# N323UP: 1997 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: 27749
- Year built: 1997
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: December 14, 1997
- Certificate issued: December 16, 1997
- Expires: February 28, 2029
- Mode S code: A37B45
- 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=323UP
- Page: https://openairdocs.org/aircraft/N323UP

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/N323UP/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 (1)

From the NTSB's public API. Aircraft are matched to registry aircraft by N-number and event date, checked against the reported serial number, make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model.

- [NTSB ENG21WA043](https://openairdocs.org/ntsb/ENG21WA043), Sep 18, 2021: Boeing 767-34AF (N323UP), Bogota, Colombia, incident, no damage

## FAA accident and incident reports

None matched to N323UP.

## Service difficulty reports (161, 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 IPXA2026101442976](https://openairdocs.org/sdr/IPXA2026101442976), Oct 14, 2026: FLAP SYSTEM. FAULTED. AIR TURN BACK, EMERGENCY DECLARED. AFTER TAKEOFF ON FLAP RETRACTION EICAS MESSAGE LE SLAT ASYMMETRY. FOLLOWED QRH PROCEDURE COULD NOT RETRACT SLAT. RETURNED SDF
- [SDR IPXA2026092495235](https://openairdocs.org/sdr/IPXA2026092495235), Sep 23, 2026: PAWL. NOT SEATED. L FWD ENT DOOR SECURE HANDLE WILL NOT SEAT FOUND DEEP GOUGES IN ENTRY DOOR INTERLOCK PAWL. REPLACED INTERLOCK PAWL IAW AMM 52-11-26-404-003. OPS CHECK GOOD IAW 
- [SDR IPXA2026072263413](https://openairdocs.org/sdr/IPXA2026072263413), Jul 21, 2026: ELEVATOR. DAMAGED. ***SUPPLEMENTAL SDR*** LINE MAINTENANCE REPORTS DAMAGE TO THE UPPER SIDE OF THE LH INBOARD ELEVATOR. VERIFIED TORQUE AND SAFETIES OF ALL MOUNTING BOLTS. WITNESS
- [SDR IPXA2026072163413](https://openairdocs.org/sdr/IPXA2026072163413), Jul 21, 2026: ELEVATOR. DAMAGED. LINE MAINTENANCE REPORTS DAMAGE TO THE UPPER SIDE OF THE LT INBOARD ELEVATOR. VERIFIED TORQUE AND SAFETIES OF ALL MOUNTING BOLTS. WITNESSED OPS CHECKS PER GMM 0
- [SDR IPXA2024111257988](https://openairdocs.org/sdr/IPXA2024111257988), Nov 4, 2024: STRAP. CRACKED. CRACKED BULKHEAD OUTER CHORD STRAP AT BS 1725 S-7R. (REPAIR). COMPLETED REPAIR I.A.W EGAT WORK SHEET NO.40938 STEP D.5 AND D.6 AND D.8 AND D.10 AND D.11 AND D.1
- [SDR IPXA2024110450317](https://openairdocs.org/sdr/IPXA2024110450317), Nov 3, 2024: FLOOR PANEL. BROKEN. FOUND M/D FLOOR PNL NO. 241DFF BROKEN AT STA 731 TO STA 834 LBL-65, P/N : 145T5876-63.FABRICATED A NEW FLOOR PANEL I.A.W. SREO-9693-REQ001 REV.4.
- [SDR IPXA2024110338489](https://openairdocs.org/sdr/IPXA2024110338489), Nov 2, 2024: FLOOR PANEL. DAMAGED. FOUND M/D FLOOR PNL DENT AND BROKEN AT STA 1040 TO STA 1114 LBL-45, P/N: 145T5876-43, PANEL NO 241BGF. FABRICATED A NEW FLOOR PANEL I.A.W. SREO-9693-REQ001 REV.
- [SDR IPXA2024110436353](https://openairdocs.org/sdr/IPXA2024110436353), Nov 2, 2024: SKIN. DAMAGED. BIRD STRIKE - SKIN, UPPER FACE OF L/H WING NO.4 SLAT T/E SKIN, OSS 545.75.JOB COMPLETED AND CONDITION CHECK NORMAL AND ATTACHMENT ARE UPLOADED. I.A.W AMM 27-81-
- [SDR IPXA2024110338863](https://openairdocs.org/sdr/IPXA2024110338863), Nov 2, 2024: FLOOR PANEL. DENTED. FOUND M/D FLOOR PNL NO.241EFF DENT AT STA 746 TO STA 876 LBL 80, P/N:145T5876-1.FABRICATED A NEW FLOOR PANEL I.A.W. SREO-9693-REQ001 REV.4.
