04/01/2013 Page 1/462 - EASA
04/01/2013 Page 1/462 - EASA
04/01/2013 Page 1/462 - EASA
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<strong>EASA</strong> STC no. STC holder Old STC ref. Revision Level Foreign/NAA STC ref. Model Description Limitations Conditions Date of issue<br />
10028641 AERONAUTICAL ACCESSORIES, INC BELL 206 A & B Installation of Aft Passenger Seat Shoulder None Prior to installation of this modification it 29.<strong>01</strong>.2<strong>01</strong>0<br />
Harness/Lap Belt Assemblyfor Bell Helicopter<br />
must be determined thatthe<br />
Textron 206 A / B Models<br />
interrelationship between this modification<br />
and any other previouslyinstalled<br />
modification and/ or repair will introduce<br />
no adverse effectupon the airworthiness<br />
of the product.<br />
10028796 AERONAUTICAL ACCESSORIES, INC FAA STC SR02162LA BELL 407 Installation of Mounting Provisions for a Tail<br />
Boom Radar Altimeter inaccordance with<br />
Meeker Aviation Drawing List for Radar<br />
Altimeter MountKit, AA-TBA-16-<strong>01</strong>0, and<br />
Document List of Radar Altimeter Mount<br />
Kit, AA-TBA-16-<strong>01</strong>1.<br />
This STC provides mounting provisions only; it<br />
does not allow the holderto install an altimeter<br />
or any wiring to power an altimeter.<br />
Prior to installation of this modification it 10.02.2<strong>01</strong>0<br />
must be determined thatthe<br />
interrelationship between this modification<br />
and any other previouslyinstalled<br />
modification and/ or repair will introduce<br />
no adverse effectupon the airworthiness<br />
of the product.<br />
10028797 AERONAUTICAL ACCESSORIES, INC FAA STC ST02121LA BELL 407 Installation of a Tail Boom Antenna Mount Kit in This STC provides mounting provisions only; it Prior to installation of this modification it 10.02.2<strong>01</strong>0<br />
accordance with MeekerAviation MDL for VHF does not allow theholder to install an antenna must be determined thatthe<br />
Communication Antenna Mount Kit, AA-TBA- or any wiring to power an antenna.<br />
interrelationship between this modification<br />
<strong>01</strong>0.<br />
and any other previouslyinstalled<br />
modification and/ or repair will introduce<br />
no adverse effectupon the airworthiness<br />
of the product.<br />
10028872 AERONAUTICAL ACCESSORIES, INC FAA STC SR09325RC BELL 407 Installation of Bulged Skylight in accordance<br />
with AeronauticalAccessories, Inc. Drawing<br />
List, Report No AA-<strong>01</strong>070<br />
10028891 AERONAUTICAL ACCESSORIES, INC FAA STC SR09326RC BELL 407 Development and Installation of High Visibility<br />
Crew Door in accordancewith Aeronautical<br />
Accessories, Inc. Drawing List, Report No AA-<br />
<strong>01</strong>073<br />
10028893 AERONAUTICAL ACCESSORIES, INC FAA STC SR09376RC-D BELL 407 High Visibility Door Kits in accordance with<br />
Aeronautical Accessories,Inc. Drawing List<br />
Report No AA-05155<br />
10031747 AERONAUTICAL ACCESSORIES, INC FAA STC SR00646AT AB412, AB412EP Replacement Low Skid Landing Gear<br />
Crosstubes<br />
10033707 AERONAUTICAL ACCESSORIES, INC FAA STC SH1281SO 206A, 206B, 206L, 206L-1<br />
206L-3, 206L-4, 407<br />
10034699 AERONAUTICAL ACCESSORIES, INC FAA STC SR09536RC-D 429 Installation of Health and Usage Monitoring<br />
System (HUMS)<br />
None Prior to installation of this modification it<br />
must be determined thatthe<br />
interrelationship between this modification<br />
and any other previouslyinstalled<br />
modification and/ or repair will introduce<br />
no adverse effectupon the airworthiness<br />
of the product.<br />
16.02.2<strong>01</strong>0<br />
None Prior to installation of this modification it<br />
must be determined thatthe<br />
interrelationship between this modification<br />
and any other previouslyinstalled<br />
modification and/ or repair will introduce<br />
no adverse effectupon the airworthiness<br />
of the product.<br />
17.02.2<strong>01</strong>0<br />
None Prior to installation of this modification it<br />
must be determined thatthe<br />
interrelationship between this modification<br />
and any other previouslyinstalled<br />
modification and/ or repair will introduce<br />
no adverse effectupon the airworthiness<br />
of the product.<br />
17.02.2<strong>01</strong>0<br />
None Prior to installation of this modification it<br />
must be determined thatthe<br />
interrelationship between this modification<br />
and any other previouslyinstalled<br />
modification and/ or repair will introduce<br />
no adverse effectupon the airworthiness<br />
of the product.<br />
09.09.2<strong>01</strong>0<br />
Maintenance Step. None. Prior to installation of this modification it<br />
must be determined thatthe<br />
interrelationship between this modification<br />
and any other previouslyinstalled<br />
modification and/ or repair will introduce<br />
no adverse effectupon the airworthiness<br />
of the product.<br />
<strong>04</strong>.02.2<strong>01</strong>1<br />
The HUMS kit is installed on a non-<br />
Prior to installation of this modification it 20.<strong>04</strong>.2<strong>01</strong>1<br />
required/non-hazardous basis. Theutilization of must be determined thatthe<br />
the HUMS kit for maintenance credit is limited interrelationship between this modification<br />
to: 1)main rotor track and balance; 2) tail rotor and any other previouslyinstalled<br />
dynamic balance; and 3)frahm vibration modification and/ or repair will introduce<br />
absorber tuning. HUMS data may not be no adverse effectupon the airworthiness<br />
of the product.<br />
<strong>04</strong>/<strong>01</strong>/2<strong>01</strong>3 <strong>Page</strong> 33/<strong>462</strong>
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