# N331SW: 2026 Cirrus Design SR20 - Status: Valid registration - Airframe: Cirrus Design SR20 (registry code 2130000, TCDS A00009CH (OpenAirDocs match)) - Engine: Lycoming IO-390-C3B6 (registry code 42710, TCDS E00006NY (OpenAirDocs match)) - Serial number: 11298 - Year built: 2026 - Type: Fixed wing single engine - Airworthiness: Standard, normal - Airworthiness date: March 25, 2026 - Certificate issued: June 20, 2026 - Expires: June 30, 2033 - Mode S code: A39B2B - Registered owner: Dos Perros Largos LLC - Location: Prescott, AZ - Owner's area on the map: 34.7698° N, 112.7570° W: Placed by OpenAirDocs at the center of ZIP code 86305, within about 14 miles (OpenAirDocs) - Page: https://openairdocs.org/aircraft/N331SW 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 matched by airframe (Cirrus Design SR20) (OpenAirDocs) - [AD 2024-24-11](https://openairdocs.org/ad/2024-24-11): Power Lever · Cirrus Design SR20, SR22 and SR22T. Effective Dec 23, 2024 - [AD 2022-03-15](https://openairdocs.org/ad/2022-03-15): Fuel Quantity Indicator · Garmin G3X Touch Electronic Flight Instrument System (STC SA01899WI). Effective Mar 21, 2022 - [AD 2009-05-05](https://openairdocs.org/ad/2009-05-05): Primary Flight Displays · Avidyne Primary Flight Display (S-TEC STC SA09543AC-D or 2 others). Effective Apr 3, 2009 - [AD 2008-14-13](https://openairdocs.org/ad/2008-14-13): Upper door hinge · Cirrus Design SR20 and SR22. Effective Aug 14, 2008 - [AD 2008-11-18](https://openairdocs.org/ad/2008-11-18): Heat exchanger · Cirrus Design SR20. Effective Jul 7, 2008 - [AD 2008-03-16](https://openairdocs.org/ad/2008-03-16): Rudder, aileron, and rudder-aileron interconnect rigging · Cirrus Design SR20 and SR22. Effective Mar 11, 2008 - [AD 2007-14-03](https://openairdocs.org/ad/2007-14-03): Cirrus Airplane Parachute System (CAPS) · Cirrus Design SR20 and SR22. Effective Aug 16, 2007 - [AD 2006-21-03](https://openairdocs.org/ad/2006-21-03): Brake caliper piston O-ring seals · Cirrus Design SR20 and SR22. Effective Nov 17, 2006 - [AD 2006-19-10](https://openairdocs.org/ad/2006-19-10): Adjust crew seat break-over bolts · Cirrus Design SR20 and SR22. Effective Oct 24, 2006 - [AD 2006-07-06](https://openairdocs.org/ad/2006-07-06): Wire harness · Cirrus Design SR20 and SR22. Effective May 11, 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 2002-24-08](https://openairdocs.org/ad/2002-24-08): Cable clamp · Cirrus Design SR20 and SR22. Effective Jan 24, 2003 - [AD 2002-21-02](https://openairdocs.org/ad/2002-21-02): Self-locking retaining nut · Cirrus Design SR20 and SR22. Effective Nov 8, 2002 - [AD 2001-25-03](https://openairdocs.org/ad/2001-25-03): Rivets In Elevator and Rudder · Cirrus Design SR20 and SR22. Effective Dec 17, 2001 Historical (superseded or no longer in force): AD 2008-06-28 R1, AD 2008-06-28, AD 2005-17-19, AD 2002-05-05 ## ADs matched by engine (Lycoming IO-390-C3B6) (OpenAirDocs) - [AD 2026-04-11](https://openairdocs.org/ad/2026-04-11): Engine (Reciprocating) · Lycoming Engines AEIO-320-D1B, AEIO-320-D2B, AEIO-320-E1A and 605 more. Effective Apr 8, 2026 ## Information bulletins (advisory) - [SAIB SW-18-31](https://openairdocs.org/saib/SW-18-31): NAVIGATION, ATTITUDE, AND DIRECTION DATA SYSTEM - [SAIB CE-11-50](https://openairdocs.org/saib/CE-11-50): Flight Controls, Flaps - [SAIB CE-08-12R1](https://openairdocs.org/saib/CE-08-12R1): Electrical Power - [SAIB CE-11-09](https://openairdocs.org/saib/CE-11-09): Navigation Flight Management Computing Software System - [SAIB CE-09-46](https://openairdocs.org/saib/CE-09-46): Landing Gear, Nose - [SAIB CE-09-32](https://openairdocs.org/saib/CE-09-32): Navigation: Cirrus Aircraft Under-Glareshield GPS/WAAS Antenna Mount - [SAIB CE-09-01](https://openairdocs.org/saib/CE-09-01): Equipment - Emergency - [SAIB CE-08-12](https://openairdocs.org/saib/CE-08-12): Electrical Power - [SAIB CE-07-08](https://openairdocs.org/saib/CE-07-08): Avidyne Primary Flight display (PFD) - [SAIB CE-06-30](https://openairdocs.org/saib/CE-06-30): - [SAIB CE-06-07](https://openairdocs.org/saib/CE-06-07): - [SAIB CE-05-88](https://openairdocs.org/saib/CE-05-88): - [SAIB CE-05-77](https://openairdocs.org/saib/CE-05-77): - [SAIB CE-04-74](https://openairdocs.org/saib/CE-04-74): - [SAIB CE-03-09](https://openairdocs.org/saib/CE-03-09): - [SAIB CE-02-34](https://openairdocs.org/saib/CE-02-34): - [SAIB NE-19-08](https://openairdocs.org/saib/NE-19-08): Reciprocating Engine Cylinder Section - Lycoming Engines Parallel Valve Cylinders ## Earlier aircraft with N331SW The FAA can reassign an N-number once a registration is cancelled. These aircraft carried N331SW before. - [Cancelled 2012-12-03](https://openairdocs.org/deregistered/N331SW-2012-12-03): Boeing 737-3H4, S/N 23695, built 1988. Sale reported. Owner: Sale Reported, Vinius ## Service difficulty reports (406) - [SDR SWAA2012052304249](https://openairdocs.org/sdr/SWAA2012052304249), May 16, 2012: SLIDE. R1 DOOR EMERGENCY EVAC SLIDE PRESSURE INDICATOR PRESSURE LOW. REMOVED AND REPLACED SLIDE PER MT. - [SDR SWAA2012052904390](https://openairdocs.org/sdr/SWAA2012052904390), May 11, 2012: SKIN. SKIN CRACKED AT BS 767+3, STR 14L. REPAIRED SKIN PER EA. - [SDR SWAA2012051403975](https://openairdocs.org/sdr/SWAA2012051403975), May 11, 2012: SKIN. SKIN CRACKED AT BS 767 +3, STR 14L. REPAIRED SKIN PER SRM. - [SDR SWAA2012051403930](https://openairdocs.org/sdr/SWAA2012051403930), May 11, 2012: SKIN. SKIN CRACKED AT BS 761 + 3, STR 14L. REPAIRED SKIN PER SRM. - [SDR SWAA2012051403974](https://openairdocs.org/sdr/SWAA2012051403974), May 10, 2012: SKIN. SKIN CRACKED AT B5 767, STR 14L. REPAIRED SKIN PER SRM. - [SDR SWAA2012051403933](https://openairdocs.org/sdr/SWAA2012051403933), May 10, 2012: SKIN. SKIN CRACKED AT BS 380 + 6, STR 26L. REPAIRED SKIN PER SRM. - [SDR SWAA2012051403932](https://openairdocs.org/sdr/SWAA2012051403932), May 10, 2012: SKIN. SKIN CRACKED AT BS 767 + 5, STR 14R. REPAIRED SKIN PER EA. - [SDR SWAA2012051403931](https://openairdocs.org/sdr/SWAA2012051403931), May 10, 2012: SKIN. SKIN CRACKED AT BS 500D + 15, STR 15L. REPAIRED SKIN IAW EA. - [SDR SWAA118674](https://openairdocs.org/sdr/SWAA118674), Dec 24, 2011: LIGHT. DURING SCHEDULED MV2 CHECK, FOUND RT O/W EMERGENCY EXIT LIGHT LWR LIGHT INOP. REPLACED LAMP PER MM. - [SDR SWAA118394](https://openairdocs.org/sdr/SWAA118394), Dec 7, 2011: ACTUATOR. POSSIBLE HYDRAULIC LEAK IN LT WHEEL WELL AREA. REMOVED AND REPLACED I/B GROUND SPOILER ACTUATOR IAW MM. --- From OpenAirDocs.org, an independent open copy of FAA data. Only the Federal Register edition on govinfo.gov is the official legal text of an AD.