# N306UP: 1996 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: 27759
- Year built: 1996
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: February 1, 2005
- Certificate issued: August 4, 2008
- Expires: February 29, 2028
- Mode S code: A3376C
- Registered owner: [United Parcel Service Co](https://openairdocs.org/faa-owner/UNITED%20PARCEL%20SERVICE%20CO)
- Location: [Louisville, KY](https://openairdocs.org/faa-place/KY/Louisville)
- Owner type: Corporation
- 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=306UP
- Page: https://openairdocs.org/aircraft/N306UP

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/N306UP/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 N306UP.

## FAA accident and incident reports

None matched to N306UP.

## Service difficulty reports (127, 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 IPXA2026090945477](https://openairdocs.org/sdr/IPXA2026090945477), Sep 9, 2026: HANDLE. FAULTED. YELLOW SECURITY HANDLE WONT STOW ON CREW DOOR. REPLACED CREW ENTRY DOOR INTERLOCK PAWL IAW AMM 52-11-26. OPS CHECK GOOD.
- [SDR IPXA2026083105397](https://openairdocs.org/sdr/IPXA2026083105397), Aug 30, 2026: DOOR. FAULTED. MAIN CABIN DOOR YELLOW HANDLE WILL NOT MOVE. OPENED AND CLOSED CREW ENTRY DOOR INTERNALLY AND EXTERNALLY SEVERAL TIMES OBSERVING NORMAL EXTERNAL PRIMARY CAPTURE
- [SDR IPXA2026082496541](https://openairdocs.org/sdr/IPXA2026082496541), Aug 21, 2026: CONTROL HANDLE. FAULTED. GEAR DISAGREE MSG. WENT AROUND RAN QRH. GEAR DISAGREE MSG LIGHT EXTINGUISHED, GEAR EXTENDED ON SECOND ATTEMPT. ON EXTENSION ON FIRST TIME IT FELT STIFF GOING TO
- [SDR IPXA2026071701536](https://openairdocs.org/sdr/IPXA2026071701536), Jul 16, 2026: SKID. STUCK. EMERGENCY DECLARED GEAR DISAGREE AND TAIL SKID EICAS MESSAGE AFTER DROPPING THE GEAR ON APPROACH, DISCONTINUED, RAN CHECKLIST AND LANDED NORMALLY. POST FLIGHT S
- [SDR IPXA2025090836419](https://openairdocs.org/sdr/IPXA2025090836419), Sep 5, 2025: PAWL. FAULTED. MAIN CABIN DOOR WON`T CLOSE. R & R ENTRY/SERVICE DOOR INTERLOCK PAWL PER AMM 52-11-26/401. OPS CHECK GOOD REF AMM 52-11-26-710-801.
- [SDR IPXA2025061668615](https://openairdocs.org/sdr/IPXA2025061668615), Feb 15, 2025: SKIN. DENTED. MAJOR REPAIR, FOUND DENT AT STA 570 A/C LEFT 13.5" BELOW SKIN LAP JOINT REPAIRED DAMAGE IAW EO-92838-REQ2
- [SDR IPXA2025011354264](https://openairdocs.org/sdr/IPXA2025011354264), Jan 7, 2025: TEE FITTING. CRACKED. CRACK , SUPPORT STRUT AT L/H WING FAIRING PANEL 195CL. (REPLACE). ACCOMPLISHED REPAIR I.A.W UPS EO NO: EO-92500-REQ1 REV. 1. INSTALLED REPAIR PARTS I.A.W SRM 51
- [SDR IPXA2025011323526](https://openairdocs.org/sdr/IPXA2025011323526), Jan 4, 2025: PANEL. CRACKED. FAULT - FOUND THE BALL MAT FLOOR STRUCTURE CRACK AT AFT CARGO STA 1336 BL 0 (REPLACE). FABRICATE PARTS (P/N:451T2603-65) PER BOEING DWG NO: 451T2603 DWG SH 11 R
- [SDR IPXA2025010726757](https://openairdocs.org/sdr/IPXA2025010726757), Jan 4, 2025: NONE. NONE. ADD SDR FOR EO-82173-JIC001 (FUSELAGE DRAIN HOLES INSPECTION AND INSTALLATION AFT OF BS 1725.5 BETWEEN S-36L AND S-36R) COMPLETED SDR.
