# N340UP: 2010 Boeing 767-34AF

- Status: Valid registration
- Airframe: [Boeing 767-34AF](https://openairdocs.org/model/boeing-767-34af) (registry code 1385212, 190 seats)
- Engine: [GE CF6-80C2B6F](https://openairdocs.org/engine/ge-cf6-80c2b6f) (registry code 30109)
- Data sheets: [TCDS E13NE](https://openairdocs.org/tcds/E13NE) (General Electric Company GE Aerospace) (OpenAirDocs)
- Serial number: 37860
- Year built: 2010
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: June 18, 2010
- Certificate issued: June 24, 2010
- Expires: August 31, 2027
- Mode S code: A3BF1E
- Registered owner: [Cc&Ei LLC](https://openairdocs.org/faa-owner/CC%26EI%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=340UP
- Page: https://openairdocs.org/aircraft/N340UP

From the FAA registry file of October 24, 2026. ADs below are matched by the registry's airframe and engine model codes. They may apply; each AD's applicability can narrow it by serial number, part number or installed equipment. This is not a compliance determination.

## ADs that may apply (OpenAirDocs): 34 in force

### Matched by airframe (Boeing 767-34AF)

None in force.

### Matched by engine (GE CF6-80C2B6F)

- [AD 2023-20-08](https://openairdocs.org/ad/2023-20-08): Engine (Turbine/Turboprop) · General Electric CF6-80C2B1F, CF6-80C2B2F, CF6-80C2B4F and 4 more. Effective Oct 19, 2023
- [AD 2021-26-22](https://openairdocs.org/ad/2021-26-22): Turbine Section · General Electric CF6-80A, CF6-80A1, CF6-80A2 and 21 more. Effective Mar 14, 2022
- [AD 2021-14-11](https://openairdocs.org/ad/2021-14-11): Turbine Section · General Electric CF6-80A, CF6-80A1, CF6-80A2 and 25 more. Effective Aug 27, 2021
- [AD 2021-03-02](https://openairdocs.org/ad/2021-03-02): Fuel Control/Turbine Engines · General Electric CF6-80C2A1, CF6-80C2A2, CF6-80C2A3 and 16 more. Effective Mar 31, 2021
- [AD 2020-22-02](https://openairdocs.org/ad/2020-22-02): Engine Fuel and Control · General Electric CF6-80C2A5F, CF6-80C2B1F, CF6-80C2B2F and 13 more. Effective Dec 3, 2020
- [AD 2016-08-10](https://openairdocs.org/ad/2016-08-10): Accessory heat shield · General Electric CF6-80C2A1, CF6-80C2A2, CF6-80C2A3 and 26 more. Effective Jun 1, 2016
- [AD 2014-21-01](https://openairdocs.org/ad/2014-21-01): Fuel manifold · General Electric CF6-80C2A1, CF6-80C2A2, CF6-80C2A3 and 26 more. Effective Nov 28, 2014
- [AD 2013-08-20](https://openairdocs.org/ad/2013-08-20): Fuel tube · General Electric CF6-80C2A1, CF6-80C2A2, CF6-80C2A3 and 14 more. Effective May 31, 2013
- [AD 2012-03-12](https://openairdocs.org/ad/2012-03-12): No. 3 bearing packing · General Electric CF6-80C2A1, CF6-80C2A2, CF6-80C2A3 and 21 more. Effective Apr 5, 2012
- [AD 2012-04-05](https://openairdocs.org/ad/2012-04-05): Electronic control unit (ECU) · General Electric CF6-80C2B1F, CF6-80C2B1F1, CF6-80C2B1F2 and 8 more. Effective Mar 30, 2012
- [AD 2009-21-07](https://openairdocs.org/ad/2009-21-07): Thrust and thrust control · General Electric CF6-80C2A1, CF6-80C2A2, CF6-80C2A3 and 21 more. Effective Dec 1, 2009
- [AD 2009-07-03](https://openairdocs.org/ad/2009-07-03): Eddy current inspection (ECI) · General Electric CF6-80C2A1, CF6-80C2A2, CF6-80C2A3 and 26 more. Effective Apr 30, 2009
- [AD 2009-04-10](https://openairdocs.org/ad/2009-04-10): Critical life-limited parts · General Electric CF6-80A, CF6-80A1, CF6-80A2 and 30 more. Effective Mar 30, 2009
- [AD 2008-21-11](https://openairdocs.org/ad/2008-21-11): Low-pressure turbine (LPT) cases · General Electric CF6-80C2A1, CF6-80C2A2, CF6-80C2A3 and 25 more. Effective Nov 28, 2008
