# N351UP: 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: 37874
- Year built: 2012
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: April 19, 2012
- Certificate issued: May 4, 2012
- Expires: May 31, 2028
- Mode S code: A3EA54
- 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=351UP
- Page: https://openairdocs.org/aircraft/N351UP

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 N351UP.

## FAA accident and incident reports

None matched to N351UP.

## Service difficulty reports (44)

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 IPXA2026101806238](https://openairdocs.org/sdr/IPXA2026101806238), Oct 18, 2026: SKIN. PUNCTURED. DURING WALKAROUND, FOUND A PUNCTURE AT SLAT NR 10 (WS 624). SLAT CRACKED AT SEVERAL SPOTS, NUMEROUS RIVETS SHEARED. R/R SLAT #10 (STATION 624) IAW MM 27-81-02-0
- [SDR IPXA2026033018198](https://openairdocs.org/sdr/IPXA2026033018198), Mar 28, 2026: COUNTERBALANCE. OUT OF ADJUST. FORWARD ENTRY DOOR IS HEAVIER AND HARDER TO OPEN THAN OTHER FORWARD ENTRY DOORS. ADJUSTED THE COUNTERBALANCE IAW AMM 52-12-16.
- [SDR IPXA2026032379778](https://openairdocs.org/sdr/IPXA2026032379778), Mar 20, 2026: DOOR. BINDING. FORWARD ENTRY DOOR IS VERY HEAVY TO LIFT. PERFORMED COUNTERBALANCE SYSTEM TEST PER AMM 52-12-16-735 , LUBED DOOR TRACKS , OPS CHECK GOOD.
- [SDR IPXA2026030774969](https://openairdocs.org/sdr/IPXA2026030774969), Mar 2, 2026: FLOOR PANEL. CRACKED. AFT CARGO FLOOR PANEL CRACK AT STA 1327 BL 0. INSTALL NEW PANEL I.A.W SRM 51-40-02-0G REV.94.
- [SDR IPXA2026030561754](https://openairdocs.org/sdr/IPXA2026030561754), Mar 1, 2026: FORMER. CRACKED. NOSE FORMER, LT WING L/E OTBD DOOR LINK INNER FORMER OF THE CRACK AT OSS 499. REMOVED DAMAGED FORMER IAW SRM 51-40-02-0G, REV 94. INSTALLED NEW FORMER IAW SRM 5
- [SDR IPXA2026030561788](https://openairdocs.org/sdr/IPXA2026030561788), Mar 1, 2026: FORMER. CRACKED. LEFT WING L/E ATTACH INTERNAL FORMER CRACKED AT OSS 441, NR 5 SLAT. REMOVED DAMAGE FORMER IAW SRM 51-40-02-0G, REV 94. INSTALLED NEW FORMER IAW SRM 51-40-02-0G 
- [SDR IPXA2026030462840](https://openairdocs.org/sdr/IPXA2026030462840), Mar 1, 2026: SUPPORT BRACKET. CRACKED. CRACKED BRACKET, LT WING L/E COMPARTMENT TORQUE TUBE SUPPORT BRACKET. INSTALLED NEW BRCKET I.A.W SRM 51-40-02-0G REV. 94 AND BOEING DWG NO. 114T1240 SH. 6 REV. 
