Commercial Aircraft Directory - Aircraft Specification

BAE Systems - Avro RJ-85ER

The Avro RJ85 was an improved derivative of the BAe 146-200 Series, offered after the Avro RJ family was launched on 08 June 1992. The RJ85 was powered by the improved Honeywell LF 507 turbofans rated at 31.14kN. Other improvements included an upgraded interior with a slightly wider passenger cabin and a digital flight deck and avionics suite. The first RJ85 was modified from a BAe 146-200 and flew for the first time prior to the official programme launch date on 23 March 1992. As with the original 146 Series, Avro RJ85 and RJ100 models were available in either QT or QC Combi or Convertible form, featuring a large cargo door on the left side of the rear fuselages, but no orders for these models were forthcoming. The initial RJ85 customer, Crossair took delivery of their first aircraft on 23 April 1993 and other major RJ85 customers included Lufthansa CityLine, Sabena, Mesaba and Air Botnia. In 1995 BAe became part of the AI(R) consortium alongside Franco-Italian manufacturer ATR and continued to market the Avro RJ family. AI(R) collapsed in 1997 but RJs continued to be marketed by BAe. Planned production of the type in Malaysia by Kazanah Nasional Berhad also fell through in 1997 and BAe elected to continue production on its own. In March 2000 BAE Systems announced plans to replace the Avro RJ in production with the new RJX series, powered by Honeywell AS977 turbofans, which would again be available in three fuselage lengths as the RJX70, 85 and 100. The first RJX, an 85 model flew for the first time on 28 April 2001, and the company planned to market three versions, the RJX70, 85 and 100. However, on 27 November 2001, BAE Systems announced the cancellation of the entire RJX programme, citing the poor sales prospects for the type in the aftermath of the “9/11” attacks in the USA. When the last Avro RJ off the Woodford production line was delivered to Air Botnia in November 2003, total Avro RJ production had reached 173, of which 87 were RJ85s.

View specification units in: METRIC | IMPERIAL

SPECIFICATION

First Flight date: Feb 2001  
Certification date:  

PRINCIPAL DIMENSIONS

Fuselage width: 3.56 m 
Fuselage height: 8.61 m 
Fuselage length: 28.6 m 
Cabin length: 17.81 m 
Cabin width: 3.42 m 
Cabin height: 2.07 m 
Cabin volume: 60 m3 
Hold volume: 18 m3 

WEIGHTS

Empty operating: 24,630 kg 
Max zero fuel: 35,833 kg 
MTOW: 42,184 kg 
MLW: 38,555 kg 
Standard fuel capacity: 11,728 kg 
Max fuel capacity: 12,901 kg 

SPEEDS

Normal cruise: 703 km/h 
Max cruise: 788 km/h 

PERFORMANCE

Long Range Cruise alt: 10,668 m 
Max ceiling: 10,668 m 
Take off field length: 1,640 m 
Landing field length: 1,190 m 
Max Payload Range: 2,150 m 
Range notes: Data is for RJ85ER.Payload Max Fuel calculated at 1850 litres weighing 0.785 kg/litres.  
Max passengers: 112  
Typical passengers: 85  

POWERPLANT

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

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