# N180AV: 1996 Piaggio P180

- Status: Valid registration
- Airframe: [Piaggio P180](https://openairdocs.org/model/piaggio-p180) (registry code 6960204, 11 seats)
- Engine: [Pratt & Whitney PT6A series](https://openairdocs.org/engine/pratt-whitney-pt6a-series) (registry code 52032)
- Data sheets: [TCDS A59EU](https://openairdocs.org/tcds/A59EU) (Baykar Piaggio Aerospace S.p.A.) (OpenAirDocs)
- Serial number: 1018
- Year built: 1996
- Type: Fixed wing multi engine
- Engine type: Turbo-prop
- Airworthiness: Standard, normal
- Airworthiness date: December 12, 1996
- Certificate issued: April 4, 2022
- Expires: April 30, 2029
- Mode S code: A140C0
- Registered owner: [Adams Aviation Services Inc Trustee](https://openairdocs.org/faa-owner/ADAMS%20AVIATION%20SERVICES%20INC%20TRUSTEE)
- Location: [Wilmington, DE](https://openairdocs.org/faa-place/DE/Wilmington)
- Owner type: Corporation
- Owner's area on the map: 39.7236° N, 75.5412° W: Placed by OpenAirDocs at the center of ZIP code 19801, 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=180AV
- Page: https://openairdocs.org/aircraft/N180AV

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. The registry lists only the engine series, so ADs for every Pratt & Whitney PT6A model are included.

