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>5897 TELEDYNE BATTERY PRODUCTS <strong>EASA</strong>.IM.A.S.02<strong>01</strong>7 SA1<strong>01</strong>6SO BEECH 200<br />
Replace existing nickel-cadmium battery with FAA approved Teledyne Battery Products<br />
23.05.2006<br />
BEECH 200C<br />
Teledyne G-6381E lead-acid battery or with Airplane Flight Manual Supplement, dated<br />
BEECH 200CT<br />
Teledyne G-6381ES Sealed Recombinant lead- August 3, 1978, for G-6381E battery, or March<br />
BEECH 200T<br />
acid storage battery<br />
21, 20<strong>01</strong>, for G-6381ES battery, or later<br />
BEECH 300<br />
approved revisions is required as part of this<br />
BEECH 300LW<br />
BEECH B200<br />
BEECH B200C<br />
BEECH B200T<br />
BEECH B300C<br />
installation.<br />
10<strong>01</strong>5898 TELEDYNE BATTERY PRODUCTS <strong>EASA</strong>.IM.A.S.02<strong>01</strong>8 SA1<strong>01</strong>7SO BEECH 65-90<br />
Replace existing nickel-cadmium battery with<br />
23.05.2006<br />
BEECH 65-A90<br />
Teledyne Battery Model No. G-638E, G-6381E<br />
BEECH 65-A90-1<br />
BEECH A100<br />
BEECH B90<br />
BEECH C90<br />
BEECH E90<br />
or G-6381ES<br />
10<strong>01</strong>6852 TELEDYNE BATTERY PRODUCTS <strong>EASA</strong>.IM.R.S.<strong>01</strong>228 SR<strong>01</strong>406LA BELL 206A<br />
Aircraft Battery Replacement with Alternative -- 14.09.2006<br />
BELL 206B<br />
Designs – Replace existing nickel-cadmium<br />
BELL 206L<br />
batteries with Teledyne Battery Products Model<br />
BELL 206L-1<br />
BELL 206L-3<br />
G-641S battery<br />
10<strong>01</strong>6853 TELEDYNE BATTERY PRODUCTS <strong>EASA</strong>.IM.R.S.<strong>01</strong>229 SR<strong>01</strong>427LA MD HELICOPTERS 369A Aircraft Battery Replacement with Alternative<br />
07.06.2006<br />
MD HELICOPTERS 369D<br />
MD HELICOPTERS 369E<br />
MD HELICOPTERS 369F<br />
MD HELICOPTERS 369FF<br />
MD HELICOPTERS 369H<br />
MD HELICOPTERS 369HM<br />
MD HELICOPTERS 369HS<br />
MD HELICOPTERS 500N<br />
MD HELICOPTERS 600N<br />
Designs<br />
10<strong>01</strong>6928 TELEDYNE BATTERY PRODUCTS <strong>EASA</strong>.IM.R.S.<strong>01</strong>314 FAA STC ST1186SO BELL 212<br />
Validation of FAA STC SH1186SO Aircraft<br />
20.06.2007<br />
BELL 412<br />
BELL 412 EP<br />
Battery Replacement with Alternative Designs<br />
10027424 TELEDYNE CONTROLS - FLIGHT DATA P-<strong>EASA</strong>.A.S.034<strong>01</strong> MD-80 SERIES Installation of Wireless Quick Access Recorder. None. Prior to installation of this modification the 12.09.2009<br />
COM<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 />
10033194 TELEDYNE CONTROLS - FLIGHT DATA P-<strong>EASA</strong>.A.S.03937 B737-600/-700/-800/-900/-900ER Installation of enhanced airborne data loader This modification is only applicable to 737 Prior to installation of this modification it 22.12.2<strong>01</strong>0<br />
COM<br />
on Boeing 737 seriesaircraft<br />
aircraft that already havean ADL installed or must be determined thatthe<br />
have provisions for installation of an<br />
interrelationship between this modification<br />
ADL.Compatibility must be established for and any other previouslyinstalled<br />
each aircraft.<br />
modification and / or repair will introduce<br />
no adverse effectupon the airworthiness<br />
of the product.<br />
10<strong>01</strong>4159 TELEDYNE LIMITED <strong>EASA</strong>.A.S.<strong>01</strong>290 BOEING 767-300 Installation of Teledyne Controls Optical Quick<br />
Access recorder (OQAR) P/N 224800<br />
10<strong>01</strong>4562 TELEDYNE LIMITED <strong>EASA</strong>.A.S.02662 MD80 SERIES Installation of Optical Quick Access Recorder. 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 />
10039512 TELEDYNE LIMITED <strong>EASA</strong>.A.S.<strong>01</strong>198 REV 1 767-200, 767-300/-300F Installation of Wireless Quick Access Recorder 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 />
08.05.2<strong>01</strong>2<br />
<strong>04</strong>/<strong>01</strong>/2<strong>01</strong>3 <strong>Page</strong> 442/<strong>462</strong><br />
26.10.2005<br />
05.07.2007
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