# N328UP: 1998 Boeing 767-34AF

- Status: Valid registration
- Airframe: [Boeing 767-34AF](https://openairdocs.org/model/boeing-767-34af) (registry code 1385212, 190 seats)
- Engine: [GE CF6-45A2](https://openairdocs.org/engine/ge-cf6-45a2) (registry code 30017)
- Data sheets: [TCDS E23EA](https://openairdocs.org/tcds/E23EA) (General Electric Company) (OpenAirDocs)
- Serial number: 27754
- Year built: 1998
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: December 16, 1998
- Certificate issued: December 18, 1998
- Expires: February 28, 2029
- Mode S code: A38DD8
- 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=328UP
- Page: https://openairdocs.org/aircraft/N328UP

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): 29 in force

### Matched by airframe (Boeing 767-34AF)

None in force.

### Matched by engine (GE CF6-45A2)

- [AD 2023-04-11](https://openairdocs.org/ad/2023-04-11): Turbine Section · General Electric CF6-45A, CF6-45A2, CF6-50A and 10 more. Effective Apr 28, 2023
- [AD 2011-23-04](https://openairdocs.org/ad/2011-23-04): Forward engine mount assembly side links · General Electric CF6-45A, CF6-45A2, CF6-50A and 14 more. Effective Dec 12, 2011
- [AD 2011-07-01](https://openairdocs.org/ad/2011-07-01): Forward and aft centerbodies · General Electric CF6-45A, CF6-45A2, CF6-50A and 10 more. Effective Apr 22, 2011
- [AD 2007-19-06](https://openairdocs.org/ad/2007-19-06): Compressor discharge pressure (CDP) · General Electric CF6-45A, CF6-45A2, CF6-50A and 10 more. Effective Oct 23, 2007
- [AD 2005-26-06](https://openairdocs.org/ad/2005-26-06): Low pressure turbine (LPT) stage 2 interstage seal assemblies · General Electric CF6-45A, CF6-45A2, CF6-50A and 10 more. Effective Jan 26, 2006
- [AD 2005-07-05](https://openairdocs.org/ad/2005-07-05): Low pressure turbine (LPT) · General Electric CF6-45A, CF6-45A2, CF6-50A and 10 more. Effective May 4, 2005
- [AD 2005-08-04](https://openairdocs.org/ad/2005-08-04): Low-cycle-fatigue (LCF) · General Electric CF6-45A, CF6-45A2, CF6-50A and 10 more. Effective Apr 28, 2005
- [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 2002-05-03](https://openairdocs.org/ad/2002-05-03): Life-Limited Rotating Parts · General Electric CF6-45A, CF6-45A2, CF6-50A and 15 more. Effective Apr 12, 2002
- [AD 2002-02-09](https://openairdocs.org/ad/2002-02-09): Low Pressure Turbine Rotor (LPTR) Stage 2 Disks · General Electric CF6-45A, CF6-45A2, CF6-50A and 10 more. Effective Mar 15, 2002
- [AD 2000-11-12](https://openairdocs.org/ad/2000-11-12): High Pressure Compressor Disk Lock Slots · General Electric CF6-45A, CF6-45A2, CF6-50A and 10 more. Effective Aug 14, 2000
- [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 95-08-03](https://openairdocs.org/ad/95-08-03): High Pressure Turbine Rotor Stage 2 Disks · General Electric CF6-45A, CF6-45A2, CF6-50A and 10 more. Effective Jun 12, 1995
- [AD 91-10-03 R1](https://openairdocs.org/ad/91-10-03-R1): High Pressure Compressor · General Electric CF6-45A, CF6-45A2, CF6-50A and 10 more. Effective Apr 28, 1995
- [AD 94-08-05](https://openairdocs.org/ad/94-08-05): Fan Stator Case · General Electric CF6-45A, CF6-45A2, CF6-50A and 10 more. Effective Jul 5, 1994
- [AD 94-09-18](https://openairdocs.org/ad/94-09-18): High Pressure Turbine Disk · General Electric CF6-45A, CF6-45A2, CF6-50A and 15 more. Effective Jun 6, 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 93-13-10](https://openairdocs.org/ad/93-13-10): Compressor Spools · General Electric CF6-45A, CF6-45A2, CF6-50A and 10 more. Effective Sep 21, 1993
- [AD 91-15-16](https://openairdocs.org/ad/91-15-16): High Pressure Turbine Thermal Shields · General Electric CF6-45A, CF6-45A2, CF6-50A and 10 more. Effective Sep 4, 1991
- [AD 91-01-04](https://openairdocs.org/ad/91-01-04): Fan Disk · General Electric CF6-45A, CF6-45A2, CF6-50A and 19 more. Effective Jan 22, 1991
- [AD 90-23-15](https://openairdocs.org/ad/90-23-15): Turbine Mid-frame · General Electric CF6-45A, CF6-45A2, CF6-50A and 10 more. Effective Dec 6, 1990
- [AD 90-19-09](https://openairdocs.org/ad/90-19-09): High Pressure Turbine Stage One Disks · General Electric CF6-45A, CF6-45A2, CF6-50A and 10 more. Effective Oct 1, 1990
- [AD 90-12-06](https://openairdocs.org/ad/90-12-06): Low Pressure Turbine · General Electric CF6-45A, CF6-45A2, CF6-50A and 10 more. Effective Jun 25, 1990
- [AD 87-23-06](https://openairdocs.org/ad/87-23-06): High Pressure Turbine Impeller Spacer · General Electric CF6-45A, CF6-45A2, CF6-50A and 10 more. Effective Nov 5, 1987
- [AD 86-12-03](https://openairdocs.org/ad/86-12-03): High Pressure Turbine Rotor (HPTR) Stage 1 Disk · General Electric CF6-45A, CF6-45A2, CF6-50A and 10 more. Effective Jun 29, 1986
- [AD 84-01-01](https://openairdocs.org/ad/84-01-01): Compressor Assemblies · General Electric CF6-45A, CF6-45A2, CF6-50A and 10 more. Effective Feb 10, 1984
- [AD 82-25-08](https://openairdocs.org/ad/82-25-08): HPT Spacer/Impeller · General Electric CF6-45A, CF6-45A2, CF6-50A and 10 more. Effective Dec 30, 1982
- [AD 82-20-03](https://openairdocs.org/ad/82-20-03): Inspect First Stage HPT Disks · General Electric CF6-45A, CF6-45A2, CF6-50A and 10 more. Effective Oct 31, 1982
- [AD 85-25-56 R1](https://openairdocs.org/ad/85-25-56-R1): Seventh Stage Low Pressure Turbine (LPT) Cooling Air Manifold Tube · General Electric CF6-45A, CF6-45A2, CF6-50A and 10 more

