What it approves
Replacement of the original Pratt and Whitney PT6A-114(A) engine and propeller with a Pratt and Whitney PT6A-140 and 3-blade Hartzell Propeller HC-B3TN-3AF(Y)/T10890CN(K)-2, also Ametek MG94K-2 325 AMP Starter Generator, Howell Instruments powerplant indicating system, and associated equipment
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 23* of the Federal Aviation Regulations. *Certification basis set forth on continuation sheet 2 Original Product Type Certificate Number :
A37CE
Cessna
208, 208B Description of Type Design C hange: Replacement of the original Pratt and Whitney PT6A-114(A) engine and propeller with a Pratt and Whitney PT6A -140 and 3 -blade Hartzell Propeller HC -B3TN-3AF(Y)/T10890CN(K)-2, also Ametek MG94K -2 325 AMP Starter Generator, Howell Instruments powerplant indicating system , and associated equipment in accordance with FAA Approved Master Drawing List 201321-000, Rev IR, dated April 6, 2015, or later FAA approved revisions , Pilot’s Operating Handbook and FAA Approved Airplane Flight Manual Supplement s, AFMS 201321-208, Rev IR, dated October 09, 2015, or 201321-208B, Rev IR, dated October 09, 2015 or later FAA approved revisions. Instructions for Continued Airworthiness are contained in document ICA 201321- 30, Rev IR , dated August 2015, or later.
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 ai rworthiness of that aircraft . The approval of this modification applies to the 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 : June 30, 2014
Date of issuance : October 15, 2015
(Signature) Manager, Propulsion Branch Los Angeles Aircraft Certification Office (Ti l )
Number SA02546LA
Limitations and Conditions (continued)
• This modification is not compatible with Cessna Model 208, Serial Number 20800500 and greater or Cessna Model 208B Serial Number 208B1190, 208B1216, and 208B2000 and greater (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 23-62 for 23.1, 23.25, 23.29, 23.33, 23.45, 23.53, 23.63, 23.65,
23.69, 23.75, 23.77, 23.143, 23.145, 23.161, 23.171, 23.173, 23.175, 23.177, 23.201, 23.203,
23.207, 23.251, 23.301, 23.303, 23.305, 23.307, 23.361, 23.363, 23.601, 23.603, 23.605,
23.607, 23.609, 23.611, 23.613, 23.619, 23.625, 23.627, 23.629, 23.863, 23.865, 23.901,
23.903, 23.905, 23.907, 23.925, 23.929, 23.933, 23.937, 23.939, 23.943, 23.993, 23.997,
23.1011, 23.1017, 23.1021, 23.1023, 23.1027, 23.1041, 23.1043, 23.1045, 23.1091, 23.1093,
23.1103, 23.1121, 23.1123, 23.1141, 23.1143, 23.1145, 23.1149, 23.1153, 23.1155, 23.1163,
23.1165, 23.1183, 23.1193, 23.1301, 23.1305, 23.1309, 23.1351, 23.1353, 23.1357, 23.1359,
23.1361, 23.1365, 23.1367, 23.1519, 23.1529, 23.1541, 23.1549, 23.1581, 23.1583, 23.1585,
23.1587, except 23.1419 as amended by 23-1 through 23-14.
1. Special Condition 23-ACE-3, Dynamic Evaluation, Engine Installation. Factors from this special condition were incorporated into the whirl mode flutter analysis per 14 CFR
23.629(a)(b)(c)(e)(1) and (2).
2. Title 14 CFR 34, effective January 1, 1994, as amended by Amendment 34-0.
3. Title 14 CFR 36, effective December 1, 1969, as amended through Amendment 36-30.
-END-
ADs that name this STC · 0
An AD can apply because an STC is installed, or mention one in its text.