# N336UP: 2009 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: 37857
- Year built: 2009
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: October 23, 2009
- Certificate issued: October 27, 2009
- Expires: August 31, 2028
- Mode S code: A3ADE9
- 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=336UP
- Page: https://openairdocs.org/aircraft/N336UP

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 N336UP.

## FAA accident and incident reports

None matched to N336UP.

## Service difficulty reports (64, 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 IPXA2026091324623](https://openairdocs.org/sdr/IPXA2026091324623), Jun 18, 2026: STRUCTURE. DAMAGED. MAJOR REPAIR. APPARENT DAMAGE TO TRAILING EDGE OF RUDDER. APPROX 3/4 OF THE WAY TO THE TOP. STEPS 3-7 COMPLETED PER EO-97804-REQ3. BMS 8-301 PO: SP2917496, BMS 
- [SDR IPXA2026030592144](https://openairdocs.org/sdr/IPXA2026030592144), Jan 27, 2026: WINDOW. SCRATCHED. MULTI SCRATCHES ON OUTSIDE L2 WINDOW HARD TO SEE THOUGH NIGHT GLARE. COMPLETED REMOVING THE L2 WINDOW AND INSTALLED THE NEW L2 WINDOW AS PER B767 56-11-02. WIND
- [SDR IPXA2026012892144](https://openairdocs.org/sdr/IPXA2026012892144), Jan 27, 2026: WINDOW. SCRATCHED. MULTI SCRATCHES ON OUTSIDE L2 WINDOW, HARD TO SEE THOUGH NIGHT GLARE. R & R THE L2 WINDOW ASSY IAW AMM 56-11-02-004-001 UP TO STEP D-4.
- [SDR IPXA2025021782529](https://openairdocs.org/sdr/IPXA2025021782529), Feb 17, 2025: WEDGE. DEBONDED. NUMBER 10 SLAT OUTBOARD TRAILING EDGE, WEDGE DISBOND (REPAIR). .I.A.W AMM 20-11-00-910-802 REV.144 INSTALL 624FT,625AT. I.A.W AMM 27-81-02-424-099 REV 144 STEP 
- [SDR IPXA2025021774905](https://openairdocs.org/sdr/IPXA2025021774905), Feb 16, 2025: WEDGE. DEBONDED. NR 10 SLAT, INBOARD TRAILING EDGE, WEDGE DISBOND (REPAIR). CLEAN, SEAL AND FINFISH AT REPAIR AREA I.A.W. 767-300F SRM 51-70-10-2R-0 PARAGRAPH 22 REV.91. I.A.W A
- [SDR IPXA2025021774931](https://openairdocs.org/sdr/IPXA2025021774931), Feb 16, 2025: WEDGE. CHAFED. NUMBER 9 SLAT, OUTBOARD TRAILING EDGE, WEDGE CHAFING WORN (REPAIR). .I.A.W AMM 30-11-06-404-009 REV 144 INSTALLED THE NO.8 TO NO.9 SLAT INTERSTITIAL DUCT. I.A.W
- [SDR IPXA2025021763483](https://openairdocs.org/sdr/IPXA2025021763483), Feb 15, 2025: SKIN. DEBONDED. DISBOND - SKIN, OUTBD EDGE OF L/H WING NO.3 SLAT T/E SKIN (REPAIR). I.A.W AMM 51-21-10-307-020 REV.144, REPAINT REWORK AREA. JOB COMPLETED AND CONDITION CHECK N
- [SDR IPXA2025021900375](https://openairdocs.org/sdr/IPXA2025021900375), Feb 12, 2025: ANGLE. CRACKED. FOUND THE ANGLE CRACK AT STA 1578 RBL 80 OUTBOARD IN BULK CARGO COMPARTMENT RIGHT AREA. (REPLACE). INSTALL NEW PARTS I.A.W SRM 51-40-02-0G REV.91 AND BOEING DWG
