# STC SA00282BO

- Type: Supplemental type certificate
- Status: Current, Amended
- Holder: Avidyne Corporation
- Description: Installation of Avidyne Corporation Entegra Integrated Flight Display System
- Status date: June 16, 2014
- Data sheets: A00009CH, A00009CH, A3SO, A3SO, A3SO, A3SO, A25SO
- Certificate PDF: https://openairdocs.org/files/sha256/eb/83/eb831180547482a2f53e8a87458dc3cbd622a72c3165955cdda6ff27a3517023
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/24D8D8BA6CB57E4F86257D1D0055DEC4.0001
- Page: https://openairdocs.org/stc/SA00282BO

## ADs that name it

- [AD 2015-10-51](https://openairdocs.org/ad/2015-10-51): Navigation · Avidyne Integrated Flight Displays. Effective Jul 1, 2015. Named in the applicability

## Approved models (7)

- Cirrus Design Corporation SR20 (TCDS A00009CH)
- Cirrus Design Corporation SR22 (TCDS A00009CH)
- Piper Aircraft Inc. PA-32-301 (TCDS A3SO)
- Piper Aircraft Inc. PA-32-301FT (TCDS A3SO)
- Piper Aircraft Inc. PA-32R-301 (HP) (TCDS A3SO)
- Piper Aircraft Inc. PA-32R-301 (SP) (TCDS A3SO)
- Piper Aircraft Inc. PA-46R-350T (TCDS A25SO)

## What the certificate says

Read from the PDF's text layer, without the form's printed wording; the layout is lost and the order can differ. The PDF is the record.

Part 23 of the Federal Aviation Regulations.

Installation of Avidyne Corporation Entegra Integrated Flight Display System in accordance with Avidyne Corporation Master Document List referenced on the attached AML, or later FAA-approved revisions.

System installation consists of:

1) Two Avidyne Integrated Flight Displays (IFDs), p/n 700-00083-( ).

2) Avidyne IFD software Release 9.2 or later FAA approved version.

3) Avidyne Control/Display Unit, p/n 700-00150-( ).

4) Avidyne Magnetometer/OAT Sensor p/n 700-00011-( ) for the right side IFD.

5) Optional Becker Mode C transponder p/n ATC 4401-2-250 or Mode S Transponder p/n BXP 6402-1R-01.

6) Optional PS Engineering Audio Panel p/n 050-890-0402.

7) Other ancillary equipment such as antennas, cable assemblies, circuit breaker panels, etc.

(Limitations and Conditions continued on Page 3 of 3)

Avidyne Corporation 55 Old Bedford Road Lincoln, Massachusetts 01773

See attached FAA Approved Model List (AML), Document No. AVIFD-006, Rev 05, or later FAA approved revision, for the list of approved airplane models, applicable installation data requirements, and specific limitations.

Date of application : October 17, 2005

Date of issuance : April 24, 2009

Date amended : October 12, 2010, February 18, 2011

( Signature) Robert G. Mann Manager Boston Aircraft Certification Office

( Title)

United States Of America Department of Transportation - Federal Aviation Administration Supplemental Type Certificate (Continuation Sheet) Number SA00282BO February 18, 2011

FAA Form 8110-2-1(10-69) Page 2 of 3

Transfer the ownership of Supplemental Type Certificate Number

to (Name of transferee)

(Address of transferee) (Number and street)

( City, State, and ZIP code)

from (Name of grantor)(Print or type)

(Address of grantor) (Number & street)

(City, State, and ZIP code)

Signature of grantor ( In ink):

United States Of America Department of Transportation - Federal Aviation Administration Supplemental Type Certificate (Continuation Sheet) Number SA00282BO February 18, 2011

FAA Form 8110-2-1(10-69) Page 3 of 3

Limitations and Conditions: (continued from Page 1 of 3)

1. Operation must be in accordance with the applicable Avidyne Corporation Aircraft Flight Manual Supplement (AFMS) referenced on the attached AML, or later FAA-approved revision.

The AFMS must be carried in the aircraft during all flights.

2. Maintenance must be in accordance with the applicable Instructions for Continued Airworthiness (ICA) referenced on the attached AML, or later FAA accepted revision.