- [SDR IPXA2024110338708](https://openairdocs.org/sdr/IPXA2024110338708), Nov 2, 2024: FLOOR PANEL. DENTED. FOUND M/D FLOOR PNL NO.241WFF DENT AT STA 980 TO STA-1114 LBL11, P/N: 145T5876-73. FABRICATED A NEW FLOOR PANEL I.A.W. SREO-9693-REQ001 REV.4.
- [SDR IPXA2024110338469](https://openairdocs.org/sdr/IPXA2024110338469), Nov 2, 2024: FLOOR PANEL. DEBONDED. FOUND M/D FLOOR PNL NO.241BFF DISBOND AT STA 731 TO STA 834 LBL-22, P/N:145T5876-70. FABRICATED A NEW FLOOR PANEL I.A.W. SREO-9693-REQ001 REV.4.
- [SDR IPXA2024110338198](https://openairdocs.org/sdr/IPXA2024110338198), Nov 2, 2024: FLOOR PANEL. DENTED. DENT - FOUND M/D FLOOR PNL NO.242FFF AT STA 834 TO STA 933 RBL -45, P/N: 145T5876-61.FABRICATED A NEW FLOOR PANEL I.A.W. SREO-9693-REQ001 REV.4.
- [SDR IPXA2024110338212](https://openairdocs.org/sdr/IPXA2024110338212), Nov 2, 2024: FLOOR PANEL. DENTED. FOUND M/D FLOOR PNL DISBOND AND DENT AT STA 746 TO STA 876 RBL -80 PNL NO.242DFF, P/N: 145T5876-7. FABRICATED A NEW FLOOR PANEL I.A.W. SREO-9693-REQ001 REV.4.
- [SDR IPXA2024110338861](https://openairdocs.org/sdr/IPXA2024110338861), Nov 2, 2024: FLOOR PANEL. DENTED. FOUND M/D FLOOR PNL NO.241CFF DENT AND INSERT DAMAGE AT STA 731 TO STA 834 LBL-45, P/N:145T5876-65. FABRICATED A NEW FLOOR PANEL I.A.W. SREO-9693-REQ001 REV.4.
- [SDR IPXA2024110338563](https://openairdocs.org/sdr/IPXA2024110338563), Nov 2, 2024: FLOOR PANEL. DENTED. FOUND FLOOR PNL NO.241QFF DENT AT STA 933 TO STA 980 LBL-80, P/N: 145T5876-78. FABRICATED A NEW FLOOR PANEL I.A.W. SREO-9693-REQ001 REV.4.
- [SDR IPXA2024110338943](https://openairdocs.org/sdr/IPXA2024110338943), Nov 2, 2024: FLOOR PANEL. DENTED. FOUND M/D FLOOR PNL DENT AND INSERT DAMAGE AT STA 988 TO STA 1114 LBL 65 PNL NO.241ZFF, P/N:145T5876-77.FABRICATED A NEW FLOOR PANEL I.A.W. SREO-9693-REQ001 REV
- [SDR IPXA2024110338453](https://openairdocs.org/sdr/IPXA2024110338453), Nov 2, 2024: FLOOR PANEL. DENTED. FOUND M/D FLOOR PNL NO.241GFF DENT AT STA 834 TO STA 933 LBL-22, P/N: 145T5876-59. FABRICATED A NEW FLOOR PANEL I.A.W. SREO-9693-REQ001 REV.4.
- [SDR IPXA2024110336507](https://openairdocs.org/sdr/IPXA2024110336507), Nov 2, 2024: FLOOR PANEL. BROKEN. BROKEN - FOUND M/D FLOOR PNL BROKEN AT STA933 TO STA980 RBL-80 P/N: 145T5876-84 , PANEL NO.242MFF. FABRICATED A NEW FLOOR PANEL I.A.W. SREO-9693-REQ001 REV.4.
- [SDR IPXA2024112108973](https://openairdocs.org/sdr/IPXA2024112108973), Nov 1, 2024: TRIM PANEL. BROKEN. FOUND MAIN ENTRY DOOR DOORWAY SPLINE TRIM BROKEN. REPLACED SPLINE TRIM I.A.W AMM 52-12-02-004-001 REV.143 AND AMM 52-12-02-404-025 REV.143.
