# N348UP: 2012 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: 37872
- Year built: 2012
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: February 25, 2012
- Certificate issued: February 28, 2012
- Expires: February 29, 2028
- Mode S code: A3DCD6
- Registered owner: [C C & E I LLC](https://openairdocs.org/faa-owner/C%20C%20%26%20E%20I%20LLC)
- Location: [Louisville, KY](https://openairdocs.org/faa-place/KY/Louisville)
- Owner type: LLC
- Owner's area on the map: 38.2585° N, 85.5398° W: Placed by OpenAirDocs at the center of ZIP code 40223, within about 2 miles (OpenAirDocs). The owner's mailing address, not where the aircraft is based
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=348UP
- Page: https://openairdocs.org/aircraft/N348UP

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 N348UP.

## FAA accident and incident reports

None matched to N348UP.

## Service difficulty reports (58, 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 IPXA2026031363475](https://openairdocs.org/sdr/IPXA2026031363475), Mar 7, 2026: RECEIVER. MISSING. MISSING BUSHING, NR 2 ENGINE LT FAN COWL, LWR MID BRACKET. INSTALLED A NEW RECEIVER ASSY IAW SRM 51-40-02-0G, REV 94, AND CMM IPL 71-13-21 REV.47.
- [SDR IPXA2026031047781](https://openairdocs.org/sdr/IPXA2026031047781), Mar 6, 2026: BRACKET. CHAFED. CHAFED BRACKET, NR 2 ENG RT THRUST REVERSER LWR FAIRING T/E AREA. INSTALL A NEW BRACKET IAW SRM 51-40-02-0G, REV 94, AND ST ENGINEERING IPC 78-32-22 REV.94.
- [SDR IPXA2026031047970](https://openairdocs.org/sdr/IPXA2026031047970), Mar 6, 2026: DOOR. CHAFED. CHAFED DOOR, NR 2 ENG RT THRUST REVERSER BLOW OUT DOOR L/E AREA. INSTALL NEW BLOWOUT DOOR IAW SRM 51-40-02-0G REV.94 AND ST ENGINEERING IPC 78-32-22 REV.94 AND 
- [SDR IPXA2026031246369](https://openairdocs.org/sdr/IPXA2026031246369), Mar 6, 2026: FORMER. CRACKED. CRACKED FORMER, LEFT WING LEADING EDGE CAVITY STRUCTURE LES 565. INSTALLED A NEW FORMER IAW SRM 51-40-02-0G, REV 94, AND DWG 114T2162, SHT 6, REV -, AND SREO-50
- [SDR IPXA2026031247725](https://openairdocs.org/sdr/IPXA2026031247725), Mar 6, 2026: PLATE. WORN. WORN PLATE, NR 1 ENG LT CORE COWL INNER AFT FRAME LOWER PLATE. INSTALLED A NEW PLATE IAW SRM 51-40-02-0G, REV 94, & CMM IPL 71-13-23 REV 47.
- [SDR IPXA2026031247676](https://openairdocs.org/sdr/IPXA2026031247676), Mar 6, 2026: HINGE. WORN. WORN HINGE, NR 1 PYLON STRUT PRESSURE RELIEF DOOR 434AR UPPER HINGE. INSTALLED NEW HINGE IAW SRM 51-40-02-0G, REV 94, DWG 311T1064, SHT 1, REV G , & DWG 311T106
- [SDR IPXA2026031347798](https://openairdocs.org/sdr/IPXA2026031347798), Mar 6, 2026: BRACKET. CHAFED. CHAFED BRACKET, NR 1 ENG LT THRUST REVERSER LOWER CLOSURE PANEL AFT SIDE BRACKET. INSTALLED A NEW BRACKET IAW SRM 51-40-02-0G, REV 94 AND ST ENGINEERING IPC 78-
- [SDR IPXA2026031145649](https://openairdocs.org/sdr/IPXA2026031145649), Mar 6, 2026: BRACKET. CHAFED. CHAFED BRACKET, NR 1 ENG RT THRUST REVERSER AFT ACCESS DOOR FWD EDGE (REPLACE). INSTALL NEW BRACKET I.A.W SRM 51-40-02-0G REV.94 AND ST ENGINEERING IPC 78-32-22
- [SDR IPXA2026030943700](https://openairdocs.org/sdr/IPXA2026030943700), Mar 6, 2026: FORMER. CRACKED. CRACKED FORMER , LEFT WING LEADING EDGE CAVITY STRUCTURE OSS 499. INSTALL NEW FORMER IAW SRM 51-40-02-0G REV.94 AND DWG 114T2161 SH 6 REV: - AND SREO-50900-REQ0
- [SDR IPXA2026031245725](https://openairdocs.org/sdr/IPXA2026031245725), Mar 6, 2026: LONGERON. CHAFED. CHAFED LONGERON, NR 1 ENG LT CORE COWL LOWER LONGERON. INSTALLED NEW LONGERON IAW SRM 51-40-02-0G REV. 94 AND CMM IPL 71-13-23 REV. 47.