The ICA must be made available to the operator at the time of installation.

3. Compatibility of this design with previously approved modifications must be determined by the installer.

Certification Basis:

See attached FAA Approved Model List (AML), Document No. AVIFD-006, Rev 05, or later FAA approved revision for the Certification Basis.

If the holder agrees to permit another person to use this certificate to alter the product, the holder shall give the other person written evidence of that permission.

----------------------------------------------END--------------------------------------------------

### SA00282BO_AML.pdf

Document Number AVIFD-006 Control Category N/A Revision Description ECO Date 08 Update 9.2.4 ECO-11-382 11/17/11 09 Piper PA-32 ECO-12-314 04/04/13 10 Update 9.3 ECO-13-385 06/16/14

AVIDYNE CORPORATION 55 Old Bedford Road Lincoln, MA 01773 Avidyne 700-00083-XXX Integrated Flight Display Approved Model List

AML STC SA00282BO FAA Approved: ___________________________ Manager Boston Aircraft Certification Office Federal Aviation Administration Burlington, MA

Avidyne 700-00083-XXX Approved Model List FAA Approved Date: _____________ Confidential property of Avidyne Corporation AVIFD-006 Not to be disclosed without permission Revision: 10, Dated: 06/16/14 Page 2 of 13 Table of Contents

1. Introduction … 3

2. Log of Revisions … 4

3. Applicability … 5

3.1 IFD Variants … 5

3.2 Control Display Variants … 5

3.3 Aircraft Configuration Module Variants … 5

3.4 Magnetometer/OAT Sensor Variants … 6

4. Certification Basis … 7

5. Approved Model List … 10

Avidyne 700-00083-XXX Approved Model List FAA Approved Date: _____________ Confidential property of Avidyne Corporation AVIFD-006 Not to be disclosed without permission Revision: 10, Dated: 06/16/14 Page 3 of 13

1. Introduction This document is the FAA Approved Model List for STC SA00282BO the installation of the Avidyne 700-00083-XXX Integrated Flight Display System into eligible aircraft. Revisions to the AML must be coordinated through the STC holder, and require FAA approval. Additions to the AML must be made using the IFD AML Model Evaluation Process AVIFD-018.

IMPORTANT NOTICE This STC is only applicable to the 14 CFR Part 23 Class I, II, and III aircraft, as defined in Advisory Circular AC 23.1309-1E, which are listed in this AML.

Installations in 14 CFR Part 23 Class IV, Part 25, Part 27 and Part 29 aircraft are not authorized under this STC.

IMPORTANT NOTICE Separately approved imagery sensors (installed via TC, STC, or field approval) with RS-170 compatible (video) output can be interfaced to the Release 9 IFD System as indicated in the Avidyne IFD Installation Manual, Avidyne Document 600-00160-000.

Avidyne 700-00083-XXX Approved Model List FAA Approved Date: _____________ Confidential property of Avidyne Corporation AVIFD-006 Not to be disclosed without permission Revision: 10, Dated: 06/16/14 Page 4 of 13

2. Log of Revisions

Revision Number Revised Pages Description of Revisions FAA Approval Date 01 ALL Initial Release Robert G. Mann Mgr., Boston ACO APR 24 2009 02 Pg. 6 Revised SR20/22 table Robert G. Mann Mgr., Boston ACO

JUL 15 2009 03 Pg. 3, 5-6, & 8 Updated SR20/22 Models. Added Section 3. Robert G. Mann Mgr., Boston ACO DEC 31 2009 04 Pg. 3, & 7-9 PA-46R-350T Model Addition Robert G. Mann Mgr., Boston ACO OCT 12 2010 05 Pg. 7 & 9-10 Release 9.2 Robert G. Mann Mgr., Boston ACO

FEB 18 2011 06 Pg. 9 & 10 Cirrus EVS Update Robert G. Mann Mgr., Boston ACO

APR 28 2011 07 Pg. 9 & 10 Release 9.2.2 N/A N/A 08 Pg. 9 & 10 Release 9.2.4 Robert G. Mann Mgr., Boston ACO NOV 21 2011 09 Pg. 3 & 7-12 Piper PA-32 Amendment Robert G. Mann Mgr., Boston ACO MAY 02 2013 10 Pg. 10-12 Release 9.3 Robert G. Mann Mgr., Boston ACO

Avidyne 700-00083-XXX Approved Model List FAA Approved Date: _____________ Confidential property of Avidyne Corporation AVIFD-006 Not to be disclosed without permission Revision: 10, Dated: 06/16/14 Page 5 of 13

3. Applicability The following equipment may be installed in aircraft using the installation data listed in the Master Document List, Avidyne document number AVIFD-005.

