# N354UP: 2013 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: 37862
- Year built: 2013
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: January 13, 2013
- Certificate issued: January 14, 2013
- Expires: January 31, 2029
- Mode S code: A3F579
- 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=354UP
- Page: https://openairdocs.org/aircraft/N354UP

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 N354UP.

## FAA accident and incident reports

None matched to N354UP.

## Service difficulty reports (39)

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 IPXA2026100856727](https://openairdocs.org/sdr/IPXA2026100856727), Oct 2, 2026: SKIN. DEBONDED. FAULT - DISBOND - END CAP, R/H WING T/E OUTBD FLAP INBD. MEASURE THE DAMAGE AREA (L:1.5", W:0.1", D:2PLIES, 7" FROM AFT EDGE, AT INBD EDGE). BOND THE REPAIR PLI
- [SDR IPXA2026100857298](https://openairdocs.org/sdr/IPXA2026100857298), Oct 2, 2026: SKIN. CRACKED. FAULT - CRACK - SKIN, R/H WING T/E INBD MAIN FLAP INBD UPPER. (REPAIR). MEASURE THE DAMAGE AREA (DIA:1", 16.5" FROM INBD EDGE, 3.5" FROM AFT EDGE). BOND THE REP
- [SDR IPXA2026100553573](https://openairdocs.org/sdr/IPXA2026100553573), Oct 2, 2026: FORMER. BROKEN. BROKEN FORMER, LT WING OUTBD L/E FOLDING NOSE INNER SIDE AT OSS 441.60, ADJACENT NR 5 SLAT INBD AUX TRACK. REMOVED DAMAGE FORMER IAW SRM 51-40-02-0G, REV 96. IN
- [SDR IPXA2026100503114](https://openairdocs.org/sdr/IPXA2026100503114), Sep 30, 2026: SKIN. DENTED. FAULT - DENT - SKIN , NO.1 ENG NOSE COWL INLET AT 9 O'CLOCK POSITION. CUT OUT THE DAMAGE AND CLEAN, MEASURE THE CUT OUT ( DIA : 0.2", 18.2" FROM L/E, AT 9 O'CLO
- [SDR IPXA2026100503125](https://openairdocs.org/sdr/IPXA2026100503125), Sep 30, 2026: SKIN. DENTED. FAULT - DENT - SKIN , NO.1 ENG NOSE COWL INLET AT 3 O'CLOCK POSITION. CUT OUT THE DAMAGE AND CLEAN, MEASURE THE CUT OUT ( DIA : 0.25", 20.5" FROM L/E, AT 3 O'CL
- [SDR IPXA2026100603239](https://openairdocs.org/sdr/IPXA2026100603239), Sep 30, 2026: SKIN. DENTED. FAULT - DENT - SKIN , NO.2 ENG NOSE COWL INNER BARREL AT 8 O'CLOCK. CUT OUT THE DAMAGE AND CLEAN, MEASURE THE CUT OUT ( DIA : 0.3", 8.2" FROM T/E, AT 8 O'CLOCK 
- [SDR IPXA2026100603252](https://openairdocs.org/sdr/IPXA2026100603252), Sep 30, 2026: SKIN. DENTED. DENTED SKIN , NR 2 ENG NOSE COWL INNER BARREL AT 5 O'CLOCK. CUT OUT THE DAMAGE AND CLEAN, MEASURE THE CUT OUT ( DIA : 0.3", 7" FROM T/E, AT 5 O'CLOCK ON THE INN
- [SDR IPXA2026100465120](https://openairdocs.org/sdr/IPXA2026100465120), Sep 28, 2026: STIFFENER. CRACKED. MAJOR REPAIR, STIFFENER CRACK AT CENTER FRONT BS 785.9 RBL 33. ACCOMPLISH THE REPAIR I.A.W SRM 57-10-10-2R-2 REV.96 AND EGAT WORK SHEET NO.60769 AND UPS SREO-58
- [SDR IPXA2026100465056](https://openairdocs.org/sdr/IPXA2026100465056), Sep 28, 2026: STIFFENER. CRACKED. STIFFENER CRACK AT CENTER FRONT BS 785.9 LBL 55. ACCOMPLISH THE REPAIR I.A.W SRM 57-10-10-2R-2, REV 96 AND EGAT WORK SHEET NR 60770 AND SREO-58151-REQ001 REV 2.
