# Alexandria 17-30A - Type: Aircraft model (FAA registry) - Registry code: 1250021 - Manufacturer (registry): ALEXANDRIA AIRCRAFT LLC - Model: 17-30A - Aircraft type: Fixed wing single engine - Category: Airplane - Engines: 1 · Reciprocating - Seats: 4 - Weight class: Up to 12,499 lb - Certification: Type certificated - Data sheet: [TCDS A18CE](https://openairdocs.org/tcds/A18CE) (OpenAirDocs) - Holder: Bellanca Aircraft Inc. - Registered aircraft: 1 - Page: https://openairdocs.org/model/alexandria-17-30a Model codes come from the FAA registry's reference file. ADs are matched to them by model name and maker. ## ADs that may apply (OpenAirDocs) Matched to this model by model name and maker. Each AD's applicability may narrow it by serial number, part number or equipment. - [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 2014-20-12](https://openairdocs.org/ad/2014-20-12): Fuselage · Alexandria 14-19-3A, 17-30, 17-30A and 4 more. Effective Nov 12, 2014 - [AD 2008-05-11](https://openairdocs.org/ad/2008-05-11): Muffler and tailpipe assemblies · Alexandria 17-30, 17-30A, 17-31 and 2 more. Effective Apr 8, 2008 - [AD 2006-03-08](https://openairdocs.org/ad/2006-03-08): Vacuum pumps · Aero Advantage 14-19, 14-19-2, 14-19-3 and 299 more. Effective Mar 10, 2006 - [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 98-21-21 R1](https://openairdocs.org/ad/98-21-21-R1): Electric Inflatable Door Seals · Cessna 17-30, 17-30A, 17-31 and 267 more. Effective May 1, 2000 - [AD 96-18-07](https://openairdocs.org/ad/96-18-07): Nose Landing Gear Drag Strut Brackets · Alexandria 17-30, 17-30A, 17-31 and 3 more. Effective Oct 25, 1996 - [AD 90-02-17](https://openairdocs.org/ad/90-02-17): Landing Gear Fitting Assemblies · Alexandria 14-19-3, 14-19-3A, 17-30 and 5 more. Effective Feb 5, 1990 - [AD 87-11-01 R1](https://openairdocs.org/ad/87-11-01-R1): Fuel Caps & Drains · Alexandria 17-30, 17-30A, 17-31 and 3 more. Effective Aug 28, 1987 - [AD 86-25-06](https://openairdocs.org/ad/86-25-06): Wing Main and Auxiliary Fuel Tanks · Alexandria 17-30, 17-30A, 17-31 and 3 more. Effective Dec 22, 1986 - [AD 77-22-02](https://openairdocs.org/ad/77-22-02): Nose Landing Gear Engine Mount · Alexandria 14-19-3, 14-19-3A, 17-30 and 1 more. Effective Nov 2, 1977 - [AD 76-08-04](https://openairdocs.org/ad/76-08-04): Wood Deterioration · Alexandria 14-19, 14-19-2, 14-19-3 and 7 more. Effective Sep 9, 1976 - [AD 73-05-02](https://openairdocs.org/ad/73-05-02): Rudder Control System · Alexandria 17-30A, 17-31A and 17-31ATC. Effective Mar 7, 1973 - [AD 73-03-03](https://openairdocs.org/ad/73-03-03): Engine Induction Box Bolts · Alexandria 17-30A. Effective Feb 7, 1973 - [AD 72-01-03](https://openairdocs.org/ad/72-01-03): Engine Fuel Hose · Alexandria 17-30A, 17-31A and 17-31ATC. Effective Jan 5, 1972 Historical (superseded or no longer in force): - [AD 76-23-03 R1](https://openairdocs.org/ad/76-23-03-R1) (historical): Exhaust System · Alexandria 17-30, 17-30A, 17-31 and 1 more. Effective Nov 7, 1986 - [AD 75-20-06](https://openairdocs.org/ad/75-20-06) (historical): Vertical