# STC SA8334SW

- Type: Supplemental type certificate
- Status: Current, Reissued
- Holder: Peter C. Morrison
- Description: Installation of dual toe brakes including rudder pedals, linkages and torque tubes.
- Status date: March 20, 2024
- Data sheets: 1A6, 1A6, 1A6, 1A6, 1A6
- Certificate PDF: https://openairdocs.org/files/sha256/64/c4/64c4ead59f66e8c93c9968ac23a933bd5ed755189ed669523ee718aa5d413ed0
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID131922335220240321134227.0001
- Page: https://openairdocs.org/stc/SA8334SW

## ADs that name it

None.

## Approved models (5)

- Piper Aircraft Inc. PA-22 (TCDS 1A6)
- Piper Aircraft Inc. PA-22-108 (TCDS 1A6)
- Piper Aircraft Inc. PA-22-135 (TCDS 1A6)
- Piper Aircraft Inc. PA-22-150 (TCDS 1A6)
- Piper Aircraft Inc. PA-22-160 (TCDS 1A6)

## What the certificate says

Read from the PDF's text layer, without the form's printed wording; the layout is lost and the order can 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.

----------END---------- 3 3

## Every issue (2)

- March 20, 2024: Reissued, Current. [certificate](https://openairdocs.org/files/sha256/64/c4/64c4ead59f66e8c93c9968ac23a933bd5ed755189ed669523ee718aa5d413ed0)
- September 8, 2006: Reissued, Historical. [certificate](https://openairdocs.org/files/sha256/f2/e5/f2e5cf9efd1db4e6c05f6548435e333646ac4e73eddc4abbb6203ed402925955)

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From OpenAirDocs.org, an independent open copy of FAA data. Only the Federal Register edition on govinfo.gov is the official legal text of an AD.
