# N315UP: 1996 Boeing 767-34AF

- Status: Valid registration
- Airframe: [Boeing 767-34AF](https://openairdocs.org/model/boeing-767-34af) (registry code 1385212, 190 seats)
- Engine: [GE CF6-80 series](https://openairdocs.org/engine/ge-cf6-80-series) (registry code 30025)
- Data sheets: [TCDS E13NE](https://openairdocs.org/tcds/E13NE) (General Electric Company GE Aerospace) (OpenAirDocs)
- Serial number: 27743
- Year built: 1996
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: December 12, 1996
- Certificate issued: December 15, 2008
- Expires: February 28, 2029
- Mode S code: A35B34
- 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=315UP
- Page: https://openairdocs.org/aircraft/N315UP

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. The registry lists only the engine series, so ADs for every GE CF6-80 model are included.

## ADs that may apply (OpenAirDocs): 61 in force

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

None in force.

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

- [AD 2024-24-03](https://openairdocs.org/ad/2024-24-03): Engine Exhaust · Boeing MD-11, MD-11F and CF6-80C2D1F. Effective Jan 13, 2025
- [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 2022-02-18](https://openairdocs.org/ad/2022-02-18): Engine Mount Section · General Electric CF6-80C2A1, CF6-80C2A2, CF6-80C2A3 and 3 more. Effective Feb 25, 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 2018-07-05](https://openairdocs.org/ad/2018-07-05): Turbine Section · General Electric CF6-80A, CF6-80A1, CF6-80A2 and 1 more. Effective May 11, 2018
- [AD 2017-11-15](https://openairdocs.org/ad/2017-11-15): Turbine/ Turboprop Engine--Turbine Section · General Electric CF6-80C2L1F. Effective Jul 13, 2017
- [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 2011-23-04](https://openairdocs.org/ad/2011-23-04): Forward engine mount assembly side links · General Electric CF6-45A, CF6-45A2, CF6-50A and 14 more. Effective Dec 12, 2011
- [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 2009-14-08](https://openairdocs.org/ad/2009-14-08): High-pressure compressor rotor (HPCR) stages 11-14 spool/ shafts · General Electric CF6-80C2B5F. Effective Aug 5, 2009
- [AD 2009-08-06](https://openairdocs.org/ad/2009-08-06): Stage 1 high-pressure turbine (HPT) rotor  
 disks · General Electric CF6-80A, CF6-80A1, CF6-80A2 and 1 more. Effective May 18, 2009
- [AD 2009-07-10](https://openairdocs.org/ad/2009-07-10): High-pressure turbine rotor (HPTR) · General Electric CF6-80A, CF6-80A1, CF6-80A2 and 1 more. Effective May 6, 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 2008-02-17](https://openairdocs.org/ad/2008-02-17): Thrust reverser actuation systems · General Electric CF6-50A, CF6-50C, CF6-50C1 and 16 more. Effective Feb 28, 2008
- [AD 2007-24-07](https://openairdocs.org/ad/2007-24-07): Thermal spray coating on certain stage 1 fan disks · General Electric CF6-80C2B1. Effective Jan 2, 2008
- [AD 2007-22-07](https://openairdocs.org/ad/2007-22-07): Electronic control unit (ECU) · General Electric CF6-80C2D1F. Effective Nov 28, 2007
- [AD 2007-21-06](https://openairdocs.org/ad/2007-21-06): Electronic control unit (ECU) · General Electric CF6-80C2A5F. Effective Nov 15, 2007
- [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 2006-06-08](https://openairdocs.org/ad/2006-06-08): Latching system of the fan reverser · General Electric CF6-80C2D1F. Effective Apr 25, 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 2005-06-07](https://openairdocs.org/ad/2005-06-07): Directional pilot valve (DPV) assembly · General Electric CF6-80A1, CF6-80A3, CF6-80C2A1 and 5 more. Effective Apr 25, 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 2004-07-13](https://openairdocs.org/ad/2004-07-13): High pressure turbine (HPT) stage 1 disks · General Electric CF6-80C2A5F, CF6-80C2B5F, CF6-80C2B7F and 1 more. Effective May 6, 2004
- [AD 2003-12-08](https://openairdocs.org/ad/2003-12-08): Directional pilot valve · General Electric CF6-80A1, CF6-80A3, CF6-80C2A1 and 5 more. Effective Jul 23, 2003
- [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 2001-06-09](https://openairdocs.org/ad/2001-06-09): Aft Engine Mount Link Assemblies · General Electric CF6-80A3. Effective May 1, 2001
- [AD 2000-12-08](https://openairdocs.org/ad/2000-12-08): Mount Link Assemblies · General Electric CF6-80C2A1, CF6-80C2A2, CF6-80C2A3 and 4 more. Effective Aug 28, 2000
- [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 95-17-16](https://openairdocs.org/ad/95-17-16): Compressor Rear Frame · General Electric CF6-80A, CF6-80A1, CF6-80A2 and 1 more. Effective Nov 7, 1995
- [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 94-07-04](https://openairdocs.org/ad/94-07-04): High Pressure Turbine Disk · General Electric CF6-80A, CF6-80A1, CF6-80A2 and 1 more. Effective May 23, 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