## ADs that may apply (OpenAirDocs): 81 in force

### Matched by airframe (Piaggio P180)

- [AD 2026-06-05](https://openairdocs.org/ad/2026-06-05): Vertical Stabilizer Structure · Baykar Piaggio Aerospace P-180. Effective May 11, 2026
- [AD 2026-05-10](https://openairdocs.org/ad/2026-05-10): Flight Control System · Baykar Piaggio Aerospace P-180. Effective Apr 27, 2026
- [AD 2025-26-05](https://openairdocs.org/ad/2025-26-05): Hydraulic System, Main · Baykar Piaggio Aerospace P-180. Effective Feb 17, 2026
- [AD 2025-15-10](https://openairdocs.org/ad/2025-15-10): Horizontal Stabilizer Structure · Piaggio P-180. Effective Sep 3, 2025
- [AD 2023-16-04](https://openairdocs.org/ad/2023-16-04): Elevator Structure · Piaggio P-180. Effective Aug 30, 2023
- [AD 2022-22-07](https://openairdocs.org/ad/2022-22-07): Fuselage Main, Plate/Skin · Piaggio P-180. Effective Dec 23, 2022
- [AD 2022-19-07](https://openairdocs.org/ad/2022-19-07): Pitot/Static System · Piaggio P-180. Effective Nov 3, 2022
- [AD 2022-17-13](https://openairdocs.org/ad/2022-17-13): Air Data Computer · Piaggio Aero Industries P-180. Effective Oct 11, 2022
- [AD 2020-19-10](https://openairdocs.org/ad/2020-19-10): Landing Gear · Piaggio Aero Industries P-180. Effective Nov 3, 2020
- [AD 2017-20-13](https://openairdocs.org/ad/2017-20-13): Flight Controls · Piaggio Aero Industries P-180. Effective Nov 16, 2017
- [AD 2015-19-11](https://openairdocs.org/ad/2015-19-11): Fuselage · Piaggio Aero Industries P-180. Effective Nov 3, 2015
- [AD 2014-18-01](https://openairdocs.org/ad/2014-18-01): Navigation · Bombardier ATR42-200, ATR42-300, ATR42-320 and 23 more. Effective Oct 14, 2014
- [AD 2014-09-04](https://openairdocs.org/ad/2014-09-04): Landing Gear · Piaggio Aero Industries P-180. Effective Jun 13, 2014
- [AD 2014-03-20](https://openairdocs.org/ad/2014-03-20): Flight Controls · Piaggio Aero Industries P-180. Effective Apr 1, 2014
- [AD 2013-18-04](https://openairdocs.org/ad/2013-18-04): Landing Gear · Piaggio Aero Industries P-180. Effective Oct 18, 2013
- [AD 99-07-10 R1](https://openairdocs.org/ad/99-07-10-R1): Nacelles/Pylons · Piaggio Aero Industries P-180. Effective Sep 19, 2013
- [AD 2000-07-11 R1](https://openairdocs.org/ad/2000-07-11-R1): Landing Gear · Piaggio Aero Industries P-180. Effective Nov 21, 2012
- [AD 2003-17-03 R1](https://openairdocs.org/ad/2003-17-03-R1): Fuel · Piaggio Aero Industries P-180. Effective Nov 14, 2012
- [AD 2012-18-06](https://openairdocs.org/ad/2012-18-06): Flight Controls · Piaggio Aero Industries P-180. Effective Oct 22, 2012
- [AD 2011-26-01](https://openairdocs.org/ad/2011-26-01): Doors · Piaggio Aero Industries P-180. Effective Jan 17, 2012
- [AD 2011-24-01](https://openairdocs.org/ad/2011-24-01): Landing Gear · Piaggio Aero Industries P-180. Effective Dec 22, 2011
- [AD 2011-09-51](https://openairdocs.org/ad/2011-09-51): Fuselage · Piaggio Aero Industries P-180. Effective May 31, 2011
- [AD 2011-05-01](https://openairdocs.org/ad/2011-05-01): Cargo and Accessory Compartments · Piaggio Aero Industries P-180. Effective Mar 31, 2011
- [AD 2010-23-01](https://openairdocs.org/ad/2010-23-01): Stabilizers · Piaggio Aero Industries P-180. Effective Dec 10, 2010
- [AD 2010-21-14](https://openairdocs.org/ad/2010-21-14): Fuselage · Piaggio Aero Industries P-180. Effective Nov 18, 2010
- [AD 2010-21-09](https://openairdocs.org/ad/2010-21-09): Engine oil · Piaggio Aero Industries P-180. Effective Nov 18, 2010
