What it approves
Installation of Structural OML 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 SA02001WINumber:
This certificate issued to: AIRtec Inc.
46610 Expedition Drive, Suite 100 Lexington Park, MD 20653 BB__.
Make:Original Product A24CE 7\SH&HUWLILFDWH1XPEHU Textron Aviation (Beechcraft) B200GTModel:
Installation of Structural OML Provisions. Data required:
1. Master Data List, No. 22-020-DC4301 Rev. 0, FAA Approved February 8, 2023, or later FAA approved revision;
2. Airplane Flight Manual Supplement, No. 20-022-FT2901, Rev. IR, FAA Approved January 10, 2023, or later FAA approved revision.
1. The installer must determine whether this design change is compatible with previously approved modifications.
2. This STC is applicable to serial numbers: BY-207, BY-239, BY-250 and On.
May 14, 2021Date of Application: Date Reissued:
February 8, 2023Date of Issuance: Date Amended:
Kathryn Oatman Aeronautix Project ODA Administrator Title: ODA-834865-CE $Q\DOWHUDWLRQRIWKLVFHUWLILFDWHLVSXQLVKDEOHE\D ILQHRIQRWH[FHHGLQJRULPSULVRQPHQWQRWH[FHHGLQJ\HDUVRUERWK7KLVFHUWLILFDWHPD\EHWUDQVIHUUHGRUPDGH DYDLODEOHWRWKLUGSHUVRQVE\OLFHQVLQJDJUHHPHQWVLQDFFRUGDQFHZLWK&)53RVVHVVLRQRIWKLV6XSSOHPHQWDO7\SH&HUWLILFDWH 67& GRFXPHQWE\SHUVRQVRWKHUWKDQ WKH67&KROGHUGRHVQRWFRQVWLWXWHULJKWVWRWKHGHVLJQGDWDQRUWRDOWHUDQDLUFUDIWDLUFUDIWHQJLQHRUSURSHOOHU7KH67&¶VVXSSRUWLQJGRFXPHQWDWLRQ GUDZLQJVLQVWUXFWLRQV SURSHOOHUPXVWSURYLGHWKDWSHUVRQZLWKZULWWHQSHUPLVVLRQDFFHSWDEOHWRWKH)$$ 5HI&)5 )$$)RUP 3DJH RIBBB 4
I o United States of America Department of Transportation Federal AviationAdministration Supplemental Type Certificate SA02001WINumber:
Date oI transfer:
$Q\DOWHUDWLRQRIWKLVFHUWLILFDWHLVSXQLVKDEOHE\D ILQHRIQRWH[FHHGLQJRULPSULVRQPHQWQRWH[FHHGLQJ\HDUVRUERWK7KLVFHUWLILFDWHPD\EHWUDQVIHUUHGRUPDGH DYDLODEOHWRWKLUGSHUVRQVE\OLFHQVLQJDJUHHPHQWVLQDFFRUGDQFHZLWK&)53RVVHVVLRQRIWKLV6XSSOHPHQWDO7\SH&HUWLILFDWH 67& GRFXPHQWE\SHUVRQVRWKHUWKDQ WKH67&KROGHUGRHVQRWFRQVWLWXWHULJKWVWRWKHGHVLJQGDWDQRUWRDOWHUDQDLUFUDIWDLUFUDIWHQJLQHRUSURSHOOHU7KH67&’s supporting documentation (drawings, instructions, SURSHOOHUPXVWSURYLGHWKDWSHUVRQZLWKZULWWHQSHUPLVVLRQDFFHSWDEOHWRWKH)$$ 5HI&)5 )$$)RUP 3DJH RIBBB 4
United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate (Continuation Sheet) SA02001WINumber:
Issuance Date: February 8, 2023 Limitations and Conditions (continued from Page 1):
3. This STC includes the following prerequisite installations:
A. CenTex Aerospace STC SA11103SC.
B. BLR Aerospace STC SA02131SE. This STC includes the following prerequisite installations:
I. BLR Aerospace STC SA01615SE.
II. Raisbeck Engineering STC SA3366NM.
III. Textron Aviation STC SA02130SE.
C. Raisbeck Engineering STC SA3591NM.
D. Rockwell Collins Pro Line Fusion
4. The following BLR Aerospace UPP items are not included in this STC:
A. High Flotation Landing Gear B. High Altitude / Operations from Airports above 10,000 ft
5. This approval is limited to only the structural provisions for the belly mounted special mission equipment and belly mounted turret sensor shape. The FAA has not certified the equipment for which these provisions are intended. You must get additional FAA approval to install this equipment.
