STC SA10822SC

SA10822SC * Part 23 Regulations Aspen Avionics, Inc.

5001 Indian School Rd. NE Albuquerque, NM 87110 [*See attached FAA Approved Model List (AML)] [*See attached FAA Approved Model List (AML)]

1. Installation of EFD1000 Primary Flight Display in accordance with Aspen Avionics Installation Manual document #A-01-126-00, Revision C, dated 3/28/2008, or later approved FAA revision. Airplane Flight Manual Supplement document #A-01-175-00, Revision B, dated 3/17/2008 or document #A-01-179-00, Revision A, dated 3/17/2008, or later FAA approved revision is required.

(Continued on Page 3 of 7)

1) The installer must determine whether this design change is compatible with previously approved modification.

2) 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.

3) Activation of the Angle of Attack (AOA) indication is only permitted for airplanes with flaps.

4) Installation of EFD1000 E5 system is approved for Class I and II airplanes only.

June 22, 2007 March 28, 2008 April 18, 2008 February 13, 2009;

September 29, 2009 Rev. 2; July 17, 2015;

December 7, 2018; June 28, 2019; July 15, 2021 Jim Grigg Manager, Fort Worth ACO Branch Compliance and Airworthiness Division Aircraft Certification Service

SA10822SC

FAA Form 8110-2 (03/21) Page 3 of 7 United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate Number SA10822SC:

Description of Type Design Change (Continued):

2. Installation of EFD1000/EFD500 Evolution Flight Display(s) System in accordance with Aspen Avionics Installation Manual document #900-00003-001, Revision D, dated September 28, 2009, or later approved FAA revision, and installation of the EWR50 Datalink Receiver component of the EFD1000/500 Evolution Flight Display(s) System in accordance with Aspen Avionics EWR50 Installation Manual document #900-00007-001, Revision C, dated September 28, 2009, or later approved FAA revision. Airplane Flight Manual Supplement document #900-00008-001, Revision A, dated September 28, 2009, or later FAA approved revision is required.

3. Installation of EFD1000 E5 system in accordance with Aspen Avionics Installation Manual document #900-00041-001, Revision C, dated December 5, 2018 or later approved FAA revision, and in accordance with Master Drawing List #033-00017-001, Revision C, released date December 4, 2018, or later approved FAA revision. Airplane Flight Manual Supplement document #900-00038-001, Revision D, dated December 10, 2018, or later FAA approved revision is required.

Certification Basis:

1. For the installations described in above description 1 and 2:

EFD1000/500 Software versions prior to 2.10 - High Intensity Radiated Fields (HIRF), Docket No. CE278, Special Condition 23-218-SC, Equivalent Level of Safety Memo# ACE-09-15 and 14 CFR Part 23 as follows:

§23.305(a)(b) 23-45 §23.307(a) 23-Original §23.561(b3) 23-48 §23.601 23-Original §23.603(a) 23-23 §23.605(a) 23-23 §23.609(a) 23-Original §23.611 23-48 §23.613(a)(b)(c) 23-45 §23.671(a)(b) 23-Original §23.771(a) 23-14 §23.773(a2) 23-45C §23.777(a)(b) 23-51 §23.867(a)(b) 23-49 §23.1301 23-20 (Continued on Page 4 of 7)

FAA Form 8110-2 (03/21) Page 4 of 7 United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate Number SA10822SC:

Certification Basis (Continued):

§23.1303(f) 23-49 §23.1309(a1)(a2)(a3) 23-49 §23.1309(b)(b1)(b2)(b3)(b4)(c)(d)(e) 23-49 §23.1311(a1)(a2)(a3)(a5)(a6)(a7)(b) 23-49 §23.1321(a)(c)(d)(e) 23-49 §23.1322(a)(b)(c)(d)(e) 23-43 §23.1323(a) 23-49 §23.1327(a) 23-20 §23.1331(a) 23-43 §23.1351(a) 23-49 §23.1353(a)(b)(c)(d)(e)(h) 23-49 §23.1357(a)(b)(c)(d) 23-43 §23.1359(c) 23-43 §23.1365(a)(b)(d)(e) 23-43 §23.1367 (a)(b)(c)(d) 23-Original §23.1381(a)(b) 23-Original §23.1431(a)(b) 23-49 §23.1501 23-21 §23.1525 23-45 §23.1529 23-26 §23.1541(a1)(b1) 23-21 §23.1543 (b)(c) 23-50 §23.1545(a)(b) 23-50 §23.1555(e2) 23-50 §23.1581(a)(b2)(c)(f) 23-50 §23.1583(m) 23-50 §23.1585(j) 23-50 EFD1000/500 Software version 2.10 and subsequent FAA approved version - High Intensity Radiated Fields (HIRF), Docket No. CE278, Special Condition 23-218-SC, Equivalent Level of Safety Memo # ACE-09-15, Equivalent Level of Safety Memos # ACE-09-15, Equivalent Level of Safety Memos # SA02949A-A-S-1 and 14 CRF Part 23 as follows:

§23.305(a)(b) 23-45 §23.307(a) 23-Original §23.561(b3) 23-48 §23.601 23-Original §23.603(a) 23-23 §23.605(a) 23-23 §23.609(a) 23-Original (Continued on Page 5 of 7)

FAA Form 8110-2 (03/21) Page 5 of 7 United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate Number SA10822SC:

Certification Basis (Continued):

§23.611 23-48 §23.613(a)(b)(c) 23-45 §23.671(a)(b) 23-Original §23.771(a) 23-14 §23.773(a2) 23-45C §23.777(a)(b) 23-51 §23.853 23-49 §23.863 23-34 §23.867(a)(b) 23-49 §23.1301 23-20 §23.1303(f) 23-49 §23.1306 23-61 §23.1308 23-57 §23.1309(a1)(a2)(a3) 23-49 §23.1309(b)(b1)(b2)(b3)(b4)(c)(d)(e) 23-49 §23.1311(a)(a1)(a2)(a3)(a4)(a5)(a6)(a7)(b)(c) 23-62 §23.1321(a)(c)(d)(e) 23-49 §23.1322(a)(b)(c)(d)(e) 23-43 §23.1323(a) 23-49 §23.1327(a) 23-20 §23.1331(a) 23-43 §23.1351(a) 23-49 §23.1353(a)(b)(c)(d)(e)(h) 23-49 §23.1357(a)(b)(c)(d) 23-43 §23.1359(c) 23-43 §23.1365(a)(b)(d)(e) 23-43 §23.1367 (a)(b)(c)(d) 23-Original §23.1381(a)(b) 23-Original §23.1431(a)(b) 23-49 §23.1501 23-21 §23.1525 23-45 §23.1529 23-26 §23.1541(a1)(b1) 23-21 §23.1543 (b)(c) 23-50 §23.1545(a)(b) 23-50 §23.1555(e2) 23-50 §23.1581(a)(b2)(c)(f) 23-50 §23.1583(m) 23-50 §23.1585(j) 23-50 (Continued on Page 6 of 7)

FAA Form 8110-2 (03/21) Page 6 of 7 United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate Number SA10822SC:

Certification Basis (Continued):

3. For the installation described in above description 3: Equivalent Level of Safety Memo #SA02680AC-A-S-1 and 14 CFR Part 23 as follows:

§23.305(a)(b) 23-45 §23.307(a) 23-Original §23.561(b3) 23-48 §23.601 23-Original §23.603(a) 23-23 §23.605(a) 23-23 §23.609(a) 23-Original §23.611 23-48 §23.613(a)(b)(c) 23-45 §23.671(a)(b) 23-Original §23.771(a) 23-14 §23.773(a2) 23-45C §23.777(a)(b) 23-51 §23.853 23-49 §23.867(a)(b) 23-49 §23.1301(a)(b)(c)(d) 23-20 §23.1303(f) 23-49 §23.1306 23-61 §23.1308 23-57 §23.1309(a1)(a2)(a3) 23-49 §23.1309(b)(b1)(b2)(b3)(b4)(c)(d)(e) 23-49 §23.1311(a1)(a2)(a3)(a5)(a6)(a7)(b) 23-49 §23.1321(a)(c)(d)(e) 23-49 §23.1322(a)(b)(c)(d)(e) 23-43 §23.1323(a) 23-49 §23.1327(a) 23-20 §23.1331(a) 23-43 §23.1351(a) 23-49 §23.1353(a)(b)(c)(d)(e)(h) 23-49 §23.1357(a)(b)(c)(d) 23-43 §23.1359(c) 23-43 §23.1365(a)(b)(d)(e) 23-43 §23.1367 (a)(b)(c)(d) 23-Original §23.1381(a)(b) 23-Original §23.1431(a)(b) 23-49 §23.1501 23-21 (Continued on Page 7 of 7)

FAA Form 8110-2 (03/21) Page 7 of 7 United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate Number SA10822SC:

Certification Basis (Continued):

§23.1529 23-26 §23.1541(a1)(b1) 23-21 §23.1543 (b)(c) 23-50 §23.1545(a)(b) 23-50 §23.1525 23-45 §23.1555(e2) 23-50 §23.1581(a)(b2)(c)(f) 23-50 §23.1583(m) 23-50 §23.1585(j) 23-50 ----------END----------