- [AD 2010-21-08](https://openairdocs.org/ad/2010-21-08): Engine oil · Piaggio Aero Industries P-180. Effective Nov 18, 2010
- [AD 2010-09-09](https://openairdocs.org/ad/2010-09-09): Fuel · Piaggio Aero Industries P-180. Effective Jun 3, 2010
- [AD 2010-03-09](https://openairdocs.org/ad/2010-03-09): Fuselage · Piaggio Aero Industries P-180. Effective Mar 11, 2010
- [AD 2010-03-04](https://openairdocs.org/ad/2010-03-04): Electric power · Piaggio Aero Industries P-180. Effective Mar 11, 2010
- [AD 2008-03-14](https://openairdocs.org/ad/2008-03-14): Emergency exit door · Piaggio Aero Industries P-180. Effective Mar 11, 2008
- [AD 2007-24-15](https://openairdocs.org/ad/2007-24-15): Longitudinal flight control cables · Piaggio Aero Industries P-180. Effective Jan 7, 2008
- [AD 2007-18-07](https://openairdocs.org/ad/2007-18-07): Hydraulic fluid of the steering system · Piaggio Aero Industries P-180. Effective Oct 11, 2007
- [AD 2007-13-12](https://openairdocs.org/ad/2007-13-12): Main wing outboard flap · Piaggio Aero Industries P-180. Effective Aug 3, 2007
- [AD 2005-01-19](https://openairdocs.org/ad/2005-01-19): Mode S transponders · GARMIN International GTX 330D, GTX 330, GTX 33D and 830 more. Effective Feb 23, 2005
- [AD 2003-04-08](https://openairdocs.org/ad/2003-04-08): Placard (Inside of the lavatory door) · Piaggio Aero Industries P-180. Effective Apr 11, 2003
- [AD 2002-23-10](https://openairdocs.org/ad/2002-23-10): First Outboard Flap Control Rod and the Bleed Air Duct · Piaggio Aero Industries P-180. Effective Dec 17, 2002
- [AD 2002-14-19](https://openairdocs.org/ad/2002-14-19): Collins Air Data Computers (ADC) · Boeing DC-8-11, DC-8-12, DC-8-21 and 36 more. Effective Aug 23, 2002
- [AD 2002-08-04](https://openairdocs.org/ad/2002-08-04): Horizontal Stabilizer Hinge Bushings · Piaggio Aero Industries P-180. Effective Jun 10, 2002
- [AD 2001-05-04](https://openairdocs.org/ad/2001-05-04): Flap Actuators · Piaggio Aero Industries P-180. Effective Apr 27, 2001
- [AD 2000-03-19 REM](https://openairdocs.org/ad/2000-03-19-REM): Pneumatic Deicing Boots · Piaggio Aero Industries P-180. Effective Jan 2, 2001
- [AD 99-11-06](https://openairdocs.org/ad/99-11-06): Environmental Control System Bleed Tubes · Piaggio Aero Industries P-180. Effective Jul 5, 1999
- [AD 99-07-10](https://openairdocs.org/ad/99-07-10): Engine Nacelle Inner Panels · Piaggio Aero Industries P-180. Effective May 10, 1999
- [AD 98-23-14](https://openairdocs.org/ad/98-23-14): Elevator & Aileron Control Retaining Pins · Piaggio Aero Industries P-180. Effective Dec 18, 1998
- [AD 98-13-07](https://openairdocs.org/ad/98-13-07): Lavatory Water Tube/Hose Connections · Piaggio Aero Industries P-180. Effective Aug 1, 1998
- [AD 98-12-13](https://openairdocs.org/ad/98-12-13): Low Pitch Stop Switch Support · Piaggio Aero Industries P-180. Effective Jul 18, 1998
- [AD 98-08-05](https://openairdocs.org/ad/98-08-05): Main Landing Gear Drag Brace Link and Retraction Actuator · Piaggio Aero Industries P-180. Effective May 26, 1998
- [AD 98-06-05](https://openairdocs.org/ad/98-06-05): AFM, POH - Autopilot · Piaggio Aero Industries P-180. Effective Apr 2, 1998
- [AD 97-22-11](https://openairdocs.org/ad/97-22-11): Airplane Flight Manual (AFM) - Limitations Section - Power Levers · Piaggio Aero Industries P-180. Effective Dec 5, 1997
- [AD 97-15-14](https://openairdocs.org/ad/97-15-14): Torque Tube Bottom Flange Assembly · Piaggio Aero Industries P-180. Effective Sep 19, 1997

