# N352UP: 2012 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: 37875
- Year built: 2012
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: May 21, 2012
- Certificate issued: May 22, 2012
- Expires: May 31, 2028
- Mode S code: A3EE0B
- 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=352UP
- Page: https://openairdocs.org/aircraft/N352UP

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 N352UP.

## FAA accident and incident reports (1)

From the FAA Accident/Incident Data System. Reports are matched to registry aircraft by N-number and event date, checked against the reported make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model.

- [Incident 20150519012399I](https://openairdocs.org/incident/20150519012399I), May 19, 2015: Boeing 767-34AF (N352UP), Miami, FL, No damage. On 5/19/2015 1306Z at Miami, FL (7SW): a significant uas-unmanned aerial systems / drone mor was reported by mia when UPS417, B763, westbound @ 5,500' reported…

## Service difficulty reports (85, 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 IPXA2026041572484](https://openairdocs.org/sdr/IPXA2026041572484), Apr 13, 2026: DEPRESSOR. DENTED. DENTED DEPRESSURE SEAL, MAIN DECK CARGO DOOR CUTOUT AFT SIDE DEPRESSOR. INSTALLED MAIN DECK CARGO DEPRESSOR SEAL AT AFT SIDE I.A.W AMM 20-11-00-910-802 REV.147,
- [SDR IPXA2026041413576](https://openairdocs.org/sdr/IPXA2026041413576), Apr 9, 2026: GUARD. CRACKED. MEC DOOR CUTOUT, DOOR STOP GUARD CRACKED. INSTALLED A NEW GUARD IAW SRM 51-40-02-0G, REV 94, AND DWG 141T6300, SHT 1, REV J.
- [SDR IPXA2026041113551](https://openairdocs.org/sdr/IPXA2026041113551), Apr 9, 2026: SPLICE STRAP. CRACKED. CRACKED SPLICE STRAP, LT WING INBD T/E FWD LOWER RIB SUPPORT, WS 298. INSTALLED A NEW STRAP IAW SRM 51-40-02-0G, REV 94, AND DWG 113T1639, SHT 1, REV G.
- [SDR IPXA2026041087740](https://openairdocs.org/sdr/IPXA2026041087740), Apr 8, 2026: RESTRAINT. CRACKED. FOUND MAIN DECK CARGO HANDLING CL ROLLOVER RESTRAINT ASSY CRACK AT STA 990 BL 0 I.A.W AMM 25-58-03-004-001 AND AMM 25-58-03-404-004 REV.147 REPLACED CL ROLLOVER
- [SDR IPXA2026041087715](https://openairdocs.org/sdr/IPXA2026041087715), Apr 8, 2026: LOCK. WORN. FOUND MAIN DECK CARGO HANDLING BASE OF LOCK ASSY WORN STA 1250 RBL 33.50 AND STA 1131 RBL 77.50, LBL11.50 I.A.W AMM 25-58-01-004-001 AND AMM 25-58-01-404-005 RE
- [SDR IPXA2026041087701](https://openairdocs.org/sdr/IPXA2026041087701), Apr 8, 2026: LOCK. WORN. FAULT-FOUND MAIN DECK CARGO HANDLING BASE OF LOCK ASST WORN AT STA 880 RBL 11.50, STA 1000 RBL 77.50 I.A.W AMM 25-58-01-004-001 AND AMM 25-58-01-404-005 REV.147
- [SDR IPXA2026041087582](https://openairdocs.org/sdr/IPXA2026041087582), Apr 8, 2026: TRAY. CRACKED. FOUND MAIN DECK CARGO HANDLING BALL TRAY ASSY CRACK AT: STA 654+44 STA + 654+88 RBL 11.50. I.A.W AMM 25-57-02-004-029 AND AMM 25-57-02-404-016 REV.147 REPLACED 
- [SDR IPXA2026041087754](https://openairdocs.org/sdr/IPXA2026041087754), Apr 8, 2026: TRAY. CRACKED. FOUND MAIN DECK CARGO HANDLING BALL TRAY ASSY CRACK AT: STA 500 RBL 33.50, RBL11.50 I.A.W AMM 25-57-02-004-029 AND AMM 25-57-02-404-016 REV.147 REPLACED BALL TR
- [SDR IPXA2026041087635](https://openairdocs.org/sdr/IPXA2026041087635), Apr 8, 2026: GUIDE. WORN. FOUND MAIN DECK CARGO HANDLING LATERAL GUIDE ASSY DAMPER WORN AT: STA 500 RBL 66.50 AND STA 620 LBL 66.50 TOTAL:2EA I.A.W AMM 25-57-08-004-015 AND AMM 25-57-08-
- [SDR IPXA2026041087549](https://openairdocs.org/sdr/IPXA2026041087549), Apr 8, 2026: ROLLER. DEFORMED. FAULT-FOUND MAIN DECK CARGO HANDLING SHAFT OF ROLLER RAIL ASSY DEFORM TOTAL:1EA AT STA 977 LBL 77.50 (REPLACE). I.A.W AMM 25-57-05-004-001 AND AMM 25-57-05-404-
- [SDR IPXA2026041492530](https://openairdocs.org/sdr/IPXA2026041492530), Apr 8, 2026: BUSHING. WORN. WORN BUSHING, NR 2 ENGINE RT CORE COWL PRESSURE RELIEF DOOR INNER AREA. INSTALLED A NEW BUSHING IAW SRM 51-40-02-0G, REV 94, AND CMM IPL 71-13-24, REV 50.
