# STC SA1753NM

- Type: Supplemental type certificate
- Status: Current, Issued
- Holder: Comanche Aircraft Products Co, United States
- Description: Removal of the factory equipped vertical fin mounted rotating beach and installation of a vertical fin mounted Whelen strobe light assembly
- Applied: December 4, 1981
- Status date: October 13, 1982
- Product: Aircraft, Small Airplane
- Certification basis: Part 21
- Data sheets: [TCDS A1EA](https://openairdocs.org/tcds/A1EA)
- Certificate PDF: https://openairdocs.org/files/sha256/68/f2/68f2ed7c77e2ad190e102715bf2de7118a3c3cdbb6c82fcd70c06dd0868e0fd1
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/A27ECECE8D565BCB862579FB006DF411.0001
- DRS record last changed: December 5, 2025
- Page: https://openairdocs.org/stc/SA1753NM

## ADs that name it (0)

None.

## Approved models (1)

- Piper Aircraft Inc. PA-30 ([TCDS A1EA](https://openairdocs.org/tcds/A1EA))

## 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: SA1753NM This certificute, iedte Comanche Aircraft Products Company Furt 3 fithe CIViT Air Pugulations:, dated May 15, 1956 and FAR 23.1401 dated July 10, 1977.

Original Product - Type Certificate Number: ATEA Make: Piper Model: PA-30 Description of Type Design Change: Removal of the factory equipped vertical fin mounted rotating beacon and installation of a vertical fin mounted Whelen strobe light assembby in accordance with FAA Approved CAPCO Descriptive Data List Number 7059Y-5A, dated August 3, 1982, or later FAA Approved revision.

NOTE: This Whelen light installation does not meet the Anticollision Light requirement of CAR 3, and is only considered to be a supplemental light.

The aircraft must be equipped with an FAA approved anticollision light system for all night operations.

timilations and anditione:

Data pertaining to this modification are considered inadequate for duplication in other aircraft. This approval is limited to the installation on Piper PA-30 airplane S/N 30-70, R/N N-7059Y, only. A copy of this STC should be maintained in the aircraft records while this modification is installed.

Intesf applicution: December 4, 1981 Date Reissued:

Latesfience: • October 13, 1982 Date Amended:

FEDERAL AVIATIO mistrea (Signature ) TAHINIST RAND Acting Manager, Seattle Aircraft Certification Office (Title)

**FAA FORM 8110-7 (10-66)**

## Every issue (1)

- October 13, 1982: Issued, Current. [certificate](https://openairdocs.org/files/sha256/68/f2/68f2ed7c77e2ad190e102715bf2de7118a3c3cdbb6c82fcd70c06dd0868e0fd1)

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