### Historical (superseded or no longer in force)

- [AD 2012-02-07](https://openairdocs.org/ad/2012-02-07) (historical): LPT rotor stage 3 disks · General Electric CF6-45A, CF6-45A2, CF6-50A and 10 more. Effective Mar 6, 2012
- [AD 2011-18-01](https://openairdocs.org/ad/2011-18-01) (historical): LPT rotor stage 3 disks · General Electric CF6-45A, CF6-45A2, CF6-50A and 9 more. Effective Sep 26, 2011
- [AD 2011-02-07](https://openairdocs.org/ad/2011-02-07) (historical): Rotor · General Electric CF6-45A, CF6-45A2, CF6-50A and 9 more. Effective Feb 22, 2011
- [AD 2010-12-10](https://openairdocs.org/ad/2010-12-10) (historical): High-pressure turbine (HPT) · General Electric CF6-45A, CF6-45A2, CF6-50A and 9 more. Effective Jun 24, 2010
- [AD 2010-06-15](https://openairdocs.org/ad/2010-06-15) (historical): Low-pressure turbine (LPT) stage 3 disks · General Electric CF6-45A, CF6-45A2, CF6-50A and 9 more. Effective Apr 1, 2010
- [AD 2009-04-17](https://openairdocs.org/ad/2009-04-17) (historical): Long fixed core exhaust nozzle (LFCEN) assembly · General Electric CF6-45A, CF6-45A2, CF6-50A and 10 more. Effective Apr 2, 2009
- [AD 2006-12-24](https://openairdocs.org/ad/2006-12-24) (historical): Five-link forward mount assembly · General Electric CF6-45A, CF6-45A2, CF6-50A and 14 more. Effective Jul 21, 2006
- [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 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 99-08-18](https://openairdocs.org/ad/99-08-18) (historical): General Electric CF6-45A, CF6-45A2, CF6-50A and 15 more. Effective May 13, 1999

## Information bulletins (advisory)

None matched.

## NTSB investigations

None matched to N328UP.

