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>5985 HARTZELL SERVICE CENTER <strong>EASA</strong>.IM.A.S.02138 FAA STC SA<strong>01</strong>024CH PIPER PA-28R-2<strong>01</strong>T<br />
Installation of a Hartzell PHC-C3YF-<br />
The aircraft complies with annex 16, volume I,<br />
09.11.2006<br />
PIPER PA-28RT-2<strong>01</strong>T<br />
1RF/F7663-4T propeller and C-3570(P) third edition, amendment 7, chapter 6. The<br />
spinner in accordance with Hartzell installation certified noise level is 75.1 dB(A) at 2575<br />
instructions HP2834 dated February 3, 1999 or rpmThis STC is approved only for the product<br />
later approved revision (validation of FAA STC configuration as defined in the approved design<br />
SA<strong>01</strong>024CH)<br />
data referred to in the parag<br />
10<strong>01</strong>6516 HARTZELL SERVICE CENTER <strong>EASA</strong>.IM.A.S.02887 FAA STC SA2078CH CESSNA R172K Installation of a Hartzell Propeller Inc. 75” This STC is compatible with STC SA1437CE<br />
Diameter 3-Blade Propellermodel (P)HC-C3YF- that installs the TCM IO-360-K, or –KB, engine<br />
1RF/F7392 with A-2295-1(P) spinneror model as modified by STC SE1436CE. The re-rated<br />
(P)HC-G3YF-1RF/F7392 with C-4582-(P) engine is designated IO-360-KC, or –KBC,<br />
spinneron a Cessna R172K (Hawk XP) which increases the power rating to<br />
Landplane aircraft.<br />
210hp@2800 rpm for five minutes at takeoff<br />
and 1<br />
10<strong>01</strong>5337 HAWKER BEECHCRAFT<br />
CORPORATION<br />
10<strong>01</strong>5472 HAWKER BEECHCRAFT<br />
CORPORATION<br />
10<strong>01</strong>5473 HAWKER BEECHCRAFT<br />
CORPORATION<br />
10<strong>01</strong>5644 HAWKER BEECHCRAFT<br />
CORPORATION<br />
10<strong>01</strong>5861 HAWKER BEECHCRAFT<br />
CORPORATION<br />
10<strong>01</strong>5862 HAWKER BEECHCRAFT<br />
CORPORATION<br />
10<strong>01</strong>5863 HAWKER BEECHCRAFT<br />
CORPORATION<br />
10<strong>01</strong>5864 HAWKER BEECHCRAFT<br />
CORPORATION<br />
10<strong>01</strong>5865 HAWKER BEECHCRAFT<br />
CORPORATION<br />
10<strong>01</strong>5866 HAWKER BEECHCRAFT<br />
CORPORATION<br />
10<strong>01</strong>5867 HAWKER BEECHCRAFT<br />
CORPORATION<br />
10<strong>01</strong>5868 HAWKER BEECHCRAFT<br />
CORPORATION<br />
10<strong>01</strong>5869 HAWKER BEECHCRAFT<br />
CORPORATION<br />
10<strong>01</strong>5870 HAWKER BEECHCRAFT<br />
CORPORATION<br />
<strong>EASA</strong>.IM.A.S.00364 REV. 2 FAA STC SA2824SW-D BAE 125 SERIES 800A<br />
HAWKER 800, 800XP, 850XP<br />
HAWKER HS 125-700<br />
<strong>EASA</strong>.IM.A.S.<strong>01</strong>224 REV. 3 FAA STC ST10385SC-D HAWKER 800 XP<br />
HAWKER 850 XP<br />
HAWKER 900 XP<br />
<strong>EASA</strong>.IM.A.S.<strong>01</strong>225 REV. 3 FAA STC ST10369SC-D HAWKER 750<br />
HAWKER 800 XP<br />
HAWKER 850 XP<br />
HAWKER 900 XP<br />
05.08.2008<br />
Installation of a Long Range Oxygen System This STC is approved only for the product Prior to installation of this modification the 18.02.2<strong>01</strong>0<br />
configuration as defined inthe approved design installer must determinethat the<br />
data referred to in the paragraph<br />
interrelationship between this modification<br />
"Description".Compatibility with other and any otherpreviously installed<br />
aircraft/engine configurations shall<br />
modification will introduce no adverse<br />
bedetermined by the installer.<br />
effect uponthe airworthiness of the<br />
product.<br />
Installation of a Rockwell Collins CMS-1 Cabin<br />
Management System.<br />
<strong>EASA</strong>.IM.A.S.<strong>01</strong>608 FAA STC ST<strong>01</strong>342WI-D HAWKER 800 XP Installation of Collins Integrated Flight<br />
Information System (IFIS 5000) and Pro Line<br />
