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>04</strong>0826 GOMOLZIG FLUGZEUG- UND<br />
0<strong>01</strong>0<strong>01</strong>6836-0<strong>01</strong> LBA STC EMZ SA <strong>01</strong>00/2025 CESSNA 340A 1. Camera Modification Kit System C340- As referred in AFM Must be maintained iaw. Original Cessna 27.07.2<strong>01</strong>2<br />
MASCHINENBAU<br />
8120002. C340 Camera Hatch Installation<br />
MM and in addition<br />
System C340-812500Change Note<br />
iawII_2027313_rev0_2<strong>01</strong>2<strong>04</strong>02or later<br />
CN_2027313_rev0_2<strong>01</strong>2<strong>04</strong>02<br />
approved revisions.Prior to installation of<br />
this modification it must be determined<br />
thatthe interrelationship between this<br />
modification and any other previouslyi<br />
10<strong>01</strong>6207 GOODRICH CORPORATION <strong>EASA</strong>.IM.A.S.02452 FAA STC ST02551CH BOEING 747-400F Installation of Centerline Restraint System on<br />
the main cargo deck of a B747-400F in<br />
accordance with Master Data List MDL<br />
10026859 GOODRICH CORPORATION P-<br />
<strong>EASA</strong>.IM.A.S.03106<br />
Prior to installation of this modification the<br />
installer must determine that the<br />
interrelationship between this modification and<br />
7M39300. Validation of FAA STC ST02551CH. any other previously installed modification will<br />
introduce no adverse effect upon the<br />
airworthiness of the product.<br />
02.07.2008<br />
FAA STC ST00989SE-D B767-300F Installation of the CHS (Cargo Handling The operation of the STC is only approved The applicant has to show and maintain 18.08.2009<br />
System) on the B767-300FMD:<br />
when installed on theprovisions of the Boeing the compliance to JAR 25.1309 atchange<br />
MDL7N10000FAA STC: ST00989SE-D A/C B767-300F.<br />
13.Remarks: The STC is part of the<br />
equipment for the Boeing A/C<br />
modelB767-300F. The provisions for the<br />
Cargo Handling System must beinstalled<br />
prior to the installation of the STC<br />
10031947 GOODRICH CORPORATION REV. 1 TCCA STC SA10-3 DHC-8-4<strong>01</strong>, DHC-8-402 Installation of Goodrich De-Icer boots on the<br />
Aircraft Wings, HorizontalStabilizer and Vertical<br />
StabilizerFAA STC ST02834NY, reissued<br />
September 20, 2<strong>01</strong>0(identical with TCCA STC<br />
SA10-3, Issue 2)<br />
10<strong>01</strong>60<strong>01</strong> GOODRICH INTERIORS <strong>EASA</strong>.IM.A.S.02161 REV. 2 FAA STC ST<strong>01</strong>691LA B767-200/-300 Installation of "Sentry One" Flight Deck Door<br />
Camera Surveillance System<br />
10<strong>01</strong>6<strong>462</strong> GOODRICH INTERIORS <strong>EASA</strong>.IM.A.S.02808 REV. 1 FAA STC ST<strong>01</strong>788LA DC-9-81 (MD-81),<br />
DC-9-82 (MD-82),<br />
DC-9-83 (MD-83),<br />
DC-9-87 (MD-87),<br />
MD-88, MD-90-30.<br />
Installation of Sentry One Flight Deck Door<br />
Surveillance Camera System.<br />
10<strong>01</strong>6505 GOODRICH INTERIORS <strong>EASA</strong>.IM.A.S.02869 REV. 1 FAA STC ST<strong>01</strong>007LA-D 737-800 Installation of Hollingsead Sentry One Cabin<br />
Video Camera System.<br />
10<strong>01</strong>6523 GOODRICH INTERIORS <strong>EASA</strong>.IM.A.S.02896 REV. 1 FAA STC ST<strong>01</strong>638LA 737-300, 737-400, 737-500 Installation of Hollinsead Sentry One Cabin<br />
mounted Video Camera System.<br />
100299<strong>01</strong> GOODRICH INTERIORS REV. 1 FAA STC ST<strong>01</strong>472LA-D 747-100, 747-100B,<br />
747-100B SUD, 747-200B,<br />
747-300, 747-400, 747-SP<br />
Installation of Hollingsead International Sentry<br />
One Cockpit Entry DoorSurveillance Camera<br />
System.<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 />
20.06.2<strong>01</strong>2<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 />
16.08.2<strong>01</strong>2<br />
None Prior to installation of this modification the 08.11.2<strong>01</strong>2<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 />
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 />
08.11.2<strong>01</strong>2<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 />
07.11.2<strong>01</strong>2<br />
None FAA approved Flight Manual<br />
Supplement, document No. 2763-<br />
AFM,revision NC, dated May 25,<br />
20<strong>04</strong> is required for the B747-400 series.<br />
FAA approved Flight Manual<br />
Supplement, document No. 2763-AFM-<br />
1,revision NC, dated July 21, 20<strong>04</strong><br />
is required for th<br />
08.11.2<strong>01</strong>2<br />
<strong>04</strong>/<strong>01</strong>/2<strong>01</strong>3 <strong>Page</strong> 240/<strong>462</strong>
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