- [SDR IPXA2026041192806](https://openairdocs.org/sdr/IPXA2026041192806), Apr 8, 2026: SEAL. BROKEN. BROKEN SEAL, NR 1 PYLON RT SIDE PANEL 436CR. INSTALLED A NEW SEAL STRIP IAW SRM 51-40-02-0G, REV 94, AND DWG 311T2570, SH 16, REV -.
- [SDR IPXA2026041493823](https://openairdocs.org/sdr/IPXA2026041493823), Apr 8, 2026: RUB STRIP. CHAFED. CHAFED WEAR STRIP, NR 2 ENG R/H CORE COWL INNER AFT UPPER EDGE. INSTALLED NEW WEAR STRIP I.A.W SRM 51-40-02-0G REV.94 AND CMM IPL 71-13-24 REV. 50
- [SDR IPXA2026040994656](https://openairdocs.org/sdr/IPXA2026040994656), Apr 8, 2026: SKIN. DEBONDED. DEBONDED SKIN, INBD AFT EDGE OF LT WING T/E OUTBD FLAP T/E SKIN, WBL 289.45. PERFORMED NDT/UT FOR THE REWORKED AREA & PLUS 2 INCHES HEATED AREA , IAW NDT MANUAL
- [SDR IPXA2026041094116](https://openairdocs.org/sdr/IPXA2026041094116), Apr 8, 2026: FORMER. CRACKED. CRACKED FORMER, FWD SIDE OF LT WING OTBD L/E NOSE BEAM, OSS 499.6. INSTALL NEW FORMER IAW SRM 51-40-02-0G REV.95 AND DWG 114T2511 SH 1 REV: D
- [SDR IPXA2026041094070](https://openairdocs.org/sdr/IPXA2026041094070), Apr 8, 2026: FORMER. CRACKED. CRACKED FORMER, FWD SIDE OF LT WING OTBD L/E NOSE BEAM, OSS 441.6. INSTALLED NEW FORMER I.A.W SRM 51-40-02-0G REV.94 AND BOEING DWG NO. 114T2241 SH 4 REV - AND 
- [SDR IPXA2026041094681](https://openairdocs.org/sdr/IPXA2026041094681), Apr 8, 2026: FORMER. CRACKED. CRACKED FORMER, RT WING OTBD LE WS 510. INSTALL NEW FORMER I.A.W SRM 51-40-02-0G REV.94 AND BOEING DWG NO. 114T2161 SH 6 REV - AND UPS SREO-50900-REQ001 REV2.
- [SDR IPXA2026041192577](https://openairdocs.org/sdr/IPXA2026041192577), Apr 8, 2026: BRACKET. GOUGED. GOUGED BRACKET, NR 1 ENG RT CORE COWL HOLD-OPEN ROD RECEIVER. INSTALLED A NEW BRACKET IAW SRM 51-40-02-0G, REV 94, AND CMM IPL 71-13-24, REV 50.
