Performance Specification

Make	ASTRA	ASTRA	ASTRA
Model	1125	1125SP	1125SPX
Serial Number	ORIGINAL	ORIGINAL	ORIGINAL
ENGINES
Number	2	2	2
Make	GARRETT	GARRETT	GARRETT
Model	TFE-731-3A-200G	TFE-731-3A-200G	TFE-731-40R-200G
Thrust LB Per Engine	3,700.00	3,700.00	4,250.00
Shaft HP Per Engine	0.00	0.00	0.00
Common TBO (hours)	4,200	4,200	4,200
FUSELAGE DIMENSIONS
Length	55.60	55.60	55.70
Height	18.20	18.20	18.20
Wing Span	52.70	52.70	54.70
TYPICAL CONFIGURATION
Crew	2	2	2
Passengers	6	6	6
Pressurization (psi)	8.80	8.80	8.80
WEIGHTS (LBS)
Max Ramp	23,650	23,650	24,800
Max Takeoff	23,500	23,500	24,650
Zero Fuel	16,000	16,000	17,000
Basic Operating	12,870	13,225	13,700
Max Landing	20,700	20,700	20,700
FUEL CAPACITY
Standard lbs/gal	9,365  /  1,398	9,365  /  1,398	9,365  /  1,398
Optional lbs/gal	0  /  0	0  /  0	0  /  0
TAKEOFF PERFORMANCE
SL ISA BFL (ft)	5,250	5,250	5,395
5000+20C BFL (ft)	7,400	9,360	8,700
LANDING PERFORMANCE
FAA Field Length	2,720	2,720	2,920
RANGE (NAUTICAL MILES)
Max Range (NBAA IFR)	2,643	2,727	2,949
CLIMB (SL ISA MTOW)
Normal (fpm)	3,700	3,700	3,800
Engine Out (fpm)	1,010	1,010	0
SPEEDS (KNOTS)
Vs (Clean)	114	114	0
Vso (Landing)	97	97	0
Normal Cruise TAS	448	448	456
Vmo (Max Operating) IAS	363	363	353