LIMITATIONS Flashcards
1
Q
- Runway Slope
A
+/- 2%
2
Q
- Max Tailwind / Crosswind
A
15 / 36 (max demonstrated x-wind w/winglets = 33 kts)
3
Q
- Max Speed
A
320 / .82
4
Q
- Turbulent Speed
A
280 / .78
5
Q
- Max Altitude
A
41,000 ft
6
Q
- Max Takeoff & Landing Altitude
A
8,400 ft
7
Q
- Max Ramp Weight
A
174,700 lbs (IGW) 156,000 lbs (STD)
8
Q
- Max Takeoff Weight (MTOW)
A
174,200 lbs (IGW) 155,500 lbs (STD)
9
Q
- Max Landing Weight (MLW)
A
144,000 lbs
10
Q
- Max Zero Fuel Weight (MZFW)
A
136,000 lbs
11
Q
- Max Cabin Differential Pressure
A
9.1 PSI
12
Q
- APU Bleed and Electrical
A
10,000 ft*
13
Q
- APU Bleed Only
A
17,000 ft
14
Q
- APU Electrical Only
A
41,000 ft
15
Q
- Min Altitude for A/P ON after Takeoff
A
400 ft
16
Q
- Min Altitude for A/P ON During Non-Pre App
A
50 ft below minimums
17
Q
- Maximum Engine Limits
A
Redline
18
Q
- Minimum Engine Limits
A
Redline
19
Q
- Caution Limits
A
Amber
20
Q
- Engine Ignition Must be ON for …
A
Takeoff, Landing, Heavy Rain, Anti-Ice
21
Q
- Max Flap Extension Altitude
A
20,000 ft
22
Q
- Min Altitude For Speed Brake Use
A
1,000 ft
23
Q
- Alternate Flap Duty Cycle (down & up)
A
Flaps 1 thru 15 = 5 min; Flaps > 15 = 25 mins
24
Q
- Fuel System Minimum Temperatures
A
- 43 degrees C or fuel freeze plus 3 degrees C
25
Q
- Fuel System Maximum Temperatures
A
+ 49 degrees C
26
Q
- Fuel IMBAL For Taxi / Takeoff / Landing
A
1,000lbs
27
Q
- Icing Condition Temperature
A
10C / 50F
28
Q
- ADIRU Alignment Must Not be Attempted at Latitudes Greater than
A
78 degrees 15 minutes
*Under Captain’s Emergency Authority, APU has demonstrated the capability to supply both bleed air and electrical power up to 20,000 feet altitude.
