# N338UP: 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: 37944
- Year built: 2010
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: March 25, 2010
- Certificate issued: March 29, 2010
- Expires: November 30, 2029
- Mode S code: A3B557
- Registered owner: [United Parcel Service Co](https://openairdocs.org/faa-owner/UNITED%20PARCEL%20SERVICE%20CO)
- Location: [Louisville, KY](https://openairdocs.org/faa-place/KY/Louisville)
- Owner type: Corporation
- 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=338UP
- Page: https://openairdocs.org/aircraft/N338UP

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 N338UP.

## FAA accident and incident reports

None matched to N338UP.

## Service difficulty reports (55, 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 IPXA2025102120943](https://openairdocs.org/sdr/IPXA2025102120943), Oct 12, 2025: FLOOR SUPPORT. CRACKED. MAIN DECK FLOOR FITTING WAS DAMAGE AT BS 1109, BL 0. REMOVED DAMAGE FITTING IAW SRM 51-40-02-0G REV 93.2. INSTALLED NEW FITTING IAW SRM 51-40-02-0G REV 93, AND 
- [SDR IPXA2025102120558](https://openairdocs.org/sdr/IPXA2025102120558), Oct 12, 2025: ANGLE. CRACKED. FOUND CRACKED ANGLE, BULK CGO COMPT CEILING AREA, BS 1577, LBL 74, INBD SIDE. (REPLACE) INSPECTION COMPLETED FOR MAIN DECK CARGO INSPECTION OF FLOOR PANEL OK TO
- [SDR IPXA2025102120546](https://openairdocs.org/sdr/IPXA2025102120546), Oct 12, 2025: ANGLE. CRACKED. FOUND CRACKED ANGLE, BULK CARGO CEILING AREA, BS 1577, RBL 74, INBD SIDE. INSPECTION COMPLETED, FLOOR PANEL OK TO INSTALL AT BS 1540 - 1599, RBL 54 - 88, PANEL 
- [SDR IPXA2025102120275](https://openairdocs.org/sdr/IPXA2025102120275), Oct 12, 2025: ANGLE. CRACKED. FOUND CRACKED ANGLE, BULK CGO COMPT CEILING AREA, STA 1577 RBL 74 OUTBD SIDE. (REPLACE) INSPECTION COMPLETED FOR DADO PANEL OK TO CLOSE CHECK AT STA 1578 RH SID
- [SDR IPXA2025101320911](https://openairdocs.org/sdr/IPXA2025101320911), Oct 12, 2025: FLOOR PANEL. DAMAGED. FOUND MAIN DECK FLOOR PANEL DAMAGE, PANEL 231AFF. THIS REPAIR IS CLASSIFIED AS MAJOR PER GMM 05-04-01-02. REPAIRED IAW AMM 25-58-01-404-005, AMM 25-57-02-404-16
- [SDR IPXA2025101321049](https://openairdocs.org/sdr/IPXA2025101321049), Oct 12, 2025: FLOOR PANEL. DAMAGED. FOUND MAIN DECK FLOOR PANEL DAMAGE, PANEL 231KFF. THIS REPAIR IS CLASSIFIED AS MAJOR PER GMM 05-04-01-02. REPAIRED IAW AMM 53-01-06-400-801 REV 146. INSTALLED M
- [SDR IPXA2025101320871](https://openairdocs.org/sdr/IPXA2025101320871), Oct 12, 2025: FLOOR PANEL. DAMAGED. FOUND MAIN DECK FLOOR PANEL DAMAGE, PANEL NO : 232JFF. THIS REPAIR IS CLASSIFIED AS MAJOR PER GMM 05-04-01-02. REPAIRED IAW AMM 25-58-04-404-015, AMM 25-57-02-4
