STC SA1533WE

Supplemental type certificate · Staggerwing Museum Foundation Inc.

Holder
Staggerwing Museum Foundation Inc. · United States
Status
Current · Reissued
Status date
September 3, 2004
Applied
May 23, 1967
Product
Aircraft · Small Multi-Engine
Certification basis
Part 3, Part 21
Data sheet
TCDSA-765

From FAA DRS, with our copy of the certificate PDF. DRS record last changed December 6, 2025.

What it approves

Spar reinforcement.

What the certificate says

From the PDF’s text layer, without the form’s printed wording. Layout and order may differ; the PDF is the record.

This Certificate issued to Staggerwing Museum Foundation, Inc.

560 Old Shelbyville Highway Tullahoma, TN 37388 Part 03 of the Civil Air Regulations, dated November 13, 1945, and Part 3 dated November 1, 1949 as amended by 3-14.

A-765 BEECH D18S, E18S, E18S-9700, G18S, H18, C45G, TC-45G, C-45H, TC-45H, SNB-5, JRB-6, 3N, 3NM, 3TM Description of Type Design Change: Spar reinforcement per FAA sealed Hamilton Aircraft Co.

(formerly identified under ATE Co.) top drawing No. 878.

Limitations and Conditions: See page 2s

Date of application : May 23, 1967

Date of issuance : October 20, 1967

Date reissued: May 17, 1971; April 28, 1977;

September 3, 2004

Date amended: May 17, 1971; August 15, 1973

( Signature)

Manager, Technical & Administrative Support Staff, Los Angeles Aircraft Certification Office ( Title)

Number SA1533WE

Limitations and Conditions:(Continued)

The approval of this change in type design applies basically to Beech Models:

D18S, E18S, E18S-9700, G18S, H18, C-45G, TC-45G, C-45H, TC-45H, SNB-5, JRB-6, 3N, 3NM and 3TM aircraft only. This approval should not be extended to other aircraft and these models on which other previously approved modifications are incorporated unless it is determined by the installer that the interrelationship between this change and any of those other previously approved modifications will introduce no adverse effect upon the airworthiness of that aircraft.

The special inspections of the lower spar cap required by AD 72-20-5 must be conducted at the time of installation of this modification.

This installation constitutes a reinforcement approved by Chief, Engineering and Manufacturing Branch, FAA Central Region, Kansas City, Missouri, and thereafter negates in the special inspection requirements of AD 72-20-5, provided 300 hour visual inspections are accomplished in the areas specified by AD 72-20-5.

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.

- END -

ADs that name this STC · 1

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

Approved models · 14

MakeModelData sheet
Raytheon Aircraft Company3NA-765
Raytheon Aircraft Company3NMA-765
Raytheon Aircraft Company3TMA-765
Raytheon Aircraft CompanyC-45GA-765
Raytheon Aircraft CompanyC-45HA-765
Raytheon Aircraft CompanyD18SA-765
Raytheon Aircraft CompanyE18SA-765
Raytheon Aircraft CompanyE18S-9700A-765
Raytheon Aircraft CompanyG18SA-765
Raytheon Aircraft CompanyH18A-765
Raytheon Aircraft CompanyJRB-6A-765
Raytheon Aircraft CompanyTC-45GA-765
Raytheon Aircraft CompanyTC-45HA-765
Raytheon Aircraft CompanyUC-45J (SNB-5)A-765