Installation of Continental IO-520-B engine derated to power shown in the appropriate Airplane Flight Manual Supplement and Hartzell HC-C3YF-1/8468A-8R (Low 10.0° ± .2, High 36.0° ± 1.0 Blade Angle Stop at 30 inch Sta.) propeller or McCauley 2A36C23/84B-2 (Low 13.3°, High 29.7° Blade Angle Stop from Ref. Sta. 30) propeller in accordance with AeroStol drawing 3100B, Sheet 1, Rev. B, dated 11/15/75 and 3100, Sheet 2, dated 9/18/75, or later FAA approved revisions, for all of the above Beech model aircraft, except Model G33. For Model 33 installation of the Continental IO-520-BB engine derated to the power shown in the appropriate Airplane Flight Manual Supplement and McCauley 2A36C23/84B-O (Low 13.3°, High 29.7° Blade Angle Stop, Ref. Sta. 30) propeller in accordance with D’Shannon Products Drawing G3M2686BB, Rev. 1, dated 2/27/86 (5 sheets), or later FAA approved revisions.For Model H35 installation of the Continental IO-520-BB engine derated to the power shown in the appropriate Airplane Flight Manual Supplement and McCauley 3A32C406/82NDB-2 propeller in accordance with D’Shannon Products Drawing H353A32C406BB Rev. 1, dated 11/25/86 (5 sheets), or later FAA approved revisions.

Please contact modification supplier for further details.

STC Status: Reissued
STC Date: 17/06/11
Responsible Office: Chicago Aircraft Certification Office (ACE-115C), Tel: (847) 294-7358

Hawker Beechcraft Corporation

• 35-33
• 35-A33
• 35-B33
• 35-C33
• E33
• F33
• G33
• H35
• J35
• K35
• M35
• N35
• P35