# N341UP: 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: 37861
- Year built: 2010
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: July 15, 2010
- Certificate issued: July 15, 2010
- Expires: November 30, 2027
- Mode S code: A3C2D5
- 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=341UP
- Page: https://openairdocs.org/aircraft/N341UP

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 (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 DCA16WA150](https://openairdocs.org/ntsb/DCA16WA150), May 6, 2016: Boeing 767 (N341UP), Cologne, Germany, incident, no damage

## FAA accident and incident reports

None matched to N341UP.

## Service difficulty reports (91, 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 IPXA2026060273867](https://openairdocs.org/sdr/IPXA2026060273867), May 27, 2026: SEAL DEPRESSOR. DEFORMED. FOUND MAIN DECK SIDE CARGO DOOR UPPER - AFT SIDE DEPRESSOR SEAL DEFORM AND SCRATCH. INSTALLED THE DEPRESSOR SEAL. IAW AMM I.A.W AMM 20-11-00-910-802 REV.148.TOR
- [SDR IPXA2026060256189](https://openairdocs.org/sdr/IPXA2026060256189), May 26, 2026: STIFFENER. CRACKED. CRACKED BRACKET, NR .2 ENG LT T/R FWD TORQUE BOX SUPPORT FITTING NEAR 9:30 AND 10:00 POS. REMOVED DAMAGE BRACKET I.A.W SRM 51-40-02-0G REV. 95. INSTALLED NEW BR
- [SDR IPXA2026060257012](https://openairdocs.org/sdr/IPXA2026060257012), May 26, 2026: FORMER. CRACKED. RIGHT WING OTBD L/E, NOSE FORMER CRACK, OSS 499.60. REMOVED DAMAGE FORMER IAW SRM 51-40-02-0G REV.95. INSTALL NEW FORMER I.A.W SRM 51-40-02-0G REV.95 AND DWG 11
- [SDR IPXA2026053056047](https://openairdocs.org/sdr/IPXA2026053056047), May 26, 2026: ATTACH BRACKET. CRACKED. CRACK - BRACKET, L/H WING INBOARD L/E COMPARTMENT. (REPLACE) INSTALLED NEW BRACKET I.A.W SRM 51-40-02-0G REV. 95 AND BOEING DWG NO. 114T1240 SH. 6 REV. -.
- [SDR IPXA2026053056997](https://openairdocs.org/sdr/IPXA2026053056997), May 26, 2026: ATTACH BRACKET. CRACKED. RIGHT WING INBOARD L/E CAVITY, PANEL RIB ATTACH BRACKET CRACK, ISS 285. (REPLACE) INSTALLED NEW BRACKET I.A.W SRM 51-40-02-0G REV. 95 AND BOEING DWG NO. 114T124
- [SDR IPXA2026060158500](https://openairdocs.org/sdr/IPXA2026060158500), May 26, 2026: SKIN. CRACKED. RIGHT WING OUTBOARD FLAP, INBOARD T/E END CAP SKIN, UPPER AND LOWER FOUND SKIN DAMAGE. I.A.W UPS SREO-70175-REQ001 REV. 1 PERFORM REPAIR .
- [SDR IPXA2026052956860](https://openairdocs.org/sdr/IPXA2026052956860), May 26, 2026: SUPPORT ANGLE. CRACKED. CRACKED ANGLE , NR 2 PYLON AFT FAIRING INNER AFT FRAME OTBD SIDE SUPPORT ANGLE.
