# STC SA1645NM

- Type: Supplemental type certificate
- Status: Current, Reissued
- Holder: Globe Fiberglass LTD, Inc, United States
- Description: Installation of a Fiberglass lower tail cone
- Applied: May 13, 1982
- Status date: May 30, 1986
- Product: Aircraft, Small Airplane
- Certification basis: Part 21
- Data sheets: [TCDS A7SO](https://openairdocs.org/tcds/A7SO)
- Certificate PDF: https://openairdocs.org/files/sha256/85/18/8518814b35f911637880be151e23664da9a1069fdd08abb53651a306899b47fa
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/712E8FF866BBE04F86257AC200549B5D.0001
- DRS record last changed: December 6, 2025
- Page: https://openairdocs.org/stc/SA1645NM

## ADs that name it (0)

None.

## Approved models (3)

- Piper Aircraft Inc. PA-34-200 ([TCDS A7SO](https://openairdocs.org/tcds/A7SO))
- Piper Aircraft Inc. PA-34-200T ([TCDS A7SO](https://openairdocs.org/tcds/A7SO))
- Piper Aircraft Inc. PA-34-220T ([TCDS A7SO](https://openairdocs.org/tcds/A7SO))

## 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: SA1645N4 This certificate issued to: Globe Fiberglass Ltd, Inc.

Part 23 of the Federal Avi at ion Regulations.

Original Product -Typebertificate Number: A750 Make: Piper Model: PA-34 Series Description of Type Design Change: Installation of a Fiberglass lower tail cone in accordance with 3-D Enterprises, Ltd. Specification and Drawing No. 823D004.

NOTE: This installation is a replacement for the comparable Piper component.

Limitations and Conditions: Approval of this change in type design applies to the above model aircraft only. This approval should not be extended to 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 shall be maintained as part of the permanent records for the modified aircraft.

Date of Application: May 13, 1982 Date Reissued: December 14, 1984; May 30, 1986 Date of Issuance: May 19, 1982 Date Amended:

FEDERAL AVIATION By Direction of the Administrator (Signature ) T MINISTRATOS Manager, Seattle Aircraft Certification Office (Title )

47.

## Every issue (1)

- May 30, 1986: Reissued, Current. [certificate](https://openairdocs.org/files/sha256/85/18/8518814b35f911637880be151e23664da9a1069fdd08abb53651a306899b47fa)

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