# N161CA: Diamond Aircraft Ind DA20-C1

- Status: Valid registration
- Airframe: [Diamond Aircraft Ind DA20-C1](https://openairdocs.org/model/diamond-aircraft-ind-da20-c1) (registry code 2990001, 2 seats)
- Engine: [Continental IO-240-B](https://openairdocs.org/engine/continental-io-240-b) (registry code 17177)
- Data sheets: [TCDS TA4CH](https://openairdocs.org/tcds/TA4CH) (Diamond Aircraft Industries Inc.), [TCDS E7SO](https://openairdocs.org/tcds/E7SO) (Continental Aerospace Technologies, Inc.) (OpenAirDocs)
- Serial number: C0372
- Type: Fixed wing single engine
- Engine type: Reciprocating
- Airworthiness: Standard, utility
- Airworthiness date: June 5, 2006
- Certificate issued: August 20, 2024
- Expires: August 31, 2031
- Mode S code: A0F598
- Registered owner: [Aerodynamic LLC](https://openairdocs.org/faa-owner/AERODYNAMIC%20LLC)
- Location: [Aurora, OR](https://openairdocs.org/faa-place/OR/Aurora)
- Owner type: LLC
- Owner's area on the map: 45.2403° N, 122.7936° W: Placed by OpenAirDocs at the center of ZIP code 97002, within about 4 miles (OpenAirDocs). The owner's mailing address, not where the aircraft is based
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=161CA
- Page: https://openairdocs.org/aircraft/N161CA

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): 5 in force

### Matched by airframe (Diamond Aircraft Ind DA20-C1)

- [AD 2026-15-18](https://openairdocs.org/ad/2026-15-18): Emergency Locator Beacon · Diamond Aircraft Industries DA20-C1. Effective Sep 8, 2026
- [AD 2022-03-15](https://openairdocs.org/ad/2022-03-15): Fuel Quantity Indicator · Garmin G3X Touch Electronic Flight Instrument System (STC SA01899WI or SA02658SE). Effective Mar 21, 2022
- [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

### Matched by engine (Continental IO-240-B)

- [AD 2012-03-06](https://openairdocs.org/ad/2012-03-06): Fuel servo diaphragm · Continental Motors 6-260-A, 6-285-A, 6-285-B and 482 more. Effective Feb 24, 2012
- [AD 2010-11-04](https://openairdocs.org/ad/2010-11-04): Hydraulic lifters · Continental Motors FSO-470-A, GIO-470-A, GTSIO-520-C and 190 more. Effective Jun 16, 2010

### Historical (superseded or no longer in force)

- [AD 2009-24-51](https://openairdocs.org/ad/2009-24-51) (historical): Hydraulic lifters · Teledyne Continental Motors FSO-470-A, GIO-470-A, GTSIO-520-C and 156 more

## Information bulletins (advisory) (8 in force)

- [SAIB SW-18-31](https://openairdocs.org/saib/SW-18-31): NAVIGATION, ATTITUDE, AND DIRECTION DATA SYSTEM. Issued Nov 21, 2018
- [SAIB CE-12-09](https://openairdocs.org/saib/CE-12-09): Landing Gear, Nose: Diamond DA20 Nose Landing Fork Assembly. Issued Dec 22, 2011
- [SAIB NE-16-13](https://openairdocs.org/saib/NE-16-13): Powerplant - Prohibited use of sealant. Issued Mar 8, 2016
- [SAIB NE-13-15](https://openairdocs.org/saib/NE-13-15): Engine Controls: Continental Motors, Inc. (CMI) Throttle and Mixture Control Levers. Issued Feb 8, 2013
- [SAIB NE-13-04](https://openairdocs.org/saib/NE-13-04): Continental Motors, Inc. (CMI) Connecting Rod Piston Pin Bushing Inspection. Issued Oct 31, 2012
- [SAIB NE-10-09](https://openairdocs.org/saib/NE-10-09): Reciprocating Engine Power Section: Hydraulic Valve Lifters. Issued Nov 20, 2009
- [SAIB NE-05-38](https://openairdocs.org/saib/NE-05-38): . Issued Mar 18, 2005
- [SAIB CE-98-21R1](https://openairdocs.org/saib/CE-98-21R1): . Issued Jun 10, 1998

## NTSB investigations

None matched to N161CA.