- [SDR IPXA2026041590371](https://openairdocs.org/sdr/IPXA2026041590371), Apr 8, 2026: BEAM. CRACKED. DURING PERFORMANCE OF EO-63801-JIC001, FOUND LEFT WING TRAILING EDGE SUPPORT BEAM CRACKED AT WS 1079.95. INSTALLED A NEW BEAM IAW SRM 51-40-02-0G, REV.94 AND DW
- [SDR IPXA2026041492581](https://openairdocs.org/sdr/IPXA2026041492581), Apr 8, 2026: ADAPTER. CHAFED. CHAFED ADAPTER AND BRACKET, NR 2 ENG LT CORE COWL HOLD OPEN ROD SUPPORT BRACKET AREA. INSTALLED A NEW BRACKET AND ADAPTER IAW SRM 51-40-02-0G, REV 94, AND CMM I
- [SDR IPXA2026041492647](https://openairdocs.org/sdr/IPXA2026041492647), Apr 8, 2026: BRACKET. CHAFED. CHAFED ADAPTER & BRACKET, NR 2 ENG, RT CORE COWL HOLD OPEN ROD SUPPORT BRACKET AREA. INSTALLED A NEW BRACKET & ADAPTER IAW SRM 51-40-02-0G, REV 94, AND CMM IPL 
- [SDR IPXA2026041590118](https://openairdocs.org/sdr/IPXA2026041590118), Apr 8, 2026: BRACKET. CRACKED. NR 2 ENGINE LT CPRSR REAR FRAME SENSOR SUPPORT BRACKET CRACKED, NEAR 10 O'CLOCK. REPLACED THE BRACKET IAW AMM 70-50-00-912-001-H00, REV 147.
- [SDR IPXA2026041590099](https://openairdocs.org/sdr/IPXA2026041590099), Apr 8, 2026: CLAMP. BROKEN. BROKEN CLAMP, NR 1 ENGINE LOWER -D- SUMP OIL SUPPLY TUBE, FWD SUPPORT. REPLACED THE CLAMP IAW AMM 20-11-00-910-802, REV 147,
- [SDR IPXA2026041192828](https://openairdocs.org/sdr/IPXA2026041192828), Apr 8, 2026: BRACKET. BROKEN. NR 1 ENG, LT THRUST REVERSER COWL INNER DRAIN TUBE SUPPORT CLAMP ATTACH PLATE BROKEN AT 11:00 O'CLOCK. INSTALLED A NEW BRACKET IAW SRM 51-40-02-0G, REV 94, AND 
- [SDR IPXA2026041492935](https://openairdocs.org/sdr/IPXA2026041492935), Apr 8, 2026: SUPPORT ANGLE. CRACKED. NR 2 PYLON AFT FAIRING R/H AFT STIFFENER SUPPORT ANGLE CRACKED. INSTALLED A NEW SUPPORT ANGLE IAW SRM 51-40-02-0G, REV 94, AND DWG 313T2303, SHT 131, REV- , AND
- [SDR IPXA2026041193805](https://openairdocs.org/sdr/IPXA2026041193805), Apr 8, 2026: BRACKET. GOUGED. GOUGED BRACKET, NR 1 ENG RT CORE COWL PRESSURE RELIEF DOOR LOWER LATCH STOP PAD. INSTALLED A NEW BRACKET IAW SRM 51-40-02-0G, REV 94, AND CMM IPL 71-13-24, REV 
- [SDR IPXA2026041394644](https://openairdocs.org/sdr/IPXA2026041394644), Apr 8, 2026: SUPPORT. CRACKED. RT WING NR 6 FLAP TRACK SUPPORT FAIRING INBD AFT SIDE CRACKED. PERFORMED NDT/UT FOR THE REWORKED AREA AND PLUS 6 INCHES, AROUND HEATED AREA IAW NDT MANUAL PART 
- [SDR IPXA2026041092520](https://openairdocs.org/sdr/IPXA2026041092520), Apr 8, 2026: BRACKET. CHAFED. CHAFED BRACKET, NR 1 ENG RT THRUST REVERSER COWL LOWER CLOSURE PANEL T/E INNER SIDE. INSTALLED A NEW BRACKET IAW SRM 51-40-02-0G, REV 94, AND IPC 78-32-22, REV 
- [SDR IPXA2026041092657](https://openairdocs.org/sdr/IPXA2026041092657), Apr 8, 2026: BRACKET. GOUGED. NR 1 ENG LT CORE COWL HOLD-OPEN ROD RECEIVER ATTACH BRACKET GOUGED. INSTALLED A NEW BRACKET IAW SRM 51-40-02-0G, REV 94, AND CMM IPL 71-13-23, REV 47.