- [SDR IPXA2025110634788](https://openairdocs.org/sdr/IPXA2025110634788), Nov 6, 2025: LANDING GEAR. VIBRATION. HEAVY VIBRATIONS FROM EITHER NOSE GEAR OR MAIN GEAR ON T/O ROLL. INTENSIFIED AS SPEED INCREASED. VERY NOISY AFTER WT OFF WHEELS UNTIL GEAR RETRACTED JACKED NOSE
- [SDR IPXA2025110521634](https://openairdocs.org/sdr/IPXA2025110521634), Nov 5, 2025: SWITCH. BROKEN. EMERGENCY LIGHT SWITCH PANEL, KORRY SWITCH BROKEN €˜UNARMED€? ANNUNCIATOR KORRY LIGHT BROKEN. NIL SPARE AVAILABLE. REMOVED AND REPLACED EMERGENCY LIGHTS CONTR
- [SDR IPXA2025070103289](https://openairdocs.org/sdr/IPXA2025070103289), Jul 1, 2025: GASKET. LEAKING. EMERGENCY DECLARED, LEFT HYD QTY ICAS MESSAGE QTY AT.45. PILOT STATED IT DID GO TO ZERO. REMOVED AND REPLACED YDS ELECTROHYDRAULIC SERVOVALVE AND SOLENOID VALVE
- [SDR IPXA2024092758498](https://openairdocs.org/sdr/IPXA2024092758498), Sep 18, 2024: DRAIN. NONE. (FUSELAGE DRAIN HOLES INSPECTION AND INSTALLATION AFT OF BS 1725.5 BETWEEN S-36L AND S-36R) COMPLETED SDR.
- [SDR IPXA2024092360016](https://openairdocs.org/sdr/IPXA2024092360016), Sep 18, 2024: ANGLE. CRACKED. FOUND THE ANGLE CRACK AT STA 1578 RBL 80 INBOARD IN BULK CARGO COMPARTMENT RIGHT AREA (REPLACE) REMOVED DAMAGE PART I.A.W SRM 51-40-02-0G REV. 90. INSTALL NEW P
- [SDR IPXA2024092358669](https://openairdocs.org/sdr/IPXA2024092358669), Sep 18, 2024: ANGLE. CRACKED. FOUND THE ANGLE CRACK AT STA 1578 LBL 80 OUTBOARD BULK CARGO COMPARTMENT LEFT AREA (REPLACE) I.A.W AMM 25-57-05-404-006 AND AMM 25-58-04-404-015 REV.142 INSTALL
- [SDR IPXA2024092359974](https://openairdocs.org/sdr/IPXA2024092359974), Sep 18, 2024: ANGLE. CRACKED. FOUND THE ANGLE CRACK AT STA 1578 RBL 80 OUTBOARD IN BULK CARGO COMPARTMENT RIGHT AREA (REPLACE) I.A.W AMM 25-57-05-404-006 AND AMM 25-58-04-404-015 REV.142 INS
- [SDR IPXA2024091860300](https://openairdocs.org/sdr/IPXA2024091860300), Sep 18, 2024: FLOOR PANEL. CRACKED. MAJOR REPAIR. FOUND MAIN DECK FLOOR PANEL WITH CRACK DAMAGE, PANEL NO.251XFF, P/N: 146T5869-135 (REPAIR) I.A.W AMM 25-57-05-404-006, AMM 25-58-01-404-005, AMM 2
- [SDR IPXA2024091858498](https://openairdocs.org/sdr/IPXA2024091858498), Sep 18, 2024: NONE. NO DISCREPANCY. **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)
- [SDR IPXA2024091860330](https://openairdocs.org/sdr/IPXA2024091860330), Sep 18, 2024: FLOOR PANEL. CRACKED. MAJOR REPAIR. FOUND MAIN DECK FLOOR PANEL WITH CRACK DAMAGE. PANEL NO.252UFF, P/N: 146T5869-134 (REPAIR).
