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Beechcraft D17S Staggerwing — Other Documents

2 other documents references for the Beechcraft D17S Staggerwing.

Overview
Type Acceptance Report TAR 4/21B/16 – Beech G17S · 2004

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
2 documents
Beechcraft D17S Staggerwing — Other Documents FAQ
How many Other Documents documents does Sprinkle have for the Beechcraft D17S Staggerwing?

Sprinkle has 2 Other Documents documents on file for the Beechcraft D17S Staggerwing.

What year is the Beechcraft D17S Staggerwing Other Documents?

The Beechcraft D17S Staggerwing Other Documents on file is dated 2004.

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The Beechcraft D17S Staggerwing Other Documents runs 8 pages.

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This Beechcraft D17S Staggerwing Other Documents was originally published by www.aviation.govt.nz and is hosted on Sprinkle with full text and specs.