# N265AV: 2006 Cessna 750

- Status: Valid registration
- Airframe: [Cessna 750](https://openairdocs.org/model/cessna-750) (registry code 2076810, 12 seats)
- Engine: [Allison AE-3007C1](https://openairdocs.org/engine/allison-ae-3007c1) (registry code 03053)
- Data sheets: [TCDS T00007WI](https://openairdocs.org/tcds/T00007WI) (Textron Aviation Inc.), [TCDS TE6CH](https://openairdocs.org/tcds/TE6CH) (Rolls-Royce Corporation) (OpenAirDocs)
- Serial number: 750-0256
- Year built: 2006
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: November 18, 2020
- Certificate issued: June 28, 2022
- Expires: June 30, 2029
- Mode S code: A291A4
- Registered owner: [Bank Of Utah Trustee](https://openairdocs.org/faa-owner/BANK%20OF%20UTAH%20TRUSTEE)
- Location: [Salt Lake City, UT](https://openairdocs.org/faa-place/UT/Salt%20Lake%20City)
- Owner type: Corporation
- Owner's area on the map: 40.7558° N, 111.8843° W: Placed by OpenAirDocs at the center of ZIP code 84111, within about a mile (OpenAirDocs). The owner's mailing address, not where the aircraft is based
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=265AV
- Page: https://openairdocs.org/aircraft/N265AV

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): 17 in force

### Matched by airframe (Cessna 750)

- [AD 2026-13-02](https://openairdocs.org/ad/2026-13-02): Navigation · Airbus Canada Limited Partnership 18, 49-46, 80-A and 555 more. Effective Jul 1, 2026
- [AD 2023-10-02](https://openairdocs.org/ad/2023-10-02): Indicating/Recording System, Navigation · Boeing 18, 23, 35 and 1,060 more. Effective May 26, 2023
- [AD 2013-04-03](https://openairdocs.org/ad/2013-04-03): Pitot/Static Anti-Ice System · Cessna 750. Effective Apr 11, 2013
- [AD 2012-18-16](https://openairdocs.org/ad/2012-18-16): Electrical power · Cessna 750. Effective Oct 24, 2012
- [AD 2011-03-16](https://openairdocs.org/ad/2011-03-16): Electrical power · Cessna 750. Effective Mar 22, 2011
- [AD 2010-20-10](https://openairdocs.org/ad/2010-20-10): Flight Controls · Cessna 750. Effective Nov 1, 2010
- [AD 2007-11-17](https://openairdocs.org/ad/2007-11-17): Wires for the positive and negative terminal studs of the engine and/or auxiliary power unit (APU) fire extinguishing bottles. · Cessna 500, 501, 550 and 5 more. Effective Jul 6, 2007
- [AD 2006-24-01](https://openairdocs.org/ad/2006-24-01): Auxiliary power unit (APU) fuel tube assembly · Cessna 750. Effective Dec 6, 2006
- [AD 98-16-17 R1](https://openairdocs.org/ad/98-16-17-R1): Secondary horizontal stabilizer · Textron 750. Effective Oct 23, 2003
- [AD 2002-23-05](https://openairdocs.org/ad/2002-23-05): Circuit Breakers for the Auxiliary Hydraulic Pump System and the King KHF 950 High Frequency Communication System(s) · Cessna 750. Effective Dec 26, 2002
- [AD 2001-07-04](https://openairdocs.org/ad/2001-07-04): Roll Control System · Cessna 750. Effective May 15, 2001
- [AD 98-05-02](https://openairdocs.org/ad/98-05-02): Aileron Feel Cartridge Assembly Shaft · Cessna 750. Effective Mar 16, 1998

### Matched by engine (Allison AE-3007C1)

- [AD 2017-26-06](https://openairdocs.org/ad/2017-26-06): Turbine/turboprop Engine, Turbine · Rolls-Royce AE 3007A, AE 3007A1, AE 3007A1/1 and 7 more. Effective Jan 31, 2018
- [AD 2017-11-05](https://openairdocs.org/ad/2017-11-05): Turbine/ turboprop Engine, Turbine Section · Rolls-Royce AE 3007C and AE 3007C1. Effective Jul 18, 2017
- [AD 2015-02-08](https://openairdocs.org/ad/2015-02-08): Turbine wheels · Rolls-Royce AE 2100D2, AE 2100D2A, AE 2100D3 and 11 more. Effective Mar 11, 2015
- [AD 2009-24-04](https://openairdocs.org/ad/2009-24-04): Fan spinner · Rolls-Royce AE 3007A1, AE 3007A1E, AE 3007A1P and 5 more. Effective Dec 28, 2009
- [AD 2007-24-05](https://openairdocs.org/ad/2007-24-05): Engine oil temperature · Rolls-Royce AE 3007A, AE 3007A1, AE 3007A1/1 and 8 more. Effective Jan 2, 2008