### 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 2006-12-24](https://openairdocs.org/ad/2006-12-24) (historical): Five-link forward mount assembly · General Electric CF6-45A, CF6-45A2, CF6-50A and 14 more. Effective Jul 21, 2006
- [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 2003-01-05](https://openairdocs.org/ad/2003-01-05) (historical): Dovetail slots · General Electric CF6-80A, CF6-80A1, CF6-80A2 and 1 more. Effective Jan 28, 2003
- [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 2000-08-12](https://openairdocs.org/ad/2000-08-12) (historical): Life-limited Parts · General Electric CF6-80A, CF6-80A1, CF6-80A2 and 10 more. Effective Oct 23, 2000
- [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 99-18-20](https://openairdocs.org/ad/99-18-20) (historical): Inadvertent In-flight Thrust Reverser · General Electric Aircraft Engines CF6-50 Series (all), CF6-80A1, CF6-80A3 and 6 more. Effective Nov 2, 1999
- [AD 99-18-19](https://openairdocs.org/ad/99-18-19) (historical): Inadvertent Thrust Reverser · General Electric CF6-80A, CF6-80A1, CF6-80A2 and 7 more. Effective Sep 24, 1999
- [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 98-15-17](https://openairdocs.org/ad/98-15-17) (historical): Link Assembly · General Electric CF6-80A3. Effective Aug 7, 1998
- [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

All 80: https://openairdocs.org/aircraft/N315UP/ads.md

## Information bulletins (advisory) (5 in force)

- [SAIB 2023-15](https://openairdocs.org/saib/2023-15): Falsified Forms from AOG Technics. Issued Dec 19, 2023
- [SAIB NE-11-27](https://openairdocs.org/saib/NE-11-27): Fuel Injector Nozzle - CF6-80 Improperly Welded Fuel Nozzles. Issued Apr 5, 2011
- [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 N315UP.

## FAA accident and incident reports

None matched to N315UP.