## FAA accident and incident reports

None matched to N328UP.

## Service difficulty reports (119, 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 IPXA2026101456665](https://openairdocs.org/sdr/IPXA2026101456665), Oct 14, 2026: ADC. MALFUNCTIONED. EMERGENCY DECLARED, IN CRUISE EXPERIENCED AIRSPEED UNRELIABLE SITUATION PER QRH CHECKLIST WE DETERMINED THE LEFT SIDE WAS UNRELIABLE. DUE TO NON SPECIFIC FIM TA
- [SDR IPXA2026071799616](https://openairdocs.org/sdr/IPXA2026071799616), Jul 16, 2026: FUEL SYS. OUT OF BALANCE. FUEL BALANCED AT TAKEOFF,3 HOURS IN TO FLIGHT GOT FUEL CONFIG LIGHT-RAN QRH TO BALANCE FUEL.2 HOURS AFTER BALANCING FUEL WE HAD A 700 LB FUEL IMBALANCE.LANDED W
- [SDR IPXA2026051823210](https://openairdocs.org/sdr/IPXA2026051823210), May 16, 2026: DOOR. UNSECURE. THE LEFT FWD ENTRY DOOR WILL NOT LATCH CLOSE. ARM LEVER WILL NOT GO INTO SECURED POSITION ADJUSTED CREW ENTRY DOOR HANDLE REFERENCE AMM 52-12-25. DOOR OPERATION
- [SDR IPXA2025080870685](https://openairdocs.org/sdr/IPXA2025080870685), Jul 29, 2025: SKIN. CORRODED. CORROSION, FUSELAGE SKIN STA 1410 BETWEEN S-38R AND S-39R (REPAIR). REPAIR DAMAGE AREA I.A.W UPS EO-94636-REQ1 REV1.
- [SDR IPXA2025080670685](https://openairdocs.org/sdr/IPXA2025080670685), Jul 29, 2025: SKIN. CORRODED. CORROSION, FUSELAGE SKIN STA 1410 BETWEEN S-38R AND S-39R. RESPECTIVELY PART MARK THE REPAIR PART(S) PER BAC5307 CODE M AS BELOW. REPAIR FILLER: F2025A53M-1650-
- [SDR IPXA2025081456371](https://openairdocs.org/sdr/IPXA2025081456371), Jul 28, 2025: ACOUSTIC LINER. DAMAGED. BROKEN-ACOUSTIC LINER, NO.2 ENG FAN CASE MIDDLE 7:00 AREA . I.A.W AMM 72-33-01-004-001-H00 AND 72-33-01-404-011-H00 REV.145, REPLACED THE ACOUSTIC LINER SEGMENT
- [SDR IPXA2025072856371](https://openairdocs.org/sdr/IPXA2025072856371), Jul 28, 2025: ACOUSTIC LINER. BROKEN. BROKEN ACOUSTIC LINER, NR 2 ENG FAN CASE MIDDLE 7:00 AREA. OK TO WORK.
- [SDR IPXA2025080644382](https://openairdocs.org/sdr/IPXA2025080644382), Jul 27, 2025: FILLER. CORRODED. FOUND FILLER WITH CORROSION DAMAGE AT STA 1602 LBL 62 IN BULK CARGO COMPARTMENT. REMOVED DAMAGE FILLER I.A.W SRM 51-40-02-0G REV.92. REMOVED DAMAGE FILLER I.A.W
- [SDR IPXA2025080734467](https://openairdocs.org/sdr/IPXA2025080734467), Jul 26, 2025: FITTING. CRACKED. FAULT- FOUND THE MAIN DECK CARGO RESTRAINT FLOOR ADAPTER FITTING WITH CRACK DAMAGE AT STA 1197 BL0. (FLOOR PANEL NO. 251AFF). I.A.W AMM 53-01-06-000-801 REV.145
- [SDR IPXA2025072734622](https://openairdocs.org/sdr/IPXA2025072734622), Jul 26, 2025: FLOOR PANEL. CRACKED. FOUND MAIN DECK FLOOR PANEL WITH CRACK DAMAGE, P/N: 146T5869-89 PANEL NO: 251XFF STA 1400~ STA 1520 LBL 55~ LBL 77. I.A.W AMM 53-01-06-000-801 REV.145 REMOVE MA
