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
10034324 POLICE AVIATION SERVICES Ltd. MD902 CONFIG. P&W 206&207 Aircraft Role Configuration none The approval holder shall fulfill the
obligations of Part 21,
Paragraph21.A109Prior to installation of
this modification it must be determined
thatthe interrelationship between this
modification and any other
previouslyinstalled modification and/ or
repair
25.03.2011
10036834 POLICE AVIATION SERVICES Ltd. REV. 1 VULCANAIR P.68.TC
Airborne Surveillance System Installation None Prior to installation of this modification it 24.11.2011
'OBSERVER'
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.
10015338 PRATT & WHITNEY EASA.IM.A.S.00373 REV. 2 AIR TRACTOR AT-402 A
AIR TRACTOR AT-501
AIR TRACTOR AT-502 B
AIR TRACTOR AT-503
AIR TRACTOR AT-802
AIR TRACTOR AT-802 A
BEECH 1900
BEECH 200
BEECH 300
BEECH C90
CESSNA 208
CESSNA 208A
CESSNA 208B
PILATUS PC-6/B-H2
PILATUS PC-6/B1-H2
PILATUS PC-6/B2-H2
PILATUS PC-6/B2-H4
10015554 PRATT & WHITNEY EASA.IM.A.S.01451 REV. 1 FAA STC SA00196BO BEECH 1900
BEECH 200
BEECH 300
BEECH C90
CESSNA 208
CESSNA 208A
CESSNA 208B
10015834 PRATT & WHITNEY EASA.IM.A.S.01925 REV 1 FAA STC ST00228BO DC-9-81 (MD-81)
DC-9-82 (MD-82)
DC-9-83 (MD-83)
DC-9-87 (MD-87)
MD-88
10016426 PRATT & WHITNEY EASA.IM.A.S.02765 FAA STC SA00095BO, LBA SA 1346 BEECH 1900
BEECH 1900C, AIRLINER
BEECH 1900D
BEECH 200
BEECH 200C
BEECH 200CT
BEECH 200T
BEECH 300
BEECH 300LW
BEECH A200
BEECH A200C
BEECH A200CT
BEECH B200
BEECH B200C
BEECH B200CT
BEECH B200T
BEECH B300
BEECH B300C
Installation of Pratt & Whitney Data Acquisition
System ADAS+, p/n ADAS-K-010.
1. Compatibility of this modification with other
previously approved modifications must be
determined by the installer.2. This Major
Change to STC EASA.IM.A.S.00373 is issued
as a result of the validation of the Altair
Avionics Corporation STC No SA0
Installation of Altair Avionics Corporation Data This STC is approved only for the product
Transmission Unit in accordance with configuration as defined in the approved design
instructions listed in Approved Model List (AML) data referred to in the paragraph "Description".
DTU-T-225-1, Rev - or later approved Compatibility with other aircraft/engine
revisions. FAA STC SA00196BO refers configurations shall be determined by the
installer.
Installation of P&W JT8D-200 Series Engines
incorporating the improved forward Fan Case
as described in the P&W SB JT8D 6478,
Rev.1, dated 1 August 2007.
10016692 PRATT & WHITNEY EASA.IM.E.S.01006 FAA STC SE00033EN CFM56-3B1 Installation of Pratt & Whitney (P&W) Global
Material Solutions (GMS) CFM56-3 High
Pressure Compressor Module in accordance
with P&W GMS Drawing List 880500-01C
dated May 06, 2008 or later EASA-approved
revisionEASA Certification Basis:1.
Airworthiness
This STC is approved only for the product
configuration as defined in the approved design
datareferred to in the paragraph "Description".
Prior to installation of this modification the
installermust determine that the
interrelationship between this modific
Installation of Pratt & Whitney Engine Services, 1. Pratt & Whitney Engine Services,Inc.
Inc. Twin Engine Aircraft Data Acquisition Aircraft Flight Manual Supplement for
System ADAS/ADAS+ Upgrade, P/N TWIN-K- Raytheon Aircraft Company Models 200,
010
200C, 200CT, 200T, A200, A200C, A200CT,
B200, B200C, B200CT, B200T, 300, 300LW,
B300C, 1900, 1900C, 1900D, Document No.
TWIN-T-250-1, Revisi
Limitations:1. The limitations of the EASA
Engine Type Certificate Data Sheet E.066
issue 1, dated November 28, 2008 apply to this
Supplemental Type Certificate.2. Life limits
for the parts approved by this Supplemental
Type Certificate are published
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04.10.2007
07.03.2008
22.12.2008