| 词条 | Beechcraft Premier I | |||||||||||||||||
| 释义 |
The Beechcraft Premier I is a light business jet aircraft manufactured by the Beechcraft division of Hawker Beechcraft. The aircraft was designed to compete with the Cessna CitationJet series of aircraft.[3] DevelopmentDesign of the Premier I began early in 1994 under the designation PD-374 (PD for Preliminary Design), and development was authorized to continue early the following year. The aircraft was officially launched at the annual National Business Aviation Association Convention in September 1995 and construction of the first prototype commenced late in 1996.[3] In the mid-1990s, the light jet was to be priced at $5 million.[6] The Premier I prototype was rolled out on 19 August 1998 and its first flight was on 22 December 1998; four prototypes were used in the flight test program.[3] Its FAA Type Certificate was issued on 23 March 2001.[4] After development delays, the aircraft entered service in 2001 but with poor runway performance, erratic lift dump and brakes, a noisy cabin and substandard cockpit. It was upgraded as the Premier IA in 2006 for $7 million with better brakes, avionics and cabin, and 163 were built in five years.[6] It was certified on 22 September 2005.{{dubious|reason=IA not in FAA TCDS, EASA TCDS only states "The Model 390 with avionics and interior upgrades is also known as the Premier IA, serial numbers RB-102 and RB-135 and after": not a dated approval, only a SN range|date=February 2019}} In 2018, used aircraft from 2003 to 2011 were priced at $1.28 to 2.4 million.[5] DesignThe Premier I is constructed with a high-strength composite, carbon fiber/epoxy honeycomb structure fuselage. The Premier I and IA can be certified as light aircraft for operation by a single pilot. The powerplants are Williams International FJ44-2A engines. Its cabin is nearly as wide as a Citation Excel with {{cvt|3|in}} less headroom, and seating is {{cvt|11.2|ft}} long, similar to a CJ2, with a four-seat club plus two aft chairs and an enclosed, {{cvt|2.3|ft}} long aft lavatory. BOWs are usually around {{cvt|8,400|lb}}, leaving {{cvt|570|lb}} for the payload at full tanks.The Premier 1A has a Mach 0.8 MMo, {{cvt|451|kn|km/h}} cruise at FL310 and a {{cvt|817|lb}}/h fuel burn at {{cvt|424|kn|km/h}} and midweight. It can fly four passengers over {{cvt|1,105 or 1,365|nmi|km}} with two passengers and can take off within {{cvt|3,792|ft}} at ISA temperatures and sea-level.[6] Line maintenance comes at 200 h intervals, A checks at 600 h and B checks at 1,200 h, plus calendar inspections, approximating $300 per hour. Engine maintenance is budgeted for $300 per h for both, with 2,500 h hot section inspections and 5,000 h TBOs. Competition used include the CJ2 and the Nextant 400XT, both have tighter cabins but better airfield performance, the CJ2 can fly four passengers over {{cvt|1,500|nmi|km}} but is {{cvt|30-40|kn|km/h}} slower and around $1 million more expensive, while the 400XT can fly {{cvt|1,800|nmi|km}} for the same value but are usually high-time jets.[6] Variants
Specifications (Premier IA){{Aircraft specs|ref=Hawker Beechcraft[7] |prime units?= imp |crew= 1 |capacity= 6 / 7 |length m=14.02 |span m=13.56 |height m=4.67 |wing area sqm=22.9 |wing area sqft=247 |wing area note=[8] |aspect ratio={{#expr:13.56/(22.9/13.56)round2}} |airfoil= |empty weight kg=3,901 |empty weight note=Basic Operating |max takeoff weight kg=5,670 |fuel capacity=3,670 lb / 1,665 kg |more general=
|eng1 number=2 |eng1 name=Williams FJ44-2A |eng1 type=Turbofan |eng1 kn=10.23 |eng1 lbf= |eng1 note= |max speed kmh=841 |max speed note=max cruise |range km=1,530 |range note=Max Payload |ferry range km=2,750 |ceiling m=12,500 |wing loading lb/sqft={{#expr:12500/247round1}} |fuel consumption lb/mi={{#expr:817/(424*1.15078)round2}}[6] |thrust/weight={{#expr:2300*2/12500round2}} |more performance=
|avionics=
}} See also{{Aircontent||related=
|similar aircraft=
|lists= |see also= }} References1. ^1 {{cite news |url= https://www.flightglobal.com/news/articles/nbaa-business-jet-designs-that-changed-the-industry-452471/ |title= NBAA: Business jet designs that changed the industry |date= 12 Oct 2018 |author= Murdo Morrison |work= FlightGlobal}} 2. ^{{cite news |url= http://awin.aviationweek.com/portals/awin/pdfs/BCAOpPlanningGuide/2012_Production.pdf |title= Operations Planning Guide |publisher= Aviation Week |work= Business & Commercial Aviation |date= August 2012}} 3. ^1 2 Airliners.net Premier I page. Retrieved: 23 August 2008. 4. ^{{cite web |url= https://rgl.faa.gov/Regulatory_and_Guidance_Library/rgMakeModel.nsf/0/0fddeeff04b2f4c6862580fe00586e42/$FILE/A00010WI_Rev_10.pdf |title= Type Certificate data sheet No. A00010WI |date= October 12, 2016 |publisher= FAA}} 5. ^{{cite magazine |url= https://www.ainonline.com/sites/default/files/full-issues/ain_1218.pdf |title= For many models, market hitting the apex |magazine= Aviation International News |author= Mark Huber |date= December 2018 |pages= 20-21, 24}} 6. ^1 2 3 4 {{cite news |url= https://aviationweek.com/business-aviation/hawker-beechcraft-premier-1a-midsize-cabin-light-jet-airframe |title= Hawker Beechcraft Premier 1A: Midsize Cabin On Light-Jet Airframe |date= Feb 22, 2019 |author= Kent S. Jackson |work= Business & Commercial Aviation}} 7. ^{{cite web |url= https://web.archive.org/web/20130103171551/http://www.hawkerbeechcraft.com/beechcraft/premier_ia/specifications.aspx |title= Specifications |work= Premier IA |publisher= Hawker Beechcraft}} 8. ^{{cite web |url= https://www.easa.europa.eu/sites/default/files/dfu/TCDS%20EASA.IM_.A.073%20Issue%2002.pdf |title= Type certificate data sheet No. EASA.IM.A.073 for Beechcraft 390 (Premier I and IA) |date= 13 March 2018 |publisher= EASA}} External links{{Commons category|Beechcraft Premier}}
6 : United States business aircraft 1990–1999|Beechcraft aircraft|Twinjets|Low-wing aircraft|T-tail aircraft|Aircraft first flown in 1998 |
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