- [SDR IPXA2025101320914](https://openairdocs.org/sdr/IPXA2025101320914), Oct 12, 2025: FLOOR PANEL. DAMAGED. FOUND MAIN DECK FLOOR PANEL DAMAGE, PANEL 232FFF. THIS REPAIR IS CLASSIFIED AS MAJOR PER GMM 05-04-01-02. REPAIRED IAW AMM 25-57-02-404-016 REV.146. INSTALLED M
- [SDR IPXA2025101320971](https://openairdocs.org/sdr/IPXA2025101320971), Oct 12, 2025: FLOOR PANEL. DAMAGED. FOUND MAIN DECK FLOOR PANEL DAMAGE, PANEL 231EFF. THIS REPAIR IS CLASSIFIED AS MAJOR PER GMM 05-04-01-02. REPAIRED IAW AMM 53-01-06-400-801, REV 146. INSTALLED 
- [SDR IPXA2025101321062](https://openairdocs.org/sdr/IPXA2025101321062), Oct 12, 2025: FLOOR PANEL. DAMAGED. FOUND MAIN DECK FLOOR PANEL DAMAGE, PANEL 231CFF. THIS REPAIR IS CLASSIFIED AS MAJOR PER GMM 05-04-01-02. REPAIRED IAW AMM 53-01-06-400-801 REV.146. INSTALLED M
- [SDR IPXA2025101320957](https://openairdocs.org/sdr/IPXA2025101320957), Oct 12, 2025: FLOOR PANEL. DAMAGED. FOUND MAIN DECK FLOOR PANEL DAMAGE, PANEL 231BFF. THIS REPAIR IS CLASSIFIED AS MAJOR PER GMM 05-04-01-02. REPAIRED IAW AMM 53-01-06-400-801 REV.146. INSTALLED M
- [SDR IPXA2025101321174](https://openairdocs.org/sdr/IPXA2025101321174), Oct 12, 2025: FLOOR PANEL. DAMAGED. FOUND MAIN DECK FLOOR PANEL DAMAGE, PANEL 231DFF. THIS REPAIR IS CLASSIFIED AS MAJOR PER GMM 05-04-01-02. REPAIRED IAW AMM 53-01-06-400-801 REV.146. INSTALLED M
- [SDR IPXA2025101321023](https://openairdocs.org/sdr/IPXA2025101321023), Oct 12, 2025: FLOOR PANEL. DAMAGED. FOUND MAIN DECK FLOOR PANEL DAMAGE, PANEL 231HFF. REPAIRED IAW AMM 25-57-02-404-016 REV.146, INSTALLED MAIN DECK CARGO HANDLING AND CONDITION CHECK NORMAL
- [SDR IPXA2025101320979](https://openairdocs.org/sdr/IPXA2025101320979), Oct 12, 2025: FLOOR PANEL. DAMAGED. FOUND MAIN DECK FLOOR PANEL DAMAGE, PANEL 232CFF. REPAIRED IAW AMM 53-01-06-400-801 REV.146, INSTALLED MAIN DECK CARGO FLOOR PANEL AND CONDITION CHECK NORMAL.
- [SDR IPXA2025101320990](https://openairdocs.org/sdr/IPXA2025101320990), Oct 12, 2025: FLOOR PANEL. DAMAGED. FOUND MAIN DECK FLOOR PANEL DAMAGED, PANEL 231FFF. REPAIRED IAW AMM 53-01-06-400-801 REV.146. INSTALLED MAIN DECK CARGO FLOOR PANEL AND CONDITION CHECK NORMAL.
- [SDR IPXA2025101321005](https://openairdocs.org/sdr/IPXA2025101321005), Oct 12, 2025: FLOOR PANEL. DAMAGED. FOUND MAIN DECK FLOOR PANEL DAMAGE, PANEL 231GFF. FOUND MAIN DECK FLOOR PANEL, CHECK NORMAL.
- [SDR IPXA2025101320955](https://openairdocs.org/sdr/IPXA2025101320955), Oct 12, 2025: FLOOR PANEL. BROKEN. FOUND MAIN DECK FLOOR PANEL DAMAGED, PANEL 232GFF. REPAIRED IAW AMM 53-01-06-400-801, REV146. INSTALLED MAIN DECK CARGO FLOOR PANEL AND CONDITION CHECK NORMAL.
- [SDR IPXA2025101988628](https://openairdocs.org/sdr/IPXA2025101988628), Oct 10, 2025: BATTERY PACK. NO TEST. FOUND EMERGENCY BATTERY PACK CAPACITY TEST FAILED. IAW AMM 33-51-07-022-001, 33-51-07-422-012, REV.146 REPLACED BATTERY PACK.
