# N349UP: 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: 37947
- Year built: 2012
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: March 30, 2012
- Certificate issued: April 2, 2012
- Expires: April 30, 2028
- Mode S code: A3E08D
- 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=349UP
- Page: https://openairdocs.org/aircraft/N349UP

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 N349UP.

## FAA accident and incident reports

None matched to N349UP.

## Service difficulty reports (36)

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 IPXA2026040717262](https://openairdocs.org/sdr/IPXA2026040717262), Apr 3, 2026: BLOWOUT DOOR. CHAFED. CHAFED- SKIN PNL, NO.1 ENG RH THRUST REVERSER FWD ACCESS DOOR INNER FWD EDGE. REMOVED DAMAGE BLOWOUT DOOR I.A.W SRM 51-40-02-0G REV.94. INSTALL NEW BLOWOUT DOOR
- [SDR IPXA2026040817475](https://openairdocs.org/sdr/IPXA2026040817475), Apr 3, 2026: BRACKET. CRACKED. CRACKED BRACKET, FWD SIDE OF LT WING NR 3 SLAT INBD SEAL DOOR. I.A.W AMM 57-41-56-004-001 REV 147 AND AMM 57-41-56-404-009 REV 147 REPLACED THE BRACKET.
- [SDR IPXA2026040715773](https://openairdocs.org/sdr/IPXA2026040715773), Apr 3, 2026: BRACKET. CHAFED. CHAFED BRACKET, NR 2 ENG RT THRUST REVERSER CLOSEOUT DOOR T/E. REMOVED DAMAGE BRACKET I.A.W SRM 51-40-02-0G REV.94. INSTALL NEW BRACKET I.A.W SRM 51-40-02-0G RE
- [SDR IPXA2026040715792](https://openairdocs.org/sdr/IPXA2026040715792), Apr 3, 2026: ADAPTER. CHAFED. CHAFED BRACKET, NR 2 ENG RT CORE COWL HOLD OPEN ROD SUPPORT BRACKET. REMOVED DAMAGE BRACKET I.A.W SRM 51-40-02-0G REV.94. INSTALL NEW BRACKET I.A.W SRM 51-40-02
- [SDR IPXA2026040415856](https://openairdocs.org/sdr/IPXA2026040415856), Apr 3, 2026: HINGE. WORN. WORN HINGE, NR 1 PYLON STRUT PRESSURE RELIEF DOOR 434AR UPPER AND LOWER SIDE HINGE. REMOVED DAMAGE HINGE IAW SRM 51-40-02-0G, REV 94. INSTALL NEW HINGE IAW SRM 
- [SDR IPXA2026040417247](https://openairdocs.org/sdr/IPXA2026040417247), Apr 3, 2026: BRACKET. CRACKED. CRACKED BRACKET, LT WING INBD L/E NR 6 SLAT DRIVE TORQUE TUBE SUPPORT, LES 285. REMOVED DAMAGE BRACKET I.A.W SRM 51-40-02-0G REV.94. INSTALL NEW BRACKET I.A.W S
- [SDR IPXA2026040792671](https://openairdocs.org/sdr/IPXA2026040792671), Apr 2, 2026: LATCH. WORN. WORN LATCH, NR 1 ENG RH FAN COWL OIL TANK ACCESS DOOR FWD AND UPPER SIDE QTY: 2EA. REMOVED DAMAGE LATCH I.A.W SRM 51-40-02-0G REV.94. INSTALL NEW LATCH I.A.W SR