- [SDR IPXA2026030462846](https://openairdocs.org/sdr/IPXA2026030462846), Mar 1, 2026: SUPPORT BRACKET. CRACKED. CRACKED SUPPORT, RT WING L/E NR.7 SLAT PNL NO. 611KB TORQUE TUBE SUPPORT. INSTALLED NEW BRCKET I.A.W SRM 51-40-02-0G REV. 94 AND BOEING DWG NO. 114T1240 SH. 6 R
- [SDR IPXA2026030647430](https://openairdocs.org/sdr/IPXA2026030647430), Feb 28, 2026: SEAL. BROKEN. BROKEN - SPRING SEAL, PNL NO. 446CR (REPLACE) 1.REMOVED DAMAGE SEAL STRIP I.A.W SRM 51-40-02-0G REV.94. INSTALL NEW SEAL STRIP I.A.W SRM 51-40-02-0G REV.94 AND 
- [SDR IPXA2026030650740](https://openairdocs.org/sdr/IPXA2026030650740), Feb 28, 2026: FORMER. CRACKED. CRACKED FORMER, RT WING L/E NO.8 SLAT INBD AUXILIARY TRACK OSS 441 (REPLACE) 1. REMOVED DAMAGE FORMER I.A.W SRM 51-40-02-0G REV. 94. INSTALLED NEW FORMER I.A.W 
- [SDR IPXA2026030347899](https://openairdocs.org/sdr/IPXA2026030347899), Feb 28, 2026: BRACKET. CHAFED. CHAFING - BRACKET, NR 1 ENG LT THRUST REVERSER FWD LWR CLOSURE DOOR T/E AREA. INSTALLED NEW BRACKET I.A.W SRM 51-40-02-0G REV. 94 AND ST ENGINEERING IPC 78-32-2
- [SDR IPXA2026030634122](https://openairdocs.org/sdr/IPXA2026030634122), Feb 27, 2026: DOOR. CHAFED. CHAFING DOOR, NO.1 ENG R/H T/R BLOWOUT DOOR FWD SIDE (REPLACE) REMOVED DAMAGE BLOWOUT DOOR I.A.W SRM 51-40-02-0G REV.94. INSTALL NEW BLOWOUT DOOR I.A.W SRM 51-4
- [SDR IPXA2026030633793](https://openairdocs.org/sdr/IPXA2026030633793), Feb 27, 2026: SEAL. BROKEN. BROKEN SPRING SEAL, PNL NO.446CL (REPLACE). REMOVED DAMAGE SEAL I.A.W SRM 51-40-02-0G REV.94 INSTALL NEW SEAL I.A.W SRM 51-40-02-0G REV 94 AND BOEING DWG NO:311
- [SDR IPXA2026030629248](https://openairdocs.org/sdr/IPXA2026030629248), Feb 27, 2026: BULKHEAD. CRACKED. CRACK-BULKHEAD, NO.2 ENG L/H T/R FWD TORQUE BOX UPPER SIDE SUPPORT. IAW AMM 70-50-00-912-001-H00 REV.147 INSTALLED THE TUBES AND CONNECTOR. I.A.W. AMM 78-31-00-
- [SDR IPXA2026030633729](https://openairdocs.org/sdr/IPXA2026030633729), Feb 27, 2026: BRACKET. WORN. WORN-BRACKET, NO.2 PYLON AFT FAIRING DOOR HOLD OPEN ROD FWD SUPPORT BRACKET WORN (REPLACE) 1. REMOVED DAMAGE BRACKET I.A.W SRM 51-40-02-0G REV. 94. 2. INSTALLED
- [SDR IPXA2026030328705](https://openairdocs.org/sdr/IPXA2026030328705), Feb 27, 2026: ANGLE. CRACKED. CRACK-CLIP, NR 1 PYLON AFT FAIRING INNER AFT FRAME OUTBD SIDE SUPPORT CLIP (REPLACE) PAPER FINAL REVIEW COMPLETED
- [SDR IPXA2026030612569](https://openairdocs.org/sdr/IPXA2026030612569), Feb 26, 2026: SEAL. BROKEN. BROKEN SEAL , NO. 1 PYLON AFT FAIRING PNL 436CL SPRING SEAL AREA. REMOVED DAMAGE SEAL STRIP I.A.W SRM 51-40-02-0G REV.94 2. INSTALL NEW SEAL STRIP I.A.W SRM 51-
- [SDR IPXA2026030512672](https://openairdocs.org/sdr/IPXA2026030512672), Feb 26, 2026: ANGLE. WORN. NR 1 PYLON TORQUE BOX PANEL 436AR INNER CABLE SUPPORT AREA ANGLE. REMOVED DAMAGE ANGLE I.A.W SRM 51-40-02-0G REV. 94. 2. INSTALL NEW ANGLE I.A.W SRM 51-40-02-0G
- [SDR IPXA2024053099671](https://openairdocs.org/sdr/IPXA2024053099671), May 29, 2024: BATTERY PACK. NO TEST. AIRCRAFT EMERGENCY LIGHT FOUND TO BE INOP ON TEST. AS PER FIM 33-51 FAULT TREE 803 EMERGENCY BATTERY PACK REPLACED I.A.W AMM 33-51-07-022-001/33-51-07-422-012 R
- [SDR IPXA2024051799026](https://openairdocs.org/sdr/IPXA2024051799026), May 16, 2024: SEAL. LOOSE. ENTRY DOOR LOUD HISSING THRU 15,000€™. ENTRY DOOR LOWER SEAL FOUND TO BE LOOSE - UPON ARRIVAL.
