Specifications
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SABRE 40 |
SABRE 60 |
SABRE 75 |
SABRE 75A/80 |
SABRE 65 |
World's First
Twin-Engine Jet
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| SPECIFICATIONS | | | | | |
| Model Designation |
NA265-40 |
NA265-60 |
NA265-70 |
NA265-80 |
NA265-65 |
| Total Manufactured |
137 |
146 |
9 |
72 |
76 |
First &
Last Delivered |
Oct. 1963 -
Sept. 1974 |
July 1967 -
Sept. 1979 |
Jan. 1972 -
Sept. 1973 |
Feb. 1974 -
July 1979 |
Dec. 1979 -
Oct. 1981 |
| ENGINES | | | | | |
| Manufacturer |
Pratt & Whitney |
Pratt & Whitney |
Pratt & Whitney |
General Electric |
Honeywell |
| Type |
JT12A-8 |
JT12A-8 |
JT12A-8 |
CF700-2D-2 |
TFE731-3R-1D |
| Thrust |
3300 Lbs. |
3300 Lbs. |
3300 Lbs. |
4500 Lbs. |
3700 Lbs. |
| MAXIMUM WEIGHTS | | | | | |
| Ramp (Max. Gross) |
19,922 Lbs. |
20,372 Lbs. |
21,200 Lbs. |
23,000 Lbs. |
24,000 Lbs. |
| Take Off |
19,612 Lbs. |
20,172 Lbs. |
21,000 Lbs. |
22,800 Lbs. |
24,000 Lbs. |
| Landing |
17,500 Lbs. |
17,500 Lbs. |
21,000 Lbs. |
22,000 Lbs. |
21,755 Lbs. |
| Zero Fuel |
12,800 Lbs. |
13,800 Lbs. |
14,300 Lbs. |
15,620 Lbs. |
16,250 Lbs. |
| PERFORMANCE | | | | | |
| Range (45 min. Reserve, 6 PAX) |
1650NM
(1900SM) |
1650NM
(1900SM) |
1300NM
(1497SM) |
1678NM
(1932SM) |
2890NM
(3326SM) |
| Max. Cruise Speed |
.80 Mach
459 Knots |
.80 Mach
459 Knots |
.80 Mach
459 Knots |
.80 Mach
459 Knots |
.81 Mach
465 Knots |
| Max. Operating Altitude |
45,000 Ft. |
45,000 Ft. |
45,000 Ft. |
45,000 Ft. |
45,000 Ft. |
| Balanced Field Take Off Distance |
4900 Ft. |
5100 Ft. |
5500 Ft. |
4460 Ft. |
5450 Ft. |
Landing Distance at Max.
Landing Weight |
2950 Ft. |
2935 Ft. |
3750 Ft. |
3450 Ft. |
3345 Ft. |
| Max.Usable Fuel |
1063 Gal./
7122 Lbs. |
1063 Gal./
7122 Lbs. |
1101 Gal./
7377 Lbs. |
1101 Gal./
7377 Lbs. |
1317 Gal./
8824 Lbs. |
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