See Section 5 for approved aircraft.

3.1 IFD Variants The following table lists the 700-00083-XXX variants covered by this AML STC:

Part Number Description 700-00083-000 IFD with the following modules:

MPIO, ACR, ADAHRS, VHF NAV/Com, GPS 700-00083-001 IFD with the following modules:

MPIO, ACR, VHF NAV/Com, GPS Table 1: IFD Variants

3.2 Control Display Variants The following table lists the 700-00150-XXX variants covered by this AML STC:

Part Number Description 700-00150-001 Alphabetic Layout 700-00150-002 QWERTY Layout Table 2: Control Display Variants

3.3 Aircraft Configuration Module Variants The following table lists the 700-00156-XXX variants covered by this AML STC:

Part Number Description 700-00156-000 1 Megabyte/5 Volt Table 3: Aircraft Control Module

Avidyne 700-00083-XXX Approved Model List FAA Approved Date: _____________ Confidential property of Avidyne Corporation AVIFD-006 Not to be disclosed without permission Revision: 10, Dated: 06/16/14 Page 6 of 13

3.4 Magnetometer/OAT Sensor Variants The following table lists the 700-00011-XXX variants covered by this AML STC:

Part Number Description 700-00011-000 Magnetometer/OAT Sensor 700-00011-001 3.38” dia. Magnetometer/OAT Sensor Table 4: Magnetometer/OAT Sensors

Avidyne 700-00083-XXX Approved Model List FAA Approved Date: _____________ Confidential property of Avidyne Corporation AVIFD-006 Not to be disclosed without permission Revision: 10, Dated: 06/16/14 Page 7 of 13

4. Certification Basis Based on 14 CFR § 21.115 and §21.101, and the FAA policy for significant changes in FAA Order 8110.48, the certification basis for installation of this modification in Class I, II, and III aircraft listed in this AML, is the latest amendment of 14 CFR Part 23 subparts and is identified (by model) in the table below:

a. The type certification basis for part not changed or affected by the change is identified in the Type Certificate Data Sheet for each aircraft included in this AML

b. The certification basis for parts changed or affected by the change since the reference date of application, October 17, 2005, is based on 14 CFR Part 23 as amended by amendment 23- 55.

c. The certification basis for parts changed or affected by the change since the reference date of amendment, December 8, 2010, is based on 14 CFR Part 23 as amended by amendment 23- 59.

d. The certification basis for parts changed or affected by the change since the reference date of amendment, December 19, 2011, is based on 14 CFR Part 23 as amended by amendment 23- 61.

Avidyne 700-00083-XXX Approved Model List FAA Approved Date: _____________ Confidential property of Avidyne Corporation AVIFD-006 Not to be disclosed without permission Revision: 10, Dated: 06/16/14 Page 8 of 13

Aircraft Make Aircraft Models TCDS Certification Basis Cirrus Design Corporation

SR20 SR22

A00009CH

Regulations at the latest amendment 23-0 through 23-55:

23.301 [Amdt. 23-48] (a), (b), (c), (d), 23.303 [Amdt. Orig], 23.305 [Amdt. 23-45]

(a), (b), 23.307 [Amdt. Orig] (a), 23.321 [Amdt. 23-45] (a), (b), (c), 23.337 [Amdt.

