What it approves
Installation of metal leading edge extension and a metal skin replacement on the aft fuselage
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: SA1187N4 This certificate issued to: Paul Hanes Part 3 fithe CIVil Air Regulations:
Original Product - Type bentificate Number: 1A2 Make: Piper Model: PA-18A (Standard/Restricted) Description of Type Design Change: Installation of metal leading edge extension (12" to the rear of the front spar on the upper surface) and a metal skin replacement on the aft (top) fuselage in accordance with Lemen Aircraft Service Sketches A & B.
NOTE: Operating Limitations dated March 5, 1981, are applicable and shall be maintained in the aircraft at all times.
Limitations and Conditions: Data pertaining to this modification are considered inadequate for duplication in other aircraft. This approval is limited to the installation in Piper PA-18A, Serial Number 18-3287 only. A copy of this Certificate shall be maintained as part of the permanent records for the modified aircraft.
Date of Application: February 11, 1981 Date Reissued:
Dulesfissuance: March 5, 1981 Date Amended:
FEDERAL AVIATION By Direction of the Administrator (Signature) TOMIN STRANDS Acting Chief, Seattle Area Aircraft Certification Office (Title)
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-18A | 1A2 |