- [AD 2007-11-20](https://openairdocs.org/ad/2007-11-20): Fuel shroud retaining rings · General Electric CF6-80C2A1, CF6-80C2A2, CF6-80C2A3 and 22 more. Effective Jul 10, 2007
- [AD 2007-05-14](https://openairdocs.org/ad/2007-05-14): Cast titanium weld- repaired forward engine mount platforms · General Electric CF6-80C2A1, CF6-80C2A2, CF6-80C2A3 and 16 more. Effective Apr 9, 2007
- [AD 2006-16-06](https://openairdocs.org/ad/2006-16-06): Certain stage 1 high- pressure turbine (HPT) rotor disks · General Electric CF6-80A, CF6-80A1, CF6-80A2 and 21 more. Effective Sep 5, 2006
- [AD 2005-17-05](https://openairdocs.org/ad/2005-17-05): High pressure compressor rotor (HPCR) · General Electric CF6-80C2A1, CF6-80C2A2, CF6-80C2A3 and 25 more. Effective Sep 27, 2005
- [AD 2004-22-07](https://openairdocs.org/ad/2004-22-07): Stage 2 nozzle guide vanes (HPT S2 NGVs) · General Electric CF6-80C2A1, CF6-80C2A2, CF6-80C2A3 and 16 more. Effective Dec 1, 2004
- [AD 2003-02-07](https://openairdocs.org/ad/2003-02-07): Low pressure turbine (LPT) shrouds · General Electric CF6-50A, CF6-50C, CF6-50C1 and 30 more. Effective Mar 3, 2003
- [AD 2002-25-08](https://openairdocs.org/ad/2002-25-08): High pressure compressor rotor · General Electric CF6-45A, CF6-45A2, CF6-50A and 40 more. Effective Jan 23, 2003
- [AD 2002-22-12](https://openairdocs.org/ad/2002-22-12): Titeflex hoses · BAE Systems ATP, Avro 146-RJ100A, Avro 146-RJ70A and 122 more. Effective Dec 13, 2002
- [AD 2000-03-04](https://openairdocs.org/ad/2000-03-04): General Electric CF6-80C2A1, CF6-80C2A2, CF6-80C2A3 and 19 more. Effective Apr 10, 2000
- [AD 99-01-01](https://openairdocs.org/ad/99-01-01): Accessory Gearbox (AGB) idler adapters · General Electric CF6-80C2A1, CF6-80C2A2, CF6-80C2A3 and 19 more. Effective Jan 21, 1999
- [AD 98-22-06](https://openairdocs.org/ad/98-22-06): Fan Disks · General Electric CF6-45A, CF6-45A2, CF6-50A and 41 more. Effective Nov 23, 1998
- [AD 97-22-14](https://openairdocs.org/ad/97-22-14): (HPCR) 3-9 Spool · General Electric CF6-50A, CF6-50C, CF6-50C1 and 29 more. Effective Nov 17, 1997
- [AD 96-16-07](https://openairdocs.org/ad/96-16-07): Rear Right Hand Mount Link · General Electric CF6-80C2A1, CF6-80C2A2, CF6-80C2A3 and 17 more. Effective Aug 28, 1996
- [AD 95-10-11](https://openairdocs.org/ad/95-10-11): Fan Reversers · General Electric CF6-80C2A1, CF6-80C2A2, CF6-80C2A3 and 17 more. Effective May 31, 1995
- [AD 94-20-06](https://openairdocs.org/ad/94-20-06): Oil System · General Electric CF6-80C2A1, CF6-80C2A2, CF6-80C2A3 and 16 more. Effective Dec 27, 1994
- [AD 94-06-03](https://openairdocs.org/ad/94-06-03): High Pressure Turbine Disk · General Electric CF6-80C2A1, CF6-80C2A2, CF6-80C2A3 and 16 more. Effective Apr 29, 1994
- [AD 93-14-18](https://openairdocs.org/ad/93-14-18): High pressure turbine (HPT) thermal shields · General Electric CF6-45A, CF6-45A2, CF6-50A and 40 more. Effective Oct 4, 1993
- [AD 91-15-25](https://openairdocs.org/ad/91-15-25): High Pressure Compressor Rotor · General Electric CF6-80A, CF6-80A1, CF6-80A2 and 16 more. Effective Sep 6, 1991
- [AD 91-11-05](https://openairdocs.org/ad/91-11-05): High Pressure Compressor Rotor · General Electric CF6-80A, CF6-80A1, CF6-80A2 and 16 more. Effective Jul 5, 1991
- [AD 91-05-21](https://openairdocs.org/ad/91-05-21): High Pressure Turbine · General Electric CF6-80C2A5, CF6-80C2B6, CF6-80C2B6F and 1 more. Effective Mar 27, 1991

