# N355UP: 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: 37863
- Year built: 2013
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: February 14, 2013
- Certificate issued: February 28, 2013
- Expires: February 28, 2029
- Mode S code: A3F930
- 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=355UP
- Page: https://openairdocs.org/aircraft/N355UP

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 N355UP.

## FAA accident and incident reports

None matched to N355UP.

## Service difficulty reports (48)

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 IPXA2026092286713](https://openairdocs.org/sdr/IPXA2026092286713), Sep 17, 2026: COWLING. CRACKED. CRACKED SKIN, NR 1 ENG RT CORE COWL LOWER FWD SKIN NEAR NO.1 LATCH. PERFORM REPAIR I.A.W UPS EO-98690-REQ1 REV.1.
- [SDR IPXA2026092191640](https://openairdocs.org/sdr/IPXA2026092191640), Sep 17, 2026: PANEL. ERODED. ERODED VERTICAL STAB LE PANEL 321E. REMOVED THE DAMAGE MATERIALS AND CLEAN. BONDED THE REPAIR PLIES WITH FILM ADHESIVE CURED AT 260 F FOR 130 MINUTES WITH MINIM
- [SDR IPXA2026092289443](https://openairdocs.org/sdr/IPXA2026092289443), Sep 17, 2026: NOSE COWL. DENTED. DENTED NR 1 NOSE COWL INLET AT 7 O'CLOCK POSITION. BOND THE SPACER WITH FILM ADHESIVE CURED AT 250°F FOR 2 HOURS AND FILL THE CUT OUT WITH ADHESIVE CURED AT 20
- [SDR IPXA2026092290656](https://openairdocs.org/sdr/IPXA2026092290656), Sep 17, 2026: NOSE COWL. DENTED. DENTED NR 1 ENG NOSE COWL INLET AT 5 O'CLOCK POSITION. BOND THE SPACER WITH FILM ADHESIVE CURED AT 250°F FOR 2 HOURS AND FILL THE CUT OUT WITH ADHESIVE CURED A
- [SDR IPXA2026092290813](https://openairdocs.org/sdr/IPXA2026092290813), Sep 17, 2026: NOSE COWL. DENTED. DENTED SKIN, NR 2 ENG NOSE COWL INNER BARREL NEAR 2:00 TO 6:00 POS. BOND THE SPACER WITH FILM ADHESIVE CURED AT 250°F FOR 2 HOURS AND FILL THE CUT OUT WITH ADH
- [SDR IPXA2026092290842](https://openairdocs.org/sdr/IPXA2026092290842), Sep 17, 2026: NOSE COWL. DENTED. DENTED NR 1 ENGINE NOSE COWL INLET AT 6 O'CLOCK POSITION. UT OUT THE DAMAGE AND CLEAN, MEASURE THE CUT OUT ( ‘ DIA : 0.2", 27" FROM FWD EDGE, 31.5" FROM UPPER 
- [SDR IPXA2026092186627](https://openairdocs.org/sdr/IPXA2026092186627), Sep 17, 2026: FLOOR PANEL. CRACKED. CRACKED PANEL, AFT CARGO FLOOR STRUCTURE, BS 1329, BL 0. REMOVED DAMAGE PANEL I.A.W SRM 51-40-02-0G REV. 96. INSTALLED FABRICATED PANEL I.A.W SRM 51-40-02-0G RE
- [SDR IPXA2026092267592](https://openairdocs.org/sdr/IPXA2026092267592), Sep 16, 2026: FAIRING. DEBONDED. DEBONDED SKIN , RT AFT WING TO BODY FAIRING LATCH PANEL 198 CR. REMOVE THE DISBOND MATERIALS AND CLEAN. BOND THE REPAIR PLIES WITH RESIN CURED AT 200°F FOR 220