23-48] (a)(1), (b)(1), 23.341 [Amdt. 23-48] (a), 23.473[Amdt. 23-48] (d), (g),

23.561[Amdt. 23-48] (a), (b)(1), (b)(3), 23.601[Amdt. Orig], 23.603[Amdt. 23-23]

(a)(1), (a)(2), (a)(3), (b), 23.605[Amdt. 23-23] (a), (b), 23.607[Amdt. 23-48] (a), (b),

(c), 23.609 [Amdt. Orig] (a), (b), 23.611[Amdt. 23-48], 23.613[Amdt23-45] (a),

(b)(1), (b),(2), (c), (d), (e), 23.771[Amdt. 23-14] (a), 23.773[Amdt. 23-45] (a)(2),

23.777[Amdt. 23-51] (a), (b), 23.867[Amdt. 23-49] (b)(1), (b)(2), 23.1301[Amdt. 23- 20], 23.1303[Amdt. 23-49] (a), (b), (f), 23.1305[Amdt. 23-52] (a)(2), (a)(3), (b)(2),

(b)(3), (b)(4), (b)(5), b(6), 23.1307[Amdt. 23-49], 23.1309[Amdt. 23-49] a(1), a(2), b(1), b(2), b(3), b(4), (c)(1), (c)(2)(iii), (c)(3), (d), (e), 23.1311[Amdt. 23-49],

23.1321[Amdt. 23-49] (a), (c), (d), (e), 23.1322[Amdt. 23-43], 23.1323[Amdt. 23- 49] (a), (c), 23.1325[Amdt. 23-50] (b)(1), (b)(2), (b)(3), 23.1326(a), (b)(2)[Amdt. 23- 49,] 23.1327[Amdt. 23-20], 23.1329[Amdt 23-49] (e), (f), (g), (h), 23.1331[Amdt.

23-43], 23.1335[Amdt. 23-20], 23.1337[Amdt. 23-51] (a)(1), (a)(2), (c),

23.1351[Amdt. 23-49] (a)(1), (a)(2)(i), (b)(2), (b)(3), (d)(1), (g), 23.1353[Amdt. 23- 49] (a), (d), (e), (h), 23.1357[Amdt. 23-42] (a)(2), (b), (c), (d), 23.1359[Amdt. 23-49]

(c), 23.1365[Amdt. 23-49] (a), (b), (d), (e), (f), 23.1367[Amdt. Orig], 23.1381[Amdt.

Orig] (a), (b), 23.1431[Amdt. 23-49] (a), (b), (d), (e), 23.1501[Amdt. 23-21],

23.1523[Amdt. 23-34], 23.1525[Amdt. 23-45], 23.1529[Amdt. 23-26],

23.1541[Amdt. 23-21] (a), 23.1543[Amdt. 23-50] (b), (c), 23.1545[Amdt. 23-50] (a),

(b)(1), (b)(2), (b)(3), (b)(4), (c), 23.1549[Amdt. 23-45], 23.1555[Amdt. 23-50] (a),

(b), (d), 23.1581[Amdt. 23-50] (a), (b)(2), (b)(3), (f), 23.1583[Amdt. 23-50] (m),

23.1585[Amdt. 23-50] (j) Special condition 23-184A-SC Protection of Systems for High Intensity Radiated Fields (HIRF) Equivalent Level of Safety Findings have been made for 14 CFR §23.1326(b)(1) Pitot Heat Indication Systems, documented in ELOS Memorandum ACE-09-05

Avidyne 700-00083-XXX Approved Model List FAA Approved Date: _____________ Confidential property of Avidyne Corporation AVIFD-006 Not to be disclosed without permission Revision: 10, Dated: 06/16/14 Page 9 of 13 Piper PA-46R-350T A25SO Regulations at the latest amendment 23-0 through 23-59:

23.301 [Amdt. 23-48] (a), (b), (c), (d), 23.303 [Amdt. Orig], 23.305 [Amdt. 23-45]

(a), (b), 23.307 [Amdt. Orig] (a), 23.321 [Amdt. 23-45] (a), (b), (c), 23.337 [Amdt.

23-48] (a)(1), (b)(1), 23.341 [Amdt. 23-48] (a), 23.473[Amdt. 23-48] (d), (g),

23.561[Amdt. 23-48] (a), (b)(1), (b)(3), 23.601[Amdt. Orig], 23.603[Amdt. 23-23]

(a)(1), (a)(2), (a)(3), (b), 23.605[Amdt. 23-23] (a), (b), 23.607[Amdt. 23-48] (a), (b),

(c), 23.609 [Amdt. Orig] (a), (b), 23.611[Amdt. 23-48], 23.613[Amdt23-45] (a),

(b)(1), (b),(2), (c), (d), (e), 23.771[Amdt. 23-14] (a), 23.773[Amdt. 23-45] (a)(2),

23.777[Amdt. 23-51] (a), (b), (g), 23.867[Amdt. 23-49] (b)(1), (b)(2), 23.1301[Amdt.

