CAL\UAL B737 limitations Flashcards
Rev #60 (107 cards)
0
Q
Flaps Down G-Loading
A
+2.0 to 0.0g
1
Q
Flaps Up G-Loading
A
+2.5g to -1.0g
2
Q
Max Altitude NG
A
41,000ft
3
Q
Max Takeoff/Landing Altitude-NG
A
10,000ft
4
Q
Max Operating Latitude-NG
A
82N to 82S (do not align above 78 deg 15 mins)
5
Q
Runway Slope
A
+ or - 2%
6
Q
Max unrestricted takeoff/landing tailwind
A
15
7
Q
Max restricted takeoff/landing tailwind 7,8,9
A
15
8
Q
MMO
A
.82
9
Q
Landing gear placard speeds. Retract, Extend, Extended
A
Retract: 235 knots
Extend: 270 knots/.82m
Extended: 320 knots/ .82m
10
Q
Climb & Descent Severe Turb Speeds-NG
A
280 knots / .76 Mach
11
Q
Cruise Severe Turb Speed
A
TURB N1 setting from cruise page
12
Q
-700 flap speeds
A
1 to 5 - 250 10-210 15-195 25-170 30-165 40-156
13
Q
800 flap speeds
A
1 to 5 - 250 10-210 15-200 25-190 30-175 40-162
14
Q
900 flap speeds
A
1 to 5 - 250 10-205 15-200 25-195 30-180 40-170
15
Q
NG Takeoff Tailwinds up to 15 knots?
A
Valid Accuload Runway clear and dry Antiskid and Thrust reversers operational No Reduced Auto spoilers Used
16
Q
Recommended Takeoff Crosswind Component
A
Dry…..34
Wet….25
Standing Water/ Slush….15
Snow - No Melting……25
17
Q
Recommended Landing Crosswind Component
A
Dry….40
Wet…40
Standing Water/ Slush…20
Snow - No Melting….35
18
Q
-700 Weight Limits
A
Taxi….155,000
Takeoff….154,500
Landing….129,200
ZFW….121,700
19
Q
-800 Weight Limits
A
Taxi….174,700
Takeoff….174,200
Landing…144,000/146,300
ZFW….136,000/138,300
20
Q
-900 Weight Limits
A
Taxi….174,700
Takeoff….174,200
Landing….147,300
ZFW….140,690
21
Q
-900 ER Weight Limits
A
Taxi….188,200
Takeoff….187,700
Landing….157,300
ZFW….149,300
22
Q
Max Differential Pressure -NG
A
9.10 PSI
23
Q
Max Differential Pressure for t/o & landing
A
.125 psi
24
Operating Differential Pressure above 37000
8.35 ± .1 psi
25
Operating Differential Pressure 28,000 to 37,000
7.8 ± .1 psi
26
Operating Differential Pressure below 28,000
7.45 ± .1 psi
27
Minimum duct pressure for two pack operation from one bleed
20 - 25 psi
28
Minimum Altitude For Autopilot Engagement
800 AGL
29
Max Winds for Autoland
Headwind....25 Knots
Crosswind....15 Knots
Tailwind....10 Knots
30
Max Winds for Autoland-Headwind
25
31
Max Winds for Autoland-crosswind
15
32
Max Winds for Autoland-Tailwind on 7,8,9er, flaps 30 and 40
10
33
Max Winds for Autoland-Tailwind on 900 (401-412) flaps 30
10
34
Max Winds for Autoland-900 (401-412) flaps 30, field elevation 4000 or less
10
35
Max Winds for Autoland-900 (401-412) flaps 30, field elevation 4001-6000
5
36
Max Winds for Autoland-900 (401-412) flaps 30, field elevation 6001 and above
0
37
Do not Use Autopilot Below___at Airports Above____.
100 feet RA.....8,400 feet PA.
38
Max Altitude for Autoland
8,400 feet PA
39
Autoland with Flaps____ and____
30 or 40....both engines operating
40
Max and Min Glideslope for Autoland___and___.
3.25 and 2.5
41
APU Bleed and Electrical Max Altitude
10,000 Feet
42
APU Bleed Max Altitude
17,000 Feet
43
APU Electrical Load Max Altitude-NG
41,000 Feet
44
APU Start cooling requirements-NG
ground and air: 15 minute cooling after 3rd attempt
45
APU Shutdown-wait a minimum of --- before switching battery off-NG
120 Seconds
46
NG single engine generator load
75kva-215 amps (ground)
47
Minimum battery voltage for APU start
23 volts
48
Ice and Rain Takeoff prohibited when?
