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
10014400 STEINBEIS FLUGZEUG- UND
EASA.A.S.01695 DG LS8-T LS8-th Hydraulic extension systemExchange of This STC is approved only for the product
06.07.2006
LEICHTBAU G
the electric driven engine extension system to a configuration as defined in the approved design
hand-driven hydraulic system
data referred to in the paragraph "Description".
Compatibility with other aircraft/engine
configurations shall be determined by the
installer.
10034286 STEINBEIS FLUGZEUG- UND
P-EASA.A.S.03832 LS 6 & LS 6-A STC: "Winglet Retrofit" / "Nachrüstung mit None Prior to installation of this modification it 23.03.2011
LEICHTBAU G
Winglets"
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
10015396 STG AEROSPACE INC. EASA.IM.A.S.01098 ST02993AT BOEING 747-400 Installation of SafTGIo Inc. Photoluminescent 1. The photoluminescent FPEEPMS is only
floor proximity emergency escape path eligible for installation on aircraft model
marking system (FPEEPMS) in accordance numbers with interior arrangements approved
with SafTGIo MDL Report M39-2, rev. B dated in the SafTGIo MDL, incorporating SafTGIo
October 11, 2004 or later FAA-approved drawing SG-B747 rev B dated October 7, 2004
revision
or later FAA-approved revision.2. El
10015428 STG AEROSPACE INC. EASA.IM.A.S.01161 FAA STC ST02691AT AIRBUS A300 MODEL B2
AIRBUS A300 MODEL B4
AIRBUS A310-200
AIRBUS A310-300
10015429 STG AEROSPACE INC. EASA.IM.A.S.01163 FAA STC ST02664AT AIRBUS A340-200
AIRBUS A340-300
10015430 STG AEROSPACE INC. EASA.IM.A.S.01164 REV. 1 FAA STC ST02529AT ATR 42-200/-300/-320/-500
ATR 72-101/-102/-201/-202/-211
ATR 72-212/-212A
Installation of SafTGlo photoluminiscent floor
proximity emergency escape path marking
system (FPEEPMS). - Validation of FAA STC
No. ST02691AT).
Installation of SafTGlo photoluminescent floor
proximity emergency escape path marking
system (FPEEPMS) – Validation of FAA STC
N° ST02664AT
Installation of SafTGlo Photoluminescent Floor
Proximity EmergencyEscape Path Marking
System (PFPEEPMS).(Validation of FAA STC
ST02529AT)The STC installs a
photoluminescent aisle path marking
system(PFPEEPMS).This revision 01 adds
ATR 72 aircraft models in
10015431 STG AEROSPACE INC. EASA.IM.A.S.01165 FAA STC ST02637AT BOEING 717-200 Installation of SaftGlo Inc. Phtoluminescent
floor proximity emergency escape path
marking system (FPEEPMS)
10015432 STG AEROSPACE INC. EASA.IM.A.S.01166 FAA STC ST01641AT BOEING 727-100 SERIES
BOEING 727-200 SERIES
10015433 STG AEROSPACE INC. EASA.IM.A.S.01168 FAA STC ST02221AT BOEING 757-200
BOEING 757-300
10015434 STG AEROSPACE INC. EASA.IM.A.S.01169 FAA STC ST02521AT BOEING 767-200 SERIES
BOEING 767-300 SERIES
Installation of a phtoluminiscent Floor Proximity
Emergency Escape Path Marking System
according to Diversified Aviation Services Inc
FAA STC No. ST01641AT.
Installation of SafTGlo Inc. Phtoluminescent
floor proximity emergency escape path
marking system (FPEEPMS)
Installation of SaftGlo Inc. Phtoluminescent
floor proximity emergency escape path
marking system (FPEEPMS)
1. The approval of this STC is limited to the
identified aircraft models with interior
arrangements approved in the SafTGlo MDL
No.L66-2 Revision D, dated 16 MAR 2004, for
Airbus A300 incorporating SafTGlo Drawings
SGA300 and for A310 incorporating SafTGlo
1. 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
configurations shall be determined by the
installer.2. The approval
16.03.2005
06.09.2005
16.11.2005
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.
15.04.2011
Cabin and exit lightning levels must be
measured for acceptability on each installation
in accordance with STG Aerospace Report
No.P51-12, Revision A dated November 13,
2002 and P51-10, Revision I.R., dated August
15, 2002 or later approved revisions
Cabin and exit lighting levels must be
measured for acceptability on each installation
in accordance with STG Aerospace Report No.
L21-12, Revision I.R. dated September 22,
2000 an L21-10, Revision I.R., dated
September 21, 2000 or later approved
revisions
Cabin and exit lighting levels must be
measured for acceptability on each installation
in accordance with STG Aerospace Report No.
M40-12, Revision A dated October 11, 2001
and M40-10. Revision C, dated May 6. 2002 or
later approved revisions
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26.08.2005
21.09.2005
26.07.2005
26.07.2005