What it approves
Fabrication of North River Avia. Model 8400 brake booster assembly, and modify Scott Avia. Model B-711 brake master cylinders.
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.
6041 Mackay Street Suite 102 Anchorage, AK 99518
Part 3 of the Civil Air Regulations.
Original Product Type Certificate Number: 780 Piper Make: Model: PA-12
Description of Type Design Change: Fabrication of North River Aviation Model 8400 brake booster assemblies, and modification of Scott Aviation Model B-711 brake master cylinders by installation of said assemblies, both in accordance with North River Aviation, Inc., Drawing List No. 84-100, revised April 17, 1993, or later FAA approved revision.
Limitations and Conditions: The approval of this change in type design applies to the basic Piper PA-12 airplanes that have been equipped with FAA approved high-pressure brake lines, and with brakes FAA approved for a maximum available hydraulic pressure of at least 1698 PSI, only. This approval should not be extended to other aircraft of these models on which other previously approved modifications are incorporated, unless it is determined by the installer that the modification will introduce no adverse effect on the airworthiness of such aircraft.
(See Continuation of Limitations and Conditions)
Date of application: March 20, 1985
Date of issuance: August 5, 1987 Date reissued: July 19, 2004; January 26, 2006
Date amended: July 19, 2004; January 26, 2006
( Signature) Gregory J. Holt Manager Anchorage Aircraft Certification Office
(Title)
FAA Form 8110-2-1(10-69) Page 3 of 3
Number SA3633NM Date reissued: July 19, 2004; January 26, 2006 Date amended: July 19, 2004; January 26, 2006
Limitations and Conditions (Continued)
FAA approved high-pressure brake lines, under the meaning of this Certificate, are brake lines which the FAA has found to be sufficiently flexible for their intended purpose, compatible with MIL-H-5606BB (red) hydraulic fluid, and capable of sustaining an ultimate internal hydraulic pressure of at least 2547 PSI for at least 3 seconds without failure or leakage; and which the FAA has approved for installation on the airplane. The modification approved by this Certificate is also eligible on Piper PA-22S “150” and PA- 22S “160” airplanes that have been converted to landplanes in accordance with FAA approved data.
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.
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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 |
|---|---|---|
| The New Piper Aircraft Inc. | PA-12 | A-780 |