04/01/2013 Page 1/462 - EASA

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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 04/01/2013 Page 434/462 26.08.2005 21.09.2005 26.07.2005 26.07.2005
EASA STC no. STC holder Old STC ref. Revision Level Foreign/NAA STC ref. Model Description Limitations Conditions Date of issue 10015435 STG AEROSPACE INC. EASA.IM.A.S.01170 FAA STC ST02687AT BOMBARDIER CL-600-2B19 Installation of SaftGlo Inc. Phtoluminescent Cabin and exit lighting levels must be 28.07.2005 BOMBARDIER CL-600-2C10 floor proximity emergency escape path measured for acceptability on each installation marking system (FPEEPMS) in accordance with STG Aerospace Report No. M41-12, Revision A dated June 30, 2002 and M41-10, Revision I.R, dated June 5, 2003 or later approved revisions. 10015437 STG AEROSPACE INC. EASA.IM.A.S.01175 FAA STC ST02131AT DC 10-30 CF SERIES DC 10-30 SERIES DC-10-10 SERIES MD-11 10015438 STG AEROSPACE INC. EASA.IM.A.S.01176 FAA STC ST01893AT BOMBARDIER DHC-7-100 BOMBARDIER DHC-7-102 10015439 STG AEROSPACE INC. EASA.IM.A.S.01179 FAA STC ST02406AT FOKKER F.28 MARK 0070 FOKKER F.28 MARK 0100 FOKKER F.28 MARK 1000 FOKKER F.28 MARK 2000 FOKKER F.28 MARK 3000 FOKKER F.28 MARK 4000 10016295 STG AEROSPACE INC. EASA.IM.A.S.02592 REV. 2 FAA STC ST03465AT B737-300/-400/-500 B737-700/-800/-900 10016490 STG AEROSPACE INC. EASA.IM.A.S.02846 FAA STC ST01829A BOEING 737-100 BOEING 737-200 BOEING 737-300 BOEING 737-400 BOEING 737-500 BOEING 737-600 BOEING 737-700 BOEING 737-800 BOEING 737-900 Installation of SaftGlo Inc. Photo luminescent floor proximity emergency escape path marking system in accordance with FAA STC ST02131AT 10028318 STG AEROSPACE INC. FAA TCDS T00001SE B777-200 Installation of SafTGlo, Inc photoluminescent floor proximity emergencyescape path marking system 10028633 STG AEROSPACE INC. P- EASA.IM.A.S.03118 REV. 2 FAA STC ST03629AT B767-200, -300 Installation of STG Aerospace PowerSmart Emergency Primary Power System(WEPPS). 10028634 STG AEROSPACE INC. REV. 1 FAA STC ST03692AT B757-200 Installation of STG Aerospace PowerSmart Emergency Primary Power System(WEPPS). 1. The Photoluminescent FPEEPM is only eligible for installation on aircraft model numbers with interior arrangements approved in the STG Aerospace document K17-2 Reviosn C, dated February 7, 2003, incorporating STG Aerospace drawing SG- 15.11.2005 Installation of SaftGlo Inc. Phtoluminescent DC10 rev B ISNT DWG Cabin and exit lighting levels must be 28.07.2005 floor proximity emergency escape path measured for acceptability on each installation marking system (FPEEPMS) in accordance with DAS Report No. G34-12, Revision A dated April 16, 1999 and G34-10, Revision A, dated April 17, 1999 or later approved revisions. Installation of photo luminescent floor proximity 1. The Photoluminescent FPEEPM is only emergency escape path marking system FAA eligible for installation on aircraft model 15.11.2005 STC ST02406AT numbers with interior arrangements approved in the STG Aerospace document H61-2 Reviosn F, dated October 4, 2004, incorporating STG Aerospace drawing SG-F28 rev D, dated Aug Installation of an STG Aerospace PowerSmart None If non-rechargeable lithium batteries used 08.08.2011 Wireless Emergency PrimaryPower System in this installation are notTSO-C142 and (WEPPS) in accordance with STG Master DO-227 compliant, or if rechargeable Drawing List (MDL)No. 71430000 batteries are used inthis installation, additional requirements may apply. Any change to theLithium chemistry of the battery is conside Installation of the SAFTGLO Non-electrical The photo luminescent Floor Proximity 14.04.2008 Photoluminescent Escape Path Marking Emergency Escape Path Marking System is System to include all 737 models. only eligible for installation on aircraft model numbers with interior arrangements approved in the SafTGlo MDL No. E74-2, Rev. I.R. for the B 737 incorporating SafTGlo Drawing S 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. 17.12.2009 None If the non-rechargeable lithium batteries used in this installation arenot TSO-C142 and DO-227 compliant, or if rechargeable batteries are usedin this installation, additional requirements may apply. Any change tothe Lithium chemistry of the battery is con 03.03.2011 None If the non-rechargeable lithium batteries used in this installation arenot TSO-C142 and DO-227 compliant, or if rechargeable batteries are usedin this installation, additional requirements may apply. Any change tothe Lithium chemistry of the battery is con 23.03.2011 04/01/2013 Page 435/462
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04/01/2013 Page 1/462 - EASA

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