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Description:

The Learjet 35A is considered "The Ultimate Light Jet.” The Lear 35A offers seating for up to eight passengers. Whether you want to work quietly and confidentially or simply recline, rest and relax, the Lear 35 lets you do it in style. Learjet is synonymous for speed. With this Lear 35A, you get where you are going fast.

 

Specs:

Passengers: 8 (default)

Lavatory: Enclosed

Maximum Speed: 872 km/h

Maximum Altitude: 51,000 ft.

Range: 2,100nm (default)

Cabin Size: 4’9” (width) x 12’9” (length) x 4’3” (height)

Baggage Capacity: 40 cu. ft. (default)

 

CABIN

The cabin has a floor level cabin width of 0.9m and can seat up to eight passengers. The cabin is fitted with a club-style three-seater divan and four Erda adjustable seats and folding tables. There is 1.13m³ of baggage space and an external baggage locker is available which increases the total baggage capacity to 1.47m³.

FLIGHT DECK

The cockpit is equipped with conventional and manual controls for the pilot and co-pilot. The aircraft can be fully manually controlled in flight. The Honeywell digital avionics system includes a five-tube electrical flight instrumentation system, EFIS 50, with a UNS-1M FMS flight management system, a KFC 3100 dual digital three-axis autopilot and flight director and a dual Series III navigation and communications system.

The wing, engine intakes and the windscreen are fitted with bleed air de-icing and the tail plane has an electrical de-icing system. The radome is equipped with an alcohol spray that prevents ice from being shed and entering the engines.

ENGINES

The two rear mounted turbofan engines, Honeywell TFE73131-2b’s, are fitted with a digital electronic engine control system, an engine synchronizer and a Dee Howard thrust reverser. The engines provide 15.56kN at takeoff.

The integral wing fuel tanks can hold 1,272kg of fuel and, with an optional fuselage tank; the total fuel can be increased to 1,871kg. The aircraft has single point pressure re-fuelling and the fuselage fuel is transferred by gravity or by pump.

PERFORMANCE

With full seating and maximum fuel capacity, the aircraft can take off from runways shorter than 1,067m (3,500ft) and can climb to 15,545m (51,000ft). The aircraft can turn through 180° in a turning radius of 11.9m.

The normal cruise speed is 872km/h and the maximum operating altitude is 51,000ft (15,545m). With a crew of two and eight passengers, the aircraft's maximum range is 2100nm.

 

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