### Historical (superseded or no longer in force)

- [AD 2020-20-13](https://openairdocs.org/ad/2020-20-13) (historical): Turbine Section · General Electric CF6-80A, CF6-80A1, CF6-80A2 and 21 more. Effective Nov 12, 2020
- [AD 2018-15-04](https://openairdocs.org/ad/2018-15-04) (historical): Turbine/Turboprop Engine--Turbine Section · General Electric CF6-80A, CF6-80A1, CF6-80A2 and 21 more. Effective Oct 2, 2018
- [AD 2009-05-02](https://openairdocs.org/ad/2009-05-02) (historical): Drainless fuel manifold assemblies · General Electric CF6-80C2A1, CF6-80C2A2, CF6-80C2A3 and 26 more. Effective Mar 31, 2009
- [AD 2007-12-07](https://openairdocs.org/ad/2007-12-07) (historical): Electronic control units (ECUs) · General Electric CF6-80C2B1F, CF6-80C2B2F, CF6-80C2B4F and 5 more. Effective Jul 11, 2007
- [AD 2004-04-07](https://openairdocs.org/ad/2004-04-07) (historical): Stage 1 HPT rotor disks · General Electric CF6-80A, CF6-80A1, CF6-80A2 and 21 more. Effective Mar 12, 2004
- [AD 2002-07-12](https://openairdocs.org/ad/2002-07-12) (historical): Life Limits Section of Continued Airworthiness (ICA) - Selected Critical Life-limited Parts · General Electric CF6-80A, CF6-80A1, CF6-80A2 and 27 more. Effective May 15, 2002
- [AD 2001-10-07](https://openairdocs.org/ad/2001-10-07) (historical): High Pressure Turbine Rotor Disks · General Electric CF6-80C2A1, CF6-80C2A2, CF6-80C2A3 and 19 more. Effective Jun 18, 2001
- [AD 2000-16-12](https://openairdocs.org/ad/2000-16-12) (historical): High Pressure Compressor Rotor Stage 3-9 Spools · General Electric CF6-45A, CF6-45A2, CF6-50A and 39 more. Effective Sep 5, 2000
- [AD 2000-04-14](https://openairdocs.org/ad/2000-04-14) (historical): Fuel tube flange seating · General Electric CF6-80C2A1, CF6-80C2A2, CF6-80C2A3 and 12 more. Effective May 1, 2000
- [AD 99-24-15](https://openairdocs.org/ad/99-24-15) (historical): High Pressure Compressor Rotor (HPCR) Stage 3-9 Spools · General Electric CF6-45A, CF6-45A2, CF6-50A and 39 more. Effective Jan 28, 2000
- [AD 99-08-13](https://openairdocs.org/ad/99-08-13) (historical): General Electric CF6-80A, CF6-80A1, CF6-80A2 and 26 more. Effective May 13, 1999
- [AD 91-20-02](https://openairdocs.org/ad/91-20-02) (historical): Fuel Manifolds · General Electric CF6-80C2A1, CF6-80C2A2, CF6-80C2A3 and 12 more. Effective Nov 25, 1991
- [AD 90-26-01](https://openairdocs.org/ad/90-26-01) (historical): Fuel Manifold Systems · General Electric CF6-80C2A1, CF6-80C2A2, CF6-80C2A3 and 11 more. Effective Dec 20, 1990

## Information bulletins (advisory) (4 in force)

- [SAIB 2023-15](https://openairdocs.org/saib/2023-15): Falsified Forms from AOG Technics. Issued Dec 19, 2023
- [SAIB NE-10-37](https://openairdocs.org/saib/NE-10-37): Engine Fuel and Control: FADEC Fuel Metering Valve Resolver Feedback Faults. Issued Jul 12, 2010
- [SAIB NE-08-44](https://openairdocs.org/saib/NE-08-44): Engine Thrust Reverser  Transcowl Clevis Pin. Issued Sep 3, 2008
- [SAIB NE-07-01](https://openairdocs.org/saib/NE-07-01): Dual engine flameouts on twin engine airplanes. Issued Oct 12, 2006

## NTSB investigations

None matched to N340UP.

## FAA accident and incident reports

None matched to N340UP.