- [SDR IPXA2026040795033](https://openairdocs.org/sdr/IPXA2026040795033), Apr 2, 2026: BRACKET. CHAFED. FAULT - CHAFING , NO.2 ENG L/H T/R CLOSE OUT DOOR T/E BRACKET. REMOVED DAMAGE BRACKET I.A.W SRM 51-40-02-0G REV.94. INSTALL NEW BRACKET I.A.W SRM 51-40-02-0G RE
- [SDR IPXA2026040496728](https://openairdocs.org/sdr/IPXA2026040496728), Apr 2, 2026: BRACKET. CRACKED. CRACKED BRACKET, R/H WING L/E NO.7 SLAT AREA PNL 611KB TORQUE SUPPORT BRACKET AT LES 281. REMOVED DAMAGE BRACKET I.A.W SRM 51-40-02-0G REV.94. INSTALL NEW BRACK
- [SDR IPXA2026040792937](https://openairdocs.org/sdr/IPXA2026040792937), Apr 2, 2026: ANGLE. CRACKED. CRACKED CLIP , NR 2 PYLON AFT FAIRING AFT STIFFENER L/H SUPPORT CLIP , AT NAC STA 376. REMOVED DAMAGE ANGLE IAW SRM 51-40-02-0G, REV 94. INSTALLED A NEW ANGLE I
- [SDR IPXA2026040355846](https://openairdocs.org/sdr/IPXA2026040355846), Mar 31, 2026: CLAMP. CRACKED. CRACKED LOCK CLAMPS, NR 1 PYLON AFT STRUT FAIRING HOLD OPEN ROD STOW BRACKET.
- [SDR IPXA2026040553062](https://openairdocs.org/sdr/IPXA2026040553062), Mar 31, 2026: SEAT TRACK. WORN. FOUND CAPTAIN SEAT TRACK ASSY WORN AT : INBOARD AFT, OUTBOARD AFT TOTAL: 1EA. I.A.W AMM 25-11-01-822-095-001 REV.147 REPLACED TRACK ASSY.
- [SDR IPXA2026040156320](https://openairdocs.org/sdr/IPXA2026040156320), Mar 31, 2026: FLOOR PANEL. DAMAGED. MAJOR REPAIR. FOUND MAIN DECK FLOOR PANEL DAMAGED, 251XFF. REPAIRED IAW AMM 25-57-02-404-016, AMM 25-57-05-404-006, AMM 25-58-01-404-005 AND AMM 25-58-04-404-01
- [SDR IPXA2026040158907](https://openairdocs.org/sdr/IPXA2026040158907), Mar 31, 2026: SKIN. DEBONDED. DEBONDED SKIN , LOWER FACE OF L/H WING T/E INBD AFT FLAP LOWER SKIN , REMOVE THE DISBOND MATERIALS AND CLEAN. BOND THE REPAIR PLIES WITH RESIN CURED AT 150°F F
- [SDR IPXA2024030699882](https://openairdocs.org/sdr/IPXA2024030699882), Feb 28, 2024: FUEL LINE. CRACKED. FAULT - FOUND THE CRACK TUBE INSIDE THE PANEL NO.632BB. (REPLACE) I.A.W. AMM 28-22-07-004-017 REV.141 AND AMM 28-22-07-404-008 REV.141 REPLACED THE FUEL TUBE. C
- [SDR IPXA2024022777559](https://openairdocs.org/sdr/IPXA2024022777559), Feb 27, 2024: FLOOR PANEL. CRACKED. FOUND THE FLOOR PANEL NO.241WFF WITH CRACK DAMAGE, AT STA 984, LBL 6. (FLOOR PANEL PN: 145T5876-87) (REPAIR) I.A.W AMM 53-01-06-400-801 REV.141 INSTALL MAIN DEC
- [SDR IPXA2023101848956](https://openairdocs.org/sdr/IPXA2023101848956), Oct 18, 2023: DOOR SEAL. DAMAGED. LOUD SQUEAL COMING FROM ENTRY DOOR. APPARENTLY FROM BOTTOM SEAL. STARTED CLIMBING ABOVE. 280. REPAIRED MAIN ENTRY DOOR LOWER SEAL PER AMM 52-09-00/801.
