# STC SA3860NM

- Type: Supplemental type certificate
- Status: Current, Issued
- Holder: Madras Air Service, United States
- Description: Installation of Madras Air Service Model 102 wing tips.
- Applied: March 24, 1987
- Status date: June 26, 1987
- Product: Aircraft, Single-Engine
- Certification basis: Part 21
- Data sheets: [TCDS 2A13](https://openairdocs.org/tcds/2A13)
- Certificate PDF: https://openairdocs.org/files/sha256/5b/52/5b5242f97b44a01aaa209822672959b8f74e69c6eb2e6d186648f35f13e4b099
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/2956F4EE2BBECFC585256CC2000C5B16.0001
- DRS record last changed: December 6, 2025
- Page: https://openairdocs.org/stc/SA3860NM

## ADs that name it (0)

None.

## Approved models (3)

- The New Piper Aircraft Inc. PA-28-151 ([TCDS 2A13](https://openairdocs.org/tcds/2A13))
- The New Piper Aircraft Inc. PA-28-161 ([TCDS 2A13](https://openairdocs.org/tcds/2A13))
- The New Piper Aircraft Inc. PA-28-181 ([TCDS 2A13](https://openairdocs.org/tcds/2A13))

## 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: SA3860NM This certificate issued to: Madras Air ServICe Part 3 of the CIV11 Air Regulations.

Original Product - Typebertificate Number: 2A13 Make: Piper Model: PA-28-151, PA-28-161 and PA-28-181 Description of Type Design Change:

Installation of Madras Air Service Model 102 wing tips in accordance with Madras Air Service Installation Instructions for fiberglass "super tips" and Drawing No. MAS 102, dated March 26, 1987, or later FAA approved revisions.

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, must be maintained as part of the permanent records for the modified aircraft.

Date of Application: March 24, 1987 Date Reissued:

Date of Issuance: June 26, 1987 Date Amended:

FEDERAL AVIATION Assistant Manager, Seattle Aircraft Certification Office (Title)

## Every issue (1)

- June 26, 1987: Issued, Current. [certificate](https://openairdocs.org/files/sha256/5b/52/5b5242f97b44a01aaa209822672959b8f74e69c6eb2e6d186648f35f13e4b099)

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