Max Takeoff Weight
347,451kg
Max Taxi Weight
348,358kg
Max Landing Weight
260,815 kg
Zero Fuel Weight
248,115 Kg
Reverse Thrust Limitations
-No backing up
-Do not deploy in flight
Minimum Fuel Temperature for takeoff
Not less than:
-3* above fuel freezing point
- -40
Minimum fuel temperature for cruise
3* above fuel freezing point
Maximum fuel temperature
49*
Maximum runway slope
+/- 2*
Maximum tailwind component
10kts
Maximum operating altitude
43,100’
Maximum demonstrated crosswind
38kts
Turbulent air penetration speed
- Above 25,000’ less of 280kts/m.82
- Below 25,000’ 270kts
When on Mach maintain 15kts above Va
No HF when
Refueling
No wx radar when
- inside a hangar
- persons are in vicinity of Radom
Max flap altitude
20,000’
Max flap speed
- 1* - 265
- 5* - 245
- 15* - 230
- 20* - 225
- 25* - 200
- 30* - 180
Approved fuels
- Jet-A
- Jet-A1
- JP5
- JP8
No ‘B4’
Minimum altitude for autopilot engagement
200’
Maximum crosswind for auto land
25kts
Maximum crosswind for CAT2/CAT3
15kts
Maximum headwind for auto land
25kts
Minimum and maximum glide slope for autopilot operations
- 2.5
- 3.25
Maximum takeoff and landing elevation
9800’ psi alt
9650’ field elevation
N704GT = 8400’ psi alt
