# STC SA00082MC - Type: Supplemental type certificate - Status: Current, Reissued - Holder: L-3 Communications Integrated Systems LP, United States - Description: Installation of communication and surveillance equipment - Applied: June 29, 2011 - Status date: November 6, 2012 - Product: Aircraft, Small/Large Airplane - Certification basis: Part 21, Part 23 - Data sheets: [TCDS A24CE](https://openairdocs.org/tcds/A24CE) - Certificate PDF: https://openairdocs.org/files/sha256/42/28/42288db7745242e50d368ea786c0255ca79d97fa8f801d8dbc81c4c81304d5c7 - FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/E0921DFA978E421986257B120051DE2F.0001 - DRS record last changed: December 5, 2025 - Page: https://openairdocs.org/stc/SA00082MC ## ADs that name it (0) None. ## Approved models (1) - Textron Aviation Inc. 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 SA00082MC 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 *SEE PAGE 3 Make : Hawker Beechcraft Corporation Model : B300 Description of Type Design Change: Installation of communication and surveillance equipment in accordance with (1) L-3 Communications Integrated Systems, L.P. Sealed Drawing List SDL 18267-1 Revision C dated 04 Sept 2012, (2) L-3 Flight Manual Supplement dated Aug. 2012, or (3) later FAA/ODA approved revisions of (1) and/or (2). Limitations and Conditions: 1. This 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. (Limitations and Conditions continued on page 3 of 3) Date of application : 29 June 2011 Date reissued : 06 Nov 2012 Date of issuance : 06 Sept 2012 Date amended : Dr. Michael E. Hopper ( Signature) ODA-750173-SW Administrator (Title) Transfer the ownership of Supplemental Type Certificate Number to (Name of transferee) (Address of transferee) (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): Number SA00082MC Date of Reissuance: 06 November 2012 Limitations and Conditions: (Continued) 2. Instructions for Continued Airworthiness (ICA), L-3 Communications Integrated Systems, Document No. G18267.28.08 Revision -, dated 23 March 2012, or later FAA accepted revision must be made available to the operator at the time of installation. 3. 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. 4. This airplane is restricted from flight in known icing conditions. 5. Flight Environments STC SA00087MC is a prerequisite for this STC. 6. In accordance with FAA Order 8110.101 the ALE 47 self protect flare dispensers and the MX-15 HD, are installed under a limited approval. The ARC-231 radios, 96 MP LDG and AWAPS systems are installed non-operational, as safe carriage equipment. 7. This STC includes provisions for installation in the mission system equipment racks of the ARC-231 radio, Blue Force Tracker, Data Management, Primary Mission Equipment, TCDL, and SAT Phone. The equipment for which these provisions are intended have not been certified. Additional FAA approval is required for the installation of this equipment and must be evaluated to assure satisfactory compliance with the applicable airworthiness standards. Certification Basis: Based on 14 CFR ยงยง 21.115 and 21.101, the certification basis for the Hawker Beechcraft B300 aircraft is as follows: a. The type certification basis for Hawker 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, 29 June 2011, is as shown in TCDS A24CE plus later amendment levels for the following paragraphs: 14 CFR Part 23, effective February 1, 1965 including the latest applicable requirements of Amendments 23- 1 through 23-59. The following lists the applicable regulations for this change through Amendment 23-59: 23.23 23.29 23.45 23.51 23.55 23.65 23.67 23.77 23.141 23.171 23.201 23.207 23.251 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 23.783 23.787 23.803 23.807 23.811 23.813 23.815 23.853 23.863 23.867 23.1301 23.1307 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 23.1447 23.1449 23.1501 23.1524 23.1529 23.1541 23.1555 23.1557 23.1561 23.1581 23.1583 23.1585 23.1587 --------------------------------------------------END----------------------------------------------- ## Every issue (2) - November 6, 2012: Reissued, Current. [certificate](https://openairdocs.org/files/sha256/42/28/42288db7745242e50d368ea786c0255ca79d97fa8f801d8dbc81c4c81304d5c7) - September 6, 2012: Issued, Historical. [certificate](https://openairdocs.org/files/sha256/8f/2c/8f2c9c8ddf4ed8954e7cf6f8aeb13ec7bb3305eb531e1a5f43f783d2e8d6a0cb) --- 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.