Tubes · Alexandria 14-19-3A, 17-30, 17-31 and 4 more. Effective Sep 26, 1975 ## Information bulletins (advisory) (2) - [SAIB 2025-07](https://openairdocs.org/saib/2025-07): Reciprocating Engine Supercharger. Issued Jul 28, 2025 - [SAIB SW-18-31](https://openairdocs.org/saib/SW-18-31): NAVIGATION, ATTITUDE, AND DIRECTION DATA SYSTEM. Issued Nov 21, 2018 ## Registered aircraft (1) - [N183SV](https://openairdocs.org/aircraft/N183SV): [Quality Feed Grains Inc](https://openairdocs.org/faa-owner/QUALITY%20FEED%20GRAINS%20INC), [Harrison, AR](https://openairdocs.org/faa-place/AR/Harrison), S/N 05-301031 ## NTSB investigations None matched to aircraft with this model. ## FAA accident and incident reports None matched to aircraft with this model. ## Service difficulty reports (29) As reported by operators and repair stations, by the model named in the report. - [SDR 2024FA0000814](https://openairdocs.org/sdr/2024FA0000814), Nov 4, 2024: ALTERNATOR. DEFECTIVE. AT THE END OF A FLIGHT TOTALING 2.5 HOURS THE AMMETER INDICATED A DISCHARGE AND LOW VOLTAGE WARNING LIGHT ILLUMINATED. I WAS ALMOST OVERHEAD MY POINT OF INTENDE - [SDR 2024FA0000772](https://openairdocs.org/sdr/2024FA0000772), Dec 30, 2023: ENGINE. POWER LOSS. TOTAL LOSS OF POWER AT 400 FEET AS I INITIATED MY LEFT PATTERN TURN OUT THE 2ND TIME. THE FIRST TIME WAS 2 WEEKS BEFORE, SAME THING EXCEPT I WAS AT 500 FEET. CO - [SDR 2018FA0000140](https://openairdocs.org/sdr/2018FA0000140), Apr 15, 2018: WHEEL HALF. SEPARATED. UPON TAXI OUT LT MAIN WHEEL FELT LIKE A FLAT SPOT ON TIRE, PULLED OFF RUNWAY NOTICE RIM OF TIRE RUBBING ON BRAKE CALIPER WHEN WHEEL WAS TURNING, 40-75E WHEEL, U - [SDR 2016FA0000385](https://openairdocs.org/sdr/2016FA0000385), Jul 30, 2016: DUMP VALVE. BYPASSING. INTERNAL FAILURE OF THE DUMP VALVE IN THE HYDRAULIC SYSTEM PREVENTED THE NOSE LANDING GEAR FROM PROPERLY EXTENDING AND LOCKING EVEN AFTER THE EMERGENCY GEAR EXT - [SDR CA151208017](https://openairdocs.org/sdr/CA151208017), Dec 8, 2015: LEG ASSY. CRACKED. (CAN) DURING ANNUAL INSPECTION THE LT MLG STRUT WOULD NOT HOLD A NITROGEN CHARGE. UPON FURTHER INVESTIGATION IT WAS OBSERVED THAT THE UPPER LEG OF THE MLG ASSY - [SDR 2014FA0000267](https://openairdocs.org/sdr/2014FA0000267), Mar 25, 2014: LANDING GEAR. COLLAPSED. ON TOUCHDOWN, LT MLG COLLAPSED AND THE ACFT VEERED OFF TO THE LT AND CAME TO A STOP IN THE GRASSY AREA OF THE NEUTRAL ZONE OF THE RUNWAY. - [SDR 2010FA0000831](https://openairdocs.org/sdr/2010FA0000831), Jul 30, 2010: ROD END. FAILED. DURING TOUCHDOWN, NLG FAILED AND PARTIALLY COLLAPSED UPON CONTACT WITH THE RUNWAY. DURING THE INVESTIGATION AND RESEARCH INTO THE NLG SYS AND LINKAGE, IT APPEAR - [SDR 2007FA0000678](https://openairdocs.org/sdr/2007FA0000678), Jun 24, 2007: SHUTTLE VALVE. MALFUNCTIONED. THE AIRCRAFT LOST ELECTRICAL POWER AND PILOT TRIED TO EXTEND THE LANDING GEAR USING THE EMERGENCY LEVER. THE EMERGENCY LOWERING OF THE LANDING GEAR DID NOT TAKE - [SDR 2007FA0000093](https://openairdocs.org/sdr/2007FA0000093), Dec 25, 2006: CRANKSHAFT. BROKEN. CRANKSHAFT IS BROKEN IN AREA OF NR6, NR5 ROD JOURNAL. CRANKSHAFT BROKE ON APPROACH TO LANDING AS PROP RPM CONTROL WAS ADVANCED ON SHORT FINAL. ENGINE POWER UNDE - [SDR 2006FA0000881](https://openairdocs.org/sdr/2006FA0000881), Aug 30, 2006: COVER. CRACKED. 