# N327UP: 1998 Boeing 767-34AF - Status: Valid registration - Airframe: [Boeing 767-34AF](https://openairdocs.org/model/boeing-767-34af) (registry code 1385212, 190 seats) - Engine: [GE CF6-80 series](https://openairdocs.org/engine/ge-cf6-80-series) (registry code 30025) - Data sheets: [TCDS E13NE](https://openairdocs.org/tcds/E13NE) (General Electric Company GE Aerospace) (OpenAirDocs) - Serial number: 27753 - Year built: 1998 - Type: Fixed wing multi engine - Engine type: Turbo-fan - Airworthiness: Standard, transport - Airworthiness date: December 11, 1998 - Certificate issued: December 14, 1998 - Expires: February 28, 2029 - Mode S code: A38A21 - 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=327UP - Page: https://openairdocs.org/aircraft/N327UP 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. The registry lists only the engine series, so ADs for every GE CF6-80 model are included. ## ADs that may apply (OpenAirDocs): 61 in force ### Matched by airframe (Boeing 767-34AF) None in force. ### Matched by engine (GE CF6-80 series) - [AD 2024-24-03](https://openairdocs.org/ad/2024-24-03): Engine Exhaust · Boeing MD-11, MD-11F and CF6-80C2D1F. Effective Jan 13, 2025 - [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 2022-02-18](https://openairdocs.org/ad/2022-02-18): Engine Mount Section · General Electric CF6-80C2A1, CF6-80C2A2, CF6-80C2A3 and 3 more. Effective Feb 25, 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 2018-07-05](https://openairdocs.org/ad/2018-07-05): Turbine Section · General Electric CF6-80A, CF6-80A1, CF6-80A2 and 1 more. Effective May 11, 2018 - [AD 2017-11-15](https://openairdocs.org/ad/2017-11-15): Turbine/ Turboprop Engine--Turbine Section · General Electric CF6-80C2L1F. Effective Jul 13, 2017 - [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 2011-23-04](https://openairdocs.org/ad/2011-23-04): Forward engine mount assembly side links · General Electric CF6-45A, CF6-45A2, CF6-50A and 14 more. Effective Dec 12, 2011 - [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 2009-14-08](https://openairdocs.org/ad/2009-14-08): High-pressure compressor rotor (HPCR) stages 11-14 spool/ shafts · General Electric CF6-80C2B5F. Effective Aug 5, 2009 - [AD 2009-08-06](https://openairdocs.org/ad/2009-08-06): Stage 1 high-pressure turbine (HPT) rotor disks · General Electric CF6-80A, CF6-80A1, CF6-80A2 and 1 more. Effective May 18, 2009 - [AD 2009-07-10](https://openairdocs.org/ad/2009-07-10): High-pressure turbine rotor (HPTR) · General Electric CF6-80A, CF6-80A1, CF6-80A2 and 1 more. Effective May 6, 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 2008-02-17](https://openairdocs.org/ad/2008-02-17): Thrust reverser actuation systems · General Electric CF6-50A, CF6-50C, CF6-50C1 and 16 more. Effective Feb 28, 2008 - [AD 2007-24-07](https://openairdocs.org/ad/2007-24-07): Thermal spray coating on certain stage 1 fan disks · General Electric CF6-80C2B1. Effective Jan 2, 2008 - [AD 2007-22-07](https://openairdocs.org/ad/2007-22-07): Electronic control unit (ECU) · General Electric CF6-80C2D1F. Effective