# N339UP: 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: 37859
- Year built: 2010
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: April 27, 2010
- Certificate issued: April 29, 2010
- Expires: February 28, 2030
- Mode S code: A3B90E
- Registered owner: [Cc & E I LLC](https://openairdocs.org/faa-owner/CC%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=339UP
- Page: https://openairdocs.org/aircraft/N339UP

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 N339UP.

## FAA accident and incident reports

None matched to N339UP.

## Service difficulty reports (56, 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 IPXA2026020384940](https://openairdocs.org/sdr/IPXA2026020384940), Jan 20, 2026: FLOOR PANEL. CORRODED. FOUND MAIN DECK FLOOR PANEL CORRODED, BS 1601, RBL 33. INSTALLED FLOOR PANEL IAW AMM 20-11-00-910-802, REV 147.
- [SDR IPXA2026020385077](https://openairdocs.org/sdr/IPXA2026020385077), Jan 20, 2026: CARGO TRACK. CORRODED. FOUND MAIN DECK CARGO TRACK CORRODED, BS 1601, RBL 11 IN THE AFT BULK CARGO BAY. . INSTALLED FABRICATED CARGO TRACK IAW SRM 51-40-02-0G.
- [SDR IPXA2025080729838](https://openairdocs.org/sdr/IPXA2025080729838), Aug 6, 2025: FCE. FAULTED. AIR TURN BACK, LE SLAT DISAGREE. PERFORMED FSEU BITE PER FIM 27-51 FT 809. FOUND EXISTING FAULT MSG: LVR RVDT 2 MISRIG WITH FAULT CODE 27-51023. ALSO PREVIOUS L
- [SDR IPXA2024121958268](https://openairdocs.org/sdr/IPXA2024121958268), Dec 12, 2024: A/C PACK. ODOR. LEFT PACK IS DISCHARGING FOULSMELL. DEBRIEFED INBOUND CREW, REPORTING FOUL SMELL NOT BEING PRESENT ON GROUND OR FLIGHT. NO OIL/GLYCOL CONTAMINATION FOUND, REACT
- [SDR IPXA2024072611426](https://openairdocs.org/sdr/IPXA2024072611426), Jul 26, 2024: WARNING MESSAGE. FALSE ACTIVATION. **EMERGENCY DECLARED**ON FINAL APPROACH, WHEN ON G/S, SELECTED FLAPS 20 DG, TE FLAP DISAGREE EICAS MESSAGE SPEED 180KTS, ALT 3500-. PERFORMED GA, RAN THE QRH PR
- [SDR IPXA2024013128494](https://openairdocs.org/sdr/IPXA2024013128494), Jan 19, 2024: SKIN. DEBONDED. FAULT - DISBOND SKIN, LH WING LE NO.4 SLAT INBD TE CORNER. (REPAIR) C/W REVIEW. ADJUSTMENT AND OPERATIONAL TEST OF THE LH WING NO.4 SLAT. I.A.W AMM 27-88-01-722
- [SDR IPXA2024013128280](https://openairdocs.org/sdr/IPXA2024013128280), Jan 19, 2024: RIB. CRACKED. FAULT - CRACK - RIB, NO.1 PYLON INSIDE OF MID TORQUE BOX SUPPORT, CAN ACCESS FROM PANEL #436AL (REPLACE) C/W REVIEW REMOVED DAMAGE PART I.A.W SRM 51-40-02-0G RE
- [SDR IPXA2024013128251](https://openairdocs.org/sdr/IPXA2024013128251), Jan 19, 2024: ACCESS PANEL. CRACKED. FAULT - CRACK - RIB, NO.1 PYLON INSIDE OF MID TORQUE BOX SUPPORT, CAN ACCESS FROM PANEL #436AR (REPLACE) REVIEWED REMOVED DAMAGE PARTS I.A.W SRM 51-40-02-0G REV
