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 />
10027831 NORTHERN AVIONICS S.R.L. A109S NAV-396 "Installation of Helicopter Egress None. Prior to installation of this modification it 09.11.2009<br />
Light System (HEEL)"<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 />
10035325 NORTHERN AVIONICS S.R.L. REV. 1 AW109SP Installation of a Relay box and Control Panel<br />
for ICS VIP application.<br />
10035500 NORTHERN AVIONICS S.R.L. AB206B NAV 427 "Installation of Alternate Static This STC is applicable only to the helicopters<br />
System" - This kits consistsin the installation of S/Ns from 8590 to 8758.<br />
an additional line to the original static lineand a<br />
3-way valve/switch (with the air inlet port) to<br />
pick up the staticpressure in the cabin when the<br />
external ports<br />
10035741 NORTHERN AVIONICS S.R.L. REV. 1 AW109SP Installation of In-flight Entertainment System<br />
(IES) (composed by kitP/N KNAV-419 and<br />
KNAV-420) Certificate rev. 1 issued due to<br />
change of Modification BulletinRevision level.<br />
10036508 NORTHERN AVIONICS S.R.L. AW109SP NAV 434 "Installation of Helicopter Emergency<br />
Egress Light (HEEL)"<br />
10036765 NORTHERN AVIONICS S.R.L. P-<strong>EASA</strong>.R.S.<strong>01</strong>575 A109 AII Installation of a retractable swivelling landing<br />
light (searchlight).<br />
10039669 NORTHERN AVIONICS S.R.L. AW109SP Installation of In-flight Entertainment System<br />
(IES) (composed by KitPIN KNAV-419 and<br />
KNAV-442).<br />
10<strong>01</strong>5366 NORTHROP GRUMMAN GUIDANCE<br />
AND<br />
10<strong>01</strong>5825 NORTHROP GRUMMAN GUIDANCE<br />
AND<br />
<strong>EASA</strong>.IM.A.S.00759 REV 2 FAA STC ST<strong>01</strong>149LA AIRBUS A300 MODEL B2-203<br />
AIRBUS A300 MODEL B4-103<br />
AIRBUS A300 MODEL B4-203<br />
Installation of Litton Heading and Attitude<br />
System (LHAS) LTR-97.This STC is the result<br />
of the FAA STC No. ST<strong>01</strong>149LA validation.<br />
<strong>EASA</strong>.IM.A.S.<strong>01</strong>897 REV 1 FAA STC SA8027NM Replacement of old inertial navigation<br />
equipment with newer technology<br />
Required pre-modification: Agusta<br />
Prior to installation of this modification it 05.08.2<strong>01</strong>1<br />
electrical/mechanical provision nº109-B810-30- must be determined thatthe<br />
( )<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 />
Must be installed in conjunction with Northern<br />
Avionics kit P/N KNAV-418<br />
Prior to installation of this modification it 27.06.2<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 />
Prior to installation of this modification it 21.10.2<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 />
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 />
14.09.2<strong>01</strong>1<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 />
05.10.2<strong>01</strong>1<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 />
16.05.2<strong>01</strong>2<br />
1. This STC is limited to the installation of three<br />
LHAS LTR-97 (triple configuration).2.The<br />
Airplane Flight Manual Supplement, Document<br />
No. 434593-<strong>EASA</strong> dated 25 May 2005 is<br />
required as part of this installation.3. This STC<br />
is approved only for the product<br />
Litton Airplane Flight Manual Supplement, Doc<br />
No 464427, N/C, FAA approved on August 8,<br />
1994, or later approved revisions, is required<br />
as part of this modificationThis STC is<br />
approved only for the Boeing 747-287 model<br />
airplanes, and it applies only when th<br />
<strong>04</strong>/<strong>01</strong>/2<strong>01</strong>3 <strong>Page</strong> 345/<strong>462</strong><br />
31.07.2006<br />
28.11.2006
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