### Matched by engine (Pratt & Whitney PT6A series)

- [AD 2024-04-51](https://openairdocs.org/ad/2024-04-51): Turbine Section · Pratt & Whitney Canada PT6A-64, PT6A-66, PT6A-66A and 17 more. Effective Mar 28, 2024
- [AD 2022-08-13](https://openairdocs.org/ad/2022-08-13): Turbine Section · Pratt & Whitney Canada PT6A-34, PT6A-34B, PT6A-34AG and 2 more. Effective May 27, 2022
- [AD 2016-05-13](https://openairdocs.org/ad/2016-05-13): Corrosion and perforation of the two-ply Cu-Be bellows in Woodward FCUs. · Pratt & Whitney Canada PT6A-60AG, PT6A-65AG, PT6A-67AF and 1 more. Effective Apr 22, 2016
- [AD 2014-17-08 R1](https://openairdocs.org/ad/2014-17-08-R1): Compressor turbine (CT) blades · Pratt & Whitney Canada PT6A-114 and PT6A-114A. Effective Jun 5, 2015
- [AD 2014-11-05](https://openairdocs.org/ad/2014-11-05): Reinforcement liner to the power turbine (PT) containment   
  ring and, for certain PT containment rings, adding scallops · Pratt & Whitney Canada PT6A-11, PT6A-110, PT6A-112 and 18 more. Effective Aug 5, 2014
- [AD 2012-09-10](https://openairdocs.org/ad/2012-09-10): First stage sun gears · Pratt & Whitney Canada PT6A-110, PT6A-112, PT6A-114 and 12 more. Effective May 23, 2012
- [AD 2011-25-12](https://openairdocs.org/ad/2011-25-12): Sun gear · Pratt & Whitney Canada PT6A-15AG, PT6A-27, PT6A-28 and 4 more. Effective Dec 28, 2011
- [AD 2011-20-51](https://openairdocs.org/ad/2011-20-51): Gears · Pratt & Whitney Canada PT6A-15AG, PT6A-27, PT6A-28 and 4 more. Effective Nov 1, 2011
- [AD 2004-25-18](https://openairdocs.org/ad/2004-25-18): Propeller governor assemblies · Pratt & Whitney Canada PT6A-60A and PT6A-65B. Effective Jan 18, 2005
- [AD 2002-23-13](https://openairdocs.org/ad/2002-23-13): Turbine Exhaust Ducts · Pratt & Whitney Canada PT6A-11, PT6A-110, PT6A-112 and 20 more. Effective Dec 31, 2002
- [AD 2001-20-01](https://openairdocs.org/ad/2001-20-01): Compressor Bleed Valve Assembly · Pratt & Whitney Canada PT6A-114A and PT6A-25C. Effective Nov 5, 2001
- [AD 97-04-12](https://openairdocs.org/ad/97-04-12): Compressor Bleed-off Valve · Pratt & Whitney Canada PT6A-11, PT6A-110, PT6A-112 and 52 more. Effective Mar 14, 1997
- [AD 95-13-08](https://openairdocs.org/ad/95-13-08): Compressor Turbine Disk · Pratt & Whitney Canada PT6A-67D. Effective Jul 12, 1995
- [AD 93-23-06](https://openairdocs.org/ad/93-23-06): Airframe Chip Detector Flag System · Pratt & Whitney Canada PT6A-50. Effective Jan 26, 1994
- [AD 92-15-11](https://openairdocs.org/ad/92-15-11): Compressor Delivery Air Line (P3) Filter Assembly · Pratt & Whitney Canada PT6A-20, PT6A-20A, PT6A-21 and 7 more. Effective Aug 17, 1992
- [AD 90-12-05](https://openairdocs.org/ad/90-12-05): Engine Overhaul · Pratt & Whitney Canada PT6A-15AG, PT6A-27, PT6A-28 and 3 more. Effective May 30, 1990
- [AD 86-10-05](https://openairdocs.org/ad/86-10-05): First Stage Compressor Hub · Pratt & Whitney Canada PT6A-42. Effective Jun 5, 1986
- [AD 80-08-12](https://openairdocs.org/ad/80-08-12): Fuel Pump Drive Coupling Splines · Pratt & Whitney Canada PT6A-11, PT6A-112, PT6A-135 and 24 more. Effective Apr 18, 1980
- [AD 80-04-02](https://openairdocs.org/ad/80-04-02): Push-Pull Control Terminal · Pratt & Whitney Canada PT6A-20, PT6A-6A, PT6A-6B and 1 more. Effective Feb 8, 1980
- [AD 78-17-07](https://openairdocs.org/ad/78-17-07): Fuel Control Unit · Pratt & Whitney Canada PT6A-38, PT6A-41 and PT6A-45A. Effective Aug 31, 1978
- [AD 78-12-04](https://openairdocs.org/ad/78-12-04): No. 2 Bearing Pressure Oil Transfer Tube Assembly · Pratt & Whitney Canada PT6A-38, PT6A-41 and PT6A-45A. Effective Jun 19, 1978
- [AD 75-06-01](https://openairdocs.org/ad/75-06-01): Gearbox Deterioration · Pratt & Whitney Canada PT6A-20, PT6A-20A, PT6A-20B and 11 more. Effective Apr 1, 1977
- [AD 75-11-04](https://openairdocs.org/ad/75-11-04): Reduction Gearbox Engine Distress · Pratt & Whitney Canada PT6A-20, PT6A-20A, PT6A-20B and 8 more. Effective May 20, 1975
- [AD 70-16-01](https://openairdocs.org/ad/70-16-01): Turbo Propeller Governors · Pratt & Whitney Canada PT6A-11, PT6A-11AG, PT6A-15AG and 5 more. Effective Aug 4, 1970
- [AD 69-23-06](https://openairdocs.org/ad/69-23-06): Fuel Pumps · Pratt & Whitney Canada PT6A-20, PT6A-27, PT6A-28 and 4 more. Effective Nov 15, 1969
- [AD 68-05-03](https://openairdocs.org/ad/68-05-03): Reverse Mode · Pratt & Whitney Canada PT6A-20 and PT6A-6B. Effective Feb 28, 1968

