# N330UP: 1999 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: 27756
- Year built: 1999
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: August 9, 1999
- Certificate issued: October 5, 1999
- Expires: August 31, 2028
- Mode S code: A3979F
- 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=330UP
- Page: https://openairdocs.org/aircraft/N330UP

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/N330UP/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 N330UP.

## FAA accident and incident reports

None matched to N330UP.

## Service difficulty reports (131, 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 IPXA2026080344837](https://openairdocs.org/sdr/IPXA2026080344837), Jul 31, 2026: LENS. BROKEN. EXIT SIGN AT CREW ENTRY DOOR BROKEN/DETACHED. RESECURED EXIT SIGN COVER ON CREW ENTRY DOOR IAW AMM 20-00-00 STANDARD MAINTENANCE PRACTICES.
- [SDR IPXA2026062998437](https://openairdocs.org/sdr/IPXA2026062998437), Jun 28, 2026: FLOOR PANEL. DAMAGED. MAJOR REPAIR, FOUND MAIN DECK FLOOR PANEL DAMAGE , P/N : 145T5876-81 PANEL NO : 241MFF. FABRICATE A NEW FLOOR PNL IAW SREO-9693-REQ001 REV.4.
- [SDR IPXA2026070783417](https://openairdocs.org/sdr/IPXA2026070783417), Jun 27, 2026: STRAP. CORRODED. MAJOR REPAIR, FORWARD CARGO COMPARTMENT L/H CEILING STRAP CORROSION BETWEEN BS 654+22 AND BS 676, LBL 67.5". ACCOMPLISH THE REPAIR IAW EO-97934-REQ1, REV1 AND E
- [SDR IPXA2026070784329](https://openairdocs.org/sdr/IPXA2026070784329), Jun 27, 2026: SEAL. BROKEN. AERODYNAMIC SEAL BROKEN, FWD LT ENTRY DOOR. REMOVED DAMAGE SILICONE RUBBER I.A.W SRM 51-40-02-0G REV.95. INSTALLED NEW SILICONE RUBBER I.A.W SRM 51-40-02-0G REV
- [SDR IPXA2026070384110](https://openairdocs.org/sdr/IPXA2026070384110), Jun 27, 2026: SEAT TRACK. WORN. FOUND CAPTAIN`S SEAT TRACK ASSY WORN AT INBD FWD, OTBD AFT TOTAL: 2EA. IAW AMM 25-11-01-822-095-001, REV 148. REPLACED THE SEAT TRACK ASSY.
- [SDR IPXA2026070286250](https://openairdocs.org/sdr/IPXA2026070286250), Jun 27, 2026: ANGLE. CRACKED. FOUND CRACKED ANGLE, BULK CARGO COMPT CEILING AREA, STA 1577 LBL 74 INBD SIDE. MAIN DECK CARGO FLOOR PANEL AND DADO PANEL OK TO INSTALL CHECK OK. INSTALLED NEW 
- [SDR IPXA2026070286244](https://openairdocs.org/sdr/IPXA2026070286244), Jun 27, 2026: ANGLE. CRACKED. FOUND CRACKED ANGLE, BULK CGO COMPT CEILING AREA, BS 1577 LBL 74 OUTBD SIDE. REMOVED DAMAGE ANGLE I.A.W SRM 51-40-02-0G REV. 95. INSTALLED NEW ANGLE I.A.W SRM 5
- [SDR IPXA2026062984329](https://openairdocs.org/sdr/IPXA2026062984329), Jun 27, 2026: SEAL. BROKEN. AERODYNAMIC SEAL BROKEN, FWD LH ENTRY DOOR (REPLACE) 1. I.A.W AMM 52-12-01-004-001 REV. 148 REMOVE CREW ENTRY DOOR.
- [SDR IPXA2026070870975](https://openairdocs.org/sdr/IPXA2026070870975), Jun 26, 2026: LINER. BROKEN. FOUND MAIN DECK DOORWAY LINING BROKEN TTL:1AREA. REMOVE THE BROKEN MATERIALS AND CLEAN. BOND THE REPAIR PLIES WITH RESIN IAW CMM 25-00-66, REPAIR 1-1, REV. 148.