Nov 28, 2007 - [AD 2007-21-06](https://openairdocs.org/ad/2007-21-06): Electronic control unit (ECU) · General Electric CF6-80C2A5F. Effective Nov 15, 2007 - [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 2006-06-08](https://openairdocs.org/ad/2006-06-08): Latching system of the fan reverser · General Electric CF6-80C2D1F. Effective Apr 25, 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 2005-06-07](https://openairdocs.org/ad/2005-06-07): Directional pilot valve (DPV) assembly · General Electric CF6-80A1, CF6-80A3, CF6-80C2A1 and 5 more. Effective Apr 25, 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 2004-07-13](https://openairdocs.org/ad/2004-07-13): High pressure turbine (HPT) stage 1 disks · General Electric CF6-80C2A5F, CF6-80C2B5F, CF6-80C2B7F and 1 more. Effective May 6, 2004 - [AD 2003-12-08](https://openairdocs.org/ad/2003-12-08): Directional pilot valve · General Electric CF6-80A1, CF6-80A3, CF6-80C2A1 and 5 more. Effective Jul 23, 2003 - [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 2001-06-09](https://openairdocs.org/ad/2001-06-09): Aft Engine Mount Link Assemblies · General Electric CF6-80A3. Effective May 1, 2001 - [AD 2000-12-08](https://openairdocs.org/ad/2000-12-08): Mount Link Assemblies · General Electric CF6-80C2A1, CF6-80C2A2, CF6-80C2A3 and 4 more. Effective Aug 28, 2000 - [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 95-17-16](https://openairdocs.org/ad/95-17-16): Compressor Rear Frame · General Electric CF6-80A, CF6-80A1, CF6-80A2 and 1 more. Effective Nov 7, 1995 - [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 94-07-04](https://openairdocs.org/ad/94-07-04): High Pressure Turbine Disk · General Electric CF6-80A, CF6-80A1, CF6-80A2 and 1 more. Effective May 23, 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 ### 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 2006-12-24](https://openairdocs.org/ad/2006-12-24) (historical): Five-link forward mount assembly · General Electric CF6-45A, CF6-45A2, CF6-50A and 14 more. Effective Jul 21, 2006 - [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 2003-01-05](https://openairdocs.org/ad/2003-01-05) (historical): Dovetail slots · General Electric CF6-80A, CF6-80A1, CF6-80A2 and 1 more. Effective Jan 28, 2003 - [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 2000-08-12](https://openairdocs.org/ad/2000-08-12) (historical): Life-limited Parts · General Electric CF6-80A, CF6-80A1, CF6-80A2 and 10 more. Effective Oct 23, 2000 - [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 99-18-20](https://openairdocs.org/ad/99-18-20) (historical): Inadvertent In-flight Thrust Reverser · General Electric Aircraft Engines CF6-50 Series (all), CF6-80A1, CF6-80A3 and 6 more. Effective Nov 2, 1999 - [AD 99-18-19](https://openairdocs.org/ad/99-18-19) (historical): Inadvertent Thrust Reverser · General Electric CF6-80A, CF6-80A1, CF6-80A2 and 7 more. Effective Sep 24, 1999 - [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 98-15-17](https://openairdocs.org/ad/98-15-17) (historical): Link Assembly · General Electric