Brainscape's Knowledge GenomeTM

Browse over 1 million classes created by top students, professors, publishers, and experts.


See full index

unnamed > E8 General Knowledge > Flashcards

E8 General Knowledge Flashcards

1
Q

Re-compute applicable takeoff data if change occurs greater than…

___ Pressure Altitude

A

+/-500 feet

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
2
Q

Re-compute applicable takeoff data if change occurs greater than…

___ Gross Weight

A

+/-5000 pounds

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
3
Q

Re-compute applicable takeoff data if change occurs greater than…

___ CG

A

+/-.5%

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
4
Q

CFL is increased/decreased approximately ___ by increases of 1 C, +/-100’ pressure altitude, or +/-1,000 pounds gross weight

A

+/-100 ft

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
5
Q

With any increase in temperature, obstacle clearance calculations will be re-accomplished if obstacle clearance is ___ feet or less

A

100 feet

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
6
Q

Increase rotation speed ___ knots for every ___ knots of tailwind

A

4 knots; 10 knots

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
7
Q

When increasing rotation, takeoff and climbout speeds for gusts on takeoff, the maximum allowable increase is ___ knots

A

10 knots

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
8
Q

When correcting approach speed for headwind and gusts, the total wind correction must not exceed ___ knots

A

20 knots

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
9
Q

A/R airspeed from level off until 2 NM

A

M .76 or 310 KIAS, whichever is lower

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
10
Q

A/R airspeed at 1 NM

A

M .72 or 290 KIAS, whichever is lower

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
11
Q

A/R airspeed at 1/2 NM

A

M .69 or 285 KIAS, whichever is lower

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
12
Q

A/R airspeed in contact

A

M .66 or 275 KIAS whichever is lower

Unless you want to remain in contact - in that case, fly as fast as the tanker

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
13
Q

KC-135 inner limit

A

6 feet

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
14
Q

KC-135 center extension

A

12 feet

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
15
Q

KC-135 outer extension limit

A

18 feet

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
16
Q

KC-135 left/right limits

A

10 degrees

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
17
Q

KC-135 upper vertical limit

A

20 degrees

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
18
Q

KC-135 vertical center

A

30 degrees

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
19
Q

KC-135 lower vertical limit

A

40 degrees

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
20
Q

KC-10 inner extension limit

A

6 feet

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
21
Q

KC-10 extension center

A

13 feet

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
22
Q

KC-10 outer extension limit

A

21 feet

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
23
Q

KC-10 left/right limits

A

19 degrees

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
24
Q

KC-10 upper vertical limit

A

20 degrees

25
Q

KC-10 vertical center

A

Approximately 30 degrees

26
Q

KC-10 lower vertical limit

A

40 degrees

27
Q

A maximum of ___ KC-10 aerial refueling transfer pumps should be used during refueling operation to prevent over pressurization of refueling system

A

4

28
Q

Flap indicators may indicate ___ degrees of actual flap extension

A

+/-3 degrees

29
Q

Flaps will not be extended above _____

A

20,000 feet MSL

30
Q

Leading edge flaps extend and retract as the _____ trailing edge flaps pass through the _____ degree position

A

Inboard; 6 +/-3 degree

31
Q

If the bell rings before ___ or ___ is indicated, the point at which the bell begins to ring is limiting

A

Vmo or Mmo

32
Q

The airplane battery is a ___ volt, ___ amp-hour, lead acid unit located in the _____ section

A

24 volt; 31 amp-hour; right lower nose

33
Q

Rudder pressure should be approximately ___ PSI when rudder is set to the high range and ___ PSI when rudder is in low range

A

3000 PSI; 2250 PSI

34
Q

The altimeter must check within ___ feet of a known location (RESET/STBY mode)

A

75 feet

35
Q

Allowable tolerance between both RMDIs

A

2.5 degrees

36
Q

Allowable difference between the RMDI and an HSI repeater )if on the same compass system)

A

1 degree

37
Q

During the ADI test, the indicator should display ___ degrees of right bank, and ___ degrees of nose-up pitch

A

20 degrees; 10 degrees

38
Q

Oxygen pressure should be ____ PSI

A

290 to 430 PSI

39
Q

The LOX converter stores ___ liters of LOX at a nominal pressure of ___ PSI

A

75 liters; 300 PSI

40
Q

Oxygen Level Low light comes on at or below ___ liters or when system pressure is below ___ PSI

A

7.5 liters; 42 PSI

41
Q

The utility hydraulic reservoir is located in the ___ main wheel well. All airplanes have an extended filler neck and an expansion tank which has a capacity of ___ gallons

A

Left; 6.0 gallons

42
Q

Hydraulic fluid above the ___ gallon level replenishes the auxiliary system reservoirs

A

3.2 gallon

43
Q

RUDDER BOOST LOW PRESS light indicates pressure in supply line to the rudder power unit is below approximately ___ PSI. It is armed with _____ flaps down ___ degrees or greater and rudder draulic pressure in the high range

A

2500 PSI; inboard; 2 degrees

44
Q

YAW DAMP DISENG light will come on when rudder pressure drops below ___ PSI or yaw damper _____ power is lost or when certain circuit _____ occur within the yaw damper circuits

A

1200 PSI; electric; faults

45
Q

Hydraulic pump LOW PRESS lights come on when pressure decreases to approximately ___ PSI. The lights go out when pressure increases to approximately ___ PSI.

A

1100 PSI; 1200 PSI

46
Q

When fuel temperature is ___ C or below, turn on fuel heat for ___ minute(s) prior to takeoff

A

0 C; 1 minute

47
Q

If engines have been operating at idle thrust for ___ minutes or more, fuel heaters may be operated with engines at idle. Otherwise, fuel flow should be increased to ___ PPH before the heaters are turned on and maintain at least ___ PPH for 2 minutes after the heaters are turned off.

A

5 minutes; 1500 PPH; 1500 PPH

48
Q

Turn fuel heaters to ___ for takeoff

A

Off

49
Q

Turn on engine anti-icing during ground operations whenever icing conditions exist for takeoff (outside air temperature ___ C or lower and visible moisture present)

A

10 C

50
Q

If the nose cowl anti-ice valve does not open in ___ second(s) at idle thrust, increase thrust to ___ N1

A

1 second; 40% N1

51
Q

Do not exceed ___ N1 on the ground with engine anti-ice operating. If a valve does not open within ___ second(s) at ___ N1, valve has failed

A

40% N1; 1 second; 40% N1

52
Q

Do not use wing anti-ice for takeoff or until reaching ___ feet AGL

A

100 feet AGL

53
Q

OIL LOW PRESS caution light will come on at ___ PSI or ___ PSID. It will go out at ___ PSI on increasing pressure. Light should go off within ___ second(s) after engine reaches stabilized idle

A

32 +/-2 PSI; 50 PSID; 36 PSI; 30 seconds

54
Q

Fuel flow at light-off above ___ pph indicates an impending hot start

A

1400 pph

55
Q

Normal fuel flow at light off is less than ___ pph

A

100 pph

56
Q

Fuel flow peaks at _____ pph during acceleration and stabilizes at ___ pph at idle

A

1600-1800 pph; 1100 pph

57
Q

A rise in EGT should occur within ___ second(s) after start lever is advanced

A

20 seconds

58
Q

Re-compute applicable takeoff data if change occurs greater than…

___ Runway Temp

A

+/-2 C

unnamed (11 decks)

Brainscape helps you reach your goals faster, through stronger study habits.
© 2024 Bold Learning Solutions. Terms and Conditions