- [SDR IPXA2026092166138](https://openairdocs.org/sdr/IPXA2026092166138), Sep 16, 2026: SKIN. PUNCTURED. SKIN, RT MLG W/W DOOR MID PUNCTURED. PERFORMED NDT/UT FOR THE REWORKED AREA AND PLUS 6 INCHES AROUND HEATED AREA, IAW NDT MANUAL PART 1, 51-01-01, REV 144. REMO
- [SDR IPXA2026092172110](https://openairdocs.org/sdr/IPXA2026092172110), Sep 16, 2026: BRACKET. CRACKED. CRACKED BRACKET, LT WING INBD SLAT TORQUE TUBE SUPPORT AT INBD L/E CAVITY AT ISS 285.233. REMOVED DAMAGE BRACKET I.A.W SRM 51-40-02-0G REV. 96. INSTALLED NEW BR
- [SDR IPXA2026092172477](https://openairdocs.org/sdr/IPXA2026092172477), Sep 16, 2026: ANGLE. CRACKED. CRACKED ANGLE, NR 1 PYLON AFT BULKHEAD REAR LT ANGLE. REMOVED DAMAGE ANGLE I.A.W SRM 51-40-02-0G REV. 96. INSTALLED NEW ANGLE I.A.W SRM 51-40-02-0G REV. 96 AND 
- [SDR IPXA2026092150993](https://openairdocs.org/sdr/IPXA2026092150993), Sep 15, 2026: FORMER. CRACKED. CRACKED FORMER, RT WING OTBD L/E CAVITY CURTAIN SUPPORT BRACKET, NEAR WS 441.596. REMOVED DAMAGE FORMER I.A.W SRM 51-40-02-0G REV.96. INSTALL NEW FORMER I.A.W S
- [SDR IPXA2026091850925](https://openairdocs.org/sdr/IPXA2026091850925), Sep 15, 2026: BRACKET. CRACKED. CRACKED BRACKET, RT WING INBD L/E CAVITY TORQUE TUBE SUPPORT BRACKET. REMOVED DAMAGE BRACKET I.A.W SRM 51-40-02-0G REV.96. INSTALL NEW BRACKET I.A.W SRM 51-40-0
- [SDR IPXA2026091850918](https://openairdocs.org/sdr/IPXA2026091850918), Sep 15, 2026: ANGLE. CRACKED. THE BULK CARGO OUTBOARD ANGLE AT STA 1578 LBL 80 IS CRACKED. REMOVED DAMAGE ANGLE I.A.W SRM 51-40-02-0G REV. 96. INSTALLED NEW ANGLE I.A.W SRM 51-40-02-0G REV. 
- [SDR IPXA2026091850822](https://openairdocs.org/sdr/IPXA2026091850822), Sep 15, 2026: ANGLE. CRACKED. THE BULK CARGO OUTBOARD ANGLE AT STA 1578 RBL 80 IS CRACKED. REMOVED DAMAGE ANGLE I.A.W SRM 51-40-02-0G REV. 96. INSTALLED NEW ANGLE I.A.W SRM 51-40-02-0G REV. 
- [SDR IPXA2026091850792](https://openairdocs.org/sdr/IPXA2026091850792), Sep 15, 2026: ANGLE. CRACKED. THE BULK CARGO INBOARD ANGLE AT STA 1578 RBL 80 IS CRACKED. REMOVED DAMAGE ANGLE I.A.W SRM 51-40-02-0G REV. 96. INSTALLED NEW ANGLE I.A.W SRM 51-40-02-0G REV. 9
- [SDR IPXA2026091850818](https://openairdocs.org/sdr/IPXA2026091850818), Sep 15, 2026: ANGLE. CRACKED. THE BULK CARGO INBOARD ANGLE AT STA 1578 LBL 80 IS CRACKED. REMOVED DAMAGE ANGLE I.A.W SRM 51-40-02-0G REV. 96. <BR>2. INSTALLED NEW ANGLE I.A.W SRM 51-40-02-0G
- [SDR IPXA2026070613325](https://openairdocs.org/sdr/IPXA2026070613325), Jul 5, 2026: OXYGEN MASK. NO TEST. OBSERVERS OXYGEN MASK DOES NOT FLOW WHEN EMERGENCY BUTTON IS PUSHED. REMOVED AND REPLACED OBSERVER`S OXYGEN MASK IAW AMM 35-11-51. OPS CHKD GOOD.