CF6-80A3. Effective Aug 7, 1998 - [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 All 80: https://openairdocs.org/aircraft/N327UP/ads.md ## Information bulletins (advisory) (5 in force) - [SAIB 2023-15](https://openairdocs.org/saib/2023-15): Falsified Forms from AOG Technics. Issued Dec 19, 2023 - [SAIB NE-11-27](https://openairdocs.org/saib/NE-11-27): Fuel Injector Nozzle - CF6-80 Improperly Welded Fuel Nozzles. Issued Apr 5, 2011 - [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 N327UP. ## FAA accident and incident reports (1) From the FAA Accident/Incident Data System. Reports are matched to registry aircraft by N-number and event date, checked against the reported make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model. - [Incident 20171112021099I](https://openairdocs.org/incident/20171112021099I), Nov 12, 2017: Boeing 767-34AF (N327UP), Phoenix, AZ, Minor damage. Phoenix, AZ (phx): UPS858, B763, diverted from kabq to kphx for precautionary mechanical reasons. Declared an emergency for hydraulic failure. Requested… ## Service difficulty reports (167, newest 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 IPXA2026102276179](https://openairdocs.org/sdr/IPXA2026102276179), Oct 22, 2026: LOCK MECHANISM. FAULTED. CREW REPORTS RIGID BARRIER DOOR UNABLE TO OPEN ON PREFLIGHT. PRIMARY LATCH LOCKING MECHANISM FAULTY. PRM ISO VALVE C/B K-3 AT P-33 OPENED AND COLLARED TO SHUT O - [SDR IPXA2026093004390](https://openairdocs.org/sdr/IPXA2026093004390), Sep 30, 2026: HANDLE. BINDING. LIFE RAFT BIN HANDLE HARD TO OPEN LUBRICATED AS NEEDED. HANDLE. OPS CK OK - [SDR IPXA2026071787701](https://openairdocs.org/sdr/IPXA2026071787701), Jul 16, 2026: WARNING MESSAGE. FALSE ACTIVATION. EMERGENCY DECLARED AFTER LANDING UPON FLAP/SLAT RETRACTION RECEIVED LE SLAT DISAGREE EICAS AND LE SLAT SHUTDOWN STATUS MESSAGES FLAPS INDICATED 1. RESET MESSAGE - [SDR IPXA2025060310145](https://openairdocs.org/sdr/IPXA2025060310145), May 10, 2025: ANGLE. CRACKED. CRACK-ANGLE, AFT CARGO COMPARTMENT FORWARD WALL R/H SUPPORT BELOW FLOOR AREA, STA 1087, S-35R.REMOVED DAMAGE CLIP I.A.W SRM 51-40-02-0G REV.92.INSTALLED NEW CLI - [SDR IPXA2025051510145](https://openairdocs.org/sdr/IPXA2025051510145), May 10, 2025: ANGLE. CRACKED. CRACK-ANGLE, AFT CARGO COMPARTMENT FORWARD WALL R/H SUPPORT BELOW FLOOR AREA, STA 1087, S-35R. (REPLACE) 1. REMOVED DAMAGE CLIP I.A.W SRM 51-40-02-0G REV.92 2. - [SDR IPXA2025060345194](https://openairdocs.org/sdr/IPXA2025060345194), May 7, 2025: FLOOR PANEL. DENTED. FOUND MAIN DECK FLOOR PANEL WITH DENT DAMAGE , P/N: 143T5876-76 PANEL NO
:232AFF , STA 412~STA 530 RBL11~RBL33.I.A.W AMM 25-57-02-004-029 AND AMM 25-58-01-00 - [SDR IPXA2025060346286](https://openairdocs.org/sdr/IPXA2025060346286), May 7, 2025: FLOOR PANEL. DENTED. FOUND MAIN DECK FLOOR PANEL WITH DENT DAMAGE , P/N: 143T5876-72 PANEL NO: 232CFF , STA 412~STA 530 RBL 55~RBL77.I.A.W AMM 25-57-02-004-029 AND AMM 25-58-01-004- - [SDR IPXA2025060346534](https://openairdocs.org/sdr/IPXA2025060346534), May 7, 2025: FLOOR PANEL. DENTED. FOUND MAIN DECK FLOOR PANEL WITH DENT DAMAGE , P/N:143T5876-85 PANEL NO: 231FFF , STA 530~STA 654+22 LBL 11~ RBL 11. I.A.W AMM 25-57-02-004-029 AND AMM 25-58-01 - [SDR IPXA2025060346576](https://openairdocs.org/sdr/IPXA2025060346576), May 7, 2025: FLOOR PANEL. DENTED. FOUND MAIN DECK FLOOR PANEL WITH DENT DAMAGE , P/N:143T5876-80 PANEL NO: 232HFF , STA 530 ~ STA 654+22 RBL 55~RBL 77. I.A.W AMM 25-57-02-004-029 AND AMM 25-58-0 - [SDR IPXA2025060346582](https://openairdocs.org/sdr/IPXA2025060346582), May 7, 2025: FLOOR PANEL. DENTED. FOUND MAIN DECK FLOOR PANEL WITH DENT DAMAGE , P/N:143T5876-84 PANEL NO: 232FFF , STA 530 ~ STA 654+22 RBL 11~ RBL 33.I.A.W AMM 25-57-02-004-029 AND AMM 25-58-0 - [SDR IPXA2025060346809](https://openairdocs.org/sdr/IPXA2025060346809), May 7, 2025: FLOOR PANEL. DENTED. FOUND MAIN DECK FLOOR PANEL WITH DENT DAMAGE , P/N:143T5876-82 PANEL NO: 232GFF , STA 530 ~ STA 654+22 RBL 33~ RBL 55. I.A.W AMM 25-57-02-004-029 AND AMM 25-58- - [SDR IPXA2025060346838](https://openairdocs.org/sdr/IPXA2025060346838), May 7, 2025: FLOOR PANEL. DENTED. FOUND MAIN DECK FLOOR PANEL WITH DENT DAMAGE , P/N:143T5876-79 PANEL NO: 231JFF , STA 530 ~ STA 645+22 LBL 55~ LBL 77.I.A.W AMM 25-57-02-004-029 AND AMM 25-58-0 - [SDR IPXA2025050746534](https://openairdocs.org/sdr/IPXA2025050746534), May 7, 2025: FLOOR PANEL. DAMAGED. MAJOR REPAIR, FOUDN MAIN DECK FLOOR PANEL WITH DENT DAMAGE , P/N:143T5876-85 PANEL NO: 231FFF , STA 530~STA 654+22 LBL 11~ RBL 11. (REPAIR) I.A.W AMM 25-57-02-0 - [SDR IPXA2025050746809](https://openairdocs.org/sdr/IPXA2025050746809), May 7, 2025: FLOOR PANEL. DAMAGED. MAJOR REPAIR, FOUND MAIN DECK FLOOR PANEL WITH DENT DAMAGE , P/N:143T5876-82 PANEL NO: 232GFF , STA 530 ~ STA 654+22 RBL 33~ RBL 55.(REPAIR) I.A.W AMM 25-57-02- - [SDR IPXA2025050746576](https://openairdocs.org/sdr/IPXA2025050746576), May 7, 2025: FLOOR PANEL. DAMAGED. *** SDR FILED OPEN *** MAJOR REPAIR *** FAULT - FOUND MAIN DECK FLOOR PANEL WITH DENT DAMAGE , P/N:143T5876-80 PANEL NO: 232HFF , STA 530 ~ STA 654+22 RBL 55~RB - [SDR IPXA2025050746582](https://openairdocs.org/sdr/IPXA2025050746582), May 7, 2025: FLOOR PANEL. DAMAGED. *** SDR FILED OPEN *** MAJOR REPAIR *** FAULT - FOUND MAIN DECK FLOOR PANEL WITH DENT DAMAGE , P/N:143T5876-84 PANEL NO: 232FFF , STA 530 ~ STA 654+22 RBL 11~ R - [SDR IPXA2025050745194](https://openairdocs.org/sdr/IPXA2025050745194), May 7, 2025: FLOOR PANEL. DAMAGED. *** SDR FILED OPEN *** MAJOR REPAIR *** FAULT - FOUND MAIN DECK FLOOR PANEL WITH DENT DAMAGE , P/N: 143T5876-76 PANEL NO
:232AFF , STA 412~STA 530 RBL11~RBL3 - [SDR IPXA2025050746286](https://openairdocs.org/sdr/IPXA2025050746286), May 7, 2025: FLOOR PANEL. DAMAGED. *** SDR FILED OPEN *** MAJOR REPAIR *** FAULT - FOUND MAIN DECK FLOOR PANEL WITH DENT DAMAGE , P/N: 143T5876-72 PANEL NO: 232CFF , STA 412~STA 530 RBL 55~RBL77. - [SDR IPXA2025050746838](https://openairdocs.org/sdr/IPXA2025050746838), May 7, 2025: FLOOR PANEL. DAMAGED. *** SDR FILED OPEN *** MAJOR REPAIR *** FAULT - FOUND MAIN DECK FLOOR PANEL WITH DENT DAMAGE , P/N:143T5876-79 PANEL NO: 231JFF , STA 530 ~ STA 22 LBL 55~ LBL 7 - [SDR