# STC SA00240BO

- Type: Supplemental type certificate
- Status: Current, Issued
- Holder: Northrop Grumman Corporation 
California Microwave Systems, United States
- Description: Installation of Auxiliary Aircraft Power System
- Applied: June 22, 2005
- Status date: December 18, 2006
- 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/sha256/63/a1/63a12335d19bbf826feb55478b1d50327757c4a7d26045e1a1bd170db99bb11f
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/FB5E6119E97AF8E5862572510059C16F.0001
- DRS record last changed: December 5, 2025
- Page: https://openairdocs.org/stc/SA00240BO

## ADs that name it (0)

None.

## Approved models (2)

- Raytheon Aircraft Company 300 ([TCDS A24CE](https://openairdocs.org/tcds/A24CE))
- Raytheon Aircraft Company B300 ([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.

FAA Form 8110-2(10-68) Page 1 of 2 Number SA00240BO This Certificate issued to Northrop Grumman Corporation 18450 Showalter Road Hagerstown, MD 21742

Part 23 of the Federal Aviation Regulations.

Original Product Type Certificate Number : A24CE Make : Raytheon Model : 300, B300

Installation of Auxiliary Aircraft Power System in accordance with Northrop Grumman Auxiliary Aircraft Power System Manufacturing Drawing List 360291DL Revision A, dated September 27, 2006, and Northrop Grumman Auxiliary Aircraft Power System Installation Drawing List 360290DL Revision B, dated October 23, 2006.

1. Northrop Grumman Airplane Flight Manual Supplement, Report No. 360203ER, Revision -, dated December 18, 2006, or later FAA-approved revision is required and must be carried in the aircraft during all flights.

2. Instructions for Continued Airworthiness, Report No. 360208ER, Revision C, dated August 3, 2006, or later FAA- accepted revision, shall be made available to the operator at the time of installation.

3. Compatibility of this design with previously approved modifications must be determined by the installer.

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 : June 22, 2005

Date of issuance : December 18, 2006

( Signature) Robert G. Mann Manager Boston Aircraft Certification Office

( Title)

Certification Basis :

Regulations at the amendment level in TCDS A24CE:

23.561 Regulations at the latest amendment 23-1 through 23-54:

23.1, 23.29, 23.301, 23.303, 23.305, 23.307, 23.333, 23.337, 23.341, 23.365, 23.571, 23.573, 23.574, 23.575, 23.601,

23.603, 23.605, 23.607, 23.609, 23.613, 23.619, 23.621, 23.623, 23.627, 23.773, 23.777, 23.901, 23.1163, 23.1191,

23.1193, 23.1301, 23.1309, 23.1322, 23.1327, 23.1351, 23.1353, 23.1357, 23.135,9 23.1361, 23.1365, 23.1367,

23.1431, 23.1501, 23.1529, 23.1541, 23.1547, 23.1555, 23.1581, 23.1583, 23.1585, 23.1587

--------------------------------------------------------END--------------------------------------------------------

## Every issue (1)

- December 18, 2006: Issued, Current. [certificate](https://openairdocs.org/files/sha256/63/a1/63a12335d19bbf826feb55478b1d50327757c4a7d26045e1a1bd170db99bb11f)

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