- [SDR IPXA2025021900355](https://openairdocs.org/sdr/IPXA2025021900355), Feb 12, 2025: ANGLE. CRACKED. FOUND THE ANGLE CRACK AT STA 1578 LBL 80 OUTBOARD IN BULK CARGO COMPARTMENT LEFT AREA. (REPLACE). I.A.W AMM 25-59-01-404-019 REV.144 INSTALL MAIN DECK CARGO DAD
- [SDR IPXA2025021982679](https://openairdocs.org/sdr/IPXA2025021982679), Feb 11, 2025: STIFFENER. CRACKED. CRACK, CENTER WING FRONT SPAR STIFFENER AT STA 785.9 RBL 11 (REPAIR). REPAIR DAMAGE AREA I.A.W SRM 57-10-10-2R-2 REV. 91, EGAT WORK SHEET NO.50116 AND UPS SREO-
- [SDR IPXA2025021982753](https://openairdocs.org/sdr/IPXA2025021982753), Feb 11, 2025: STIFFENER. CRACKED. CRACK, CENTER WING FRONT SPAR STIFFENER AT STA 785.9 RBL 33 (REPAIR). REPAIR DAMAGE AREA I.A.W SRM 57-10-10-2R-2 REV.91, EGAT WORK SHEET NO. 50115 AND UPS SREO-
- [SDR IPXA2025021982583](https://openairdocs.org/sdr/IPXA2025021982583), Feb 11, 2025: STIFFENER. CRACKED. CRACK, CENTER WING FRONT SPAR STIFFENER AT STA 785.9 LBL 11 (REPAIR). REPAIR DAMAGE AREA I.A.W SRM 57-10-10-2R-2 REV.91, EGAT WORK SHEET NO. 50114 AND UPS SREO-
- [SDR IPXA2025021584056](https://openairdocs.org/sdr/IPXA2025021584056), Feb 11, 2025: FLOOR PANEL. DENTED. FOUND MAIN DECK FLOOR PANEL WITH DENT DAMAGE, P/N: 143T5876-80 PANEL NO.232HFF STA532~STA654+22 RBL55~RBL77 (REPAIR). FABRICATE A NEW FLOOR PANEL I.A.W. SREO-96
- [SDR IPXA2025021584089](https://openairdocs.org/sdr/IPXA2025021584089), Feb 11, 2025: FLOOR PANEL. DENTED. FOUND MAIN DECK FLOOR PANEL WITH DENT DAMAGE, P/N:146T5869-67 PANEL NO.251HFF STA 1197+22~STA1197+120 LBL33~LBL55 (REPAIR). FABRICATE A NEW FLOOR PANEL I.A.W. S
- [SDR IPXA2025021584028](https://openairdocs.org/sdr/IPXA2025021584028), Feb 11, 2025: FLOOR PANEL. DENTED. FOUND MAIN DECK FLOOR PANEL WITH DENT DAMAGE, P/N: 146T5869-10 PANEL NO.252HFF STA 1197+22~STA1197+120 RBL77~RBL88 (REPAIR). FABRICATE A NEW FLOOR PANEL I.A.W. 
- [SDR IPXA2025021584025](https://openairdocs.org/sdr/IPXA2025021584025), Feb 11, 2025: FLOOR PANEL. DENTED. FOUND MAIN DECK FLOOR PANEL WITH DENT DAMAGE, P/N:143T5876-82 PANEL NO.252GFF STA 532~STA 654+22 RBL33~RBL55 (REPAIR). FABRICATE A NEW FLOOR PANEL I.A.W. SREO-9
- [SDR IPXA2024061787089](https://openairdocs.org/sdr/IPXA2024061787089), Jun 17, 2024: CDU. FAILED. AIR TURNBACK, AT LEVELING OFF AT CRUISE THE LEFT FMC SCREEN WENT BLANK. LEFT CDU IS INOP. WHEN NAV SELECT SWITCH SET TO CDU-L RECEIVED A VTK FLAG ON NAV DISPLAY
- [SDR IPXA2023122183975](https://openairdocs.org/sdr/IPXA2023122183975), Dec 21, 2023: DOOR. LEAKING. DURING CLIMB LOUD SQUEAL FROM MAIN CABIN DOOR, STOPS AT CRUISE. MAIN ENTRY DOOR SEAL REINSTALLED IAW AMM 52-09-01-424-019.
- [SDR IPXA2023113091796](https://openairdocs.org/sdr/IPXA2023113091796), Nov 21, 2023: WINDOW. LEAKING. **SUPPLEMENTAL SDR**L2 WINDOW SQUEALING IN FLT R/R L2 WINDOW SEAL PER AMM 56-11-11. LEAK CHECKS GOOD.