- [SDR IPXA2025080634499](https://openairdocs.org/sdr/IPXA2025080634499), Jul 26, 2025: FILLER. CORRODED. ETOPS, FOUND FILLER WITH CORROSION DAMAGE AT STA 1602 RBL 62 IN BULK CARGO COMPARTMENT. REMOVED DAMAGE FILLER I.A.W SRM 51-40-02-0G REV.92. FABRICATE FILLER (P/
- [SDR IPXA2025080633038](https://openairdocs.org/sdr/IPXA2025080633038), Jul 26, 2025: FLOORBEAM. CORRODED. FOUND FLOOR BEAM CLIP WITH CORROSION DAMAGE AT STA 1596.5 RBL 55 IN BULK CARGO COMPARTMENT. I.A.W AMM 53-01-06-000-801 REV.145 REMOVE MAIN DECK CARGO FLOOR PANE
- [SDR IPXA2025080633067](https://openairdocs.org/sdr/IPXA2025080633067), Jul 26, 2025: FLOORBEAM. CORRODED. FOUND FLOOR BEAM CLIP WITH CORROSION DAMAGE AT STA 1596 LBL 57 IN BULK CARGO COMPARTMENT. REMOVED DAMAGE CLIP I.A.W SRM 51-40-02-0G REV.92 FABRICATE CLIP (P/N: 
- [SDR IPXA2025080633177](https://openairdocs.org/sdr/IPXA2025080633177), Jul 26, 2025: SUPPORT STRAP. CORRODED. CORROSION - STRAP, FWD CARGO CEILING LINER SUPPORT AT STA 478-610 RBL 39. REMOVED DAMAGE STRAP I.A.W SRM 51-40-02-0G REV.92. I.A.W. UPS EO NO.:EO-94540-REQ1 REV
- [SDR IPXA2025080534497](https://openairdocs.org/sdr/IPXA2025080534497), Jul 26, 2025: ANGLE. CRACKED. FOUND THE ANGLE CRACK AT STA 1578 LBL 80 INBOARD IN BULK CARGO COMPARTMENT LEFT AREA. (REPLACE) 1. REMOVED DAMAGE ANGLE I.A.W SRM 51-40-02-0G REV.92 INSTALL NEW
- [SDR IPXA2025080533093](https://openairdocs.org/sdr/IPXA2025080533093), Jul 26, 2025: ANGLE. CRACKED. FOUND THE ANGLE CRACK AT STA 1578 LBL 80 OUTBOARD IN BULK CARGO COMPARTMENT LEFT AREA. .I.A.W AMM 53-01-06-000-801 REV.145 REMOVE MAIN DECK CARGO FLOOR PANEL AN
- [SDR IPXA2025080534499](https://openairdocs.org/sdr/IPXA2025080534499), Jul 26, 2025: FILLER. CORRODED. FOUND FILLER WITH CORROSION DAMAGE AT STA 1602 RBL 62 IN BULK CARGO COMPARTMENT. (REPLACE) 1. REMOVED DAMAGE FILLER I.A.W SRM 51-40-02-0G REV.92 FABRICATE FILLE
- [SDR IPXA2025072734706](https://openairdocs.org/sdr/IPXA2025072734706), Jul 26, 2025: FLOOR PANEL. CRACKED. FOUND MAIN DECK FLOOR PANEL WITH CRACK DAMAGE, P/N: 146T5869-88 PANEL NO: 252UFF STA 1400~ STA 1520 RBL 55~ RBL 77. I.A.W AMM 53-01-06-000-801 REV.145 REMOVE MA
- [SDR IPXA2025011091744](https://openairdocs.org/sdr/IPXA2025011091744), Jan 8, 2025: BRACKET. CORRODED. AFT PIT DOOR FWD CORNER VERTICAL BRACKET CORRODED I/B OF FWD SEAL DEPRESSOR IN LOWER CORNER. REPLACED SECTION 46 FUSELAGE DOOR SURROUND LOWER SILL SHEAR TIE PER
- [SDR IPXA2023092298048](https://openairdocs.org/sdr/IPXA2023092298048), Sep 19, 2023: DOOR. INOPERATIVE. LWR FWD CARGO DOOR INDICATED OPEN **OII 2** R/R PROX SENSOR S215 IAW AMM 52-41-02/201 AND SWPM 20-30-12 OPS CHECK GOOD.
- [SDR IPXA2023091998048](https://openairdocs.org/sdr/IPXA2023091998048), Sep 19, 2023: UNKNOWN. UNKNOWN. **SDR FILED OPEN** **ATB**LWR FWD CARGO DOOR INDICATED OPEN **OII 2** DEFERRERAL LWER FWD CARGO DOOR INDICATION INOP PER MEL 52-71-1-1. ACCOMPLISHED DMP. PLACCA
