# N337UP: 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: 37858
- Year built: 2010
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: January 21, 2010
- Certificate issued: January 22, 2010
- Expires: May 31, 2029
- Mode S code: A3B1A0
- 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=337UP
- Page: https://openairdocs.org/aircraft/N337UP

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 N337UP.

## FAA accident and incident reports

None matched to N337UP.

## 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 IPXA2026031657601](https://openairdocs.org/sdr/IPXA2026031657601), Mar 13, 2026: WINDOW. DELAMINATED. R2 WINDOW DELAMINATION FO SIDE. BUBBLE IN WINDOW AS WELL, IN LINE OF SIGHT FOR VISION DEGRADATION. R&R R2 SLIDING WINDOW IAW AMM 56-11-02. LEAK AND OPS CHECK GO
- [SDR IPXA2026031357601](https://openairdocs.org/sdr/IPXA2026031357601), Mar 13, 2026: WINDOW. DELAMINATED. R2 WINDOW DELAMINATION FO SIDE. BUBBLE IN WINDOW AS WELL, IN LINE OF SIGHT FOR VISION DEGRADATION.
- [SDR IPXA2025090334054](https://openairdocs.org/sdr/IPXA2025090334054), Aug 30, 2025: FLOOR PANEL. DAMAGED. FOUND MAIN DECK FLOOR PANEL DAMAGE , P/N : 143T5876-83 PANEL NO : 231GFF. I.A.W AMM 53-01-06-000-801 REV.146 REMOVE MAIN DECK CARGO FLOOR PANEL AND SEALANT, G.V
- [SDR IPXA2025090334048](https://openairdocs.org/sdr/IPXA2025090334048), Aug 30, 2025: FLOOR PANEL. DAMAGED. FOUND MAIN DECK FLOOR PANEL DAMAGE , P/N : 143T5876-82 PANEL NO : 232GFF. I.A.W AMM 53-01-06-000-801 REV.146 REMOVE MAIN DECK CARGO FLOOR PANEL AND SEALANT, G.V
- [SDR IPXA2025090334158](https://openairdocs.org/sdr/IPXA2025090334158), Aug 30, 2025: FLOOR PANEL. DAMAGED. FOUND MAIN DECK FLOOR PANEL DAMAGE . I.A.W AMM 53-01-06-000-801 REV.146 REMOVE MAIN DECK CARGO FLOOR PANEL AND SEALANT, G.V.I AND CONDITION CHECK NORMAL. FABRIC
- [SDR IPXA2025090334100](https://openairdocs.org/sdr/IPXA2025090334100), Aug 30, 2025: FLOOR PANEL. DAMAGED. FOUND MAIN DECK FLOOR PANEL DAMAGE, PANEL NO : 232FFF. IAW AMM 53-01-06-000-801 REV.146 REMOVE MAIN DECK CARGO FLOOR PANEL, G.V.I AND CONDITION CHECK NORMAL. IA
- [SDR IPXA2025090334225](https://openairdocs.org/sdr/IPXA2025090334225), Aug 30, 2025: FLOOR PANEL. DAMAGED. FOUND MAIN DECK FLOOR PANEL DAMAGE, 232AFF. I.A.W AMM 53-01-06-000-801 REV.146 REMOVED MAIN DECK CARGO FLOOR PANEL, G.V.I AND CONDITION CHECK NORMAL. IAW AMM 53
- [SDR IPXA2025090334252](https://openairdocs.org/sdr/IPXA2025090334252), Aug 30, 2025: FLOOR PANEL. DAMAGED. FOUND MAIN DECK FLOOR PANEL DAMAGE , P/N : 143T5876-78 PANEL NO : 231AFF. I.A.W AMM 53-01-06-000-801 REV.146 REMOVE MAIN DECK CARGO FLOOR PANEL AND SEALANT , G.
