Dash-1 Chap 2 Numbers to Know

Question 1

Normally data transfer from PCMICIA card will take

Answer 1

< 1 min.

Question 2

Lower stop of cabin altitude controller

Answer 2

-7000 feet

Question 3

After power application check EGT caution lights within

Answer 3

5 sec.

Question 4

The APU fire extinguisher may discharge if the FIRE/DSBLD switch is pressed with a battery reading of

Answer 4

21 volts

Question 5

WXR-700X color radar warm up times above 0C

Answer 5

2 min.

Question 6

WXR-700X color radar warm up times between -15 C and 0C

Answer 6

5 min.

Question 7

WXR-700X color radar warm up times below -15C

Answer 7

30 min

Question 8

During oxygen check, breathe normally for a minimum of

Answer 8

3 cycles

Question 9

Right hydraulic system quantity

Answer 9

4.0 – 4.5 gal.

Question 10

Left system hydraulic quantity with gear doors open

Answer 10

3.75 – 4.25 gal.

Question 11

Left system hydraulic quantity with gear doors closed

Answer 11

4.0 – 4.5 gal.

Question 12

During antiskid test when switch is released, brake indicators should continue to show REL for

Answer 12

≈1 sec.

Question 13

Oil temperature selector test goes to near full scale then decreases to

Answer 13

175C – 195C

Question 14

FSAS I-BIT takes

Answer 14

≈18 sec.

Question 15

Normal hydraulic pressure

Answer 15

2400 – 3050 psi

Question 16

Before control and trim check stab trim should be set to

Answer 16

6 – 11 units nose up

Question 17

Aileron control wheel movement may be prevented in one direction with a tailwind of

Answer 17

12 knots

Question 18

The control column may be locked against either forward or aft movement with a tailwind of

Answer 18

17 knots

Question 19

During control and trim check rotate Stab trim control wheel ___ turns in each direction

Answer 19

5

Question 20

Before checking stab trim control switches ensure the electric stab trim motor has not run for

Answer 20

30 sec.

Question 21

With initial activation of the left half of the pilot’s trim switch a slight trim wheel oscillation or movement is allowed up to

Answer 21

¼ turn

Question 22

When checking the right half of the pilot and copilot’s stab trim switch ensure the trim wheel does not move more than

Answer 22

½ turn

Question 23

During ground check ____ trim units will move rudder trim tab full throw

Answer 23

5

Question 24

During EFAS and SYD test set SYD switch to test and then on within

Answer 24

3 sec.

Question 25

Check that ENGAGE SYSTEM, EFAS FAILED, and ASM THRUST cautionlights come on then go out within

Answer 25

60 sec.

Question 26

Check that DISENG caution light comes on then goes out within

Answer 26

35 sec.

Question 27

Ensure each altimeter indicates within ____ of a known elevation

Answer 27

75’

Question 28

Ensure each altimeter indicates within ____ of each other

Answer 28

30’

Question 29

Ensure difference of Pilot’s altimeter between NORM and STBY is (with FMS air data source set to NORM or ADC1)

Answer 29

20’

Question 30

Pilot’s altimeter diff. between NORM & STBY for ADC2

Answer 30

80’

Question 31

Copilot’s altimeter difference regardless of FMS Data source

Answer 31

80’

Question 32

During a Radio Altimeter check the RA counts up to approximately

Answer 32

100’

Question 33

VOR check should be within

Answer 33

±4 degrees

Question 34

The DME during a TACAN check should read

Answer 34

0 – 0.5

Question 35

After break-lock the TACAN course should read

Answer 35

180 degrees ±3

Question 36

Autopilot warm-up

Answer 36

≈1 min.

Question 37

The Autopilot test takes

Answer 37

≈50 – 100 sec.

Question 38

During autopilot test you should receive a VALID or INVALID indication

Answer 38

20 sec.

Question 39

The TCAS test duration is approximately

Answer 39

12 sec.

Question 40

For takeoff & landing open all tank to engine manifold valves if the fuel in any main tank is below

Answer 40

10,500#

Question 41

Open the line valve for all takeoffs when the gross weight is

Answer 41

> 200,000#

Question 42

Close the line valve for all takeoffs when the gross weight is

Answer 42

< 200,000#

Question 43

APU start accumulators are recharged to

Answer 43

3000 ±350 psi

Question 44

The APU surge damper accumulators are charged to

Answer 44

1600 psi

Question 45

RCR inputs of 9 (wet) or 4 (icy, snow, slush) are automatically converted by the FMAC for calculation of VMCG & max x-wind to _____

Answer 45

16 or 5

Question 46

If hydraulic warm-up is selected what hydraulic temp is used by the box

Answer 46

-7C

Question 47

Delta height has a maximum of

Answer 47

999’

Question 48

To load 50 selected waypoints & their attributes in the FSAS may take up to

Answer 48

8 min.

