B738 NG Limitations

1. Maximum Operating Altitude 41,000'
2. Maximum Takeoff and Landing Altitude 8,400'
3. Maximum Taxi Weight 174,700 / 79,244

Maximum Takeoff Weight 174,200 / 79,017

Maximum Landing Weight 144,000 / 65,317

Maximum Zero Fuel Weight 136,000 / 61,688

1. Maximum Takeoff and Landing Tailwind Component 15 knots
2. Maximum Takeoff and Landing Crosswind Component 20 knots
3. Maximum Takeoff and Landing Headwind Component 25 knots
4. APU bleed: max alt 17,000 ' (ground)

APU electrical load: max alt 41,000' (ground)

APU bleed + electrical load: max alt 15,000 ' (ground)

APU bleed + electrical load: max alt 10,000 ' (inflight)

1. Max flap extension altitude is 20,000 '
2. Do not deploy the speedbrakes in flight at radio altitudes less than 1,000'
3. Lateral imbalance between main tanks 1 and 2 must be scheduled to be zero. Random

fuel imbalance must not exceed 1000 lbs / 453 kgs.

1. Main tanks 1 and 2 must be scheduled to be full if center tank fuel is loaded more than

1000 lbs / 453 kgs.

12. The Minimum Use Height (MUH) for single channel autopilot operation is defined as 158 feet AGL.

The autopilot must be disengaged before the airplane descends more than 50 feet below the minimum descent altitude (MDA).

13. The use of VNAV or LNAV with the altimeters referenced to QFE is prohibited.

14. CG should be between 13% and 33%.

Дата добавления: 2015-10-21