Moderate / Heavy Freezing Rain or Hail
49
Ignition must be on for:
Takeoff, Landing, Engine Anti-Ice Operation, Heavy Rain
50
Oil pressure for takeoff
must be in normal range
51
NG min oil press
13 psi
52
NG Oil Temp (max)
155C
53
NG Oil Temp (max continuous)
140C
54
NG Oil Temp (max allowable)
140C-155C (45 min)
55
NG Max EGT (Takeoff 5 min)
950 C
56
NG Max EGT (Max Continuous)
925 C
57
NG Max EGT (Start)
725C
58
Starter duty cycle NG___?
2 minutes with 10 second cooling.
Extended motoring-15 min for first 2 motoring with 2 min. between each attempt. for third and more motoring a minimum of 2 min needed for each attempt
59
Reduced thrust takeoff prohibited
with anti-skid inop
60
Reverse thrust limited to____?
ground only
61
Successful starts not assured above?
FL 250
62
NG Max N1
104.0%
63
NG Max N2
105.0%
64
NG EEC- both EEC's must
Must be ON or ALT for takeoff
65
EEC or PMC "ALT" or "OFF" No____ takeoffs
reduced power takeoffs
66
Minimum duct pressure for start
30 psi @ sea level decreasing .5 psi per 1000ft ASL
67
Cargo Fire suppression activation
Must land at nearest suitable airport within 60 minutes
68
Engine fire extinguisher bottle pressure
800 psi @ 70F
69
Max flap extension altitude
20,000 feet
70
NG Holding limit...
holding in icing conditions with flaps extendended is prohibited
71
Speed brakes in flight
do not deploy below 1000 RA
72
Alternate flaps-when extending/retracting wait----before moving switch to a new position
15 seconds
73
alternate flaps-after a complete extend/retract cycle, allow---cooling before attempting another one
5 minutes
74
Alternate flaps- max speed to extend
230
75
Speed brake should not be deployed with flaps more then-------
15
76
Mach trim fail(both channels) max speed NG
280 or .82
77
RVSM max difference between CA & FO
200 feet
78
Recommended Takeoff Crosswind Component Split Scimitar Winglet
Dry-33
| Wet-25
79
RVSM on ground 0-5000ft max difference between CA & FO NG
50 ft
80
RVSM on ground 10,000ft max difference between CA & FO NG
60
81
RVSM on ground max difference between CA or FO & field elevation NG & 500
75
82
Max fuel tank temp
49C
83
Fuel- minimum jet A temp
-37
84
Fuel- minimum jet A-1 temp
-44
85
Jet A fuel freeze point ____?
-40C
86
Min fuel tank temp for takeoff
-43 C
87
Fuel- max wing capacity NG
8630 lbs.
88
Fuel- max center tank capacity NG
28803 lbs
89
Lateral fuel imbalance must not exceed ____?
1000 pounds
90
Fuel crossfeed valve must be ____?
closed for takeoff and landing
91
Fuel pump circuit breaker ____?
do not reset
92
Center tank fuel pumps-Takeoff- if center tank fuel is less then---, both center pumps got to be -----
5000, off
93
Center tank fuel pumps-initial climb- if center tanks are less then--- and pitch reduced to accelerate to 250 turn--- center pump----
5000,right,on
94
Center tank fuel pumps-climb, cruise, descent- if center tank is more then--- turn--- pump----
5000, left, off
95
Fuel config light come on when?
more then 1600 lbs of fuel in center tanks, and both center fuel pumps are off
96
Minimum fuel for stationary ground operations of electric hydraulic pumps ____?
1,676 pounds in each wing tank
97
Hydraulic- max quantity NG
105%
98
Hydraulic- minimum quantity NG
76%
99
Max Tire ground Speed
195 Knots
100
Arming RTO is required ____?
on all takeoffs, if operable
101
700 Va speeds @ SL, 10,000, 20,000 30,000 32,000
```
SL-250
10,000-262
20,000-276
30,000-294
32,000-298/.82
```
102
800/900 Va speeds @ SL, 10,000, 20,000 30,000 32,000
```
SL-260
10,000-272
20,000-287
30,000-306
30,600-307/.82
```
103
900ER Va speeds @ SL, 10,000, 20,000 30,000 32,000
```
SL-287
10,000-296
20,000-306
25,000-314
28,500-321/.82
```
104
Minimum Ground time after landing-steel brakes, Carbon brakes
700/800/900 Steel brakes - 67 min
| 900/900ER - Carbon Brakes - 48 min
105
Recommended Landing Crosswind Component Split Scimitar Winglet
Dry-37
| Wet-37
106
Max Winds for Autoland 900 (401-412) flaps 30
4000-10 knots
4001 to 6000-5 knots
6001- 0 knots