- [SDR IPXA2025011384372](https://openairdocs.org/sdr/IPXA2025011384372), Jan 1, 2025: RIB. CRACKED. FAULT - CRACK - CHORD, L/H WING OUTBD L/E UPPER RIB LOWER CHORD, OSS 531.71. (REPLACE). REMOVED DAMAGE PART I.A.W SRM 51-40-02-0G REV. 91. INSTALLED NEW PART I.
- [SDR IPXA2025011281553](https://openairdocs.org/sdr/IPXA2025011281553), Jan 1, 2025: ANGLE. CRACKED. FAULT - CRACK - ANGLE BULK CARGO COMPARTMENT LEFT OUTBOARD AREA STA 1578 LBL 60. (REPLACE). REMOVED DAMAGE PART I.A.W SRM 51-40-02-0G REV. 91. INSTALLED NEW PAR
- [SDR IPXA2025011281531](https://openairdocs.org/sdr/IPXA2025011281531), Jan 1, 2025: ANGLE. CRACKED. FAULT - CRACK - ANGLE BULK CARGO COMPARTMENT RIGHT OUTBOARD AREA STA 1578 RBL 60. (REPLACE). REMOVED DAMAGE PART I.A.W SRM 51-40-02-0G REV. 91. INSTALLED NEW PA
- [SDR IPXA2025010985385](https://openairdocs.org/sdr/IPXA2025010985385), Jan 1, 2025: CYLINDER. CORRODED. FOUND OUTER CYLINDER INNER SURFACE CORROSION OF RIGHT MAIN GEAR. (EVALUATE). ACCOMPLISHED REPAIR I.A.W UPS EO NO: EO-92452-REQ1 REV. 1. JOB COMPLETED.
- [SDR IPXA2025010882763](https://openairdocs.org/sdr/IPXA2025010882763), Jan 1, 2025: SKIN. DEBONDED. DISBOND FOUND RUDDER R/H SPAR AND ADJACENT STRUCTURE BETWEEN RUDDER STATION 106 AND STATION 181. (REPAIR). REPAIR DELAMINTION ON RH RUDDER SKIN PANEL AT RUD STA
- [SDR IPXA2025010985793](https://openairdocs.org/sdr/IPXA2025010985793), Jan 1, 2025: LATCH. CORRODED. CORROSION - LATCH, KEEL BEAM AFT SECTION PANEL 149BL AFT SIDE. (REPLACE). REMOVED DAMAGE PARTS I.A.W SRM 51-40-02-0G REV. 91. INSTALL NEW PARTS I.A.W SRM 51-40-
- [SDR IPXA2025010153642](https://openairdocs.org/sdr/IPXA2025010153642), Dec 30, 2024: FLOOR PANEL. DENTED. FOUND MAIN DECK FLOOR PANEL DENT, P/N:143T5876-68 (REPAIR). TO FABRICATE A NEW FLOOR PANEL I.A.W. SREO-9693-REQ001 REV.4. CONDITION CHECK IS SATISFACTORY. I.A.W
- [SDR IPXA2025010153645](https://openairdocs.org/sdr/IPXA2025010153645), Dec 30, 2024: FLOOR PANEL. DENTED. FOUND MAIN DECK FLOOR PANEL DENT, P/N: 143T5876-19 (REPAIR). TO FABRICATE A NEW FLOOR PANEL I.A.W. SREO-9693-REQ001 REV.4. CONDITION CHECK IS SATISFACTORY. I.A.