- [SDR IPXA2025091013085](https://openairdocs.org/sdr/IPXA2025091013085), Aug 29, 2025: ANGLE. CRACKED. FOUND CRACK -ANGLE, BULK CGO COMPT CEILING AREA, STA 1577 LBL 74 INBOARD SIDE. I.A.W AMM 53-01-06-000-801 REV.146 REMOVE MAIN DECK CARGO FLOOR PANEL AND SEALANT
- [SDR IPXA2024032926686](https://openairdocs.org/sdr/IPXA2024032926686), Mar 29, 2024: WARNING MESSAGE. ILLUMINATED. GEAR DOOR LIGHT ILLUMINATED FOLLOWED BY GEAR DOOR EICAS MSG GEAR EXTENDED AT 170 KTS, SEE PREVIOUS LOGBOOK ENTRY TROUBLESHOT REF FIM 32-3- TREE 806.FOUND LAST F
- [SDR IPXA2024013037780](https://openairdocs.org/sdr/IPXA2024013037780), Jan 15, 2024: COVER. INOPERATIVE. **SUPPLEMENTAL SDR**COVER TO LOCK ON CABIN DOOR WILL NOT STOW TO DOWN POSITION REMOVED DEBRIS FROM HINGE REF IPC 52-11-02-10A ITEM 170. OPS CHK THE CREW ENTRY D
- [SDR IPXA2024011637780](https://openairdocs.org/sdr/IPXA2024011637780), Jan 15, 2024: UNKNOWN. UNKNOWN. COVER TO LOCK ON CABIN DOOR WILL NOT STOW TO DOWN POSITION DEFERRED DOOR ARMING LEVER HINGE COVER REF MEL 52-11-2, PLACARDS INSTALLED.
- [SDR IPXA2023082549891](https://openairdocs.org/sdr/IPXA2023082549891), Aug 19, 2023: FLOOR PANEL. DEFORMED. FOUND MAIN DECK CARGO FLOOR PANEL DEFORM PANEL, P/N:146T5869-89 I.A.W AMM 25-57-02-404-016 AND AMM 25-57-05-404-006 AND AMM 25-58-01-404-005 AND AMM 25-58-04-40
- [SDR IPXA2023041814430](https://openairdocs.org/sdr/IPXA2023041814430), Apr 18, 2023: UNKNOWN. VIBRATION. *SUPPLEMENTAL SDR* *ATB* DURING CLIMB WITH THRUST AT N1 106.0 LEFT AND RIGHT VIBRATION FELT THRU AIRFRAME. VIB INDICATION PEAKED AT LEFT 2.8 FAN / RIGHT 2.5 FAN
- [SDR IPXA2021090373496](https://openairdocs.org/sdr/IPXA2021090373496), Aug 28, 2021: STIFFENER. CRACKED. 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.81.00 AND UPS 
- [SDR IPXA2021090373495](https://openairdocs.org/sdr/IPXA2021090373495), Aug 28, 2021: STIFFENER. CRACKED. INSPECTION TYPE:C6CRACK ON CENTER WING TANK STIFFENER (P/N: 111T2008-12) ON STA 785.9, RBL 33.REPAIR I.A.W 767-300F SRM 57-10-10-2R-2 REPAIR 2 REV.81.00 AND UPS
- [SDR IPXA2021080272322](https://openairdocs.org/sdr/IPXA2021080272322), Aug 1, 2021: SKIN. DAMAGED. INSPECTION TYPE:N/ADAMAGE AT UPPER SKINREPAIR IAW EO B767-5750-80271
- [SDR IPXA2021072572048](https://openairdocs.org/sdr/IPXA2021072572048), Jul 25, 2021: FLOOR PANEL. DAMAGED. INSPECTION TYPE:N/AMAIN CARGO DECK FLOOR PANEL DAMAGED ALONG CENTERLINE OF POSITIONMANUFACTURED NEW PANEL IAW UPS E.O. B767-5320-9693-I ON NRC 663732
- [SDR IPXA2020071755824](https://openairdocs.org/sdr/IPXA2020071755824), Jul 15, 2020: LIGHT. INOPERATIVE. EXTERIOR EMERGENCY EGRESS LIGHT WAS INOPERATIVE. REPLACED THE LAMPS FOR THE EXTERIOR EMERGENCY ESCAPE LIGHT IAW AMM 33 51 16. OPS CHECKED NORMAL.
