HAWKER 400A — Pilot's Operating Handbook
1 pilot's operating handbook reference for the HAWKER 400A.
Overview
Type Certificate Data Sheet No. 69 · 2010
This document is the Type Certificate Data Sheet for the Hawker 400A aircraft, issued by the Japan Civil Aviation Bureau. It outlines the airworthiness requirements, engine specifications, operational limits, and other essential information for the aircraft's certification and operation.
- Type Certificate No. 69 issued for Hawker 400A.
- Equipped with 2 Pratt & Whitney Canada JT15D-5 or JT15D-5R turbofan engines.
- Maximum takeoff weight is 16,100 lb.
- Maximum operating altitude is 45,000 ft.
- Minimum crew requirement is 2 persons.
- Total fuel capacity is 217.2 gallons per wing tank.
- Maximum baggage capacity is 350 lb in the aft cabin.
- Aircraft must operate under specific airworthiness regulations.
1 document
HAWKER 400A — Pilot's Operating Handbook FAQ
How many Pilot's Operating Handbook documents does Sprinkle have for the HAWKER 400A?
Sprinkle has 1 Pilot's Operating Handbook document on file for the HAWKER 400A.
What year is the HAWKER 400A Pilot's Operating Handbook?
The HAWKER 400A Pilot's Operating Handbook on file is dated 2010.
Where does Sprinkle's HAWKER 400A Pilot's Operating Handbook come from?
This HAWKER 400A Pilot's Operating Handbook was originally published by go.jp and is hosted on Sprinkle with full text and specs.