IPXA2025062628664](https://openairdocs.org/sdr/IPXA2025062628664), May 6, 2025: FLOOR PANEL. DAMAGED. FOUND MAIN DECK FLOOR PANEL WITH DENT DAMAGE, P/N:143T5876-73 PANEL NO.231DFF, STA 412~STA 530 LBL 55~ LBL 77 (REPAIR) I.A.W AMM 25-57-05-404-006, AMM 25-57-02- - [SDR IPXA2025062627837](https://openairdocs.org/sdr/IPXA2025062627837), May 6, 2025: FLOOR PANEL. DAMAGED. FOUND MAIN DECK FLOOR PANEL WITH DENT DAMAGE, P/N: 143T5876-66 PANEL NO.232DFF, STA 412~STA 530 RBL 77 ~ LBL 88 (REPAIR) I.A.W AMM 25-57-05-404-006, AMM 25-57-0 - [SDR IPXA2025060529484](https://openairdocs.org/sdr/IPXA2025060529484), May 6, 2025: FLOOR PANEL. DENTED. FOUND MAIN DECK FLOOR PANEL WITH DENT DAMAGE, P/N:146T5869-28 PANEL NO:252SFF STA 1373~STA1480 RBL77~R BL88.I.A.W AMM 25-57-05-004-001, AMM 25-57-02-004-029 AND - [SDR IPXA2025060529457](https://openairdocs.org/sdr/IPXA2025060529457), May 6, 2025: FLOOR PANEL. DENTED. FOUND MAIN DECK FLOOR PANEL WITH DENT DAMAGE, FLOOR PANEL NR 252YFF. BS 1510 - 1560, RBL 55 - 88 IAW AMM 25-57-05-004-001, AMM 25-57-02-004-029, AND AMM 25-58-0 - [SDR IPXA2025060529501](https://openairdocs.org/sdr/IPXA2025060529501), May 6, 2025: FLOOR PANEL. DENTED. FOUND MAIN DECK FLOOR PANEL WITH DENT DAMAGE, FLOOR PANEL NR 232LFF, BS 654+22 - 680, RBL 33 - 55 IAW AMM 25-57-05-004-001, AMM 25-57-02-004-029 & AMM 25-58-01- - [SDR IPXA2025060529512](https://openairdocs.org/sdr/IPXA2025060529512), May 6, 2025: FLOOR PANEL. DENTED. FOUND MAIN DECK FLOOR PANEL WITH DENT DAMAGE, FLOOR PANEL NR 232KFF, BS 654+22 - 680, RBL 11 - 33 IAW AMM 25-57-05-004-001, AMM 25-57-02-004-029 AND AMM 25-58-0 - [SDR IPXA2025060529518](https://openairdocs.org/sdr/IPXA2025060529518), May 6, 2025: FLOOR PANEL. DENTED. FOUND MAIN DECK FLOOR PANEL WITH DENT DAMAGE, FLOOR PANEL NR 231MFF, BS 654+22 - 680, LBL 11- 33 IAW AMM 25-57-05-004-001, AMM 25-57-02-004-029 AND AMM 25-58-01 - [SDR IPXA2025060529542](https://openairdocs.org/sdr/IPXA2025060529542), May 6, 2025: FLOOR PANEL. DENTED. FOUND MAIN DECK FLOOR PANEL WITH DENT DAMAGE, FLOOR PANEL NR 252WFF, BS 1480 - 1569, RBL 33 - 55 IAW AMM 25-57-05-004-001, AMM 25-57-02-004-029 AND AMM 25-58-01 - [SDR IPXA2025060529548](https://openairdocs.org/sdr/IPXA2025060529548), May 6, 2025: FLOOR PANEL. DENTED. FOUND MAIN DECK FLOOR PANEL WITH DENT DAMAGE, FLOOR PANEL NR 252UFF, BS 1440 - 1500 RBL 55 - 77.IAW AMM 25-57-05-004-001, AMM 25-57-02-004-029 AND AMM 25-58-01- - [SDR IPXA2025060529526](https://openairdocs.org/sdr/IPXA2025060529526), May 6, 2025: FLOOR PANEL. DENTED. FOUND MAIN DECK FLOOR PANEL WITH DENT DAMAGE, P/N:146T5869-89 PANEL NO:251XFF, STA 1440~STA 1500 LBL55~LBL77.I.A.W AMM 25-57-05-004-001, AMM 25-57-02-004-029 AN - [SDR IPXA2025060529579](https://openairdocs.org/sdr/IPXA2025060529579), May 6, 2025: FLOOR PANEL. DENTED. FOUND MAIN DECK FLOOR PANEL WITH DENT DAMAGE, P/N:143T5876-63 PANEL NO:231EFF, STA 412~STA 530 LBL77~LBL88.I.A.W AMM 25-57-05-004-001, AMM 25-57-02-004-029 AND - [SDR IPXA2025060529565](https://openairdocs.org/sdr/IPXA2025060529565), May 6, 2025: FLOOR PANEL. DENTED. FOUND MAIN DECK FLOOR PANEL WITH DENT