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                 

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