- [SDR IPXA2025101088628](https://openairdocs.org/sdr/IPXA2025101088628), Oct 10, 2025: BATTERY PACK. NO TEST. -FOUND EMERGENCY BATTERY PACK CAPACITY TEST FAIL (REPLACE)
- [SDR IPXA2025030410453](https://openairdocs.org/sdr/IPXA2025030410453), Mar 1, 2025: LIGHT. INOPERATIVE. UNARMED EMERGENCY LIGHT INOP. (SWITCH BROKEN) R/R EMERGENCY UNARMED LIGHT ASSY IAW SWPM 20-84-18. OPS CHECK SAT.
- [SDR IPXA2024112227733](https://openairdocs.org/sdr/IPXA2024112227733), Nov 21, 2024: COVER. DETACHED. PLASTIC COVER FOR LEVER TO SECURE ENTER DOOR FOUND ON FLOOR DURING FLIGHT REINSTALLED ENTERY DOOR ARM LEVER COVER PER AMM 52-12-00,
- [SDR IPXA2024030479473](https://openairdocs.org/sdr/IPXA2024030479473), Mar 4, 2024: SKIN. DAMAGED. *SDR FILED OPEN* L/W INBD UPPER FLAP UPPER SURFACE SKIN DAMAGE FOUND ADDITIONAL DAMAGE TO INNER SKIN AT REPAIR LOCATION. STOP DRILLS THRU LOWER SKIN AT TWO LOCA
- [SDR IPXA2023093034734](https://openairdocs.org/sdr/IPXA2023093034734), Sep 22, 2023: STIFFENER. CRACKED. MAJOR REPAIR, CRACK WING CENTER FRONT SPAR STIFFENER AT STA 785.9 LBL 11 (REPAIR)ACCOMPLISHED REPAIR I.A.W SRM 57-10-10-2R-2 REV.87 AND UPS SREO-58151-REQ001 RE
- [SDR IPXA2023093034802](https://openairdocs.org/sdr/IPXA2023093034802), Sep 22, 2023: STIFFENER. CRACKED. FAULT - CRACK WING CENTER FRONT SPAR STIFFENER AT STA 785.9 RBL 11 (REPAIR) REVIEW COMPLETE
- [SDR IPXA2023100550888](https://openairdocs.org/sdr/IPXA2023100550888), Sep 14, 2023: ARMING LEVER. INOPERATIVE. *SUPPLEMENTAL SDR* MAIN ENTRY DOOR ARMING LEVER HINGED COVER WILL NOT REMAIN FLUSH WITH WALL. PROTRUDES STRAIGHT OUT. I.A.W AMM 20-11-00-910-802 REV.139 REPLACE
- [SDR IPXA2023091450888](https://openairdocs.org/sdr/IPXA2023091450888), Sep 14, 2023: UNKNOWN. UNKNOWN. *SDR FILED OPEN* MAIN ENTRY DOOR ARMING LEVER HINGED COVER WILL NOT REMAIN FLUSH WITH WALL. PROTRUDES STRAIGHT OUT ARMING HANDLE HINGED COVER DEFERRED PER MEL 5
- [SDR IPXA2023091285154](https://openairdocs.org/sdr/IPXA2023091285154), Sep 8, 2023: FAN. SMOKE. *EMERGENCY DECLARED* SMOKE AND FUMES ODOR IN THE COCKPIT. DECLARED EMERGENCY ON BASE LEG. LANDED UNEVENTFULLY. EVACUATED AIRCRAFT. DURING R&R OF FWD RACK EXHAUS
- [SDR IPXA2023060589577](https://openairdocs.org/sdr/IPXA2023060589577), Jun 1, 2023: ENGINE. WARNING MESSAGE. AIRTURN BACK. RIGHT ENGINE OVHT EICAS AND R ENG OVH PEDESTAL LIGHT ILLUMINATED. DUCT AND CLAMP REPLACED ON FAULT T3F18E001XK2Z PER AMM 36-11-01/401. SUBTASK C/W
- [SDR IPXA2023011089769](https://openairdocs.org/sdr/IPXA2023011089769), Jan 9, 2023: BATTERY PACK. INOPERATIVE. EMERGENCY LIGHTS INOPERATIVE. R & R THE EMERGENCY LIGHTS BATTERY PACK IAW AMM 33-51-07, OPS CK GOOD.
