What it approves
Installation of dual toe brakes including rudder pedals, linkages and torque tubes.
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.
IMPORT SA8334SW Peter C. Morrison 17 Ohio Rd.
Shediac, New Brunswick Canada E4P 2J8 Part 3 the Civil Air Regulations 1A6 Piper Aircraft, Inc.
PA-22, PA-22-108, PA-22-135, PA-22-150, PA-22-160
1. Installation of dual toe brakes including rudder pedals, linkages, and torque tubes must be in accordance with Williams Aircraft Company drawing list WAC-01, dated June 1, 1992, or later Transport Canada Civil Aviation (TCCA) approved revision.
1. This modification is limited to aircraft which have been converted to a tail wheel configuration by FAA STC SA45RM.
(See continuation sheet 3) November 5, 1991 September 8, 2006; March 20, 2024 May 8, 1992
Anthony E. Gallo Manager, International Validation Branch Compliance & Airworthiness Division Aircraft Certification Service 3
IMPORT SA8334SW SA8334SW 3
IMPORT SA8334SW Date Reissued: March 20, 2024
2. If the holder agrees to permit another person to use this certificate to alter a product, the holder must give the other person written evidence of that permission.
3. The installer must determine whether this design change is compatible with previously approved modifications.
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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 · 5
Every issue · 2
DRS keeps each issue of an STC as its own record, with its own certificate and attachments.
| Date | Status | Files |
|---|---|---|
| March 20, 2024 | Reissued, current | Certificate |
| September 8, 2006 | Reissued, earlier issue | Certificate |