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

- [AD 2006-23-05](https://openairdocs.org/ad/2006-23-05) (historical): Inboard- hinge brackets · Cessna 750. Effective Nov 22, 2006
- [AD 2006-04-10](https://openairdocs.org/ad/2006-04-10) (historical): Identification sleeves · Cessna Aircraft Company, The 500, 550, 560 and 3 more. Effective Mar 24, 2006
- [AD 2005-09-01](https://openairdocs.org/ad/2005-09-01) (historical): Auxiliary power unit (APU) fuel tube assembly · Cessna Aircraft Company, The 750. Effective May 10, 2005
- [AD 98-16-17](https://openairdocs.org/ad/98-16-17) (historical): Secondary Horizontal Stabilizer Trim Actuator · Cessna Aircraft Company, The 750. Effective Aug 24, 1998

## Information bulletins (advisory) (6 in force)

- [SAIB AIR-21-15R1](https://openairdocs.org/saib/AIR-21-15R1): Navigation System. Issued Sep 16, 2021
- [SAIB CE-10-49R1](https://openairdocs.org/saib/CE-10-49R1): Equipment/Furnishings Drain Mast Heater. Issued Jan 5, 2011
- [SAIB NM-10-45](https://openairdocs.org/saib/NM-10-45): Landing Gear: Nose/Tail Landing Gear Attach Section. Issued Aug 11, 2010
- [SAIB CE-10-29R1](https://openairdocs.org/saib/CE-10-29R1): Lights  Aft Side Ledger Divider Light. Issued May 21, 2010
- [SAIB NM-10-13](https://openairdocs.org/saib/NM-10-13): Navigation: Flight Management System. Issued Jan 7, 2010
- [SAIB NE-11-22](https://openairdocs.org/saib/NE-11-22): Engine Controls. Issued Feb 23, 2011
- [SAIB AIR-21-15](https://openairdocs.org/saib/AIR-21-15) (historical): Navigation System. Issued Aug 26, 2021
- [SAIB CE-10-49](https://openairdocs.org/saib/CE-10-49) (historical): Equipment/Furnishings Drain Mast Heater. Issued Sep 23, 2010
- [SAIB CE-10-29](https://openairdocs.org/saib/CE-10-29) (historical): Lights  Aft Side Ledger Divider Light. Issued Apr 28, 2010

## NTSB investigations

None matched to N265AV.

## FAA accident and incident reports

None matched to N265AV.

## Reports on N265AV not matched to an aircraft (1)

They name N265AV, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft.

- [Incident 20080517835079I](https://openairdocs.org/incident/20080517835079I), May 17, 2008: Airbus A320212 (N265AV), Miami, FL, Minor damage. (-23) Usa 3000 contracted aar certificate [privacy data omitted] to provide maintenance support for a lease return check on aircraft N265AV. On may 17, 2008 an…

## Service difficulty reports

None filed for this aircraft. Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.

## Service difficulty reports on N265AV not matched to an aircraft (25)

They name N265AV, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft.