- [SDR IPXA2026052957094](https://openairdocs.org/sdr/IPXA2026052957094), May 26, 2026: ANGLE. CRACKED. CRACKED ANGLE, NR 1 PYLON AFT FAIRING AFT INNER CAVITY INBD ANGLE CRACK. INSTALL NEW CLIP I.A.W SRM 51-40-02-0G REV.95 AND BOEING DWG NO:313T2303 SH 131 REV.- A
- [SDR IPXA2026052946995](https://openairdocs.org/sdr/IPXA2026052946995), May 25, 2026: ANGLE. CRACKED. THE BULK CARGO INBOARD ANGLE AT STA 1578 RBL 80 IS CRACKED. INSTALLED NEW ANGLE I.A.W SRM 51-40-02-0G REV. 95 AND BOEING DWG NO. 146T5650 SH. 5 REV. C
- [SDR IPXA2026052947168](https://openairdocs.org/sdr/IPXA2026052947168), May 25, 2026: ANGLE. UNKNOWN. THE BULK CARGO OUTBOARD ANGLE AT STA 1578 LBL 80 IS CRACKED. CONDITION CHECK NORMAL. INSTALLED NEW ANGLE I.A.W SRM 51-40-02-0G REV. 95 AND BOEING DWG NO. 146T56
- [SDR IPXA2026052947183](https://openairdocs.org/sdr/IPXA2026052947183), May 25, 2026: ANGLE. UNKNOWN. THE BULK CARGO INBOARD ANGLE AT BS 1578 LBL 80 IS CRACKED. CONDITION CHECK NORMAL. INSTALLED NEW ANGLE I.A.W SRM 51-40-02-0G REV. 95 AND BOEING DWG NO. 146T5650
- [SDR IPXA2026060536086](https://openairdocs.org/sdr/IPXA2026060536086), May 24, 2026: ANGLE. CRACKED. FOUND THE FIRE DETECTION LOOP FASTENER ANGLE CRACK AT STA 1562 LBL 76 IN BULK CARGO COMPARTMENT. INSTALLED FABRICATED ANGLE I.A.W SRM 51-40-02-0G REV. 95 AND BO
- [SDR IPXA2026052424821](https://openairdocs.org/sdr/IPXA2026052424821), May 23, 2026: STIFFENER. CRACKED. CRACKED STIFFENER, FLOOR SUPPORT STRUCTURE STA 785.9 RBL 11. ACCOMPLISH THE REPAIR I.A.W SRM 57-10-10-2R-2 REV. 95 AND EGAT WORK SHEET NO: 60431 AND EO-58151-RE
- [SDR IPXA2026052425094](https://openairdocs.org/sdr/IPXA2026052425094), May 23, 2026: STIFFENER. CRACKED. CRACKED STIFFENER, FLOOR SUPPORT STRUCTURE STA 785.9 LBL 55. ACCOMPLISH THE REPAIR I.A.W SRM 57-10-10-2R-2 REV. 95 AND EGAT WORK SHEET NO: 60432 AND EO-58151-RE
- [SDR IPXA2026052425098](https://openairdocs.org/sdr/IPXA2026052425098), May 23, 2026: STIFFENER. CRACKED. CRACKED STIFFENER, FLOOR SUPPORT STRUCTURE STA 785.9 RBL 55. ACCOMPLISH THE REPAIR I.A.W SRM 57-10-10-2R-2 REV. 95 AND EGAT WORK SHEET NO: 60430 AND EO-58151-RE
- [SDR IPXA2026052841073](https://openairdocs.org/sdr/IPXA2026052841073), May 12, 2026: FLOOR PANEL. DAMAGED. LOADER REPORT LOWER AFT CARGO R/H SIDE NEAR DOORWAY FLOOR PANEL EDGE DAMAGE 1. I.A.W. 767-300F SRM 53-00-50-2R-0 REV. 95 PERFORM REPAIR AS BELOW STEP. :CUT OUT 
- [SDR IPXA2024062474860](https://openairdocs.org/sdr/IPXA2024062474860), Jun 22, 2024: HOUSING. MISSING. INTERIOR EMG LT. COVER PLATE MISSING LIGHT HOUSING, FWD MAIN ENT DOOR. R/R EMG. EXIT SIGN IAW AMM 33-51-01-022 AND -402. OPS CKS GOOD.
- [SDR IPXA2024052960336](https://openairdocs.org/sdr/IPXA2024052960336), May 26, 2024: ANGLE. CRACKED. CRACK - ANGLE BULK CARGO COMPARTMENT LEFT AREA STA 1578 LBL 60. I.A.W AMM 25-57-05-404-006 AND AMM 25-58-04-404-015 REV.142 RESTORED MAIN DECK CARGO HANDLING. J
- [SDR IPXA2024052960326](https://openairdocs.org/sdr/IPXA2024052960326), May 26, 2024: ANGLE. CRACKED. CRACK - ANGLE BULK CARGO COMPARTMENT RIGHT AREA STA 1578 RBL 60. I.A.W AMM 25-57-05-404-006 AND AMM 25-58-04-404-015 REV 142 RESTORED MAIN DECK CARGO HANDLING. 