## Service difficulty reports (61, 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 IPXA2026090361862](https://openairdocs.org/sdr/IPXA2026090361862), Sep 3, 2026: LAMP. INOPERATIVE. L1271 EMERGENCY CEILING LT INOPERATIVE. REPLACED THE LAMP AND LIGHT TEST OK, IAW AMM 33-51-11/201.
- [SDR IPXA2026040275634](https://openairdocs.org/sdr/IPXA2026040275634), Apr 1, 2026: JUMPER. DAMAGED. FOUND FORWARD CARGO DOOR JUMPER DAMAGED AT FWD & AFT SIDE (REPLACE). .I.A.W AMM 52-33-01-004-060 REV.147 AND AMM 52-33-01-404-061 REV.147 REPLACED FWD CARGO DOO
- [SDR IPXA2026032822628](https://openairdocs.org/sdr/IPXA2026032822628), Mar 23, 2026: FILLER. BROKEN. BROKEN FILLER, RT HORIZONTAL STAB TIP AFT OTBD CORNER. INSTALLED A NEW FILLER IAW SRM 51-40-02-0G, REV 94, AND DWG 189T0001, SHT 1, REV E.
- [SDR IPXA2026032822558](https://openairdocs.org/sdr/IPXA2026032822558), Mar 23, 2026: FILLER. DAMAGED. LIGHTNING STRIKE, FILLER, LT HORIZONTAL STAB TIP AFT OTBD CORNER. INSTALLED A NEW FILLER IAW SRM 51-40-02-0G, REV 94, AND DWG 189T0001, SHT 1, REV E.
- [SDR IPXA2026032609725](https://openairdocs.org/sdr/IPXA2026032609725), Mar 22, 2026: BUSHING. MISSING. FAULT- MISSING- BUSHING, NO.1 ENG L/H FAN COWL NO.2 LATCH AREA. (REPLACE). INSTALL NEW RECEIVER I.A.W SRM 51-40-02-0G REV.94 AND GOODRICH AEROSTRUCTURES CMM IPL
- [SDR IPXA2026040110702](https://openairdocs.org/sdr/IPXA2026040110702), Mar 22, 2026: FITTING. CRACKED. FOUND THE MAIN DECK CARGO RESTRAINT FLOOR ADAPTER FITTING WITH CRACK DAMAGE AT BS 632, BL 0, FLOOR PANEL. JOB COMPLETED AND CONDITION CHECK NORMAL. REPLACED FLO
- [SDR IPXA2026032712143](https://openairdocs.org/sdr/IPXA2026032712143), Mar 22, 2026: BLOWOUT DOOR. CHAFED. CHAFED SKIN, NR 1 ENGINE, RT THRUST REVERSER BLOWOUT DOOR INNER L/E AREA. INSTALLED A NEW BLOWOUT DOOR IAW SRM 51-40-02-0G, REV 94, AIPC 78-31-51-03, REV 141, &
- [SDR IPXA2026033112189](https://openairdocs.org/sdr/IPXA2026033112189), Mar 22, 2026: ANGLE. CRACKED. CRACKED ANGLE, LT WING LE REFUELING STATION LOWER DOOR CUTOUT INBD STOP SPRING, ACCESS PANEL 521QB. INSTALLED A NEW ANGLE IAW SRM 51-40-02-0G, REV 94, & DWG 114
- [SDR IPXA2026033112225](https://openairdocs.org/sdr/IPXA2026033112225), Mar 22, 2026: CLAMP. BROKEN. BROKEN CLAMP, NR 1 PYLON AFT FAIRING INNER HOLD OPEN ROD SUPPORT BRACKET AREA. INSTALLED NEW BRACKET I.A.W SRM 51-40-02-0G REV. 95. AND BOEING DWG NO.313T3349 S
- [SDR IPXA2026032810500](https://openairdocs.org/sdr/IPXA2026032810500), Mar 22, 2026: BRACKET. CHAFED. CHAFED BRACKET, NR 1 ENGINE LT CORE COWL INNER HOLD OPEN ROD SUPPORT BRACKET. INSTALLED A NEW BRACKET IAW SRM 51-40-02-0G, REV 94, AND CMM IPL 71-13-23, REV 47.
- [SDR IPXA2026032612126](https://openairdocs.org/sdr/IPXA2026032612126), Mar 22, 2026: BLOWOUT DOOR. CHAFED. CHAFED SKIN, NR 2 ENGINE, RT THRUST REVERSER LWR BLOWOUT DOOR, L/E AREA. INSTALLED A NEW BLOWOUT DOOR ASSY IAW SRM 51-40-02-0G, REV 94, AND AIPC 78-31-51-03, RE
- [SDR IPXA2026032711985](https://openairdocs.org/sdr/IPXA2026032711985), Mar 22, 2026: BRACKET. CHAFED. CHAFED BRACKET, NR 2 ENG LT THRUST REVERSER LOWER CLOSURE DOOR T/E AREA. INSTALLED A NEW BRACKET IAW SRM 51-40-02-0G, REV 94, AND IPC 78-32-21, REV.94.