- [SDR IPXA2023082838869](https://openairdocs.org/sdr/IPXA2023082838869), Aug 26, 2023: SWITCH. INOPERATIVE. EMERGENCY EXIT LIGHT SWITCH NOT RIGGED RIGHT. DOES NOT TURN OFF. PERFORMED OPERATIONAL CHECK ON EMERGENCY LIGHTS REF AMM 33-51-00. OPS CHECK GOOD.
- [SDR IPXA2023082057266](https://openairdocs.org/sdr/IPXA2023082057266), Aug 20, 2023: BATTERY. UNSERVICEABLE. FLIGHT DECK EMERGENCY LIGHTS INOP ACCOMPLISHED REPLACEMENT OF EMERGENCY LIGHTING POWER SUPPLY BATTERY PACK REF AMM 33-51-07. FLIGHT DECK EMERGENCY LIGHT NOW CHE
- [SDR IPXA2023072588376](https://openairdocs.org/sdr/IPXA2023072588376), Jul 20, 2023: STIFFENER. CRACKED. *MAJOR REPAIR* FAULT - CRACK - STIFFENER CENTER WING FRONT SPAR CRACK IN STIFFENER AT STA 785.9 RBL 11 (REPAIR) PERFORM REPAIR I.A.W SRM 57-10-10-2R-2 REPAIR IN
- [SDR IPXA2023072888384](https://openairdocs.org/sdr/IPXA2023072888384), Jul 20, 2023: STIFFENER. CRACKED. *MAJOR REPAIR* FAULT - CRACK - STIFFENER CENTER WING FRONT SPAR CRACK IN STIFFENER AT STA 785.9 RBL 55 (REPAIR) PERFORM REPAIR I.A.W SRM 57-10-10-2R-2 REPAIR IN
- [SDR IPXA2023040392540](https://openairdocs.org/sdr/IPXA2023040392540), Apr 3, 2023: ANTI-SKID SYS. WARNING MESSAGE. ANTISKID INOP EICAS MSG QRH PROCEDURE ACCOMPLISHED. ANTISKID/AUTOBRAKE CONTROL UNIT SHOWS VLV 7 NIL TIME OR PARTS AT EMA. XFERD TO MIL IAW MEL 32-42-1-1A DEACTI
- [SDR IPXA2023032692264](https://openairdocs.org/sdr/IPXA2023032692264), Mar 26, 2023: RADAR. WARNING MESSAGE. INSPECTION TYPE:N/A**ATB** -WEATEHR SYSTEM FAIL WXR SYS STATUS MESSAGE`R&R WXR TRANSCEIVER IAW AMM 34-43-01. OPS CK GOOD.
- [SDR IPXA2023080320184](https://openairdocs.org/sdr/IPXA2023080320184), Dec 6, 2022: SKIN. DENTED. *MAJOR REPAIR* FUSELAGE SKIN DAMAGE BETWEEN STA 220.5 TO 228.5 AND S-16L TO S-17L REPAIR***AWE/REPAIR*** ACCOMPLISHED REPAIR I.A.W EO-87808-REQ1 REV1. ATTACHEME
- [SDR IPXA2022031179994](https://openairdocs.org/sdr/IPXA2022031179994), Mar 11, 2022: NONE. FAILED. INSPECTION TYPE:ETOP** ETOPS FILED OPEN**STATUS MSG WXR SYS WXR FAIL INDICATION CAME ON DURING CLIMB OUT AND STAYED ON FOR REST OF FLIGHT. AT ALL RANGES. DEFERR
- [SDR IPXA2021072271936](https://openairdocs.org/sdr/IPXA2021072271936), Jul 13, 2021: SKIN. CRACKED. INSPECTION TYPE:C12CRACK DAMAGE WAS FOUND ON NO.1 PYLON OUTBD SKIN ASSEMBLY (P/N:311T2450-25) NEAR NAC STA 237.5PERFORM REPAIR I.A.W. BOEING SR 4-5188323591 AND
- [SDR IPXA2020011350814](https://openairdocs.org/sdr/IPXA2020011350814), Jan 11, 2020: FLOOR PANEL. DAMAGED. INSPECTION TYPE:N/AFLOOR PANEL P/N 141T5856-13 DAMAGED POS 2R.FABRICATED NEW FLOOR PANEL IAW E.O. B767-5320-9396-I.
