SA970NE

Installation of wing filler for auxiliary fuel tanks, miscellaneous structural modifications and optional radome, dual alternator system, bow compartment covers, upper fin revision, disassembly provisions and dual rudder/aileron electric trim system in accordance with Aerofab, Inc. Drawing List 4-0001, Revision I, dated October 23, 1996, or later FAA-approved revision. The installation is applicable in the following configurations: United States of America Department of Transportation - Federal Aviation Administration Supplemental Type Certificate (Continuation Sheet) ___________________________________________________________________________________________________________________________________ Any alteration of this certificate is punishable by a fine of not exceeding $1,000, or imprisonment not exceeding 3 years, or both. ___________________________________________________________________________________________________________________________________ FAA Form 8110-2-1(10-69) PAGE 4 of 4 PAGES This certificate may be transferred in accordance with FAR 21.47. United States of America Department of Transportation -- Federal Aviation Administration Supplemental Type Certificate _____________________________________________________________________________________________________________________________________ Any alteration of this certificate is punishable by a fine of not exceeding $1,000, or imprisonment not exceeding 3 years, or both. _____________________________________________________________________________________________________________________________________ FAA Form 8110-2(10-68) PAGE 1 of 1 PAGES This certificate may be transferred in accordance with FAR 21.47. CONFIGURATION 1: Basic installation with aft seats installed in accordance with Configuration 1 of STC SA469NE. Optional items may be installed in any combination as follows: Option 1: Radome In accordance with drawings 150017, 190011, 190018 and 190019. Mass with an equivalent weight of 35 lbs. may be installed with a center of gravity no farther forward than 6.61 inches aft of bulkhead 190011-11, as defined in Aerofab, Inc. Engineering Report 4-250-2, dated November 4, 1991, and drawing 190019. This STC does not approve the installation of a radar, antenna, wave guide or transmitter, nor radar/radome system compatibility. Option 2: Dual Alternator System In accordance with drawings 4-7781 and 4-7782. Option 3: Bow Compartment Covers In accordance with drawing 4-3501. Option 4: Upper Fin Revision In accordance with drawing 4-2652, Revision C. Option 5: Disassembly Provisions In accordance with drawing 300015. Option 6: Dual Rudder/Aileron Electric Trim System In accordance with drawing 4-3519 and STC SA1142SO. CONFIGURATION 2: Same as Configuration 1 except aft sets installed in accordance with Configuration 2 of STC SA469NE and aft seat weight restriction placard installed in accordance with drawing 4-7003. Held by Revo INC, which holds 13 approved modifications in all. Last revised September 30, 2004. System: flight controls.