# STC SA02523LA - Type: Supplemental type certificate - Status: Current, Issued - Holder: Blackhawk Modifications Inc., United States - Description: Replacement of the original Cessna Caravan 208 and 208B Starter/Generator with an AMETEK 325A Starter/Generator (MG94K-2) and associated equipment. - Applied: May 8, 2012 - Status date: November 10, 2014 - Product: Aircraft, Small Airplane - Certification basis: Part 21, Part 23 - Data sheets: [TCDS A37CE](https://openairdocs.org/tcds/A37CE) - Certificate PDF: https://openairdocs.org/files/sha256/69/1a/691aae99754b19a0458bf834fee85a9e67c5ae87d2d195edb7f533b9c2391e59 - FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/FBBF6D8D330CABAC86257D93005008AB.0001 - DRS record last changed: December 6, 2025 - Page: https://openairdocs.org/stc/SA02523LA ## ADs that name it (0) None. ## Approved models (2) - Cessna Aircraft Company 208 ([TCDS A37CE](https://openairdocs.org/tcds/A37CE)) - Cessna Aircraft Company 208B ([TCDS A37CE](https://openairdocs.org/tcds/A37CE)) ## 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 Blackhawk Modifications Inc. 7601 Karl May Drive Waco, Texas 76708 Part 23* of the Federal Aviation Regulations. *Certification basis set forth on continuation sheet 3 Original Product Type Certificate Number : A37CE Cessna 208, 208B Description of Type Design C hange: Replacement of the original Cessna Caravan 208 and 208B Starter/Generator with an AMETEK 325A Starter/Generator (MG94K -2) and associated equipment. Equipment is in accordance with FAA Approved Master Drawing List 201207-000, Rev IR, dated May 3 0, 2014, or later FAA approved revisions, Pilot’s Operating Handbook and FAA Approved Airplane Flight Manual Supplements, AFMS 201207, Rev IR, dated November 6, 2014, or later FAA approved revisions , and Blackhawk Modifications Inc. Instructions for Contin ued Airworthiness document ICA 201207-30, Rev IR, dated August 29, 2014, or later revisions. Limitations and Conditions : The installation should not be incorporated in any aircraft unless it is determined that the interrelationship between this insta llation and any previously approved configuration will not introduce any adverse effect upon the airworthiness of that aircraft . The approval of this modification applies to t he above -noted airplane models only. 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. (CONTINUED on page 3) Date of application : May 8, 2012 Date of issuance : November 10, 2014 (Signature) Manager, Propulsion Branch Los Angeles Aircraft Certification Office (Title) United States Of America Department of Transportation - Federal Aviation Administration Supplemental Type Certificate Number SA02523LA (Continuation Sheet) Limitations and Conditions(continued) • This modification must be installed in conjunction with Blackhawk STC SA02467LA (208) or Blackhawk STC SA02357LA (208B). • This modification and applicable supplements must be accompanied by the Pilot’s Operating Handbook and FAA Approved Airplane Flight Manual, Document Numbers D1307-34-13PH or D1352-7-13PH and applicable Supplements for Blackhawk STC SA02467LA (208) or D1309-29-13PH or D1329-23-13PH and applicable Supplements for Blackhawk STC SA02357LA (208B). • This modification is not compatible with Cessna Model 208 Serial Number 2080500 and greater or Cessna Model 208B Serial Number 208B2000 and greater, aircraft equipped with Garmin 1000 installations, and aircraft equipped with TKS installation. Certification Basis The certification basis for this modification is as follows: 14 CFR part 23 of the Federal Aviation Regulations effective February 1, 1965, as amended by Amendments 23-1 through 23-53 for 23.1, 23.29, 23.901, 23.1041, 23.1043, 23.1045, 23.1163, 23.1301, 23.1309, 23.1351, 23.1357, 23.1359, 23.1365, 23.1367, 23.1519, 23.1529, 23.1581. -END- ## Every issue (1) - November 10, 2014: Issued, Current. [certificate](https://openairdocs.org/files/sha256/69/1a/691aae99754b19a0458bf834fee85a9e67c5ae87d2d195edb7f533b9c2391e59) --- 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.