1988 ASTRA/GULFSTREAM 1125


  • For Sale
  • 1988
  • ASTRA/GULFSTREAM 1125
  • N902AU
  • Not Listed
  • Miami, FL USA

385000 $385,000 USD
AS IS , OBO

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  • For Sale
  • 1988
  • ASTRA/GULFSTREAM 1125
  • N902AU
  • Not Listed
  • Miami, FL USA

General Specs (cont.)

10660

1473 STOH

1514 STOH

24650 lb

Used

2017

2017

BTH

9

Additional Classifications

Detailed Description

This is a beautiful, well-maintained Jet!
FOR SALE AS IS
No C inspection (Which can be performed at the local airport at a great price). 
No ADSB
Israel Aerospace Industries (IAI) developed the Astra from its Model 1124 Westwind business jet. Work on an improved Westwind began in the late 1970s, with the first prototype flight on 19 March 1984.

The original 1125 Astra was replaced by the Astra SP, announced in 1989; 37 were built. The third variant, the Astra SPX, flew for the first time in August 1994. This variant was renamed G100 from September 2002 following Gulfstream's acquisition of Galaxy Aerospace, which held the Astra type certificate, in May 2001.
Comfortable cabin
Separate Lavatory
Ample Room for Baggage
Separate A/C and Heat Controls for each passager.
Medium size Gallery for Hot and Cold Food and Drinks.
Crew: 2
Capacity: 6-9 passengers

Avionics / Equipment

Collins Pro Line 4

Airframe

Total Time = 10,660 hrs.
Total Landings = 8699

Engines / Mods / Prop

Powerplant: 2 × Honeywell TFE731-40-R-200G turbofans, 18.9 kN (4,250 lbf) thrust each
Engine 1 Time Remaining = 1,473 hrs.
Engine 2 Time Remaining = 1,514 hrs.

Interior / Exterior

New Interior
Beige with wooden accents
Good Paint
White with Blue and Red lines.

Remarks

Length: 16.94 m (55 ft 7 in)
Wingspan: 16.64 m (54 ft 7 in) (over winglets)
Height: 5.54 m (18 ft 2 in)
Wing area: 29.41 m2 (316.6 sq ft)
Aspect ratio: 8.8:1
Airfoil: IAI Sigma-2
Empty weight: 6,214 kg (13,700 lb)
Max takeoff weight: 11,181 kg (24,650 lb)
Fuel capacity: 4,910 L (1,300 US gal; 1,080 imp gal) usable
Maximum speed: Mach 0.875
Cruise speed: 896 km/h (557 mph, 484 knots)
Range: 5,462 km (3,394 mi, 2,949 nmi) (max fuel, four passengers)
Service ceiling: 14,000 m (45,000 ft)
Rate of climb: 19.33 m/s (3,805 ft/min)
Fuel consumption: 1750 lb. per hour