- [SDR IPXA2024013128068](https://openairdocs.org/sdr/IPXA2024013128068), Jan 19, 2024: PANEL. CRACKED. FAULT - CRACK PNL, LH WING NO.4 SLAT LOWER CLOSEOUT PNL UNDER OUTBD AUX TRACK. (REPAIR) REVIEWED REMOVED CLOSURE PANEL AT NO.4 SLAT I.A.W SRM 51-40-02-0G REV.88
- [SDR IPXA2024012228068](https://openairdocs.org/sdr/IPXA2024012228068), Jan 19, 2024: PANEL. DAMAGED. *SDR FILED OPEN* FAULT - CRACK PNL, LH WING NO.4 SLAT LOWER CLOSEOUT PNL UNDER OUTBD AUX TRACK. (REPAIR) PER B767 NDT MANUAL PART 1, 51-01-01 & PART 4, 51-00-02
- [SDR IPXA2024012228251](https://openairdocs.org/sdr/IPXA2024012228251), Jan 19, 2024: SUPPORT. CRACKED. *SDR FILED OPEN* FAULT - CRACK - RIB, NO.1 PYLON INSIDE OF MID TORQUE BOX SUPPORT, CAN ACCESS FROM PANEL #436AR (REPLACE) OK TO WORK
- [SDR IPXA2024012228494](https://openairdocs.org/sdr/IPXA2024012228494), Jan 19, 2024: SKIN. DEBONDED. *SDR FILED OPEN* *MAJOR REPAIR* FAULT - DISBOND SKIN, LH WING LE NO.4 SLAT INBD TE CORNER. (REPAIR) 1.OK TO INSTALL CHECK SATISFIED.<BR>2.I.A.W. AMM 27-81-02-42
- [SDR IPXA2024012228280](https://openairdocs.org/sdr/IPXA2024012228280), Jan 19, 2024: SUPPORT. CRACKED. *SDR FILED OPEN* FAULT - CRACK - RIB, NO.1 PYLON INSIDE OF MID TORQUE BOX SUPPORT, CAN ACCESS FROM PANEL #436AL (REPLACE) OK TO WORK
- [SDR IPXA2024012227720](https://openairdocs.org/sdr/IPXA2024012227720), Jan 19, 2024: CAP. CRACKED. FAULT - CRACK, LH WING OUTBD FLAP END CAP. (REPAIR). PERFORMED NDT/UT FOR REWORKED AREA PLUS 6'' AROUND HEATED AREA I.A.W. 767 NTM PART1 51-01-01 REV:136. RESUL
- [SDR IPXA2024012227663](https://openairdocs.org/sdr/IPXA2024012227663), Jan 19, 2024: SKIN. DAMAGED. FAULT - CHIP SKIN, LH WING INBD MAIN FLAP OUTBD UPR SEAL LE AREA. (REPAIR). 1. REMOVE THE UNWANTED MATERIALS AND CLEAN AT LEFT HAND WING INBOARD MAIN FLAP OUTBO
- [SDR IPXA2024013145304](https://openairdocs.org/sdr/IPXA2024013145304), Jan 16, 2024: LINER. MISSING. **SUPPLEMENTAL SDR**FAULT - FOUND ENTRY DOOR FORWARD DOORWAY LINING TRIM MISSING (REPLACE) C/W REVIEW INSTALLED NEW DOOR LINING I.A.W AMM 52-12-02-004-001
- [SDR IPXA2024011745304](https://openairdocs.org/sdr/IPXA2024011745304), Jan 16, 2024: LINER. UNKNOWN. FOUND ENTRY DOOR FORWARD DOORWAY LINING TRIM MISSING (REPLACE) OK TO WORK
- [SDR IPXA2024011636099](https://openairdocs.org/sdr/IPXA2024011636099), Jan 15, 2024: STIFFENER. CRACKED. FAULT - CRACK WING CENTER TANK FRONT SPAR STIFFENER AT STA 785.9 RBL 11 (REPAIR) THIS REPAIR IS CLASSIFIED AS MAJOR. ACCOMPLISH THE REPAIR PER SRM 57-10-10-2R-2
- [SDR IPXA2023071059404](https://openairdocs.org/sdr/IPXA2023071059404), Jul 9, 2023: ESCAPE ROPE. LOOSE. CAPT SIDE EMERGENCY ESCAPE ROPE CHASE PANEL IS LOOSE FIXED PER AMM 25-61-02-201