- [SDR IPXA2024092758398](https://openairdocs.org/sdr/IPXA2024092758398), 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 IPXA2024091858398](https://openairdocs.org/sdr/IPXA2024091858398), 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 IPXA2024091811151](https://openairdocs.org/sdr/IPXA2024091811151), Sep 15, 2024: FLOOR PANEL. BROKEN. MAJOR REPAIR. FOUND MAIN DECK CARGO FLOOR PANEL BROKEN PART NUMBER : 146T5869-135 (REPAIR) I.A.W AMM 53-01-06-400-801 REV.142 INSTALL MAIN DECK CARGO FLOOR PANE
- [SDR IPXA2024092710203](https://openairdocs.org/sdr/IPXA2024092710203), Sep 15, 2024: COVER. WORN. FOUND CREW ENTRY DOOR FORWARD DOORWAY ARMING LEVER COVER SCREW WORN (REPLACE) REPLACED DOORWAY ARMING LEVER COVER I.A.W AMM 20-11-00-910-802 REV.142.
- [SDR IPXA2024091811112](https://openairdocs.org/sdr/IPXA2024091811112), Sep 15, 2024: FLOOR PANEL. BROKEN. MAJOR REPAIR. FOUND MAIN DECK CARGO FLOOR PANEL BROKEN PART NUMBER : 146T5869-134 (REPAIR) I.A.W AMM 53-01-06-400-801 REV.142 INSTALL MAIN DECK CARGO FLOOR PANE
- [SDR IPXA2024091610203](https://openairdocs.org/sdr/IPXA2024091610203), Sep 15, 2024: LEVER. WORN. **SDR FILED OPEN** FAULT - FOUND CREW ENTRY DOOR FORWARD DOORWAY ARMING LEVER COVER SCREW WORN (REPLACE) OK TO WORK
- [SDR IPXA2024092052030](https://openairdocs.org/sdr/IPXA2024092052030), Jul 28, 2024: SKIN. DENTED. **SDR FILED OPEN** LH INBD FLAP, TRAILING EDGE AND MID FLAP HAS DENT/DAMAGE INSTALLED L/H INBD MID FLAP LWR PNL I.A.W SRM 51-40-02-0G REV.90 AND BOEING DWG NO:1
- [SDR IPXA2023082171352](https://openairdocs.org/sdr/IPXA2023082171352), Aug 21, 2023: BATTERY. DISCHARGED. EMERGENCY ESCAPE LIGHTING INOP. R&R'D EMERGENCY EXIT LIGHT BATTERY ASSY. OPS CK GOOD, REF AMM 33-51-07-201.