- [SDR IPXA2022101107029](https://openairdocs.org/sdr/IPXA2022101107029), Oct 10, 2022: POWER SUPPLY. INOPERATIVE. INSPECTION TYPE:N/AEMERGENCY EXIT SIGN BY DOOR INOP SUSPECT BLOWN FUSER&R POWER SUPPLY FOR EMERGENCY EXIT SIGN PER MM 33-51-07 OPS CHECKS OK ESR 33-51-07-32 ITE
- [SDR IPXA2022100686891](https://openairdocs.org/sdr/IPXA2022100686891), Oct 6, 2022: BATTERY PACK. INOPERATIVE. INSPECTION TYPE:N/AF/D EMERGENCY LIGHT INOP. R/R THE CHARGER ASSY AND BATTERY, OPS CK OK PER AMM33-51-07-201,
- [SDR IPXA2022081385188](https://openairdocs.org/sdr/IPXA2022081385188), Aug 12, 2022: LIGHT. INOPERATIVE. INSPECTION TYPE:N/AEMG LIGHTS INOP.REMOVED POWER SUPPLY, CHARGED FOR 3 HOURS AND REINSTALLED IAW AMM 33-51-07. OPS CHECK SAT.
- [SDR IPXA2022033080674](https://openairdocs.org/sdr/IPXA2022033080674), Mar 30, 2022: LIGHT. INOPERATIVE. INSPECTION TYPE:N/AEMERGENCY EXIT SIGN BY ENTRY DOOR LOWER CENTER BULB INOPRELAMPED LOWER CENTER BULB ON EMERGENCY EXIT SIGN BY ENTRY DOOR OPS CHK PER MM 33 51 
- [SDR IPXA2021100174452](https://openairdocs.org/sdr/IPXA2021100174452), Sep 20, 2021: NONE. NONE. INSPECTION TYPE:C6CHAFING ON FRANGIBLE ASSY ON OUTBD EDGE OF L/H WING INBD AFT FLAP.REPAIR I.A.W BOEING SR 4-5204920531 AND UPS EO B767-5750-81767-A
- [SDR IPXA2021093074416](https://openairdocs.org/sdr/IPXA2021093074416), Sep 20, 2021: NONE. NONE. INSPECTION TYPE:C6CHAFING ON FRANGIBLE ASSY ON OUTBD EDGE OF L/H WING INBD AFT FLAP.REPAIR I.A.W BOEING SR 4-5204920531 AND UPS EO B767-5750-81767-A.
- [SDR IPXA2021092774293](https://openairdocs.org/sdr/IPXA2021092774293), Sep 19, 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 EO 
- [SDR IPXA2021091373828](https://openairdocs.org/sdr/IPXA2021091373828), Sep 12, 2021: TUBE. BLOWN. ATB - EMERGENCY DECLARED -LT ENGINE FIRE INDICATION ON EICAS AND FUEL CONTROL SWITCH. ACTICATED ON CLIMB AND THEN EXTINGUISHED AFTER ABOUT 45 SECONDS RESULTING 
- [SDR IPXA2020071317667](https://openairdocs.org/sdr/IPXA2020071317667), Jul 11, 2020: LAMP. INOPERATIVE. EXTERIOR EMERGENCY LIGHT LAMP INOPERATIVE. R & R THE EXTERIOR EMERGENCY LIGHT LAMP IAW AMM 33 51 16 962 001. OPS CHECKED GOOD.
