# N148AS: 2025 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: C0782 - Year built: 2025 - Type: Fixed wing single engine - Engine type: Reciprocating - Airworthiness: Standard, utility - Airworthiness date: April 29, 2025 - Certificate issued: August 5, 2025 - Expires: August 31, 2032 - Mode S code: A0C079 - Registered owner: [Skyline Aviation Inc](https://openairdocs.org/faa-owner/SKYLINE%20AVIATION%20INC) - Location: [San Angelo, TX](https://openairdocs.org/faa-place/TX/San%20Angelo) - Owner type: Corporation - Owner's area on the map: 31.2870° N, 100.4236° W: Placed by OpenAirDocs at the center of ZIP code 76904, within about 12 miles (OpenAirDocs). The owner's mailing address, not where the aircraft is based - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=148AS - Page: https://openairdocs.org/aircraft/N148AS From the FAA registry file of October 22, 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 N148AS. ## FAA accident and incident reports None matched to N148AS. ## 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 N148AS not matched to an aircraft (29) They name N148AS, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft. - [SDR BJNA201604200001](https://openairdocs.org/sdr/BJNA201604200001), Apr 11, 2016: SKIN. CRACKED. LEFT ELEVATOR HAS A 1.0" CRACK ON THE LOWER SURFACE AT BS 154, WL 260. REMOVED DAMAGE IAW CIN-16-0012-016, ACCOMPLISHED BOND TEST IAW NDT PART 4, PROCEDURE 1, N - [SDR BJNA2016040006](https://openairdocs.org/sdr/BJNA2016040006), Apr 4, 2016: SKIN. PUNCTURED. LEFT ELEVATOR HAS PUNCTURE OF 0.490 ON UPPER SURFACE AT ELEVATOR BS 109, WL 264. REMOVED DAMAGE ON LT ELEVATOR AND PREPPED FOR LAYUP IAW SRM 51-70-17, MATERIAL - [SDR BJNA201604190002](https://openairdocs.org/sdr/BJNA201604190002), Apr 4, 2016: FRAME. CRACKED. ELECTRONIC ENGINE COMPARTMENT LOWER FRAME, AT BS 312, RBL 32, WATERLINE 199. HAS A 0.50" CRACKED. REMOVED ALL FASTENERS COMMON TO CRACK IAW SRM 51-40-02, AND SR - [SDR BJNA201604250007](https://openairdocs.org/sdr/BJNA201604250007), Apr 3, 2016: SKIN. CRACKED. FUSELAGE SKIN AT BS 951, RBL 45, WL 260, THERE IS A 1.00" CRACK AFT GALLEY DOOR UPPER HINGE CUTOUT. REMOVED WEB FORWARD OF GALLEY DOOR, IAW SRM 51-40-02. REMOVE - [SDR BJNA201604190003](https://openairdocs.org/sdr/BJNA201604190003), Apr 3, 2016: SKIN. CRACKED. DURING SB 737-53-1287-01, TWO CRACKS WERE FOUND AT BS 727D, LBL 1 - RBL 1, WL 148.5. LBL CRACK IS 1.13 INCHES & RBL CRACK IS 1.42. HF ANTENNA AND HARDWARE WERE - [SDR BJNA201604250005](https://openairdocs.org/sdr/BJNA201604250005), Apr 2, 2016: FRAME. CRACKED. ELECTRONIC EQUIPMENT COMPARTMENT AT BS 312, LBL 12, WL 199, THERE IS A CRACK 0.750 IN THE FRAME STRAP. REMOVED ALL FASTENERS COMMON TO THE STRAP IAW SRM 51-40-0 - [SDR BJNA20151125001](https://openairdocs.org/sdr/BJNA20151125001), Nov 