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 10039944 AEROLITE MAX BUCHER AG LBA STC RC 1240 REV. 1 MBB-BK117 C-2 Change to LBA STC No.RC 1240 on EMS Not applicable Prior to installation of this modification it 04.06.2012 Equipment P/N 145170-501:Addition of variant must be determined thatthe P/N 145169-501This change introduces:EMS interrelationship between this modification variant P/N 145169-501 composed by:- and any other previouslyinstalled Introduction of the new Cargo Platform Inst. modification and/ or repair will introduce P/N 145-0000835-501- Introduction of the new no adverse effectupon the airworthiness Cover I of the product. 10040646 AEROLITE MAX BUCHER AG REV. 1 EC 135 P1 EC 135 P2 EC 135 P2+ EC 135 T1 EC 135 T2 EC 135 T2+ EC 635 P2+ EC 635 T1 EC 635 T2+ 10015544 AEROMECH INC. EASA.IM.A.S.01429 FAA STC SA5800NM BEECH 200 BEECH 200C BEECH 300 BEECH 300LW BEECH B200 BEECH B200C BEECH B300 BEECH B300C 10015820 AEROMECH INC. EASA.IM.A.S.01892 ST01413SE HAWKER HS 125-700A HAWKER HS 125-700B 10016064 AEROMECH INC. EASA.IM.A.S.02243 REV. 3 FAA STC ST01526SE 500 (CITATION I) 550 (CITATION II) 560 (CITATION V) S550 (CITATION S/II) 10016065 AEROMECH INC. EASA.IM.A.S.02244 FAA STC #ST01522SE CESSNA 500 CESSNA 551 10026757 AEROMECH INC. P- EASA.IM.A.S.03086 Ballast Platform Installation P/N 135-0012762- 501. Group approval for reduced vertical separation minimum. Approval of Reduced Vertical Separation Minimum (RVSM). Group Aircraft Approval for Reduced Vertical Separation Minimum (RVSM)for Cessna Model 500/550/S550/560.This STC is an update of STC EASA.IM.A.S.02243 Rev 1, and incorporatesan added class of avionics as applicable to the RVSM Group approval inaccordancewi Validation of FAA STC ST01522SE:Group aircraft approval for RVSM capability. FAA STC SA01602SE CESSNA 441 SERIES Group Approval for Reduced Vertical Separation Minimum (RVSM) 10016739 AEROMETALS EASA.IM.R.S.01064 FAA STC SH3756NM MD HELICOPTERS 369HE MD HELICOPTERS 369HS 10016740 AEROMETALS EASA.IM.R.S.01065 FAA STC SH5055NM MD HELICOPTERS 369D MD HELICOPTERS 369E MD HELICOPTERS 369F MD HELICOPTERS 369FF 10016931 AEROMETALS EASA.IM.R.S.01317 FAA STC SR01524SE MD HELICOPTERS 369A MD HELICOPTERS 369HE MD HELICOPTERS 369HM MD HELICOPTERS 369HS Installation of Aerometals tailboom P/N 369X3500-505 or Yehnert tailboom P/N YH- 203.The present STC is the validation of the FAA STC SH3756NM amended on 30/11/99, limited to MDHI 369H, HS and HE models. Installation of- Aerometals tailboom:- P/N 369X23500-505 as replacement of MDHI tailboom P/N 369D23500-505, or-P/N 369X23500-507 as replacement of MDHI tailboom P/N 369D2300-507, or- Yehnert tailboom :- P/N YH-228-1 as replacement of MDHI tailboom P/N 369D Horizontal stabilizer, P/N AM369A3600- 603Validation of FAA STC SRSR01524SE reissued June 28, 2006 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. 20.07.2012 1. AFMS No. AMI-AFMS-KAIR-0429A Rev "Original", dated 30 September 2004 is required on-board for operation with Beech 200, 200C,B200, B200C, 300 and 300LW series.2. AFMS No. AMI-AFMS-KAIR-0429B Rev "Original", dated 30 September 2004 is required on-b 1. Only applicable to Aircraft Serial 257037.2. This STC must be installed after Avionics Mobile STC ref AM/1518. The installation is to be completed by the embodiment of Avionics Mobile Minor change AM/1532 installation of RVSM ADM’s. 24.11.2005 17.10.2006 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. 