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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>6938 HELI-LYNX <strong>EASA</strong>.IM.R.S.<strong>01</strong>326 TCCA STC SH05-20 ISSUE 2 EUROCOPTER FRANCE AS 350 AS350/AS355 Rear Shoulder Harness Installation of a Rear Shoulder Harness on<br />

<strong>04</strong>.09.2007<br />

EUROCOPTER FRANCE AS 350 Installation.(Modiciation approved by TCCA AS350B3 with the modification OP-3369<br />

B1<br />

EUROCOPTER FRANCE AS 350<br />

B2<br />

EUROCOPTER FRANCE AS 350<br />

B3<br />

EUROCOPTER FRANCE AS 350<br />

BA<br />

EUROCOPTER FRANCE AS 350<br />

C<br />

EUROCOPTER FRANCE AS 350<br />

D<br />

EUROCOPTER FRANCE AS 350<br />

D1<br />

EUROCOPTER FRANCE AS<br />

350B<br />

EUROCOPTER FRANCE AS 355<br />

SERIE<br />

EUROCOPTER FRANCE AS<br />

355E<br />

EUROCOPTER FRANCE AS<br />

355F<br />

EUROCOPTER FRANCE AS<br />

355F1<br />

EUROCOPTER FRANCE AS<br />

355F2<br />

EUROCOPTER FRANCE AS<br />

355N<br />

under STC SH05-20 Issue 2.)<br />

incorporated is not approved.<br />

10035276 HELI-ONE TCCA STC SH05-46 S-61N Sealed Lead Acid Battery Installation 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 />

15.06.2<strong>01</strong>1<br />

10027687 HELI-ONE (NORWAY) AS P-<strong>EASA</strong>.R.S.<strong>01</strong>307 AS332C<br />

AS332C1<br />

AS332L<br />

AS332L1<br />

10036393 HELI-ONE (NORWAY) AS AS332 L1/L2 Installation of STAR SAFIRE FLIR system<br />

consisting of external mount,internal and<br />

external cabling and installation of mission<br />

console inCabin.<br />

EFIS 520 Installation. None. Prior to installation of this modification the 21.10.2009<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.<br />

Flight into known Icing Conditions prohibited. 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 />

06.09.2<strong>01</strong>1<br />

10<strong>04</strong>0394 HELI-ONE (NORWAY) AS AS 332 L, AS 332 L1 Goodrich Dual Hoist Installation 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 />

29.06.2<strong>01</strong>2<br />

10037034 HELI-ONE CANADA INC. S-61L & N Lower Housing Weld Repair Applicable only to Sikorsky S-61N Lower<br />

Housing Assembly Part No'sS6135-20670-9,<br />

S6135-20670-42, S6135-20670-43, S6135-<br />

20629-102,S6135-20629-1<strong>04</strong>.<br />

10<strong>01</strong>6796 HELI-ONE NORWAY AS <strong>EASA</strong>.IM.R.S.<strong>01</strong>149 - AS 332 L1 BPOL 332L1 Police equipment Installation Helicopter modified in accordance with this<br />

STC are not approved for NVG operations<br />

Prior to installation of this modification it 26.10.2<strong>01</strong>1<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 />

<strong>04</strong>/<strong>01</strong>/2<strong>01</strong>3 <strong>Page</strong> 271/<strong>462</strong><br />

12.06.2006

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