22, 2015: WINDOW. CRACKED. ENROUTE, ON CLIMBOUT- APPROXIMATELY FL220, F/O'S WINDOW CRACKED, SHATTERED. OPS IAW QRH, OK TO CONTINUE LAND W/NO FUTURE ISSUE. REMOVED NR 1 WINDOW IAW AMM 56-1 - [SDR BJNA20151006001](https://openairdocs.org/sdr/BJNA20151006001), Oct 5, 2015: LAMP. INOPERATIVE. THE R2 DOOR EXTERIOR EMERGENCY LIGHT WILL NOT ILLUMINATE. REPLACED THE LAMP IAW 33-51-31. - [SDR BJNA2015FA0000084](https://openairdocs.org/sdr/BJNA2015FA0000084), Feb 20, 2015: SKIN. DENTED. FOUND DAMAGE TO FUSELAGE SKIN FORWARD OF THE FWD LWR CARGO DOOR BELOW SKIN SPLICE. - [SDR FOTR20140829020](https://openairdocs.org/sdr/FOTR20140829020), Aug 26, 2014: CHANNEL. CORRODED. AFT CARGO BAY TRANSITION PANEL SUPPORT AT LBL 20 BS 857 HAS CORROSION ON OLD REPAIR. REPAIRED ON FAS N148AS-01-01, NR 61224. - [SDR FOTR20140903025](https://openairdocs.org/sdr/FOTR20140903025), Aug 11, 2014: SKIN. DENTED. DENT FOUND IN SKIN ABOVE S26L, APPROXIMATELY BS 892. REPAIRED ON FAS N148AS-01-01, NR 61159. - [SDR FOTR20140918028](https://openairdocs.org/sdr/FOTR20140918028), Aug 7, 2014: FLOORBEAM. CORRODED. MAIN CABIN ON FLOORBEAM 986 BL 0 - LBL 45 HAS LIGHT CORROSION. REPAIRED IAW N148AS-01-01. - [SDR FOTR20140902024](https://openairdocs.org/sdr/FOTR20140902024), Aug 7, 2014: FITTING. CORRODED. MAIN CABIN AT BS 990, LBL 32 TIE DOWN FITTING HAS LIGHT CORROSION. REPLACED IAW FAS N148AS-01-01. - [SDR FOTR20140828017](https://openairdocs.org/sdr/FOTR20140828017), Aug 7, 2014: FRAME. CRACKED. MAIN CABIN FRAME, BS 907 BELOW STRINGER 8R CRACKED. REPAIRED IAW FAS W/O N148AS-01-01. - [SDR FOTR20140828016](https://openairdocs.org/sdr/FOTR20140828016), Aug 7, 2014: FRAME. CRACKED. MAIN CABIN AT FRAME BS 380, BELOW STRINGER 8L CRACKED. REPAIRED IAW FAS N148AS-01-01. - [SDR FOTR20140823015](https://openairdocs.org/sdr/FOTR20140823015), Aug 7, 2014: FRAME. CRACKED. MAIN CABIN FRAME BS 827 BELOW STRINGER 8L CRACKED AROUND RIVET. REPAIRED ON FAS WO N148AS-01-01. - [SDR FOTR20140821013](https://openairdocs.org/sdr/FOTR20140821013), Aug 7, 2014: FRAME. CRACKED. MAIN CABIN AT FRAME BS 400 BELOW STG 8R AROUND RIVET CRACKED. REPAIRED ON FAS WO N148AS-01-01. - [SDR FOTR20140821011](https://openairdocs.org/sdr/FOTR20140821011), Aug 7, 2014: FRAME. CRACKED. MAIN CABIN AT FRAME BS 400 BELOW STG 8L AROUND RIVET CRACKED. - [SDR FOTR20140829021](https://openairdocs.org/sdr/FOTR20140829021), Aug 6, 2014: CHANNEL. CORRODED. MAIN CABIN BETWEEN BS 327-333, RBL 60 CHANNEL CORRODED. REPAIRED ON FAS N148AS-01-01, NR 60860. - [SDR FOTR20140821014](https://openairdocs.org/sdr/FOTR20140821014), Aug 6, 2014: FLOORBEAM. CORRODED. MAIN CABIN AT FLOORBEAM BS 366 BETWEEN BL 0 - LBL 20 HAS LIGHT CORROSION. REPAIRED ON FAS WO N148AS-01-01. - [SDR FOTR20140821012](https://openairdocs.org/sdr/FOTR20140821012), Aug 