# STC SA2400WE

- Type: Supplemental type certificate
- Status: Current, Reissued
- Holder: SOUTHWESTERN AERO EXCHANGE INC., United States
- Description: Installation of fiberglass nose cap left hand outer wing leading edge.
- Applied: August 5, 1971
- Status date: February 27, 2006
- Product: Aircraft, Small Multi-Engine
- Certification basis: Part 21
- Data sheets: [TCDS A-765](https://openairdocs.org/tcds/A-765)
- Certificate PDF: https://openairdocs.org/files/sha256/98/bf/98bf58a77e408d4739bff89ddf65d8664782b2ae1550b69d0d5e22295f775ec9
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/A4980C2EE810EC5086257130006244EF.0001
- DRS record last changed: December 5, 2025
- Page: https://openairdocs.org/stc/SA2400WE

## ADs that name it (0)

None.

## Approved models (1)

- Raytheon Aircraft Company G18S ([TCDS A-765](https://openairdocs.org/tcds/A-765))

## What the certificate says

Read from the PDF's text layer, without the form's printed wording; the layout is lost and the order can 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 -

## Every issue (1)

- February 27, 2006: Reissued, Current. [certificate](https://openairdocs.org/files/sha256/98/bf/98bf58a77e408d4739bff89ddf65d8664782b2ae1550b69d0d5e22295f775ec9)

---
OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.