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 />
10037056 DASSAULT FALCON SERVICE F900B, F900C & F900EX Cabin Master installation.A Cabin Master Not applicable Prior to installation of this modification it 27.10.2<strong>01</strong>1<br />
Switch is installed on Co-pilot console.<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 />
10037415 DASSAULT FALCON SERVICE F900B, F900C, F900EX<br />
F900EX EASY<br />
FR14 CABIN PARTITION WITH<br />
MECHANICAL POCKET SLIDING DOOR.<br />
As per DFS Change Approval Sheet DFS9654- Prior to installation of this modification it 25.11.2<strong>01</strong>1<br />
CAS Issue A dated 06.08.2<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 />
10037417 DASSAULT FALCON SERVICE F900EX F900EX S/N 038 Cabin Layout Modification. Restricted to F900EX S/N 038 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 />
25.11.2<strong>01</strong>1<br />
10038490 DASSAULT FALCON SERVICE REV. 2 F900EX EASY TCAS 2000 upgrade to TCAS change 7.1 on<br />
F900EX EASyMajor Change to <strong>EASA</strong> STC<br />
10038490This Major Change consists in<br />
removing the former limitation (onlyVersion 1<br />
(F900EX EASy Step 3+) was approved)<br />
10039335 DASSAULT FALCON SERVICE F2000EX EASY TCAS 2000 upgrade to TCAS change 7.1 on<br />
F2000EX EASy<br />
10<strong>04</strong>1183 DASSAULT FALCON SERVICE MYSTERE-FALCON 50 Mode S transponder upgrade to comply with<br />
Elementary and<br />
EnhancedSurveillance.Honeywell transponder<br />
MST-67A version is upgraded and ATC/TCAS<br />
ControlBox is replaced by new Honeywell PS-<br />
578A unit.<br />
10<strong>04</strong>1623 DASSAULT FALCON SERVICE F2000, F2000EX WiFi activation on Falcon 2000, F2000EX<br />
aircraft.<br />
10<strong>01</strong>5747 DAYTON-GRANGER Inc. <strong>EASA</strong>.IM.A.S.<strong>01</strong>779 REV. 4 FAA STC NO. ST02241NY CL-600-2B19<br />
CL-600-2C10<br />
CL-600-2D15<br />
CL-600-2D24<br />
CL-600-2E25<br />
10<strong>01</strong>6<strong>04</strong>3 DC AEROSPACE <strong>EASA</strong>.IM.A.S.02214 REV. 1 ST03<strong>01</strong>1AT BOEING 727-100 SERIES<br />
BOEING 727-200 SERIES<br />
Installation of Winglet and Horizontal Stabilizer<br />
End Cap LightningProtection Kits<br />
Installation of Sandel ST3400 Terrain<br />
Awareness and Warning System (TAWS) in<br />
Boeing 727 Series Aircraft according to FAA<br />
STC ST03<strong>01</strong>1AT dated 22 December 20<strong>04</strong><br />
As per DFS Change Approval Sheet DFS9664- Prior to installation of this modification it 08.05.2<strong>01</strong>2<br />
CAS Issue B dated 05.<strong>04</strong>.2<strong>01</strong>2<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 />
As per DFS Change Approval Sheet DFSD149-Prior<br />
to installation of this modification it 26.<strong>04</strong>.2<strong>01</strong>2<br />
CAS Issue A dated 07 March 2<strong>01</strong>2<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 />
28.08.2<strong>01</strong>2<br />
F2000 and F2000EX aircraft equipped with<br />
WiFi equipments installationcompliant with<br />
prerequisite note DT-0<strong>01</strong>-12.<br />
Prior to installation of this modification it 02.10.2<strong>01</strong>2<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 />
24.06.2<strong>01</strong>1<br />
SANDEL mandatory SB 3400-09 to be<br />
incorporatedThe limitations as listed in FAA<br />
STC ST03<strong>01</strong>1AT apply.<br />
<strong>04</strong>/<strong>01</strong>/2<strong>01</strong>3 <strong>Page</strong> 179/<strong>462</strong><br />
23.07.2007
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