- [SDR IPXA2019101877980](https://openairdocs.org/sdr/IPXA2019101877980), Oct 16, 2019: PNEUMATIC SYSTEM. FLUCTUATES. INSPECTION TYPE:ETOP**ETOPS FILED OPEN** APU OPS NORMAL PNUE PRESS DROP IS ECCESSIVE WHEN USING APU BLEED AIR FOR ENG START. APU & ENG START NORMAL, DROPS FROM 
- [SDR IPXA2019091146607](https://openairdocs.org/sdr/IPXA2019091146607), Sep 10, 2019: HINGE. BROKEN. INSPECTION TYPE:N/A**SUPPLEMENTAL SDR** L1 CREW DOOR SECONDARY / ARMING LEVER ACCESS DOOR BROKEN. DEFERRED IAW MEL 52-11-02. NO DMP PLACARD INSTALLED. REPLACED 
- [SDR IPXA2019071644515](https://openairdocs.org/sdr/IPXA2019071644515), Jul 8, 2019: SKIN. CRACKED. INSPECTION TYPE:C11 CRACK WAS FOUND ON RT SKIN (P/N: 148T3121-2) NEAR STA 1725.5. REPAIR IAW SRM 53-80-01-2R-5 REPAIR 5 REV.74.00, SRID: #4-4544702333, EO B767-
- [SDR IPXA2019041741132](https://openairdocs.org/sdr/IPXA2019041741132), Apr 16, 2019: HINGE. BROKEN. ENTRY DOOR HANDLE LEVER COVER HINGE BROKEN.REPLACED HINGE IAW AMM 20 10 00
- [SDR IPXA2019020638742](https://openairdocs.org/sdr/IPXA2019020638742), Feb 6, 2019: SWITCH. DIRTY. FWD ACCESS DOOR EICAS MSG DISPLAYED DEF IAW 52-71-1-1 DMP 52-71-1-1. PERF INSP OF S200 PROX SWITCH AND CLEANED SWITCH & DOOR PLUNGER PER WDM 52-71-14. OPS CK GO
- [SDR IPXA2017091621784](https://openairdocs.org/sdr/IPXA2017091621784), Sep 16, 2017: PITOT TUBE. OUT OF LIMITS. EMERGENCY DECLARED FOR THE PITOT STATIC PROBE ANTI-ICE EICAS MESSAGE, LT AUX PITOT SHOWS, LIGHT STAYS ON UNTIL LANDING. TROUBLESHOOTING PERFORMED IAW FIM 30-31-
- [SDR IPXA2017071419270](https://openairdocs.org/sdr/IPXA2017071419270), Jul 6, 2017: KEELBEAM. CORRODED. INSPECTION TYPE: C10, CORROSION ON KEEL BEAM AT BS 890 , LBL 9 TO RBL 9. REPAIRED IAW SRM 53-50-12-1A-1, ALLOWABLE DAMAGE , REV 68.
- [SDR IPXA2017071419269](https://openairdocs.org/sdr/IPXA2017071419269), Jul 6, 2017: SPLICE. CORRODED. INSPECTION TYPE: C10, CORROSION ON SPLICE TEE OF KEEL BEAM AT BS 960 , LBL 9 TO RBL 9. REPLACED THE SPLICED TEE.
- [SDR IPXA2017071319268](https://openairdocs.org/sdr/IPXA2017071319268), Jul 4, 2017: SKIN. CRACKED. INSPECTION TYPE: C10, CRACK FOUND ON THE INBD SIDE SKIN AND DOUBLER OF THE NR 2 PYLON. REPAIRED IAW EO B767-5430-64819-A.
- [SDR IPXA2017071319267](https://openairdocs.org/sdr/IPXA2017071319267), Jul 4, 2017: STIFFENER. CRACKED. INSPECTION TYPE: C10, CRACK FOUND ON THE STIFFENER UPPER SIDE AT BS 785.9, RBL 33. REPAIRED IAW SRM 57-10-10-2R-2, REPAIR 2, REV 68, AND EO B767-5740-58151-A.
- [SDR IPXA2017071319266](https://openairdocs.org/sdr/IPXA2017071319266), Jul 4, 2017: STIFFENER. CRACKED. INSPECTION TYPE: C10, CRACK FOUND ON THE STIFFENER UPPER SIDE AT BS 785.9 , LBL 55. REPAIRED IAW SRM 57-10-10-2R-2, REPAIR 2, REV 68, AND EO B767-5740-58151-A.