- [SDR IPXA2024091860270](https://openairdocs.org/sdr/IPXA2024091860270), Sep 18, 2024: FLOOR PANEL. DENTED. MAJOR REPAIR. FOUND MAIN DECK FLOOR PANEL WITH DENT DAMAGE. PANEL NO.231FFF, P/N: 143T5876-99 (REPAIR) I.A.W AMM 25-57-03-404-005, AMM 25-58-01-404-018, AMM 25-
- [SDR IPXA2024091860190](https://openairdocs.org/sdr/IPXA2024091860190), Sep 18, 2024: FLOOR PANEL. DENTED. MAJOR REPAIR. FOUND MAIN DECK FLOOR PANEL WITH DENT DAMAGE. PANEL NO.231VFF P/N: 143T5876-27 (REPAIR) I.A.W AMM 25-57-05-404-006 AND AMM 25-58-04-404-015 REV. 1
- [SDR IPXA2023041092794](https://openairdocs.org/sdr/IPXA2023041092794), Apr 10, 2023: LIGHT. INOPERATIVE. INSPECTION TYPE:NAEMER LIGHTS COVER SPRING DOES NOT CLEAR TOGGLE SWITCHADJUSTED TOGGLE COVER SPRING ON EMERGENCY LIGHTS CONTROL PANEL OPS CHECK GOOD AT THIS TIM
- [SDR IPXA2023010989756](https://openairdocs.org/sdr/IPXA2023010989756), Jan 9, 2023: BATTERY PACK. NO TEST. DURING PDC FOUND EMG LIGHTS INOP. R & R EMG LIGHT BATT IAW AMM 33-51-07. OPS CHECK SAT.
- [SDR IPXA2020111362324](https://openairdocs.org/sdr/IPXA2020111362324), Nov 12, 2020: ECU. FAILED. INSPECTION TYPE: NA ATB-AC OUT OF SERVICE. EMERGENCY DECLARED, LANDED W/OUT INCIDENT, NO EMERGENCY EQUIPMENT USED. APU FAULT, APU SHUTDOWN WHICH RESULTED IN AN 
- [SDR IPXA2020081258951](https://openairdocs.org/sdr/IPXA2020081258951), Aug 11, 2020: WARNING MESSAGE. ILLUMINATED. AIR TURNBACK. GEAR DISAGREE NOSE AFTER TAKEOFF. NOSE GEAR PIN IN PLACE WITHOUT A STREAMER ATTACHED TO PIN. (NO LOGBOOK ENTRY) REMOVED PIN AS REQUIRED. REMOVED N
- [SDR IPXA2020052765828](https://openairdocs.org/sdr/IPXA2020052765828), Apr 21, 2020: ENGINE. SMOKE. INSPECTION TYPE:N/AWHILE STARTING THE LEFT ENGINE, THE MECHANIC CALLED FOR US TO SHUTDOWN THE LEFT ENGINE DUE TO EXCESSIVE FLUID AND SMOKE COMING FROM THE ENGIN
- [SDR IPXA2018102935437](https://openairdocs.org/sdr/IPXA2018102935437), Oct 19, 2018: FLOOR PANEL. DAMAGED. DAMAGE FOUND ON THE M/D CARGO FLOOR PANEL 251MF AT BS 1208 -1313, LBL 11 - LBL 33. FABRICATED A REPLACEMENT FLOOR PANEL IAW EO B767-5320-9693-I.
- [SDR IPXA2018052129809](https://openairdocs.org/sdr/IPXA2018052129809), May 17, 2018: COMPRESSOR. DAMAGED. WHILE AIRBORNE, AT THE TOP OF DECENT, THE RIGHT ENGINE THRUST REDUCED TO IDLE POWER ABNORMALLY. AT IDLE THRUST, THE LEFT AND RIGHT ENGINES DIFFERED IN PARAMETER
- [SDR IPXA2017061918390](https://openairdocs.org/sdr/IPXA2017061918390), Jun 17, 2017: EVAS UNIT. FAILED. CAPTAIN`S EVAS UNIT BLOWER CHECK FAILED IAW MM 25-69-00 PB 401. INSTALLED A SERVICEABLE UNIT BATTERY, BLOWER CHECKED GOOD.
