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SPAR APPLICABLE STCs
To link to the applicable STCs,please click on the STC number in the right hand column. To download an Adobe Acrobat copy of the FAA AMOC letter verifying that the GHTI Fin Spar Repair Kit has been designated as a terminating action for compliance to AD 99-25-12, click here.
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| NOTE: ALL OF THE ABOVE INSTALLATIONS ARE LIMITED TO THE AIRCRAFT SHOWN WITH STANDARD TAIL BOOM CONFIGURATIONS, ORIGINAL ENGINE TYPES AND ORIGINAL 204 TAIL ROTOR SYSTEM. |
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| NOTE: THE ABOVE INSTALLATIONS ARE LIMITED TO THE AIRCRAFT LISTED WITH STANDARD TAIL BOOM CONFIGURATIONS HAVING 204-031-090-1 CAMBERED FIN INSTALLED |
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