## FAA accident and incident reports

None matched to N161CA.

## 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 2010FA0001049](https://openairdocs.org/sdr/2010FA0001049), Sep 21, 2010: DATA CARD. FAILED. GPS IFR DATA CARD FAILED IN FLIGHT. THE G430 USES A DATA CARD REFRESHED BY THE OPERATOR EVERY 28 DAYS. THE GPS UNIT ACCESSES THE CARD CONTINUOUSLY. IF THE CARD 

## Service difficulty reports on N161CA not matched to an aircraft (43)

They name N161CA, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft.

- [SDR SWIA200110197](https://openairdocs.org/sdr/SWIA200110197), Sep 19, 2001: CONTROL ARM. MALFUNCTIONED. NOSE WHEEL STEERING PULLS LEFT WITH OR WITHOUT TILLER ENGAGED. ABORTED TAKEOFF BELOW 80 KNOTS. CENTERED FEEDBACK POT AND REPLACED NOSE WHEEL STEERING TILLER. OP
- [SDR SWIA200110148](https://openairdocs.org/sdr/SWIA200110148), Sep 2, 2001: SELECTOR SWITCH. MALFUNCTIONED. ON TAXI CHECK, WHEN FLAPS 15 DEGREES WERE SELECTED THE MAP LIGHT ''FLAPS'' AND ''ADV SWS'' ILLUMINATED WITH AN ASSOCIATED CONTROL FAULT ON FLAP WARNING PANEL WI
- [SDR SWIA972627](https://openairdocs.org/sdr/SWIA972627), Jun 11, 2001: BOOT. DAMAGED. DURING FLIGHT IN ICING CONDITIONS RIGHT OUTBOARD DEICE BOOT FAILED TO INFLATE AFTER ASSOCIATED INOP LIGHT. INSTALLED BOOT PATCH ON RIGHT OUTBOARD WING IAW BF 74
- [SDR SWIA972593](https://openairdocs.org/sdr/SWIA972593), May 22, 2001: STRAP. BROKEN. AFTER TAKEOFF AND GEAR SELECTED UP, HAD A HIGH FREQUENCY THUMPING NOISE. RETURNED TO SFO. WHEN SELECTED GEAR DOWN NOISE WENT AWAY. FOUND NOSE LANDING GEAR STRUT
- [SDR SWIA971994](https://openairdocs.org/sdr/SWIA971994), Sep 26, 2000: INDICATOR. MALFUNCTIONED. IN CRUISE FLIGHT, BOTH SYSTEM A LIGHTS (GREEN AND RED) FOR NOSE GEAR ILLUMINATED. GEAR CYCLE ATTEMPTED, ALL RED LIGHTS ILLUMINATED EXCEPT RED NOSE A DISAGREEMEN
- [SDR SWIA971913](https://openairdocs.org/sdr/SWIA971913), Aug 5, 2000: WIRE. BROKEN. BONDING STRAP LOOSE AFTER TAKEOFF. RETURNED TO PDX. REPLACED BROKEN BOND WIRE PER WIRE MANUAL 20-30-00.
- [SDR SWIA971830](https://openairdocs.org/sdr/SWIA971830), Jun 22, 2000: CONTROLLER. MALFUNCTIONED. AIRCRAFT CONDITIONED TO PITCH UP WITH AUTOPILOT OFF PULLED DISCONNECT TO CONTROL AIRCRAFT TROUBLESHOT AUTO PILOT AND TRIM SYSTEM FOUND BAD APP 65A. REMOVED AND 
- [SDR SWIA971730](https://openairdocs.org/sdr/SWIA971730), Mar 8, 2000: BOOT. FAILED. AFTER DEPARTURE MIDDLE LEFT WING DEICE BOOT FAILED TWICE. RETURNED TO SFO. OPERATED LEADING EDGE DEICE THROUGH SEVERAL CYCLES, COULD NOT DUPLICATE PROBLEM. SWAP