- [SDR IPXA2022102487418](https://openairdocs.org/sdr/IPXA2022102487418), Oct 22, 2022: FAN. VIBRATION. ATB, DURING CLIMBOUT LEFT ENGINE N2 FAN VIBE DISPLAYED 5.0 WITH SIGNIFICANT VIBRATION AND NOISE ON FLIGHT DECK. CONFIRMED BIRDSTRIKE TO LEFT ENGINE. REF LOGPAGE
- [SDR IPXA2022022479365](https://openairdocs.org/sdr/IPXA2022022479365), Feb 18, 2022: STIFFENER. NONE. INSPECTION TYPE:C6CRACK ON CENTER WING TANK STIFFENER(P/N:111T2011-6) ON STA 785.9, RBL 55.REPAIR I.A.W 767-300F SRM 57-10-10-2R-2 REPAIR 2 REV.82.01 AND UPS EO
- [SDR IPXA2022022479364](https://openairdocs.org/sdr/IPXA2022022479364), Feb 18, 2022: FLOOR PANEL. NONE. INSPECTION TYPE:C6DAMAGE ON M/D CARGO FLOOR PANEL AT STA 850, RBL 11-LBL11.FABRICATE THE REPLACEMENT FLOOR PANEL PER EO NO. B767-5320-9693-I
- [SDR IPXA2021102975440](https://openairdocs.org/sdr/IPXA2021102975440), Oct 29, 2021: SEAL. NONE. INSPECTION TYPE:NACLIMBING OUT OF FL200 A VERY LOUD HISSING SOUND CAME FROM NEAR FWD ENTRY DOOR. SOUND REMAINED CONSTANT. NO PRESSURIZATION ISSUES NOTED.FOUND D
- [SDR IPXA2021021765784](https://openairdocs.org/sdr/IPXA2021021765784), Feb 17, 2021: BATTERY PACK. INOPERATIVE. INSPECTION TYPE: NA EMERGENCY LTS INOP. REMOVED AND REPLACED EMERGENCY LT BATTERY PACK IAW MM 33-51-07 OPS CK NORMAL IPC 33-51-07-32 20J.
- [SDR IPXA2021012764978](https://openairdocs.org/sdr/IPXA2021012764978), Jan 26, 2021: RETAINER. DAMAGED. INSPECTION TYPE: N/A CLIMBING THRU 17000FT A VERY LOUD POP WAS HEARD, FOLLOWED BY LOUD HISSING SOUND COMING FROM THE BOTTOM OF MAIN CABIN DOOR. CABIN ALT REMAIN
- [SDR IPXA2020120863218](https://openairdocs.org/sdr/IPXA2020120863218), Dec 7, 2020: TRANSMITTER. MALFUNCTIONED. INSPECTION TYPE: NA, EMERGENCY DECLARED-NO EQUIPMENT USED. TRAILING EDGE DISAGREE ON APPROACH WHEN SELECTING FLAPS 5 DEG TO 20 DEG. QRH PROCEDURE COMPLETED. TRA
- [SDR IPXA2020102261573](https://openairdocs.org/sdr/IPXA2020102261573), Oct 20, 2020: WARNING MESSAGE. ILLUMINATED. INSPECTION TYPE: N/A ATB EMERGENCY DECLARED. LANDING UNEVENTFUL. CLIMBING OUT AT 11000 CABIN ALTITUDE HORN, LIGHT AND EICAS MESSAGE THEN CABIN ALTITUDE AUTO AND
- [SDR IPXA2020051155128](https://openairdocs.org/sdr/IPXA2020051155128), May 10, 2020: SKIN. DAMAGED. INSPECTION TYPE:N/ALH WING INBOARRD AILERON LOWER SKIN DAMAGE RE: EO B767-5750-76127-B. NON-BALANCED SURFACE PER ENGINEERING.SANDED DAMAGED AREAS. REMOVED DAMAG
- [SDR IPXA2020051055129](https://openairdocs.org/sdr/IPXA2020051055129), May 10, 2020: SKIN. DAMAGED. INSPECTION TYPE:N/A **SUPPLEMENTAL SDR** (CLOSED) LEFT WING INBOARD AILERON LOWER SKIN DAMAGE. THIS IS A MAJOR REPAIR TRANSFERRED TO NON-ROUTINE CARD # 663200 D
- [SDR IPXA2018121756948](https://openairdocs.org/sdr/IPXA2018121756948), Dec 15, 2018: CONTROL PANEL. INOPERATIVE. EMERGENCY LIGHTS BACK GROUND PLATE LIGHTS INOPERATIVE. R & R EMERGENCY LIGHTS CONTROL PANEL IAW MM 33-51-08-4, OPS CHECKED GOOD.
