# STC SA1773NM

- Type: Supplemental type certificate
- Status: Current, Amended
- Holder: Ray Raineri, United States
- Description: Installation of a Lycoming IO-540-K1A5 engine.
- Applied: January 19, 1982
- Status date: January 13, 1998
- Product: Aircraft, Small Airplane
- Certification basis: Part 21
- Data sheets: [TCDS 3A15](https://openairdocs.org/tcds/3A15)
- Certificate PDF: https://openairdocs.org/files/sha256/28/4f/284fc7b01bffe2dbf19502f1f2571aa29d622c243a08e32336c525569db499db
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/164CDE3B0C7C9876862579FE00563D2C.0001
- DRS record last changed: December 5, 2025
- Page: https://openairdocs.org/stc/SA1773NM

## ADs that name it (0)

None.

## Approved models (10)

- Hawker Beechcraft Corporation H35 ([TCDS 3A15](https://openairdocs.org/tcds/3A15))
- Hawker Beechcraft Corporation J35 ([TCDS 3A15](https://openairdocs.org/tcds/3A15))
- Hawker Beechcraft Corporation K35 ([TCDS 3A15](https://openairdocs.org/tcds/3A15))
- Hawker Beechcraft Corporation M35 ([TCDS 3A15](https://openairdocs.org/tcds/3A15))
- Hawker Beechcraft Corporation N35 ([TCDS 3A15](https://openairdocs.org/tcds/3A15))
- Hawker Beechcraft Corporation P35 ([TCDS 3A15](https://openairdocs.org/tcds/3A15))
- Hawker Beechcraft Corporation S35 ([TCDS 3A15](https://openairdocs.org/tcds/3A15))
- Hawker Beechcraft Corporation V35 ([TCDS 3A15](https://openairdocs.org/tcds/3A15))
- Hawker Beechcraft Corporation V35A ([TCDS 3A15](https://openairdocs.org/tcds/3A15))
- Hawker Beechcraft Corporation V35B ([TCDS 3A15](https://openairdocs.org/tcds/3A15))

## What the certificate says

This is OCR from the scanned FAA certificate. OCR can misread letters and numbers.

Book United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate Number: SA1773NM This certificate issued to: Ray Raineri Box #57 Pavas 1200 San Jose, Costa Rica C.A.

Certifies that the change in the type design for the following product with the limitations and conditions therefor as specified herean meets the airworthiness requirement's of Part 3 of the Civil Air Regulations.

Original Product -Type Certificate Number 3A15 Make: Beech Model: H35 through V35B Description of Type Design Change: Installation of a Lycoming 10-540-K1A5, -K1A5D, -K1F5, -K1F5D, -K1G5, -K1G5D, or -S1A5 engine, Hartzell HC-F2YR-1BF/F8475D-4 (2-blade) or Hartzell HC-F3YR-1RF/F8468A- 8Q (3-blade) propeller, and associated systems in accordance with Raineri Super B Installation Document No.

82FS04401 (Revision A).

NOTE: Beech Models H35 through M35 require the installation of the same elevator control cable and bob-weight systems as applied by Beech on Models N35 and after. (Refer to Beech Parts Manual 35-590015-9C, Fig. 28, Item 3A).

Limitations and Conditions: . Approval of this change in type design applies to the above model aircraft only.

This approval should not be extended to other aircraft of these models on which other previously approved modifications are incorporated unless it is determined by the installer 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 and Airplane Flight Manual Supplement must be maintained as part of the permanent records for the modified aircraft.

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.

Date of Application: January 19, 1982 Date Reissued:

Date of Issuance: January 3, 1983 Date Amended: January 13, 1998 FEDERAL AVIATION r of the Administrator (Signature) Acting Manager, Seattle Aircraft TOMINIST RATION Certification Office (Title)

## Every issue (1)

- January 13, 1998: Amended, Current. [certificate](https://openairdocs.org/files/sha256/28/4f/284fc7b01bffe2dbf19502f1f2571aa29d622c243a08e32336c525569db499db)

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