## Service difficulty reports (144, 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 IPXA2026081225594](https://openairdocs.org/sdr/IPXA2026081225594), Aug 11, 2026: LIFE VEST. EXPIRED. FLT DECK RT SUPERNUMERARY SEAT CREW LIFE VEST EXPIRED. REMOVED AND REPLACED RT SUPERNUMERARY SEAT CREW LIFE VEST PER AMM 25-62-00.
- [SDR IPXA2026060515616](https://openairdocs.org/sdr/IPXA2026060515616), Jun 4, 2026: SENSOR. FAULTED. AIR TURN BACK, EMERGENCY DECLARED, PASSING FL200 ON DEPARTURE LT ENG OIL TEMP CLIMBED INTO AMBER RANGE (HIGH AS 164) RUN QRH AND OIL TEMP SLOWLY RETURNED TO SAM
- [SDR IPXA2026031892051](https://openairdocs.org/sdr/IPXA2026031892051), Mar 16, 2026: A/C PACK. ODOR. STRONG LOCKER ROOM SMELL AFTER TAKE-OFF. ISOLATING RIGHT PACK SEEMED TO CAUSE SMELL TO DISAPPEAR IE RIGHT PACK OFF. ACCOMPLISHED ENGINE IDLE RUN IAW AMM 71-00-0
- [SDR IPXA2026031692051](https://openairdocs.org/sdr/IPXA2026031692051), Mar 16, 2026: A/C PACK. ODOR. STRONG LOCKER ROOM SMELL AFTER TAKE-OFF. ISOLATING RIGHT PACK SEEMED TO CAUSE SMELL TO DISAPPEAR IE RIGHT PACK OFF. FURTHER TROUBLE SHOOTING REQUIRED. RIGHT AIR
- [SDR IPXA2025071363969](https://openairdocs.org/sdr/IPXA2025071363969), Mar 14, 2025: SKIN. DAMAGED. EVIDENCE OF LIGHTNING STRIKE ON RUDDER R/H SIDE TRAILING EDGE AT APPROXIMATELY RUDDER STATION 255. PERMANENT REPAIR COMPLIED WITH PER EO-93077-REQ3. DEFERRAL RE
- [SDR IPXA2025012814198](https://openairdocs.org/sdr/IPXA2025012814198), Jan 27, 2025: DOOR. LEAKING. AIR LEAK COMING FROM L2 LOWER LEFT HAND CORNER AT 390 FT CABIN ALT 6800 DIFF 8.4 ACCOMPLISHED PNEUMATIC LEAK TEST IAW MM 21-31-00-705-009. BROUGHT CABIN DIFFERE
- [SDR IPXA2024061326915](https://openairdocs.org/sdr/IPXA2024061326915), Jun 13, 2024: FMC. INOPERATIVE. **DIVERSION** BOTH FMC€™S -> PUSHING NUMEROUS FUNCTION BUTTONS PULLS UP WRONG PAGE. REMOVED AND REPLACED F/O FMC IAW AMM 34-61-02. OPS CHECK GOOD.
- [SDR IPXA2024020267014](https://openairdocs.org/sdr/IPXA2024020267014), Feb 2, 2024: FLOOR PANEL. CRACKED. FOUND MAIN DECK CARGO FLOOR PANEL CRACK AT STA 1432-1520, LBL 55 - LBL 77.5, P/N: 146T5869-43 (REPAIR) IAW AMM 53-01-06-400-801 REV.141 INSTALL MAIN DECK CARGO 
- [SDR IPXA2024020320072](https://openairdocs.org/sdr/IPXA2024020320072), Jan 31, 2024: FLOOR PANEL. CRACKED. MAJOR REPAIR, FOUND MAIN DECK CARGO FLOOR PANEL CRACK AT STA 1432 ~ 1520, LBL55~ LBL77.5, P/N:146T5869-89 (REPLACE) REMOVE MAIN DECK CARGO FLOOR PANEL AREA SEAL
- [SDR IPXA2024022083876](https://openairdocs.org/sdr/IPXA2024022083876), Jan 29, 2024: HINGE. DEFORMED. FOUND MAIN ENTRY DOOR DOORWAY ARMING LEVER HINGE ASSY DEFORM. REPLACED HINGE ASSY I.A.W AMM 20-11-00-910-802 REV.141.