- [SDR SWIA971602](https://openairdocs.org/sdr/SWIA971602), Nov 17, 1999: SENSOR. FAILED. AFTER TAKEOFF, CYCLED GEAR AND IT DID NOT RETRACT. CYCLED GEAR 4 TIMES AND IT STILL DID NOT WORK. RETURNED TO SEA. INSTALLED NEW LEFT MAIN GEAR A UPLOCK SENSOR 
- [SDR SWIA971309](https://openairdocs.org/sdr/SWIA971309), Nov 10, 1998: DE-ICE BOOT. FAILED. LEFT OUTBOARD AND RIGHT OUTBOARD WINGS DEICE BOOTS FAILED. RETURNED TO FAT. REPLACED OUTBOARD WING EJECTOR FLOW CONTROL VALVE, OPS CHECKS GOOD.
- [SDR COMA9810070](https://openairdocs.org/sdr/COMA9810070), Mar 18, 1998: TQ SIGNAL COND. MALFUNCTION. AUTO FEATHER SYSTEM DOES NOT TEST. REPLACED THE LEFT ENGINE TORQUE SIGNAL CONDITIONER.
- [SDR COMA9710501](https://openairdocs.org/sdr/COMA9710501), Dec 21, 1997: ANNUNCIATOR PNL. MALFUNCTION. FLAP CONTROL FAULT, ASYMMETRY AND DISAGREEEMENT WARNINGS. REPLACED THE FLAP ANNUNCIATOR PANEL.
- [SDR COMA9710438](https://openairdocs.org/sdr/COMA9710438), Oct 24, 1997: ACTUATOR. MALFUNCTIONED. FLAP DISAGREEMENT WARNING AFTER TAKEOFF. COULD NOT DUPLICATE DISCREPANCY. REPLACED RIGHT HAND OUTBOARD FLAP ACTUATOR FOR TROUBLESHOOTING.
- [SDR COMA9710437](https://openairdocs.org/sdr/COMA9710437), Oct 22, 1997: FLAP CONTROL. MALFUNCTION. FLAP DISAGREEMENT WARNING AFTER TAKEOFF. REPLACED THE FLAP CONTROL UNIT.
- [SDR COMA9710345](https://openairdocs.org/sdr/COMA9710345), Jul 31, 1997: ELECTRIC LATCH. SHORTED. WHILE PERFORMING A C-1 CHECK ZONE 200 TASK NR 35-09 (VERIFY LATCH MECHANISM) IT WAS DISCOVERED THAT THE CIRCUIT BREAKER CB0067 WAS POPPING. UPON FURTHER INVESTI
- [SDR COMA9710338](https://openairdocs.org/sdr/COMA9710338), Jul 31, 1997: SOLENOID. FAILED. UPON COMPLIANCE OF C TASK 35-09, THE PAX OXYGEN MASK IN THE LAVATORY FAILED TO DROP. INVESTIGATION FOUND THE OXYGEN MASK DOOR LATCH SOLENOID FAILED. THE SOLENOI
- [SDR COMA9710192](https://openairdocs.org/sdr/COMA9710192), Mar 27, 1997: WIRE. LOOSE. TAKEOFF TRIM WARNING DURING TAKEOFF ROLL. REPAIRED LOOSE WIRING AT THE ELEVATOR TRIM TAB PROXIMITY SENSORS.
- [SDR COMA9710130](https://openairdocs.org/sdr/COMA9710130), Feb 11, 1997: PROX SENSOR. FAILED. NOSE WHEEL STEERING INOP DURING LANDING. REPLACED THE RT MLG WEIGHT ON WHEELS PROXIMITY SENSOR.
- [SDR COMA9710124](https://openairdocs.org/sdr/COMA9710124), Feb 8, 1997: ACTUATOR. MALFUNCTION. FLAP CONTROL FAULT WARNING DURING TAXI. REPLACED THE RT OUTBOARD FLAP ACTUATOR.
