What it approves
Installation of the 700-00212-110 and the 700-00212-010 12-inch Vantage Displays Systems with Attitude Reference System and the 700-00236-000 Air Data Computers System
What the certificate says
From the PDF’s text layer, without the form’s printed wording. Layout and order may differ; the PDF is the record.
SA12084BO Avidyne Corporation 4 Middlesex Green Suite 221 Concord, MA 01742 Part 23 the Federal Aviation Regulations A00009CH Cirrus Design Corporation SR20, SR22
1. The installer must determine whether this design changed is compatible with previously approved modifications.
(Limitations and Conditions Continued on page 3 of 4) 02/08/2023 07/23/2025 Rob Capezzuto Acting Manager, East Certification Branch Compliance & Airworthiness Division Aircraft Certification Service 4
1. Installation of the 700-00212-110 and the 700-00212-010 12-inch Vantage Displays Systems with Attitude Reference System and the 700-00236-000 Air Data Computers System on the Cirrus SR20 and SR22 in accordance with Master Document List AVVAN-017 rev 02, dated July 11, 2025 or later FAA approved revision. (Type Design Change Continued on page 3 of 4)
SA12084BO 4
SA12084BO Description of Type Design Change (continued from page 1 of 4)
2. Operation must be in accordance with Instructions for Continued Airworthiness AVVAN-024, dated July 11, 2025 or later FAA accepted revision.
3. Aircraft must be operated in accordance with Airplane Flight Manual Supplement dated July 23, 2025 (or FAA approved later revision). The AFMS is required to be carried on the aircraft at all times.
Limitations and Conditions (continued from page 1 of 4)
2. A copy of this STC must be included in the permanent record of the modified aircraft.
3. If the holder agrees to permit another person to use this certificate to alter a product, the holder must give the other person written evidence of that permission.
4. The following STC prerequisites are required to be applied prior to incorporation of this STC:
STC SA00166BO: Installation of Avidyne Corporation Primary Flight Display, Part Number 700-00006-000, and Magnetometer/OAT Sensor, Part Number 700-00011-000…
STC SA00143BO: Installation of Avidyne Corporation Model 700-00004-XXX-() Multi-Function Display…
STC SA00296BO: Installation of Model DFC90, part number 700-00170-000…
STC SA00343BO: Installation of a single configuration or of a dial configuration Avidyne Corporation Integrated Flight Display, Model IFD5XX and/or Model IFD4XX…
5. The aircraft must be operated in accordance with the operations limitations section of the Airplane Flight Manual referenced in the Description of Type Design section of this STC.
SA12084BO Certification Basis:
Based in 14 CFR 21.115, 21.101, and the FAA policy for significant changes in FAA Order 8110.48, the certification basis for the Cirrus Design Model SR20/22 airplane is as follows:
a. The type certification basis for the Cirrus Design SR20/22 is shown on TCDS A00009CH for parts not changed or not affected by the changed.
b. The certification basis for parts changed or affected by the change since the reference date of application, Feb 8, 2023, is based upon Part 23 as amended by Amendment 23-64.
Regulations at the latest amendment 23-1 through 23-64 §§21.20, 23.2010, 23.2100, 23.2210, 23.2230, 23.2235, 23.2250(a)(b), 23.2255(a)(c), 23.2260,
23.2265, 23.2270(a)(b)(c)(d), 23.2325 (a)(b)(c)(d), 23.2400(e), 23.2500, 23.2505, 23.2510,
23.2515, 23.2520, 23.2525, 23.2530(a), 23.2600(a)(b), 23.2605, 23.2610, 23.2615, 23.2620(a)
Regulations at an intermediate amendment None
Regulations at the amendment level in TCDS A00009CH None
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