- [SDR IPXA2024022083857](https://openairdocs.org/sdr/IPXA2024022083857), Jan 29, 2024: SPLINE. BROKEN. FOUND MAIN ENTRY DOOR DOORWAY SPLINE TRIM BROKEN. REPLACED DOORWAY SPLINE TRIM I.A.W AMM 52-12-02-004-001 REV.141 AND AMM 52-12-02-404-025 REV.141.
- [SDR IPXA2024012983876](https://openairdocs.org/sdr/IPXA2024012983876), Jan 29, 2024: HINGE. DEFORMED. FAULT - FOUND MAIN ENTRY DOOR DOORWAY ARMING LEVER HINGE ASSY DEFORM (REPLACE)
- [SDR IPXA2024012983857](https://openairdocs.org/sdr/IPXA2024012983857), Jan 29, 2024: TRIM PANEL. BROKEN. FAULT - FOUND MAIN ENTRY DOOR DOORWAY SPLINE TRIM BROKEN (REPLACE)
- [SDR IPXA2023041754147](https://openairdocs.org/sdr/IPXA2023041754147), Apr 14, 2023: LIGHT. INOPERATIVE. *SDR FILED OPEN* EXTERNAL FUSELAGE EMERGENCY LIGHT BULB INOP RELAMPED EXTERNAL EMERGENCY LIGHT REF AMM 33-51-16. OPS CK OK.
- [SDR IPXA2022120988837](https://openairdocs.org/sdr/IPXA2022120988837), Dec 9, 2022: DOOR. OUT OF ADJUST. INSPECTION TYPE:NA**ATB** DURING CLIMB OUT EICAS MSG "FWD CARGO DOOR" AIR TURN BACK. DEFERRED FWD LWR CARGO DOOR IND PER MEL 52-71-1-1. C/W DMP 52-71-1-1 FWD LW
- [SDR IPXA2022010777620](https://openairdocs.org/sdr/IPXA2022010777620), Dec 28, 2021: NONE. NONE. INSPECTION TYPE:C13DISBOND DAMAGE (APPROX 7.0'' X 6'') ON R/H VST TORQUE BOX PANEL (P/N:175T2001-4) AT LWR AFT SIDEREPAIR I.A.W 767-300F SRM 55-30-01-2R-1 REV.8
- [SDR IPXA2022010577543](https://openairdocs.org/sdr/IPXA2022010577543), Dec 28, 2021: NONE. NONE. INSPECTION TYPE:C13DISBOND DAMAGE ON R/H VST TORQUE BOX PANEL (P/N:175T2001-4) AT LWR AFT SIDE.REPAIR I.A.W 767-300F SRM 55-30-01-2R-1 REV.82.01 AND 767-300F SR
- [SDR IPXA2022010577544](https://openairdocs.org/sdr/IPXA2022010577544), Dec 27, 2021: NONE. NONE. INSPECTION TYPE:C13DAMAGE ON M/D CARGO FLOOR PNL AT STA 287-STA412 , RBL 77 - RBL 88.FABRICATE THE REPLACEMENT FLOOR PNL PER EO NO. B767-5320-9693-I
- [SDR IPXA2020092860712](https://openairdocs.org/sdr/IPXA2020092860712), Sep 28, 2020: ATTACH ANGLE. CORRODED. INSPECTION TYPE: LDS CORROSION FOUND ON SUPPORT ANGLE AT FS 212-237, LBL 64.0 (FLIGHT DECK FLOOR). SUPPORT ANGLE AT FS 212-237, LBL 64.0 (FLIGHT DECK FLOOR) REP
- [SDR IPXA2020051355260](https://openairdocs.org/sdr/IPXA2020051355260), May 13, 2020: CONTROL PANEL. FAILED. INSPECTION TYPE:N/AWHEN SWITCH IS CLOSED FOR NORMAL POSITION OF FLIGHT THE SWITCH FUNCTION GOES TO "OFF" AND THE "DISARMED" LIGHT ILLUMINATES.REMOVED AND REPLAC
- [SDR IPXA2020020315646](https://openairdocs.org/sdr/IPXA2020020315646), Jan 18, 2020: STIFFENER. CRACKED. INSPECTION TYPE:C12CRACK ON CENTER WING TANK STIFFENER (P/N : 111T2011-5) ON STA 785.9 , LBL 55REPAIR I.A.W 767-300F SRM 57-10-10-2R-2 REPAIR 2 REV.76.01 , UPS 
