Commercial Aircraft Directory - Aircraft Specification

BAE Systems - BAe 146-300QT

As originally proposed in 1984, the BAe 146-300 would have featured a fuselage stretch of 3.2 metres, allowing six-abreast seating for up to 134, new more powerful Allied Signal LF 507 turbofans, new winglets and a host of other minor changes. In the end however US customers were more interested in a more modest stretch of the Series 200 which would allow for 100 passengers to be accommodated in a more spacious five-abreast seating layout and it was this configuration which was adopted for production. The aerodynamic prototype of the BAe 146-300 was converted from a Series 100 airframe and flew for the first time on 1 May 1987. The first production Series 300 took to the air for the first time in June 1988. The Series 300 retained the same engines and wing from the earlier variants and differed from the Series 200 essentially in the addition of fuselage plugs forward and aft of the wing which added 2.39 meters to its length. The UK Type Certificate was awarded in September 1988. Lead customer and United Express carrier Air Wisconsin took delivery of their first aircraft on 16 December 1988, placing the type into service later that month. The later Avro RJ100 and proposed RJ115 were improved derivatives of the 300 Series, powered by the improved Honeywell LF 507 turbofan rated at 31.1kN. Other improvements included an upgraded interior with a slightly wider passenger cabin and a digital flight deck and avionics suite. The 300QC was a proposed combi version and the 300QT a dedicated freighter, both of which featured a large freight door 3.33m (l) x 1.93m (h) on the port side fuselage aft of the wing. The first RJ100 customer, Aegean Airlines took delivery of their first aircraft on 30 April 1999. Although BAe marketed the RJ115 with additional emergency exits allowing for a maximum seating capacity of 128 passengers in a high density six-abreast layout, no orders were forthcoming. When production was completed 221 BAe 146s of all variants had been produced. This included 60 Series 300s and 10 Series 300QTs. Total Avro RJ production reached 132, of which 49 were RJ100s.

View specification units in: METRIC | IMPERIAL

SPECIFICATION

First Flight date: 1 May 1987  
Certification date: 6 Sep 1988  
Launch customer(s): United Express
 

PRINCIPAL DIMENSIONS

Fuselage width: 3.56 m 
Fuselage height: 8.61 m 
Fuselage length: 30.99 m 
Cabin length: 20.2 m 
Cabin width: 3.42 m 
Cabin height: 2.03 m 
Cabin volume: 69 m3 
Hold volume: 23 m3 

WEIGHTS

Empty operating: 24,800 kg 
Max zero fuel: 36,514 kg 
MTOW: 45,132 kg 
MLW: 39,235 kg 
Standard fuel capacity: 11,728 kg 
Max fuel capacity: 12,901 kg 

SPEEDS

Normal cruise: 699 km/h 
Max cruise: 789 km/h 

PERFORMANCE

Long Range Cruise alt: 8,839 m 
Max ceiling: 9,449 m 
Take off field length: 2,133 m 
Landing field length: 1,265 m 
Max Payload Range: 1,927 m 
Range notes: Payload Max Fuel calculated at 11728 litre weighing 0.785 kg/litre.  
Max passengers: 116  
Typical passengers: 103  

POWERPLANT

Category: Turbofan  
Manufacturer: Honeywell  
Model/Submodel: ALF502 R-6  
Thrust: 33 kN  

POWERPLANT

Category: Turbofan  
Manufacturer: Honeywell  
Model/Submodel: LF507 1H  
Thrust: 31 kN  

MAINTENANCE PROVIDERS

National Jet Systems