STC SA03140CH-D

Part 23 of the Federal Aviation Regulations. (See Page 3 for complete certification basis)

Installation of a removable tail cone and additional aft bulkhead mounting structure in accordance with Standard Aero Master Data List 1022526, Revision (G), dated November 06, 2012 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 document number 1023215, Rev. (B) dated November 06, 2012, or later FAA approved revision is a required part of this modification.

3. Airworthiness Limitations specified in Standard Aero document 1023097, Rev. (B) dated November 02, 2012, or later FAA approved revision, must be complied with in addition to the basic airplane maintenance manuals.

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.

Standard Aero 1200 North Airport Drive Springfield, IL 62707 A24CE Make: Hawker Beechcraft Corporation Model: B300

Date of application: June 27, 2012

Date of issuance: November 07, 2012 Date reissued:

( Signature) Tim Winiesdorffer, ODA Administrator Standard Aero, Springfield, IL ODA-100079-CE

( Title)

Transfer the ownership of Supplemental Type Certificate Number

to (Name of transferee)

(Address of transferee)

(Number and street)

(City, State, and Zip code)

from (Name of grantor) (Print or type)

(Address of grantor)

(Number and street)

(City, State, and Zip code)

Signature of grantor (In ink):

Supplemental Type Certificate Number: SA03140CH-D Date of issuance: November 07, 2012 Date of amendment:

Date of reissue:

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 Hawker Beechcraft Corporation B300 Installation of a removable tail cone and additional aft bulkhead mounting structure RF Transparent Pod is as follows:

a. The type certification basis for Hawker Beechcraft Corporation B300 is shown on TCDS A24CE 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, June 27, 2012, is based upon TCDS A24CE. 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 in TCDS A24CE

23.1(a, b)(23-34), 23.21(a1)(Original), 23.51(d)(23-34), 23.57(a-d)(23-34), 23.59(a)(23-34), 23.65(a1-3,

c)(23-34), 23.67(e)(23-34), 23.77(c)(23-34), 23.143(a)(23-17), 23.145(a-e)(23-17), 23.147(a, b)(Original),

23.149(a)(23-21), 23.153(a-c)(23-14), 23.157(a-d)(23-14), 23.171(Original), 23.173(a-c)(23-34), 23.175(a,

d)(23-34), 23.177(a)(23-21), 23.181(a, b)(23-21), 23.251(23-45), 23.253(a, b1, b3, c) (23-26), 23.301(a-

b)(Original), 23.333(a-d)(23-34), 23.335(a-d)(23-34), 23.337(a-c)(23-34), 23.341(23-34), 23.347(Original),

23.349(a, b)(23-34), 23.351(Original), 23.365(a, b, d)(Original), 23.421(a, b)(23-7), 23.423(a, b)(23-7),

23.425(a-d)(23-7), 23.427(a-c)(23-14), 23.441(a-c)(23-28), 23.443(a-d)(23-34), 23.471 (Original), 23.477 (Original), 23.479 (a-d)(23-17), 23.561(a-e)(23-34), 23.571(a, b)(23-34), 23.572(b)(23-34), 23.601(Original),

23.603(a, b)(23-23), 23.605(a)(b)(23-23), 23.607(23-17), 23.609(a, b)(Original), 23.611(23-7), 23.613(a-

23.853(d3ii)(23-34), 23.1301(a-d)(23-20), 23.1309(a-d)(23-49), 23.1322(c, d)(23-17), 23.1351(a, b)(23-49),

23.1357(a-e)(23-43), 23.1365(a, b)(23-14), 23.1381(a-c)(Original), 23.1401(a1, 2, b-f)(23-20), 23.1431(a-

23.1541(a2, b)(23-21), 23.1581(a1-2, b1, b3, c, d, f)(23-50), 23.1583(a1, a3i, iii, h)(23-50), 23.1587(a, c,

d)(23-34)

Regulations at the latest amendment.

36.1(a-h)(36-26), 36.2(a-c)(36-24), 36.3(36-14), 36.6(a-e)(36-26), 36.9(a, b)(36-19), 36.501(a-c)(36-19),

36.1501(a, b)(36-15), 36.1581(a-c, e, g)(36-25), G36.101(a-c)(36-16), G36.105(a-g)(36-24), G36.107(a)(36-

22), G36.109(a-g)(36-16), G36.111(a-c)(36-27), G36.201(a-d)(36-22), G36.203(a, b)(36-16), G36.301(b,

c)(36-28).

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