- [SDR IPXA2022111588129](https://openairdocs.org/sdr/IPXA2022111588129), Nov 13, 2022: FLOOR PANEL. DAMAGED. INSPECTION TYPE:C5, DAMAGE ON MAIN DECK CARGO FLOOR PANEL BETWEEN STA 930 AND STA 972, AND BETWEEN LBL 11.0 AND RBL 11.0FABRICATE REPLACEMENT FLOOR PANEL PER UP
- [SDR IPXA2022111588126](https://openairdocs.org/sdr/IPXA2022111588126), Nov 13, 2022: FLOOR PANEL. DAMAGED. INSPECTION TYPE:C5, DAMAGE ON MAIN DECK CARGO FLOOR PANEL BETWEEN STA 1114.8 AND STA 1197+22, AND BETWEEN LBL 11.0 AND RBL 11.0FABRICATE REPLACEMENT FLOOR PANEL
- [SDR IPXA2022111588123](https://openairdocs.org/sdr/IPXA2022111588123), Nov 13, 2022: FLOOR PANEL. DAMAGED. INSPECTION TYPE:C5DAMAGE ON MAIN DECK CARGO FLOOR PANEL BETWEEN STA 1351 AND STA 1480, AND BETWEEN LBL 11.0 AND RBL 11.0.FABRICATE REPLACEMENT FLOOR PANEL PER U
- [SDR IPXA2022111588128](https://openairdocs.org/sdr/IPXA2022111588128), Nov 10, 2022: FLOOR PANEL. DAMAGED. INSPECTION TYPE:C5, DAMAGE ON MAIN DECK CARGO FLOOR PANEL BETWEEN STA 972 AND STA 1114.8, AND BETWEEN LBL 11.0 AND RBL 11.0FABRICATE REPLACEMENT FLOOR PANEL PER
- [SDR IPXA2022111588125](https://openairdocs.org/sdr/IPXA2022111588125), Nov 10, 2022: FLOOR PANEL. DAMAGED. INSPECTION TYPE:C5, DAMAGE ON MAIN DECK CARGO FLOOR PANEL BETWEEN STA 1197+22 AND STA 1208, AND BETWEEN LBL 11.0 AND RBL 11.0FABRICATE REPLACEMENT FLOOR PANEL P
- [SDR IPXA2022111588124](https://openairdocs.org/sdr/IPXA2022111588124), Nov 10, 2022: FLOOR PANEL. DAMAGED. INSPECTION TYPE:C5DAMAGE ON MAIN DECK CARGO FLOOR PANEL BETWEEN STA 1208 AND STA 1351, AND BETWEEN LBL 11.0 AND RBL 11.0FABRICATE REPLACEMENT FLOOR PANEL PER UP
- [SDR IPXA2021082473122](https://openairdocs.org/sdr/IPXA2021082473122), Aug 24, 2021: LAMP. INOPERATIVE. INSPECTION TYPE:N/AEXTERNAL EMERGENCY EXIT LIGHT INOPEXTERNAL EMERGENCY EXIT LIGHT RELAMPED AND TESTED SERVICEABLE IAW B767 AMM 33-51-16-962-001
- [SDR IPXA2020111462354](https://openairdocs.org/sdr/IPXA2020111462354), Nov 9, 2020: SKIN. BROKEN. INSPECTION TYPE: C4 BROKEN ON LOWER SKIN (P/N:114T4114-23) OF NR 8 SLAT TRAILING EDGE WEDGE NEAR OSS 432.15. REPAIR IAW B767-300F SRM 57-43-02-2R-1 SRM 51-70-10
- [SDR IPXA2020111462352](https://openairdocs.org/sdr/IPXA2020111462352), Nov 9, 2020: SKIN. BROKEN. INSPECTION TYPE: C4 BROKEN ON LOWER SKIN (P/N:114T4114-23) OF NR 8 SLAT TRAILING EDGE WEDGE NEAR OSS 498. REPAIR IAW B767-300F SRM 57-43-02-2R-1, SRM 51-70-10-2
- [SDR IPXA2020083159644](https://openairdocs.org/sdr/IPXA2020083159644), Aug 31, 2020: FLOOR PANEL. DAMAGED. INSPECTION TYPE:N/A MAIN CARGO DECK POSITION 2L INTERIM REPAIR TO FLOOR PANEL DAMAGE 20IN FWD OF BALLMAT AND 15IN FROM CENTER LINE. FABRICATE NEW PANEL REF EO B
