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
10032527 VIKING AIR LIMITED TCCA STC SA10-69 DHC-6 SERIES 400 Installation of RW Martin Air Conditioning None Prior to installation of this modification it 12.11.2010
System in accordance withTCCA STC SA10-
must be determined thatthe
69.
interrelationship between this modification
and any other previouslyinstalled
modification and/ or repair will introduce
no adverse effectupon the airworthiness
of the product.
10015333 VISIONSAFE CORPORATION EASA.IM.A.S.00354 REV. 6 FAA STC ST00892LA SEE EASA APPROVED MODEL
LIST
Installation of Emergency Vision Assurance
System (EVAS,TM). Change toSTC
EASA.IM.A.S.00354 Issue 4, update of relating
approved model listissue 4
10015744 VISIONSAFE CORPORATION EASA.IM.A.S.01774 FAA STC ST01012WI BOMBARDIER CL-600-1A11 (CL- Installation of Emergency Vision Assurance
600
BOMBARDIER CL-600-2A12 (CL-
601
BOMBARDIER CL-600-2B16
BOMBARDIER CL-600-2B19
System (EVAS TM)
10016007 VISIONSAFE CORPORATION EASA.IM.A.S.02172 REV. 1 FAA STC ST01057W1 BOMBARDIER BD-700-1A10
BOMBARDIER BD-700-1A11
10016045 VISIONSAFE CORPORATION EASA.IM.A.S.02216 FAA STC ST00892LA AIRBUS A330-201
AIRBUS A330-202
AIRBUS A330-203
AIRBUS A330-223
AIRBUS A330-243
AIRBUS A330-301
AIRBUS A330-321
AIRBUS A330-322
AIRBUS A330-323
AIRBUS A330-341
AIRBUS A330-342
AIRBUS A330-343
10016155 VISIONSAFE CORPORATION EASA.IM.A.S.02357 FAA STC ST00731LA BOEING 767-200
BOEING 767-300 SERIES
None Prior to installation of this modification the
installer must determinethat the
interrelationship between this modification
and any otherpreviously installed
modification will introduce no adverse
effect uponthe airworthiness of the
1) Certification Basis: applicable requirements
of a. r. TCDSs2) This STC is approved only for
the product configuration as defined in the
approved design data referred to in the
paragraph "Description". Compatibility with
other aircraft/engine configurati
Installation of Emergency Vision Assurance See AFMSPrior to installation of this
System (EVAS) model: 107 STC-191 and 107 modification the installer must determine that
STC-192Validation of FAA STC the interrelationship between this modification
ST01057WIMDL: Midcoast Aviation 35- and any other previously installed modification
416G001 Rev A or Vision Safe No. 206 Rev will introduce no adverse effect upon the
H or later EASA approved revisionsFAA Letter airworthiness of the product.
of SoC:
Installation of Emergency Vision Assurance
System (EVASTM) / EASA Validation of FAA
approved Supplemental Type Certificate
ST00892LA. 1. Boeing 737-600, -700, -700C, -
800 and -9002. Airbus 330-201, -202, -203, -
223, 243; Airbus 330-301, -321, 322, -323, -3
Installation of Emergency Vision Assurance
System (EVAS) in accordance with FAA
Approved Vision Safe Corporation Master
Drawing List Number 144, Revision “C” dated
June 9, 1999, or later FAA Approved
Revisions. Vision Safe Corporation Airplane
10030483 VISIONSAFE CORPORATION FAA STC ST00892LA BD100-1A10
Flight Manua
Installation of Emergency Vision Assurance
System (EVAS) Model107STC-235 and
107STC-236 on Bombardier BD-100-
1A10EASA Validation of FAA approved
Supplemental Type Certificate ST00892LA
10027778 V-PLANE ENGINEERING GMBH P-EASA.A.S.03977 PC-12, PC-12/45, PC-12/47,
PC-12/47E
10028296 V-PLANE ENGINEERING GMBH P-EASA.A.S.03978 ERJ170-100STD, LR
ERJ170-200STD, LR
¿ Vision Safe Corporation Instructions for
Continued Airworthiness, Rev. 04, dated March
2006.
This installation should not be incorporated in
any aircraft unless it is determined that the
interrelationship between this installation and
any previously approved configuration will not
introduce any adverse effect upon the
airworthiness of the aircraft
Heavy Duty Floor Heavy Duty Floor P/N 0127258 is limited to
from S/N 101 to S/N 999except S/N 545 with
configuration in accordance with Bucher
OMME014-16-01 Heavy Duty Floor P/N
0127470 and P/N 0127470-401 is limited to
from S/N1001 on which configuration in
accordance wit
product. The installati
28.06.2011
22.12.2005
10.02.2009
23.07.2007
30.03.2007
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.
17.06.2010
Prior to installation of this modification it 03.11.2009
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.
Installation of a removable stretcher 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.
16.12.2009
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