- [SDR IPXA2024110905997](https://openairdocs.org/sdr/IPXA2024110905997), Nov 1, 2024: SKIN. CORRODED. CORROSION , FUSELAGE SKIN STA 1410 BETWEEN S-38R AND S-39R. ACCOMPLISH REPAIR PER EO-91974-REQ1 AND EGAT EI F2024A53M-2800, REV. 0 AND 1.
- [SDR IPXA2024110908905](https://openairdocs.org/sdr/IPXA2024110908905), Nov 1, 2024: ADAPTER. CRACKED. FOUND THE MAIN DECK CARGO RESTRAINT FLOOR ADAPTER FITTING WITH CRACK DAMAGE AT STA 1109 BL 0.REMOVED DAMAGE PART I.A.W SRM 51-40-02-0G REV. 90.INSTALLED NEW PAR
- [SDR IPXA2024110207456](https://openairdocs.org/sdr/IPXA2024110207456), Nov 1, 2024: FLOOR PANEL. DENTED. FOUND THE MAIN DECK CARGO FLOOR PANEL DENT , P/N: 146T5869-134. FABRICATED A NEW FLOOR PANEL I.A.W. SREO-9693-REQ001 REV.4.
- [SDR IPXA2024110207366](https://openairdocs.org/sdr/IPXA2024110207366), Nov 1, 2024: FLOOR PANEL. DENTED. FOUND THE MAIN DECK CARGO FLOOR PANEL DENT , P/N: 146T5869-135. FABRICATED A NEW FLOOR PANEL I.A.W. SREO-9693-REQ001 REV.4.
- [SDR IPXA2024110108973](https://openairdocs.org/sdr/IPXA2024110108973), Nov 1, 2024: SPLINE. BROKEN. FOUND MAIN ENTRY DOOR DOORWAY SPLINE TRIM BROKEN. (REPLACE) OK TO WORK.
- [SDR IPXA2024103178075](https://openairdocs.org/sdr/IPXA2024103178075), Oct 31, 2024: NONE. NONE. FUSELAGE DRAIN HOLES INSPECTION AND INSTALLATION AFT OF BS 1725.5 BETWEEN S-36L AND S-36R. REVIEW COMPLETED PER EO-82173-J1C001.CONDITION CHECK OK
- [SDR IPXA2024100427643](https://openairdocs.org/sdr/IPXA2024100427643), Oct 3, 2024: FIRE SEAL. DAMAGED. *SUPPLEMENTAL SDR* #2 ENG OUTBD ACCESS PANEL FOR ENG MOUNT BOLTS HAS A DAMAGED FIRE SEAL REMOVED AND REPLACED SEAL ON #2 ENG OUTBD ACCESS PANEL REF. SRM 51-40-0
- [SDR IPXA2024100327643](https://openairdocs.org/sdr/IPXA2024100327643), Oct 3, 2024: FIRE SEAL. DAMAGED. #2 ENG OUTBD ACCESS PANEL FOR ENG MOUNT BOLTS HAS A DAMAGED FIRE SEAL REMOVED AND REPLACED SEAL ON #2 ENG OUTBD ACCESS PANEL REF. SRM 51-40-02 AND IPC 54-52-01-
- [SDR IPXA2024060603700](https://openairdocs.org/sdr/IPXA2024060603700), Jun 5, 2024: SLAT TRACK. DAMAGED. R/H WING #7 SLAT TRACK LEADING EDGE PANEL DAMAGED. REMOVE AND REPLACED LEADING EDGE SUPPORT LINK DOOR R/H INB AS PER 57-41-59 404-009, OPS CHKS GOOD-
- [SDR IPXA2024010917389](https://openairdocs.org/sdr/IPXA2024010917389), Dec 30, 2023: SPRING. BROKEN. *** SUPPLEMENTAL SDR *** CREW ENTRY DOOR ARMING LEVER HINGED COVER SPRING BROKEN REPLACED CREW ENTRY DOOR ARMING HINGE COVER REF MM 52-12-02 OPS CK GOOD THIS CL
- [SDR IPXA2023123017389](https://openairdocs.org/sdr/IPXA2023123017389), Dec 30, 2023: UNKNOWN. UNKNOWN. CREW ENTRY DOOR ARMING LEVER HINGED COVER SPRING BROKEN DEFERRED CREW ENTRY DOOR HINGED COVER IAW MEL 52-11-2, PLACARDS INSTALLED. OPEN
