STC SA03998AT

Part 23 of the Federal Aviation Regulations.

Description of Type Design Change : Installation of the Camera Provisions and Associated Systems Interface in accordance with Chippewa Aerospace Master Drawing List (MDL) No. E90-5310-01-0001, Rev. 4, Dated February 19, 2013, or later FAA approved revision.

Limitations and Conditions : FAA Approved Airplane Flight Manual Supplement (AFMS) for the Installation of Camera Provisions and Associated Systems Interface in the Hawker Beechcraft King Air E-90 Series Aircraft, Chippewa Aerospace Document No. E-90-5310-01-0012, Rev. IR, Dated March 22, 2013 and AFMS for the Installation for the Installation of Camera Provisions and Associated Systems Interface in the Hawker Beechcraft King Air 200 Series Aircraft, Chippewa Aerospace Document No. 200-5310-01- 0012, Rev. IR, Dated March 22, 2013, or later FAA approved revision, is a required part of this STC. This approval should not be extended to other aircraft of this model on which other previously approved modifications are incorporated, unless it is determined by the installer that the interrelationship between this change and any other previously approved modifications will produce no adverse effect upon the airworthiness of that airplane. If the holder agrees to permit another person to use this certificate to alter the product, the holder shall give the other person written evidence of that permission.

Chippewa Aerospace Inc.

1601 Executive Ave Myrtle Beach, SC 29577 3A20 and A24CE Make : Hawker Beechcraft Model : King Air E-90 and 200 Series Date of application : April 06, 2010

Date of issuance : March 22, 2013

( Signature)

Melvin D. Taylor Office Manager Atlanta Aircraft Certification Office

( Title)

Number SA03998AT

Instructions for Continued Airworthiness (ICA), Chippewa Aerospace Inc.

Document No. # P90-5310-01-0002, Rev 1, dated 07/06/2012, or later FAA accepted revision must be made available to the operator at the time of installation.

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 Hawker Beechcraft King Air 90 and 200 Series aircraft is as follows:

a. The type certification basis for Hawker Beechcraft King Air 90 and 200 Series airplane is shown on TCDS 3A20 and A24CE for parts not changed or not affected by the change.

b. The certification basis for parts changed or a ffected by the change since the reference date of application, April 06, 2010, is based upon part 23 as amended by Amendment 23-59. 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:

c. The certification basis for parts changed or a ffected by the change since the reference date of application, April 06, 2010, is based upon part 21 as amended by Amendment 21-91. 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 latest amendment 23-0 through 23-59 §§ 23.149 §§ 23.161 §§ 23.207 §§ 23.301 §§ 23.303 §§ 23.305 §§ 23.307 §§ 23.321 §§ 23.333 §§ 23.335 §§ 23.337 §§ 23.341 §§ 23.365 §§ 23.573 §§ 23.601 §§ 23.603 §§ 23.605 §§ 23.607 §§ 23.609 §§ 23.611 §§ 23.613 §§ 23.619 §§ 23.625 §§ 23.1307 §§ 23.1322 §§ 23.1357 §§ 23.1359 §§ 23.1365 §§ 23.1367 §§ 23.1541 §§ 23.1581

Regulations at the amendment level 23-62 §§ 23.49 §§ 23.67 §§ 23.177 §§ 23.201 §§ 23.251 §§ 23.561 §§ 23.571 §§ 23.1301 §§ 23.1309 §§ 23.1310

Regulations at the amendment level in TCDS 3A20 and A24CE §§ 23.1351

Regulations at the latest amendment 21-0 through 21-91 §§ 21.93

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