04/01/2013 Page 1/462 - EASA

EASA STC no. STC holder Old STC ref. Revision Level Foreign/NAA STC ref. Model Description Limitations Conditions Date of issue
10016654 ROCKWELL COLLINS, Inc. EASA.IM.A.S.03103 SEE ATTACHED EASA
Collins CMU-900 ACARS Core Software Prior to installation of this modification the
27.02.2009
APPROVED TYP
UpgradeThis modification removes the existing installer must determine that the
CMU-900 and installs the same part number interrelationship between this modification and
CMU-900 with updated core software. any other previously installed modification will
introduce no adverse effect upon the
airworthiness of the product.The installa
10035296 ROCKWELL COLLINS, Inc. FAA STC ST01886LA B767-300 Installation of Rockwell Collins CMU-900
Communications ManagementSystem, APM-
900 Airplane Personality Module, IDC-900
Integrated DatalinkController & Teledyne TP-
4499 Printer.
10037095 ROCKWELL COLLINS, Inc. REV. 1 FAA STC ST01957AT-D B747-400 Installation of Collins SAT-906 Satcom
Systems provisions in accordancewith Timco
Master Data List MDL 99T045L001, Rev. C,
dated October 21,1999 or later approved FAA
revisions.
10037522 ROCKWELL COLLINS, Inc. FAA STC NO. ST02177LA CL-600-2B16 HUD/EVS Model 6605 Validation of HUD/EVS
in a Deactivated State
10041711 ROCKWELL COLLINS, Inc. REV. 1 FAA STC NO. ST01514WI-D CL600-2B19 REGIONAL JET
A21EA
Installation of Rockwell Collins FMS-4200 to
provide WAAS/LPAcapability.
10041712 ROCKWELL COLLINS, Inc. FAA STC NO. ST01505WI-D CL-600-2B16 (CL-604 VARIANT) Installation of Rockwell Collins FMS-6000 to
provide SBAS LPVcapability.
10015977 ROCKY MOUNTAIN AIRCRAFT EASA.IM.A.S.02129 REV. 1 TCCA STC SA02-128 DHC 6-100, 6-200, 6-300 Installation of Single or Dual Sandel ST3400
Terrain Awareness WarningSystem
(TAWS)/RMI System
none Prior to installation of this modification it
must be determined thatthe
interrelationship between this modification
and any other previouslyinstalled
modification and/ or repair will introduce
no adverse effectupon the airworthiness
of the product.
14.06.2011
None. Prior to installation of this modification it
must be determined thatthe
interrelationship between this modification
and any other previouslyinstalled
modification and/ or repair will introduce
no adverse effectupon the airworthiness
of the product.
13.04.2012
Restricted to ASN 5872.This approval is for the
installation and deactivation of the HUD
andEVS in accordance with section 9 of the
Rockwell Collins Master DrawingList 9701-
1267 Revision D-1.
Prior to installation of this modification it
must be determined thatthe
interrelationship between this modification
and any other previouslyinstalled
modification and/ or repair will introduce
no adverse effectupon the airworthiness
of the product.
02.12.2011
Installation and approval of WAAS compatible Prior to installation of this modification it
GPS antennas is requiredprior to or concurrent must be determined thatthe
12.10.2012
with this modification. This STC approves the interrelationship between this modification
installation of DBU-5000 Part Number 822- and any other previouslyinstalled
2215-602(Flip Door/Gray/No AFIS/Ethernet). modification and/ or repair will introduce
Installation and approval of a Roc
no adverse effectupon the airworthiness
of the product.
Restricted to Serial Numbers 5301-5699, 5701
and subsequent. Installation and approval of
WAAS compatible GPS receivers/antennas
arerequired prior to or concurrent with this
modification. DBU-4000 and DBU-4100 Data
Base Units are incompatible with the FMC-
The audio for dual TAWS configuration must
be from a single source inaccordance with
drawings 1873419, 1873420 and 1873421
incorporatingDCN’s RMA1873419/1,
RMA18173420/2 and RMA18173422/1
respectively.
10016029 ROCKY MOUNTAIN AIRCRAFT EASA.IM.A.S.02198 TCCA STC SA01-30 Removal of Auxiliary Battery 1. An approved Main Battery Installation with
a minimum capacity of 34 Ampere-Hours must
be embodied as a pre-requisite.2. This STC
is approved only for the product configuration
as defined in the approved design data
referred to in the paragraph "De
10016030 ROCKY MOUNTAIN AIRCRAFT EASA.IM.A.S.02199 TCCA STC SA01-17 BOMBARDIER DHC-6 SERIES
300
10016033 ROCKY MOUNTAIN AIRCRAFT EASA.IM.A.S.02202 FAA STC SA02297NY BOMBARDIER DHC-6 SERIES
200
BOMBARDIER DHC-6-100
DE HAVILLAND CANADA DHC6-
300
Cabin Evacuation Lighting Control System
Change.
(1) Installation of a Universal Avionics CVR-
30B Cockpit Voice Recorder.(2) Installation of
a Fairchild A100S, Honeywell SSCVR, or L3
FA2100 Cockpit Voice Recorder.
Prior to installation of this modification the
installer must determine that the
interrelationship between this modification and
any other previously installed modification will
introduce no adverse effect upon the
airworthiness of the product. The install
The installation applies only to aircraft not
equipped with separate P.A.
microphone.Maintenance must be in
accordance with Field Aviation Company
Maintenance Manual Supplement Report No
199031, Original Issue, datedDecember 11,
2006, or later approved rev
Prior to installation of this modification it 09.10.2012
must be determined thatthe
interrelationship between this modification
and any other previouslyinstalled
modification and/ or repair will introduce
no adverse effectupon the airworthiness
of the product.
None. 17.03.2010
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22.12.2006
10.10.2008
22.10.2007