- [SDR IPXA2024030446161](https://openairdocs.org/sdr/IPXA2024030446161), Feb 19, 2024: BUMPER. MISSING. *** SUPPLEMENTAL SDR *** FAULT - FOUND FWD ENTRY DOORWAY LINING BUMPER MISSING (REPLACE) RI.A.W AMM 52-12-02-004-001 REV.141 AND AMM 52-21-02-404-025 REV.141 IN
- [SDR IPXA2024021906161](https://openairdocs.org/sdr/IPXA2024021906161), Feb 19, 2024: BUMPER. MISSING. **SDR FILED OPEN**FAULT - FOUND FWD ENTRY DOORWAY LINING BUMPER MISSING (REPLACE) OK TO WORK
- [SDR IPXA2023082966663](https://openairdocs.org/sdr/IPXA2023082966663), Aug 29, 2023: DOOR. LEAKING. CREW ENTRY DOOR LEAKED ON CLIMBOUT AS INDICATED BY A LOUD SIGNAL. ++LEAK SEEMED TO STOP ABOVE FL 300 DOOR SEAL FOUND SLIGHTLY LOOSE AND RETURNED TO PROPER POSIT
- [SDR IPXA2022021278885](https://openairdocs.org/sdr/IPXA2022021278885), Jan 30, 2022: NONE. BROKEN. INSPECTION TYPE:C5FOUND NO.1 EMERGENCY ESCAPE DESCENT DEVICE SEAL BROKEN(S/N:8982)REPLACE NEW PARTS I.A.W 767 AMM 25-61-03-402-010 AND AMM 25-61-03-422-006 REV.
- [SDR IPXA2021101975101](https://openairdocs.org/sdr/IPXA2021101975101), Oct 18, 2021: PCA. FAULTED. ATB, NO EMERGENCY DECLARED. ACFT OOS, ON TAKE OFF A/C FLAPS 5 DEG CLINGING OUT ACFT WANTED TO ROLL RT TOOK LEFT AILERON TO GO STRAIT WENT TO LEVEL FLIGHT EXTEND
- [SDR IPXA2021071271590](https://openairdocs.org/sdr/IPXA2021071271590), Jul 12, 2021: SEAL. LEAKING. INSPECTION TYPE:NABEGAN TO HEAR LOUD HISSING SOUND FROM BOTTOM OF CABIN ENTRY DOOR WHEN CLIMBING THRU 11000, SOUND DIMINISHED AT CRUISE, CABIN PRESSURE STAYED N
- [SDR IPXA2020081108867](https://openairdocs.org/sdr/IPXA2020081108867), Aug 10, 2020: SWITCH. INOPERATIVE. EMERGENCY LIGHT SWITCH NOT SEATED PROPERLY. SECURED EMERGENCY LIGHT SWITCH. OPS CHECKED GOOD IAW MM 33-51-00-715-227.
- [SDR IPXA2020071457786](https://openairdocs.org/sdr/IPXA2020071457786), Jul 13, 2020: DOOR SEAL. NOT SEATED. INSPECTION TYPE:N/A DURING INITIAL CLIMB LOUD SEAL NOISE COMING FROM ENTRY DOOR. RE-SEATED DOOR SEAL PER AMM 52-09-01. OPS CHECK GOOD PER 05-51-24.
- [SDR IPXA2020031653153](https://openairdocs.org/sdr/IPXA2020031653153), Feb 14, 2020: FLOOR PANEL. DAMAGED. INSPECTION TYPE:N/AMCD FLOOR PANEL HAS .750" HOLE IN TOP SKIN AND CORE AT POS 14R.REPAIRED FLOOR PANEL IAW SRM 53-00-50-2R PARA 4.C.
- [SDR IPXA2019111849118](https://openairdocs.org/sdr/IPXA2019111849118), Nov 17, 2019: DOOR. LEAKING. INSPECTION TYPE:N/A*** ATB *** PRESSURIZATION LEAK FROM COCKPIT DOOR LOUD HISS UPON VISUAL INSPECTION DAY LIGHT SEAN MIDPOINT BOTTOM OF DOOR.REINSTALLED LOWER S
- [SDR IPXA2019060542813](https://openairdocs.org/sdr/IPXA2019060542813), Jun 3, 2019: SEAL. LOOSE. ON CLIMB OUT, THE DOOR SEAL NOISE AROUND THE ENTRY DOOR WAS LOUDER THAN NORMAL AND IT CONTINUED TRU OUT THE FLIGHT. PRESSURIZATION INDICATIONS WERE NORMAL AND S
- [SDR IPXA2018101034889](https://openairdocs.org/sdr/IPXA2018101034889), Oct 9, 2018: SEAL. LOOSE. EXCESSIVE AIR LEAK THRU CREW ENTRY DOOR DURING CRUISE. FOUND A LOSE SEAL AT THE LOWER 6 O`CLOCK POSITION. REINSTALLED THE SEAL ON THE TRACK AND LUBRICATED THE D
- [SDR IPXA2018090533566](https://openairdocs.org/sdr/IPXA2018090533566), Sep 4, 2018: DOOR SEAL. OUT OF POSITION. LOUD HISS COMING FROM MAIN ENTRY DOOR AT CRUISE. FOUND LWR DOOR SEAL OUT OF TRACK. SECURED DOOR SEAL MAIN ENTRY DOOR PER MM 52-09-01-424-019. OK TO CONTINUE.