- [SDR IPXA2020020315645](https://openairdocs.org/sdr/IPXA2020020315645), Jan 18, 2020: STIFFENER. CRACKED. INSPECTION TYPE:C12CRACK ON CENTER WING TANK STIFFENER (P/N : 111T2005-8) ON STA 785.9 , RBL 11REPAIR I.A.W 767-300F SRM 57-10-10-2R-2 REPAIR 2 REV.76.01 , UPS 
- [SDR IPXA2020020315644](https://openairdocs.org/sdr/IPXA2020020315644), Jan 18, 2020: STIFFENER. CRACKED. INSPECTION TYPE:C12CRACK ON CENTER WING TANK STIFFENER (P/N : 111T2008-12) ON STA 785.9 , RBL 33REPAIR I.A.W 767-300F SRM 57-10-10-2R-2 REPAIR 2 REV.76.01 UPS E
- [SDR IPXA2020020315643](https://openairdocs.org/sdr/IPXA2020020315643), Jan 18, 2020: STIFFENER. CRACKED. INSPECTION TYPE:C12CRACK ON CENTER WING TANK STIFFENER (P/N : 111T2008-11) ON STA 785.9 , LBL 33REPAIR I.AW 767-300F SRM 57-10-10-2R-2 REPAIR 2 REV.76.01 , UPS 
- [SDR IPXA2020020315641](https://openairdocs.org/sdr/IPXA2020020315641), Jan 18, 2020: STIFFENER. CRACKED. INSPECTION TYPE:C12CRACK ON CENTER WING TANK STIFFENER (P/N : 111T2011-6) ON STA 785.9 , RBL 55REPAIR I.A.W 767-300F SRM 57-10-10-2R-2 REPAIR 2 REV.76.01 , UPS 
- [SDR IPXA2020020311639](https://openairdocs.org/sdr/IPXA2020020311639), Jan 18, 2020: SKIN. CRACKED. INSPECTION TYPE:C12CRACK ON #10 SLAT L/E SKIN (P/N : 114T4103-4) NEAR OSS 724REPAIR I.A.W 767-300F SRM 57-43-01-2R-1 REV.76.01
- [SDR IPXA2020020311642](https://openairdocs.org/sdr/IPXA2020020311642), Jan 17, 2020: SKIN. CRACKED. INSPECTION TYPE:C12CRACK ON #2 PYLON INBD SKIN ASSY (P/N : 311T2450-23) NEAR NAC 240.50REPAIR I.A.W BOEING SRID : 3-4623448622 AND UPS EO B767-5430-75336-A
- [SDR IPXA201910147792](https://openairdocs.org/sdr/IPXA201910147792), Oct 11, 2019: CONTROL PANEL. MALFUNCTIONED. WHEN EXTERNAL POWER TURNED OFF IN COCKPIT EMERGENCY EXIT SIGNS & LIGHTS CAME ON WITH EMERGENCY LIGHT SWITCH TURNED OFF. R&R EMERGENCY EXIT OVERHEAD PANEL ON P11
- [SDR IPXA2019090646414](https://openairdocs.org/sdr/IPXA2019090646414), Sep 5, 2019: CONTROL PANEL. DEFECTIVE. INSPECTION TYPE:N/A EMER LITE CONTROL PANEL DISARMED LIGHT WILL NOT SNAP INTO LOCKED POSITIONREF MM 33 51 08. INSTALLED SERVICES ABLE PANEL ASSY OPS CHECK GOOD 
- [SDR IPXA2019070944260](https://openairdocs.org/sdr/IPXA2019070944260), Jul 6, 2019: TIRE. BLOWN. INSPECTION TYPE:N/A EMERGENCY DECLARED - #3 MAIN TIRE BLOWN ON TAKE OFF. REMOVED #3 MAIN TIRE INSPECTED AXLE AND #3 BRAKE ASSY NO DEFECTS NOTED INSTALLED (3) RE
- [SDR IPXA2018060830400](https://openairdocs.org/sdr/IPXA2018060830400), Jun 8, 2018: WINDOW. CRACKED. RIGHT FORWARD WINDOW CRACKED. REPLACED RT 1 WINDOW IAW AMM 56-11-01-404-017 REV 124.01. EFF REF IPC: 56-11-01-01A ITEM 015K REV 94.00.