- [SDR IPXA2018121737001](https://openairdocs.org/sdr/IPXA2018121737001), Dec 11, 2018: CONTROL PANEL. INOPERATIVE. EMERGENCY LIGHTS SWITCH BACKLIGHTS INOP. R&R EMER LIGHTS CONTROL PANEL IAW MM 31-51-08-4. OPS CK GOOD.
- [SDR IPXA2018022126729](https://openairdocs.org/sdr/IPXA2018022126729), Feb 4, 2018: SKIN. DENTED. INSPECTION TYPE: C4, SKIN DENTED BS 451, STRINGER 25 - 26R. REPAIRED IAW SRID 3-4105366013 AND EO B767-5330-67377-A.
- [SDR IPXA2017012113040](https://openairdocs.org/sdr/IPXA2017012113040), Jan 21, 2017: PBE. CONTAMINATED. COCKPIT PBE MOISTURE INDICATOR SHOWS WHITE. REMOVED AND REPLACED THE PBE. SECURED IN HOLDER.
- [SDR IPXA2017010912538](https://openairdocs.org/sdr/IPXA2017010912538), Jan 7, 2017: COVER. BROKEN. CREW ENTRY DOOR ARMING LEVER HINGE COVER MISSING HINGE IS BROKEN. R&R HINGE COVER ASSY IAW AMM 20-00-00.
- [SDR IPXA2016041101942](https://openairdocs.org/sdr/IPXA2016041101942), Apr 11, 2016: FLOOR PANEL. DAMAGED. MAIN CARGO DECK FLOOR PANEL POSITION 8L HAS A DAMAGE TO UPPER SKIN. REPAIRED IAW EO B767-5320-9693-I
- [SDR IPXA2016041101943](https://openairdocs.org/sdr/IPXA2016041101943), Apr 11, 2016: FLOOR PANEL. DAMAGED. FLOOR PANEL 5/5 RT HAS DAMAGE UPPER SKIN. REPAIRED IAW EO B767-5320-9693-I.
- [SDR IPXA2016041001900](https://openairdocs.org/sdr/IPXA2016041001900), Apr 10, 2016: FLOOR PANEL. DENTED. FLOOR PANEL 12L DENT APPROXIMATELY 1", LOCATION 8" FROM EDGE. REPAIRED IAW SRM 53-00-50-2R, REV 64.
- [SDR IPXA2015060689894](https://openairdocs.org/sdr/IPXA2015060689894), Jun 6, 2015: COVER PLATE. MALFUNCTIONED. MAIN ENTRY ARMING HINGE COVER WILL NOT STOW. BLOCKING EGRESS. R & R COVER IAW SRM 51-40-02.
- [SDR IPXA2015050288543](https://openairdocs.org/sdr/IPXA2015050288543), May 1, 2015: BLOWER. INOPERATIVE. CAPTAINS EVAS BLOWER DOES NOT RUN WITH TEST TOOL REF TC 25-069-00. R & R CAPTAINS EVAS AMM 25-69-00-000-801C3, 25-60-00-400-801C3 TESTS NORMAL IAW TC 25-069-00,
- [SDR IPXA2015042688390](https://openairdocs.org/sdr/IPXA2015042688390), Apr 26, 2015: FLOOR PANEL. PUNCTURED. MAIN CARGO DECK FLOOR PANEL, PN 141T5856-13 HAS MULTIPLE DAMAGES TO UPPER SKIN AND PANEL EDGE FABRICATED REPLACEMENT PANEL IAW EO B767-5320-9693H.