- [SDR U30A200600008](https://openairdocs.org/sdr/U30A200600008), Mar 11, 2006: BEARING. SPALLED. SDR WRITTEN TO CLOSE SDR U30A200600003, WHICH READ: FLT 1013 CUN-STL; SHORTLY AFTER T/O, CREW REPORTED VIBRATION, POPPING SOUNDS COMING FROM NR 2 ENG. ENGINE RO
- [SDR U30A200600003](https://openairdocs.org/sdr/U30A200600003), Mar 11, 2006: ENGINE. MALFUNCTIONED. SHORTLY AFTER TAKE OFF, CREW REPORTED VIBRATION AND POPPING SOUNDS COMING FROM NR 2 ENGINE. ENGINE ROLLED BACK TO IDLE. CREW MAINTAINED IDLE CONDITION (ENGINE P
- [SDR U30A200600004](https://openairdocs.org/sdr/U30A200600004), Nov 29, 2005: SKIN. DENTED. PERMANENT REPAIR TO THE 1R PAX/CREW DOOR SKIN DENT AT FORWARD LOWER CORNER. REPAIRED UNDER EO 05-52-008, DATED 7 OCT 2005. WHICH INCORPORATES THE PERMANENT REPA
- [SDR U30A200300039](https://openairdocs.org/sdr/U30A200300039), Dec 26, 2003: A/C PACK. CONTAMINATED. AFTER LANDING, DURING TURNOFF FROM RUNWAY, CREW NOTED LIGHT SMOKE IN COCKPIT AND CABIN WITH NO DISTINCT ODOR OR ANY ECAM MESSAGE OR ABNORMAL INDICATION, EXCEPT 
- [SDR U30A200300037](https://openairdocs.org/sdr/U30A200300037), Nov 11, 2003: FRAME. CORRODED. CORROSION WAS FOUND AT FRAME 16, RT (R1 PAX/CREW DOOR FWD FRAME) UNDER SAFETY BARRIER ATTACH POINT. CORROSION WAS REMOVED IAW SRM 51-74-00. HFEC AND A ROTO TEST
- [SDR U30A200300036](https://openairdocs.org/sdr/U30A200300036), Oct 18, 2003: WARNING LIGHT. FALSE ACTIVATION. DURING CRUISE ON FLT 143 PUJ-BWI, THE LT AFT EMERGENCY WINDOW EXIT SHOWED ARMED ON ECAM (ABOVE FL 250). NO CHANGE IN CABIN ALTITUDE. ON GROUND, MAINTENANCE VERI
- [SDR U30A200300035](https://openairdocs.org/sdr/U30A200300035), Oct 17, 2003: CYLINDER. DISCHARGED. AFTER MAINTENANCE ACCEPTANCE FLIGHT ASSOCIATED WITH AN 8C CK & 10 YR INSP., ON FLT 9265 YWG-YWG, THE L2 PAX/CREW DOOR DAMPER & EMERGENCY OPERATION CYLINDER PRES
- [SDR U30A20030034](https://openairdocs.org/sdr/U30A20030034), Sep 17, 2003: SLIDE. MALFUNCTIONED. AIRCRAFT IN C CHECK AT YWG. DURING AN INTENTIONAL DEPLOYMENT OF THE R2 PAX/CREW DOOR SLIDE/RAFT, THE SLIDE/RAFT FAILED TO DEPLOY PROPERLY. THE DISCHARGE RIPCORD
- [SDR U30A200300033](https://openairdocs.org/sdr/U30A200300033), Aug 11, 2003: COMPUTER. MALFUNCTIONED. AFTER PUSHBACK FOR FLT 326 IN BWI, CREW RECEIVED ECAM MESSAGE FOR AUTO FLT YAW DAMPER FAULT, AFTER ENGINE START. AIRCRAFT RETURNED TO GATE. MAINTENANCE RESET TH
- [SDR U30A200300032](https://openairdocs.org/sdr/U30A200300032), Aug 8, 2003: WARNING LIGHT. ILLUMINATED. ON THE GROUND AFTER FLT 304, BWI- PUJ, THE CREW RECEIVED AN ECAM MESSAGE " F/CTL SYS NR 2 SLAT FAULT". MAINTENANCE ACCOMPLISHED TASK PER AMM 27-80-00-869-004. R
- [SDR U30A200300024](https://openairdocs.org/sdr/U30A200300024), Jul 31, 2003: SOLENOID. INTERMITTENT. ON GROUND IN CUN AFTER FLT 306 PIT-CUN, SLATS LOCKED AND WTB (WING TIP BRAKES) MESSAGE ON ECAM. CUN MAINTENANCE RESET THE WTB OF THE SLAT SYSTEM ON GROUND IAW A
- [SDR U30A200300023](https://openairdocs.org/sdr/U30A200300023), Jul 31, 2003: SMOKE DETECTOR. FAULTY. ON FLT 300, BWI-CUN, DURING TAXI IN, ECAM MESSAGE FOR SMOKE LAV AND CARGO DETECTOR FAULTED. MAINTENANCE IN CUN RESET CIRCUIT BREAKER AND PERFORMED OPS CHECK IAW
