What it approves
Installation of PA-12 metal wing spars, two aluminum wing tanks, removal of header tank, rerouting of the fuel lines, installation of electrical boost pump, installation of balanced horizontal tail surfaces, and new trim system.
What the certificate saysOCR
This is OCR from the scanned FAA certificate. OCR can misread letters and numbers.
United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate Number: SA5704NM This certificate issued to: James G. Stark Part 4a s$ theCiVil Air Regulations Original Product - Type Certificate Number: A -725 Make: J5A Make: Piper Aircraft Corporation Description of Type Design Change: Installation of PA-12 metal wing spars, installation of two aluminum wing tanks, removal of header tank, rerouting of the fuel lines, installation of electrical boost pump, installation of balanced horizontal tail surfaces, and installation of new trim system.
Loilaliens andbundiions Data pertaining to this modification are considered inadequate for other aircraft. This approval is limited to the installation in Piper Model J5A, Serial No. 5-1088, R/N N38888, only. A copy of this Certificate must be maintained as part of the permanent records for the modified aircraft.
A-725 apply except where superseded by the following:
The following placard must be located on the instrument panel in the clear view of the pilot:
TURN THE FUEL PUMP "ON" FOR
TAKE-OFF, CLIMB AND LANDING
- END-
FAA FORM 8110-2-1 (10-69)
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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 |
|---|---|---|
| FS 2001 Corp. | J5A (Army L-4F) | A-725 |