- [SDR IPXA2019090246227](https://openairdocs.org/sdr/IPXA2019090246227), Sep 1, 2019: FSEU. FAULTED. INSPECTION TYPE:N/AATB - EMERGENCY DECLARED -AT FL 350 AT MACH .80, 270 KIAS THE LEADING EDGE SLAT ASSYMETRY ANNUNCIATED. EICAS MESSAGE LE SLAT ASYM, LEADING WA
- [SDR IPXA2018101835116](https://openairdocs.org/sdr/IPXA2018101835116), Oct 17, 2018: SKIN PANEL. ERODED. VERTICAL STAB RT L/E PANEL ABOVE HF ANTENNA ERODED. REMOVED ERODED COMPOSITE AND INSTALLED COMPOSITE REPAIR IAW SRM 55-30-01-2R-6 AND 51-70-17. (MINOR)
- [SDR IPXA2018082033021](https://openairdocs.org/sdr/IPXA2018082033021), Aug 19, 2018: MANIFOLD. BROKEN. NUMBER 2 ENGINE, FROM APPROXIMATELY 5 - 6 O'CLOCK POSITIONS, TCC MANIFOLD WAS BROKEN, TWO 1/2 INCH DIAMETER TUBES HAVE SEPARATED FROM MAIN MANIFOLD. REPLACED TC
- [SDR IPXA2018081032629](https://openairdocs.org/sdr/IPXA2018081032629), Aug 10, 2018: PUMP. INOPERATIVE. CENTER FUEL PUMP EICAS AND LOW PRESS LIGHT ON WITH 1000LBS OF FUEL REMAINING IN THE CENTER TANK. LEFT PUMP CONTINUED NORMAL OPS UNTIL CENTER TANK DEPLETED. AIRC
- [SDR IPXA2017090721461](https://openairdocs.org/sdr/IPXA2017090721461), Sep 7, 2017: WARNING MESSAGE. ILLUMINATED. EICAS STATUS MESSAGE FOR THE RT ENGINE FIRE LOOP 2 DISPLAYED PRIOR TO BLOCK OUT. OPEN.
- [SDR IPXA2017080320093](https://openairdocs.org/sdr/IPXA2017080320093), Aug 2, 2017: CONNECTOR. UNSECURE. DURING DESCENT EMERGENCY EXIT LIGHTS CAME ON INTERMITTENTLY. RESET CONNECTOR ON EMERGENCY EXIT LIGHTS BATTERY PACK SYS. OPS. CHECK NORMAL IAW MM 33-51-00-715-03
- [SDR IPXA2016100108822](https://openairdocs.org/sdr/IPXA2016100108822), Oct 1, 2016: FLOOR PANEL. DAMAGED. MCD FLOOR PANEL POS 4 CTR IS DAMAGED. FABRICATED A NEW PANEL REF EO B767-5320-9693-I.