- [SDR COMA9710104](https://openairdocs.org/sdr/COMA9710104), Feb 2, 1997: FCU. MALFUNCTION. FLAP CONTROL FAULT WARNING DURING TAXI. REPLACED THE FLAP CONTROL UNIT.
- [SDR COMA9710040](https://openairdocs.org/sdr/COMA9710040), Jan 19, 1997: ROLLER. INOPERATIVE. FLAP DISAGREEMENT AFTER TAKEOFF. REPLACED LEFT OUTBOARD FLAP ROLLERS.
- [SDR COMA9610424](https://openairdocs.org/sdr/COMA9610424), Dec 24, 1996: WARNING. ACTIVATED. CARGO DOOR WARNING DURING TAKEOFF. FOUND TO BE FALSE WARNING. WARNING SYSTEM PLACED ON DEFERRED MAINTENANCE LIST.
- [SDR COMA9610392](https://openairdocs.org/sdr/COMA9610392), Dec 12, 1996: SWITCHES. OUT OF ADJUST. CARGO DOOR WARNING DURING TAKEOFF. ADJUSTED DOOR MICRO SWITCHES.
- [SDR COMA9610304](https://openairdocs.org/sdr/COMA9610304), Oct 12, 1996: LATCH. BROKEN. LT MLG FORWARD DOOR LATCH IS BROKEN, DOOR HANGS OPEN. REPLACED THE DOOR LATCH ASSY.
- [SDR COMA9610295](https://openairdocs.org/sdr/COMA9610295), Oct 7, 1996: ACTUATOR. LEAKING. RT ENGINE NACELLE, WING AND PROPELLER ARE COVERED WITH OIL. REPLACED THE PROPELLER ACTUATOR ASSY.
- [SDR COMA9610221](https://openairdocs.org/sdr/COMA9610221), Jul 8, 1996: SEALS. LEAKING. THE GROUND FEATHER TEST REQUIRED 11 SECONDS FOR PROP TO TRANSITION FROM FEATHER TO BETA RANGE. REPLACED THE LT PROPELLER TRANSFER TUBE OIL SEALS.
- [SDR COMA9610219](https://openairdocs.org/sdr/COMA9610219), Jul 3, 1996: ACTUATOR. MALFUNCTION. FLAP CONTROL FAULT WARNING DURING TAKEOFF ROLL. REPLACED THE RT INBD FLAP ACTUATOR.
- [SDR COMA9610199](https://openairdocs.org/sdr/COMA9610199), Jun 27, 1996: FLAP CONTL UNIT. MALFUNCTION. FLAP CONTROL FAULT WARNING DURING TAKEOFF. REPLACED THE FLAP CONTROL UNIT. PART TOTAL CYCLES, 8,211.
- [SDR COMA9610152](https://openairdocs.org/sdr/COMA9610152), May 17, 1996: SKIN. LIGHTNING STRIKE. DURING A LIGHTNING STRIKE INSPECTION FOUND RIGHT ELEVATOR TRAILING EDGE TO HAVE DAMAGE AT THE OUTBOARD TIP. CUT OUT THE DAMAGED AREA OF THE RIGHT ELEVATOR TRAIL
- [SDR COMA9610146](https://openairdocs.org/sdr/COMA9610146), May 14, 1996: BATTERY. DISCHARGED. EMERGENCY LIGHTING SYSTEM IS INOP. REPLACED THE EMERGENCY LIGHTS BATTERIES.
- [SDR COMA9610128](https://openairdocs.org/sdr/COMA9610128), Apr 12, 1996: ROLLERS. WORN. AFTER LANDING, OUTBD FLAPS WOULD NOT RETRACT FULLY. REPLACED THE LT OUTBD FLAP ROLLERS.
- [SDR COMA9610121](https://openairdocs.org/sdr/COMA9610121), Apr 1, 1996: SENSOR. FAILED. BURNING ELECTRICAL SMELL NOTED IN COCKPIT WHEN WINDSHIELD HEAT SELECTED ON. REPLACED THE LT WINDSHIELD CURRENT SENSOR.