- [SDR IPXA2024052552655](https://openairdocs.org/sdr/IPXA2024052552655), May 25, 2024: NONE. NONE. FUSELAGE DRAIN HOLES INSPECTION AND INSTALLATION AFT OF BS 1725.5 BETWEEN S-36L AND S-36R.
- [SDR IPXA2024020712214](https://openairdocs.org/sdr/IPXA2024020712214), Oct 28, 2023: SKIN. DAMAGED. NR 6 SLAT DAMAGED- BROKEN SKIN SLAT CHANGE INSTALLED INBD SLAT #6 UP TO AND INCLUDING STEP H(15) PER AMM 27-81-01-424-143. C/W REMAINDER OF #6 L/E SLAT INSTALLA
- [SDR IPXA2023103012214](https://openairdocs.org/sdr/IPXA2023103012214), Oct 28, 2023: UNKNOWN. UNKNOWN. MAJOR REPAIR* #6 SLAT DAMAGED- BROKEN SKIN ASSIGNED EO-88575-PRELIM1 FOR TEMPORARY REPAIR INSTRUCTIONS. OPEN
- [SDR IPXA2023091872638](https://openairdocs.org/sdr/IPXA2023091872638), Sep 15, 2023: LIGHT. INOPERATIVE. EMERGENCY LIGHTS INOP R&R EMER SUPPLY BATTERY PACK IAW 767 AMM 33-51-07-002-006. OPS CHECK GOOD. IPC 33-51-07-32
- [SDR IPXA2022050681809](https://openairdocs.org/sdr/IPXA2022050681809), May 6, 2022: STIFFENER. CRACKED. INSPECTION TYPE:C6CRACK ON CENTER WING TANK STIFFENER(P/N:111T2008-12)ON STA 785.9, RBL 33.REPAIR I.A.W 767-300F SRM. 83.01, UPS EO B767-5740-58151-C.
- [SDR IPXA2022050881846](https://openairdocs.org/sdr/IPXA2022050881846), May 2, 2022: FLOOR PANEL. DAMAGED. INSPECTION TYPE:C6DAMAGE ON M/D CARGO FLOOR PANEL AT STA 287-412, LBL 11-RBL11.FABRICATE THE REPLACEMENT FLOOR PANEL PER EO NO. B767-5320-9693-I
- [SDR IPXA2022041281120](https://openairdocs.org/sdr/IPXA2022041281120), Apr 12, 2022: LIGHT. INOPERATIVE. INSPECTION TYPE:NAEXTERIOR EMERGENCY LIGHT INOPRELAMPED EXTERIOR EMERGENCY LIGHT PER 767 MM 33-51-16-962-001. OPS CHECK NORMAL
- [SDR IPXA2020073108417](https://openairdocs.org/sdr/IPXA2020073108417), Jul 28, 2020: SEAL. DAMAGED. A LOUD HUMMING NOISE ORIGINATING CLOSE TO CREW ENTRY DOOR. STARTED AT 10000' ON CLIMB OUT AND EDED ABOUT 10000' ON DESCENT.CREW ENTRY DOOR SEALS INSPECTED AND C
- [SDR IPXA2020072978304](https://openairdocs.org/sdr/IPXA2020072978304), Jul 27, 2020: SEAL. CUT. INSPECTION TYPE:N/AA LOUD HUMMING NOISE ORIGINATING CLOSE TO CREW ENTRY DOOR. STARTED AT 10000' ON CLIMB OUT AND EDED ABOUT 10000' ON DESCENT.CREW ENTRY DOOR SE
- [SDR IPXA2020080328554](https://openairdocs.org/sdr/IPXA2020080328554), Jul 25, 2020: SEAL. NOT SEATED. GEAR DOOR VIBRATION ON CLIMB ACCELERATING TO 310KTS LOUD HUMMING AND VIBRATION OCCURS. SLOWED CLIMB SPEED TO 280KTS AND NOISE-VIBRATION WENT AWAY. ON DESCENT AT
