What it approves
Removal of upper cross bar from control yoke(s).
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: SA00854SE This certificate issued to: Jeffrey A. Morfitt 2833 Morris Ave. So.
Renton, WA 98055 Part 23 of the Federal Aviation Regulations.
Original Product —Type Certificate Number: 1A6 Make: Piper Model: PA-22-150 Description of Type Design Change: Removal of upper cross bar from control yoke(s) in accordance with Photographs contained in the FAA project file or later FAA approved data.
NOTE: This modification may be performed on the left, right, or both control yokes.
Limitations and Conditions: Data pertaining to this modification are considered inadequate for duplication in other aircraft. This approval for change in type design is limited to Piper Model PA-22-150, Serial Number 22-7497, only. A copy of this Certificate dated November 27, 2000, must be maintained as part of the permanent records for the modified aircraft.
Date of Application: November 20, 2000 Date Reissued:
Date of Issuance: November 27, 2000 Date Amended:
FEDERAL AVIATIO By Direction of the Administrator (Signature) INST RATION Acting Manager, Seaftle 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-22-150 | 1A6 |