# STC SA00133MC

- Type: Supplemental type certificate
- Status: Current, Issued
- Holder: L-3 Communications Integrated Systems LP, United States
- Description: Installation of ISR Mission Related Systems
- Applied: September 10, 2014
- Status date: January 13, 2016
- Product: Aircraft, Small/Large Airplane
- Certification basis: Part 21, Part 23, Part 36
- Data sheets: [TCDS A24CE](https://openairdocs.org/tcds/A24CE)
- Certificate PDF: https://openairdocs.org/files/sha256/23/1d/231d0a6380f6055c6b25d07c87e74c642b998d3cee76ffc693f84b223a717eb2
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/8D09CAE6A03ED36886257F69006F7537.0001
- DRS record last changed: December 5, 2025
- Page: https://openairdocs.org/stc/SA00133MC

## ADs that name it (0)

None.

## Approved models (1)

- Beechcraft Corporation 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.

Number SA00133MC

This certificate issued to: L-3 Communications Integrated Systems, L.P.

10001 Jack Finney Blvd.

Greenville, TX 75402

Part 23 of the Federal Aviation Regulations.

Original Product – Type Certificate Number: A24CE Make: Beechcraft Corporation Model: B300

Installation of ISR Mission Related Systems in accordance with (1) L-3 Communications Integrated Systems, L.P. Sealed Drawing List 13125-1 Revision B dated 13 Jan 2016, (2) Instructions for Continued Airworthiness (ICA), L-3 Communications Document No. G13125.28.08 Revision NC dated 01 Sept 2015, (3) Flight Manual Supplement dated Sept 2015 or later FAA/ODA approved revisions of (1) (2) and/or (3).

(1) If the holder agrees to permit another person to use this certificate to alter a product, the holder must give the other person written evidence of that permission.

(Limitations and Conditions continued on page 3 of 3)

Date of application: 10 Sept 2014 Date reissued:

Date of issuance: 13 Jan 2016 Date amended:

Signature

Title ODA-750173-SW Administrator Page 1 2 3 Amdt

FAA Form 8110-2 (5/14) Page 1 of 3

To (Name and address of transferee)

From (Name and address of grantor)

FAA Form 8110-2 (5/14) Page 2 of 3

Number: SA00133MC Date of Issuance: 13 Jan 2016 Limitations and Conditions: (Continued)

(2) The installer must determine whether this design change is compatible with previously approved modifications.

(3) This installation is only eligible on Beechcraft B300 aircraft that have been modified per Beechcraft Kit Drawing 130-3052- 0001.

(4) This installation is only eligible on Beechcraft B300 aircraft that have been modified per Beechcraft Kit Drawing 130-3062.

(5) This installation is only eligible on Beechcraft B300 aircraft that have been modified per Beechcraft Kit Drawing 130-5200.

(6) This installation is only eligible on Beechcraft B300 aircraft that have been modified per Beechcraft Drawing 130M000030 or Kit Drawing 130-4014.

(7) Installation of STC SA4175NM is a prerequisite for this STC.

(8) Installation of STC SA01260WI is a prerequisite for this STC.

(9) Loading or dispensing of flares is not FAA approved or civil operations. The FAA certification does not connote FAA endorsement of the deployment of anti-missile pyrotechnic devices (flares) or the effectiveness of the equipment in countering a missile threat.

(10) Laser operation is not FAA approved or civil operations. The laser is electrically disabled.

Certification Basis:

Based on 14 CFR §§ 21.115 and 21.101, and the FAA policy for significant changes in FAA Order 8110.48, the certification basis for the Beechcraft B300 aircraft is as follows:

a. The type certification basis for Beechcraft B300 series airplanes is shown on TCDS A24CE for parts not changed or not affected by the change.

b. The certification basis for parts changed or affected by the change since the reference date of application, 10 Sept 2014, is as shown in TCDS A24CE plus later amendment levels for the following paragraphs:

14 CFR Part 23, effective Feb 1. 1965, including the latest applicable requirements of Amendments 23-1 through 23-62. The following list the applicable regulations for this change through Amdt. 23-62:

23.21, 23.29, 23.45, 23.51, 23.55, 23.65, 23.67, 23.77, 23.141, 23.171, 23.201, 23.207, 23.253, 23.301, 23.303, 23.305, 23.307, 23.321,

23.331, 23.333, 23.335, 23.337, 23.341, 23.347, 23.351, 23.365, 23.367, 23.441, 23.443, 23.471, 23.481, 23.483, 23.493, 23.573, 23.574,

23.575, 23.601, 23.603, 23.605, 23.607, 23.609, 23.611, 23.613, 23.619, 23.625, 23.627, 23.771, 23.773, 23.777, 23.783, 23.787, 23.791,

23.803, 23.807, 23.811, 23.813, 23.815, 23.851, 23.853, 23.856, 23.867, 23.1301, 23.1306, 23.1308, 23.1309, 23.1321, 23.1322, 23.1351,

23.1357, 23.1359, 23.1361, 23.1365, 23.1367, 23.1381, 23.1401, 23.1411, 23.1415, 23.1431, 23.1441, 23.1443, 23.1445, 23.1447, 23.1501,

23.1524, 23.1529, 23.1541, 23.1557, 23.1561, 23.1581, 23.1583, 23.1585, 23.1587.

Additional requirements to be maintained at an earlier amendment level of the regulation:

23.143 at Amdt 23.17, 23.147 at Amdt 23-0, 223.177 at Amdt 23-21, 23-181 at Amdt 23-21, 23.233 at Amdt 23-0, 23.251 at Amdt 23-45,

23.473 at Amdt 23-28, 23.479 at Amdt 23-17, 23.485 at Amdt 23-0, 23.561 at Amdt 23-34, 23.629 at Amdt 23-31, 23.785 at Amdt 23-34,

23.1353 at Amdt 23-49, 23.1413 at Amdt 23-22, and 23.1419 at Amdt 23-14.

14 CFR part 36, effective Dec 1 1969, including the latest applicable requirements of Amendments 36-28. The following list the applicable regulation for this change:

14 CFR Part 36.9 at Amdt 36-19.

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FAA Form 8110-2 (5/14) Page 3 of 3

## Every issue (1)

- January 13, 2016: Issued, Current. [certificate](https://openairdocs.org/files/sha256/23/1d/231d0a6380f6055c6b25d07c87e74c642b998d3cee76ffc693f84b223a717eb2)

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