- [SDR IPXA2015093094120](https://openairdocs.org/sdr/IPXA2015093094120), Sep 30, 2015: SKIN. CRACKED. INSPECTION TYPE: C3, CRACK DAMAGE WAS FOUND ON FASTENER HOLE 1EA OF RT WING LOWER SKIN, PN: 112T4702-8 AT STR L-6.5, NEAR W STA 995. REPAIR IAW SR: 3-3412176606
- [SDR IPXA2015092994077](https://openairdocs.org/sdr/IPXA2015092994077), Sep 29, 2015: SLEEVE. DAMAGED. INSPECTION TYPE:C, DURING MAJOR MAINTENANCE VISIT 6764, FOUND DAMAGE - NR 1 EXHAUST SLEEVE OUTER SKIN DAMAGE 6 TO 7 O'CLOCK POSITION NAC BS 321TO 339REF EGAT NR
- [SDR IPXA2015090493121](https://openairdocs.org/sdr/IPXA2015090493121), Sep 4, 2015: COOLING FAN. INOPERATIVE. INSPECTION TYPE:ETOP, FWD EXHAUST FAN STATUS MSG DISPLAYED . ITEM DEFERRED IAW MEL 21-58-4-2-1. C/W IAW DMP 21-58-4-2-1, DMI M559969 . INSTALLED PLACARD . NR T2
- [SDR IPXA2015013085508](https://openairdocs.org/sdr/IPXA2015013085508), Jan 29, 2015: RELAY. INOPERATIVE. DURING NOSE GEAR EXTENSION, NUMERIOUS WARNING LIGHTS ILLUMINATED ON FWD INST PANEL ALONG WITH SW MODE CONTROL PANEL LIGHTS. NO ASSOCIATED WARNING HORNS OR EICAS
- [SDR IPXA2014092684424](https://openairdocs.org/sdr/IPXA2014092684424), Sep 24, 2014: WARNING MESSAGE. FALSE INDICATION. LEFT ENGINE FIRE LOOP 1 STATUS MESSAGE. OPS CHECKED IAW AMM TASK 26-00-00. NO FAULTS NOTED AT THIS TIME.
- [SDR IPXA201406043158](https://openairdocs.org/sdr/IPXA201406043158), Jun 2, 2014: FLOOR PANEL. PUNCTURED. MAIN CARGO FLOOR PANEL 6 HAS A HOLE, REPAIRED IAW SRM 53-00-50-2R-4C.
- [SDR IPXA2014060283150](https://openairdocs.org/sdr/IPXA2014060283150), Jun 1, 2014: FLOOR PANEL. DAMAGED. MAIN CARGO FLOOR PANEL DAMAGED. FABRICATED NEW FLOOR PANEL IAW EO B767-5320-9693-H.
- [SDR IPXA2014060283149](https://openairdocs.org/sdr/IPXA2014060283149), Jun 1, 2014: FLOOR PANEL. DAMAGED. MAIN CARGO FLOOR PANEL DAMAGED. FABRICATED NEW FLOOR PANEL IAW EO B767-5320-9693-H.
- [SDR IPXA2014060283144](https://openairdocs.org/sdr/IPXA2014060283144), Jun 1, 2014: FLOOR PANEL. DAMAGED. MAIN CARGO FLOOR PANEL DAMAGED. FABRICATED NEW FLOOR PANEL IAW EO-B767-5320-9693-H.
- [SDR IPXA2014052783065](https://openairdocs.org/sdr/IPXA2014052783065), May 26, 2014: FLOOR PANEL. DAMAGED. MAIN CARGO DECK FLOOR PANEL HAS NUMEROUS AREAS OF DAMAGE. FABRICATED AND REPLACED THE FLOOR PANEL IAW EO B767-5320-9693-H.
- [SDR IPXA2014052783064](https://openairdocs.org/sdr/IPXA2014052783064), May 26, 2014: FLOOR PANEL. DAMAGED. MAIN CARGO DECK FLOOR PANEL HAS NUMEROUS DAMAGES, FABRICATED AND REPLACED IAW EO B767-5320-9693-H.
- [SDR IPXA2675534](https://openairdocs.org/sdr/IPXA2675534), Sep 23, 2012: D-RING. MISSING. COCKPIT EMERGENCY ESCAPE DESCENT HARNESS HAS ONE D-RING MISSING. R & R EMERGENCY ESCAPE DESCENT HARNESS ASSY IAW GMM 25-61-00.