- [SDR IPXA2023101988956](https://openairdocs.org/sdr/IPXA2023101988956), Oct 18, 2023: DOOR SEAL. DAMAGED. LOUD SQUEAL COMING FROM ENTRY DOOR. APPARENTLY FROM BOTTOM SEAL. STARTED CLIMBING ABOVE. 280. REPAIRED MAIN ENTRY DOOR LOWER SEAL PER AMM 52-09-00/801. OPEN
- [SDR IPXA2023091573158](https://openairdocs.org/sdr/IPXA2023091573158), Sep 15, 2023: BATTERY. INOPERATIVE. EMER LIGHTS INOP REPLACED EMER LIGHTS BATTERY PACK AND OPS TESTED NORMAL PER AMM 33-51-07/201
- [SDR IPXA2022032980632](https://openairdocs.org/sdr/IPXA2022032980632), Mar 22, 2022: SKIN. CRACKED. INSPECTION TYPE:C5CRACK ON FUSELAGE SKIN (P/N:148T3121-2) ON STA 1725.5 , NEAR S-7R.REPAIR I.A.W 767-300F SRM 53-80-01-2R REPAIR 5, REV 82.01.
- [SDR IPXA2020042054395](https://openairdocs.org/sdr/IPXA2020042054395), Apr 19, 2020: CHECK VALVE. FAULTY. INSPECTION TYPE:N/A** ATB ** AT FL 350 "LEFT PACK TEMP" EICAS MESSAGE. RAN "PACK TEMP" QRH CHECKLIST. "PACK TEMP" REMAINED LEFT PACK OFF.SAT COM FLIGHT CONTROL 
- [SDR IPXA2019090946488](https://openairdocs.org/sdr/IPXA2019090946488), Sep 8, 2019: DOOR SEAL. OUT OF POSITION. INSPECTION TYPE:N/A ENTRY DOOR HAS NOISE FROM AIR LEAK, PRESS SYSTEM NORMAL. FOUND 4 INCHES OF CREW ENTRY DOOR SEAL TO HAVE COME OUT OF TRACK. REINSTALLED CREW 
- [SDR IPXA2019090346298](https://openairdocs.org/sdr/IPXA2019090346298), Aug 30, 2019: DOOR. NOISE. INSPECTION TYPE:N/A AT APPROX 10000 FEET ON DEPARTURE LOUD HISSING SOUND COMING FROM ENTRY DOOR. PERFORMED ZONAL CHECK IAW AMM 52-12-00/601, CHECK SEALS IAW AMM
- [SDR IPXA2019080214206](https://openairdocs.org/sdr/IPXA2019080214206), Jul 31, 2019: SEAL. DIRTY. LT FWD ENTRY DOOR HAS NOISE FROM AIR LEAK, BOTTOM SEAL. CLEANED THE DOOR SILL AND SEAL AREA WHERE CREW REPORTED AIR LEAK. NO TEARS IN SEAL FOUND. OK FOR SERVICE
- [SDR IPXA2018122647218](https://openairdocs.org/sdr/IPXA2018122647218), Dec 21, 2018: SEAL. OUT OF POSITION. CREW ENTRY DOOR HAS LOUD NOISE FROM AN AIR LEAK AT FL 340, PRESSURE 8.4 RATE, ZERO AT LEVEL FLIGHT CABIN ALTITYUDE 5100 FEET. CABIN ALTITUDE AND PRESSURE OK THR
- [SDR IPXA2018030827235](https://openairdocs.org/sdr/IPXA2018030827235), Feb 25, 2018: FLOOR PANEL. DAMAGED. INSPECTION TYPE: C3, DAMAGE ON THE M/D CARGO FLOOR PANEL AT BS 287 - 412, RBL 33 - 54.75. FABRICATED A REPLACEMENT FLOOR PANEL IAW EO B767-5320-9693-I.
- [SDR IPXA2017091921871](https://openairdocs.org/sdr/IPXA2017091921871), Sep 18, 2017: TRU. FAILED. APU WILL NOT START. TROUBLESHOT THE APU. FOUND FAULTY APU TRANSFORMER RECTIFIER UNIT IAW FIM 49-11-00-815-807-001, BLOCK 2. APU NOW OPERATIVE.