- [SDR IPXA2026031348628](https://openairdocs.org/sdr/IPXA2026031348628), Mar 6, 2026: BRACKET. CRACKED. CRACKED BRACKET, LEFT WING NR 4 SLAT INBOARD SIDE ROTARY ACTUATOR ROD LOWER SEAL DOOR FORWARD SUPPORT BRACKET. IAW AMM 20-11-00-910-802 REV.147 REPLACE BRACKET.
- [SDR IPXA2026031349916](https://openairdocs.org/sdr/IPXA2026031349916), Mar 6, 2026: DOOR. CRACKED. CRACKED DOOR, LOWER SURFACE OF LEFT WING LEADING EDGE LOWER 521ABB PANEL. IAW AMM 20-11-00-910-802 REV.147 REPLACED DOOR ASSEMBLY.
- [SDR IPXA2026031346226](https://openairdocs.org/sdr/IPXA2026031346226), Mar 6, 2026: BRACKET. CRACKED. CRACKED BRACKET, NR 1 PYLON AFT FAIRING INTERNAL HYD SYS VENT TUBE SUPPORT BRACKET NAC STA 350. INSTALL FABRICATE BRACKET I.A.W SRM 51-40-02-0G REV.94 AND DWG N
- [SDR IPXA2026031246244](https://openairdocs.org/sdr/IPXA2026031246244), Mar 6, 2026: BRACKET. CRACKED. CRACKED BRACKET, LT APU DOOR NR1 SUPPORT FROM FORWARD EDGE. REPLACED, CHECKED OK. INSTALLED NEW BRACKET I.A.W SRM 51-40-02-0G REV. 94 AND BOEING DWG NO. 355T520
- [SDR IPXA2026031246143](https://openairdocs.org/sdr/IPXA2026031246143), Mar 6, 2026: BRACKET. WORN. WORN BRACKET, LT APU DOOR NR 2 SUPPORT FROM FORWARD EDGE. CHECKED OK. INSTALLED NEW BRACKET IAW SRM 51-40-02-0G REV. 94 AND DWG 355T5200 SH. 1 REV. A.
- [SDR IPXA2026031329791](https://openairdocs.org/sdr/IPXA2026031329791), Mar 5, 2026: ROD. WORN. WORN RECEIVER , NR 1 ENG LT CORE COWL HOLD OPEN ROD. REMOVED DAMAGE RECEIVER IAW SRM 51-40-02-0G REV.94 2.INSTALL NEW RECEIVER IAW SRM 51-40-02-0G REV.94 AND AE
- [SDR IPXA2026031229860](https://openairdocs.org/sdr/IPXA2026031229860), Mar 5, 2026: BRACKET. WORN. WORN BRACKET , NR 2 ENG LT CORE COWL WELD ASSY. REMOVED DAMAGE BRACKET I.A.W SRM 51-40-02-0G REV.94. INSTALL NEW BRACKET IAW SRM 51-40-02-0G REV.94 AND CMM IPL 
- [SDR IPXA2026031327022](https://openairdocs.org/sdr/IPXA2026031327022), Mar 5, 2026: BRACKET. WORN. WORN BRACKET, NR 1 PYLON AFT FAIRING HOLD OPEN ROD UNIVERSAL JOINT AREA. INSTALLED NEW BRACKET IAW SRM 51-40-02-0G REV.94 AND DWG 313T2303 SHT 135 REV-.
