-51-00-815-803. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACK REF AMM 33-51-07-022-001 AND AMM 33-5
- [SDR IPXA2017121024332](https://openairdocs.org/sdr/IPXA2017121024332), Dec 9, 2017: SEAL. DAMAGED. INSPECTION TYPE:ETOPL/H ENG LEFT BULLNOSE SEGMENTS 3,4,5 FROM TOP 3" TOTAL DAMAGE.
- [SDR IPXA2017110423254](https://openairdocs.org/sdr/IPXA2017110423254), Oct 31, 2017: SEAL. LEAKING. A VERY LOUD AIR LEAK IS FROM THE MAIN ENTRY DOOR. PRESSURIZATION IS NORMALCREW ENTRY DOOR CHECK C/OUT IAW AMM 52-12-00-206-001 REV DATE 10/10/17. NO DAMAGE FOUN
- [SDR IPXA2016111710726](https://openairdocs.org/sdr/IPXA2016111710726), Nov 16, 2016: GUARD. INOPERATIVE. EMERGENCY LIGHTS DO NOT ARM PROPERLY. R & R SWITCH GUARD IAW CMM 33-51-04. OPS CHECKED OK
- [SDR IPXA2014050582866](https://openairdocs.org/sdr/IPXA2014050582866), May 4, 2014: SKIN. DAMAGED. RUDDER T/E HAS L/S DAMAGE 98" BELOW TOP OF PANEL. REPAIRED IAW EO B767-5540-53929-B.
- [SDR IPXA3678353](https://openairdocs.org/sdr/IPXA3678353), May 17, 2013: WEDGE. DENTED. INSPECTION TYPE: C2, A DENT WITH DELAMINATION WAS FOUND ON LT WING OTBD FLAP. REPAIRED IAW SRM 57-53-01 REV.56. REPAIR 1, FIG 201, TABLE II AND SRM 51-70-06 REV
- [SDR IPXA13677787](https://openairdocs.org/sdr/IPXA13677787), Apr 7, 2013: FLOOR PANEL. DAMAGED. MAIN CARGO DECK FLOOR PANEL HAS LARGE HOLE THROUGH BOTH SKINS AND CORE. FABRICATED NEW FLOOR PANEL IAW EO B767-5320-9693-H.
- [SDR IPXA2676527](https://openairdocs.org/sdr/IPXA2676527), Dec 20, 2012: FIRE WARNING. FALSE ACTIVATION. CLIMBING OUT OF 17000 FT, RECEIVED A MOMENTARY EICAS MESSAGE "WHEEL WELL FIRE" ACCOMPANIED BY "WHEEL WELL FIRE" LIGHT ON PANEL. ALL OTHER INDICATIONS NORMAL. BR
- [SDR IPXA2676195](https://openairdocs.org/sdr/IPXA2676195), Nov 7, 2012: DOOR. BINDING. ENTRY DOOR LIGHT ILLUMINATED WITH DOOR CLOSED. DOOR FEELS LIKE IT IS BINDING. ADJUSTED LOWER FWD SERRATED PLATE IAW MM 52-12-00. PRESSURIZED ACFT. NO LEAKS, NO 
- [SDR IPXA1668295](https://openairdocs.org/sdr/IPXA1668295), Jul 28, 2011: CONTROLLER. FAILED. INSPECTION TYPE:ETOP, NR1 CABIN PERSSURE CONTROLLER STICKS IN VERIFY MODE CAUSING NR1 MOTOR TO FIGHT NR 2 MOTOR DURING TEST. R & R NR1 CABIN PRESSURE CONTROLLER

## 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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