- [SDR IPXA2017082120798](https://openairdocs.org/sdr/IPXA2017082120798), Aug 21, 2017: A/C PACK. ODOR. FUMES DURING TAKEOFF AND CLIMBOUT. ISOLATED PROBLEM TO THE RIGHT PACK. ENGINE RUN PERFORMED IAW MM 71-00-00-2. NO SIGNS OF OIL LEAKS OR BLEED SYS CONTAMINATION.
- [SDR IPXA2017081520585](https://openairdocs.org/sdr/IPXA2017081520585), Aug 15, 2017: SPRING. BROKEN. SPRING ON EMERGENCY EXIT LIGHT SWITCH BROKEN. R & R SWITCH GUARD IAW AMM 33-51-00, REV 121.02.
- [SDR IPXA2017041216076](https://openairdocs.org/sdr/IPXA2017041216076), Apr 11, 2017: DOOR SEAL. OUT OF POSITION. CREW ENTRY DOOR LEAKS ALONG FLOOR, BEGAN AT FL150 & CONTINUED ENROUTE. T/S PERF ACC FIM 52-12-04-00 REV 120.02. FOUND DOOR SEAL 4" OUT OF ITS RAIL. RESEATED DOO
- [SDR IPXA2014010801213](https://openairdocs.org/sdr/IPXA2014010801213), Jan 6, 2014: FLOOR PANEL. DAMAGED. MAIN CARGO DECK FLOOR PANEL DAMAGED. FABRICATED NEW FLOOR PANEL IAW EOB767-5320-53058-A.
- [SDR IPXA3678744](https://openairdocs.org/sdr/IPXA3678744), Jun 9, 2013: FLOORBOARD. DAMAGED. NR 9R FLOORBOARD DENTED AND HAS A HOLE. FABRICATED NEW FLOORBOARD IAW EO B767-5320-9693-H.
- [SDR IPXA3678563](https://openairdocs.org/sdr/IPXA3678563), May 27, 2013: SKIN. DENTED. L/E SLAT NR 12 HAS A SMALL DENT AT THE INBD UPPER EDGE OF THE T/E WEDGE. REPAIRED IAW SRM 57-43-02
- [SDR IPXA12675605](https://openairdocs.org/sdr/IPXA12675605), Sep 30, 2012: FLOOR PANEL. DAMAGED. SMALL HOLE IN FLOOR PANEL 4R. FABRICATED FLOOR PANEL IAW EO B767-5320-9693H AND REPLACED.
- [SDR IPXA2675048](https://openairdocs.org/sdr/IPXA2675048), Aug 23, 2012: DOOR. OUT OF SEQUENCE. CREW ENTRY DOOR OUT OF SEQUENCE, DOOR WILL NOT OPEN. PUT CEILING PANEL AND DOOR BACK IN SEQUENCE IAW AMM 52-12-34-404-014 OPS CHECKED GOOD.
- [SDR IPXA2673995](https://openairdocs.org/sdr/IPXA2673995), Jun 14, 2012: MODULE. INOPERATIVE. GEAR RAISED AFTER TAKE OFF. GEAR NOT DOWN EICAS WARNING AND CONFIGUATION LIGHT ILLUMINATED. GEAR INDICATED UP WITH ALL GEAR DOOR LIGHTS AND GEAR LIGHTS EXTINGUI

## Service difficulty reports on N349UP not matched to an aircraft (1)

They name N349UP, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft.

- [SDR IPXA1669048](https://openairdocs.org/sdr/IPXA1669048), Sep 4, 2011: FLOOR PANEL. DAMAGED. FLOOR PANEL POS2 CTR HAS .5 INCH HOLE. FABRICATED FLOOR PANEL IAW EO B767-5320-9693-H AND REPLACED.

## 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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