- [SDR IPXA2026031128598](https://openairdocs.org/sdr/IPXA2026031128598), Mar 5, 2026: ANGLE. CRACKED. CRACKED ANGLE, NR 1 PYLON AFT FAIRING INTERNAL BULKHEAD NAC STA 376 INBD SIDE. INSTALLED NEW ANGLE IAW SRM 51-40-02-0G REV. 94, DWG 313T2303, SHT 136, REV -, & 
- [SDR IPXA2026031028599](https://openairdocs.org/sdr/IPXA2026031028599), Mar 5, 2026: ANGLE. CRACKED. CRACKED ANGLE, NR 1 PYLON AF FAIRING INTERNAL BULKHEAD NAC STA 376 OTBD SIDE. INSTALLED A NEW ANGLE IAW SRM 51-40-02-0G, REV 94, & DWG 313T2303, SHT 136, REV-, 
- [SDR IPXA2026030906568](https://openairdocs.org/sdr/IPXA2026030906568), Mar 4, 2026: SUPPORT BRACKET. CRACKED. CRACKED TORQUE TUBE SUPPORT BRACKET OF THE LT WING LEADING EDGE COMPARTMENT. INSTALLED A NEW BRACKET IAW SRM 51-40-02-0G, REV 94, & DWG 114T1240, SHT 6, REV -.
- [SDR IPXA2026031289808](https://openairdocs.org/sdr/IPXA2026031289808), Mar 3, 2026: BRACKET. CRACKED. CRACKED BRACKET, NR 2 ENG LT THRUST REVERSER FWD TORQUE BOX SUPPORT BRACKET NEAR 11:00 POSITION. INSTALLED A NEW STIFFENR IAW SRM 51-40-02-0G, REV 94, AND AIPC 
- [SDR IPXA2026031289779](https://openairdocs.org/sdr/IPXA2026031289779), Mar 3, 2026: STIFFENER. CRACKED. CRACKED BRACKET, NR 2 ENG RT THRUST REVERSER FWD TORQUE BOX SUPPORT BRACKET NEAR 3:00 POSITION. INSTALLED A NEW STIFFENR IAW SRM 51-40-02-0G, REV 94, AND AIPC 7
- [SDR IPXA2026031089949](https://openairdocs.org/sdr/IPXA2026031089949), Mar 3, 2026: ANGLE. CRACKED. CRACKED ANGLE, NR 2 PYLON AFT FAIRING INNER AFT FRAME INBD SIDE SUPPORT CLIP. INSTALLED A NEW CLIP I.A.W SRM 51-40-02-0G REV.94 AND DWG 313T2303, SH 136, REV -,
- [SDR IPXA2026030973683](https://openairdocs.org/sdr/IPXA2026030973683), Mar 2, 2026: BATTERY. INOPERATIVE. **SUPPLEMENTAL SDR** FAULT - FOUND EMERGENCY LIGHT DID NOT STAY ON FOR 15 MINUTES (REPLACE). I.A.W AMM 33-51-07-022-001, 33-51-07-422-012 REV. 147 REPLACED THE 
- [SDR IPXA2026030874565](https://openairdocs.org/sdr/IPXA2026030874565), Mar 2, 2026: SEAT TRACK. WORN. FOUND SEAT TRACK ASSY INBOARD AFT OF FIRST OFFICER SEAT WORN, POSITION (REPLACE) 1. I.A.W AMM 25-11-01-822-095-001 REV.147, REPLACED TRACK ASSY. JOB COMPLETED A
- [SDR IPXA2026030273683](https://openairdocs.org/sdr/IPXA2026030273683), Mar 2, 2026: LIGHT. NO TEST. FOUND EMERGENCY DID NOT STAY ON FOR 15 MINUTES.