- [SDR IPXA2026032612437](https://openairdocs.org/sdr/IPXA2026032612437), Mar 22, 2026: HOUSING. STUCK. STUCK - HOUSING ASSY, FWD CARGO DOOR CUTOUT AFT SIDE (REPLACE). I.A.W AMM 20-11-00-910-802 REV.147 REPLACE FWD CARGO DOOR HOUSING ASSY AT AFT SIDE CUTOUT AREA. 
- [SDR IPXA2026032610644](https://openairdocs.org/sdr/IPXA2026032610644), Mar 22, 2026: BRACKET. CHAFED. CHAFED BRACKET, NR 2 ENGINE, LT CORE COWL HOLD OPEN ROD SUPPORT BRACKET. INSTALLED A NEW ADAPTER IAW SRM 51-40-02-0G, REV 94, & CMM IPL 71-13-23, REV 47.
- [SDR IPXA2026032610631](https://openairdocs.org/sdr/IPXA2026032610631), Mar 22, 2026: BRACKET. CHAFED. CHAFED BRACKET, NR 1 ENG, LT THRUST REVERSER FWD LWR CLOSURE DOOR T/E AREA. NSTALLED A NEW BRACKET IAW SRM 51-40-02-0G, REV 94, & IPC 78-32-21 REV 94.
- [SDR IPXA2026032610990](https://openairdocs.org/sdr/IPXA2026032610990), Mar 22, 2026: CLAMP. DAMAGED. DAMAGED CLAMP, NR.2 PYLON AFT FAIRING DOOR SUPPORT ROD. INSTALLED A NEW CLAMP IAW SRM 51-40-02-0G, REV 94, AND DWG 313T2303, SH 135, REV -.
- [SDR IPXA2026032612020](https://openairdocs.org/sdr/IPXA2026032612020), Mar 22, 2026: BRACKET. CHAFED. CHAFED BRACKET, NR 2 ENG, RT THRUST REVERSER LOWER CLOSURE DOOR T/E AREA. INSTALLED A NEW BRACKET IAW SRM 51-40-02-0G, REV 94, AND IPC 78-32-22 REV 94.
- [SDR IPXA2026032611804](https://openairdocs.org/sdr/IPXA2026032611804), Mar 22, 2026: PLATE. CRACKED. CRACKED PLATE, NR 1 ENG LT CORE COWL INNER AFT LWR SIDE. INSTALLED A NEW PLATE IAW SRM 51-40-02-0G, REV 94, AND CMM IPL 71-13-23, REV 47.
- [SDR IPXA2026032612053](https://openairdocs.org/sdr/IPXA2026032612053), Mar 22, 2026: BRACKET. CHAFED. CHAFED BRACKET, NR 1 ENG, RT THRUST REVERSER FWD LOWER CLOSURE DOOR T/E AREA. INSTALLED A NEW BRACKET IAW SRM 51-40-02-0G, REV 94, & IPC 78-32-22 REV.94.
- [SDR IPXA2026032612072](https://openairdocs.org/sdr/IPXA2026032612072), Mar 22, 2026: BRACKET. CRACKED. CRACKED BRACKET, LT WING INBD L/E NR 6 SLAT DRIVE TORQUE TUBE SUPPORT, LES 285. INSTALL NEW BRACKET I.A.W SRM 51-40-02-0G REV.95 AND BOEING DWG NO: 114T1240 SH 
- [SDR IPXA2026032612305](https://openairdocs.org/sdr/IPXA2026032612305), Mar 22, 2026: ANGLE. CRACKED. CRACKED ANGLE, NR 1 PYLON AFT FAIRING INNER AFT BULKHEAD INBD SIDE SUPPORT ANGLE. INSTALLED A NEW ANGLE IAW SRM 51-40-02-0G, REV 94, DWG 313T2303, SHEET 131, RE
- [SDR IPXA2026040197859](https://openairdocs.org/sdr/IPXA2026040197859), Mar 21, 2026: DUCT. CHAFED. CHAFED DUCT, NR 2 ENG R/H CORE COWL PRECOOLER OULET DUCT (REPLACE). INSTALL PRECOOLER DUCT FOR ACCESS I.A.W SRM 51-40-02-0G REV.94 AND GOODRICH AEROSTRUCTURES C
- [SDR IPXA2026033100868](https://openairdocs.org/sdr/IPXA2026033100868), Mar 21, 2026: SKIN PANEL. CORRODED. LOWER FUSELAGE EXTERNAL SURFACE SKIN CORRODED NEAR DRAIN HOLE AREA AT BS 1395 - 1417, S38R - 39R. ACCOMPLISHED THE REPAIR I.A.W EGAT EI NO. F2026A53M-588 SEQUEN
- [SDR IPXA2026032072891](https://openairdocs.org/sdr/IPXA2026032072891), Mar 20, 2026: SKIN. DENTED. DENT - SKIN, LOWER FACE OF L/H WING T/E OUTBD FLAP INNER SKIN, NEAR OTEF STA 137 (REPAIR). REPAIR DENT ON LOWER SURFACE OF LWR PANEL ON LH WING OUTBD T/E FLAP N
