What it approves
Installation of the Mid-Continent MD302 Electronic Standby Indicator
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.
Part 23 of the Federal Aviation R egulations . See Type Certificate Data Sheet A24CE for complete certification basis.
Original Product --Type Certificate N umber :
Installation of the Mid-Continent MD302 Electronic Standby Indicator in accordance with Elliott Aviation Master Data List MDL- 3300-466, Revision C, dated December 17, 2013, or later FAA approved revision.
1) The installer must determine whether this design change is compatible with previously approved modifications.
2) FAA Approved Airplane Flight Manual Supplement for the Mid-Continent MD302 Electronic Standby Indicator document number FMS-3300-466, Revision IR, FAA approved January 13, 2014, or later FAA approved revision is a required part of this modification.
3) FAA Accepted Instructions for Continued Airworthiness, Elliott Aviation document ICA-3300-466, revision C, dated December 17, 2013, or later FAA accepted revision is required for this modification.
4) If the holder agrees to permit another person to use this certificate to alter the product, the holder must give the other person written evidence of that permission.
Elliott Aviation Technical Products, Inc.
Quad City International Airport P.O. Box 100 Moline, IL 61266 A24CE M ake : Hawker Beechcraft M odel : 200, 200C, B200, B200C, 300, B300 and B300C Date of application : February 8, 2012
Date of issuance : January 13, 2014
B y direction of the A dministrator
(Signature) Steven L. Lardinois Manager, Systems and Flight Test Branch Chicago Aircraft Certification Office
(Title)
United States of America Department of Transportation - Federal Aviation Administration Supplemental Type Certificate (Continuation Sheet) N umber SA03289CH Date of Issuance: January 13, 2014
FAA FORM 8110-2-1(10-69) PAGE 3 of 3 PAGES
Certification Basis:
The certification basis for the changed Hawker Beechcraft 200, 200C, B200, B200C, 300, B300 and B300C as described in this certificate is as follows:
a. The type certification basis for the Hawker Beechcraft 200, 200C, B200, B200C, 300, B300 and B300C, is shown on TCDS A24CE for parts not changed or not affected by this change.
b. The certification basis for parts changed or affected by this change since the reference date of application, February 8, 2012, is shown in TCDS A24CE and the following regulations:
Regulations at the latest amendment 23-0 through 23-62
23.301 (a); 23.303; 23.305 (a),(b); 23.307(a); 23.601; 23.603; 23.605(a); 23.609; 23.611; 23.613;
23.1301(a),(b),(c),(d); 23.1303(a),(b); 23.1306(a); 23.1308(a); 23.1309(a),(b),(c),(d),(e),(f); 23.1311(a)(5);
23.1321 (a),(c),(d),(e); 23.1322; 23.1323(a); 23.1325; 23.1331; 23.1351(a)(2);
23.1353(a),(b)(2),(c),(d),(e),(h); 23.1357 (a),(b),(c),(d); 23.1359; 23.1381; 23.1431 (a),(b); 23.1529;
23.1545(d); 23.1581; 23.1585
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