STC SA03237CH

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

External Cargo Compartment and Cabin Interior Modifications in accordance with Standard Aero Master Data List 1024494, Revision (D), dated September 16, 2013 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 1025000, Revision (B) dated September 11, 2013, or later FAA approved revision is a required part of this modification.

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.

Standard Aero 1200 North Airport Drive Springfield, IL 62707 A00007SE Make: Quest Model: Kodiak 100

Date of application: May 07, 2013

Date of issuance: September 20, 2013 Date reissued:

(Signature) Robert A. Miller, 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: SA03237CH Date of issuance: September 20, 2013 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 Quest Kodiak 100 Reconfiguration of the cabin floor plan arrangement is as follows:

a. The type certification basis for Quest Kodiak 100 aircraft is shown on TCDS A00007SE 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, May 07, 2013, is based upon TCDS A00007SE. 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 A00007SE

23.1(a, b)(23-34), 23.21(a1, b)(Original), 23.45(a)(23-50), 23.49(a2, a3, a4, a5, a6, b)(23-50),

23.53(a, b)(23-50), 23.63(a1, a2, c)(23-50), 23.65(b)(23-50), 23.69(a)(23-50), 23.71(23-50), 23.77(b)(23-50),

23.143(a)(23-50), 23.147(c)(23-50), 23.153(a-d)(23-50), 23.157(a2, b, c2, d)(23-50), 23.161(a, b1, c)(23-50),

23.171(Original), 23.173(a, b1, c)(23-34), 23.177(a, b, d)(23-50), 23.181(a, b)(23-45), 23.251(23-45),

23.301(a-c)(23-48), 23.303(Original), 23.305(a, b)(23-45), 23.307(a, b)(Original), 23.321(a, b)(23-45),

23.341(a-c)(23-48), 23.561(a, b, e)(23-48), 23.562(a, b)(23-50), 23.573(a, b)(23-48), 23.601(Original),

23.603(a, b)(23-23), 23.605(a)(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), 23.623(a)(23-7), 23.625(a-d)(23-7), 23.627(Original), 23.629(a-f)(23-48),

23.777(a, b)(23-51), 23.785(a, b, d, g, i, j, k, n)(23-49), 23.787(a1, a2)(23-49), 23.815(b)(23-46),

23.867(a-c)(23-49), 23.1301(a-d)(23-20), 23.1306(a, b)(Original), 23.1309(a1, a2, b1, b2, b4,c-f)(23-49),

23.1322(c-e)(23-43), 23.1351(a, b1, b2, b3)(23-49), 23.1357(a, c)(23-43), 23.1361(a, c)(23-49),

23.1365(a-f)(23-49), 23.1367(a-d)(Original), 23.1411(a, b1)(23-36), 23.1431(a, b)(23-49), 23.1501(a, b)(23-

21), 23.1519(Original), 23.1529(23-26), 23.1541(a2, b)(23-21), 23.1557(a)(23-45), 23.1559(c)(23-50),

23.1581(a1, a2, b1, b3, c, d, f)(23-50), 23.1583(a1, h)(23-50).

Regulations at the latest amendment.

23.201(a-f)(23-62), 23.203(a-c)(23-62).

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