STC SA1773NM

Supplemental type certificate · Ray Raineri

Holder
Ray Raineri · United States
Status
Current · Amended
Status date
January 13, 1998
Applied
January 19, 1982
Product
Aircraft · Small Airplane
Certification basis
Part 21
Data sheet
TCDS3A15

From FAA DRS, with our copy of the certificate PDF. DRS record last changed December 5, 2025.

What it approves

Installation of a Lycoming IO-540-K1A5 engine.

What the certificate saysOCR

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)

ADs that name this STC · 0

An AD can apply because an STC is installed, or mention one in its text.

No AD in this release names this STC

Approved models · 10

MakeModelData sheet
Hawker Beechcraft CorporationH353A15
Hawker Beechcraft CorporationJ353A15
Hawker Beechcraft CorporationK353A15
Hawker Beechcraft CorporationM353A15
Hawker Beechcraft CorporationN353A15
Hawker Beechcraft CorporationP353A15
Hawker Beechcraft CorporationS353A15
Hawker Beechcraft CorporationV353A15
Hawker Beechcraft CorporationV35A3A15
Hawker Beechcraft CorporationV35B3A15