- [SDR IPXA2023112291796](https://openairdocs.org/sdr/IPXA2023112291796), Nov 21, 2023: UNKNOWN. UNKNOWN. *SDR FILED OPEN* L2 WINDOW SQUEALING IN FLT PRESSURIZED A/C, FOUND LWR SECTION OF L2 WINDOW HAVING EXCESSIVE LEAKAGE. ORDERED WINDOW ON REQ.
- [SDR IPXA2023071175465](https://openairdocs.org/sdr/IPXA2023071175465), Jul 11, 2023: DOOR. INOPERATIVE. **ATB**LWR FWD CARGO DOOR MESSAGE AFTER TAKEOFF OPENED & CLOSED LWR FWD CARGO ELECTRICALLY, VERIFIED DOOR CLOSED & LOCKED & LATCHED PROPERLY. OK FOR SERVICE IAW
- [SDR IPXA2023051584890](https://openairdocs.org/sdr/IPXA2023051584890), May 3, 2023: TRAY. CRACKED. *SUPPLEMENTAL SDR* FAULT - FOUND AFT CARGO TRAY-LOCK CRACK AT STA 1336 LBL 20. (REPLACE) 1.I.A.W AMM 25-53-22-004-001 REV139.00 REMOVE AFT PALLET LOCK. DRILLING
- [SDR IPXA2023051584762](https://openairdocs.org/sdr/IPXA2023051584762), May 3, 2023: TRAY. CRACKED. *SUPPLEMENTAL SDR* FAULT - FOUND AFT CARGO TRAY-LOCK CRACK AT STA 1336 LBL 43. (REPLACE) 1.I.A.W AMM 25-53-22-004-001 REV139.00 REMOVE AFT PALLET LOCK. DRILLING
- [SDR IPXA2023050884762](https://openairdocs.org/sdr/IPXA2023050884762), May 3, 2023: UNKNOWN. UNKNOWN. *SDR FILED OPEN* FAULT - FOUND AFT CARGO TRAY-LOCK CRACK AT STA 1336 LBL 43. (REPLACE) 3.DRILLING NEW HOLDS FOR TRAY-LOCK IAW SRM51-40-05-0G REV.86.00
- [SDR IPXA2023050884890](https://openairdocs.org/sdr/IPXA2023050884890), May 3, 2023: UNKNOWN. UNKNOWN. *SDR FILED OPEN* FAULT - FOUND AFT CARGO TRAY-LOCK CRACK AT STA 1336 LBL 20. (REPLACE) DRILLING NEW HOLE FOR TRAY-LOCK I.A.W SRM 51-40-05-0G REV.86.00.
- [SDR IPXA2023040692658](https://openairdocs.org/sdr/IPXA2023040692658), Apr 6, 2023: SEAL. LOOSE. INSPECTION TYPE:NAPASSING 10000' A LOUD SQUEAL EMITTED FROM MAIN DOOR. STOPPED SQUEALING APPROX 18000'. NO CHANGES TO PRESSURIZATION, CABIN ALTITUDE, OR (ILLEG)
- [SDR IPXA2023012769293](https://openairdocs.org/sdr/IPXA2023012769293), Jan 26, 2023: SEAL. LOOSE. INSPECTION TYPE:N/ACOULD HEAR AIR LEAKING FROM UNDER LT FWD ENTRY DOOR NO OTHER INDICATIONSFOUND SEGMENT OF DOOR SEAL LOOSE AT BOTTOM SIDE OF ENTRY DOOR REINSTA
- [SDR IPXA2022120588693](https://openairdocs.org/sdr/IPXA2022120588693), Dec 5, 2022: PROXIMITY SENSOR. OUT OF ADJUST. ALERT L1 FWD ENTRY DOOR INDICATION, ADJUSTED PROX SENSORS, THEN OPS CHKD NORMAL PER AMM 52-71-00/501
- [SDR IPXA2022120588717](https://openairdocs.org/sdr/IPXA2022120588717), Dec 3, 2022: DOOR. OUT OF ADJUST. LEFT FWD ENTRY DOOR EICAS, RESULTED IN BTB. TROUBLESHOT IAW FIM 52-71-00-815-805 & WDM 52-71-11. ADJUSTED IAW AMM 52-71-00-825-141 AND ENGINE RUN CHECKED NORMAL