- [SDR IPXA2026040178486](https://openairdocs.org/sdr/IPXA2026040178486), Mar 20, 2026: FITTING. CRACKED. FOUND THE MAIN DECK CARGO RESTRAINT FLOOR ADAPTER FITTING WITH CRACK DAMAGE AT STA 1241 LBL 47.5, FLOOR PANEL NO. 251NFF (REPLACE). REPLACE FLOOR ADAPTER FITTIN
- [SDR IPXA2026040178532](https://openairdocs.org/sdr/IPXA2026040178532), Mar 20, 2026: FITTING. CRACKED. FOUND THE MAIN DECK CARGO RESTRAINT FLOOR ADAPTER FITTING WITH CRACK DAMAGE AT BS 1373, RBL 47.5, FLOOR PANEL 252QFF. INSTALLED FLOOR PANEL 252QFF IAW AMM 53-01
- [SDR IPXA2026033175660](https://openairdocs.org/sdr/IPXA2026033175660), Mar 20, 2026: PLATE. CHAFED. CHAFED PLATE, FWD EDGE LOWER FACE OF LT WING INBD L/E LOWER PLATE, ISS 250.625 - ISS 256.145. INSTALLED NEW SKIN PLATE IAW SRM 51-40-02-0G, REV 94, DWG 114T1000
- [SDR IPXA2026040178536](https://openairdocs.org/sdr/IPXA2026040178536), Mar 20, 2026: FITTING. CRACKED. FOUND THE MAIN DECK CARGO RESTRAINT FLOOR ADAPTER FITTING WITH CRACK DAMAGE AT BS 676, RBL 47.5, FLOOR PANEL 232LFF. INSTALLED FLOOR PANEL 232LFF IAW AMM 53-01-
- [SDR IPXA2026040178528](https://openairdocs.org/sdr/IPXA2026040178528), Mar 20, 2026: FITTING. CRACKED. FOUND THE MAIN DECK CARGO RESTRAINT FLOOR ADAPTER FITTING WITH CRACK DAMAGE AT BS 654+44 BL 0, FLOOR PANEL 231LFF. REPLACE FLOOR ADAPTER FITTING I.A.W AMM 20-11
- [SDR IPXA2026040178544](https://openairdocs.org/sdr/IPXA2026040178544), Mar 20, 2026: FITTING. CRACKED. FOUND THE MAIN DECK CARGO RESTRAINT FLOOR ADAPTER FITTING WITH CRACK DAMAGE AT STA 1241 BL 0, FLOOR PANEL NO. 251LFF (REPLACE). REPLACE FLOOR ADAPTER FITTING IA
- [SDR IPXA2026032278838](https://openairdocs.org/sdr/IPXA2026032278838), Mar 20, 2026: FLOOR PANEL. CRACKED. CRACKS ON THE FLOOR PANEL NO. 252UFF, AT BS 1400 - 1520, RBL 55 - 77 IN THE MAIN DECK CARGO COMPARTMENT. INSTALL THE REPLACEMENT FLOOR PANEL IAW AMM 53-01-06. C
- [SDR IPXA2026033156373](https://openairdocs.org/sdr/IPXA2026033156373), Mar 19, 2026: RETAINER. DAMAGED. FOUND NUTPLATE DAMAGED 1EA, PNL NO.611JB. FABRICATE RETAINER IAW DWG 114T1400, SH 3, REV F, PL REV BW, PSDL REV F AS A SAMPLE IAW GMM-MTX CH 9.08 REV 14.1 REQUI
- [SDR IPXA2026033032521](https://openairdocs.org/sdr/IPXA2026033032521), Mar 18, 2026: ACTUATOR. FAULTED. FOUND ROTARY ACTUATOR NOISE AT FWD CARGO DOOR. IAW AMM 52-33-04-004-027 REV.147 AND AMM 52-33-04-404-028 REV.147 REPLACED FWD CARGO DOOR ROTARY ACTUATOR.
- [SDR IPXA2026033132792](https://openairdocs.org/sdr/IPXA2026033132792), Jan 29, 2026: SUPPORT ANGLE. GOUGED. UNLOAD CREW REPORTED DAMAGE TO LOWER FWD CARGO DOOR FRAME UPPER AFT CORNER. REMOVED DAMAGE SUPPORT ANGLE I.A.W SRM 51-40-02-0G REV.94. INSTALL NEW SUPPORT ANGLE
- [SDR IPXA2024032590713](https://openairdocs.org/sdr/IPXA2024032590713), Mar 15, 2024: CYLINDER. CORRODED. *SDR FILED OPEN* FAULT - FOUND LEFT MAIN GEAR GLAND NUT AND OUTER CYLINDER THREAD CORROSION. (EVALUATE) ACCOMPLISHED EO 89873 REQUEST DMI TO REPLACE LMLG WITHIN
- [SDR IPXA2024032683572](https://openairdocs.org/sdr/IPXA2024032683572), Mar 10, 2024: NONE. NONE. FUSELAGE DRAIN HOLES INSPECTION AND INSTALLATION AFT OF BS 1725.5 BETWEEN S-36L AND S-36R) CONDITION CHECK OK.
- [SDR IPXA2024031083572](https://openairdocs.org/sdr/IPXA2024031083572), Mar 10, 2024: NONE. NONE. OPEN, FUSELAGE DRAIN HOLES INSPECTION AND INSTALLATION AFT OF BS 1725.5 BETWEEN S-36L AND S-36R) COMPLETED SDR.