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

- [AD 2023-25-03](https://openairdocs.org/ad/2023-25-03) (historical): Horizontal Stabilizer Structure · Piaggio P-180. Effective Feb 2, 2024
- [AD 2011-01-53](https://openairdocs.org/ad/2011-01-53) (historical): Fuselage · Piaggio Aero Industries P-180. Effective Jan 24, 2011
- [AD 2011-01-51](https://openairdocs.org/ad/2011-01-51) (historical): Fuselage · Piaggio Aero Industries P-180
- [AD 2009-21-08 R1](https://openairdocs.org/ad/2009-21-08-R1) (historical): Landing gear · Piaggio Aero Industries P-180. Effective Dec 14, 2009
- [AD 2009-21-08](https://openairdocs.org/ad/2009-21-08) (historical): Landing Gear · Piaggio Aero Industries P-180. Effective Dec 14, 2009
- [AD 2003-17-03](https://openairdocs.org/ad/2003-17-03) (historical): Firewall shutoff or crossfeed valve · Piaggio Aero Industries P-180. Effective Sep 3, 2003
- [AD 2003-03-14](https://openairdocs.org/ad/2003-03-14) (historical): Firewall Shutoff or Crossfeed Valve · Piaggio Aero Industries P-180. Effective Mar 8, 2003
- [AD 2000-07-11](https://openairdocs.org/ad/2000-07-11) (historical): Brake Assembly Rods and Tubings · Piaggio Aero Industries P-180. Effective May 29, 2000
- [AD 2000-03-19](https://openairdocs.org/ad/2000-03-19) (historical): Airframe Pneumatic Deicing Boots · Industrie Aeronautiche e Meccaniche P-180. Effective Apr 7, 2000
- [AD 2014-17-08](https://openairdocs.org/ad/2014-17-08) (historical): Compressor turbine (CT) blades · Pratt & Whitney Canada PT6A-114 and PT6A-114A. Effective Oct 8, 2014
- [AD 88-24-02](https://openairdocs.org/ad/88-24-02) (historical): Airframe Chip Detector Flag System · Pratt & Whitney Canada PT6A-50

All 92: https://openairdocs.org/aircraft/N180AV/ads.md

## Information bulletins (advisory) (12 in force)

- [SAIB CE-12-05](https://openairdocs.org/saib/CE-12-05): Navigation: Water freezing in Pitot-Static System. Issued Nov 2, 2011
- [SAIB CE-03-42](https://openairdocs.org/saib/CE-03-42): . Issued Jun 27, 2003
- [SAIB CE-01-40](https://openairdocs.org/saib/CE-01-40): . Issued Aug 30, 2001
- [SAIB CE-01-35](https://openairdocs.org/saib/CE-01-35): . Issued Aug 3, 2001
- [SAIB ACE-98-29](https://openairdocs.org/saib/ACE-98-29): . Issued May 13, 1998
- [SAIB ACE-96-07](https://openairdocs.org/saib/ACE-96-07): . Issued Oct 17, 1996
- [SAIB ACE-95-04](https://openairdocs.org/saib/ACE-95-04): . Issued Nov 7, 1995
- [SAIB NE-15-21](https://openairdocs.org/saib/NE-15-21): Fuel Injector Nozzle. Issued Aug 19, 2015
- [SAIB NE-12-04](https://openairdocs.org/saib/NE-12-04): Turbine/ Turboprop Engine: Reduction Gearbox. Issued Nov 1, 2011
- [SAIB NE-10-47](https://openairdocs.org/saib/NE-10-47): Turbine Engine Compressor Section. Issued Aug 30, 2010
- [SAIB NE-06-34](https://openairdocs.org/saib/NE-06-34): . Issued Mar 21, 2006
- [SAIB CE-03-24](https://openairdocs.org/saib/CE-03-24): . Issued Feb 19, 2003

## NTSB investigations

None matched to N180AV.