23-20], 23.1303[Amdt. 23-49] (a), (b), (f), 23.1305[Amdt. 23-52] (a)(1), (a)(2),

(a)(3), (b)(2), (b)(3), (b)(4), (b)(5), b(6), 23.1307[Amdt. 23-49], 23.1309[Amdt. 23- 49] a(1), a(2), b(1), b(2), b(3), b(4), (c)(1), (c)(2)(iii), (c)(3), (d), (e), 23.1311[Amdt.

23-49], 23.1321[Amdt. 23-49] (a), (c), (d), (e), 23.1322[Amdt. 23-43],

23.1323[Amdt. 23-49] (a), (c), 23.1325[Amdt. 23-50] (b)(1), (b)(2), (b)(3),

23.1326(a), (b)(2)[Amdt. 23-49,] 23.1327[Amdt. 23-20], 23.1329[Amdt 23-49] (e),

(f), (g), (h), 23.1331[Amdt. 23-43], 23.1335[Amdt. 23-20], 23.1337[Amdt. 23-51]

(a)(1), (a)(2), (b)(1), (c), 23.1351[Amdt. 23-49] (a)(1), (a)(2)(i), (b)(2), (b)(3), (d)(1),

(g), 23.1353[Amdt. 23-49] (a), (d), (e), (h), 23.1357[Amdt. 23-42] (a)(2), (b), (c),

(d), 23.1359[Amdt. 23-49] (c), 23.1365[Amdt. 23-49] (a), (b), (d), (e), (f),

23.1367[Amdt. Orig], 23.1381[Amdt. Orig] (a), (b), 23.1431[Amdt. 23-49] (a), (b),

(d), (e), 23.1501[Amdt. 23-21], 23.1523[Amdt. 23-34], 23.1525[Amdt. 23-45],

23.1529[Amdt. 23-26], 23.1541[Amdt. 23-21] (a), 23.1543[Amdt. 23-50] (b), (c),

23.1545[Amdt. 23-50] (a), (b)(1), (b)(2), (b)(3), (b)(4), (c), 23.1549[Amdt. 23-45],

23.1555[Amdt. 23-50] (a), (b), (d), 23.1581[Amdt. 23-50] (a), (b)(2), (b)(3), (f),

23.1583[Amdt. 23-50] (m), 23.1585[Amdt. 23-50] (j)

Special condition 23-184A-SC Protection of Systems for High Intensity Radiated Fields (HIRF)

Piper PA-32-301, PA-301FT, PA-32R-301 (SP), PA- 32R-301 (HP), A3SO Regulations at the latest amendment 23-0 through 23-61:

23.301 [Amdt. 23-48] (a), (b), (c), (d); 23.303 [Amdt. Orig], 23.305 [Amdt. 23- 45] (a), (b); 23.307 [Amdt. Orig] (a); 23.321 [Amdt. 23-45] (a), (b), (c);

23.337 [Amdt. 23-48] (a)(1), (b)(1); 23.341 [Amdt. 23-48] (a); 23.473[Amdt. 23-48]

(d), (g); 23.561[Amdt. 23-48] (a), (b)(1), (b)(3); 23.601[Amdt. Orig]; 23.603[Amdt.