- [SDR IPXA2025041809621](https://openairdocs.org/sdr/IPXA2025041809621), Mar 18, 2025: FLOOR PANEL. CRACKED. *** SUPPLEMENTAL SDR *** LOAD CREW REPORTS MCD FLOOR AT POS 14R CRACKED INSTALLED AFFECTED CARGO LOCK BETWEEN POS 12 AND 14 RIGHT PER AMM 25-58-01. INSTALLED AF
- [SDR IPXA2025031809621](https://openairdocs.org/sdr/IPXA2025031809621), Mar 18, 2025: FLOOR PANEL. CRACKED. LOAD CREW REPORTS MCD FLOOR AT POS 14R CRACKED INSTALLED NEW FABRICATED FLOOR PANEL AT POS 14R PER AMM 53-01-06 UP TO AND INCLUDING STEP F. (21). WAITING ON SEA
- [SDR IPXA2024122675823](https://openairdocs.org/sdr/IPXA2024122675823), Dec 24, 2024: WINDOW. DAMAGED. CAPTAINS SIDE WINDOW L2 HAD FLICKERING LIGHT ON BOTTOM EDGE MIDDLE. SHUT OFF LEFT SIDE WINDOW HEAT AND IT STOPPED AND COOLED. WAS TOO HOT TO TOUCH WHEN FLICKERI
- [SDR IPXA2024122475823](https://openairdocs.org/sdr/IPXA2024122475823), Dec 24, 2024: HEATER. FAULTED. *SDR FILED OPEN* CAPTAINS SIDE WINDOW L2 HAD FLICKERING LIGHT ON BOTTOM EDGE MIDDLE. SHUT OFF LEFT SIDE WINDOW HEAT AND IT STOPPED AND COOLED. WAS TOO HOT TO TO
- [SDR IPXA2024020284515](https://openairdocs.org/sdr/IPXA2024020284515), Jan 29, 2024: SKIN PANEL. DENTED. MAJOR REPAIR, DENT, FUSELAGE SKIN BETWEEN STA 360 - STA 384, S-16L - S-17L (REPAIR). ACCOMPLISHED REPAIR IAW SRM 53-00-01-2R-12 REV.88 AND EO-89370-REQ 1 REV. 1
- [SDR IPXA2024020571729](https://openairdocs.org/sdr/IPXA2024020571729), Jan 28, 2024: NONE. NONE. FUSELAGE DRAIN HOLES INSPECTION AND INSTALLATION AFT OF BS 1725.5 BETWEEN S-36L AND S-36R. ACCOMPLISHED SDR.
- [SDR IPXA2024012971729](https://openairdocs.org/sdr/IPXA2024012971729), Jan 28, 2024: NONE. NONE. **SDR FILED OPEN** ADD SDR FOR EO-82173-JIC001 (FUSELAGE DRAIN HOLES INSPECTION AND INSTALLATION AFT OF BS 1725.5 BETWEEN S-36L AND S-36R) ACCOMPLISHED SDR.
- [SDR IPXA2024020523240](https://openairdocs.org/sdr/IPXA2024020523240), Jan 25, 2024: ADAPTER. BROKEN. FOUND MAIN DECK CARGO RESTRAINT FLOOR ADAPTER FITTING BROKEN AT STA 676, LBL 47.5 (REPLACE) I.A.W AMM 25-57-02-404-016, AMM 25-57-05-404-006 AND AMM 25-58-01-40
- [SDR IPXA2024020512998](https://openairdocs.org/sdr/IPXA2024020512998), Jan 25, 2024: ANGLE. CRACKED. CRACKED ANGLE IN BULK CARGO COMPARTMENT LEFT AREA STA 1578 LBL 60 (REPLACE) I.A.W AMM 25-57-05-404-006 AND AMM 25-58-04-404-015 REV.141 INSTALLED MAIN DECK CARG
- [SDR IPXA2024012522998](https://openairdocs.org/sdr/IPXA2024012522998), Jan 25, 2024: ANGLE. CRACKED. FAULT - CRACK - ANGLE BULK CARGO COMPARTMENT LEFT AREA STA 1578 LBL 60 (REPLACE) I.A.W AMM 25-57-05-004-001 AND AMM 25-58-04-004-010 REV.141 REMOVED MAIN DECK C
- [SDR IPXA2024012523240](https://openairdocs.org/sdr/IPXA2024012523240), Jan 25, 2024: FITTING. BROKEN. FAULT - FOUND MAIN DECK CARGO RESTRAINT FLOOR ADAPTER FITTING BROKEN AT STA 676, LBL 47.5 (REPLACE) 1. I.A.W AMM 25-57-02-004-029, AMM 25-57-05-004-001 AND AMM 
- [SDR IPXA2024020506229](https://openairdocs.org/sdr/IPXA2024020506229), Jan 24, 2024: FIRE DETECTOR. CRACKED. CRACKED BULK CARGO FIRE DETECTION LOOP FASTENER STRIP CRACK AT STA 1562 LBL 66 (REPLACE) I.A.W AMM 26-18-01-424-014-001 REV.141 INSTALLED DUCT LEAK DETECTOR CLA
- [SDR IPXA2024012406229](https://openairdocs.org/sdr/IPXA2024012406229), Jan 24, 2024: STRIP. CRACKED. FAULT - CRACK - BULK CARGO FIRE DETECTION LOOP FASTENER STRIP CRACK AT STA 1562 LBL 66 (REPLACE) OK TO WORK
- [SDR IPXA2024010204861](https://openairdocs.org/sdr/IPXA2024010204861), Dec 29, 2023: LIGHT. INOPERATIVE. EMERGENCY LIGHTS DO NOT ILLUM WHEN SWITCH SELECTED TO "ON" REPLACED BATTERY PACK IAW AMM 33-51-07-422-012, OPS GOOD.