21 Radios<br />
<strong>EASA</strong>.IM.A.S.<strong>01</strong>974 REV. 2 FAA STC ST10066SC-D HAWKER 800 XP<br />
HAWKER 850 XP<br />
HAWKER 900 XP<br />
<strong>EASA</strong>.IM.A.S.<strong>01</strong>975 REV. 1 HAWKER 800 XP<br />
HAWKER 850 XP<br />
<strong>EASA</strong>.IM.A.S.<strong>01</strong>976 REV. 2 FAA STC ST1<strong>01</strong>08SC-D HAWKER 800 XP<br />
HAWKER 850 XP<br />
HAWKER 900 XP<br />
<strong>EASA</strong>.IM.A.S.<strong>01</strong>977 REV. 2 FAA STC ST1<strong>01</strong>09SC-D HAWKER 800 XP<br />
HAWKER 850 XP<br />
HAWKER 900 XP<br />
<strong>EASA</strong>.IM.A.S.<strong>01</strong>978 REV. 2 FAA STC ST1<strong>01</strong>28SC-D HAWKER 800 XP<br />
HAWKER 850 XP<br />
HAWKER 900 XP<br />
<strong>EASA</strong>.IM.A.S.<strong>01</strong>979 ST1<strong>01</strong>89SC HAWKER 800 XP<br />
HAWKER 850 XP<br />
<strong>EASA</strong>.IM.A.S.<strong>01</strong>980 REV. 2 FAA STC ST1<strong>01</strong>87SC-D HAWKER 800 XP<br />
HAWKER 850 XP<br />
HAWKER 900 XP<br />
<strong>EASA</strong>.IM.A.S.<strong>01</strong>982 ST1<strong>01</strong>90SC HAWKER 800 XP<br />
HAWKER 850 XP<br />
<strong>EASA</strong>.IM.A.S.<strong>01</strong>984 REV. 3 FAA STC ST09262SC-D HAWKER 750, 800XP, 850XP,<br />
HAWKER 900XP<br />
1. This modification requires installation of<br />
STC ST10369SC-D, Installation of an<br />
Emergency Light System;<br />
Installation of an Emergency Light System. Prior to installation of this modification the<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 install<br />
Installation of B.F. Goodrich WX-1000E<br />
Stormscope.<br />
1. Prior to installation and approval of<br />
Raytheon Aircraft Company Kit 149-3419-00<strong>01</strong><br />
is prerequisite to this STC.2. Prior to<br />
installation and approval of Rautheon Aircraft<br />
Company Kit 149-3420-00<strong>01</strong> is prerequisite to<br />
this STC.3. This STC is approv<br />
21.05.2008<br />
21.05.2008<br />
19.10.2005<br />
20.05.2008<br />
Installation of a Davtron Clock 23.06.2008<br />
Installation of a Cockpit Speaker Volume<br />
Recalibration.<br />
20.05.2008<br />
Installation of a Cockpit Speaker Inhibit Switch. 21.05.2008<br />
Installation of a Precise Flight Pulselight<br />
System Activated by (existing) TCAS.<br />
Installation of Digital Passenger Briefing<br />
System<br />
Installation of a Satellite Communications<br />
System.<br />
21.05.2008<br />
-- 18.09.2006<br />
Installation of CMS 400 Checklist Management --<br />
System<br />
19.09.2006<br />
Installation of a Third and Fourth 750 Liter -1<strong>01</strong> and -103 installation: Model Hawker 750; Prior to installation of this modification the 18.02.2<strong>01</strong>0<br />
Oxygen Bottle in AftEquipment Bay.<br />
Hawker 800XP; Hawker 850XP-105<br />
installer must determinethat the<br />
installation: Model Hawker 900XP<br />
interrelationship between this modification<br />
and any otherpreviously installed<br />
modification will introduce no adverse<br />
effect uponthe airworthiness of the<br />
product.<br />
<strong>EASA</strong>.IM.A.S.<strong>01</strong>985 REV. 4 FAA STC ST09651SC HAWKER 750 Installation of Cabin Interior and Avionics 1. Hawker 750 with 238M530760-0<strong>01</strong>7 and -<br />
15.12.2008<br />
Systems<br />
0<strong>01</strong>9 installations only, are limited to a<br />
maximum of 10 passengers.2. Prior to<br />
installation of this modification the installer must<br />
determine that the interrelationship between<br />
this modification andany other previous<br />
<strong>04</strong>/<strong>01</strong>/2<strong>01</strong>3 <strong>Page</strong> 261/<strong>462</strong><br />
21.05.2008
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