- [SDR IPXA2018032627845](https://openairdocs.org/sdr/IPXA2018032627845), Mar 25, 2018: PANEL. DAMAGED. CREW ENTRY DOOR HANDLE PANEL DAMAGE. REMOVED AND REPLACED L1 EXTERIOR DOOR HANDLE PANEL MM 52-11-26-004-001, AND 52-12-25-00.
- [SDR IPXA2018020126081](https://openairdocs.org/sdr/IPXA2018020126081), Jan 21, 2018: TEE FITTING. CRACKED. INSPECTION TYPE: C11, CRACK FOUND ON THE NOSE W/W AFT BULKHEAD VERTICAL TEE, BS 287 , RBL 25 , WL 173. REPAIRED IAW EO B767-5310-20118-F, AND SRM 51-70-12, FIGU
- [SDR IPXA2018020126077](https://openairdocs.org/sdr/IPXA2018020126077), Jan 21, 2018: FLOOR PANEL. DAMAGED. INSPECTION TYPE: C11, DAMAGE ON THE MAIN DECK CARGO FLOOR PANEL, BS 972 - 1112. FABRICATED A NEW FLOOR PANEL IAW EO B767-5320-9693-I.
- [SDR IPXA2017091121610](https://openairdocs.org/sdr/IPXA2017091121610), Sep 11, 2017: BATTERY PACK. INOPERATIVE. EMERGENCY LIGHTS INOPERATIVE. REPLACED THE BATTERY PACK IAW MM 33-51-07. OPS CHECKED GOOD.
- [SDR IPXA2017082520945](https://openairdocs.org/sdr/IPXA2017082520945), Aug 14, 2017: SMOKE DETECTOR. INOPERATIVE. INSPECTION TYPE: MAIN CARGO SMOKE DETECTOR 1 EICAS MESSAGE. TROUBLESHOT IAW FIM 26-14-00, FOUND TAIM INOPERATIVE. R & R THE TAIM IAW AMM 26-14-00/401, AND OPS T
- [SDR IPXA2017030814877](https://openairdocs.org/sdr/IPXA2017030814877), Mar 8, 2017: PRESSURE SWITCH. INOPERATIVE. RIGHT ENGINE OIL FILTER STATUS LIGHT ILLUMINATED IN FLIGHT, LEFT/RIGHT OIL PRESS WAS 65, LEFT/RIGHT OIL TEMP WAS 87, LEFT/RIGHT OIL QUANTITY WAS 16T/S PER FIM79
- [SDR IPXA2017012313105](https://openairdocs.org/sdr/IPXA2017012313105), Jan 22, 2017: BLOCKER DOOR. CRACKED. NR 1 ENGINE INBOARD RT THRUST REVERSER BLOCKER DOOR AT 8:00 OCLOCK POSITION HAS MULTIPLE CRACKS. REMOVED & REPLACED THE BLOCKER DOOR IAW AMM 28-31-14, OPS CHECK
- [SDR IPXA2016060704338](https://openairdocs.org/sdr/IPXA2016060704338), Jun 7, 2016: CONTROL PANEL. INOPERATIVE. OVERHEAD EMERGENCY LIGHT CONTROL PANEL NOT ARMED, LIGHT INOPERATIVE. TRIED TO RELAMP BUT LIGHT CARRIER CAME APART. NO SPARE LIGHT ASSY IN NRT. REPLACED EMERGENC
- [SDR IPXA2016051103200](https://openairdocs.org/sdr/IPXA2016051103200), May 11, 2016: STRUT. INOPERATIVE. LIFE RAFT ACCESS DOOR DOES NOT STAY OPEN. R & R GAS STRUT IAW MM 20-11-00-910. IPC REF 25-62-55-01, ITEM 480.
- [SDR IPXA2016030600384](https://openairdocs.org/sdr/IPXA2016030600384), Mar 6, 2016: FLOOR PANEL. DAMAGED. MAIN CARGO FLOOR PANEL DAMAGED AT BS 412, FABRICATED A NEW FLOOR PANEL IAW EO B767-5320-9693-I.
- [SDR IPXA2016021999602](https://openairdocs.org/sdr/IPXA2016021999602), Jan 21, 2016: STRINGER. CRACKED. INSPECTION TYPE:C10, CRACK, 3" WAS FOUND ON THE STRINGER 20R AT BS 1550. REPAIR IAW SR: PN 4-3138709764 WITH FAA APPROVED 8100-9 FORM DATE: 16FEB2016 AND EO: B7
