SBR1

ROCKWELL NA-265 Sabre 60

Aircraft
Name
NA-265 Sabre 60
Manufacturer
Body
Narrow
Wing
Fixed Wing
Position
Low wing
Tail
Regular tail, low set
WTC
M
APC
C
Type Code
L2J
Engine
Jet
Engine Count
Multi
Position
Both sides of rear fuselage
Landing gear
Tricycle retractable
Manufacturered as
NORTH AMERICAN T-39 Sabreliner
NORTH AMERICAN ROCKWELL Sabre 40
NORTH AMERICAN NA-265 Sabreliner 60
NORTH AMERICAN ROCKWELL NA-265 Sabreliner 60
NORTH AMERICAN Tp86 Sabreliner
NORTH AMERICAN ROCKWELL NA-265 Sabreliner 40
NORTH AMERICAN NA-265 Sabreliner 50
NORTH AMERICAN ROCKWELL CT-39 Sabreliner
NORTH AMERICAN NA-265 Sabreliner 40
NORTH AMERICAN ROCKWELL T-39 Sabreliner
NORTH AMERICAN NT-39 Sabreliner
ROCKWELL Sabre 65
NORTH AMERICAN CT-39 Sabreliner
ROCKWELL Sabre 60
NORTH AMERICAN Sabreliner
ROCKWELL Sabre 40
NORTH AMERICAN Sabreliner 40
ROCKWELL NA-265 Sabre 65
NORTH AMERICAN Sabreliner 50
ROCKWELL NA-265 Sabre 60
NORTH AMERICAN Sabreliner 60
ROCKWELL NA-265 Sabre 40
NORTH AMERICAN ROCKWELL Sabreliner 40
NORTH AMERICAN ROCKWELL Tp86 Sabreliner
NORTH AMERICAN ROCKWELL Sabreliner 60
NORTH AMERICAN ROCKWELL Sabreliner
NORTH AMERICAN ROCKWELL Sabre 60

SBR1

Executive corporate jet. Stretched (97 cm) NA-265 Sabre 40 for 12 passengers with two JT12-A-8 engines, five cabins each side, 130 built.

Technical Data
Wing span (metric)
13.61 m
Length (metric)
15.27 m
Height (metric)
4.88 m
Powerplant

2 x Pratt & Whitney JT12-A-8 turbojet.

Engine Model(s)
Pratt & Whitney JT12
Indicative Performance Data
Take-Off
V2
n/a
Distance
1600 m
MTOW
9100 kg
Initial Climb (to 5000 ft)
IAS
n/a
ROC
4500 ft/min
Initial Climb (to FL150)
IAS
n/a
ROC
n/a
Initial Climb (to FL240)
IAS
n/a
ROC
n/a
MACH Climb
MACH
n/a
ROC
n/a
Cruise
TAS
400 kts
MACH
n/a
Ceiling
450
Range
1710 NM
Initial Descent (to FL240)
MACH
n/a
ROD
n/a
Descent (to FL100)
IAS
n/a
ROD
n/a
Descent (FL100 & below)
IAS
n/a
MCS
n/a
ROD
n/a
Approach
Vapp (IAS)
n/a
Distance
760 m

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