Beechcraft D17S Staggerwing — Other Documents

This document is a Type Acceptance Report for the Beechcraft Model G17S, issued by the Aircraft Certification Unit in New Zealand. It outlines the basis for granting Type Acceptance Certificate No. 4/21B/16, which allows the G17S to operate in the Standard Category. The report confirms that the G17S meets the necessary airworthiness standards as validated by the FAA Type Certificate number 779. It details the aircraft's specifications, including its engine, propeller, and maximum certified takeoff weight (MCTOW). The report also highlights that there are no special import requirements for the G17S into New Zealand, making it eligible for an Airworthiness Certificate provided all operational requirements are met.

• Model: Beech G17S
• Engine: Pratt & Whitney R-985-AN-4
• Propeller: Hamilton Standard 2D30/6095A-15
• Maximum Certified Takeoff Weight (MCTOW): 4,250 lb
• Type Acceptance Certificate No. 4/21B/16 granted on January 23, 2004