- [SDR U30A200300022](https://openairdocs.org/sdr/U30A200300022), Jul 28, 2003: SMOKE DETECTOR. MALFUNCTIONED. ON GROUND AFTER FLT 326 BWI-PUJ, LAV-D SHOWS SMOKE DETECTOR FAULT. DEFERRED LAV-D PER MEL 26-17-01. ON RETURN TO BWI (7/28/03) AFTER FLT 327, BWI MAINTENANCE OP
- [SDR U30A200300021](https://openairdocs.org/sdr/U30A200300021), Jul 16, 2003: SMOKE DETECTOR. FAULTY. AFTER FLT 319 CUN-BWI, DURING "DAILY CHECK", ECAM MESSAGE SHOWED SMOKE DETECTOR IN LAV D WAS FAULTED. REMOVED AND REPLACED LAV D SMOKE DETECTOR IAW AMM 27-17-15
- [SDR U30A200300019](https://openairdocs.org/sdr/U30A200300019), Jun 30, 2003: BATTERY PACK. DISCHARGED. DURING DAILY CHECK, AFTER FLT 329 IN BWI, MAINTENANCE PERSONNEL DISCOVERED THAT ROWS 21, 25 & 27 ON LT SIDE OF AIRCRAFT AND THE L2 & R2 (LT AND RT REAR DOORS) E
- [SDR U30A200300015](https://openairdocs.org/sdr/U30A200300015), May 8, 2003: CONNECTOR. ARCED. DURING MAINTENANCE INSPECTION, DURING ENGINE RUN, AN ECAM MESSAGE FOR THE RT FUEL TANK PUMP NR 2, LOW PRESSURE. FURTHER TROUBLESHOOTING REVEALED ELECTRICAL ARCI
- [SDR U30A200300014](https://openairdocs.org/sdr/U30A200300014), May 2, 2003: RESERVOIR. LOW. DURING DAILY INSPECTION AFTER FLT 313 IN BWI, THE L2 CREW PASSENGER DOOR EMERGENCY OPERATION CYLINDER PRESSURE WAS LOW. REPLACED DIAPHRAM PN FE240-221-001 AND A
- [SDR U30A200300011](https://openairdocs.org/sdr/U30A200300011), Mar 26, 2003: LIGHT. INTERMITTENT. DURING CRUISE ON FLT 313 CUN-BWI, THE EMERGENCY EXIT LIGHTS IN THE CENTER OF AIRCRAFT FLASH SPORADICALLY. ON GROUND IN BWI, PERFORMED OPERATIONAL TEST OF EMERGE
- [SDR U30A200300010](https://openairdocs.org/sdr/U30A200300010), Mar 23, 2003: COMPUTER. FAULTY. AFTER FLT 306 BWI-CUN, IN CUN AT GATE, THE NR 1 FLIGHT MANAGEMENT GUIDANCE COMPUTER (FMGC) FAILED. DEFERRED PER MEL 22-83-01. IN BWI ON 3/25/03, RESET NR 1 FMGC
- [SDR U30A200300009](https://openairdocs.org/sdr/U30A200300009), Mar 12, 2003: LIGHT. MALFUNCTIONED. IN CRUISE DURING FLT 315 RSW-BWI AND THEN ON DESCENT, THE EMERGENCY EXIT LIGHTS IN REAR OF AIRCRAFT AND ON AFT DOORS NOT LIGHT, INOPERATIVE. OTHERS AT MID CABIN
- [SDR U30A200300007](https://openairdocs.org/sdr/U30A200300007), Mar 2, 2003: LIGHT. MALFUNCTIONED. DURING CRUISE ON FLT 307 CUN-PIT, THE LEFT MID CABIN & AFT EMERGENCY EXIT LIGHTS (OVER EXITS) WENT INOP. ON GROUND IN PIT RECYCLED EMERGENCY LIGHT ARM SWITCH & 
- [SDR U30A200300005](https://openairdocs.org/sdr/U30A200300005), Feb 9, 2003: SMOKE DETECTOR. FAULTY. DURING CRUISE ON FLT 304 BWI-PUJ, ECAM MESSAGE APPEARED "SMOKE-LAVATORY DET FAULT". ON GROUND IN PUJ TESTED SYSTEM & FOUND FWD LAV DETECTOR FAULT. DEFERRED PER 
- [SDR U30A200300003](https://openairdocs.org/sdr/U30A200300003), Jan 29, 2003: SEAL. DAMAGED. DURING WEEKLY INSPECTION AFTER FLT 315 IN BWI, THE R2 CREW PASSENGER DOOR EMERGENCY OPERATION CYLINDER PRESSURE WAS LOW. REPLACED SEAL P/N FE240-221-001 AND ASS
- [SDR U30A200300002](https://openairdocs.org/sdr/U30A200300002), Jan 9, 2003: COMPUTER. INTERMITTENT. DURING INSPECTION AFTER FLT 314 AT BWI, INTERROGATED CFDS & FOUND MESSAGE: "SEC 1 OR INPUT OF CAPT ROLL CTL SSTU 4CE1". CAATS RECOMMENDS REPLACEMENT OF SEC NR 1
- [SDR U30A200300001](https://openairdocs.org/sdr/U30A200300001), Jan 5, 2003: SEAL. DAMAGED. DURING DAILY INSPECTION AFTER FLT 305 IN BWI, THE L1 CREW/PASSENGER DOOR EMERGENCY OPERATION CYLINDER PRESSURE WAS LOW. SERVICED THE EMERGENCY OPERATION CYLINDE

