} }

Overview

The Raytheon Premier I is a small, twin turbofan-powered entry-level corporate jet configured as a cantilever low-wing monoplane with a T-tail. The retractable tricycle landing gear is of a relatively narrow track and employs straight oleo main struts. The fuselage is built in two main sections and is constructed entirely of carbon fiber and Nomex-honeycomb composite mThe preliminary design layout of the Premier I's cabin interior is to include seating for six passengers, possibly in a club-plus-two arrangement with an additional passenger seat available in the right seat on the flight deck, if desired. Cabin entry is via an airstair door located on the port side of the fuselage forward of the wing. Cabin dimensions are 13.5ft in length, 5.4ft in height, and 5.5ft in width.aterials.


Aircraft Specifications


Certified Crew

1

Typical / Maximum Cabin Passenger Capacity

6/7

Balanced Field Length [SL/ISA TMP] (FT)

3792

Length (FT)

46

Wingspan (FT)

44.5

Height (FT)

15.3

Cabin Height (FT)

5.4

Cabin Width (FT)

5.5

Cabin Length (FT)

13.5

Baggage Capacity Internal / External (CFT)

23 / 54

Powerplant

2 WMS FJ44-2A

Years Aircraft Manufactured

2001-2005

Estimated Retail Price Low

800000

Estimated Retail Price High

1150000

Aircraft Category

Light Jet



Operating Cost Overview

Aircraft variable and fixed costs are important to determine before making a purchase decisions or planning annual budgets. Our interactive graphs demonstrate the relationships between fuel cost and annual flight hour utilization.



$
hrs


If you are further along in the aircraft buying process, our comprehensive aircraft operating cost reports are the perfect companion in your decision making process. View a sample or buy a report and have it available in minutes.




Range Map

The Premier I has a range of 1,178 nautical miles. Type in your city or airport identifier for a visual representation of the NBAA IFR Range (NM) for this aircraft.


Legend



}