- [SDR IPXA2017071319265](https://openairdocs.org/sdr/IPXA2017071319265), Jul 4, 2017: STIFFENER. CRACKED. INSPECTION TYPE: C10, CRACK ON THE STIFFENER UPPER SIDE AT BS 785.9 , LBL 11. REPAIRED IAW SRM 57-10-10-2R-2, REPAIR 2, REV 68, AND EO B767-5740-58151-A.
- [SDR IPXA2017071319264](https://openairdocs.org/sdr/IPXA2017071319264), Jul 3, 2017: STIFFENER. CRACKED. INSPECTION TYPE: C10, CRACK ON STIFFENER UPPER SIDE AT BS 785.9 , LBL 33. REPAIRED IAW SRM 57-10-10-2R-2, REPAIR 2, REV 68, AND EO B767-5740-58151-A.
- [SDR IPXA2016101809527](https://openairdocs.org/sdr/IPXA2016101809527), Oct 18, 2016: TARGET. DAMAGED. INSPECTION TYPE:N/A, TARGET PLATE FOR DOOR SWITCH 5152 IS DAMAGED. LOCATED FWD LOWER CARGO DOOR FRAME FWD SIDE REMOVED & REPLACED TARGET IAW MM 52-33-00.
- [SDR IPXA2016101809528](https://openairdocs.org/sdr/IPXA2016101809528), Oct 18, 2016: DOOR FRAME. CRACKED. INSPECTION TYPE:N/A, BULK PIT DOOR CRACKED AT BOTTOM FRAME REPAIRED PER EO B767-5230-62160-A.
- [SDR IPXA2016051703496](https://openairdocs.org/sdr/IPXA2016051703496), May 13, 2016: MOUNT. CORRODED. NR 2 ENGINE EVIDENCE SURFACE CORROSION AFT ENGINE MOUNT CLEANED SURFACE NO FURTHER DEFECTS MM 54-05-03.
- [SDR IPXA2016040701793](https://openairdocs.org/sdr/IPXA2016040701793), Apr 7, 2016: POWER SUPPLY. INOPERATIVE. EMERGENCY EXIT SIGN INOPERATIVE, R & RED EMERGENCY LIGHT POWER SUPPLY REF AMM 33-51-07, EMERGENCY EXIT SIGN AND LIGHTS OPERATE NORMALLY.
- [SDR IPXA2016031300673](https://openairdocs.org/sdr/IPXA2016031300673), Mar 13, 2016: SKIN. DENTED. LH WING INBD AFT FLAP LWR SKIN DENT. REPAIRED IAW EO B767-5750-59975-B.
- [SDR IPXA2016020798984](https://openairdocs.org/sdr/IPXA2016020798984), Feb 7, 2016: FLOOR PANEL. DAMAGED. FLOOR PANEL DAMAGED. FABRICATED A NEW FLOOR PANEL IAW EO B767-5320-9693-I.

All 119: https://openairdocs.org/aircraft/N328UP/reports.md

## STCs that may be installed (OpenAirDocs) (3)

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 CF6-45A2)

- [STC SE00025EN](https://openairdocs.org/stc/SE00025EN): Installation of International Aerospace Tubes, LLC, Master Drawing List TPC Stage 7 Cooling System , revision NR, dated December 15, 2011, or later FAA-Approved Revisions. United Technologies Corporation, Pratt & Whitney Division
- [STC SA1139NW-D](https://openairdocs.org/stc/SA1139NW-D): Install fireproof blankets on Engine Fan Reverser Intermediate Fireseal in lieu of Fireproof Intumescent Coating. United Airlines Inc
- [STC SE00461LA](https://openairdocs.org/stc/SE00461LA): Install fireproof blankets on the engine fan reverser intermediate fireseal, in lieu of fireproof intumescent coating. Hi Temp Insulation Inc

## Related

- Other Boeing 767-34AF aircraft: https://openairdocs.org/model/boeing-767-34af/aircraft.md
- The GE CF6-45A2 engine: https://openairdocs.org/engine/ge-cf6-45a2.md

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