- [SDR IPXA2026070371137](https://openairdocs.org/sdr/IPXA2026070371137), Jun 26, 2026: CLOSEOUT PANEL. CRACKED. CRACKED PANEL, LT WING L/E NR 1 SLAT LOWER SURFACE INBD CLOSURE PANEL. REMOVED THE CRACK MATERIALS AND CLEAN. BOND THE REPAIR PLIES WITH FILM ADHESIVE IAW SRM 5
- [SDR IPXA2026070371125](https://openairdocs.org/sdr/IPXA2026070371125), Jun 26, 2026: CLOSEOUT PANEL. CRACKED. CRACKED PANEL, LT WING L/E NR 1 SLAT OTBD CLOSURE PANEL. REMOVED THE CRACK MATERIALS AND CLEAN. BOND THE REPAIR PLIES WITH FILM ADHESIVE CURED AT 260°F FOR 130
- [SDR IPXA2026070271137](https://openairdocs.org/sdr/IPXA2026070271137), Jun 26, 2026: PANEL. CRACKED. CRACKED PANEL, LT WING L/E NO.1 SLAT LOWER SURFACE INBD CLOSURE PNL. IAW NDT MANUAL PART 1, 51-01-01 & PART 4, 51-00-03, REV.144 TO PERFORM NDT/UT FOR THE POST 
- [SDR IPXA2026062670975](https://openairdocs.org/sdr/IPXA2026062670975), Jun 26, 2026: LINER. BROKEN. FOUND MAIN DECK DOORWAY LINING BROKEN TTL:1AREA.
- [SDR IPXA2026072943442](https://openairdocs.org/sdr/IPXA2026072943442), Jun 25, 2026: SHAFT. WORN. FOUND LH WING NO.4 FLAP TRACK JOINT 6 OUTER SHAFT INNER GEAR WORN OUT. I.A.W AMM 27-51-04-402-135 REV.148 INSTALLED LH WING NO.4 FLAP TRACK SERVICEABLE OUTER SH
- [SDR IPXA2026072945065](https://openairdocs.org/sdr/IPXA2026072945065), Jun 25, 2026: ARM. WORN. FOUND RH WING INBOARD FLAP TRACK JOINT 6, OUTER SHAFT INNER GEAR WORN OUT AND FOUND 6-9 DRIVE ARM FIXED GEAR WORN OUT. I.A.W AMM 27-51-04-402-135 REV.148 INSTAL
- [SDR IPXA2026070343513](https://openairdocs.org/sdr/IPXA2026070343513), Jun 25, 2026: FAN COWL. CRACKED. CRACKED SKIN, NR 1 ENG RT FAN COWL INNER FWD LWR CORNER AREA. IAW AMM 71-11-02-024-001-H00 REV.148 AND AMM 71-11-02-424-005-H00, REV 148 TRANSFERRED THE CHINE T
- [SDR IPXA2026070743710](https://openairdocs.org/sdr/IPXA2026070743710), Jun 25, 2026: SEAL. BROKEN. FOUND THE CREW ENTRY DOOR AFT DOORWAY LINING SEAL BROKEN. I.A.W AMM 52-12-02-404-025 REV.148 AND AMM 52-12-02-004-001 REV.148 REPLACE CREW ENTRY DOOR AFT DOORWA
- [SDR IPXA2026062643710](https://openairdocs.org/sdr/IPXA2026062643710), Jun 25, 2026: SEAL. BROKEN. FOUND THE CREW ENTRY DOOR AFT DOORWAY LINING SEAL BROKEN.
- [SDR IPXA2026070725484](https://openairdocs.org/sdr/IPXA2026070725484), Jun 24, 2026: SEAL. MISSING. FOUND THE CREW ENTRY DOOR FORWARD DOORWAY SEAL MISSING. I.A.W AMM 52-12-02-404-025 REV.148 INSTALL DOORWAY SEAL.
- [SDR IPXA2026062926186](https://openairdocs.org/sdr/IPXA2026062926186), Jun 24, 2026: ANTENNA. ERODED. VST HF ANTENNA (321E) ERODED. PANEL 321E, OK TO INSTALL CHKD OK.