- [SDR COMA9610090](https://openairdocs.org/sdr/COMA9610090), Feb 24, 1996: WARNING LIGHT. ILLUMINATED. SERVICE DOOR WARNING LIGHT ILLUMINATED DURING TAKEOFF. ALL DOORS CONFIRMED CLOSED, COULD NOT DUPLICATE DISCREPANCY. ALL DOORS INSPECTED FOR SECURITY AND FUNCTIO
- [SDR COMA9610063](https://openairdocs.org/sdr/COMA9610063), Feb 6, 1996: BRACKET. CRACKED. THE LEFT AILERON WAS STRUCK BY A GROUND VEHICLE. NO DAMAGE WAS FOUND ON THE AILERON. HOWEVER, THE BRACKET ON THE WING REAR SPAR, THAT THE AILERON SERVO TAB RODS
- [SDR COMA9610021](https://openairdocs.org/sdr/COMA9610021), Jan 15, 1996: CIRCUIT BREAKER. TRIPPED. TAKEOFF TRIM WARNING DURING TAKEOFF ROLL. FOUND THE AURAL WARNING CIRCUIT BREAKER TRIPPED. RESET BREAKER AND ACFT CONTINUED SERVICE.
- [SDR COMA9512011](https://openairdocs.org/sdr/COMA9512011), Nov 18, 1995: PCU. DEFECTIVE. LEFT PROPELLER BETA INDICATOR IS FLASHING ON AND OFF AND PROP IS LURCHING. REPLACED THE PROPELLER PITCH CONTROL UNIT.
- [SDR COMA9511986](https://openairdocs.org/sdr/COMA9511986), Oct 12, 1995: ENGINE. FAILED. THE LEFT ENGINE NH AND OIL PRESSURE DROPPED TO ZERO DURING FLIGHT. INFLIGHT SHUTDOWN PERFORMED AND DIVERTED TO MCO. REPLACED THE LEFT ENGINE ASSEMBLY.
- [SDR COMA9511978](https://openairdocs.org/sdr/COMA9511978), Sep 28, 1995: BRACKET. CRACKED. RT OUTBOARD FLAP MOVABLE PANEL, ROLLER SUPPORT BRACKET IS CRACKED. REPLACED CRACKED SUPPORT BRACKET.
- [SDR COM11896](https://openairdocs.org/sdr/COM11896), May 22, 1995: SUPPORT. CRACKED. THE FOLLOWING P/N WING SKIN SUPPORTS WERE FOUND CRACKED DURING INSPECTION TASK 5720-552/652-01I AND 5720-551/651-01I. THE SKIN SUPPORTS WERE REPAIRED IAW AERO D
- [SDR COM11882](https://openairdocs.org/sdr/COM11882), May 8, 1995: FDU 70. DEFECTIVE. YELLOW HEADING FLAP ON COPILOT'S EHSI, RED OFF FLAG ON PILOT'S RMI. REPLACED THE NR 2 FDU-70.
- [SDR COM11836](https://openairdocs.org/sdr/COM11836), Mar 24, 1995: SWITCH. DEFECTIVE. AFTER TAKEOFF THE LANDING GEAR CONTROL HANDLE COULD NOT BE MOVED TO RETRACT THE GEAR. REPLACED NLG PROXIMITY WOW SWITCH AND HARNESS ASSY.
- [SDR COM11767](https://openairdocs.org/sdr/COM11767), Feb 6, 1995: ACTUATOR. DEFECTIVE. OUTBD FLAP ASYMMETRY WARNING AFTER LANDING. REPLACED LT OUTBD FLAP ACTUATOR.
- [SDR COM11728](https://openairdocs.org/sdr/COM11728), Jan 10, 1995: FRAME. CRACKED. DURING INSPECTION FOUND THE FRAME 10 WEB IN LEFT NACELLE INBOARD SIDE TO HAVE AN APPROX .625 INCH CRACK RUNNING THROUGH THE FRAME FLANGE RADIUS JUST UNDER THE C