6, 2014: FLOORBEAM. CORRODED. MAIN CABIN FLOORBEAM AT BS 360 BL 0 HAS LIGHT CORROSION. REPAIRED ON FAS WO N148AS-01-01. - [SDR FOTR20140818010](https://openairdocs.org/sdr/FOTR20140818010), Aug 6, 2014: FLOORBEAM. CORRODED. MAIN CARGO AT FLOORBEAM, BS 907, BL0 HAS LIGHT CORROSION. REPAIRED FLOORBEAM. - [SDR FOTR20140818009](https://openairdocs.org/sdr/FOTR20140818009), Aug 6, 2014: FLOORBEAM. CORRODED. MAIN CABIN AT BS 328 FLOORBEAM BETWEEN LBL 49 AND LBL 56 HAS LIGHT CORROSION. REPAIRED ON FAS WO N148AS-01-01, NR 60853. - [SDR FOTR20140828019](https://openairdocs.org/sdr/FOTR20140828019), Aug 5, 2014: DOOR SILL. CORRODED. AFT CARGO LOWER DOOR SILL CORRODED INSIDE AROUND FASTENERS BETWEEN BS 807-845. REPAIRED ON FAS N148AS-01-01. - [SDR FOTR20140828018](https://openairdocs.org/sdr/FOTR20140828018), Aug 5, 2014: WEB. CORRODED. AFT/LOWER CARGO DOOR FRAME BS 494 STRINGER 28R UPPER WEB IS CORRODED AND GOUGED IN SEVERAL PLACES. REPAIRED ON FAS N148AS-01-01. - [SDR FOTR20140918027](https://openairdocs.org/sdr/FOTR20140918027), Jul 30, 2014: SKIN. DENTED. FUSELAGE BELLY BS 490 DENTED. REPAIRED IAW N148AS-01-01. - [SDR FOTR20140909026](https://openairdocs.org/sdr/FOTR20140909026), Jul 30, 2014: SKIN. DENTED. EXT FUSELAGE RT SIDE AT STA 495, BETWEEN 20R & 22R HAS MULTIPLE DENTS. REPAIRED ON FAS WO N148AS-01-01, NR 60228. - [SDR FOTR20140902023](https://openairdocs.org/sdr/FOTR20140902023), Jul 30, 2014: SKIN. DENTED. SKIN BS 251 BETWEEN 23-24R HAS PROTRUDING DENT. REPAIRED IAW FAS N148AS-01-01. - [SDR FOTR20140902022](https://openairdocs.org/sdr/FOTR20140902022), Jul 30, 2014: SKIN. DENTED. LEFT FUSELAGE SKIN HAS SEVERAL DENTS BETWEEN BS 907 - 947.5 STRINGERS 17 - 19 LT. REPAIRED IAW FAS N148AS-01-01. ## 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 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 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 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/N148AS/stcs.md ## Earlier aircraft with N148AS The FAA can reassign an N-number once a registration is cancelled. These aircraft carried N148AS before. - [Cancelled 2019-07-02](https://openairdocs.org/deregistered/N148AS-2019-07-02): Airbus Industrie A320-233, S/N 1400. Owner: [Aersale Inc](https://openairdocs.org/faa-owner/AERSALE%20INC), [Coral Gables, FL](https://openairdocs.org/faa-place/FL/Coral%20Gables) - [Cancelled 2007-11-02](https://openairdocs.org/deregistered/N148AS-2007-11-02): Diamond Aircraft Ind DA20-C1, S/N C0282, built 2004. Exported to Iceland. Owner: [Jmac Enterprises Inc](https://openairdocs.org/faa-owner/JMAC%20ENTERPRISES%20INC), [Asheville, NC](https://openairdocs.org/faa-place/NC/Asheville) ## 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 --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.