- [SDR IPXA2026070326099](https://openairdocs.org/sdr/IPXA2026070326099), Jun 24, 2026: SEAT TRACK. CRACKED. FOUND FIRST OFFICER SEAT TRACK ASSY CRACK AT OTBD FWD. IAW AMM 25-11-01-822-095-001, REV 148 REPLACED TRACK ASSY.
- [SDR IPXA2026070326105](https://openairdocs.org/sdr/IPXA2026070326105), Jun 24, 2026: SEAT TRACK. WORN. FOUND CAPTAIN SEAT TRACK ASSY WORN AT OTBD FWD. IAW AMM 25-11-01-822-095-001, REV 148. REPLACED THE SEAT TRACK ASSY.
- [SDR IPXA2026062425484](https://openairdocs.org/sdr/IPXA2026062425484), Jun 24, 2026: SEAL. MISSING. FOUND THE CREW ENTRY DOOR FORWARD DOORWAY SEAL MISSING.
- [SDR IPXA2026031707927](https://openairdocs.org/sdr/IPXA2026031707927), Mar 17, 2026: PAWL. INOPERATIVE. ENTRY DOOR WILL NOT CLOSE UNLESS SECURE LEVER IS ALREADY IN SECURE POSITION. REMOVED AND REPLACED PAWL IAW AMM 52-11-26 OPS CHECKED GOOD.
- [SDR IPXA2024080494365](https://openairdocs.org/sdr/IPXA2024080494365), Aug 4, 2024: SIGN. BROKEN. EMERGENCY/EXIT LIGHT FORWARD OF L1 DOOR HAS DAMAGED BASE. R&R EMERGENCY LIGHT ASSY @ L1 DOOR IAW AMM 33-51-16 OPS CKS NORMAL
- [SDR IPXA2024062032724](https://openairdocs.org/sdr/IPXA2024062032724), Jun 13, 2024: SLAT TRACK. CRACKED. FAULT - FOUND NO.8 SLAT INBD MAIN TRACK DRAIN HOUSING TUBE PORT FUEL SEEPING.I.A.W. AMM 28-11-01-004-013 REV.142 REMOVED THE FUEL PANEL NO 632FB.I.A.W. AMM 28-1
- [SDR IPXA2024061279368](https://openairdocs.org/sdr/IPXA2024061279368), Jun 4, 2024: FLOOR PANEL. CRACKED. FOUND MAIN DECK CARGO FLOOR PANEL CRACK AT STA 1432~1520, LBL 55~LBL 77.5, P/N: 146T5869-89. (REPAIR) FABRICATE A NEW FLOOR PANEL I.A.W. SREO-9693-REQ001 REV.2.
- [SDR IPXA2024061161894](https://openairdocs.org/sdr/IPXA2024061161894), Jun 2, 2024: DRAIN. NONE. **SUPPLEMENTAL SDR** ADD SDR FOR EO-82173-JIC001 (FUSELAGE DRAIN HOLES INSPECTION AND INSTALLATION AFT OF BS 1725.5 BETWEEN S-36L AND S-36R) ACCOMPLISHED SDR. P
- [SDR IPXA2024061061446](https://openairdocs.org/sdr/IPXA2024061061446), Jun 2, 2024: ANGLE. CRACKED. CRACK -ANGLE BULK CARGO COMPARTMENT LEFT AREA STA 1578 LBL60 OUTBOARD.I.A.W AMM 53-01-06-400-801 REV.142 INSTALL MAIN DECK CARGO FLOOR PANEL AND CONDITION CHECK
- [SDR IPXA2024061060582](https://openairdocs.org/sdr/IPXA2024061060582), Jun 2, 2024: ANGLE. CRACKED. CRACK - ANGLE BULK CARGO COMPARTMENT RIGHT AREA STA 1578 RBL 60 OUTBOARD I.A.W AMM 53-01-06-400-801 REV.142 INSTALL MAIN DECK CARGO FLOOR PANEL AND CONDITION CH
- [SDR IPXA2024060361894](https://openairdocs.org/sdr/IPXA2024060361894), Jun 2, 2024: NONE. NONE. **SDR FILED OPEN** ADD SDR FOR EO-82173-JIC001 (FUSELAGE DRAIN HOLES INSPECTION AND INSTALLATION AFT OF BS 1725.5 BETWEEN S-36L AND S-36R) OKAY TO WORK
