What it approves
Installation of a RF Transparent Pod
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 Regulations. (See Page 3 for complete certification basis)
Installation of a RF Transparent Pod in accordance with Standard Aero Master Data List 1021054, Revision (D), dated October 25, 2012 or later FAA approved revision.
1. The installer must determine whether this design change is compatible with previously approved modifications.
2. Airworthiness Limitations specified in Standard Aero document 1023504, Rev. (B) dated October 24, 2012, or later FAA approved revision, must be complied with in addition to the basic airplane maintenance manuals.
3. 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.
DS Technologies, LLC
D/B/A DST 18223 Air Park Road Hagerstown, MD 21742 A37CE Make: Cessna Aircraft Company Model: 208B
Date of application : November 03, 2011
Date of issuance: October 30, 2012 Date reissued : :December 19, 2012
Date amended
( Signature) Steven L. Lardinois Manager, Systems and Flight Test Branch Chicago Aircraft Certification Office
( Title)
Number SA03041CH-D Date of reissue: December 19, 2012
Certification Basis (continued)
Based on 14 CFR §§ 21.15, 21.101 and the FAA policy for significant changes in FAA Order 8110.48, the certification basis for the Cessna Aircraft Company 208B Installation of a RF Transparent Pod is as follows:
a. The type certification basis for Cessna Aircraft Company 208B is shown on TCDS A37CE for parts not changed or not affected by the change.
b. The certification basis for parts changed or affected by the change since the reference date of application, November 03, 2011, is based upon Amendment 23-61 of 14 CFR Part 23. 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 this modification was determined to be:
Regulations at the amendment level 23-61
23.1(a, b)(23-34), 23.251(23-45), 23.301(a-c)(23-48), 23.303(Original), 23.305(a, b)(23-45),
23.307(a)(Original), 23.321(a-c)(23-45), 23.331(a-c)(23-42), 23.333(a-d)(23-34), 23.335(a-c)(23-48),
23.337(a(1), b(1))(23-48), 23.341(a-c)(23-48), 23.347(a)(23-48), 23.349(a, b)(23-48), 23.351(23-42),
23.421(a, b)(23-42), 23.423(a, b)(23-42), 23.425(a-d)(23-42), 23.427(a-c)(23-42), 23.441(a-c)(23-48),
23.443(a-c)(23-48), 23.471(Original), 23.473(a-g)(23-48), 23.477(Original), 23.601(Original), 23.603(a,
b)(23-23), 23.605(a, b)(23-23), 23.607(a-c)(23-48), 23.609(a, b)(Original), 23.611(23-48), 23.613(a-e)(23-
45), 23.619(23-7), 23.625(a-c)(23-7), 23.627(Original), 23.867(a, c)(23-49), 23.901(b)(23-53), 23.999(a,
b)(23-43), 23.1519(Original), 23.1529(23-26)
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ADs that name this STC · 0
An AD can apply because an STC is installed, or mention one in its text.
Approved models · 1
| Make | Model | Data sheet |
|---|---|---|
| Cessna Aircraft Company | 208B | A37CE |
Every issue · 2
DRS keeps each issue of an STC as its own record, with its own certificate and attachments.
| Date | Status | Files |
|---|---|---|
| December 19, 2012 | Reissued, current | Certificate |
| October 30, 2012 | Issued, earlier issue | Certificate |