- [SDR IPXA2025010153633](https://openairdocs.org/sdr/IPXA2025010153633), Dec 30, 2024: FLOOR PANEL. DENTED. FOUND MAIN DECK FLOOR PANEL DENT, P/N:146T5869-9 (REPAIR). TO FABRICATE A NEW FLOOR PANEL I.A.W. SREO-9693-REQ001 REV.4. CONDITION CHECK IS SATISFACTORY. I.A.W 
- [SDR IPXA2025010153649](https://openairdocs.org/sdr/IPXA2025010153649), Dec 30, 2024: FLOOR PANEL. DENTED. FOUND MAIN DECK FLOOR PANEL DENT, P/N:143T5876-82 (REPAIR). TO FABRICATE A NEW FLOOR PANEL I.A.W. SREO-9693-REQ001 REV.4. CONDITION CHECK IS SATISFACTORY. I.A.W
- [SDR IPXA2025010930003](https://openairdocs.org/sdr/IPXA2025010930003), Oct 8, 2024: SKIN. DENTED. *SDR FILED OPEN* REF BARCODE T3F18E005AYYG DENT ON TAIL OF FUSELAGE, TO THE LEFT OF TAIL SKID. APPROXIMATELY 6" FORWARD OF STRINGER AT ST 1702.0. RE-OPENED DUE 
- [SDR IPXA2024072592231](https://openairdocs.org/sdr/IPXA2024072592231), Jul 25, 2024: SEAL. LOOSE. CREW ENTRY DOOR SEAL LOOSE ON THE UPPER FORWARD PORTION OF THE DOOR WHEN DOOR IS CLOSED. FOUND DECORATICE AND PROTECTIVE RUBBER SEAL INSIDE OF DOOR MOVED OUT OF
- [SDR IPXA2024051459511](https://openairdocs.org/sdr/IPXA2024051459511), May 8, 2024: WARNING MESSAGE. FALSE ACTIVATION. LOWERED LANDING GEAR TO DOWN. NOSE TURNED GREEN BUT LEFT&RIGHT DID NOT.EICAS GEAR DISAGREE AND GEAR DOORS MESSAGE APPEARED. VISUALLY INSPECTED BOTH MAIN LANDING
- [SDR IPXA2024050859511](https://openairdocs.org/sdr/IPXA2024050859511), May 8, 2024: LANDING GEAR. MALFUNCTIONED. LOWERED LANDING GEAR TO DOWN NOSE TURNED GREEN BUT LT & RT DID NOT.EICAS GEAR DISAGREE AND GEAR DOORS MESSAGE APPEARED. ITEM DEF PER MEL32-30-1. C/W DMP. PLACAR
- [SDR IPXA2023121481604](https://openairdocs.org/sdr/IPXA2023121481604), Dec 14, 2023: LEVER. INOPERATIVE. ENTRY/SERVICE DOOR CAPTURE LEVER WILL NOT LATCH FROM THE INSIDE. ++ FOUND BOTH ARMS OF SECONDARY LOCK PAWL BROKEN/MISSING. R&R'D SAME IAW CMM 52-11-12-81205. OP
- [SDR IPXA2023021991123](https://openairdocs.org/sdr/IPXA2023021991123), Feb 9, 2023: BRACKET. NONE. INSPECTION TYPE:C14CRACK ON BRACKET (P/N:146T1261-25) OF BULK CARGO FLOOR BEAM AT STA 1418, LBL22.INSTALL NEW PART I.A.W 767-300F SRM 51-40-02-0G, REV 85.01, BO
- [SDR IPXA2023021891102](https://openairdocs.org/sdr/IPXA2023021891102), Feb 8, 2023: BRACKET. NONE. INSPECTION TYPE:C14CRACK ON BRACKET (P/N:148T7312-43) OF L/H HORIZONTAL STABILIZER SEAL FAIRING NEAR STA 1767.25INSTALL NEW PART I.A.W 767-300F SRM 51-40-02-0G,
- [SDR IPXA2023021991122](https://openairdocs.org/sdr/IPXA2023021991122), Feb 7, 2023: NONE. NONE. INSPECTION TYPE:C14CRACK ON CLIP(P/N:140T0130-38) OF AFT CARGO COMPARTMENT FLOOR BEAM AT STA 1065, RBL26.INSTALL NEW PART I.A.W 767-300F SRM 51-40-02-0G, REV 85
- [SDR IPXA2023021891101](https://openairdocs.org/sdr/IPXA2023021891101), Feb 7, 2023: NONE. NONE. INSPECTION TYPE:C14CRACK ON CLIP(P/N:140T0130-39) OF AFT CARGO COMPARTMENT FLOOR BEAM AT STA 1065, LBL 26.INSTALL NEW PART I.A.W 767-300F SRM 51-40-02-0G, REV 8
- [SDR IPXA2023021691035](https://openairdocs.org/sdr/IPXA2023021691035), Feb 7, 2023: SKIN. CRACKED. INSPECTION TYPE:C14*MAJOR REPAIR* CRACK ON NOSE SKIN (P/N:114T4104-3) OF NO.4 SLAT AT OSS 572.549.REPAIR I.A.W 767-300F SRM 57-43-01-2R-2 REV.85.01.
