STC ST04409AT

FAA Form 8110-2 (5/14) Page 1 of 3

IMPORT Number: ST04409AT

This certificate issued to: Spookfish Aviation Pty Ltd 5 Turner Ave Bentley, Western Australia 6102 Australia

Part 23 of the Federal Aviation Regulations.

Original Product – Type Certificate Number: 1A10 Make: Piper Aircraft, Inc.

Model: PA-23-250 (see Limitations and Conditions) Description of Type Design Change:

Note: Reference CASA (Australia) STC SVA 571 Installation of Spookfish Camera Pod per SF04-MDL-0001 Issue 3 dated September 20, 2017, or later FAA approved revisions, with the following deviations:

• in lieu of SF04-FMS-0001, aircraft are to be operated in accordance with Flight manual supplement SF04-FMS-0002 Issue 2 dated November 20, 2017, or later FAA approved revisions.

• in lieu of SF04-MMS-0001, aircraft are to be maintained in accordance with Maintenance manual supplement SF04-MMS- 0002 Issue 1 dated October 12, 2017, or later FAA approved revisions

Note: Reference CASA (Australia) STC SVA 571

1. Applicable to Piper Model PA-23-250 airplane serial numbers 27-2505 through 27-4916, 27-7304917 through 27-7554168, 27-7654001 through 27-8154030 except 27-7305220, 27-7305221, 27-7305371, 27-7305377, 27-7405371, 27-7405377, 27-7405388, 27-7405396, 27-7405398, 27-7405438, 27-7405447, 27-7405451, 27-7504455, 27-7554104, 27-7654022, 27-7654031, 27-7654153, 27-7754163, 27-7854057, and 27-7854102.

Date of Application: October 20, 2016 Date Reissued:

Date of Issuance: October 20, 2017 Date Amended: November 28, 2017

Signature Title Christina M. Underwood AIR-7AO Manager, Atlanta ACO Branch

United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate Possession of this Su pplemental Type Certificate (STC) document by persons other than the STC holder does not constitute rights to the design data nor to alter an aircraft, aircraft engine, or propeller. The STC’s supporting documentation (drawings, instructions, specifications, flight manual supplements, etc.) is th e property of the STC holder.

FAA Form 8110-2 (5/14) Page 2 of 3

Transfer the ownership of Supplemental Type Certificate Number: ST04409AT

To (Name and address of transferee)

From (Name and address of grantor)

United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate (Continuation Sheet) Number: ST04409AT

Possession of this Su pplemental Type Certificate (STC) document by persons other than the STC holder does not constitute rights to the design data nor to alter an aircraft, aircraft engine, or propeller. The STC’s supporting documentation (drawings, instructions, specifications, flight manual supplements, etc.) is th e property of the STC holder.

FAA Form 8110-2 (5/14) Page 3 of 3

Date of Issuance: October 20, 2017 Date Amended: November 28, 2017

Limitations and Conditions (Continued from page 1):

2. 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.

3. 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.

Certification Basis:

Note: Reference CASA (Australia) STC SVA 571

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 PA-23-250 ‘F’ series is as follows:

a. The type certification basis as shown on TCDS 1A10 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, October 20, 2016, was determined to be:

• Civil Air Regulations, CAR 3 amendment 14 for 3.10-3.19, 3.62-3.65, 3.780, 3.791-3.792

• Title 14 of the Code of Federal. Regulations, CFR part 23 effective February 1, 1965 at amendment 23-0 for 23.1,

23.3,.23.21, 2323, 23.25, 23.29, 23.45, 23.49, 23.51, 23.65, 23.67, 23.75, 23.77, 23.141, 23.143, 23.145, 23.147, 23.161,

23.171, 23.173, 23.175, 23.177, 23.179, 23.181, 23.201, 23.203, 23.207, 23.231, 23.233, 2-3.251, 23.301, 23.303, 23.305, 23:307, 23.321, 23.333, 23.337, 23.341, 23.471, 23.473, 23.477, 23.479, 23.481, 23.483, 23.561, 23.601, 23.603, 23.605,

23.607, 23.609, 23.611, 23.613, 23.615, 23.619, 23.621., 23.6.23, 23.625, 23.627, 23.725, 23.853, 23.993, 23.999, 23.1323,

23.1325, 23.1501, 23.1505, 23.1513, 23.1519, 23:1523, 23.1525, 23.1541, 23.1557, 23.1581, 23.1583, 23.1585, 23.1589

• Title 14 of the Code of Federal Regulations, CFR part 23 effective February 1, 1965 at amendment 23-50 for 23.67,

23.147(b) in additional to 23.147 amdt 23-0, 23.149, 23.205 (Removed at amdt 23-50).

• Based on 14 CFR § 21.93(b)(3) (Amdt 21-97), No Acoustical Change has been found for the 14 CFR Part 36 noise levels regulations.

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