Certification Basis (continued from page 1):
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 change is as follows:
a. The certification basis for parts not changed or not affected by this change is shown on TCDS A24CE.
b. The certification basis for parts changed or affected by the change is as follows:
Section Amendment Section Amendment
23.1 23-34 23.143 23-50
23.21 23-0 23.145 23-50
23.29 23.21 23.147 23-50
23.45(a)(b)(1)(3)(d)(e)(f) 23-50 23.149(a)(b)(c)(d)(e) 23-50
(g)(h)(1)(2)(3)(4)(5) 23.153 23-50
23.49(a)(2)(3)(4)(5)(6)(b) 23-50 23.155(a)(1)(b)(c) 23-50
23.51(c) 23-50 23.161(a)(b)(2)(c)(d)(e) 23-50
23.53(c) 23-50 23.171 23-0
23.55 23-50 23.173 23-34
23.57 23-50 23.175 23-50
23.59(a) 23-50 23.177 23-50
23.61(a)(b)(1)(c) 23-34 23.181 23-45
23.63(a)(d) 23-50 23.201 23-50
23.67(c) 23-50 23.203 23-50
23.69 23-50 23.207(a)(c)(d)(e) 23-50
23.73(c) 23-50 23.251 23-45
23.75 23-50 23.253 23-50
23.77(c) 23-50 23.301(a) 23-48
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
United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate (Continuation Sheet) SA02001WINumber:
Issuance Date: February 8, 2023 Certification Basis (continued from page 3):
Section Amendment Section Amendment
23.305 23-45 23.1309(a)(1)(3)(4)(b)(1)(2)(3)(4) 23-49
23.307(a) 23-0 (c)(1)(2)(i)(iii)(3)(d)(e)
23.321 23-45 23.1323(b)(e) 23-49
23.331 23-42 23.1325(e) 23-50
23.333 23-34 23.1351(a)(1)(2)(b)(1)(i)(ii) 23-49
23.335 23-48 23.1353(h) 23-49
23.337(a)(1)(b)(1) 23-48 23.1357(a) 23-43
23.341 23-48 23.1359(c) 23-49
23.343(a) 23-48 23.1365(a)(d)(e) 23-49
23.345(a)(b)(c) 23-48 23.1367(a)(b) 23-0
23.347(a) 23-48 23.1381(a)(b) 23-0
23.351 23-42 23.1397(a) 23-11
23.391 23-48 23.1401 23-49
23.421 23-42 25.1419(a)(b) 25-23
23.423 23-42 23.1431(a)(b) 23-49
23.425 23-42 23.1501(a)(b) 23-21
23.441 23-48 23.1505(c) 23-7
23.443 23-48 23.1521(e) 23-50
23.471 23-0 23.1529 23-26
23.473 23-48 23.1541(a)(2)(b) 23-21
23.485 23-45 23.1545(d) 23-50
23.573(a)(b) 23-48 23.1581(a)(b)(1)(3)(c)(d)(f) 23-50
23.574(a) 23-48 23.1583(a)(3)(b)(1)(2)(c)(4)(5)(n) 23-50
23.575 23-48 23.1585(a)(1)(f) 23-50
23.601 23-0 23.1587(a)(1)(2)(3)(5)(d)(1)(2)(3) 23-50
23.603(a)(1)(2)(3)(b) 23-23 (5)(6)(7)(8)(9)(10)(11)
23.605(a) 23-23 36.1(a)(2)(b)(c) 36-31
23.607(a)(b)(c) 23-48 36.2(b) 36-24
23.609(a)(b) 23-0 36.3 36-14
23.611 23-48 36.9(a) 36-19
23.613(a)(b)(c)(d) 23-45 36.501(a)(1)(2)(c) 36-19
23.619 23-7 36.1501(a) 36-15
23.625(a)(b)(c) 23-7 36.1581(a)(2)(c) 36-25
23.627 23-0 36.1583 36-25
23.629(a)(2)(h)(i) 23-48 G36.101 36-16
23.853(a) 23-49 G36.103 36-16
23.867 23-49 G36.105 36-24
23.901(b)(1)(e)(1)(2) 23-53 G36.107 36-22
23.1011(b) 23-43 G36.109 36-16
23.1041 23-51 G36.111 36-27
23.1043(a)(1)(2)(3)(b)(c) 23-51 G36.201 36-22
23.1045 23-51 G36.203 36-16
23.1301 23-20 G36.301(b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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. | B200GT | A24CE |