# STC SA3822NM

- Type: Supplemental type certificate
- Status: Current, Amended
- Holder: Morgan Bert, United States
- Description: Installation of extended wing tips.
- Applied: March 17, 1986
- Status date: June 28, 1990
- Product: Aircraft, Single-Engine
- Certification basis: Part 21
- Data sheets: [TCDS 1A16](https://openairdocs.org/tcds/1A16)
- Certificate PDF: https://openairdocs.org/files/sha256/b8/6a/b86a74523cffffe4aaac6fee34513e5d5c74030c0fc048995f74a3077440ddc0
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/6AE25AE3371E033F85256CC2000C5AC7.0001
- DRS record last changed: December 5, 2025
- Page: https://openairdocs.org/stc/SA3822NM

## ADs that name it (0)

None.

## Approved models (3)

- Allied Ag Cat Productions Inc. G-164B ([TCDS 1A16](https://openairdocs.org/tcds/1A16))
- Allied Ag Cat Productions Inc. G-164C ([TCDS 1A16](https://openairdocs.org/tcds/1A16))
- Allied Ag Cat Productions Inc. G-164D ([TCDS 1A16](https://openairdocs.org/tcds/1A16))

## What the certificate says

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: SA3822NM This certificate issued to: Bert Morgan Part 8 of the CIVIl Air Regulations: as amended on March 19, 1957 Original Product -Typelertificate Number: 1A16 Make: Schweizer (Gruman) Model: G-164B, G-164C and G-164D Desoriplion gLype Design lahange: Installation of extended wing tips in accordance with Bert Morgan Installation Instructions, Report No. 1, Revision C, dated August 1989, and Master Drawing List No. 164-B, C and D, Revision C dated May 6, 1989, or later FAA approved revisions.

NOTE: This STC does not cover G-164D aircraft with 73-inch wing gap.

Approval of this change in type design applies to the above Limitations and Conditions: model aircraft only. This approval should not be extended to other aircraft of this model on which other previously approved modifications are incorporated unless it is determined that the relationship between this change and any of those other previously approved modifications, including changes in type design, will introduce no adverse effect upon the airworthiness of that aircraft. A copy of this Certificate, Continuation Sheet and FAA Approved Pilot's Operating Handbook Supplement, if applicable, dated November /, 1989, or later approved revision must be maintained as part of the permanent records for the modified aircraft.

Date of Application: March 17, 1986 Sute missued:

Date of Issuance: April 3, 1987 Jaleumendel November 7, 1989; June 28. 1990 FEDERAL AVIATION By Direction of the Administrator (Signature) Assistant Manager, Seattle Aircraft Certification Office (Title)

47.

**FAA FOR 8110-2 (10-68)**

United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate (Continuation Sheet) Number SA3822NM Limitations and Conditions: (CONTINUED) Model G-164B S/N 709B and up, G-164C, and Model G-164D require a Pilot's Operating Handbook Supplement (POHS) changing airspeed limits as follows:

G-164B, S/N 709B and up VNE (Never Exceed) 132 mph/115 KTS G-164C, S/N 1C and up NE (Never Exceed) 132 mph/115 KTS G-164D, S/N 1D and up NE (Never Exceed) 132 mph/115 KTS Required Placards: Install in plain view of pilot.

G-164B, S/N 709B and up VNE (Never Exceed) 132 mph/115 KTS G-164C, S/N 1C and up VNE (Never Exceed) 132 mph/115 KTS G-164D, S/N 1D and up VNE (Never Exceed) 132 mph/115 KTS NOTE: This aircraft is exempt from FAR 36 Appendix G acoustic change findings under the provisions of FAR 21.93(b) (3) (i).

**FAA FORM 8110-2-1 (10-69) PAGE 3 OF 3 PAGES**

## Every issue (1)

- June 28, 1990: Amended, Current. [certificate](https://openairdocs.org/files/sha256/b8/6a/b86a74523cffffe4aaac6fee34513e5d5c74030c0fc048995f74a3077440ddc0)

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