- [SDR IPXA2015021685969](https://openairdocs.org/sdr/IPXA2015021685969), Feb 13, 2015: SHUTOFF VALVE. INOPERATIVE. INSPECTION TYPE: E, TOP WAN NR 2253636, ACCOMPLISHED SEE LP 823263, ITEM 2.
- [SDR IPXA2014102784720](https://openairdocs.org/sdr/IPXA2014102784720), Oct 26, 2014: PLACARD. DETERIORATED. F/O EMERGENCY EXIT PULL PLACARD IS DETERIORATED. R & R THE PLACARD IAW AMM 20-10-12.
- [SDR IPXA2014061383290](https://openairdocs.org/sdr/IPXA2014061383290), Jun 12, 2014: FLAP SYSTEM. FALSE INDICATION. EMERGENCY DECLARED, FLAPS INDICATE SPLIT WITHOUT EICAS MESSAGE. CYCLED CIRCUIT BREAKER , INDICATOR NORMAL. OPS FLAPS IAW MM 27-51-00-201 WITHOUT PROBLEMS NO IND
- [SDR IPXA2014060283176](https://openairdocs.org/sdr/IPXA2014060283176), May 31, 2014: POWER SUPPLY. INOPERATIVE. EMERGENCY LIGHTS POWER SUPPLY INOPERATIVE. REPLACED EMERGENCY LIGHTS POWER SUPPLY WRT 33-51-07. OPS CHECKED OK.
- [SDR IPXA2014060283175](https://openairdocs.org/sdr/IPXA2014060283175), May 31, 2014: LAMP. INOPERATIVE. EMERGENCY LIGHT ON LT SIDE FUSELAGE INOPERATIVE. REPLACED LAMP. OPS CHECKED OK IAW MM 33-51-16.
- [SDR IPXA2013122301111](https://openairdocs.org/sdr/IPXA2013122301111), Dec 21, 2013: TRANSMITTER. INOPERATIVE. AIR TURNBACK DUE TO FLAP ASSEMETRY INDICATION. LT T/E FLAP INDICATOR STAYED AT 15 DEGREES AND THE RT WENT TO 5 DEGREES. DETERMINED THAT THE FLAP SPLIT WAS INDIC
- [SDR IPXA2672256](https://openairdocs.org/sdr/IPXA2672256), Mar 12, 2012: FLOOR PANEL. BROKEN. INSPECTION TYPE: C, MAIN DECK FLOOR PANEL NR 241AFF BROKEN AT BS 761, RBL 1. L X W=1"X1" ON UPPER SKIN AND CORE;L X W=1.2"X1" ON LOWER SKIN CUT OUT THE DAMAGE A
- [SDR IPXA2672231](https://openairdocs.org/sdr/IPXA2672231), Mar 7, 2012: WEDGE. DAMAGED. INSPECTION TYPE: C, LEFT WING OTBD T/E FLAP HAS PUNCTURE (2"X1")ON L/E. LOCATED 2' OTBD OF INBD EDGE ON THE L/E. REMOVE THE EXISTING INTERIM REPAIR FOR SIZE L X
- [SDR IPXA2672230](https://openairdocs.org/sdr/IPXA2672230), Mar 7, 2012: SKIN. DENTED. INSPECTION TYPE: C, DENTED SKIN, LT WING OTBD FLAP LOWER SKIN DENTS AT OTEF STA 250 AND OTEF STA 263.5. DENT WITH DELAMINATION DIMENSION L X W X D=2.2"X2.1"X0.0
- [SDR IPXA1669044](https://openairdocs.org/sdr/IPXA1669044), Sep 4, 2011: FLOORBOARD. DAMAGED. INSPECTION TYPE:MX POS 4 FLOORBOARD MCD CENTER INTERIM REPAIR 2 INCH HOLES 16 INCHES AFT OF CENTERLINE IDENTIFIED PANEL FROM POSITION 4. PN 143T5876-98 IAW EO B

All 56: https://openairdocs.org/aircraft/N339UP/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

---
OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.