- [SDR IPXA2019070744175](https://openairdocs.org/sdr/IPXA2019070744175), Jul 7, 2019: SKIN. DENTED. INSPECTION TYPE:N/A RIGHT WING INBOARD AFT FLAP LOWER SURFACE DENT REPAIR 58 FROM INBOARD EDGE AND 2" FROM TRAILING EDGE. 1/2" DIAMETER AND .043 DEPTH. REPAIRED
- [SDR IPXA2018083133417](https://openairdocs.org/sdr/IPXA2018083133417), Aug 31, 2018: UNKNOWN. ODOR. MUSTY ODOR FROM AIR CONDTIONING IN COCKPIT, WHEN PACKS WERE ON, AND CONDENSATION IN OUTLETS BOTH PACKS, BITE CHECKED IAW AMM 21.51.00.5 NO LEAKS, THEN PACKS OPE
- [SDR IPXA2018030727224](https://openairdocs.org/sdr/IPXA2018030727224), Mar 6, 2018: SENSOR. OUT OF LIMITS. AIR TURNBACK DUE TO A FWD CARGO DOOR INDICATION. ACCOMPLISHED DMP 52-71-01-01 BY VERIFYING FWD LWR CARGO DOOR CLOSED, LATCHED, AND LOCKED. TROUBLESHOT IAW FIM 5
- [SDR IPXA2017101622651](https://openairdocs.org/sdr/IPXA2017101622651), Oct 15, 2017: BLOWER. INOPERATIVE. LEFT EVAS UNIT BLOWER INOPERATIVE. R & R THE EVAS UNIT IAW 25-69-00-401, OPS CHECKED GOOD.
- [SDR IPXA2017092121941](https://openairdocs.org/sdr/IPXA2017092121941), Sep 21, 2017: ESCAPE ROPE. LOOSE. WHEN OPENING THE CREW DOOR, THE EMERGENCY ROPE CAME OFF. THE DOOR WAS STUCK. INGRESS ROPE WAS PROPERLY FIXED AT CREW ENTRY DOOR LOCATION IAW AMM 25-61-04-402-01
- [SDR IPXA2016021699491](https://openairdocs.org/sdr/IPXA2016021699491), Feb 15, 2016: PAWL. BROKEN. CREW ENTRY DOOR HANDLE DIFFICULT TO MOVE, OPEN AND CLOSE, DOOR CLOSED IMPROPERLY, OUT OF SEQUENCE.REPOSITIONED UPPER PAWL AND UPPER CEILING PANEL. OPERATIONALLY
- [SDR IPXA2015101094628](https://openairdocs.org/sdr/IPXA2015101094628), Oct 10, 2015: SHIELD. MISSING. CAPT'S EVAS CONTAINER IS MISSING DRIP SHIELD. INSTALLED NEW EVAS SPLASH GUARD REF AMM 25-69-00.
- [SDR IPXA2015061490136](https://openairdocs.org/sdr/IPXA2015061490136), Jun 14, 2015: FLOOR PANEL. DAMAGED. TWO DENTS, ONE INCH IN DIAMETER ON MCD FLOOR PANEL. FABRICATED A NEW FLOOR PANEL IAW EO B767-5320-9693H.
- [SDR IPXA2015061490140](https://openairdocs.org/sdr/IPXA2015061490140), Jun 14, 2015: FLOOR PANEL. DAMAGED. MAIN CARGO DECK FLOOR PANEL, HAS A ONE INCH IN DIAMETER HOLE. FABRICATED A NEW FLOOR PANEL IAW EO B767-5320-9693-H.
- [SDR IPXA2015060889951](https://openairdocs.org/sdr/IPXA2015060889951), Jun 8, 2015: FLOOR PANEL. DENTED. MAIN CARGO DECK NR 2 AFT CENTER FLOOR PANEL HAS A ONE INCH SQUARE DENT. FABRICATED A NEW FLOOR PANEL IAW EO B767-5320-9693-H.
- [SDR IPXA2015060789909](https://openairdocs.org/sdr/IPXA2015060789909), Jun 7, 2015: FLOOR PANEL. DENTED. MAIN CARGO DECK NR 2R AFT OTBD FLOOR PANEL DENTED 14.5". FABRICATED A NEW FLOOR PANEL IAW EO B767-5320-9693-H.