- [SDR IPXA2023021691034](https://openairdocs.org/sdr/IPXA2023021691034), Feb 7, 2023: SKIN. CRACKED. INSPECTION TYPE:C14*MAJOR REPAIR* CRACK ON NOSE SKIN (P/N:114T4102-3) OF NO.2 SLAT AT OSS 946.828.REPAIR I.A.W 767-300F SRM 57-43-01-2R-2 REV.85.01.
- [SDR IPXA2023021591008](https://openairdocs.org/sdr/IPXA2023021591008), Feb 6, 2023: STIFFENER. CRACKED. INSPECTION TYPE:C14*MAJOR REPAIR* CRACK ON CENTER WING TANK STIFFENER (P/N:11T2011-6) ON STA 785.9, RBL 55.REPAIR I.A.W 767-300F SRM 57-10-10-2R-2 REPAIR 2 REV.
- [SDR IPXA2023021591009](https://openairdocs.org/sdr/IPXA2023021591009), Feb 6, 2023: STIFFENER. CRACKED. INSPECTION TYPE:C14*MAJOR REPAIR* CRACK ON CENTER WING TANK STIFFENER (P/N:111T2011-5 ON STA 785.9, LBL 55.REPAIR I.A.W 767-300F SRM 57-10-10-2R-2 REPAIR 2 REV.
- [SDR IPXA2022010777616](https://openairdocs.org/sdr/IPXA2022010777616), Jan 6, 2022: WARNING MESSAGE. ILLUMINATED. EICAS MSG FIRE/ OVERHEAT SYS ON FINAL APPROACH. RAN CHECKLIST, MESSAGE CLEARED. NOTED MSG CLEARED WITH CHECKLIST, PERFORMED FIRE DETECTION TEST REF AMM 26-11-00
- [SDR IPXA2021032567241](https://openairdocs.org/sdr/IPXA2021032567241), Mar 24, 2021: LENS. DETACHED. INSPECTION TYPE:NADOOR EXIT SIGN COVER FELL OFF.INSTALLED DOOR EXIT SIGN PER AMM 33-51-01-402-030. TESTED OK.
- [SDR IPXA2021022466059](https://openairdocs.org/sdr/IPXA2021022466059), Feb 18, 2021: FLOOR PANEL. DAMAGED. INSPECTION TYPE: C13 DAMAGE ON M/D FLOOR PANEL AT STA 554 , RBL 77.5. FABRICATE THE REPLACEMENT FLOOR PANEL PER EO NO. B767-5320-9693-I.
- [SDR IPXA2021022466058](https://openairdocs.org/sdr/IPXA2021022466058), Feb 18, 2021: FLOOR PANEL. DAMAGED. INSPECTION TYPE: C13 DAMAGE ON M/D FLOOR PANEL AT STA 745, RBL 77.5. FABRICATE THE REPLACEMENT FLOOR PANEL PER EO NO.B767-5320-9693-I.
- [SDR IPXA2021022065866](https://openairdocs.org/sdr/IPXA2021022065866), Feb 15, 2021: FLOOR PANEL. DAMAGED. INSPECTION TYPE: C13 DAMAGE ON M/D FLOOR PANEL AT STA 654 PLUS 110, LBL 75. FABRICATE THE REPLACEMENT FLOOR PANEL PER EO NR B767-5320-9693-I.
- [SDR IPXA2021022065865](https://openairdocs.org/sdr/IPXA2021022065865), Feb 15, 2021: FLOOR PANEL. DAMAGED. INSPECTION TYPE: C13 DAMAGE ON M/D FLOOR PANEL AT STA 676, RBL 84. FABRICATE THE REPLACEMENT FLOOR PANEL PER EO NR B767-5320-9693-I.
- [SDR IPXA2021022065867](https://openairdocs.org/sdr/IPXA2021022065867), Feb 12, 2021: FLOOR PANEL. DAMAGED. INSPECTION TYPE: C13 DAMAGE ON M/D FLOOR PANEL AT STA 652, LBL 11 - LBL 13. FABRICATE THE REPLACEMENT FLOOR PANEL PER EO NO. B767-5320-9693-I.
