What it approves
Installation of Blackhawk Ultra Electronics Engine Instrument.
What the certificate says
From the PDF’s text layer, without the form’s printed wording. Layout and order may differ; the PDF is the record.
This Certificate issued to Blackhawk Modifications Inc.
7601 Karl May Drive Waco, Texas 76708 Part of the Federal Aviation Regulations. *Certification basis set forth on continuation sheet 2 Original Product Type Certificate Number :
See Attached FAA Approved Model List (AML) for list of approved models and Applicable airworthiness regulations]
Description of Type Design Change: Installation of Ultra FlightLine powerplant indication system in accordance with FAA Approved Model List No. SA01946LA, dated October 8, 2008, or later FAA approved revision. Airplane Flight Manual (AFM) Supplement 55023-11, Revision B, dated September 30, 2008, or later FAA approved revision is required. Instructions for Continued Airworthiness, Document No. 200809- 30, Revision A, November 2009, or latest FAA accepted revision is required.
Installation of Howell Instruments powerplant indicating system in accordance with FAA Approved Model List No.
SA01946LA, dated October 8, 2008, or later FAA a pproved revision. Airplane Flight Manual Supplement 201406, Revision IR, dated 19 February 2015, or later FAA approved revision is required. Instructions for Continued Airworthiness, Document No. 201406-30, Revision IR, February 2015, or latest FAA accepted revision is required.
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 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 : August 29, 2005
Date of issuance : December 22, 2006
Date amended : October 8, 2008, March 2, 2015
(Signature) Manager, Propulsion Branch Los Angeles Aircraft Certification Office (Title)
Number SA01946LA Limitations and Conditions(continued)
The certification basis for this STC is the same as for the original certification basis for these model airplanes as defined in Approved Model List No. SA01946LA except for:
Title 14 CFR 23 §§ 23.1, 23.29, 23.301, 23.303, 23.305, 23.307, 23.363, 23.601, 23.627, 23.771,
23.1183, 23.1301, 23.1305, 23.1309, 23.1321, 23.1322, 23.1327, 23.1351, 23.1357, 23.1359,
23.1365, 23.1381, 23.1431, 23.1437, 23.1529, 23.1541, 23.1543, 23.1549, 23.1581, 23.1583 which are amended by Amendment 23-59.
-END-
ADs that name this STC · 0
An AD can apply because an STC is installed, or mention one in its text.
Approved models · 31
| Make | Model | Data sheet |
|---|---|---|
| Beechcraft Corporation | 200 | A24CE |
| Beechcraft Corporation | 200C | A24CE |
| Beechcraft Corporation | 200CT | A24CE |
Every issue · 4
DRS keeps each issue of an STC as its own record, with its own certificate and attachments.
| Date | Status | Files |
|---|---|---|
| May 12, 2016 | Amended, current | CertificateApproved model list |
| March 2, 2015 | Amended, earlier issue | CertificateApproved model list |
| October 8, 2008 | Amended, earlier issue | Certificate |
| December 22, 2006 | Issued, earlier issue | Certificate |