- [SDR IPXA2015060789901](https://openairdocs.org/sdr/IPXA2015060789901), Jun 7, 2015: FLOOR PANEL. DAMAGED. MAIN CARGO DECK 2R AFT OTBD FLOOR PANEL DENTED 14.5" LONG BY 1" DEEP, FABRICATED A NEW FLOOR PANEL IAW EO B767-5320-9693H.
- [SDR IPXA2015051989231](https://openairdocs.org/sdr/IPXA2015051989231), May 19, 2015: CONTROL PANEL. INOPERATIVE. EMERGENCY LIGHTS INOPERATIVE, REF M33-51-1-1. REPLACED EMERGENCY LIGHT PANEL ASSY. OPS OK, REF AMM 33-51-08.
- [SDR IPXA2014031482250](https://openairdocs.org/sdr/IPXA2014031482250), Mar 12, 2014: CHANNEL. DAMAGED. CREW ENTRANCE DOOR "SLIDE TAPE" RETENTION SLEEVE DAMAGED. R & R CREW DOOR INGRESS ROPE CHANNEL IAW AMM 25-61-04.
- [SDR IPXA3679981](https://openairdocs.org/sdr/IPXA3679981), Aug 25, 2013: SKIN. DAMAGED. .8 INCH HOLE IN NR 8 SLAT T/E WEDGE UPPER SKIN 45.8" FROM OTBD END AND 7.5" FWD OF T/E. REPAIRED IAW EO B767-5750-51892-A.
- [SDR IPXA2676481](https://openairdocs.org/sdr/IPXA2676481), Dec 16, 2012: CONTROLLER. INOPERATIVE. NO CABIN PRESSURIZATION AFTER DEPARTURE. COMPLETED CHECKLIST. FOUND NR 1 AUTO CABIN PRESSURE INOPERATIVE, WOULD NOT SELF TEST. R & R NR 1 AUTO PRESSURE CONTROLL
- [SDR IPXA12674288](https://openairdocs.org/sdr/IPXA12674288), Jul 6, 2012: SKIN. DENTED. INSPECTION TYPE: 1C, FUSELAGE AT BS 1916 LBL 3" AREA DENT IS FOUND DURING DMI D478160 RECTIFICATION. REPAIRED IAW RS R53-81-37375 REV A & EO B767-5330-47814-A, 
- [SDR IPXA12674324](https://openairdocs.org/sdr/IPXA12674324), Jul 5, 2012: WEDGE. DENTED. INSPECTION TYPE: 1C, LT WING OTBD T/E FLAP, T/E WEDGE, LOWER SURFACE DENTED. COMPOSITE PREPREG LAY UP REPAIR CARRIED OUT IAW SRM 51-70-07, PAR 5A (1), FIG 9, RE
- [SDR IPXA12674322](https://openairdocs.org/sdr/IPXA12674322), Jul 5, 2012: WEDGE. DENTED. INSPECTION TYPE:1C LT WING OTBD T/E WEDGE UPPER SURFACE DENTED. COMPOSITE PREPREG LAY UP REPAIR CARRIED OUT IAW SRM 51-70-07, PAR 5A(1), FIG 9, REV 52.
- [SDR IPXA12674318](https://openairdocs.org/sdr/IPXA12674318), Jul 5, 2012: WEDGE. DENTED. INSPECTION TYPE: 1C, LT WING OTBD T/E FLAP, T/E WEDGE, UPPER SURFACE DENTED. COMPOSITE PREPREG LAY UP REPAIR CARRIED OUT IAW SRM 51-70-07, PAR 5A(1), FIG 9, REV
- [SDR IPXA12674316](https://openairdocs.org/sdr/IPXA12674316), Jul 5, 2012: SKIN. DENTED. INSPECTION TYPE: 1C, LT WING OTBD T/E FLAP, T/E WEDGE UPPER SURFACE DENTED. COMPOSITE PREPREG LAY UP REPAIR CARRIED OUT IAW SRM 51-70-07, PAR 5A(1), FIG 9, REV 

All 91: https://openairdocs.org/aircraft/N341UP/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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