Installation of fully enclosed main landing gear door system and associated actuation mechanism per Raisbeck Engineering Drawing List 84-1004, dated July 9, 1984, or later FAA approved revision. This modification must be maintained in accordance with Raisbeck Engineering Document No. 85-120 issued January 1990, or later FAA-accepted revision.

Please contact modification supplier for further details.

STC Status: Amended
STC Date: 18/04/06
Responsible Office: Seattle Aircraft Certification Office (ANM-100S), Tel: (425) 917-6400

Hawker Beechcraft Corporation

• 65-90
• 65-A90
• B90
• C90
• C90A
• C90GT
• E90