- [SDR IPXA2024042970045](https://openairdocs.org/sdr/IPXA2024042970045), Apr 18, 2024: HANDLE. DAMAGED. *SUPPLEMENTAL SDR* CREW ENTRY DOOR HANDLE LINING PANEL (REF IPC 52-11-02-10A-140) HAS A 2€?X1.5€? HOLE IN HANDLE STOWED POSITION. C/W INSTALL OF DOORWAY LININ
- [SDR IPXA2024041870045](https://openairdocs.org/sdr/IPXA2024041870045), Apr 18, 2024: PANEL. DAMAGED. *SDR FILED OPEN* CREW ENTRY DOOR HANDLE LINING PANEL (REF IPC 52-11-02-10A-140) HAS A 2€?X1.5€? HOLE IN HANDLE STOWED POSITION. ACCOMPLISHED INTERIM REPAIR PE
- [SDR IPXA2024021647669](https://openairdocs.org/sdr/IPXA2024021647669), Feb 13, 2024: ACTUATOR. INOPERATIVE. **SUPPLEMENTAL SDR**NOSE LANDING GEAR FAILED TO EXTENDED. R&R DOWN LOCK ACTUATOR IAW 32-34-02-004-001 AND AMM 32-34-02-404-017.
- [SDR 2024F00036](https://openairdocs.org/sdr/2024F00036), Feb 13, 2024: ACTUATOR. FAILED. ON ARRIVAL, PILOT REPORTED " NOSE LDG FAILED TO BE EXTENDED ON FIRST ATTEMPT. AFTER GO-AROUND AND CYCLED LDG HANDLE, ALL LDG EXTENDED NORMALLY. T/S ACC. FIM TAS
- [SDR IPXA2024021640437](https://openairdocs.org/sdr/IPXA2024021640437), Feb 13, 2024: INDICATION SYS. FALSE INDICATION. UPON LOWERING THE GEAR ON FINAL APPROACH. NOSE GEAR FAILED TO INDICATE GREEN AND GEAR DISAGREE LIGHT ILLUMINATED. AFTER ALT GEAR EXTENSION RESULTED IN SAFE GEAR
- [SDR IPXA2024021447669](https://openairdocs.org/sdr/IPXA2024021447669), Feb 13, 2024: CHECK VALVE. FAULTED. NOSE LANDING GEAR FAILED TO EXTENDED. PERFORMED FIM TASK 32-30 TREE 807.<BR><BR>STEP 1. FOUND CHECK VALVES NO.1 AND NO.4 ARE CLEANED. <BR>STEP. 2 FOUND RESTRICT
- [SDR IPXA2023122544033](https://openairdocs.org/sdr/IPXA2023122544033), Dec 25, 2023: DEPRESSOR. UNKNOWN. *ATB* CABIN ALTITUDE WARNING ALERT AT FL360 CABIN ALTITUDE AT 1600 FEET AND CLIMBING. RAN CABIN ALT CHECKLIST. DESCENDED LOWER ALTITUDE. RAN CABIN AUTOMATIC INO
- [SDR IPXA2023101818375](https://openairdocs.org/sdr/IPXA2023101818375), Oct 17, 2023: LIGHT. INOPERATIVE. **SUPPLEMENTAL SDR**EMERGENCY LIGHTS TURN ON INTERMITTENTLY IN ARMED POSITION. REPEAT WRITE UP LOG G11357 REPLACED EMER LIGHTING POWER SUPPLY AND BATT ASSY. SYS
- [SDR IPXA2023101718375](https://openairdocs.org/sdr/IPXA2023101718375), Oct 17, 2023: UNKNOWN. UNKNOWN. **SDR FILED OPEN**EMERGENCY LIGHTS TURN ON INTERMITTENTLY IN ARMED POSITION. REAPEAT WRITE UP LOG G11357
- [SDR IPXA2023101248705](https://openairdocs.org/sdr/IPXA2023101248705), Oct 12, 2023: LIGHT. INOPERATIVE. EMERG LIGHT NEXT TO CREW ENTRY DOOR BLINKS ON AND OFF PERFORMED OPS CHECK OF EMERGENCY LIGHT PER AMM 33-51-00. OPS CHECK GOOD. NO FAULT NOTED AT THIS TIME.