08.08.2011 The installer muste determine if this design is compatible with previously approved modifications. If the holder agrees to permit another person to use this certification or alter a product, the holder must give the other person written evidence of that pe This approval is issued based on the FAA STC SA01602SE, issued on 26October 2005 and later amended on 17 November 2006. 1. Service life of the Aerometals and Yehnert referenced tailbooms is established according to FAR 27.571 (e) at 10000 flight hours, with periodic inspections required at 2450 flight hours and each 2450 flight hours thereafter.2. Inspections of the Aeromet 1.Service life of the Aerometals and Yehnert referenced tailbooms is established according to FAR 27.571 (e) at 10300 flight hours,with periodic inspections required at 7300 flight hours and each 1000 flight hours hereafter.2. Inspections of- the Aerometal Limited to MDHI (Hughes) models 369HM, 369HS, 369HEall other limitation and conditions listed in FAA STC SRSR01524SE reissued June 28, 2006 apply 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 04/01/2013 Page 30/462 product. 26.04.2007 06.08.2009 30.05.2005 17.05.2005 31.05.2007
EASA STC no. STC holder Old STC ref. Revision Level Foreign/NAA STC ref. Model Description Limitations Conditions Date of issue 10017013 AEROMETALS EASA.IM.R.S.01430 FAA STC SR00981LA MD HELICOPTERS 369D Strut Assy - Landing Gear, p/n 369XH6001, 29.04.2008 MD HELICOPTERS 369E MD HELICOPTERS 369FF MD HELICOPTERS 369HE MD HELICOPTERS 369HM MD HELICOPTERS 369HS MD HELICOPTERS 500N EASA validation of FAA approved PMA part. 10017014 AEROMETALS EASA.IM.R.S.01431 FAA STC SR00766LA MD HELICOPTERS 369D Skid Tube Position Light Assys., p/n 29.04.2008 MD HELICOPTERS 369E 369XH92041, EASA validation of FAA MD HELICOPTERS 369FF MD HELICOPTERS 369HE MD HELICOPTERS 369HM MD HELICOPTERS 369HS approved PMA part. 10017015 AEROMETALS EASA.IM.R.S.01432 FAA STC SR01062LA MD HELICOPTERS 369A Exhaust Tailpipe Outlet hangar Assys., p/n 29.04.2008 MD HELICOPTERS 369D 369X8236, EASA validation of FAA approved MD HELICOPTERS 369E MD HELICOPTERS 369HE MD HELICOPTERS 369HM MD HELICOPTERS 369HS MD HELICOPTERS 500N PMA part. 10017016 AEROMETALS EASA.IM.R.S.01433 FAA STC ST01550SE MD HELICOPTERS 369D Scavenge Air Elbow Assy., p/n 29.04.2008 MD HELICOPTERS 369E AM369D290135, EASA validation of FAA MD HELICOPTERS 369FF MD HELICOPTERS 500N approved PMA part. 10017019 AEROMETALS EASA.IM.R.S.01437 FAA STC SR01136SE MD HELICOPTERS 369D Landing Gear Fillet Fairings p/n AM369A6200- 29.04.2008 MD HELICOPTERS 369E 45, -46, -57, -58; and Landing Gear Fairing MD HELICOPTERS 369HM Guides p/n AM369H6200-73, -74. EASA MD HELICOPTERS 369HS MD HELICOPTERS 500N validation of FAA approved PMA part. 10016708 AERONAUTICAL ACCESSORIES, INC EASA.IM.R.S.00548 FAA STC SR02381AT BELL 427 Manufacture and Installation of Passenger 1. Rotorcraft Flight Manual Supplement 26.01.2005 Sliding Door for Bell 427 Model Helicopters dated 7/09/2001, is a required part of this (FAA STC SR02381AT dated 19/09/2002). STC.2. 