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>4414 TELAIR INTERNATIONAL AB <strong>EASA</strong>.A.S.<strong>01</strong>713 AIRBUS A319<br />
Installation of Sliding Carpet Loading System in N/A 13.02.2006<br />
AIRBUS A320<br />
Airbus A319/320/321 in accordance with Telair<br />
AIRBUS A321<br />
International AB Master Document List (MDL)<br />
10<strong>01</strong>6023 TELAIR INTERNATIONAL INC. <strong>EASA</strong>.IM.A.S.02191 REV. 1 FAA STC ST00837 LA BOEING 747-400<br />
BOEING 747-400F<br />
Installation of a Cargo Handling System on the<br />
lower deck of the B747-400, -400F<br />
10<strong>01</strong>6031 TELAIR INTERNATIONAL INC. <strong>EASA</strong>.IM.A.S.02200 REV. 1 FAA STC ST0<strong>04</strong>59LA BOEING 747-400SF Installation of a Cargo Handling System on the<br />
main deck of the B747-400SF inaccordance<br />
with FAA approved Telair International Index<br />
List ER 193100 Rev. N/Cdated October 21,<br />
1997 or later approved revisions.Validation of<br />
FAA STC ST0<strong>04</strong>59LA<br />
10036235 TELAIR INTERNATIONAL INC. P-<br />
<strong>EASA</strong>.IM.A.S.03066<br />
10036236 TELAIR INTERNATIONAL INC. P-<br />
<strong>EASA</strong>.IM.A.S.03067<br />
REV. 1 FAA STC 02365LA B747-8F Lower Deck Cargo Handling System,<br />
Installation<br />
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 installa<br />
1. The installation of this modification by third<br />
persons is subject to writtenpermission of the<br />
approval holder2. Prior to installation of this<br />
modification the installer must determine that<br />
theinterrelationship between this modification<br />
and any other pre<br />
12.<strong>01</strong>.2009<br />
11.12.2008<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 />
26.08.2<strong>01</strong>1<br />
REV. 1 FAA STC 02367LA B747-8F Main Deck Cargo Handling System, 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 />
26.08.2<strong>01</strong>1<br />
10036941 TELAIR INTERNATIONAL INC. REV. 1 FAA STC ST02367LA 747-8F Main Deck Cargo Handling System, 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 />
20.10.2<strong>01</strong>1<br />
10036942 TELAIR INTERNATIONAL INC. REV. 1 FAA STC ST02365LA 747-8F Lower Deck Cargo Handling System,<br />
Installation<br />
10038077 TELAIR INTERNATIONAL INC. FAA STC ST02365LA 747-8 Installation of a Lower Deck Cargo Handling<br />
System<br />
10<strong>01</strong>5896 TELEDYNE BATTERY PRODUCTS <strong>EASA</strong>.IM.A.S.02<strong>01</strong>6 FAA STC SA1<strong>01</strong>3SO BEECH B99<br />
BEECH C90<br />
BEECH E90<br />
BEECH F90<br />
Replace existing nickel-cadmium battery with<br />
Gill BB638/T series lead-acid battery<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 />
20.10.2<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 />
17.<strong>01</strong>.2<strong>01</strong>2<br />
1) Beech C90 Serial Numbers LJ590 and after,<br />
E90 Serial Numbers LW58 and after, F90<br />
Serial Numbers LA-2 and after, B99 Serial<br />
Numbers U146 and U148 through U164.2)<br />
FAA approved Airplane Flight Manual<br />
Supplement, dated August 3, 1978, (C90, E90,<br />
B99), or Ja<br />
<strong>04</strong>/<strong>01</strong>/2<strong>01</strong>3 <strong>Page</strong> 441/<strong>462</strong><br />
22.05.2006
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