23-23] (a)(1), (a)(2), (a)(3), (b); 23.605[Amdt. 23-23] (a), (b); 23.607[Amdt. 23-48]

(a), (b), (c); 23.609 [Amdt. Orig] (a), (b); 23.611[Amdt. 23-48]; 23.613[Amdt23-45]

(a), (b)(1), (b),(2), (c), (d), (e); 23.671[Amdt. Orig]; 23.771[Amdt. 23-14] (a)

23.773[Amdt. 23-45] (a)(2); 23.777[Amdt. 23-51] (a), (b); 23.785[Amdt. 23-49] (e);

23.853 [Amdt. 23-49] (a); 23.867[Amdt. 23-49] (b)(1), (b)(2); 23.1301[Amdt. 23- 20]; 23.1303[Amdt. 23-49] (a), (b), (f); 23.1305[Amdt. 23-52] (a)(1), (a)(2), (a)(3),

(b)(2), (b)(3), (b)(4), (b)(5), b(6); 23.1306[Amdt. 23-61] (b); 23.1307[Amdt. 23-49];

23.1308[Amdt. 23-57] (b); 23.1309[Amdt. 23-49] a(1), a(2), b(1), b(2), b(3), b(4),

(c)(1), (c)(2)(iii), (c)(3), (d), (e); 23.1311[Amdt. 23-49]; 23.1321[Amdt. 23-49] (a),

(c), (d), (e); 23.1322[Amdt. 23-43]; 23.1323[Amdt. 23-49] (a), (c); 23.1325[Amdt.

23-50] (b)(1), (b)(2), (b)(3); 23.1326 [Amdt. 23-49] (PA-32-301FT only);

23.1327[Amdt. 23-20]; 23.1329[Amdt 23-49] (g), (h); 23.1331[Amdt. 23-43];

23.1335[Amdt. 23-20]; 23.1337[Amdt. 23-51] (b)(1), (c); 23.1351[Amdt. 23-49]

(a)(1), (a)(2)(i), (b)(2), (b)(3), (d)(1), (g); 23.1353[Amdt. 23-49] (h); 23.1357[Amdt.

23-43] (a)(2), (b), (c), (d); 23.1359[Amdt. 23-49] (b), (c); 23.1365[Amdt. 23-49] (a),

(b), (d), (e), (f); 23.1367[Amdt. Orig]; 23.1381[Amdt. Orig] (a), (b); 23.1431[Amdt.

23-49] (a), (b), (d), (e); 23.1501[Amdt. 23-21]; 23.1523[Amdt. 23-34];

23.1525[Amdt. 23-45]; 23.1529[Amdt. 23-26]; 23.1541[Amdt. 23-21] (a);

23.1543[Amdt. 23-50] (b), (c); 23.1545[Amdt. 23-50] (a), (b)(1), (b)(2), (b)(3),

(b)(4), (c); 23.1549[Amdt. 23-45]; 23.1553 [Amdt. 23-50]; 23.1555[Amdt. 23-50]

(a), (b), (d); 23.1559 [Amdt. 23-50]; 23.1581[Amdt. 23-50] (a), (b)(2), (b)(3), (f);

23.1583[Amdt. 23-50] (m); 23.1585[Amdt. 23-50] (j)

Avidyne 700-00083-XXX Approved Model List FAA Approved Date: _____________ Confidential property of Avidyne Corporation AVIFD-006 Not to be disclosed without permission Revision: 10, Dated: 06/16/14 Page 10 of 13

5. Approved Model List

Aircraft Make Aircraft Model(s) TCDS Required Approved Data and Additional Model Specific Limitations

Avidyne 700-00083-XXX Approved Model List FAA Approved Date: _____________ Confidential property of Avidyne Corporation AVIFD-006 Not to be disclosed without permission Revision: 10, Dated: 06/16/14 Page 11 of 13 Cirrus Design Corporation

SR20 SR22

A00009CH Master Document List:

AVIFD-005, Rev. 17 (or later approved revisions) 700-00083-XXX Integrated Flight Display AML STC Master Document List STC No. SA00282BO Airplane Flight Manual Supplement:

600-00712-000, Rev. 03 (or later approved revisions) Airplane Flight Manual Supplement for Installation with the 700-00083-XXX Integrated Flight Display Cirrus SR22/20 600-00712-002, Rev. 00 (or later FAA approved revisions) Airplane Flight Manual Supplement for Installation with the 700-00083-XXX Integrated Flight Display Cirrus SR2X, Release 9.3 software (or later) Instructions for Continued Airworthiness:

AVIFD-016, Rev. 09 (or later FAA accepted revisions) 700-00083-XXX Integrated Flight Display Instructions for Continued Airworthiness Additional Limitations:

Equipment Limitations:

All Installations must have Integrated Flight Displays with ACR software, Release 9.0.X, P/N 530-00206-XXX, Release 9.1.X, P/N 530-00218- XXX, or Release 9.2.X, P/N 530-00220-XXX, Release 9.3, P/N 530- 00221-XXX (or later) software installed. (Reference the IFD System Page, Setup Tab for Software Part Number) Installations interfacing to an Avidyne DFC100 Autopilot (STC SA00296BO) requires both Integrated Flight Displays to have ACR software, Release 9.2.X, P/N 530-00220-XXX installed. (Reference the IFD System Page, Setup Tab for Software Part Number) Enabling Enhanced Vision System (EVS) functionality requires STC SA02329AK configuration.

Installations using Synthetic Vision System on the Integrated Flight Display System must have an ACR with the following part numbers:

Hardware P/N: 710-00110-001 Software P/N: 530-00221-000 If a Terrain Awareness System as defined by TSO-C151 (TAWS-B, EGPWS) is installed in the airplane then the configuration for 9.3 must reflect that an existing terrain alerting system is installed. This selection will inhibit forward looking terrain alerting (FLTA) features of 9.3 that may conflict with existing approved terrain alerting systems.

Aircraft Serial Number Limitations:

Applicable to SR20: s/n 1005 and up Applicable to SR22: s/n 0002 and up Applicable to SR22 when modified by Tornado Alley Turbo STC SA10588SC (ref s/n limitation above)

Avidyne 700-00083-XXX Approved Model List FAA Approved Date: _____________ Confidential property of Avidyne Corporation AVIFD-006 Not to be disclosed without permission Revision: 10, Dated: 06/16/14 Page 12 of 13 Piper PA-46R- 350T A25SO Master Document List:

AVIFD-005, Rev. 17 (or later approved revisions) 700-00083-XXX Integrated Flight Display AML STC Master Document List STC No. SA00282BO Airplane Flight Manual Supplement:

600-00263-000, Rev. 00 (or later FAA approved revisions) Airplane Flight Manual Supplement for Installation with the 700-00083-XXX Integrated Flight Display Piper PA-46R-350T 600-00263-002, Rev. 00 (or later approved revisions) Airplane Flight Manual Supplement for Installation with the 700-00083-XXX Integrated Flight Display Cirrus SR2X, Release 9.3 software (or later)

Instructions for Continued Airworthiness:

AVIFD-016, Rev. 09 (or later FAA accepted revisions) 700-00083-XXX Integrated Flight Display Instructions for Continued Airworthiness Additional Limitations:

Equipment Limitations:

All Installations must have Integrated Flight Displays with ACR software, Release 9.1.X, P/N 530-00218-XXX, or Release 9.2.X, P/N 530-00220-XXX, Release 9.3, P/N 530-00221-XXX (or later), software installed. (Reference the IFD System Page, Setup Tab for Software Part Number)

Installations interfacing to an Avidyne DFC100 Autopilot (STC SA00310BO) requires both Integrated Flight Displays to have ACR software, Release 9.2.1 (or later), P/N 530-00220-XXX installed.

(Reference the IFD System Page, Setup Tab for Software Part Number) Installations using Synthetic Vision System (SVS) on the Integrated Flight Display System must have an ACR with the following part numbers:

Hardware P/N: 710-00110-001 (or later) Software P/N: 530-00221-000 (or later) If a Terrain Awareness System as defined by TSO-C151 (TAWS-B, EGPWS) is installed in the airplane then the configuration for 9.3 must reflect that an existing terrain alerting system is installed. This selection will inhibit forward looking terrain alerting (FLTA) features of 9.3 that may conflict with existing approved terrain alerting systems.

Aircraft Serial Number Limitations:

PA-46R-350T: Installations on Avidyne PFD equipped airplanes only.