5 INCH SPANWISE CRACK, 10 INCHES AFT OF FORWARD EDGE OF OIL SUMP COVER. - [SDR 2005FA0001599](https://openairdocs.org/sdr/2005FA0001599), Dec 19, 2005: MUFFLER. BROKEN. RT SIDE MUFFLER, REAR TAIL-PIPE OUTLET, CRACKED OFF OF THE MUFFLER ALLOWING HOT GASES TO BLOW ONTO FIREWALL AND SURROUNDING COMPONENTS. AN ENGINE FIRE OCCURRED - [SDR 2005FA0000270](https://openairdocs.org/sdr/2005FA0000270), Sep 28, 2004: CYLINDER HEAD. SEPARATED. AIRCRAFT ANNUAL INSP- 2 WEEKS PRIOR- REPLACED EXHAUST AND INTAKE VALVES ON NR 2 CYLINDER DUE TO LOW COMPRESSION. FLEW 6 HOURS PRIOR TO INCIDENT. IN CRUISE FLIGH - [SDR 2004FA0000145](https://openairdocs.org/sdr/2004FA0000145), Nov 4, 2003: LEG ASSY. CRACKED. A CRACK HAD FORMED, PREVIOUS TO INCIDENT, AROUND THE BUSHING BOSS ON THE INBOARD END OF THE MOUNT PORTION OF THE UPPER MAIN GEAR LEG. THE RESULT WAS THAT THE MA - [SDR 20001101SH006](https://openairdocs.org/sdr/20001101SH006), Aug 2, 2000: SOLENOID. FAILED. PRIOR TO TAKEOFF ON ENGINE RUN-UP, AIRCRAFT LOST ALL ELECTRICAL POWER, STARTER SOLENOID STAYED ENGAGED. THE ENGINE RAN THE STARTER, CAUSED A REVERSE CURRENT FLO - [SDR 20000404SH002](https://openairdocs.org/sdr/20000404SH002), Mar 8, 2000: GUIDE. WORN. EXCESSIVE WEAR FOUND DURING COMPRESSION TEST. EXHAUST VALVE WAS LEAKING. EX GUIDE MEASURED .4384 INCH AT THE TOP AND .4624 INCH AT THE BOTTOM. EX VALVE MEASURED - [SDR 20000404SH001](https://openairdocs.org/sdr/20000404SH001), Mar 8, 2000: EXHAUST VALVE. WORN. EXCESSIVE WEAR FOUND DURING COMPRESSION TEST. EXHAUST VALVE WAS LEAKING. EX GUIDE MEASURED .4384 INCH AT THE TOP AND .4624 INCH AT THE BOTTOM. EX VALVE MEASURED - [SDR 20000412SH008](https://openairdocs.org/sdr/20000412SH008), Feb 10, 2000: WIRE. ARCED. OPERATOR REPORTED DISCHARGE FROM ALTERNATOR IN CRUISE FLIGHT. MASTER SWITCH WAS TURNED OFF. AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE DISCOVERED ONE BRUSH W - [SDR 99ZZZX4424](https://openairdocs.org/sdr/99ZZZX4424), Nov 10, 1999: COLLECTOR. SEPARATED. OPERATOR REPORTED STRONG EXHAUST SMELL IN COCKPIT. REMOVED COWL AND FOUND THE RIGHT EXHAUST BROKEN AT THE COLLECTOR OUTLET. ATTEMPTED A WELD REPAIR, BUT FOUND T - [SDR 99ZZZX2410](https://openairdocs.org/sdr/99ZZZX2410), May 18, 1999: SUPPORT. FAILED. LEFT MG UPPER STRUT HOUSING WELD FAILED CAUSING STRUT TO TEAR LOOSE FROM TRUNNION. REMOVED RIGHT MG UPPER STRUT HOUSING AND FOUND FAILED WELD. APPEARED TO BE LA - [SDR 99ZZZX1936](https://openairdocs.org/sdr/99ZZZX1936), Apr 26, 1999: CYLINDER. LOOSE. ENGINE LOG ENTRY JANUARY 3, 1991, FOR REMOVAL AND REPLACEMENT OF ALL 6 ENGINE CYLINDERS. CYLINDERS INSTALLED WERE CERMICRON CYLINDERS, FLANGES WERE PAINTED ORAN - [SDR 98ZZZX3018](https://openairdocs.org/sdr/98ZZZX3018), Jul 1, 1998: STRUT. MALFUNCTIONED. LEFT MAIN GEAR WOULD NOT COMPLETELY RETRACT. FOUND THE STRUT PRESSURE WAS IN EXCESS OF 120 PSI WITH