## FAA accident and incident reports

None matched to N180AV.

## Service difficulty reports (1)

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 2007FA0001096](https://openairdocs.org/sdr/2007FA0001096), Nov 21, 2007: MOUNT. CHAFED. OIL COOLER RETURN LINE CHAFED AGAINST ENGINE MOUNT. DID NOT SHOW SIGNS OF CHAFING STATICALLY DURING ROUTINE INSPECTIONS, WAS CHAFING DURING FLIGHT. INSTALLED RE

## STCs that may be installed (OpenAirDocs) (158, 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 (Piaggio P180)

- [STC SA02571SE](https://openairdocs.org/stc/SA02571SE): Installation of Garmin G500/G600 TXi Integrated Avionics System (Primary Flight Display, Multi-Function Display, and Engine Indicating System Display). Garmin International Inc
- [STC SA02279AT](https://openairdocs.org/stc/SA02279AT): Installation of a Boom Beam bulb, starter, and ballast. Whelen Aerospace Technologies
- [STC SA04837NY](https://openairdocs.org/stc/SA04837NY): Installation of AeroLED's Holdings, LLC., position lights, navigation lights, strobe lights and beacon lights. AeroLED's Holdings, LLC
- [STC SA11158SC](https://openairdocs.org/stc/SA11158SC): Demonstration of aircraft tolerance to potential electromagnetic interference from certain Transmitting Potable Electronic Devices (T-PEDS). Liberty Partners Inc
- [STC SA11300DS](https://openairdocs.org/stc/SA11300DS): Upgrade previously installed Collins Aerospace Radar Altimeter. BHE & Associates Ltd
- [STC SA02738CH](https://openairdocs.org/stc/SA02738CH): Installation of L-3 Communications Avionics Systems. Acron Aviation Inc
- [STC SA04046CH PAGE 2](https://openairdocs.org/stc/SA04046CH%20PAGE%202): Installation of L-3 GENESIS (TM) Electronic Standby Instrument System (ESI-500/MAG-500). Acron Aviation Inc
- [STC SA01848WI](https://openairdocs.org/stc/SA01848WI): Modification of a Rockwell Collins Global Positioning System (GPS). Rockwell Collins Inc
- [STC SA04051CH](https://openairdocs.org/stc/SA04051CH): Certification of Automatic Dependent Surveillance - Broadcast (ADS-B) Out System with Rockwell Collins TDR-94/-94D Transponders. CMD Flight Solutions LLC
- [STC SA02658SE](https://openairdocs.org/stc/SA02658SE): Installation of Garmin GI 275 Multi-Function Display System. Garmin International Inc
- [STC SA00076IB](https://openairdocs.org/stc/SA00076IB): Installation of Photo luminescent Safety Systems. STG AEROSPACE GERMANY GmbH
- [STC SA04348CH](https://openairdocs.org/stc/SA04348CH): Installation of Parker Hannifin Corporation, Aircraft Wheel & Brake Division, Wheel and Brake Conversion Kit, part number 199- 283. Kaman Corporation Aircraft Wheel and Brake LLC
- [STC SA02203AK](https://openairdocs.org/stc/SA02203AK): Installation of FlightLogic Synthetic Vision Electronic Flight Information System (EFIS-SV). Genesys Aerosystems Inc
- [STC SA11299DS](https://openairdocs.org/stc/SA11299DS): An update to the exisiting Collins Aerospace Integrated Flight Information System (IFIS) FSU-5010 and upgrade the existing XMWR-1000 to a XMWR-1000S (Sirius XM) in Part 23 aircraf. BHE & Associates LTD
- [STC SA02254AK](https://openairdocs.org/stc/SA02254AK): Installation of "Single Screen", "2 or 3 Screen", "Dual Screen", or "4 or 6 screen". Genesys Aerosystems Inc