- [SDR IPXA2026041094730](https://openairdocs.org/sdr/IPXA2026041094730), Apr 8, 2026: BRACKET. CRACKED. CRACKED TORQUE TUBE SUPPORT BRACKET, RT WING L/E COMPARTMENT ACCESS PANEL 611LB. INSTALL A NEW BRACKET IAW SRM 51-40-02-0G, REV 94, & DWG 114T1240, SHT 6, REV -
- [SDR IPXA2026040890099](https://openairdocs.org/sdr/IPXA2026040890099), Apr 8, 2026: CLAMP. BROKEN. BROKEN CLAMP, NR 1 ENG LOWER D SUMP OIL SUPPLY TUBE FWD SUPPORT.
- [SDR IPXA2026040890118](https://openairdocs.org/sdr/IPXA2026040890118), Apr 8, 2026: BRACKET. CRACKED. CRACKED BRACKET, NR 2 ENG L/H CPRSR REAR FRAME SENSOR SUPPORT BRACKET, NEAR 10 O'CLOCK.
- [SDR IPXA2026041473323](https://openairdocs.org/sdr/IPXA2026041473323), Apr 7, 2026: CLAMP. BROKEN. DAMAGED CLAMP, NR 2 PYLON AFT FAIRING DOOR HOLD OPEN ROD LOCK CLAMP. INSTALLED A NEW CLAMP IAW SRM 51-40-02-0G, REV 94, AND DWG 313T2303, SH 135, REV -.
- [SDR IPXA2026041473398](https://openairdocs.org/sdr/IPXA2026041473398), Apr 7, 2026: SEAL. BROKEN. BROKEN SEAL, NR 1 PYLON LT SIDE PANEL 436CL. INSTALLED A NEW SEAL IAW SRM 51-40-02-0G, REV 94, AND DWG 311T2570, SH 16, REV -.
- [SDR IPXA2026041473481](https://openairdocs.org/sdr/IPXA2026041473481), Apr 7, 2026: SEAL. BROKEN. BROKEN SEAL, NR 2 PYLON FAIRING PANEL 446CL EDGE. INSTALLED A NEW SEAL STRIP IAW SRM 51-40-02-0G, REV 94, AND DWG 311T2570, SH 16, REV -.
- [SDR IPXA2026041573667](https://openairdocs.org/sdr/IPXA2026041573667), Apr 7, 2026: LIGHT. CORRODED. FOUND EXTERIOR EMERGENCY LIGHT ASSY CORROSION. REVIEWED PER GMM-MTX 09.05.01.09. I.A.W AMM 33-51-16-962-013 REV.147 ATTACHED EXTERIOR EMERGENCY LIGHT ASSY (L134
- [SDR IPXA2026041473256](https://openairdocs.org/sdr/IPXA2026041473256), Apr 7, 2026: BRACKET. CRACKED. NR 2 PYLON AFT FAIRING DOOR HOLD OPEN ROD SUPPORT BRACKET CRACKED. INSTALL NEW BRACKET IAW SRM 51-40-02-0G REV.94 AND BOEING DWG 313T2303, SHT 135, REV -.
- [SDR IPXA2026040773667](https://openairdocs.org/sdr/IPXA2026040773667), Apr 7, 2026: LIGHT. CORRODED. FOUND EXTERIOR EMERGENCY LIGHT ASSY CORROSION.
