# STC SA4162NM

- Type: Supplemental type certificate
- Status: Current, Issued
- Holder: Flight Structures Inc., United States
- Description: Installation of a belly mounted infrared lamp and pod fairing and an internally mounted electrical equipment rack
- Applied: November 11, 1987
- Status date: January 22, 1988
- Product: Aircraft
- Certification basis: Part 21
- Data sheets: [TCDS A28CE](https://openairdocs.org/tcds/A28CE)
- Certificate PDF: https://openairdocs.org/files/sha256/72/0c/720c7590aab6df0f857d62f088ae979112312c986a6d618096f33b4a88395fd9
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/861B8DCC8EC03DBB862579C200572221.0001
- DRS record last changed: December 5, 2025
- Page: https://openairdocs.org/stc/SA4162NM

## ADs that name it (0)

None.

## Approved models (1)

- Cessna Aircraft Company 441 ([TCDS A28CE](https://openairdocs.org/tcds/A28CE))

## 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 SAA162NM This certificate issued to: Flight Structures, Inc.

Purt 23 of the Federa1 Aviation Regulations.

Original Product -Type bertificate Number: A28CE Make: Cessna Model: 441 Description of Type Design Change: Installation of a belly mounted infrared 1amp and pod fairing and an internally mounted electrical equipment rack on Cessna Model 441, S/N 441-054 in accordance with an FAA sealed copy of Flight Structures, Inc. Master Drawing List No. 87FS167-1, dated January 12, 1988, or later FAA approved revision.

Limitations and Conditions: Data pertaining to this modification are considered inadequate in other aircraft. This approval is limited to the installation in Cessna Model 441, S/N 441-054 aircraft only. The modified airplane must be operated in accordance with FAA Approved Airplane Flight Manual Supplement, dated January 20, 1988, or later FAA approved revision, which, along with a copy of this Certificate, must be maintained as part of the permanent records for the modified aircraft.

Date of Application: November 11, 1987 Date Reissued:

Dale sfisance: January 22, 1988 Date Amended:

FEDERAL AVIATION By Direction of the Administrator sail Gami TO MINISTRATION Aircraft Certification Office (Title)

United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate (Continuation Sheet) Number SAA162N4 Limitations and Conditions: (continued) This approval applies to the structural aspects of this program only. The electrical and avionics aspects of the completed MLS surveillance system must receive further FAA approval.

-END-

**FAA FORM 8110-2-1 (10-69) PAGE 3 OF 3 PAGES C FAA AC 82-03578**

## Every issue (1)

- January 22, 1988: Issued, Current. [certificate](https://openairdocs.org/files/sha256/72/0c/720c7590aab6df0f857d62f088ae979112312c986a6d618096f33b4a88395fd9)

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