- [STC SA02444AK](https://openairdocs.org/stc/SA02444AK): Approval of the L-3 Communications NGT 9000/9000R ADS-B system installed. ADS-B Technologies LLC
- [STC SA09856AC](https://openairdocs.org/stc/SA09856AC): Installation of BendixKing Aerowave 100 In-flight Data Link System for non-essential, non-required aircraft Cabin Systems & Equipments. Honeywell International Inc (Bendix King)
- [STC SA11174SC PAGE 1](https://openairdocs.org/stc/SA11174SC%20PAGE%201): Installation of BendixKing by Honeywell KSN 770 and KSN 765 WAAS LPV approach capable nav/comm systems. Honeywell International Inc (Bendix King)
- [STC SA02075SE](https://openairdocs.org/stc/SA02075SE): Installation of a Mid-Continent MD835( ) Lithium Ion Battery. Mid-Continent Instrument Co. Inc
- [STC SA04199NY](https://openairdocs.org/stc/SA04199NY): Installation of Becker Avionics DVCS6500 Digital Voice Communication System. Becker Avionics Inc
- [STC SA10236SC](https://openairdocs.org/stc/SA10236SC): Installation of a GDC 31 Roll Steering Converter. DAC International Inc
- [STC SA01714WI](https://openairdocs.org/stc/SA01714WI): Installation of a Garmin transponders: (a) GTX 330/330D/33/33D with ADS-B Out functionality; (b) GTX 335/335R/345/345R with ADS-B Out and In functionality; or (c) GTX 335R/345R with ADS-B Out functionality in select airplanes installed with G950/G1000 systems. Garmin International Inc
- [STC SA04336NY](https://openairdocs.org/stc/SA04336NY): Installation of Rockwell Collins TDR-94D Transponder Upgrade-ADS-B Out. Mid Canada Mod Center
- [STC SA03345CH](https://openairdocs.org/stc/SA03345CH): Install air ambulance conversion. Spectrum Aeromed LLC dba Spectrum Aeromed
- [STC SA02878CH](https://openairdocs.org/stc/SA02878CH): Install Air Ambulance conversion. Paul/ Lanna Egan LLC
- [STC SA04165NY](https://openairdocs.org/stc/SA04165NY): Installation of Latitude Technologies Skynode S200 Satcom system must be performed. Latitude Technologies Corporation
- [STC SA02153LA-D PAGE 1](https://openairdocs.org/stc/SA02153LA-D%20PAGE%201): Installation of Garmin G600 Primary Flight Display (PFD) and Multifunction Display (MFD) System. Garmin International Inc
- [STC SA01877WI](https://openairdocs.org/stc/SA01877WI): Installation of ADS-B Out. Intercontinental Jet Service Corporation
- [STC SA02013CH](https://openairdocs.org/stc/SA02013CH): Installation of Avidyne Corporation Traffic Advisory System (TAS). Avidyne Corporation
- [STC SA01684WI](https://openairdocs.org/stc/SA01684WI): Installation of Rockwell Collins, Inc. Aircraft Information Management (AIM) System. Rockwell Collins Inc
- [STC SA01933LA-D](https://openairdocs.org/stc/SA01933LA-D): Installation of Garmin Model 400W / 500W Series GPS-WAAS Navigation System. Garmin International Inc
- [STC SA00343BO](https://openairdocs.org/stc/SA00343BO): Installation of a single configuration or a dual configuration Avidyne Corporation Integrated Flight Display, Model IFD540 loaded with Release 10.0 software (or later FAA approved release). Avidyne Corporation
- [STC SA00352BO PAGE 1](https://openairdocs.org/stc/SA00352BO%20PAGE%201): Installation of an Avidyne Corporation Mode A/C/S Transponder with ADS-B Out capability, Model AXP340 loaded with Version 3.13 software (or later FAA approved version),. Avidyne Corporation
