|
|
 |
|
 |
 |
|
|
|
|
|
|
|
| The BAe 146-200 is a stretch of the 146-100, while the Avro RJ85 in turn is a modernised version of the 146-200. The 146-200 is essentially similar to its smaller stablemate, but has a 2.39m (7ft 8in) longer fuselage, is slightly higher, features 35% greater underfloor cargo volume, has slightly different performance figures and heavier weights. The stretch consists of five extra fuselage frame pitches. The first BAe 146-200 made the type's maiden flight on August 1 1982, while the UK CAA awarded the 146-200's type certificate on February 4 the following year. The improved Avro RJ85 first flew on March 23 1992, and like the small RJ70 and larger RJ100, is a modernised development of the basic 146, with improvements including more reliably and efficient FADEC equipped AlliedSignal LF 507 engines, enhanced `Spaceliner' cabin and a digital flightdeck. |
|
|
|
|
| Seating (normal) |
85 |
Max Takeoff (lbs) |
93,000 |
| Seating (maximum) |
112 |
Certified Ceiling (ft) |
- |
|
| Engines |
4 Textron Lycoming ALF 502R5 |
To (Sealevel, ISA Temp) (ft) |
4,950 |
| Output lbs ea. Flat Rating |
6900 lbs |
Landing Distance (ft) |
3,620 |
| Maximum Mach No. |
0.73 |
Max Range (fuel) (nm) |
1,570 |
| High Speed Cruise (Kts) |
414 |
Max Range (payload) (nm) |
1,130 |
|
| Flight Time 300nm |
- |
Flight Time 1000nm |
- |
| Flight Time 600nm |
- |
|
|
|
| External |
|
Internal |
|
| Length (ft) |
93.90 |
Length (ft) |
58.40 |
| Height (ft) |
28.10 |
Height (ft) |
6.70 |
| Span (ft) |
86.00 |
Width: Max floor (ft) |
11.20 |
|
|
|
 |
|
 |
|
|
|