- [SDR IPXA2024032673650](https://openairdocs.org/sdr/IPXA2024032673650), Mar 9, 2024: SEAL. WORN. FOUND ENTRY DOOR AFT SIDE DOORWAY SEAL WORN (REPLACE) REVIEW COMPLETE
- [SDR IPXA2024031173650](https://openairdocs.org/sdr/IPXA2024031173650), Mar 9, 2024: SEAL. WORN. OPEN, FOUND ENTRY DOOR AFT SIDE DOORWAY SEAL WORN (REPLACE) OK TO WORK
- [SDR IPXA2024030479506](https://openairdocs.org/sdr/IPXA2024030479506), Mar 4, 2024: BATTERY. FAILED. EMER LIGHT SYS TEST FAILED. REMOVED AND REPLACED EMER BATT PER AMM 33-51-07/401. OPS CHECK GOOD.
- [SDR IPXA2022042281381](https://openairdocs.org/sdr/IPXA2022042281381), Apr 17, 2022: STIFFENER. CRACKED. INSPECTION TYPE:C6CRACK ON CENTER WING TANK STIFFENER (P/N : 111T2008-12) ON STA 785.9 , RBL 33REPAIR IA.W 767-300F SRM 57-10-10-2R-2 REPAIR 2 REV.83.00 , UPS E
- [SDR IPXA2022042281380](https://openairdocs.org/sdr/IPXA2022042281380), Apr 17, 2022: STIFFENER. CRACKED. INSPECTION TYPE:C6CRACK ON CENTER WING TANK STIFFENER (P/N : 111T2011-6) ON STA 785.9 , RBL 55REPAIR I.A.W 767-300F SRM 57-10-10-2R-2 REPAIR 2 REV.83.00 , UPS E
- [SDR IPXA2019071044303](https://openairdocs.org/sdr/IPXA2019071044303), Jul 10, 2019: FUEL CAP. MISSING. INSPECTION TYPE:INSP DUE TO WAN 2937896 AND DMI M676316 FUELING RECEPTACLE CAP. FUEL CAP ASSY INSTALLED IAW AMM 28-21-01-401 REV 127.04. THIS CLOSES DMI M676316
- [SDR IPXA2019040440760](https://openairdocs.org/sdr/IPXA2019040440760), Apr 3, 2019: STRUCTURE. PUNCTURED. R. ENGINE COWL EXTERIOR HAS LG PUNCTURE HOLE WITH FIBERGLASS PROTRUDING FROM ENTRY HOLE. NOTICED ON PREFLIGHT WALK AROUND DAMAGE IS PROB. 4-6 INCHES LONG. 3 INC
- [SDR IPXA2018110523567](https://openairdocs.org/sdr/IPXA2018110523567), Nov 1, 2018: ARMING LEVER. DAMAGED. DOOR ARMING LEVER HINGED DOOR MECHANISM WAS DAMAGED. R & R THE FWD ENTRY DOOR HINGE ASSY IAW AMM 52-12-02, PB 401, REV 124.05. OPS NORMAL.
- [SDR IPXA2018091734075](https://openairdocs.org/sdr/IPXA2018091734075), Sep 14, 2018: COVER. UNSECURE. CREW ENTRY DOOR ARMING COVER WILL NOT STOW. REMOVED COVER. REMOVED AND REPLACED FORWARD L1 DOOR HINGE AND HANDLE. OPS NORMAL IAW MM 52-12-02. OK FOR SERVICE.
- [SDR IPXA2017112623900](https://openairdocs.org/sdr/IPXA2017112623900), Nov 26, 2017: FLOOR PANEL. PUNCTURED. MCD FLOOR PANEL AT POS 10, WL 200, BL 0 FWD , CTR HAS TWO HOLES IN PANEL. FABRICATED A NEW FLOOR PANEL IAW EO B767-5320-9693-I
- [SDR IPXA2017030114550](https://openairdocs.org/sdr/IPXA2017030114550), Feb 28, 2017: SKIN. DAMAGED. FUSELAGE SKIN DAMAGED AT BS 132.5 BETWEEN STRINGERS 24 - 30R. DAMAGE MEASURES 12 INCHES CIRCUMFERENTIAL BY 2.25 INCHES FORE & AFT AND 1.5 INCHES OUTWARD DEFLECC
- [SDR IPXA2017022214316](https://openairdocs.org/sdr/IPXA2017022214316), Feb 19, 2017: LAMP. INOPERATIVE. EXTERIOR EMERGENCY LIGHT FAILED ON TEST. REMOVED AND REPLACED THE LAMP, AND TESTED IAW AMM 33-51-16-201, REV 120.02. TESTED OK.
- [SDR IPXA2017013013469](https://openairdocs.org/sdr/IPXA2017013013469), Jan 29, 2017: SEAL. LEAKING. L1 DOOR SEAL DEVELOPED A LEAK STARTING AT FL 200. LEAK CONTINUED ENTIRE FLIGHT. FOUND LOWER DOOR SEAL PULLED OUT OF RETAINER. REINSTALLED L1 DOOR SEAL IAW MM 52

