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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 />

10036054 BOMBARDIER INC. REV. 1 TCCA STC SA<strong>04</strong>-113 BD-700-1A10 Installation, Complete Custom Aircraft Interior - Restricted to ASN 94061. Refer to the Prior to installation of this modification it 08.08.2<strong>01</strong>1<br />

ASN 9406<br />

Limitations sections of the required AFM must be determined thatthe<br />

Supplement andto the referenced FCOMS2. interrelationship between this modification<br />

WLAN system is compatible only to IEEE and any other previouslyinstalled<br />

802.11(b)<br />

modification and/ or repair will introduce<br />

no adverse effectupon the airworthiness<br />

of the product.<br />

10036058 BOMBARDIER INC. TCCA STC SA05-60 BD-700-1A11 Installation, Complete Custom Aircraft Interior -<br />

ASN 9421<br />

10036060 BOMBARDIER INC. REV. 1 TCCA STC SA<strong>04</strong>-113 BD-700-1A10 Installation of cabin systems and custom<br />

furnishings applicable toBD-700-1A10 serial<br />

number 9393<br />

10036095 BOMBARDIER INC. TCCA STC C-LSA<strong>01</strong>-452/D BD-700-1A10 Interior Modification - ASN 9020 - Installation,<br />

Modifications to APUBay Light, Galley Oven,<br />

Smoke Detector Wiring and Equipment<br />

BayProvisions<br />

Restricted to ASN 9421 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 />

09.08.2<strong>01</strong>1<br />

Restricted to ASN 93931. Refer to the<br />

Limitations sections of the required AFM<br />

Supplement andto the referenced FCOMS.2.<br />

WLAN system is compatible only to IEEE<br />

802.11(b).<br />

Restricted to ASN 9020.Previous embodiment<br />

of <strong>EASA</strong> STC No. 10<strong>01</strong>6140 (refers to PN<br />

0<strong>01</strong>0<strong>01</strong>1877)(Installation of a Complete<br />

Custom Aircraft Interior in accordance withFAA<br />

STC SA8164NM-D) is mandatory.<br />

10036096 BOMBARDIER INC. TCCA STC Q-LSA02-065/D BD-700-1A10 Miscellaneous Cabin Modifications Restricted to ASN 9020.Previous embodiment<br />

of <strong>EASA</strong> STC No. 10<strong>01</strong>6140 (refers to PN<br />

0<strong>01</strong>0<strong>01</strong>1877)(Installation of a Complete<br />

10036344 BOMBARDIER INC. TCCA STC NO. SA11-69 BD-700-1A10, -1A11 Installation, Structural Provisions for Shower<br />

Drain Feedthrough<br />

10036603 BOMBARDIER INC. TCCA STC SA05-60 BD-700-1A11 Installation, Complete Custom Aircraft Interior -<br />

ASN 9427<br />

10037<strong>04</strong>0 BOMBARDIER INC. TCCA STC NO. SA<strong>04</strong>-113 ISSUE 1 BD-700-1A10 Installation, Complete Custom Aircraft Interior -<br />

ASN 9413<br />

10037055 BOMBARDIER INC. TCCA STC NO. SA<strong>04</strong>-113 ISSUE 1 BD-700-1A10 Installation, Complete Custom Aircraft Interior -<br />

ASN 9238<br />

Custom Aircraft Interior in accordance withFAA<br />

STC SA8164NM-D) is mandatory.<br />

Prior to installation of this modification it 09.08.2<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<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<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 />

10.08.2<strong>01</strong>1<br />

10.08.2<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 />

02.09.2<strong>01</strong>1<br />

Restricted to ASN 9427 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 />

22.09.2<strong>01</strong>1<br />

Restricted to ASN 9413 and1. Refer to the<br />

Limitations sections of the required AFM<br />

Supplement andto the referenced FCOMS.2.<br />

WLAN System is compatible only to IEEE<br />

802.11(b).<br />

Restricted to ASN 9238 and1. Refer to the<br />

Limitations sections of the required AFM<br />

Supplement andto the referenced FCOMS.2.<br />

WLAN System is compatible only to IEEE<br />

802.11(b).<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 />

Prior to installation of this modification it 27.10.2<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> 135/<strong>462</strong>

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