04/01/2013 Page 1/462 - EASA
04/01/2013 Page 1/462 - EASA
04/01/2013 Page 1/462 - EASA
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<strong>EASA</strong> STC no. STC holder Old STC ref. Revision Level Foreign/NAA STC ref. Model Description Limitations Conditions Date of issue<br />
10<strong>01</strong>5414 BLACKHAWK MODIFICATIONS Inc. <strong>EASA</strong>.IM.A.S.<strong>01</strong>134 REV. 1 FAA STC SA10341SC BEECH C90<br />
Installation of Pratt & Whitney PT6A-135A AFMS No 19003-00, Rev a, dated 7th october<br />
20.<strong>04</strong>.2006<br />
BEECH C90A<br />
engine with:1. Hartzell propellers HC-D4N- 20<strong>04</strong> or later approved revision is required for<br />
BEECH E90<br />
3C/D9290(S,K) with a diameter of 93 inches (4 the Raytheon C90, C90A or E90 airplane with<br />
blades) in accordance with Blackhawk Pratt & Whitney Canada PT6A-135A engines.<br />
Modification, Inc.Drawing No 19003-<strong>01</strong>, Rev B, Note that the shaft horspower is limited to 550<br />
dated 1st April 20<strong>04</strong>, "Installation Instruc at 1900 RPMEach engine mount mu<br />
10<strong>01</strong>6078 BLACKHAWK MODIFICATIONS Inc. <strong>EASA</strong>.IM.A.S.02262 FAA STC SA10567SC Installation of Pratt and Whitney PT6A-135A<br />
engines in place of PT6A-135 engines.<br />
10<strong>01</strong>6079 BLACKHAWK MODIFICATIONS Inc. <strong>EASA</strong>.IM.A.S.02263 REV. 1 FAA STC SA0<strong>04</strong>33AT BEECH 200C<br />
BEECH 200CT<br />
BEECH 200T<br />
10<strong>01</strong>6156 BLACKHAWK MODIFICATIONS Inc. <strong>EASA</strong>.IM.A.S.02359 REV. 2 FAA STC SA<strong>01</strong>946LA BEECH 200<br />
BEECH 200C<br />
BEECH 200CT<br />
BEECH 200T<br />
BEECH A200<br />
BEECH A200C<br />
BEECH A200CT<br />
BEECH B200<br />
BEECH B200C<br />
BEECH B200CT<br />
BEECH B200T<br />
BEECH C90<br />
BEECH C90A<br />
BEECH E90<br />
BEECH F90<br />
1. Installation limited to Serial Number LA-2<br />
thru LA-2<strong>04</strong>, except for LA-202.2.<br />
Compatibility of this modification with other<br />
previously approved modifications must be<br />
determined by the installer.3. This STC is<br />
approved only for the product config<br />
Installation of Pratt and Whitney PT6A-42<br />
engines in place of PT6A-41 engines. This<br />
project is to amend <strong>EASA</strong> TSC No.<br />
<strong>EASA</strong>.IM.A.S. 02263 using the data from the<br />
amended FAA-STC SA0<strong>04</strong>33AT dated 22.<br />
August 2007 to include Beechcraft Super King<br />
Air 200C, 200T<br />
Installation of Ultra Electronics Engine 1. Blackhawk Modifications, Inc. STC<br />
Instruments.Revision 1: Installation of SA10341SC or SA10364SC is a prerequisite<br />
powerplant indication system. This project is to for this modification.2. Prior to installation of<br />
amend <strong>EASA</strong> of <strong>EASA</strong> STC No.<br />
this modification the installer must determine<br />
<strong>EASA</strong>.IM.A.S.02359.<br />
that the interrelationship between this<br />
modification and any other previous<br />
10<strong>01</strong>6381 BLACKHAWK MODIFICATIONS Inc. <strong>EASA</strong>.IM.A.S.02705 REV. 1 FAA STC SA10560SC KING AIR C90GTI Installation of Wing Mounted Auxiliary Fuel<br />
Transfer Tank in BeechC90GTi. This project is<br />
to amend <strong>EASA</strong> STC No.<br />
<strong>EASA</strong>.IM.A.S.02705.<br />
10<strong>01</strong>6403 BLACKHAWK MODIFICATIONS Inc. <strong>EASA</strong>.IM.A.S.02732 REV. 1 FAA STC SA10737SC BEECH 200, 200C<br />
BEECH 200T, 200CT, A200,<br />
A200C<br />
BEECH A200CT, B200, B200C,<br />
BEECH B200CT, B200T<br />
10<strong>01</strong>6484 BLACKHAWK MODIFICATIONS Inc. <strong>EASA</strong>.IM.A.S.02839 FAA STC SA10824SC ; RICK RITZ BEECH 200<br />
BEECH 200C<br />
BEECH 200CT<br />
BEECH 200T<br />
BEECH B200<br />
BEECH B200C<br />
BEECH B200CT<br />
BEECH B200T<br />
Installation of Pratt and Whitney PT6A-61<br />
engines in Beech 200 Series.This project is to<br />
amend <strong>EASA</strong> STC No. <strong>EASA</strong>.IM.A.S. 02732.<br />
Upgrade Super King Air 200, A200 and B200<br />
Series King Airs to Pratt and Whitney Canada<br />
PT6A-52 engines.<br />
None Prior to installation of this modification the<br />
installer must determinethat the<br />
interrelationship between this modification<br />
and any otherpreviously installed<br />
modification will introduce no adverse<br />
effect uponthe airworthiness of the<br />
23.<strong>01</strong>.2007<br />
<strong>01</strong>.<strong>04</strong>.2008<br />
27.05.2009<br />
16.09.2<strong>01</strong>1<br />
product. The installati<br />
None Prior to installation of this modification the 05.07.2<strong>01</strong>0<br />
installer must determinethat the<br />
interrelationship between this modification<br />
and any otherpreviously installed<br />
modification will introduce no adverse<br />
effect uponthe airworthiness of the<br />
product. The installati<br />
Prior to installation of this modification the<br />
25.08.2008<br />
installer must determine that the<br />
interrelationship between this modification and<br />
any other previously installed modification will<br />
introduce no adverse effect upon the<br />
airworthiness of the product.The installa<br />
10<strong>01</strong>6559 BLACKHAWK MODIFICATIONS Inc. <strong>EASA</strong>.IM.A.S.02944 FAA STC SA5786SW CESSNA 425 Installation of Pratt and Whitney Canada PT6A - None.<br />
135A engines on Cessna Conquest 425<br />
airplanes.<br />
16.02.2009<br />
10031080 BLACKHAWK MODIFICATIONS Inc. <strong>EASA</strong>.IM.A.S.03186 FAA STC SA4705SW BEECH 65-A90, B90, C90 Upgrade King Air 65-A90, B90 and C90 Engines can be either type certified Pratt and Prior to installation of this modification it 26.07.2<strong>01</strong>0<br />
airplanes with PT6A-28 engines<br />
Whitney PT6A-27 orPT6A-28 engines, or must be determined thatthe<br />
converted PT6A-27 or PT6A-28 engines from interrelationship between this modification<br />
PT6A-21engines in accordance with Atlantic and any other previouslyinstalled<br />
Turbines International Inc STCSE02290NY, or modification and/ or repair will introduce<br />
converted PT6A-27 or PT6A-28 engines from no adverse effectupon the airworthiness<br />
of the product.The ins<br />
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