# STC SA02332LA

- Type: Supplemental type certificate
- Status: Current, Issued
- Holder: L-3 Communications Integrated Systems LP, United States
- Description: Increase in maximum zero fuel weight
- Applied: July 22, 2010
- Status date: December 20, 2010
- Product: Aircraft, Large Multi-Engine
- Certification basis: Part 21, Part 23
- Data sheets: [TCDS A24CE](https://openairdocs.org/tcds/A24CE)
- Certificate PDF: https://openairdocs.org/files/sha256/de/11/de115e6bc5fa6e37e56a0bb279b3084f9d644826cb24395419629e89ab3bccb2
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/EE6BD7E5F8DF01D18625781000796558.0001
- DRS record last changed: December 6, 2025
- Page: https://openairdocs.org/stc/SA02332LA

## ADs that name it (0)

None.

## Approved models (2)

- Hawker Beechcraft Corporation B300 ([TCDS A24CE](https://openairdocs.org/tcds/A24CE))
- Hawker Beechcraft Corporation B300C (C-12W) ([TCDS A24CE](https://openairdocs.org/tcds/A24CE))

## 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.

This Certificate issued to L-3 Communications 10001 Jack Finney Blvd Greenville, Texas 75403 Part 23* of the Federal Aviation Regulations.

*C tifi ti b i i t f th i T C tifi t D t Sh t A24CEOriginal Product Type Certificate Number :

A24CE Hawker Beechcraft Corporation B300/B300C Description of Type Design Change: Increase in maximum zero fuel weight in accordance with FAA approved L-3 Communications Master Data List J2MDL 10-0024, Revision Original, dated December 15, 2010 and. or later FAA approved revisions. “Pilot’s Operating Handbook and FAA Approved Airplane Flight Manual Supplement” J2AFMS 10-0021-MZFW, Revision Original, dated December 17, 2010. or later FAA approved revisions is required as part of this installation.

Limitations and Conditions: The installation should not be incorporated in any aircraft unless it is determined that the interrelationship between this installation and any previously approved configuration will not introduce any adverse effect upon the airworthiness of the aircraft. A copy of this STC must be included in the permanent records of 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 : July 22, 2010

Date of issuance : December 20, 2010

( Signature) Manager, Airframe Branch Los Angeles Aircraft Certification Office ( Title)

Transfer the ownership of the Supplemental Type Certificate Number to (Name of transferee) (Address of transfer) (Number and street)

(City, State, and Zip code) from (Name of grantor) (Print or type) (Address of grantor) (Number and street)

(City, State, and Zip code) Extent of Authority (if licensing agreement):

Signature of grantor (In ink):

## Every issue (1)

- December 20, 2010: Issued, Current. [certificate](https://openairdocs.org/files/sha256/de/11/de115e6bc5fa6e37e56a0bb279b3084f9d644826cb24395419629e89ab3bccb2)

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