- [SDR IPXA2018071831795](https://openairdocs.org/sdr/IPXA2018071831795), Jul 17, 2018: HANDLE. DEFECTIVE. ENTRY DOOR INSIDE HANDLE COVER STICKS OUT. WILL NOT REMAIN CLOSED. R&R HINGE ASSY AND DOOR HANDLE IAW AMM 52-12-02-401.
- [SDR IPXA2018070231321](https://openairdocs.org/sdr/IPXA2018070231321), Jun 30, 2018: ACCESS DOOR. DEFECTIVE. CREW ENTRY FWD SIDE DOORWAY. CLEAR SMALL ACCESS DOOR WOULD NOT CLOSE (ARMING LEVER HINGED COVER). DEFERRED PER MEL 52-11-2. R&R ENTRY DOOR ARMING COVER AND HING
- [SDR IPXA2016041202010](https://openairdocs.org/sdr/IPXA2016041202010), Apr 4, 2016: FLOOR PANEL. DAMAGED. INSPECTION TYPE: C2, DAMAGE ON M/D FLOOR PANEL 241 ZFF. FABRICATED A NEW REPLACEMENT FLOOR PANEL IAW NR B767-5320-9693-I.
- [SDR IPXA2016031100608](https://openairdocs.org/sdr/IPXA2016031100608), Mar 10, 2016: SEAL. LEAKING. CREW ENTRY DOOR SEAL LEAKS AT MID BOTTOM OF DOOR. CREW ENTRY DOOR SEAL REINSTALLED IAW AMM 52-09-01-424-019, REV 117.00. DOOR TESTED, ALL SATISFACTORY.
- [SDR IPXA2016030700417](https://openairdocs.org/sdr/IPXA2016030700417), Mar 5, 2016: SEAL. LEAKING. CREW ENTRY DOOR LEAKS AT LOWER LT CORNER LOWER MIDDLE SEAL FOUND ADRIFT, SEAL RE-SEATED INTO DOOR CARRIER AND SEAL NOW SATISFACTORY.
- [SDR IPXA2016030100176](https://openairdocs.org/sdr/IPXA2016030100176), Feb 29, 2016: SENSOR. OUT OF ADJUST. CLIMBING OUT OF 12,000 FT HAD FWD CARGO DOOR EICAS MESSAGE. FOLLOWED QRH PROCEDURE ALSO HAD CARGO DOOR OVERHEAD LIGHT. ADJUSTED LOWER FWD CARGO DOOR CLOSED SENS
- [SDR IPXA2015111595806](https://openairdocs.org/sdr/IPXA2015111595806), Nov 15, 2015: FLOOR PANEL. DAMAGED. HOLE IN FLOOR PANEL POSITION NR 2 CENTER. REPAIRED IAW SRM 53-00-50-2R.
- [SDR IPXA2015111595805](https://openairdocs.org/sdr/IPXA2015111595805), Nov 15, 2015: FLOOR PANEL. DAMAGED. 2 HOLES IN FLOOR PANEL, POSITION NR 2 CENTER. REPAIRED IAW SRM 53-00-50-2R.
- [SDR IPXA2015083092889](https://openairdocs.org/sdr/IPXA2015083092889), Aug 30, 2015: FLOOR PANEL. DAMAGED. MAIN CARGO DECK FLOOR PANEL DAMAGED 1 X 2 INCH HOLE IN UPPER SKIN. REPAIRED IAW SRM 53-00-50-2R.
- [SDR IPXA2015083092888](https://openairdocs.org/sdr/IPXA2015083092888), Aug 30, 2015: FLOOR PANEL. DAMAGED. MAIN DECK FLOOR PANEL DAMAGED ONE INCH DIA HOLE IN UPPER SKIN. REPAIRED IAW SRM 53-00-50-2R.
- [SDR IPXA2015040287647](https://openairdocs.org/sdr/IPXA2015040287647), Apr 1, 2015: SEAL. DISLODGED. MAIN DOOR SEAL "WHISTLED" OR LEAKED FROM LIFTOFF TO SHORT FINAL. FOUND CREW ENTRY DOOR SEAL OUT OF SEAL RETAINER. RE-INSTALLED SEAL IAW AMM 52-09-01-4, REV 114.

## 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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