STC SA02013WI

United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate Number 

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A200 (C-12C), B200/B200C A24CE BLR Winglet Performance Analysis at Centex Increased Gross Weight

1) BLR Aerospace, Pilot's Operating Handbook and FAA Approved Airplane Flight Manual Supplement, AFMS-B200-4, dated 10/17/2023 or later FAA accepted revision for Model B200/B200C.

(continuation of description on Page 3 of this STC)

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

(Limitations continued on Page 3 of this STC) April 22, 2022 2/25/25 October 17, 2023 11/26/24 William Eckler ODA Administrator ODA-833355-CE 5

United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate Number  (IIHFWLYH'DWH I Transferr Endorsementt Transfer the ownership of Supplemental Type Certificate Number:

Too (Name and address of transferee):

Date oI transfer:

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(Continuation Sheet) Number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escription of Type Design Change (continuation)

2) BLR Aerospace, Pilot's Operating Handbook and FAA Approved Airplane Flight Manual Supplement, AFMS-B200-6, dated 10/17/2023 or later FAA accepted revision for Model B200/B200C.

3) BLR Aerospace, Pilot's Operating Handbook and FAA Approved Airplane Flight Manual Supplement, AFMS-A200-2, Revision IR, Dated 06/21/2024 for Model A200 (C-12C).

4) Master Data List (MDL) 3S22-017-1001, Revision 2.0, Dated 11/25/2024 or later FAA approved revision.

Limitations and Conditions (continuation)

2) 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.

3) Approval of this change in type design applies to the above model aircraft only.

4) A copy of this certificate and the AFMS shall be maintained in the airplane permanent records.

(Continuation on page 4) 35 02/25/25

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5) STC SA11103SC is a prerequisite STC.

Specific configuration requirements for King Air Model A200 (C-12C) aircraft:

i. King Air model A200 (C-12C) airplane operating in commuter category with a maximum takeoff weight of 14,000 pounds.

ii. King Air model A200 (C-12C) airplane with the Beech "tension fitting" wing design. Serial numbers BC-1 through BC-61 and BD-1 through BD-30 that have been modified per Service Instructions (SI) C-12-0076, and re-designated as Model A200 (C-12C), and serial numbers BC-62 and on.

iii. King Air model A200 (C-12C) airplane equipped with BLR Aerospace's Winglet System in accordance with STC SA01615SE.

iv. King Air model A200 (C-12C) airplane equipped with Pratt and Whitney PT6A-42 engines.

Specific configuration requirements for King Air Model B200 aircraft:

v. King Air model B200, B200C airplane operating in commuter category with a maximum takeoff weight of either 13,420 or 14,000 pounds.

vi. King Air model B200, B200C airplane with the Beech "shear fitting" wing design. Serial numbers BB-1158, BB-1167, BB-1193 and up; model B200C serial numbers BL-73 and up.

vii. King Air model B200, B200C, airplane equipped with BLR Aerospace's Winglet System in accordance with STC SA01615SE.

Certification Basis:

Based on 14 CFR §21.115 and §21.101, and the FAA policy for significant changes in FAA Order 8110.48A, the certification basis for the applicable 14 CFR Part 23 aircraft affected is as follows:

a. As specified on the applicable Type Certificate Data Sheet (TCDS) of the aircraft for parts not changed or not affected by this STC.

b. Regulations at the amendment levels defined within the following for parts changed or affected by the STC since the reference date of STC application.

(Continuation on page 5) 45 02/25/25

(Continuation Sheet) Number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ertification Basis (continuation) -------------------------------------------Applicable to All Models------------------------------------------ §23.45 [Amdt. 23-50] §23.1501(a)(b) [Amdt. 23-21] §23.49(a)(2)(3)(4)(5)(6)(b) [Amdt. 23-50] §23.1581 [Amdt. 23-50] §23.51 [Amdt. 23-50] §23.1583 [Amdt. 23-50] §23.53(c) [Amdt. 23-50] §23.1585 [Amdt. 23-50] §23.55 [Amdt. 23-50] §23.1587 [Amdt. 23-50] §23.57 [Amdt. 23-50] §23.1589 [Amdt. 23-50] §23.59 [Amdt. 23-50] §23.61 [Amdt. 23-34] §23.63(a)(d)(1) [Amdt. 23-50] §23.66 [Amdt. 23-50] §23.67(c)(1)(2)(3) [Amdt. 23-50] §23.69 [Amdt. 23-50] §23.77(c) [Amdt. 23-50] §23.1501(a)(b) [Amdt. 23-21] ------------------------------Applicable to Models B200 and B200C Only------------------------------- §23.53(a)(b) [Amdt. 23-50] §23.63(c) [Amdt. 23-50] §23.65(b) [Amdt. 23-50] §23.67(b) [Amdt. 23-50] §23.77(b) [Amdt. 23-50] --------------------------------Applicable to Model A200 (C-12C) Only---------------------------------- §23.63(d)(2) [Amdt. 23-50] §23.67(c)(4) [Amdt. 23-50] -------------------------------------------------------END------------------------------------------------------- 55 02/25/25