## STCs that may be installed (OpenAirDocs) (73, first 50)

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 airframe (Cessna 750)

- [STC ST01305WI-D](https://openairdocs.org/stc/ST01305WI-D): Modification of a Collins ALT-50A or ALT-55B Radio Altimeter system installation to a Collins ALT-1000 or ALT-4000 Radio Altimeter system installation in accordance with Collins Drawing Index as listed on AML No. ST01305WI-D, Revision -, or later FAA approved revision. Rockwell Collins Inc
- [STC ST12461IB](https://openairdocs.org/stc/ST12461IB): Installation of Cockpit Voice Recorder with optional RIPS Upgrade. Mid- Canada Mod Center
- [STC ST00197IB](https://openairdocs.org/stc/ST00197IB): Installation of the Universal Quick Access Recorder (uQAR). Flight Data Technologies Inc
- [STC ST04578CH](https://openairdocs.org/stc/ST04578CH): Installation of SmartSky system. Apcela ATG
- [STC ST12344IB](https://openairdocs.org/stc/ST12344IB): Replacement of the Halon Type 1211 portable fire extinguisher with Halotron BrX portable fire extinguisher with Halotron BrX portable fire extinguisher. Cessna Duesseldorf Citation Service Center GmbH
- [STC SA2622NM](https://openairdocs.org/stc/SA2622NM): Installation of Precise Flight Pulselite Control Unit in landing/taxi system. (767-200 B17) (DHC-8 101). Precise Flight Inc
- [STC ST04269AT](https://openairdocs.org/stc/ST04269AT): Installation of Send Solutions, LLC Airtext Messaging System which connects the passengers phones and portable electronic devices via Bluetooth to provide the passengers with in-flight messaging service via the Iridium Satellite Communication Network. Send Solutions LLC
- [STC ST00892LA](https://openairdocs.org/stc/ST00892LA): Installation of Emergency Vision Assurance System (EVAS). VisionSafe LLC
- [STC ST03885AT](https://openairdocs.org/stc/ST03885AT): Installation of an Avionica, Inc. avCM Cellular Module. Aircraft Systems and Manufacturing Inc
- [STC ST11873SE](https://openairdocs.org/stc/ST11873SE): Installation of Starlink Aviation System. AeroMech Incorporated
- [STC ST12016IB](https://openairdocs.org/stc/ST12016IB): Installation of Gogo AVANCE L5/LX5. Sky Service F.B.O Inc
- [STC ST02472AT](https://openairdocs.org/stc/ST02472AT): Installation of a mini Quick Access Recorder (QAR) model MKI, MKII, or MKIII. Aircraft Systems and Manufacturing Inc
- [STC ST01117DE](https://openairdocs.org/stc/ST01117DE): Installation of the Gogo ATG C1. Peregrine
- [STC ST01936WI](https://openairdocs.org/stc/ST01936WI): Installation of LED lights. AeroLED's Holdings LLC
- [STC ST04159CH](https://openairdocs.org/stc/ST04159CH): Upgrade of Honeywell Primus II Communications Units RCZ-8XX Transponders to support Certification of Automatic Dependent Surveillance -Broadcast (ADS-B) Out. CMD Flight Solutions LLC
- [STC ST03424CH](https://openairdocs.org/stc/ST03424CH): Certification of Automatic Dependent Surveillance - Broadcast (ADS-B) Out System with Rockwell Collins TDR-94/-94D Transponders. CMD Flight Solutions LLC
- [STC ST04575AT](https://openairdocs.org/stc/ST04575AT): Installation of the Rockwell Collins ALT-1000+/ -4000+ with 5G Filtering. Chippewa Aerospace Inc
- [STC ST01070DE](https://openairdocs.org/stc/ST01070DE): Installation of the Curtiss-Wright Fortress Flight Data Recorder (with Cockpit Voice Recorder). Peregrine