- [SDR IPXA2022112888492](https://openairdocs.org/sdr/IPXA2022112888492), Nov 28, 2022: PROXIMITY SENSOR. NOT REPORTED. LEFT FWD ENTRY DOOR INDICATION SYS. C/W E.O NO.B767-5210-85344-A. DOOR FUNCTION OPS SATISFACTORY. INSTALLED L1 ENTRY DOOR PROXIMITY SENSOR SUPPORT BRACKET DOOR 
- [SDR IPXA2022112888467](https://openairdocs.org/sdr/IPXA2022112888467), Nov 28, 2022: SEAL. DIRTY. INSPECTION TYPE:N/ATHE CREW ENTRY DOOR WAS MAKING LOUD NOISE AND HISSING SOUND WHEN AIRBONE. DOOR APPEARED TO BE OUT OF ALIGNMENTINSPECTED CREW ENTRY DOOR SEALS
- [SDR IPXA2022110787910](https://openairdocs.org/sdr/IPXA2022110787910), Nov 5, 2022: SEAL. OUT OF POSITION. INSPECTION TYPE:NALOUD SQUEAL HEARD FROM ENTRY DOOR ON CLIMB OUTFOUND 6" SECTION OF ENTRY DOOR FLOOR SIDE SEAL OUT OF TRACK. RE INSTALLED LOOSE SEAL I.A.W AMM 5
- [SDR IPXA2022041881272](https://openairdocs.org/sdr/IPXA2022041881272), Apr 15, 2022: NONE. INOPERATIVE. INSPECTION TYPE:N/AENTRY DOOR EXCESSIVE NOISE DURING PRESSURIZATION.FOUND SEATING OF CREW ENTRY DOOR SEAL PULLED OUT OF TRACK, REINSTALLED SEAL OPS CK GOOD AT T
- [SDR IPXA2022032280374](https://openairdocs.org/sdr/IPXA2022032280374), Mar 22, 2022: DOOR. INOPERATIVE. INSPECTION TYPE:N/AFRM CODE 5210400 APPARENT AIR LEAK FROM CREW ENTRY DOOR DURING CLIMB LOWER DOOR SEAL SUSPECTEDINSPECTED CREW ENTRY DOOR SEALS FOUND SEAL OUT 
- [SDR IPXA2022021378909](https://openairdocs.org/sdr/IPXA2022021378909), Feb 12, 2022: NONE. NONE. INSPECTION TYPE:NACREW ENTRY DOO HAS LOUD AIR LEAK AT THE BOTTOM LEFT SIDEFOUND A 4' SECTION OF SEAL OUTSIDE THE SEAL TRACK AT BOTTOM OF THE DOOR. REINSTALLED S
- [SDR IPXA2022020378603](https://openairdocs.org/sdr/IPXA2022020378603), Feb 2, 2022: NONE. NONE. INSPECTION TYPE:NAAIR NOISE FROM LOWER RIGHT CORNER OF CREW ENTRY DOORINSPECTED CREW ENTRY DOOR, FOUND DOOR SEAL OUT OF THE TRACK. REINSTALLED DOOR SEAL IAW AMM
- [SDR IPXA2022012678293](https://openairdocs.org/sdr/IPXA2022012678293), Jan 26, 2022: NONE. NONE. INSPECTION TYPE:N/ADURING CLIMB, PASSING 14000FT HAD PRESSURE SQUEAL COMING FROM MAIN ENTRY DOOR- CABIN PRESS WAS FINE FOR ENTIRE FLIGHT JUST HAD NOISE- SQUEAL 
- [SDR IPXA2022011177766](https://openairdocs.org/sdr/IPXA2022011177766), Jan 10, 2022: NONE. NONE. INSPECTION TYPE:ETOP**SUPPLEMENTAL ETOPS**AT FL 340 L AFT FUEL PUMP EICAS MSG. TRANSFERED TO DEFERRAL MEL 28-22-1 DMI C/WWIRING REPLACED IAW WDM 28-22-11. OPS C
- [SDR IPXA2021113076487](https://openairdocs.org/sdr/IPXA2021113076487), Nov 30, 2021: NONE. NONE. INSPECTION TYPE:N/AGEAR DISAGREE EICAS AND GEAR DOORS EICAS MSGS SHOWS RIGHT GEAR STUCK IN DOWN POSITION.T/SHOOTED PER FIM32-30-00-815-820 BLOCK 4, FOUND HYD LE
- [SDR IPXA2021093074446](https://openairdocs.org/sdr/IPXA2021093074446), Sep 30, 2021: DOOR. LEAKING. INSPECTION TYPE:N/ACREW ENTRY DOOR LEAKS VERY LOUD DURING CLIMB / CRZ CABIN ALT PRESS NORMALFOUND ENTRY DOOR SEAL OUT OF TRACK AT LOWER END ABOUT 8" REINSTALLED