- [SDR IPXA2020083159643](https://openairdocs.org/sdr/IPXA2020083159643), Aug 30, 2020: FLOOR PANEL. CRACKED. INSPECTION TYPE:N/A MAIN CARGO DECK POSITION 2L INTERIM REPAIR TO FLOOR PANEL 26 INCH FWD OF BALL AMOUNT AND 20 INCH FROM LEFT SIDE WALL. FABRICATED NEW FLOOR P
- [SDR IPXA2020021051991](https://openairdocs.org/sdr/IPXA2020021051991), Feb 8, 2020: SEAL. TORN. ATB - HEAVY VIB CLIMBING OUT OF 7000 FT AND GOT WORSEW AS WE ACCELERATED ABOVE 10,000 FT, VIB WAS FELT IN BOTH CONTROL COLUMNS AND FLOOR. SLOWED TO 290 / 0.78 A
- [SDR IPXA2019072945020](https://openairdocs.org/sdr/IPXA2019072945020), Jul 29, 2019: WARNING SYSTEM. FALSE ACTIVATION. INSPECTION TYPE:INSPL FWD ENTRY DOOR EICAS MESSAGE. T/S PER FIM 52-90-17-41, CKD SENSOR S194 & LATCHING MECHANISM, NO FAULTS NOTED. FWD ENTRY DOOR IND OPS CKD N
- [SDR IPXA2019011537866](https://openairdocs.org/sdr/IPXA2019011537866), Jan 15, 2019: WARNING SYSTEM. FALSE ACTIVATION. INSPECTION TYPE:ETOP LEFT FUEL QUANTITY BLANK & EICAS STATUS MSG "FUEL QTY IND" CONDITION INTERMITTENT. FOUND AT BITE CHECK FUEL COMPUTER LM TANK UNIT 9 OPEN LO
- [SDR IPXA2016121611787](https://openairdocs.org/sdr/IPXA2016121611787), Dec 13, 2016: ENGINE. MALFUNCTIONED. DURING DESCENT, THE RT ENGINE FAILED TO RESPOND TO ANY THROTTLE MOVEMENTS. EGT REMAINED HIGH AT 670'C WITH N1 & N2 BACK AT IDLE. LOST CONTROL OF ANY THRUST ON R
- [SDR IPXA2016111810785](https://openairdocs.org/sdr/IPXA2016111810785), Nov 17, 2016: COUNTERBALANCE. FAILED. CREW ENTRY DOOR STUCK HALF WAY OPEN. REPLACED COUNTERBALANCE SYSTEM L1 DOOR IAW AMM 52-12-16.
- [SDR IPXA2016051103204](https://openairdocs.org/sdr/IPXA2016051103204), May 11, 2016: FLOORBOARD. GOUGED. FLOORBOARD IS GOUGED BEYOND SRM LIMITS. FABRICATED NEW FLOORBOARD IAW REO B767-5320-9693-I.
- [SDR IPXA2016051103236](https://openairdocs.org/sdr/IPXA2016051103236), May 11, 2016: FLOORBOARD. GOUGED. FLOORBOARD GOUGED BEYOND SRM LIMITS. FABRICATED NEW FLOOR PANEL IAW SREO B767-5320-9693-I.
- [SDR IPXA2014071683611](https://openairdocs.org/sdr/IPXA2014071683611), Jul 14, 2014: STRINGER. DAMAGED. STRINGER 31L DAMAGED 7 INCHES FWD OF BS 1285. REPAIRED IAW EO B767-5310-54925-A.
- [SDR IPXA2014071683610](https://openairdocs.org/sdr/IPXA2014071683610), Jul 14, 2014: SKIN. DAMAGED. FUSELAGE SKIN DAMAGE BS 1270-1285 BETWEEN S30L AND S32L. REPAIRED IAW EO B767-5330-54923-A.
- [SDR IPXA2014071683609](https://openairdocs.org/sdr/IPXA2014071683609), Jul 14, 2014: SKIN. DAMAGED. FOUND DAMAGE TO THE FUSELAGE SKIN, BS 1197-1222. REPAIRED IAW EO B767-5330-54924-A.
- [SDR IPXA13678924](https://openairdocs.org/sdr/IPXA13678924), Jun 18, 2013: CDU. INOPERATIVE. ALL KEYS ON CAPTAIN`S CDU INOPERATIVE WITH NORMAL AND ALTERNATE FMC SELECTED. R & R NR 1 CDU IAW AMM 34-61-02-022-195 AND IPC 34-61-02-02A.

## 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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