## STCs that may be installed (OpenAirDocs) (89, 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 (Diamond Aircraft Ind DA20-C1)

- [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 SA01800SE](https://openairdocs.org/stc/SA01800SE): Fabrication and installation of new or replacement of existing instrument panel lights dimmer control. TCW Technologies, LLC
- [STC SA01861SE](https://openairdocs.org/stc/SA01861SE): Fabrication and installation of Landing Light Controller. TCW Technologies, LLC
- [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 SA12406WI](https://openairdocs.org/stc/SA12406WI): Installation of a Garmin AXIS Flight Display System. Garmin International Inc
- [STC SA02636SE](https://openairdocs.org/stc/SA02636SE): Installation of Garmin GPS 175 Navigation System and GNX 375 Navigation System with ADS-B In/Out Transponder. Garmin International Inc
- [STC SA02019SE-D](https://openairdocs.org/stc/SA02019SE-D): Installation of Garmin Model GTN 625/635/650; 725/750 Navigation System. Garmin International Inc
- [STC SA00079NY](https://openairdocs.org/stc/SA00079NY): Installation of Airwolf remote mounted engine oil filter kit AFC-K008 on single and multi engine fixed wing light aircraft incorporating Teledyne Continental reciprocating engines of 450 horsepower or less. Airwolf Filter Corporation
- [STC SA02738CH](https://openairdocs.org/stc/SA02738CH): Installation of L-3 Communications Avionics Systems. Acron Aviation Inc
- [STC SA04046CH PAGE 1](https://openairdocs.org/stc/SA04046CH%20PAGE%201): Installation of L-3 GENESIS (TM) Electronic Standby Instrument System (ESI-500/MAG-500). Acron Aviation Inc
- [STC SA04378CH](https://openairdocs.org/stc/SA04378CH): Installation of an engine modified per STC SE04349CH. SureFly Partners Ltd
- [STC SA02658SE](https://openairdocs.org/stc/SA02658SE): Installation of Garmin GI 275 Multi-Function Display System. Garmin International Inc
- [STC SA01899WI](https://openairdocs.org/stc/SA01899WI): Installation of Garmin G3X Touch Electronic Flight Instrument System. Garmin International Inc
- [STC SA02019WI](https://openairdocs.org/stc/SA02019WI): Installation of the Trig Avionics TX56, TX56A, TX57, or TX57A VHF Nav-Com Radio. Peregrine
- [STC SA02987CH](https://openairdocs.org/stc/SA02987CH): Installation of the Electroair Electronic Ignition System. Electroair Acquisition Corporation
- [STC SA01967WI](https://openairdocs.org/stc/SA01967WI): Use of GAMI G100UL High Octane Unleaded Avgas. General Aviation Modifications 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 SA01818WI](https://openairdocs.org/stc/SA01818WI): Installation of Garmin G5 Electronic Flight Instrument. Garmin International Inc
- [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 SA10822SC](https://openairdocs.org/stc/SA10822SC): Installation of EFD1000 Primary Flight Display. Aspen Avionics Inc
- [STC SA00401BO](https://openairdocs.org/stc/SA00401BO): Installation of a SkyTrax100B UAT receiver. Avidyne Corporation
- [STC SA00410BO](https://openairdocs.org/stc/SA00410BO): Installation of an AV-30-C Multi-Mode Indicator. uAvionix Corporation
- [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 SA04032CH](https://openairdocs.org/stc/SA04032CH): Install rocker switch assemblies. Electroair Acquisition Corporation
- [STC SA00344BO PAGE 1](https://openairdocs.org/stc/SA00344BO%20PAGE%201): Installation of Parmetheus Plus LED PAR36 and PAR46 taxi and landing lights. Whelen Aerospace Technologies