- [SDR IPXA2021040267650](https://openairdocs.org/sdr/IPXA2021040267650), Apr 1, 2021: SEAL. LOOSE. CREW ENTRY DOOR HAS NOISE FROM AIR LEAK. THE NOISE BEGAN AROUND 14,000' AND SLOWLY DISSIPATED AS WE CLIMBED INTO THE MID 20'S.FOUND LOOSE SEAL UNDER CREW ENTRY 
- [SDR IPXA2021032567266](https://openairdocs.org/sdr/IPXA2021032567266), Mar 25, 2021: CONTROL PANEL. INOPERATIVE. INSPECTION TYPE:N/AEMER LIGHTS: WITH OVHD SWITCH OFF, EMER LIGHTS EICAS ILLUMINATED, BUT OVHD LIGHT DID NOT ILLUMINATE.R&R EMERGENCY LIGHT PANEL ASSY IAW AMM 33
- [SDR IPXA2020111962565](https://openairdocs.org/sdr/IPXA2020111962565), Nov 18, 2020: DOOR. LEAKING. INSPECTION TYPE: N/A CREW ENTRY DOOR SEAL AIR LEAK FROM 5 PSI DIFF TO MAX DIFFERENTIAL PRESSURIZATION NORMAL, REF AMM 52 09 01 401. RESECURED DOOR SEAL AT LOWER
- [SDR IPXA2019112759394](https://openairdocs.org/sdr/IPXA2019112759394), Nov 25, 2019: SEAL. DAMAGED. INSPECTION TYPE:N/AFWD ENTRY DOOR FWD/SIDE DOORWAY SEAL DAMAGE PARTS ON ORDER REF. REQ #292308AREMOVED & REPLACED ENTRY DOOR FWD/SIDE DOORWAY SEAL PER IAW /AMM 
- [SDR IPXA2019111549000](https://openairdocs.org/sdr/IPXA2019111549000), Nov 13, 2019: PANEL. INOPERATIVE. ENTRY DOOR LATCH GUARD PANEL WILL NOT CLOSE. DEFER PER MEL 52-11-2. PLACARD INSTALLED, ITEM #M689473REPLACED CREW ENTRY DOOR COVER HINGE IAW AMM 52-12-25-402-01
- [SDR IPXA2019080214198](https://openairdocs.org/sdr/IPXA2019080214198), Jul 31, 2019: LAMP. INOPERATIVE. EXTERIOR EMERGENCY LIGHT INOPERATIVE .RELAMPED EXTERIOR EMERGENCY LIGHT IAW AMM 33-51-16-962-001. OPS CHECK OK.
- [SDR IPXA2018111205834](https://openairdocs.org/sdr/IPXA2018111205834), Nov 9, 2018: TRU. FAILED. APU FAULT LIGHT ILLUMINATED ON START ATTEMPT, OBSERVED EGT MAX 770 DEG. TROUBLESHOT IAW FIM 49-11-00-815-001. 103 & MINI FLAG 34 APPEARED & SUMMARY SHOWED LUR M
- [SDR IPXA2018110755708](https://openairdocs.org/sdr/IPXA2018110755708), Nov 5, 2018: WARNING MESSAGE. ILLUMINATED. AFTER BLOCK OUT, HAD A LEFT FORWARD WINDOW HEAT EICAS MESSAGE. ACCOMPLISHED AOM PROCEDURE AND IT RESET AFTER ONE RESET. OPERATED NORMALLY. BITE TEST CARRIED OUT
- [SDR IPXA2017050416742](https://openairdocs.org/sdr/IPXA2017050416742), May 2, 2017: BATTERY PACK. INOPERATIVE. INSPECTION TYPE: C4, FOUND EXIT EMERGENCY LIGHTS NOT ILLUMINATING. REPLACED THE BATTERY PACK IAW AMM 33-51-07-022-001, AND AMM 33-51-07-422-012, REV 121. PERFOR
- [SDR IPXA2017050316724](https://openairdocs.org/sdr/IPXA2017050316724), Apr 25, 2017: FLOOR PANEL. DAMAGED. INSPECTION TYPE: C4, DAMAGE ON MAIN DECK CARGO FLOOR PANEL 241WFF, FABRICATED A REPLACEMENT FLOOR PANEL IAW EO B767-5320-9693-I.

