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Aircraft model

RAYTHEON AIRCRAFT COMPANY 390

Everything here is true of every aircraft of the type, not of any one aircraft.

The Premier I is a light jet with a composite fuselage built by filament winding, which let Raytheon make the cabin wider than any competitor of its size without the weight penalty of metal. It cruises at 451 knots and is certified single-pilot, and the cabin is genuinely the roomiest in the entry-level class. The registry string covers both the Premier I and the Premier IA, and the difference is worth knowing. Raytheon announced the IA in May 2005 and certified it that October, with production switching at serial RB-435: the same FJ44-2A engines and the same numbers, but a redesigned interior with an acoustic liner and better seating, updated Pro Line 21 avionics and a list of systems fixes that addressed the early aircraft's reputation for teething trouble. Externally nothing changed. A 2006 or later aircraft is a IA; a 2001 to 2005 one is a I, and the price gap between them reflects the interior and the support history more than the aeroplane.

The complication is runway performance. The Premier has no thrust reversers and a relatively high approach speed, and its landing distance requirement is long for a light jet — it needs more runway than its size suggests and that limits which airports it can realistically use. Later aircraft addressed some of this. The composite fuselage requires specialist repair, and Beechcraft's bankruptcy and the type's discontinuation in 2013 leave support running through Textron for a small fleet. A type rating is required.

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What it is

Seats8
Landing geartricycle
Engines2
EngineWilliams FJ44-2A
Horsepower—
FuelJetA
Certification basisFAR23
Production start2001
Production end2013
Endorsements requiredmulti-engine

Performance

Cruise speed451 KTAS
Range1,160 nm
Service ceiling41,000 ft
Climb rate3,300 ft/min
Stall speed (Vso)85 KCAS
Takeoff over 50 ft3,792 ft
Landing over 50 ft3,170 ft

Load and fuel

Seats8
Useful load4,000 lb
Full-fuel payload583 lb
Max takeoff weight12,500 lb
Empty weight8,500 lb
Usable fuel510 gal
Fuel burn at cruise130 gal/h

Cost of ownership

Price, low$1,100,000
Price, high$2,500,000
Prices as of2026
Engine TBO—
Overhaul cost, low$500,000
Overhaul cost, high$700,000

The fleet and its record

Registered, all time188
Active fleet130
Median year built2004.0
NTSB events, last 10 years2
Fatal events, last 10 years1
Events per 1,000 active, last 10 years15.381
Personal-flying events per 1,000 active02
Ownership transfers, last 24 months38
Transfers per 100 active29.233
Airworthiness directives22
Directives, last 5 years0
Rate confidenceok
  1. Events per 1,000 active, last 10 years: per 1,000 active aircraft · base 130 active.
  2. Personal-flying events per 1,000 active: per 1,000 active aircraft · base 130 active.
  3. Transfers per 100 active: per 100 active aircraft · base 130 active.

Peer scores6

Peer classFixed wing multi-engine, turbo-fan, 2 engines, 7+ seats
Accident record—1
Severity—2
Access1.7 of 103
Support4.7 of 104
Liquidity3.4 of 105

These record scores treat RAYTHEON AIRCRAFT COMPANY 390 as one design with the same aircraft registered under other names: it includes 64 aircraft registered under HAWKER BEECHCRAFT CORP. Prices are not combined.

  1. Accident record: class median 1.23 · 42 models in class.
  2. Severity: class median 10.
  3. Access: class median 9,850.
  4. Support: class median 197.5.
  5. Liquidity: class median 32.81.
  6. Each of the five categories places the model within its peer class, from 0 (the worst of the class) to 10 (the best): a position among comparable models, not a grade. The overall score is the sum of the categories shown that are scored, out of 10 for each (50 when all five are); it is given only when at least 4 of the five are scored, and it can be set against another model's only when both are in the same peer class and scored on the same categories.
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