- [SDR IPXA2021022566089](https://openairdocs.org/sdr/IPXA2021022566089), Feb 9, 2021: SEAT TRACK. CORRODED. INSPECTION TYPE:C13CORROSION ON M/D SEAT TRACK (P/N:143T5243-10) BETWEEN STA 434 AND STA654 PLUS 11 AT RBL 88.50.PART REPLACEMENT I.A.W. BOEING DRAWING 143T5226
- [SDR IPXA2021022466062](https://openairdocs.org/sdr/IPXA2021022466062), Feb 9, 2021: SKIN. CRACKED. INSPECTION TYPE: C13 CRACK FOUND ON FUSELAGE SKIN AT STA 1654.5, S-13AR. REPAIR IAW SRID: 3-4978953707 AND UPS EO B767-5330-79406-A.
- [SDR IPXA2019090546386](https://openairdocs.org/sdr/IPXA2019090546386), Sep 5, 2019: HOLDER. MISSING. INSPECTION TYPE:N/A FLIGHT DECK FWD ENTRY DOOR EMERGENCY EXIT GIN FLOOR ILLUMINATION LAMPS INOP. REMOVED ENTRY DOOR EMERGENCY SIGN LENS FOUND FLOOR ILLUMINATION
- [SDR IPXA2019030139558](https://openairdocs.org/sdr/IPXA2019030139558), Feb 18, 2019: FITTING. MISSING. INSPECTION TYPE:C12 DURING C12 CHECK OF DATUM AIRCRAFT M FITTING WAS MISSING (P/N : 114T4302-4) ON NR 9 SLAT. REPAIR IAW SRID 4-4361059322 AND EO B767-5750-7176
- [SDR IPXA2019022739499](https://openairdocs.org/sdr/IPXA2019022739499), Feb 18, 2019: FLOOR PANEL. DAMAGED. INSPECTION TYPE:C12DAMAGE ON M/D CARGO FLOOR PANEL AT STA 533 - STA 654 PLUS 22 , RBL 55 - RBL 77 , PNL NO. 232HFFFABRICATE THE REPLACEMENT FLOOR PANEL PER EO N
- [SDR IPXA2019022739498](https://openairdocs.org/sdr/IPXA2019022739498), Feb 18, 2019: FLOOR PANEL. DAMAGED. INSPECTION TYPE:C12DAMAGE ON M/D CARGO FLOOR PANEL AT STA 533 - STA 654 PLUS 22 , LBL 33 - LBL 55 , PNL NO. 231HFFFABRICATE THE REPLACEMENT FLOOR PANEL PER EO N
- [SDR IPXA2019022739497](https://openairdocs.org/sdr/IPXA2019022739497), Feb 18, 2019: FLOOR PANEL. DAMAGED. INSPECTION TYPE:C12DAMAGE ON M/D CARGO FLOOR PANEL AT STA 533 - STA 654 PLUS 22 , LBL 11 - LBL 33 , PNL NO . 231GFFFABRICATE THE REPLACEMENT FLOOR PANEL PER EO 
- [SDR IPXA2019022769454](https://openairdocs.org/sdr/IPXA2019022769454), Feb 18, 2019: STIFFENER. CRACKED. INSPECTION TYPE:C12CRACK ON THE CENTER WING FRONT SPAR STIFFENER (P/N : 111T2005-7) UPPER SIDE AT STA 785.9 , LBL 11REPAIR I.A.W 767-300F SRM 57-10-10-2R-2 REPA
- [SDR IPXA2019022769453](https://openairdocs.org/sdr/IPXA2019022769453), Feb 18, 2019: STIFFENER. CRACKED. INSPECTION TYPE:C12CRACK ON THE CENTER WING FRONT SPAR STIFFENER (P/N : 111T2008-11) UPPER SIDE AT STA 785.9 , LBL 33REPAIR I.A.W 767-300F SRM 57-10-10-2R-2 REP
- [SDR IPXA2018101034874](https://openairdocs.org/sdr/IPXA2018101034874), Oct 9, 2018: COVER. BROKEN. DOOR LOCK COVER PLATE WAS BROKEN OFF. REPLACED THE HINGE AND COVER.
- [SDR IPXA2018070931471](https://openairdocs.org/sdr/IPXA2018070931471), Jul 8, 2018: WINDOW. FAULTY. "L SIDE WINDOW" EICAS MSG DURING CRUISE. AFTER RESET IAW QRH PROC, "L SIDE WINDOW' EICAS AND ASSOC INOP LITE OUT. R&R L2 SIDE WINDOW PER MM 56-11-02-004-001/404

All 127: https://openairdocs.org/aircraft/N306UP/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

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