DAMAGE, P/N:143T5876-19 PANEL NO:231QFF, STA 654+22~STA 680 LBL77~LBL88.I.A.W AMM 25-57-05-004-001, AMM 25-57-02-004-029 A - [SDR IPXA2025060529602](https://openairdocs.org/sdr/IPXA2025060529602), May 6, 2025: FLOOR PANEL. DENTED. FOUND MAIN DECK FLOOR PANEL WITH DENT DAMAGE, P/N:143T5876-89 PANEL NO:231KFF, STA 544~STA 654+22 LBL77~LBL88.I.A.W AMM 25-57-05-004-001, AMM 25-57-02-004-029 A - [SDR IPXA2025060529614](https://openairdocs.org/sdr/IPXA2025060529614), May 6, 2025: FLOOR PANEL. DENTED. FOUND MAIN DECK FLOOR PANEL WITH DENT DAMAGE, P/N:141T5856-50 PANEL NO:222CFF, STA 287~STA 412 RBL54.75~RBL77.5.I.A.W AMM 25-57-05-004-001, AMM 25-57-02-004-029 - [SDR IPXA2025060529627](https://openairdocs.org/sdr/IPXA2025060529627), May 6, 2025: FLOOR PANEL. DENTED. FOUND MAIN DECK FLOOR PANEL WITH DENT DAMAGE, P/N:141T5856-47 PANEL NO:221CFF, STA 287~STA 412 RBL11~LBL11.I.A.W AMM 25-57-05-004-001, AMM 25-57-02-004-029 AND - [SDR IPXA2025060529638](https://openairdocs.org/sdr/IPXA2025060529638), May 6, 2025: FLOOR PANEL. DENTED. FOUND MAIN DECK FLOOR PANEL WITH DENT DAMAGE, P/N:143T5876-78 PANEL NO:231AFF, STA 412~STA 530 RBL11~LBL11.I.A.W AMM 25-57-05-004-001, AMM 25-57-02-004-029 AND - [SDR IPXA2025060529640](https://openairdocs.org/sdr/IPXA2025060529640), May 6, 2025: FLOOR PANEL. DENTED. FOUND MAIN DECK FLOOR PANEL WITH DENT DAMAGE, P/N:143T5876-38 PANEL NO:232BFF, STA 412~STA 530 RBL33~RBL55.I.A.W AMM 25-57-05-004-001, AMM 25-57-02-004-029 AND - [SDR IPXA2025060529719](https://openairdocs.org/sdr/IPXA2025060529719), May 6, 2025: FLOOR PANEL. DENTED. FOUND MAIN DECK FLOOR PANEL WITH DENT DAMAGE, P/N:143T5876-20 PANEL NO:232NFF, STA 654+22~STA 680 RBL77~RBL88.I.A.W AMM 25-57-05-004-001, AMM 25-57-02-004-029 A - [SDR IPXA2025060529729](https://openairdocs.org/sdr/IPXA2025060529729), May 6, 2025: FLOOR PANEL. DENTED. FOUND MAIN DECK FLOOR PANEL WITH DENT DAMAGE, P/N:143T5876-75 PANEL NO:231CFF, STA 412~STA 530 LBL33 ~LBL55.I.A.W AMM 25-57-05-004-001, AMM 25-57-02-004-029 AND - [SDR IPXA2025060529745](https://openairdocs.org/sdr/IPXA2025060529745), May 6, 2025: FLOOR PANEL. DENTED. FOUND MAIN DECK FLOOR PANEL WITH DENT DAMAGE, P/N: 143T5876-77 PANEL NO.231BFF, STA 412~STA530 LBL11~LBL33.I.A.W AMM 25-57-05-004-001, AMM 25-57-02-004-029 AND - [SDR IPXA2025050628664](https://openairdocs.org/sdr/IPXA2025050628664), May 6, 2025: FLOOR PANEL. DAMAGED. *** SDR FILED OPEN *** MAJOR REPAIR *** FAULT - FOUND MAIN DECK FLOOR PANEL WITH DENT DAMAGE, P/N:143T5876-73 PANEL NO.231DFF, STA 412~STA 530 LBL 55~ LBL 77 (R - [SDR IPXA2025050729745](https://openairdocs.org/sdr/IPXA2025050729745), May 6, 2025: FLOOR PANEL. DAMAGED. *** SDR FILED OPEN *** MAJOR REPAIR *** FAULT - FOUND MAIN DECK FLOOR PANEL WITH DENT DAMAGE, P/N: 143T5876-77 PANEL NO.231BFF, STA 412~STA530 LBL11~LBL33 (REPA - [SDR IPXA2025050729602](https://openairdocs.org/sdr/IPXA2025050729602), May 6, 2025: FLOOR PANEL. DAMAGED. *** SDR FILED OPEN *** MAJOR REPAIR *** FAULT-FOUND MAIN DECK FLOOR PANEL WITH DENT DAMAGE, P/N:143T5876-113 PANEL NO:231KFF, STA 544~STA 654+22 LBL77~LBL88 (RE - [SDR