- [SDR IPXA2015111595813](https://openairdocs.org/sdr/IPXA2015111595813), Nov 15, 2015: FLOOR PANEL. DELAMINATED. MCD FLOOR PANEL DAMAGED, POSITION NR 11 CENTER. FABRICATED A NEW FLOOR PANEL IAW EO B767-5320-9693-H.
- [SDR IPXA2015110395438](https://openairdocs.org/sdr/IPXA2015110395438), Nov 2, 2015: SPRING. WORN. CREW DOOR EXTERNAL DOOR HANDLE ASSY IS WORN IN 2 PLACES. R & R PAWL, SPRING AND PIN. OPS CHECKED NORMAL IAW MM 52-12-215. ACFT OK FOR SERVICE.
- [SDR IPXA2015100794502](https://openairdocs.org/sdr/IPXA2015100794502), Oct 7, 2015: LINE. RUPTURED. DURING CLIMB, LEFT ENGINE FAILED. AIR RETURN. R & R RUPTURED FUEL LINE.
- [SDR IPXA2014030382123](https://openairdocs.org/sdr/IPXA2014030382123), Mar 2, 2014: FLOOR PANEL. DAMAGED. MAIN CARGO DECK FLOOR PANEL BS 280-412 RT SIDE DAMAGED AT AFT END. REPAIRED IAW SRM 53-00-50-2R.
- [SDR IPXA2014012081484](https://openairdocs.org/sdr/IPXA2014012081484), Jan 15, 2014: SKIN. DENTED. INSPECTION C09, DENT ON THE T/E WEDGE UPPER SKIN OF LT WING INBD AFT FLAP AT AT IFS 142.25. REPAIR IAW SRM 57-53-01-2R-1 REPAIR 1 FIG 201, REV 58, & SRM 51-70-1
- [SDR IPXA4681483](https://openairdocs.org/sdr/IPXA4681483), Jan 15, 2014: SKIN. DENTED. INSPECTION C09, THREE DENTS ON THE T/E WEDGE UPPER SKIN OF LT WING INBD AFT FLAP. REPAIRED IAW SRM 57-53-01-2R-1, REPAIR 1, FIG 201, REV 58.0, SRM 51-70-10-2R-2
- [SDR IPXA2014012081482](https://openairdocs.org/sdr/IPXA2014012081482), Jan 15, 2014: SKIN. DENTED. INSPECTION C09, DENT ON THE LT WING OTBD FLAP UPPER PANEL INNER SURFACE AT T/E FLAP STA 78.75. REPAIRED IAW -SRM 57-53-01-2R-1 REPAIR 1, FIG 201, REV.58, SRM 51
- [SDR IPXA2014012081481](https://openairdocs.org/sdr/IPXA2014012081481), Jan 15, 2014: SKIN. DENTED. INSPECTION C09, DENT ON THE T/E COVER PANEL UPPER SKIN OF LT WING INBD MAIN FLAP AT IFS 184.7. REPAIR IAW SRM 57-53-01-2R-1, REPAIR 1, FIGURE 201, REV 58.0 0. 2

All 144: https://openairdocs.org/aircraft/N315UP/reports.md

## STCs that may be installed (OpenAirDocs) (6)

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 CF6-80 series)

- [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. Lists CF6-80A
- [STC SE01478CH](https://openairdocs.org/stc/SE01478CH): Installation of Cook Airtomic alignment joint p/n AIR 22912. Cook Airtomic. Lists CF6-80C2 Series
- [STC SE00969CH](https://openairdocs.org/stc/SE00969CH): Install AeroControlex P/N 2605290-001 variable stator feedback control cable. AeroControlex Group TransDigm Inc. Lists CF6-80A
- [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. Lists CF6-80C2A1
- [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

## Related

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

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