- [SDR IPXA2023101102152](https://openairdocs.org/sdr/IPXA2023101102152), Oct 10, 2023: LIGHT. INOPERATIVE. ON TAXI IN, AFTER LANDING, EMER LIGHTS CAME ON AND STAYED ON WITH SWITCH IN ARMED POSITION DISCONNECTED AND RECONNECTED EMERGENCY LIGHTING BATTERY PACK IAW MM 3
- [SDR IPXA2023080819059](https://openairdocs.org/sdr/IPXA2023080819059), Aug 8, 2023: TRANSCEIVER. ARCED. ATB, ON CLIMB OUT,(WXR FAIL) DISPLAYED ON BOTH CAPT AND FO ND. INTERMITTENT (WXR SYS) STATUS MESSAGE DISPLAYED. RESULTED IN AIR TURN BACK. OII 1 FOUND EVIDENCE 
- [SDR IPXA2022082285505](https://openairdocs.org/sdr/IPXA2022082285505), Aug 22, 2022: FMC. INOPERATIVE. INSPECTION TYPE:N/A**ATB** AT CRUISE BOTH FMC'S LOST FP AND FROZE UP ,LOST ALL VNAV, NO INPUTS WOULD WORK.C/W'D FIM, 34-61-00-854, GROUND TEST-OPERATION-PASSED.
- [SDR IPXA2022072584553](https://openairdocs.org/sdr/IPXA2022072584553), Jul 25, 2022: CIRCUIT BREAKER. INOPERATIVE. INSPECTION TYPE:ETOPRIGHT ENGINE EEC POWER CH "A" CIRCUIT BREAKER OPENR & R # 2 ENG EEC CH "A" RELAYS K01171 , K01039 K01174 IAW SWPM 20-81-22 NO FIX 5079816 07
- [SDR IPXA2022062483433](https://openairdocs.org/sdr/IPXA2022062483433), Jun 13, 2022: SKIN PANEL. CRACKED. INSPECTION TYPE:C12CRACK ON NOSE SKIN (P/N: 114T4105-23) OF NO.5 SLAT AT OSS 492.45REPAIR I.A.W 767-300F SRM 57-43-01-2R-2 REV.83.02
- [SDR IPXA2022031980268](https://openairdocs.org/sdr/IPXA2022031980268), Mar 19, 2022: NONE. NONE. INSPECTION TYPE:NA** AIR TURN BACK ** L ENG BLEED OFF EICAS ILLUMINATED. L ENG BLEED OFF LIGHT REMAINED ILLUMINATED . QRH PROCEDURE COMPLETED. TURNBACK AFTER CO
- [SDR IPXA2021111275914](https://openairdocs.org/sdr/IPXA2021111275914), Nov 12, 2021: NONE. NONE. INSPECTION TYPE:NAIT TOOK SEVERAL ATTEMPTS TO PUSH YELLOW DOOR HANDLE TO PROPER POSITIONR&RED FWD ENTRY DOOR CAPTURE SYSTEM PAWL & SPRING REF IPC 52-12-25-02 IT
- [SDR IPXA2021062470913](https://openairdocs.org/sdr/IPXA2021062470913), Jun 23, 2021: CIRCUIT CARD. FALSE INDICATION. ATB** EMERGENCY DECLARED** LANDED UNEVENTFULLY** ON TAKEOFF ROLL JUST PRIOR TO V1 WE GOT A CONFIG LIGHT, SPEED BRAKES LIGHT GEAR NOT DOWN EICAS MESSAGE AND SPOI
- [SDR IPXA2021042168494](https://openairdocs.org/sdr/IPXA2021042168494), Apr 21, 2021: SENSOR. MALFUNCTIONED. DUE TO INBOUND ITEM "GEAR NOT DOWN" EICAS MESSAGE. CHECKED GEAR DOWN LOCK SENSORS REF SSM 32 61 01 SH. 1 FOUND TARGET NEAR VALUES AS FOLLOWS. S236 AT 5.25 MH, S

All 131: https://openairdocs.org/aircraft/N330UP/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.