STC SA2400WE

Supplemental type certificate · SOUTHWESTERN AERO EXCHANGE INC.

Holder
SOUTHWESTERN AERO EXCHANGE INC. · United States
Status
Current · Reissued
Status date
February 27, 2006
Applied
August 5, 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 5, 2025.

What it approves

Installation of fiberglass nose cap left hand outer wing leading edge.

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.

Number SA2400WE

This Certificate issued to Southwestern Aero Exchange, Inc.

18502 East 108th Street, North Owasso, OK 74055-8124 Part 03 of the Civil Air Regulations.

A-765 BEECH G18S Description of Type Design Change: The installation of fiberglass nose cap left hand outer wing leading edge per Aircraft Technical Service Drawing No. 1356.

Limitations and Conditions: This approval is limited to one airplane. Serial No. BA 463, N243B only because the data are not sufficiently complete for duplication in other aircraft.

This certificate and the supporting data, which is the basis for approval, shall remain in effect until surrendered, suspended, revoked or a termination date is otherwise established by the Administrator of the Federal Aviation Administration.

Date of application: 05 August 1971

Date of issuance: 06 August 1971

Date reissued: January 23, 1998; February 27, 2006

Date amended: October 26, 1973

( Signature)

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

NOTE:

DO NOT DELETE THIS PAGE.

DO NOT ADD ANY DATA TO THIS PAGE.

THIS PAGE IS FOR PAGE NUMBERING PURPOSES, PLEASE DISCARD PRINTED COPY.

Number SA111WE

Limitations and Conditions (Continued)

Gross weights in excess of those shown on aircraft specification A-765 but not in excess of 9772 lbs. landing and extension of rear C.G. extremes cannot be realized unless a gross weight basic modernization kit (STC SA2-820 or SA4-1462 or equivalent) is incorporated. FAA Approved Flight Manual dated 05/03/62 required as part of the installation. Airplane Flight Supplement revision dated 04/03/64 required when rear C.G. extremes are extended.

- 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 · 1

MakeModelData sheet
Raytheon Aircraft CompanyG18SA-765