STC SA2353WE

Supplemental type certificate · Staggerwing Museum Foundation Inc.

Holder
Staggerwing Museum Foundation Inc. · United States
Status
Current · Reissued
Status date
September 3, 2004
Applied
April 27, 1971
Product
Aircraft · Small Multi-Engine
Certification basis
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

Installation of cargo pod.

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, effective November 13, 1945, and Part 3 of CAR effective November 1, 1949, as amended by 3-14.

765 BEECH D18C, D18S, E18S, E18S-9700, G18S, H18, C-45G, TC-45G, C-45H, TC-45H, TC-45J (SNB-5), JRB-6, 3N, 3NM, 3TM

Description of Type Design Change: Installation of cargo pod in accordance with FAA Sealed Hamilton Aircraft Co. Inc. Drawing List No. 786.

(See Page 2)

Date of application : April 27, 1971

Date of issuance : June 16, 1971

Date reissued: August 10, 1971; April 28, 1977;

September 3, 2004

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

Number SA2353WE

D a t e : April 28, 1977; September 3, 2004 S T C : SA2353WE BEECH D18C, D18S, H18, C-45G, TC-45G, C-45H, TC-45H, TC-45J (SNB-5), JRB-6, 3N, 3NM, 3TM

SUPPLEMENTAL TYPE CERTIFICATE ADDENDUM NO. SA2353WE

Aircraft must incorporate the provisions of STC SA1016WE, conventional landing gear (tail wheel type), and Pratt and Whitney PT6A-20 engines. Aircraft must also incorporate a wing lower spar reinforcement equivalent to the provisions of STC SA2000WE. The cargo pod is limited to a maximum load of 1,000 lbs. (See FAA approved AFM Supplement, Hamilton Aviation Co.

Document No. D-127, to ATECO Basic Flight Manual No. 900-A).

The approval of this change in type design applies basically to the models listed 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 interrelationship between this change and any of those other previously approved modifications will introduce no adverse effect upon the airworthiness of that aircraft. This determination should include consideration of significant changes in weight distribution such as an increase in the fixed disposable weight in the fuselage. 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 · 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 · 15

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 CompanyD18CA-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 CompanyTC-45JA-765