- [SDR IPXA12673048](https://openairdocs.org/sdr/IPXA12673048), Apr 17, 2012: INDICATOR. FAILED. DUE TO CAPTAIN`S AIRSPEED INDICATION INOPERATIVE, ALTERNATE AIR DATA SELECTED, FAILED TO CORRECT PROBLEM. CHECKED CAPTAIN`S AIRSPEED INDICATOR CONDITION, POWER 
- [SDR IPXA2672594](https://openairdocs.org/sdr/IPXA2672594), Mar 22, 2012: CONNECTOR. LOOSE. T/E FLAP DISAGREE ON APPROACH, WHEN FLAPS SELECTED PAST 5. ACCOMPLISHED T/E DISAGREE AND LANDED FLAPS 20. EMERGENCY DECLARED. LANDED WITHOUT INCIDENT. FOUND NR 
- [SDR IPXA12672517](https://openairdocs.org/sdr/IPXA12672517), Mar 22, 2012: CONNECTOR. LOOSE. T/E FLAP DISAGREE ON APP WHEN FLAPS SELECTED PAST 5, ACCOMPLISHED T/E DISAGREE AND LANDED FLAPS 20 EMERGENCY DECLARED. FOUND NR 3 FLAP POSITION TRANSDUCER CONNE
- [SDR IPXA1668640](https://openairdocs.org/sdr/IPXA1668640), Aug 15, 2011: SHUTOFF VALVE. DIRTY. INSPECTION TYPE: ETOP, LT ENGINE BLEED EICAS MSG AND SWITCH LIGHT ILLUMINATED. MANUALLY CYCLED PRSOV AND CLEANED C/P. ENG RAN BY CREW CHECK OK IAW AMM 36-11-00-
- [SDR IPXA1666288](https://openairdocs.org/sdr/IPXA1666288), Apr 30, 2011: COUNTERBALANCE. OUT OF ADJUST. CREW ENTRY DOOR VERY DIFFICULT TO OPEN (DOOR ITSELF, NOT HANDLE). NO FEELING OF "ASSIST" IN RAISING DOOR TO OPEN POSITION. ADJUSTED COUNTER BALANCE IAW MM 52-12
- [SDR IPXA1664029](https://openairdocs.org/sdr/IPXA1664029), Jan 5, 2011: SEAL. DAMAGED. MAIN CABIN DOOR VERY STIFF DURING OPERATION. EXCESSIVE FORCE REQUIRED TO OPEN AND CLOSE. FOUND FWD DOOR TRIM SEAL BUNCHING UP AT 30-35 IN FROM FLOOR REF IPC 52-
- [SDR IPXA10663317](https://openairdocs.org/sdr/IPXA10663317), Oct 24, 2010: FLOORBOARD. DENTED. REF DMI D429161, MAIN CARGO DECK POS NR 2 RT FLOORBOARD - 2ND BOARD IN FROM OTBD HAS A 1-INCH BY 1-INCH DENT. REPLACED FLOORBOARD WORKING WITH EO B767-5320-9693
- [SDR IPXA10662386](https://openairdocs.org/sdr/IPXA10662386), Sep 7, 2010: DETECTOR. INOPERATIVE. INSPECTION TYPE:E, TOP ATB - RT DUCT LEAK LIGHT ILLUM AND ASSOCIATED EICAS MSG R BLD DUCT LEAK DISPLAYED. IAW FIM 26-18-00, FIG 104. R & R M691 CONDITION RECURS
- [SDR IPXA10662140](https://openairdocs.org/sdr/IPXA10662140), Aug 25, 2010: SKIN. GOUGED. RT SIDE FUSELAGE SKIN GOUGED AFT OF FWD LOWER CARGO DOOR AT STA 610R AND BETWEEN STRINGERS S30 & S29 RT. ACCOMPLISHED PERMANENT REPAIR OF SKIN DAMAGE AT STA 612
- [SDR IPXA10660753](https://openairdocs.org/sdr/IPXA10660753), Jun 26, 2010: LAMP. INOPERATIVE. INSPECTION TYPE:PS, EMERGENCY LIGHT BELOW CREW ENTRANCE OUT. RELAMPED IAW AMM33-51-16-2.

## 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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