All 64: https://openairdocs.org/aircraft/N336UP/reports.md

## STCs that may be installed (OpenAirDocs) (5)

Approved for this aircraft's airframe or engine model, in force first, then newest. The registry doesn't record which STCs an aircraft has; its records do.

### Approved for the engine (GE CF6-80C2B6F)

- [STC SE01543CH](https://openairdocs.org/stc/SE01543CH): Replace Hamilton Sundstrand P/N 778839-13, 778839-14, 778839-19, 778839-20, 778839-37, 778839-38, 816682-1, 840618-2, 880724 carbon bushings with Cook Airtomic P/N AIR22947 Slotted Entry Busing in the High Pressure Shutoff Valve. Cook Airtomic
- [STC SE01478CH](https://openairdocs.org/stc/SE01478CH): Installation of Cook Airtomic alignment joint p/n AIR 22912. Cook Airtomic
- [STC SE01471AT](https://openairdocs.org/stc/SE01471AT): Replace right and left side Rohr, Inc. fire detection harness on GE CF6-80C2 engine. Unison Industries. Lists CF6-80C2 Series
- [STC SE00463LA](https://openairdocs.org/stc/SE00463LA): Install fireproof blankets on the engine fan reverser intermediate fireseal, in lieu of fireproof intumescent coating. This STC is jointly by owned by Hi Temp Insulation and MRA Systems acting through Middle River Aircraft Systems, 103 Chesapeake Park Plaza, Baltimore, MD 21220. Hi Temp Insulation Inc
- [STC SA2227SO](https://openairdocs.org/stc/SA2227SO): Installation of wiring and associated components for utilization of the Rolls Royce, Inc., ARINC, interface/readers UT1317 or UT1317/1, for the purpose of acquisition, recording, and analysis in real time of engine/aircraft/ systems. (767 SERIES POWERED BY RR RB-11-524 SERIES. Rolls Royce, Inc. Lists CF6-80 Series

## Related

- Other Boeing 767-34AF aircraft: https://openairdocs.org/model/boeing-767-34af/aircraft.md
- The GE CF6-80C2B6F engine: https://openairdocs.org/engine/ge-cf6-80c2b6f.md

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