What it approves
Installation of Dual (forward/aft) Belly Mounted Retractable Turret Provisions
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.
United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate SA00897DE Number:
This certificate issued to: Paravion Technology, Inc.
2001 Airway Ave.
Fort Collins, CO 80524 BB__.
Make: Textron Aviation Inc. Original Product A37CE 7\SH&HUWLILFDWH1XPEHU Model: 208B Description of Type Design Change:
Installation of Dual (forward/aft) Belly Mounted Retractable Turret Provisions in accordance with Doc No.
DL-C208RT-100, Master Drawing List, Rev. J dated 11/6/2020, FAA approved 3/8/2021 or later FAA approved revisions. Doc No. PR-C208RT-120M, Instructions for Continued Airworthiness (ICA), Rev. B dated 10/1/2020, FAA accepted 3/4/2021 or later FAA accepted revision are required to be made available at installation.
Continued Page 3 of 4 Limitations and Conditions:
1. This STC is applicable to all serial numbers for the Textron Aviation Inc. 208B Continued Page 3 of 4
February 9, 2021 Date of Application: Date Reissued:
March 17, 2021 Date of Issuance: Date Amended:
Kreg R. Voorhies, ODA Lead administrator Cert Works, LLC ODA Title: ODA No. ODA(AIR)-833887-NM $Q\DOWHUDWLRQRIWKLVFHUWLILFDWHLVSXQLVKDEOHE\DILQHRIQRWH[FHHGLQJRULPSULVRQPHQWQRWH[FHHGLQJ\HDUVRUERWK7KLVFHUWLILFDWHPD\EHWUDQVIHUUHGRUPDGH DYDLODEOHWRWKLUGSHUVRQVE\OLFHQVLQJDJUHHPHQWVLQDFFRUGDQFHZLWK&)53RVVHVVLRQRIWKLV6XSSOHPHQWDO7\SH&HUWLILFDWH 67& GRFXPHQWE\SHUVRQVRWKHUWKDQ WKH67&KROGHUGRHVQRWFRQVWLWXWHULJKWVWRWKHGHVLJQGDWDQRUWRDOWHUDQDLUFUDIWDLUFUDIWHQJLQHRUSURSHOOHU7KH67&¶VVXSSRUWLQJGRFXPHQWDWLRQ GUDZLQJVLQVWUXFWLRQV SURSHOOHUPXVWSURYLGHWKDWSHUVRQZLWKZULWWHQSHUPLVVLRQDFFHSWDEOHWRWKH)$$ 5HI&)5 )$$)RUP 683(56('(635(9,286(',7,21 3DJHRIBBB 4
United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate SA00897DE Number:
Date oI transfer:
$Q\DOWHUDWLRQRIWKLVFHUWLILFDWHLVSXQLVKDEOHE\DILQHRIQRWH[FHHGLQJRULPSULVRQPHQWQRWH[FHHGLQJ\HDUVRUERWK7KLVFHUWLILFDWHPD\EHWUDQVIHUUHGRUPDGH DYDLODEOHWRWKLUGSHUVRQVE\OLFHQVLQJDJUHHPHQWVLQDFFRUGDQFHZLWK&)53RVVHVVLRQRIWKLV6XSSOHPHQWDO7\SH&HUWLILFDWH 67& GRFXPHQWE\SHUVRQVRWKHUWKDQ WKH67&KROGHUGRHVQRWFRQVWLWXWHULJKWVWRWKHGHVLJQGDWDQRUWRDOWHUDQDLUFUDIWDLUFUDIWHQJLQHRUSURSHOOHU7KH67&’s supporting documentation (drawings, instructions, SURSHOOHUPXVWSURYLGHWKDWSHUVRQZLWKZULWWHQSHUPLVVLRQDFFHSWDEOHWRWKH)$$ 5HI&)5 )$$)RUP 683(56('(635(9,286(',7,21 3DJHRIBBB 4
United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate (Continuation Sheet) Number: SA00897DE Description Continued:
Document No. PR-C208RT-100M, FAA Approved Airplane Flight Manual Supplement (AFMS), Revision 2 dated 2/23/2021, FAA approved 3/8/2021 or later FAA approved revision is required for this installation.