CORrECT PRESSURE. OPS CHECKED OK. - [SDR 98ZZZX3073](https://openairdocs.org/sdr/98ZZZX3073), Jun 18, 1998: EXTENSION ASSY. SEPARATED. ON LANDING, ROD END SEPARATED FROM NLG EXTENSION ASSEMBLY. - [SDR 97ZZZX2879](https://openairdocs.org/sdr/97ZZZX2879), May 29, 1997: RELAY. DETACHED. RELAY CAME LOOSE FROM SOCKET. RELAY IS MOUNTED UPSIDE DOWN IN AIRCRAFT. NO WAY TO ATTACH IN HOLDER. NEEDS SOME TYPE OF POSITIVE LOCKING. IF SWITCH COMES LOOSE O - [SDR 96ZZZX362](https://openairdocs.org/sdr/96ZZZX362), Dec 24, 1995: STEERING COLLAR. FAILED. DURING TAKEOFF ROLL, NOSE GEAR COLLAPSED. UPON INVESTIGATION, THE REAR STEERING COLLAR ASSEMBLY WAS FOUND BROKEN, WHICH ALLOWED NOSE WHEEL TO PIVOT FREELY. THE - [SDR 95ZZZX6300](https://openairdocs.org/sdr/95ZZZX6300), Oct 26, 1995: CONNECTOR. SHORTED. LANDING GEAR MOTOR AND WARNING LIGHT WOULD NOT GO OFF IN THE DOWN MODE, BUT DID HAVE THREE GREEN DOWN LIGHTS. FOUND AMPHENOL CONNECTOR WHICH CONTAINS LIGHT DIOD - [SDR 95ZZZX4514](https://openairdocs.org/sdr/95ZZZX4514), Aug 16, 1995: BULKHEAD. CRACKED. PROPELLER BULKHEAD CRACK FOUND DURING ANNUAL INSPECTION. POSSIBLE CAUSE OF CRACK IS SLIGHT DISHING OF BULKHEAD THAT IS FLATTENED OUT WHEN MOUNT BOLTS ARE TIGHTE - [SDR 95ZZZX4513](https://openairdocs.org/sdr/95ZZZX4513), Aug 16, 1995: BRACKET. CRACKED. BRACKET PASSED 10X INSPECTION ON AIRCRAFT. NOSE GEAR REMOVAL FOR REBUILD ALLOWED BRACKET INSPECTION WITH DRAG LINK REMOVED. DYE PENETRANT REVEALED CRACKS OUT OF - [SDR 95ZZZX4386](https://openairdocs.org/sdr/95ZZZX4386), Aug 16, 1995: COOLER. CRACKED. REPAIR STATION FOUND CRACKS IN MOUNTING BASE OF OIL COOLER DURING OVERHAUL TO CORRECT LEAK IN TUBES. EXCHANGE UNIT WAS INSTALLED. - [SDR 95ZZZX3129](https://openairdocs.org/sdr/95ZZZX3129), May 26, 1995: PROP CONTROL. BOLT WORN. WHILE RUNNING THE ACFT AFTER AN ANNUAL INSPECTION, FOUND PROP CONTROL VERY STIFF. EVENTUALLY, AFTER ATTEMPTING TO MOVE THE CONTROL, IT BROKE OFF. THE POINT OF B ## STCs that may be installed (OpenAirDocs) (157, first 50) Approved for this model: the STC's model list names it on its data sheet, or a series that includes it. In force first, then newest. The registry doesn't record which STCs an aircraft has. - [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 SA12428CH](https://openairdocs.org/stc/SA12428CH): Installation of the Lycoming Engines Electronic Ignition System (EIS). Lycoming Engines, An Operating Division of AVCO Corporation - [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 SA01005DE](https://openairdocs.org/stc/SA01005DE): Installation of a EarthX ETX900-TSO Lithium battery. EarthX Inc - [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 SA7965SW](https://openairdocs.org/stc/SA7965SW): Application of fabric and polyurethane finishing system. Shady Aviation LLC - [STC SA04378CH](https://openairdocs.org/stc/SA04378CH): Installation of an engine modified per STC SE04349CH. SureFly Partners Ltd - [STC SA02594SE](https://openairdocs.org/stc/SA02594SE): SkyView HDX Instrumentation and Autopilot System manufactured. Dynon Avionics - [STC