British Aerospace ATP Aircraft

ATP, RV Smith from British Built Aircraft

Production Details

Design Company:

British Aerospace

First Flight:

6 August 1986

ATP:

63 - British Aerospace

J61:

4 - British Aerospace

Type Specification

Applies to:

British Aerospace ATP

Type:

Turboprop powered regional airliner

Wing:

Low wing cantilever monoplane. All metal structure. Wing has dihedral and tapers from root to tip, unswept

Fuselage:

All metal, pressurized circular fuselage

Tail Unit:

Single fin and rudder with tailplane mounted on fuselage

Landing Gear:

Retractable tricycle undercarriage. Nose gear retracts forwards into fuselage with main gear retracting forward into engine nacelles

Power Plant:

Two 2,653 shp Pratt & Whitney Canada PW126A turboprops driving six blade constant speed propellers mounted in nacelles on wing leading edge

Accommodation:

Flightcrew of two. Typical seating for 68 in cabin

Span:

100 ft 6 in

Length:

85 ft 4 in

Height:

24 ft 11 in

Wing Area:

842.8 sq ft

Empty:

31,290 lb

Max Takeoff:

50,550 lb

Max Cruise:

266 kt

Range:

800 nm

Preserved in British Museums

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