What it approves
Installation of Spookfish Camera Pod per SF04-MDL-0001 Issue 1 dated May 24, 2017, or later Previously listed as ST04409AT
What the certificate says
From the PDF’s text layer, without the form’s printed wording. Layout and order may differ; the PDF is the record.
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 1 of 3
IMPORT Number: SA04409AT
This certificate issued to: Spookfish Innovating Pty Ltd 4/14 Brodie-Hall Drive 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-0002 Issue 1 dated February 13, 2018, or later FAA approved revisions, with the following:
• aircraft are to be operated in accordance with Flight manual supplement SF04-FMS-0002 Issue 3 dated February 13, 2018, or later FAA approved revisions.
• aircraft are to be maintained in accordance with Maintenance manual supplement SF04-MMS-0002 Issue 2 dated February 13, 2018, 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, April 19, 2018, January 15, 2020
Signature Title Christina M. Underwood AIR-7AO Manager, Atlanta ACO Branch
FAA Form 8110-2 (5/14) Page 2 of 3
Transfer the ownership of Supplemental Type Certificate Number: SA04409AT
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: SA04409AT
FAA Form 8110-2 (5/14) Page 3 of 3
Date of Issuance: October 20, 2017 Date Amended: November 28, 2017, April 19, 2018, January 15, 2020
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, 23.23, 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, 23.251, 23.301, 23.303, 23.305, 23.307,
23.321, 23.333, 23.335, 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, 23.623, 23.625, 23.627, 23.725, 23.771, 23.773, 23.807, 23.853,
23.993, 23.999, 23.1301, 23.1307, 23.1321, 23.1323, 23.1325, 23.1331, 23.1351, 23.1357, 23.1361, 23.1365, 23.1367,
23.1411, 23.1431, 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 December 20, 1973 at amendment 23-14 for 23.1309.
• 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).
• Title 14 of the Code of Federal Regulations, CFR part 25 effective December 10, 2007 at amendment 25-123 for 25.869(a).
• 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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ADs that name this STC · 0
An AD can apply because an STC is installed, or mention one in its text.
Approved models · 1
| Make | Model | Data sheet |
|---|---|---|
| Piper Aircraft Inc. | PA-23-250 | 1A10 |