- [SDR IPXA2026041457936](https://openairdocs.org/sdr/IPXA2026041457936), Apr 6, 2026: LOCK. CRACKED. FAULT- FOUND MAIN DECK CARGO HANDLING POSITION 3 LOCK ASSY CRACK TOTAL: 2EA AT STA 500 LBL 55.50 RBL 55.50. (REPLACE). I.A.W AMM 25-58-01-004-014 AND AMM 25-58-
- [SDR IPXA2026041057919](https://openairdocs.org/sdr/IPXA2026041057919), Apr 6, 2026: RESTRAINT. CRACKED. FOUND MAIN DECK CARGO HANDLING CL DOOR AREA RESTRAINT ASSY CRACK AT STA 522 STA 566 BL 0. I.A.W AMM 25-58-03-404-031 AND AMM 25-58-03-404-017 REV.147 REPLACED C
- [SDR IPXA2025010305925](https://openairdocs.org/sdr/IPXA2025010305925), Jan 3, 2025: WARNING MESSAGE. FALSE ACTIVATION. *AIR TURN BACK* FWD CARGO DOOR EICAS MSG ON DEPARTURE. WHILE TROUBLESHOOTING FORWARD LOWER CARGO DOOR INDICATION FOUND CONNECTOR D6266P NOT LOCKED. LOCKED CONNE
- [SDR IPXA2024040743593](https://openairdocs.org/sdr/IPXA2024040743593), Mar 30, 2024: SUPPORT ANGLE. BROKEN. FAULT - BROKEN - DOOR SILL, FWD CARGO DOOR CUTOUT UPPER EDGE AT STA 489 RBL 91 (REPLACE) INSTALL SILL COVER OF FWD CARGO DOOR CUTOUT UPPER SIDE STA 478~522. I.A
- [SDR IPXA2024040143541](https://openairdocs.org/sdr/IPXA2024040143541), Mar 30, 2024: BRACKET. CRACKED. **SDR FILED OPEN**FAULT - CRACK - BRACKET, AFT CARGO COMPARTMENT INNER FWD INTERCOSTAL LOWER FLOOR BEAM SUPPORT AT STA 1065 RBL 26 (REPLACE) OK TO WORK
- [SDR IPXA2024040145064](https://openairdocs.org/sdr/IPXA2024040145064), Mar 30, 2024: BRACKET. CRACKED. BRACKET, AFT CARGO COMPARTMENT INNER FWD INTERCOSTAL LOWER FLOOR BEAM SUPPORT AT STA 1065 LBL 26 (REPLACE) I.A.W AMM 53-01-05-404-004 REV.141. INSTALL AFTER CAR
- [SDR IPXA2024040124327](https://openairdocs.org/sdr/IPXA2024040124327), Mar 29, 2024: FITTING. BROKEN. FOUND MAIN DECK CARGO RESTRAINT FLOOR ADAPTER FITTING BROKEN AT STA 742 BL0. (REPLACE) I.A.W AMM 25-57-05-404-006 AND AMM 25-58-01-404-005 REV.141 INSTALLED MAI
- [SDR IPXA2024040127476](https://openairdocs.org/sdr/IPXA2024040127476), Mar 29, 2024: FITTING. BROKEN. FOUND MAIN DECK CARGO RESTRAINT FLOOR ADAPTER FITTING BROKEN AT STA 1109 BL0. (REPLACE) I.A.W AMM 25-57-05-404-006 AND AMM 25-58-01-404-005 REV.141 INSTALLED MA
- [SDR IPXA2024040108204](https://openairdocs.org/sdr/IPXA2024040108204), Mar 28, 2024: ANGLE. CRACKED. ANGLE CRACK AT BULK CARGO COMPARTMENT RIGHT AREA STA 1578 RBL 60 OUTBOARD. (REPLACE) I.A.W AMM 25-57-05-404-006 AND AMM 25-58-04-404-015 REV.141 INSTALLED MAIN 
- [SDR IPXA2024040108240](https://openairdocs.org/sdr/IPXA2024040108240), Mar 28, 2024: ANGLE. CRACKED. ANGLE BULK CARGO COMPARTMENT LEFT AREA STA 1578 LBL 60 INBOARD. (REPLACE) I.A.W AMM 25-57-05-404-006 AND AMM 25-58-04-404-015 REV.141 INSTALLED MAIN DECK CARGO 
- [SDR IPXA2024040870859](https://openairdocs.org/sdr/IPXA2024040870859), Mar 26, 2024: NONE. NONE. FUSELAGE DRAIN HOLES INSPECTION AND INSTALLATION AFT OF BS 1725.5 BETWEEN S-36L AND S-36R ACCOMPLISHED SDR
- [SDR IPXA2024032670859](https://openairdocs.org/sdr/IPXA2024032670859), Mar 26, 2024: NONE. NONE. *** SDR FILED OPEN *** ADD SDR FOR EO-82173-JIC001 (FUSELAGE DRAIN HOLES INSPECTION AND INSTALLATION AFT OF BS 1725.5 BETWEEN S-36L AND S-36R)

All 85: https://openairdocs.org/aircraft/N352UP/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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