Avidyne 700-00083-XXX Approved Model List FAA Approved Date: _____________ Confidential property of Avidyne Corporation AVIFD-006 Not to be disclosed without permission Revision: 10, Dated: 06/16/14 Page 13 of 13 Piper PA-32- 301, PA- 301FT, PA-32R- 301 (SP), PA-32R- 301 (HP) A3SO Master Document List:

AVIFD-005, Rev. 17 (or later approved revisions) 700-00083-XXX Integrated Flight Display AML STC Master Document List STC No. SA00282BO Airplane Flight Manual Supplement:

600-00289-000, Rev. 00 (or later FAA approved revisions) Airplane Flight Manual Supplement for Installation with the 700-00083-XXX Integrated Flight Display Piper PA-32 600-00289-001, Rev. 00 (or later approved revisions) Airplane Flight Manual Supplement for Installation with the 700-00083-XXX Integrated Flight Display PA-32, Release 9.3 software (or later)

Instructions for Continued Airworthiness:

AVIFD-016, Rev. 09 (or later FAA accepted revisions) 700-00083-XXX Integrated Flight Display Instructions for Continued Airworthiness Additional Limitations:

Equipment Limitations:

All Installations must have Integrated Flight Displays with ACR software, Release 9.2.X, P/N 530-00220-XXX or Release 9.3, 530- 00221-000 (or later) software installed. (Reference the IFD System Page, Setup Tab for Software Part Number) Installations using Synthetic Vision System on the Integrated Flight Display System must have an ACR with the following part numbers:

Hardware P/N: 710-00110-001 (or later) Software P/N: 530-00221-000 (or later) If a Terrain Awareness System as defined by TSO-C151 (TAWS-B, EGPWS) is installed in the airplane then the configuration for 9.3 must reflect that an existing terrain alerting system is installed. This selection will inhibit forward looking terrain alerting (FLTA) features of 9.3 that may conflict with existing approved terrain alerting systems.

Aircraft Serial Number Limitations:

PA-32-301: 32-8006002 - 32-8606023, 3206001 - 3206019, 3206042 - 32060444, 3206047, 3206050 - 3206055, 3206060.

PA-32-301FT: 3232001 and up (28V) PA-32R-301 (SP): 32R-8013001 - 32R-8613006, 3213001 - 3213028, 3213030 – 3213041 PA-32R-301 (HP): 3213029, 3213042 - 3213103, 3246001 – 3246017 PA-32R-301 (HP): 3246018 and up (28v)

## Every issue (5)

- June 16, 2014: Amended, Current. [certificate](https://openairdocs.org/files/sha256/eb/83/eb831180547482a2f53e8a87458dc3cbd622a72c3165955cdda6ff27a3517023), [SA00282BO_AML.pdf](https://openairdocs.org/files/sha256/f3/65/f3654ee09730645e4ece13772fb00095c1d1e2a2b07218daacd45c3825c45ead)
- April 4, 2013: Amended, Historical. [certificate](https://openairdocs.org/files/sha256/eb/83/eb831180547482a2f53e8a87458dc3cbd622a72c3165955cdda6ff27a3517023), [AML_SA00282BO.pdf](https://openairdocs.org/files/sha256/3d/c5/3dc58d73afe8c51827e9955d3cde44bb2fe1a4ec134b567a07ecd28e34a4d172)
- February 18, 2011: Amended, Historical. [certificate](https://openairdocs.org/files/sha256/eb/83/eb831180547482a2f53e8a87458dc3cbd622a72c3165955cdda6ff27a3517023), [SA00282BO AML.pdf](https://openairdocs.org/files/sha256/d6/3c/d63c149ad35cfa6b859df61b583cd81313c556e4b52aa3e1d3cd26d315500889)
- October 12, 2010: Amended, Historical. [certificate](https://openairdocs.org/files/sha256/8a/06/8a0630df5b276104484b10d098c457352f14e22a1a66aec95306e8b1bf0b5311), [SA00282BO AML.pdf](https://openairdocs.org/files/sha256/d6/3c/d63c149ad35cfa6b859df61b583cd81313c556e4b52aa3e1d3cd26d315500889)
- April 24, 2009: Issued, Historical. [certificate](https://openairdocs.org/files/sha256/17/da/17da08d7f5edf254b59c2c50cb632765fbd597e5e5cc7b5e37637c0b9674e262), [SA00282BO AML.pdf](https://openairdocs.org/files/sha256/f6/e3/f6e3feb9be9c02a4e18559f3baee310a5d5f9d1db4e9c21b3a3c98c5c33e47d3)

---
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.