# STC SH2216NM

- Type: Supplemental type certificate
- Status: Current, Reissued
- Holder: Honeywell International Inc, United States
- Description: Installation of a Sperry Primus 500 weather radar system.
- Applied: July 20, 1982
- Status date: March 18, 2020
- Product: Aircraft, Rotorcraft
- Certification basis: Part 21, Part 29
- Data sheets: [TCDS H10EU](https://openairdocs.org/tcds/H10EU)
- Certificate PDF: https://openairdocs.org/files/sha256/df/38/df389566515d6ac7d144c53825ab9041d8d7263d38c542f1e1c120897bf9d514
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/A950A880366DD5E68625862A004E89FC.0001
- DRS record last changed: December 6, 2025
- Page: https://openairdocs.org/stc/SH2216NM

## ADs that name it (0)

None.

## Approved models (1)

- Eurocopter France SA-365N ([TCDS H10EU](https://openairdocs.org/tcds/H10EU))

## What the certificate says

Read from the PDF's text layer, without the form's printed wording; the layout is lost and the order can differ. The PDF is the record.

United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate Page 1 of 3 FAA Form 8110-2 (5/14)

Number: SH2216NM This certificate issued to: Honeywell International Inc.

21111N 19th Ave Phoenix, Arizona 85027 Part 29of the Federal Aviation Regulations.

Original Product – Type Certificate Number: Make: Societe Nationale Industrielle Model:

H10EU SA-365N

Installation of a Sperry Primus 500 Weather Radar System in accordance with FAA approved Sperry Flight Systems Indentured Drawing List, Specification No. 5300-362, Revision “B”, dated October 17, 1983, or later FAA approved revision.

Sperry Flight Systems FAA approved Rotorcraft Flight Manual Supplement, Publication No. 27-5130-19-00, dated October 17, 1983, or later FAA approved revision is required with this installation.

The approval of this change in type design appliesbasically to Model SA365N only. This approval should not be extended to other aircraft of this model on which other previously approved modificationsare incorporated unlessit is determined by the installer that the interrelationship between this change any any of those other previously approved modificationswill not introduce any adverse effect upon the airworthinessof the aircraft. This determination should include consideration of significant changes in weight distribution such asan increase in the fixed disposable weight in the fuselage.

Date of Application: July 20, 1982 October 31, 1985, April 8, 1987, Date Reissued: February 11, 2009, March 19, 2020 Date of Issuance: October 18, 1983

Signature

Title Richard B. Sleigh ODA Administrator, ODA-602216-NM

United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate Page 2 of 3 FAA Form 8110-2 (5/14)

To (Name and address of transferee)

From (Name and address of grantor)

FAA Form 8110-2 (5/14) Page 3 of 3

(Continuation Sheet) Number: SH2216NM

Limitationsand Conditions: (continued) If the holder agrees to permit another person to use this certificate to alter the product, the holder shall give the other person written evidence of that permission.

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## Every issue (2)

- March 18, 2020: Reissued, Current. [certificate](https://openairdocs.org/files/sha256/df/38/df389566515d6ac7d144c53825ab9041d8d7263d38c542f1e1c120897bf9d514)
- February 11, 2009: Reissued, Historical. [certificate](https://openairdocs.org/files/sha256/f6/fb/f6fb9a6349f0a35a15f441552675a77cc8fabdb24c6346b9e80cb50ba6d42c64)

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