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 />
10028498 KEYSTONE HELICOPTER<br />
P-<br />
REV. 1 FAA STC SR<strong>01</strong>127NY-D S-76A, S-76B, S-76C Installation of a Keystone Medical Interior - See As specified in the approved RFMS. RFMS N° 00549 is required for this 03.02.2<strong>01</strong>0<br />
CORPORATION<br />
<strong>EASA</strong>.IM.R.S.<strong>01</strong>562<br />
Conditions<br />
installation with configurations 1,2,3,4,5<br />
and 6 The following configurations are<br />
approved for this installation:<br />
Configuration No. 1 -P/N 02076-10E000-<br />
1 Lifeport litter base installedwith one or<br />
two litters, control cab<br />
100285<strong>01</strong> KEYSTONE HELICOPTER<br />
CORPORATION<br />
10028503 KEYSTONE HELICOPTER<br />
CORPORATION<br />
10029641 KEYSTONE HELICOPTER<br />
CORPORATION<br />
10030668 KEYSTONE HELICOPTER<br />
CORPORATION<br />
P-<br />
<strong>EASA</strong>.IM.R.S.<strong>01</strong>563<br />
P-<br />
<strong>EASA</strong>.IM.R.S.<strong>01</strong>564<br />
FAA STC SR00910NY S-76A, S-76B, S-76C Structural provisions for the installation of a<br />
Spectrolab SX5Searchlight to the left or right<br />
side of the S76.<br />
FAA STC SR00642NY S-76A, S-76B, S-76C Installation of a Liquid Oxygen System for<br />
Medevac use<br />
As specified in the approved RFMS. This STC covers the structural provisions 18.<strong>01</strong>.2<strong>01</strong>0<br />
for the installation of an SX5searchlight.<br />
Wiring and associated control of the SX5<br />
and assessment ofthe effects on aircraft<br />
performance and handling must be the<br />
subject ofseparate modification action.<br />
Prior to ins<br />
- This approval should not be incorporated in<br />
any aircraft of thisspecific model on which<br />
other approved modifications are<br />
incorporated,unless it is determined that the<br />
interrelationship between this changeand any<br />
other previously incorporated approved mod<br />
Not Applicable 18.<strong>01</strong>.2<strong>01</strong>0<br />
FAA STC SR02588NY-D S-76C Installation of Goodrich Auxiliary Utility Hoist As specified in the approved RFMS Installation of the Auxiliary Hoist requires:<br />
1. Pre-installation of the Goodrich<br />
Primary Hoist p/n 42325-18-1<br />
inaccordance with Sikosrsky TC Option<br />
33776-061154.and 2. On aircraft with<br />
Turbomeca Arriel 1S1 or 2S1<br />
engines,pre-installation of FAA STC<br />
SR<strong>01</strong>61<br />
FAA STC SR02597NY-D S92A Installation of a tail mounted, forward facing<br />
camera.<br />
08.<strong>04</strong>.2<strong>01</strong>0<br />
None. Prior to installation of this modification it<br />
must be determined thatthe<br />
interrelationship between this modification<br />
and any other previouslyinstalled<br />
modification and/ or repair will introduce<br />
no adverse effectupon the airworthiness<br />
of the product.<br />
30.06.2<strong>01</strong>0<br />
10<strong>04</strong>1473 KMLEX AVIATION INC. TCCA STC Q-LSA10-<strong>04</strong>7/D FALCON 50EX Relocation of Radio Altimeter<br />
Restricted to S/N 278 Prior to installation of this modification it 19.09.2<strong>01</strong>2<br />
ConverterValidation of TCCA STC N° Q-<br />
must be determined thatthe<br />
LSA10-<strong>04</strong>7/D issue dated November <strong>04</strong>, 2<strong>01</strong>0.<br />
interrelationship between this modification<br />
and any other previouslyinstalled<br />
modification and/ or repair will introduce<br />
no adverse effectupon the airworthiness<br />
of the product.<br />
10<strong>04</strong>1475 KMLEX AVIATION INC. TCCA STC Q-LSA10-<strong>04</strong>8/D FALCON 50EX Replacement of Aft lavatory faucet adapter -<br />
Dassault Falcon 50EXaircraft MSN<br />
278Validation of TCCA STC N° Q-LSA10-<br />
<strong>04</strong>8/D issue dated November <strong>04</strong>, 2<strong>01</strong>0.<br />
10<strong>01</strong>5415 KNH AVIATION SERVICES, INC. <strong>EASA</strong>.IM.A.S.<strong>01</strong>136 FAA STC ST09993SC FAIRCHILD DORNIER DO 328-<br />
300<br />
FAA STC ST09993SC; 12 Seats configuration 1. This STC may be installed only in<br />
(extended to 14 seats throught minor change, combination with Change Notice CN-F0535, -<br />
part of Avcraft CN-F 0535)Installation of F0<strong>04</strong>0,-F<strong>01</strong>25 owned by Avcraft Germany<br />
interior shell, cabinetry ,seats, card tables, and RUAG minor Changes “In Seat Power<br />
monitors, entertainment system, system wiring, Supply and FI Switch” and “Installation of<br />
and lavatory in accordance with<br />
Double Latches on drawers” .2. The water<br />
pumping syste<br />
10<strong>01</strong>5482 KNH AVIATION SERVICES, INC. <strong>EASA</strong>.IM.A.S.<strong>01</strong>242 FAA STC ST09468AC DORNIER D328-100 installation of a corporate/executive interior 1. According to the application as forwarded by<br />
FAA letter dated 27 April 2005 and FAA STC<br />
ST09468AC, the approval is limited to the<br />
aircraft S/N 30952. Furthermore this installation<br />
has to be performed in combination with the<br />
installation of FAA STC ST094<br />
Restricted to S/N 278 Prior to installation of this modification it<br />
must be determined thatthe<br />
interrelationship between this modification<br />
and any other previouslyinstalled<br />
modification and/ or repair will introduce<br />
no adverse effectupon the airworthiness<br />
of the product.<br />
19.09.2<strong>01</strong>2<br />
<strong>04</strong>/<strong>01</strong>/2<strong>01</strong>3 <strong>Page</strong> 299/<strong>462</strong><br />
20.06.2006<br />
15.08.2005
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