- [SDR IPXA2023030191440](https://openairdocs.org/sdr/IPXA2023030191440), Mar 1, 2023: SLAT. INOPERATIVE. INSPECTION TYPE:NA*EMERGENCY DECLARED* LEADING EDGE SLATS DISAGREE RAN CHECKLIST AND CONFIGURED SUCCESFULLYBITE CARRIED OUT IAW FIM 27-51-00-815-809 FLAPS/SLATS
- [SDR IPXA2022102587489](https://openairdocs.org/sdr/IPXA2022102587489), Oct 24, 2022: SKIN. MISREPAIRED. TEMP BLIND FASTENER INSTALLED FUSELAGE 8" FWD OR STA 676 - 1 INCH O/B OF S39LREPAIRED IAW E.O. B767-5330-85085-B ON NRC 684229
- [SDR IPXA2022102487432](https://openairdocs.org/sdr/IPXA2022102487432), Oct 24, 2022: SKIN. MISINSTALLED. INSPECTION TYPE:N/ATEMP BLIND FASTENER INSTALLED FUSELAGE 8 INCH FWD OR STA 676 - 1 INCH O/B OF S39LFABRICATED REPAIR DOUBLER IAW UPS E.O.B767-5330-85085-A ON N
- [SDR IPXA2022032480431](https://openairdocs.org/sdr/IPXA2022032480431), Mar 24, 2022: THRUST REVERSER. INOPERATIVE. INSPECTION TYPE:**ETOPS FILED OPEN** ON LANDING, L THRUST REV WOULD NOT DEPLOY. DEFERRED LEFT ENG T/R PER MEL 78-31-1 C/W DMP 78-31-
- [SDR IPXA2021092074049](https://openairdocs.org/sdr/IPXA2021092074049), Sep 18, 2021: ENGINE. SURGES. IFSD, ATB, EMERGENCY DECLARED, AIRCRAFT OOS, APPROXIMATELY 200' AFTER TAKE OFF, ENG STARTED TO SURGE. DURING THE CLIMB THE L ENG HAD NO RESPONSE FROM THE L THRU
- [SDR IPXA2021020565355](https://openairdocs.org/sdr/IPXA2021020565355), Jan 31, 2021: PANEL. DAMAGED. INSPECTION TYPE: C12 DAMAGE ON MD CARGO FLOOR PANEL BETWEEN STA 510 - 620, LBL 11 - RBL 11. FABRICATE THE REPLACEMENT FLOOR PANEL PER EO NR B767-5320-9693-I.
- [SDR IPXA2021020665376](https://openairdocs.org/sdr/IPXA2021020665376), Jan 27, 2021: FLOORBEAM. CORRODED. INSPECTION TYPE:C12CORROSION WAS FOUND ON FLOOR BEAM (P/N : 146T5143-5) OF MAIN DECK FLOOR STRUCTURE AT STA 1518 , RBL 70 - RBL 90REPAIR I.A.W BOEING SR 3-49425
- [SDR IPXA2021020565350](https://openairdocs.org/sdr/IPXA2021020565350), Jan 27, 2021: FLOORBEAM. CORRODED. INSPECTION TYPE: C12 CORROSION WAS FOUND ON FLOOR BEAM PN 146T5144-11 OF MAIN DECK FLOOR STRUCTURE AT STA 1540, LBL 60 - LBL 80. REPAIR IAW BOEING SR 3-49424087
- [SDR IPXA2021020565349](https://openairdocs.org/sdr/IPXA2021020565349), Jan 27, 2021: FLOORBEAM. CORRODED. INSPECTION TYPE: C12 CORROSION WAS FOUND ON FLOOR BEAM PN 146T5144-11 OF MAIN DECK FLOOR STRUCTURE AT STA 1540, RBL 60 - RBL 80. REPAIR IAW BOEING SR 3-49424087
- [SDR IPXA2021020365255](https://openairdocs.org/sdr/IPXA2021020365255), Jan 24, 2021: STIFFENER. CRACKED. INSPECTION TYPE:C12CRACK ON CENTER WING TANK STIFFENER (P/N : 111T2008-11) ON STA 785.9 , LBL 33REPAIR I.A.W 767-300F SRM 57-10-10-2R-2 REPAIR 2 REV.79.01 AND U