- [STC ST00011WI](https://openairdocs.org/stc/ST00011WI): Installation of Concorde RG380E/40 and 40B battery. Aero-Mach Wilco LLC
- [STC ST04519CH](https://openairdocs.org/stc/ST04519CH): Installation of a Honeywell FANS-1/A+ Datalink Communications System in accordance with West Star Aviation Master Data List, Doc. No. A21311L-658, Revision A, dated November 3, 2021, or later FAA-approved revision. West Star Aviation
- [STC SA04518CH](https://openairdocs.org/stc/SA04518CH): Installation of a Honeywell Flight Management System Software Update to version NZ 6.2.1 in accordance with West Star Aviation Master Data List, Doc. No. A21312L-652, Revision I/R, dated October 4, 2021, or later FAA-approved revision. West Star Aviation
- [STC ST02715SE](https://openairdocs.org/stc/ST02715SE): Installation of the Honeywell RDR-7000 Volumetric Buffer Weather Radar System. Honeywell International Inc
- [STC ST00818DE](https://openairdocs.org/stc/ST00818DE): Installation of Honeywell Control Display Unit (CDU) model CD-830. Premier Air Center LLC d/b/a West Star Aviation
- [STC ST04177AT](https://openairdocs.org/stc/ST04177AT): Installation of a Talon Aerospace LED Replacement General Purpose Lamps. Aaxico Technical Services Inc
- [STC ST03595NY](https://openairdocs.org/stc/ST03595NY): Installation of Honeywell Laseref IV Upgrade. Dassault Aircraft Services (DAS)
- [STC ST01950WI](https://openairdocs.org/stc/ST01950WI): Installation of Gogo Business Aviation AVANCE L5 Broadband. Duncan Aviation Inc
- [STC ST01942WI](https://openairdocs.org/stc/ST01942WI): Installation of Garmin G5000 System Release v4.5. Wichita Citation Center
- [STC SA01452CH](https://openairdocs.org/stc/SA01452CH): Installation of an air ambulance conversion kit. Med-Pac Inc
- [STC ST00954DE](https://openairdocs.org/stc/ST00954DE): Demonstration of Aircraft Compatibility to Wireless Fidelity (WiFi) Data Transmissions (Ground & Flight). West Star Aviation
- [STC ST01859WI](https://openairdocs.org/stc/ST01859WI): Installation of Gogo Business Aviation's Gogo Biz 4G Air-to-Ground System. Textron Aviation Inc Wichita Citation Service Center
- [STC ST00934DE](https://openairdocs.org/stc/ST00934DE): Installation of Becker Avionics BXT6553 transponder. Peregrine
- [STC ST02119LA](https://openairdocs.org/stc/ST02119LA): Installation of a Patient Loading and Utility System (PLUS). LifePort LLC
- [STC ST04340NY](https://openairdocs.org/stc/ST04340NY): Installation of TCAS 7.1 (ACAS II) upgrade of Prior Existing TCAS 7.0. Scandinavian Avionics Design ApS
- [STC ST00347BO](https://openairdocs.org/stc/ST00347BO): Modification to upgrade a BendixKing CAS 67A TCAS II system to CAS 67B TCAS II Change 7.1. Pro Star Aviation, LLC
- [STC ST00361BO](https://openairdocs.org/stc/ST00361BO): Installation of a Honeywell Primus II (XS-852) ADS-B Out System. Pro Star Aviation, LLC
- [STC ST00135BO](https://openairdocs.org/stc/ST00135BO): Modification of Honeywell TCAS II system installation with R/T 910 and software Version 6.4a to R/T 910 with Change 7.0 software; or TCAS 2000 system with R/T 950, 951 and software Version 6.4a to R/T 950, 951 with Change 7.0 software. Pro Star Aviation, LLC
- [STC ST04146NY](https://openairdocs.org/stc/ST04146NY): Upgrade for ADS-B Out capability on aircraft equipped with Primus II Radio Suites. 328 Support Services GmbH