'Instruction for Continued Airworthiness', AAI Report No. AA-99043, Revision A dated 6/10/2000 is also a required part of this STC.3. This STC is approve 10016762 AERONAUTICAL ACCESSORIES, INC EASA.IM.R.S.01091 FAA STC SR09324RC-D BELL 407 Installaton of Passenger photo Window for Bell 1. The compatibility of this design change 407 Model Helicopters in accordance with:-the with other previously approved modifications FAA STC SR09324RC-D dated 22/9/2003-AAI must be determined by the installer.2. This 22.08.2005 Master Drawing List Report AA-01095, STC is approved only for the product Revision B, dated 19/3/2003. configuration as defined in the approved design data referred to in the paragraph 10016767 AERONAUTICAL ACCESSORIES, INC EASA.IM.R.S.01098 FAA STC SR01450LA BELL 407 Installation of Apical Industries, Inc. Emergency 1. The compatibility of this design change Float Assemply, Part number 604.9501 for Bell with other previously approved modifications 22.08.2005 407 Model Helicopters in accordancewith:-the must be determined by the installer.2. This FAA STC SR01450LA dated 27/5/2003.- STC is approved only for the product Master document List MD407-11 Revision C, configuration as defined in the approved design dated 28/4/2003. data referred to in the paragraph 10016770 AERONAUTICAL ACCESSORIES, INC EASA.IM.R.S.01102 FAA STC SR09239RC BELL 407 Installation of a Steerable Landing Light. None 10.05.2007 10016771 AERONAUTICAL ACCESSORIES, INC EASA.IM.R.S.01105 FAA STC SR01849AT BELL 212, 412, 412 EP Light weight nitrogen reservoir kit/Replacement of nitrogen cylinder for emergency flotation system kit. 20.12.2007 10016777 AERONAUTICAL ACCESSORIES, INC EASA.IM.R.S.01116 FAA STC SR02074AT BELL 427 Manufacture of Automatic Door Opener for Bell 1. The compatibility of this design change with 15.07.2005 427 Model Helicopters in accordance with the other previously approved modifications must FAA STC SR02074AT. AAI Master Drawing be determined by the installer.2. This STC is List Report AA-98109 dated 30/10/1998. FAA approved only for the product configuration as STC SR 02047AT dated 14/02/2000 (Atlanta defined in the approved design data referred to Aircraft Certification Office). in the paragraph "Desc 10016791 AERONAUTICAL ACCESSORIES, INC EASA.IM.R.S.01139 FAA STC SR01411AI BELL 407 Manufacture and Installation of console assembly 26.01.2006 10016840 AERONAUTICAL ACCESSORIES, INC EASA.IM.R.S.01211 FAA STC SR01844AT A109, A109A, A109A II, A109C Installation of Tail Rotor Lockout Kit for Agusta Compatibilty of this design change with 06.04.2006 A109E, A109K2, A119 A109, A109A, A109AII, A109C, A109E, previously approved modifications must be A109K2, A119 Model Helicopter determined by the installer. If the holder agreesto permit another person to use this certificate to alter the product, the holder shall give the other person written evidenc 10016860 AERONAUTICAL ACCESSORIES, INC EASA.IM.R.S.01236 FAA STC SR00235AT 206A, 206B, 206L, 206L-1, 206L-2, 206L-3, 206L-4, 407 Installation of Headset Retention Brackets None 29.08.2006 10016872 AERONAUTICAL ACCESSORIES, INC EASA.IM.R.S.01248 FAA STC SR02070AT BELL 427 Installation of Baggage Floor Protector 25.10.2006 10016902 AERONAUTICAL ACCESSORIES, INC EASA.IM.R.S.01279 FAA STC SR01687AT BELL 407 Manufacture of crew and passenger emergency push out windows 16.11.2006 10016920 AERONAUTICAL ACCESSORIES, INC EASA.IM.R.S.01305 FAA STC SR09373RC-D BELL 412, 412EP Bell Helicopter Vibration monitor (BHVM) System 31.05.2007 04/01/2013 Page 31/462
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