- [STC SA1644GL](https://openairdocs.org/stc/SA1644GL): Install Egan Aviation Air Ambulance Stretcher P/N 125 using Installation Kit P/N 805. Paul/ Lanna Egan LLC
- [STC SA01806WI](https://openairdocs.org/stc/SA01806WI): Modification of Rockwell Collins TCAS II System Installation with DC powered TCAS Transmitter Receiver Processor. Rockwell Collins Inc
- [STC SA02119SE PAGE 2](https://openairdocs.org/stc/SA02119SE%20PAGE%202): Installation of Garmin GDL 88 ADS-B UAT Transceiver System. Garmin International Inc
- [STC SA01969SE](https://openairdocs.org/stc/SA01969SE): Installation of a Mid-Continent MD302 Standby Attitude Module. Mid-Continent Instruments and Avionics
- [STC SA01229SE PAGE 1](https://openairdocs.org/stc/SA01229SE%20PAGE%201): Installation of GNS 480 (CNX80) GPS WAAS Navigator with integrated VHF Navigation and Communication radios. Garmin International Inc
- [STC SA02442AK PAGE 2](https://openairdocs.org/stc/SA02442AK%20PAGE%202): Approval of the L-3 Communications NGT 2000/2500 ADS-B system. ADS-B Technologies, LLC
- [STC SA01933LA-D PAGE 1](https://openairdocs.org/stc/SA01933LA-D%20PAGE%201): Installation of Garmin Model 400W / 500W Series GPS-WAAS Navigation System. Garmin International Inc
- [STC SA02121SE](https://openairdocs.org/stc/SA02121SE): Installation of Garmin GTS 825 (TAS) or GTS 855 (TCAS I) Traffic System. Garmin International Inc
- [STC SA00269BO](https://openairdocs.org/stc/SA00269BO): Installation of Avidyne Corporation TWX 670 Tactical Weather Detection System P/N 850-00026-000-( ) consisting of Avidyne Processor P/N 700-00033-000-( ), Sensor Systems Inc. Antenna P/N S72-1715-1 with doubler plate P/N S72-171530-1, and Avidyne Mounting Tray P/N 700-00034-000. Avidyne Corporation
- [STC SA02717NY PAGE 2](https://openairdocs.org/stc/SA02717NY%20PAGE%202): Installation of VoiceFlight Systems LLC VFS101 Speech Recognition Module. VoiceFlight Systems LLC
- [STC SA01430WI-D](https://openairdocs.org/stc/SA01430WI-D): Modification of a Rockwell Collins, Inc. Data Base Unit (DBU). Rockwell Collins Inc
- [STC SA10950SC](https://openairdocs.org/stc/SA10950SC): Installation of a 4 place Passenger Seating Arrangement. Piaggio America Inc
- [STC SA01434WI-D](https://openairdocs.org/stc/SA01434WI-D): Modification of a Rockwell Collins, Inc. Global Positioning System (GPS) installation. Rockwell Collins Inc
- [STC SA01692SE](https://openairdocs.org/stc/SA01692SE): Installation of a Garmin GMX 200 Multi-Function Display. Garmin International Inc
- [STC SA03148NY](https://openairdocs.org/stc/SA03148NY): The installation of the Latitude Technologies Corporation S100 Tracking System. Latitude Technologies Corporation
- [STC SA01676WI](https://openairdocs.org/stc/SA01676WI): Modification of a Rockwell Collins, Inc. File Server Unit (FSU). Rockwell Collins Inc
- [STC SA00674WI-D](https://openairdocs.org/stc/SA00674WI-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 158: https://openairdocs.org/aircraft/N180AV/stcs.md

## Related

- Other Piaggio P180 aircraft: https://openairdocs.org/model/piaggio-p180/aircraft.md
- The Pratt & Whitney PT6A series engine: https://openairdocs.org/engine/pratt-whitney-pt6a-series.md

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