Chapter 1 Flashcards

(55 cards)

1
Q

Max land Weight

A

164000

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2
Q

Max Zero FUEL Weight
(No Fuel]

A

155000

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3
Q

Max T/O Weight

A

196800

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4
Q

Yaw damper INOP : 1 or both
Max Speed

A

270

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5
Q

Max Flaps extension speeds

A

2 - 245
5 - 230
15 - 205
20 - 195
25 - 185
30- 185

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6
Q

Max leading edge devices extension speed

A

245

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7
Q

Landing gear retraction
V lo

A

200

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8
Q

Land gear extension speed
V le

A

270 / .83

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9
Q

Landing gear EXTENDED
(Main gear doors closed)

A

320 / .83

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10
Q

Max Tire Speed

A

195

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11
Q

Turbulent air penetration
Below 15000
Above 15000

A

Below - 250
Above - 280/ .80

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12
Q

Max operating Speed Vmo

A

SL - 350

27700 - 345 /.87

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13
Q

Max crosswind T/0 and Land

A

29 kts

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14
Q

Max Tailwind component

A

10 kts

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15
Q

Main cargo door wind limits

A

40 kts

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16
Q

Max runway slope

A

+/- 2%

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17
Q

Max water or slush on wet runway

A

1/2 inch

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18
Q

Max dry snow on runway

A

4 inch

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19
Q

Chine on tires must be on

A

Nose wheel

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20
Q

Max T/O and Landing altitudes

A

9000
8300

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21
Q

Minimum Altitude for Auto-Pilot

A

1020 AGL

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22
Q

Auto pilot
Non-precision App

A

50 feet below MDA but not less than 1100 AGL

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23
Q

Auto pilot
Precision App

24
Q

RVSM
290 TO 410
Max alt deviation

25
Max gen drive oil IN temp Max rise Max combined
120 deg C 20 130 deg C
26
Gen Load Limit
3 Gen. - 102.5kw 2 Gen - 54 kw Any isolated Gen- 36kw Max differential - 7kw
27
APU LIMITATION Ground Gen Limit
APU 165 amps Max external load - 200 amps
28
Generator Voltage & Frequency
115 V +/- 5 volts 400 hz +/- 8 hz
29
Transformer Rectifier
Minimum voltage-24 volts Max load no cooling - 50 amps Max load w/cooling- 65 amps
30
Airplane battery
Min. Voltage- 22 volts
31
Altimeter difference (Between primary and back up)
+/- 75 FEET OF EACH OTHER
32
Altimeter in RVSM
Pilot and Co-Pilot altimeter must be within 200 feet of each other
33
Equipment requirement for RVSM
#1 & 2 Altimeter 1 altitude reporting Transponder 2 digital air data computers 1 altitude alert system 1 auto pilot with altitude Hold capability
34
Can you reset a tripped fuel circuit breaker?
No
35
The fuel weight Difference in tanks 1 & 3 is
No more than 1000lbs
36
For T/O; enroute; and Landing the fuel quantity in Tank #1. And 3. Shall not exceed the quantity in Tank 2 by
2000lbs
37
Maximum Tank fuel temp Minimum Tank fuel temp
49 deg C -36 deg C
38
Do not operate speed brakes in flight when...
Flaps are extended
39
Minimum Hydraulic fluid system A
3 gallons
40
Minimum Hydraulic fluid System B Standby system
Full
41
Maximum Flap Extension altitude
20000 ft
42
Window heat limitation
Must be ON 10 minutes prior to T/O
43
Flight controls must be verified by 2 Crew
Thrust levers Start levers Engine Fire Have Handles Fuel shut off valves Hydraulic A shutoff switches Flight controls switches CSD disconnect switches
44
Max speed with Window Heat Inop
250
45
Engine AntiIce must be on when
Operating in icing conditions
46
Define icing conditions
When moisture is present and outside Temperature is 10 deg or lower
47
What is moisture
Ceiling 400 ft or less When standing water slush ice snow is in taxi way runway Vis less than 1 mile and there are clouds fog mist rain snow etc
48
How do we determine ice accumulation
Accumulating in wiper bolt On windows Or window frames
49
Wing anti ice must be turned off until
400 ft AGL
50
Thrust requirements for using anti ice
-7 deg or above. 55% N1 -7 deg or below or moderate to severe icing. 70%
51
If only 1 outboard engine applying bleed air for wing anti-ice N1. ?
75% N1
52
Maximum time for taxi turn off lights or inboard lights On the ground is
5 min
53
Anti-skid Inop
Take off on contaminated runways is prohibited
54
Minimum oxygen pressure for dispatch
1500 psi at 70F
55
On ground System B Hyd pump should Not be operated with
Least than 1340lbs of fuel in Tank #1