- [SDR IPXA2020041554205](https://openairdocs.org/sdr/IPXA2020041554205), Apr 13, 2020: BATTERY. DISCHARGED. INSPECTION TYPE:N/AEMERGENCY LIGHTS INOPR&R EMERGENCY BATTERY PACK PER AMM 33-51-07-201 OPS CKS GOOD
- [SDR IPXA2019121875136](https://openairdocs.org/sdr/IPXA2019121875136), Dec 16, 2019: WARNING MESSAGE. FALSE ACTIVATION. LEFT FWD ENTRY DOOR EICAS ILLUMINATED DURING PUSH-BACK. INSPECTED DOOR SENSORS S195 AND S194. NO BITE HISTORY OF LT FWD ENTRY DOOR. SENSOR AND TARGET POSITION T
- [SDR IPXA2019071244363](https://openairdocs.org/sdr/IPXA2019071244363), Jul 12, 2019: WARNING SYSTEM. FALSE ACTIVATION. INSPECTION TYPE:N/A EICAS MSG R ENG HPSOV ON SHORT FINAL. XFERRED TO STATUS MSG AFTER TOUCHDOWN. ACC FIM 36-10-00-815-833-001 1 TO BOX 5. NO MESSAGES.
- [SDR IPXA201904241398](https://openairdocs.org/sdr/IPXA201904241398), Apr 22, 2019: STRAP. DAMAGED. INSPECTION TYPE:NAL1 ENTRY DR WARNING STRAP DAMAGEDR&R'D W/R/T IPC 52 11 57 11
- [SDR IPXA2018070331355](https://openairdocs.org/sdr/IPXA2018070331355), Jul 3, 2018: LIGHT. INOPERATIVE. EMERGENCY LIGHT BULB AT ENTRY WAY INOP. RELAMPED EMERGENCY LIGHT BULB ENTRY WAY PER AMM 33-15-11.
- [SDR IPXA2017120924325](https://openairdocs.org/sdr/IPXA2017120924325), Dec 9, 2017: LAMP. INOPERATIVE. INSPECTION TYPE:N/AEXTERIOR EMERENCY LIGHT INOPRELAMPED OPS CHECK GOOD PER MM 33-51-16
- [SDR IPXA2017041816252](https://openairdocs.org/sdr/IPXA2017041816252), Apr 18, 2017: SWITCH. INOPERATIVE. EMERGENCY LIGHT SWITCH ON OVERHEAD PANEL DOES NOT STAY ON WITH SWITCH COVER CLOSED. R & R GUARDED SWITCH COVER IAW AMM 33-51-08
- [SDR IPXA2017040615875](https://openairdocs.org/sdr/IPXA2017040615875), Apr 5, 2017: HINGE. BROKEN. :MAIN ENTRY DOOR ARMING COVER HINGE BROKEN. R & R THE BROKEN COVER HINGE FOR THE ARMING LEVER IAW SRM 51-40-02.
- [SDR IPXA2017012013011](https://openairdocs.org/sdr/IPXA2017012013011), Jan 20, 2017: ENGINE. UNKNOWN. INSPECTION TYPE:ETOP IFSD - DURING CLIMBOUT, EICAS MSG L OIL FILTER DISPLAYED. PERFORMED QRH PROCEDURE AND SHUTDOWN THE LEFT ENGINE. R&R NR 1 ENGINE IAW TC 6002
- [SDR IPXA2017011212633](https://openairdocs.org/sdr/IPXA2017011212633), Jan 11, 2017: MODULE. INOPERATIVE. ON LANDING AT N120 KNOTS, RECEIVED AN AURAL CONFIGURATION WARNING. SPOILER, STABILIZER AND CONFIG. EICAS MESSAGES SPEEDBRAKE HANDLE UP NORMALLY BUT NO RESEQUENC
- [SDR IPXA2016052703896](https://openairdocs.org/sdr/IPXA2016052703896), May 27, 2016: SWITCH. INOPERATIVE. EMERGENCY EXIT SWITCH SPRING INOPERATIVE EMERGENCY LIGHTS SWITCH AUTO TO ARM. SPRING RELOCATED TO CORRECT POSITION IAW AMM 33-50-00.
- [SDR IPXA2016022599896](https://openairdocs.org/sdr/IPXA2016022599896), Feb 24, 2016: DOOR. OPEN. CAPT'S OVERHEAD EMERGENCY ESCAPE ROPE DOOR OPENED INFLIGHT DUE TO TURBULENCE AND WILL NOT STAY CLOSED. CAPTAIN'S ESCAPE ROPE DOOR CLOSED AND SECURED IAW AMM 25-

All 55: https://openairdocs.org/aircraft/N338UP/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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