- [SDR IPXA2017050816882](https://openairdocs.org/sdr/IPXA2017050816882), May 6, 2017: STRUT. INOPERATIVE. FOUND LIFE RAFTS STOWAGE GAS STRUT INOPERATIVE. THE GAS STRUT WAS REPLACED IAW AMM 20-11-00-201, REV 121.
- [SDR IPXA2017033115700](https://openairdocs.org/sdr/IPXA2017033115700), Mar 31, 2017: BRACKET. BENT. FWD ENTRY DOOR EICAS MESSAGE. FOUND THE BRACKET FOR FWD ENTRY DOOR PROXMITY SENSOR BENT. REPLACED THE BRACKET AND ADJUSTED THE PROXIMTIY SWITCH IAW AMM 52-71-00
- [SDR IPXA2017030714858](https://openairdocs.org/sdr/IPXA2017030714858), Mar 7, 2017: WARNING SYSTEM. FALSE ACTIVATION. L FWD ENT DOOR EICAS AFTER BLOCK OUT. ACCOMPLISHED FIM 52-71-00-815-805 AND 32-09-03-815-808 SYS OPS CK NORMAL.
- [SDR IPXA2017010912500](https://openairdocs.org/sdr/IPXA2017010912500), Jan 5, 2017: FLOOR PANEL. DAMAGED. INSPECTION TYPE: C2, M/D CARGO FLOOR PANEL AT BS 654 - 676, DAMAGED. FABRICATES A REPLACEMENT FLOOR PANEL IAW EO B767-5320-9693-I.
- [SDR IPXA2015122196934](https://openairdocs.org/sdr/IPXA2015122196934), Dec 18, 2015: LIGHT. UNKNOWN. EXTERIOR EMERGENCY LIGHT INOPERATIVE. CHECKED EXTERIOR EMERGENCY LIGHT, OPS CHECKED OK.
- [SDR IPXA2015080391898](https://openairdocs.org/sdr/IPXA2015080391898), Aug 3, 2015: SKIN. DENTED. FUSELAGE SKIN DENTED AT BS 632 BETWEEN STRINGERS 34-35L. REPAIRED IAW EO B767-5330-57724B.
- [SDR IPXA2015030586693](https://openairdocs.org/sdr/IPXA2015030586693), Mar 5, 2015: LAMP. INOPERATIVE. EMERGENCY LIGHT BELOW ENTRY DOOR IS INOPERATIVE. RELAMPED EMERGENCY EXTERIOR LIGHT IAW AMM 33-51-16-962-001.
- [SDR IPXA2014070983545](https://openairdocs.org/sdr/IPXA2014070983545), Jul 7, 2014: FLOOR PANEL. PUNCTURED. FLOOR PANEL PUNCTURE DAMAGE APPROXIMATELY .781 X .500 AT POS 6, AFT, RT OF CENTERLINE ACCOMPLISHED EO B767-5320-27379-B, 6 A AND OPENED DEFERRAL FOR RE-CHECK, N
- [SDR IPXA2014072883546](https://openairdocs.org/sdr/IPXA2014072883546), Jul 4, 2014: FLOOR PANEL. DAMAGED. FOUND A ONE INCH HOLE IN FLOOR PANEL AT 4 RT POSITION. DAMAGE FOUND TO BE MINOR. NO STRUCTURAL INTEGRITY LOST. REPAIRED IAW AMM 25-00-00-308-015.
- [SDR IPXA2014022482030](https://openairdocs.org/sdr/IPXA2014022482030), Feb 22, 2014: FLOOR PANEL. DAMAGED. MAIN CARGO DECK FLOOR PANEL DAMAGED AT FRAMES 9-10, RBL64. FABRICATED NEW FLOOR PANEL IAW EO B767-5320-53448-A.

## 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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