STC SA02036CH

3 Civil Air

(See Type Certificate Data Sheet No. 3A20 for complete certification basis)

Installation of two Walter a.s. Model M601E-11A engines and AVIA propeller model V510/90A/B five bladed propellers on Raytheon (Beechcraft) King Air 100 and A100 model airplanes in accordance with Premier Conversions, LLC Installation Manual, Initial Release, dated September 8, 2004 and Master Drawing List, Initial Release, dated September 8, 2004, or later FAA approved revision.

1. Compatibility of this design change with previously approved modifications must be determined by the installer.

2. FAA Approved Premier Conversions LLC Airplane Flight Manual Supplement modified in accordance with this STC, dated, August 31, 2004, FAA Approved August 31, 2004 or later FAA Approved revision, i s required.

3. Aircraft Specifications are the same as listed on Type Certificate Data Sheet A14CE except as listed in the FAA Approved Airplane Flight Manual Supplement for Raytheon 100 and A100 modified in accordance with this STC.

(cont…)

Nextant Aerospace, LLC 18601 Cleveland Parkway Cleveland, OH 44135

A14CE Raytheon Aircraft Company 100, A100 December 29, 2003

September 10, 2004

November 08, 2006; December 05, 2013;

June 05, 2017

(Signature) Roy Boffo Manager, Propulsion & Program Management Branch Chicago Aircraft Certification Office

(Title)

FAA FORM 8110-2-1(10-69) PAGE 3 of 3 PAGES

SA02036CH

LIMITATIONS AND CONDITIONS: (Continued)

4. Limits for Walter a.s. turboprop engine model M601E-11A and AVIA propeller model V510/90A/B are as published in the FAA Approved Airplane Flight Manual Supplement for Raytheon 100 and A100.

5. The life limit for the AVIA propeller model V510, in accordance with Type Certificate Data Sheet Number P2BO, and as referenced in the AVIA Maintenance Manual, is 6,000 flight hours.

6. Power lever positions below flight idle (Beta range) when aircraft is prohibited in flight and can result in severe overspeeding and/or loss of aircraft control.

7. Maximum weights for the Raytheon (Beech King Air) model 100 aircraft are as published in the FAA Type Certificate Data Sheet Number A14CE: Ramp 10,688 lb.; Takeoff 10,600 lb.; Landing 10,600lb.

8. Maximum weights for the Raytheon (Beech King Air) model A100 aircraft are as published in the FAA Type Certificate Data Sheet Number A14CE: Ramp 11,568 lb.; Takeoff 11,500 lb.; Landing 11,210 lb.; Maximum zero fuel 9,600 lb.

9. If the holder agrees to permit another person to use this certificate to alter the product, the holder shall give the other person written evidence of that permission.

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