SA04568CH](https://openairdocs.org/stc/SA04568CH): Installation of the uAvionix tailBeaconX, a tail mounted position light with integrated Automatic Dependent Surveillance - Broadcast (ADS-B) Out and 1090MHz Mode-S transponder functionality. uAvionix Corporation - [STC SA4503NM](https://openairdocs.org/stc/SA4503NM): Remove original cloth covering and install Ceconite covering. Ceconite Division of Poly-Fiber Inc - [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 SA00756DE](https://openairdocs.org/stc/SA00756DE): Installation of Automatic Dependent Surveillance Broadcast (ADS-B) Out Equipment using a Trig Avionics TT22 Transponder and an approved Global Positioning System (GPS) Position Sensor. Peregrine - [STC SA04776NY](https://openairdocs.org/stc/SA04776NY): The HIPEC Covering and Finishing System must be performed and maintained. HIPEC Aircraft Coatings 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 SA2510NM](https://openairdocs.org/stc/SA2510NM): Installation of inflatable door seal. TALCO Aviation Corp - [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 SA02268CH](https://openairdocs.org/stc/SA02268CH): Installation of Airwolf Filter Corp. Air Oil Separator. Airwolf Filter Corporation - [STC SA1257CE](https://openairdocs.org/stc/SA1257CE): Installation of King KFC 200, 2 axis, flight control system with a KI 255 (or -256) flight command indicator or a KG 258 attitude horizon gyro with a KC 292 mode controller or stand alone electric trim. Honeywell 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 SA03286CH](https://openairdocs.org/stc/SA03286CH): Install an electronic engine ignition system. Electroair Acquisition Corporation - [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 SA615EA](https://openairdocs.org/stc/SA615EA): Installation of a Whelen Anti-Collision Strobe Light System as replacement for originally installed anti-collision 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 SA04165NY](https://openairdocs.org/stc/SA04165NY): Installation of Latitude Technologies Skynode S200 Satcom system must be performed. Latitude Technologies Corporation - [STC SA01435SE](https://openairdocs.org/stc/SA01435SE): Installation of J.P. Instruments (JPI) Primary Engine Data Management System. J. P. Instruments - [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 SA3688WE](https://openairdocs.org/stc/SA3688WE): Installation of an air/oil separator. Airwolf Filter Corporation - [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 SA00382BO](https://openairdocs.org/stc/SA00382BO): Installation of Globalstar Antenna and Cradle provisions to support a Globalstar GPS-1700 in non-composite airplanes. Avidyne Corporation - [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 All 157: https://openairdocs.org/model/alexandria-17-30a/stcs.md ## The same model under other registry codes Amateur-built copies and renamed makers get their own codes. - [Bellanca 17-30A](https://openairdocs.org/model/bellanca-17-30a): 399 registered aircraft, registry code 1220433 --- 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.