- [SDR IPXA2023082545816](https://openairdocs.org/sdr/IPXA2023082545816), Aug 24, 2023: DOOR. UNKNOWN. CREW ENTRY DOOR BINDING WHEN OPENING AND CLOSING ACCOMPLISHED DOOR LUBRICATION OF CREW ENTRY DOOR IAW AMM 12-21-18. OPS CK OK
- [SDR IPXA2023052395167](https://openairdocs.org/sdr/IPXA2023052395167), May 23, 2023: FLAP SYSTEM. WARNING MESSAGE. ON FINAL FLAPS 25 AND CONFIGURED LE SLAT ASYM EICAS BEFORE RUNNING QRH PROCEDURE EICAS CLEARED . RAN QRH LANDED UNEVENTFULLY. C/W FIM TC 27-81-00-815-809
- [SDR IPXA2022111088024](https://openairdocs.org/sdr/IPXA2022111088024), Nov 9, 2022: SIGN. INOPERATIVE. INSPECTION TYPE:NAEMERGENCY EXIT SIGN BY ENTRY DOOR MISSING BOTTOM 3 BULB SEGMENTR & R EMERGENCY EXIT SIGN ASSY PER MM 33 41 01 OPS CKS OK ESR 52 11 02 10A ITEM
- [SDR IPXA2023051319370](https://openairdocs.org/sdr/IPXA2023051319370), Jul 1, 2022: FLOORBOARD. DAMAGED. MAIN CARGO COMPARTMENT FLOOR PANEL REPAIR (SREO) 2 DENTS, 1WX 2.25LX .5D, AND .7***SM13/LMX8*** INSTALLED NEW FLOOR PANEL IAW AMM 53-01-06
- [SDR IPXA2021090173403](https://openairdocs.org/sdr/IPXA2021090173403), Aug 31, 2021: ESCAPE ROPE. FAULTED. INSPECTION TYPE:N/ACAPT ESCAPE ROPE DOOR KEEPS FALLING OPENRESTORED CAPT. ROPE PER AMM 25-61-13 OPS CK GOOD
- [SDR IPXA2020030352723](https://openairdocs.org/sdr/IPXA2020030352723), Mar 3, 2020: WARNING SYSTEM. FALSE ACTIVATION. INSPECTION TYPE:NA**AIR TURN BACK - SDR FILED OPEN** DURING INITIAL CLIMB OUT FROM MAD AT APPROX 7000' MSL THE FWD CARGO DOOR EICAS MSG AND CARGO DOORS OVERHEAD
- [SDR IPXA2019100447543](https://openairdocs.org/sdr/IPXA2019100447543), Oct 3, 2019: BLADE. NICKED. LEFT ENGINE, 1 X FAN BLADE LEADING EDGE NICK DAMAGE AT 564 MM FROM ROOT. BLEND REPAIR C/O IAW AMM 72-31-02. C/W INSPECTION OF THE LT ENGINE ONE FAN BLADE IAW AM
- [SDR IPXA2018100634752](https://openairdocs.org/sdr/IPXA2018100634752), Oct 5, 2018: CONNECTOR. DIRTY. REV INTERLOCK STATUS MESSAGE DURING CLIMB OUT. T/S PERFORMED IAW FIM 78-36-815-805-H00. EXAMINED CONNECTOR D71990, CONNECTOR CLEANED. TESTED T/R IAW AMM 78-31-0
- [SDR IPXA2018053030154](https://openairdocs.org/sdr/IPXA2018053030154), May 29, 2018: SKIN. GOUGED. GOUGE IN SKIN AT FR 1197 S26R. APPLIED DOUBLER PER EO B767-5330-68408-D.

All 58: https://openairdocs.org/aircraft/N348UP/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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