- [STC SA00744DE](https://openairdocs.org/stc/SA00744DE): Installation of the Automatic Dependent Surveillance Broadcast (ADS-B) Out Equipment using a Trig Avionics TT31 Transponder and an approved position sensor. Peregrine
- [STC SA00765DE](https://openairdocs.org/stc/SA00765DE): Installation of Automatic Dependent Surveillance Broadcast (ADS-B) Out functionality using the BendixKing KT74 Transponder and qualified position sensor. Peregrine
- [STC SA04112CH](https://openairdocs.org/stc/SA04112CH): Installation of Appareo Systems, LLC Stratus ESG ADS-B transponder. Appareo Systems 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 SA02013CH](https://openairdocs.org/stc/SA02013CH): Installation of Avidyne Corporation Traffic Advisory System (TAS). Avidyne Corporation
- [STC SA01835WI](https://openairdocs.org/stc/SA01835WI): Installation of Trig Avionics TY-96 or TY-97 VHF Communications Radio. Peregrine
- [STC SA01933LA-D](https://openairdocs.org/stc/SA01933LA-D): Installation of Garmin Model 400W / 500W Series GPS-WAAS Navigation System. Garmin International Inc
- [STC SA02212AK](https://openairdocs.org/stc/SA02212AK): Replacement of existing landing and/or taxi light reflector and bulbs with high intensity discharge (HID) lighting systems. Seaplanes North LLC
- [STC SA2586NM](https://openairdocs.org/stc/SA2586NM): Installation of J.P. Instruments temperature monitoring systems. J P Instruments
- [STC SA02428SE](https://openairdocs.org/stc/SA02428SE): Installation of an Air Stream Switch for an electric time recording device on non-pressurized aircraft. Henry F Rogers/David E Polley
- [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 SA11172SC](https://openairdocs.org/stc/SA11172SC): Installation of an ADS600-B Automatic Dependent Surveillance-Broadcast (ADS-B) Universal Access Transceiver (UAT) and Global Positioning System (GPS) antenna. NavWorx Inc
- [STC SA02119SE PAGE 1](https://openairdocs.org/stc/SA02119SE%20PAGE%201): Installation of Garmin GDL 88 ADS-B UAT Transceiver System. Garmin International Inc
- [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 1](https://openairdocs.org/stc/SA02442AK%20PAGE%201): 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 SA02930NY](https://openairdocs.org/stc/SA02930NY): Installation of Insight Instrument Corporation Graphic Engine Monitor (GEM 610C) models G3, G2, and G1 and 1200C model G4 as primary Cylinder Head Temperature (CHT), Exhaust Gas Temperature (EGT), and Turbine Inlet Temperature (TIT) Instruments. Insight Instrument Corporation
- [STC SA02283SE PAGE 1](https://openairdocs.org/stc/SA02283SE%20PAGE%201): Installation of Electronics International Inc. Glass Panel Engine Monitor (with In Flight Data) CGR-30P. Electronics International Inc
- [STC SA02402SE PAGE 1](https://openairdocs.org/stc/SA02402SE%20PAGE%201): Installation of Electronics International Inc. Glass Panel Engine Monitor (with In-Flight Data) CGR-30C. Electronics 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 1](https://openairdocs.org/stc/SA02717NY%20PAGE%201): Installation of VoiceFlight Systems LLC VFS101 Speech Recognition Module. VoiceFlight Systems LLC

All 89: https://openairdocs.org/aircraft/N161CA/stcs.md

## Related

- Other Diamond Aircraft Ind DA20-C1 aircraft: https://openairdocs.org/model/diamond-aircraft-ind-da20-c1/aircraft.md
- The Continental IO-240-B engine: https://openairdocs.org/engine/continental-io-240-b.md

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