All 61: https://openairdocs.org/aircraft/N340UP/reports.md

## STCs that may be installed (OpenAirDocs) (5)

Approved for this aircraft's airframe or engine model, in force first, then newest. The registry doesn't record which STCs an aircraft has; its records do.

### Approved for the engine (GE CF6-80C2B6F)

- [STC SE01543CH](https://openairdocs.org/stc/SE01543CH): Replace Hamilton Sundstrand P/N 778839-13, 778839-14, 778839-19, 778839-20, 778839-37, 778839-38, 816682-1, 840618-2, 880724 carbon bushings with Cook Airtomic P/N AIR22947 Slotted Entry Busing in the High Pressure Shutoff Valve. Cook Airtomic
- [STC SE01478CH](https://openairdocs.org/stc/SE01478CH): Installation of Cook Airtomic alignment joint p/n AIR 22912. Cook Airtomic
- [STC SE01471AT](https://openairdocs.org/stc/SE01471AT): Replace right and left side Rohr, Inc. fire detection harness on GE CF6-80C2 engine. Unison Industries. Lists CF6-80C2 Series
- [STC SE00463LA](https://openairdocs.org/stc/SE00463LA): Install fireproof blankets on the engine fan reverser intermediate fireseal, in lieu of fireproof intumescent coating. This STC is jointly by owned by Hi Temp Insulation and MRA Systems acting through Middle River Aircraft Systems, 103 Chesapeake Park Plaza, Baltimore, MD 21220. Hi Temp Insulation Inc
- [STC SA2227SO](https://openairdocs.org/stc/SA2227SO): Installation of wiring and associated components for utilization of the Rolls Royce, Inc., ARINC, interface/readers UT1317 or UT1317/1, for the purpose of acquisition, recording, and analysis in real time of engine/aircraft/ systems. (767 SERIES POWERED BY RR RB-11-524 SERIES. Rolls Royce, Inc. Lists CF6-80 Series

## Related

- Other Boeing 767-34AF aircraft: https://openairdocs.org/model/boeing-767-34af/aircraft.md
- The GE CF6-80C2B6F engine: https://openairdocs.org/engine/ge-cf6-80c2b6f.md

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