IPXA2025050729638](https://openairdocs.org/sdr/IPXA2025050729638), May 6, 2025: FLOOR PANEL. DAMAGED. FOUND MAIN DECK FLOOR PANEL WITH DENT DAMAGE, P/N:143T5876-78 PANEL NO:231AFF, STA 412~STA 530 RBL11~LBL11(REPAIR) STEP 5. REMOVE MAIN DECK CARGO FLOOR PANEL SE - [SDR IPXA2025050629512](https://openairdocs.org/sdr/IPXA2025050629512), May 6, 2025: FLOOR PANEL. DAMAGED. FOUND MAIN DECK FLOOR PANEL WITH DENT DAMAGE, P/N:143T5876-88 PANEL NO:232KFF, STA 654+22~STA 680 RBL11~RBL33. (REPAIR) STEP 5. REMOVE MAIN DECK CARGO FLOOR PAN - [SDR IPXA2025050729579](https://openairdocs.org/sdr/IPXA2025050729579), May 6, 2025: FLOOR PANEL. DAMAGED. FOUND MAIN DECK FLOOR PANEL WITH DENT DAMAGE, P/N:143T5876-63 PANEL NO:231EFF, STA 412~STA 530 LBL77~LBL88 (REPAIR) STEP 5. REMOVE MAIN DECK CARGO FLOOR PANEL S - [SDR IPXA2025050729729](https://openairdocs.org/sdr/IPXA2025050729729), May 6, 2025: FLOOR PANEL. DAMAGED. FOUND MAIN DECK FLOOR PANEL WITH DENT DAMAGE, P/N:143T5876-75 PANEL NO:231CFF, STA 412~STA 530 LBL33 ~LBL55 (REPAIR) STEP 5. REMOVE MAIN DECK CARGO FLOOR PANEL - [SDR IPXA2025050729614](https://openairdocs.org/sdr/IPXA2025050729614), May 6, 2025: FLOOR PANEL. DAMAGED. FOUND MAIN DECK FLOOR PANEL WITH DENT DAMAGE, P/N:141T5856-50 PANEL NO:222CFF, STA 287~STA 412 RBL54.75~RBL77.5 (REPAIR) STEP 5. REMOVE MAIN DECK CARGO FLOOR PA - [SDR IPXA2025050629457](https://openairdocs.org/sdr/IPXA2025050629457), May 6, 2025: FLOOR PANEL. DAMAGED. FOUND MAIN DECK FLOOR PANEL WITH DENT DAMAGE, P/N:146T5869-42PANEL NO:252YFF STA 1510~STA1560 RBL55~RBL88 (REPAIR) STEP 5. REMOVE MAIN DECK CARGO FLOOR PANEL SE - [SDR IPXA2025050629501](https://openairdocs.org/sdr/IPXA2025050629501), May 6, 2025: FLOOR PANEL. DAMAGED. FAULT-FOUND MAIN DECK FLOOR PANEL WITH DENT DAMAGE, P/N:143T5876-86 PANEL NO:232LFF, STA 654+22~STA 680 RBL33~RBL 55. (REPAIR) STEP 5. REMOVE MAIN DECK CARGO FL - [SDR IPXA2025050629526](https://openairdocs.org/sdr/IPXA2025050629526), May 6, 2025: FLOOR PANEL. DAMAGED. OUND MAIN DECK FLOOR PANEL WITH DENT DAMAGE, P/N:146T5869-135 PANEL NO:251XFF, STA 1440~STA 1500 LBL55~LBL77 (REPAIR) STEP 5. REMOVE MAIN DECK CARGO FLOOR PANEL All 167: https://openairdocs.org/aircraft/N327UP/reports.md ## STCs that may be installed (OpenAirDocs) (6) 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 CF6-80 series) - [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. Lists CF6-80A - [STC SE01478CH](https://openairdocs.org/stc/SE01478CH): Installation of Cook Airtomic alignment joint p/n AIR 22912. Cook Airtomic. Lists CF6-80C2 Series - [STC SE00969CH](https://openairdocs.org/stc/SE00969CH): Install AeroControlex P/N 2605290-001 variable stator feedback control cable. AeroControlex Group TransDigm Inc. Lists CF6-80A - [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. Lists CF6-80C2A1 - [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 ## Related - Other Boeing 767-34AF aircraft: https://openairdocs.org/model/boeing-767-34af/aircraft.md - The GE CF6-80 series engine: https://openairdocs.org/engine/ge-cf6-80-series.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.