2. The installer must determine whether this design change is compatible with previously approved modifications.
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 FAA has not certified the equipment for which these provisions are intended. Additional FAA approval is required to install equipment. The FAA must evaluate the installation to ensure it complies with the applicable airworthiness standards.
5. Flight into Known Icing or forecast icing conditions with payload exposed outside of the cargo pod profile is prohibited.
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 the Dual (forward/aft) Belly Mounted Retractable Turret Provisions in Textron Aviation Inc. 208B is as follows:
a. The type certification basis for Textron Aviation Inc. 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, 2/9/2021, is based upon 14 CFR Part 23, effective February 1, 1965 plus Amendments 23-1 through 23-28. 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 latest amendment; None Regulations at an intermediate amendment; None Continued Sheet 4 of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
United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate (Continuation Sheet) Number: SA00897DE Certification Basis Continued Regulations at the amendment level in TCDS A37CE;
14 CFR Sections: 21.93(b) Amdt. 21-81; 23.23 Amdt. 23-17; 23.29 Amdt. 23-21; 23.49(a),(b)(1),(c-d),(e)
(2) Amdt. 23-21; 23.51(a),(c)(2),(e) Amdt. 23-21; 23.65(a,c) Amdt. 23-21; 23.77 Amdt. 23-21; 23.141 Amdt. 23-17; 23.143 Amdt. 23-17; 23.153 Amdt. 23-14; 23.161 Amdt. 23-21; 23.171 Amdt. - ; 23.173 Amdt. 23-14; 23.175(a,b,d) Amdt. 23-21; 23.177(a,b) Amdt. 23-21; 23.181 Amdt. 23-21; 23.201 Amdt.
23-14; 23.203 Amdt. 23-14; 23.207 Amdt. 23-7; 23.251 Amdt. - ; 23.253 Amdt. 23-26; 23.301(a-c) Amdt.
23-28; 23.303 Amdt. - ; 23.305(a,b) Amdt. - ; 23.307(a) Amdt. - ; 23.321 Amdt. - ; 23.333(a-c) Amdt.
23-7; 23.337(a)(1),(b)(1) Amdt. 23-7; 23.341 Amdt. 23-7; 23.471 Amdt. - ; 23.473(a,d,g) Amdt. 23-28;
23.561(a,b,e) Amdt. 23-7; 23.601 Amdt. - ; 23.603 Amdt. 23-23; 23.605(a) Amdt. 23-23; 23.607 Amdt.
23-17; 23.609 Amdt. - ; 23.611 Amdt. 23-7; 23.613 Amdt. 23-23; 23.619 Amdt. 23-7; 23.623(a) Amdt.
23-7; 23.625(a) Amdt. 23-7; 23.771(a) Amdt. 23-14; 23.773(a)(1,2) Amdt. 23-45; 23.777(a,b) Amdt.
23-51; 23.831 Amdt. - ; 23.853(a) Amdt. 23-25; 23.863(a,b,d) Amdt. 23-23; 23.867 Amdt. 23-7; 23.1301 Amdt. 23-20; 23.1309(a)(c) Amdt. 23-17; 23.1322 Amdt. 23-43; 23.1351(a),(b)(1)(2) Amdt. 23-20;
23.1353(a-e) Amdt. 23-21; 23.1357(a-d) Amdt. 23-20; 23.1365(a,b) Amdt. 23-14; 23.1367 Amdt. - ;
23.1419(b) Amdt. 23-14; 23.1435(a,b) Amdt. 23-14; 23.1438 Amdt. 23-20; 23.1501 Amdt. 23-21;
23.1529 Amdt. 23-26; 23.1541(a,b) Amdt. 23-21; 23.1555(a),(b) Amdt. 23-21; 23.1557(a) Amdt. 23-23;
23.1581(a,b,d) Amdt. 23-21; 23.1583 Amdt. 23-7; 23.1585(a) Amdt. 23-23 End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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 |
|---|---|---|
| Textron Aviation Inc. | 208B | A37CE |