- [STC ST01720WI](https://openairdocs.org/stc/ST01720WI): Installation of a Safe Flight Instrument Corporation Auto Throttle System. Textron Aviation Inc
- [STC ST03271CH](https://openairdocs.org/stc/ST03271CH): Upgrade existing Honeywell Mark V Enhanced Ground Proximity Warning System software level and activate the Runway Awareness Advisory System (including enhanced features known as SmartRunway SmartLanding). Textron Aviation Inc
- [STC ST11071SC](https://openairdocs.org/stc/ST11071SC): Demonstration of aircraft critical equipment and antenna systems tolerance of radio frequency interference (RFI) from intentional or spurious transmissions from certain Portable Electronic Devices (PEDs). Liberty Partners Inc
- [STC ST04194CH](https://openairdocs.org/stc/ST04194CH): Install Honeywell Liquid Crystal Display (LCD) Flight Displays. Pentastar Aviation LLC
- [STC ST03957AT](https://openairdocs.org/stc/ST03957AT): Activation of Aircell Axxess Cabin Telecommunications Router (CTR) Wireless Local Area Network (WLAN) in accordance with Constant Aviation LLC, Master Drawing List DB1107001, Revision IR, dated December 9, 2011, or later FAA approved revision. Nextant Aerospace
- [STC ST03776NY](https://openairdocs.org/stc/ST03776NY): Modification to upgrade existing Rockwell Collins TCAS (Model: TTR-920, TTR-921, and TTR-4000) at VERSION 7.0 to Rockwell Collins TCAS (Model: TTR-921, TTR-4000, and TTR-4100) at VERSION 7.1 (ACAS II). Scandinavian Avionics Design ApS
- [STC ST01545WI](https://openairdocs.org/stc/ST01545WI): Installation of winglets, wing structural reinforcement, and related system changes. Winglet Technology LLC
- [STC ST00881WI-D](https://openairdocs.org/stc/ST00881WI-D): Modification of a TCAS II system installation to Change 7.0 or Change 7.1. Rockwell Collins Inc
- [STC ST00796DE](https://openairdocs.org/stc/ST00796DE): Installation of Teledyne Battery Products P/N 7638-44T Lead-Acid Battery. Teledyne Battery Products
- [STC ST01399WI](https://openairdocs.org/stc/ST01399WI): Installation of Honeywell DL-950 Data Loader. Textron Aviation Inc
- [STC SA04006CH](https://openairdocs.org/stc/SA04006CH): Installation of Fuel Vent Scoop. Textron Aviation Inc
- [STC ST02127LA](https://openairdocs.org/stc/ST02127LA): Installation of a Crane Aerospace & Electronics Tire Sensor Assembly. ELDEC Corporation
- [STC ST00673WI-D](https://openairdocs.org/stc/ST00673WI-D): Modification of Collins VHF-22A/VHF-22B VHF COMM Receiver Transmitter with CTL-22 Control Pro Line II System Installation to a Collins VHF-22C/VHF-22D VHF COMM Receiver Transmitter with CTL-22C Control 8.33 kHz Pro Line II System installation. Rockwell Collins Inc

All 73: https://openairdocs.org/aircraft/N265AV/stcs.md

## Earlier aircraft with N265AV

The FAA can reassign an N-number once a registration is cancelled. These aircraft carried N265AV before.

- [Cancelled 2017-10-31](https://openairdocs.org/deregistered/N265AV-2017-10-31): Bombardier CL-600-2B19, S/N 7128. Exported to Canada. Owner: [Wells Fargo Bank Northwest Na Trustee](https://openairdocs.org/faa-owner/WELLS%20FARGO%20BANK%20NORTHWEST%20NA%20TRUSTEE), [Salt Lake City, UT](https://openairdocs.org/faa-place/UT/Salt%20Lake%20City)

## Related

- Other Cessna 750 aircraft: https://openairdocs.org/model/cessna-750/aircraft.md
- The Allison AE-3007C1 engine: https://openairdocs.org/engine/allison-ae-3007c1.md

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