# Alexanderia 17-31A - Type: Aircraft model (FAA registry) - Registry code: 1250022 - Manufacturer (registry): ALEXANDERIA AIRCRAFT LLC - Model: 17-31A - 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: 0 - Page: https://openairdocs.org/model/alexanderia-17-31a 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 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 75-11-06](https://openairdocs.org/ad/75-11-06): Check Valve · Alexandria 17-31, 17-31A, 17-31ATC and 1 more. Effective Jun 25, 1975 - [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 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) (1) - [SAIB SW-18-31](https://openairdocs.org/saib/SW-18-31): NAVIGATION, ATTITUDE, AND DIRECTION DATA SYSTEM. Issued Nov 21, 2018 ## Registered aircraft None registered with this model now. ## NTSB investigations None matched to aircraft with this model. ## FAA accident and incident reports None matched to aircraft with this model. ## Service difficulty reports (8) As reported by operators and repair stations, by the model named in the report. - [SDR 2007FA0000687](https://openairdocs.org/sdr/2007FA0000687), Jul 24, 2007: POWERPACK. BURNED OUT. THIS COMPONENT WAS INSTALLED FRESHLY OVERHAULED ON APRIL 6, 2006 AND HAS A TOTAL IN USE TIME OF 18.0 HOURS. AFTER TAKEOFF THE PILOT NOTICED THE LANDING GEAR WOU - [SDR 2007FA0000068](https://openairdocs.org/sdr/2007FA0000068), May 21, 2006: SPRING. WEAK. AFTER AN INFLIGHT LANDING GEAR POWER PACK FAILURE, THE PILOT WAS UNABLE TO PERFORM AN EMERGENCY NOSE GEAR EXTENSION EVEN THOUGH THE MAIN GEAR WAS SAFELY EXTENDE - [SDR 20010604CW016](https://openairdocs.org/sdr/20010604CW016), May 11, 2001: HINGE. FAILED. PILOT DID NOT REPORT ANY ABNORMAL OPERATION. AIR BOX WAS REMOVED AT ANNUAL INSPECTION FOR SERVICING AND ALTERNATE AIR DOOR FELL ON FLOOR. ALL HINGE PIN SEGMENTS - [SDR 20001101SH008](https://openairdocs.org/sdr/20001101SH008), Oct 16, 2000: ALT AIR DOOR. FAILED. PILOT REPORTED LOSS OF POWER ON TAKEOFF CLIMB. AFTER RETURNING TO THE AIRPORT, INVESTIGATION REVEALED A FAILED ALTERNATE AIR DOOR. (X) - [SDR 99ZZZX3602](https://openairdocs.org/sdr/99ZZZX3602), Sep 3, 1999: AIR DOOR. BROKEN. AIRCRAFT LOST POWER ON TAKEOFF AND HAD TO MAKE AN EMERGENCY LANDING. AIRCRAFT WAS ABLE TO RETURN TO AIRPORT. TOWER REPORTED A LARGE AMOUNT OF BLACK SMOKE COMING - [SDR CA970902023](https://openairdocs.org/sdr/CA970902023), Jun 28, 1997: IMPULSE COUPLING. WORN. (CAN) AIRCRAFT EXPERIENCED LOSS OF ENGINE POWER IN FLIGHT. EMERGENCY NO POWER LA NDING CARRRIED OUT IN FIELD. AIRCRAFT REMOVED FROM FIELD AND DISASSEMBLY OF ENG - [SDR 96ZZZX4228](https://openairdocs.org/sdr/96ZZZX4228), Aug 4, 1996: COLLAR. WELD CRACKED. WHILE PUTTING A HAND TOW BAR ON THE NOSE FORK, NOTICED PAINT FLAKING OFF THE FRONT STEERING COLLAR. REMOVED ALL THE PAINT OFF THE COLLAR AND NOTICED THE WELD WA - [SDR 95ZZZX1596](https://openairdocs.org/sdr/95ZZZX1596), Jan 28, 1995: CONTROL CABLE. RUSTED. THE PILOT REPORTED FLAP CABLE BROKE DURING FLIGHT. PILOT STATED WHEN ON FULL FLAP POSITION, HE HEARD A LOUD THUMP AND AIRCRAFT STARTED TO ROLL ON RIGHT WING. PI ## STCs that may be installed (OpenAirDocs) (156, 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 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 SA01375AT](https://openairdocs.org/stc/SA01375AT): Installation of an adapter ring, P/N J1001-1, and fuel cap assembly (usher type), P/N Uo03,. Bellanca Aircraft Incorporated - [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 SA01435LA](https://openairdocs.org/stc/SA01435LA): Installation of engines modified with Firewall Forward Technologies LLC modified camshaft. Centri-Lube Technologies LLC - [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 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 156: https://openairdocs.org/model/alexanderia-17-31a/stcs.md ## The same model under other registry codes Amateur-built copies and renamed makers get their own codes. - [Bellanca 17-31A](https://openairdocs.org/model/bellanca-17-31a): 70 registered aircraft, registry code 1220435 - [Bellanca 17-31A](https://openairdocs.org/model/bellanca-17-31a): 1 registered aircraft, registry code 1250031 --- 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.