AIRCRAFT
“Rockwell/NA 265 Sabre - L2J / T39A”
REFERENCE INFORMATION (by Aircraft performance
database)
*****Aircraft
Features*****
Wing position: Low wing
Engine position: Both sides of rear fuselage
Tail configuration: Regular tail, mid set
Landing gear: Tricycle retractable
Wing Span: 13.6 m
Length: 14.3 m
Height: 4.9 m
Power plant: 2 x 20.2 kN GE
CF700-2D-2 turbofans.
Accommodation: Flightcrew of two and up to 10 passengers.
Notes: Executive corporate jet. In service since 1979. Improved, stretched
turbofanpowered development of NA-265-60 (ICAO
Designator: SBR1).
Production
ceased in 1981. Most are still in service. Both models are used by several
military organisations and American Federal services.
Alternative names:
NORTH AMERICAN NA-265
Sabre 75, ROCKWELL
NA-265 Sabre 75/80
NA-265 Sabre 75/80.
*****Total
Flight Simulator aircraft weight with full fuel*****
000,000 lbs - 10.430 kg
VMO - Maximum Operating Speed 450 KIAS
MMO - Maximum Operating Speed Mach 0,78 Mach
Turbulent Air Penetration Speed 000 KIAS/.00 Mach
VLO - Maximum Gear Operating Speed 000 KIAS
VLE - Maximum Landing Gear Extension Speed 000 KIAS/.00 Mach
*****Maximum
Flap Placard Speeds*****
Flaps degr KIAS/pitch°
0 0°
1 10° 200/0°
190/0°
180/1°
2 25° 180/1°
160/3°
140/5°
3 40° 140/4°
130/5°
120/7°
110/10°
Full gear 140/4°
130/5°
120/7°
110/10°
100/12°
STALL limit 100/15°
*****Take-off*****
WTC: L
Distance: 1.300
mt
V2 (IAS): 145
kts
*****Climbing*****
-(to 5000 ft)
IAS: 130
kt
ROC: 4700
ft/min
-(to FL150)
IAS: 290
kt
ROC: 2500
ft/min
-(to FL240)
IAS: 290
kt
ROC: 1500
ft/min
-(mach)
mach: 0,72
ROC: 1.000
ft/min
*****Cruise*****
TAS: 450
kt
MACh: 0,78
Ceiling: FL450
Range: 2400
NM
*****Descent
*****
- (to FL240)
mach: 0,72
ROD: 1.000
ft/min
- (to FL100)
IAS: 290
kt
ROD: 2000
ft/min
*****Approach*****
IAS: 250
kt
MCS: 180
kt
ROD: 1500
ft/min
*****Landing*****
Vht
(IAS): 140 kt
APC: C
Distance: 800
mt