- [SDR IPXA2021020365254](https://openairdocs.org/sdr/IPXA2021020365254), Jan 24, 2021: STIFFENER. CRACKED. INSPECTION TYPE:C12CRACK ON CENTER WING TANK STIFFENER (P/N : 111T2011-5) ON STA 785.9 , LBL 55REAPIR I.A.W 767-300F SRM 57-10-10-2R-2 REPAIR 2 REV.79.01 AND UP
- [SDR IPXA2021011864585](https://openairdocs.org/sdr/IPXA2021011864585), Jan 18, 2021: ACTUATOR. LEAKING. INSPECTION TYPE: NA, ATB, NO EMERGENCY DECLARED & NO EQUIPMENT USED. T/O & 38 MINS GOT L HYD QUANTITY EICAS LT QUANTITY L HYD PRIM PUMP. EICAS LIGHT CAME ON WHE
- [SDR IPXA2020092160443](https://openairdocs.org/sdr/IPXA2020092160443), Sep 20, 2020: MODULE. MALFUNCTIONED. INSPECTION TYPE: N/A ATB- EMERGENCY DECLARED. RECEIVED FIRE WARNING BELL ON TAKE OFF ROTATION COULD NOT EXTINGUISH. R & R M1000 BELL CHIME MODULE BOARD, PER MM 
- [SDR IPXA201902138893](https://openairdocs.org/sdr/IPXA201902138893), Jan 27, 2019: STIFFENER. CRACKED. INSPECTION TYPE:C11CRACK ON VERTICAL STIFFENER AT WHEEL WELL BULKHEAD AT STA 287,RBL 25, WL 159.REPAIR I.A.W UPS EO B767-5310-20118-F AND 767-300F SRM 51-70-12 
- [SDR IPXA2018121436920](https://openairdocs.org/sdr/IPXA2018121436920), Dec 14, 2018: SHUTOFF VALVE. FAULTY. INSPECTION TYPE:N/A ATB - DUE TO CABIN ALTITUDE. AFTER ACCOMPLISHING THE QRH PROC CABIN REMAINED UNCONTROLLABLE. PERFORMED PRESSURE CONTROLLER BITE PROCEDURE FO
- [SDR IPXA2018110213543](https://openairdocs.org/sdr/IPXA2018110213543), Nov 1, 2018: CONTROLLER. MALFUNCTIONED. EICAS MESSAGE FOR THE AFT CABIN TEMP INOPERATIVE. OPEN
- [SDR IPXA2018093034543](https://openairdocs.org/sdr/IPXA2018093034543), Sep 29, 2018: BLADE. MISSING. INSPECTION TYPE:N/A**SUPPLEMENTAL SDR** PERFORMED BORESCOPE INSPECTION #2 ENG PER PMC 6. FOUND 1ST STAGE HPT BLADE MISSING MATERIAL ON LEADING EDGE MEASURING DI
- [SDR IPXA2018100194543](https://openairdocs.org/sdr/IPXA2018100194543), Sep 29, 2018: BLADE. DAMAGED. PERFORMED A BORESCOPE INSPECTION ON THE NR 2 ENGINE IAW PMC 6. FOUND 1ST STAGE HPT BLADE MISSING MATERIAL ON THE LEADING EDGE, MEASURING DIMENSION GREATER THAN 
- [SDR IPXA2018090533586](https://openairdocs.org/sdr/IPXA2018090533586), Sep 4, 2018: PUMP. MALFUNCTIONED. ENGINE FUEL FEED SYSTEM L, FWD FUEL PUMP EICAS MSG SHOWS AND L FWD PUMP PRESS LIGHT IS ON WITH SWITCH ON. REPLACED L FWD FUEL PUMP GFI, RELAY REF FIM 28-22-00 F
- [SDR IPXA2018041628640](https://openairdocs.org/sdr/IPXA2018041628640), Apr 12, 2018: MODULE. FAULTED. AIR TURNBACK. AFTER TAKEOFF, THE RUDDER RATIO EICAS ILLUMINATED. FOUND THE RIGHT RUDDER RATIO CHANGER MODULE FAULTED. R & R THE MODULE IAW MM 27-09-00. OPS CHEC

All 161: https://openairdocs.org/aircraft/N323UP/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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