Question 49

Max motoring is defined as less than ___ increase in N2 in ____

Answer 49

1% 5 sec.

Question 50

During engine start initial fuel flow is

Answer 50

300 – 680 pph

Question 51

Fuel flow after ignition is

Answer 51

≈900 pph

Question 52

With a tailwind of ___ knots do not advance throttles to START until N2 RPM is at least ___

Answer 52

20 knots 20%

Question 53

A hot start will occur if the fuel flow exceeds ____ before light off

Answer 53

680 pph

Question 54

After placing throttle to START check for EGT rise within

Answer 54

2 – 3 sec.

Question 55

Abort start if EGT does not rise within

Answer 55

10 sec.

Question 56

If engine fails to start after 2nd try, motor with throttle in cutoff for

Answer 56

2 min.

Question 57

During engine start move throttle to idle at

Answer 57

50% N2

Question 58

Prior to advancing to high thrust setting allow engine to operate at idle for

Answer 58

2 min.

Question 59

Stabilized ground idle is

Answer 59

54 – 62% N2

Question 60

To avoid APU bypassing initiate start on the next engine at

Answer 60

42% N2

Question 61

Automatic closure of the start valves occurs between

Answer 61

43 – 45% N2

Question 62

Automatic closure of the start valve takes

Answer 62

3 – 9 sec.

Question 63

With starter valve open light on damage to starter can occur if engine RPM exceeds

Answer 63

63% N2

Question 64

Set starter valves to ignition for temperatures at and below

Answer 64

0C (32F)

Question 65

At idle thrust danger area around engine is __ front & side & __ to the back.

Answer 65

25’ 5’

Question 66

At TRT thee danger area around engine is __ front & side & __ to the back.

Answer 66

50’ 6’

Question 67

If a blast fence is not available clear the area behind the airplane to a minimum distance of

Answer 67

900’

Question 68

When only battery power is used for engine start all engine oil pressure & fuel flow gages are inoperative until a generator is online with

Answer 68

28V AC

Question 69

Engine oil low pressure warning switches actuate at

Answer 69

12.5 (+0.5, -1.5)psi

Question 70

Hyd. & flight control warm-up procedures should be used for temps below

Answer 70

20F (-6C)

Question 71

For EFAS test advance outboard throttle to

Answer 71

≈31% N1

Question 72

Engines will accelerate to flight idle if battery power switch is allowed to remain off for more than

Answer 72

2 sec.

Question 73

To clear any water and check valve operation turn on engine anti-ice for

Answer 73

15 sec.

Question 74

In icing greater than light to prevent damage to acoustical panels initiate engine ice shedding procedures every

Answer 74

30 min.

Question 75

Engine ice shedding procedures say to accelerate engines to

Answer 75

35% N1

Question 76

If no problems are evident slowly accelerate engines to

Answer 76

70% N1 for 30 sec.

Question 77

Turn on anti-ice if there is standing water, fog or visible moisture with temp

Answer 77

10C (50F)

Question 78

The minimum fuel required in CWT to check override pumps is

Answer 78

3500#

Question 79

During ADC1&2 test the altimeter readout will slew to

Answer 79

5000’ (±10)

Question 80

During ADC1&2 test the airspeed readout will slew to

Answer 80

260 KIAS (±1)

Question 81

The recommended rate to advance throttles from flight idle to TRT is

Answer 81

3 – 5 sec.

Question 82

Flap indicators should indicate all main flaps within

Answer 82

2 degrees

Question 83

To check rudder power, full left to full right rudder pedal travel should be accomplished in approximately

Answer 83

1 sec.

Question 84

Rudder power will drop momentarily but should return within

Answer 84

3 sec.

Question 85

A takeoff is considered critical if CFL +_____ exceeds runway available or the 3 engine climb gradient is less than _____

Answer 85

2000’ 4%

Question 86

Re-compute takeoff data if the runway temperature changes

Answer 86

±5C

Question 87

Re-compute takeoff data if the pressure altitude changes

Answer 87

±250’

Question 88

Re-compute takeoff data if the gross weight changes

Answer 88

2500#

Question 89

Re-compute takeoff data if the % MAC changes

Answer 89

1.0%

Question 90

For a critical takeoff re-compute the data if the actual temp vs. temp used varies more than

Answer 90

2C

Question 91

For better weather radar returns during takeoff set tilt to

Answer 91

5 degrees

Question 92

When AUTO is depressed the radar automatically scans manual tilt setting

Answer 92

±4

Question 93

Skin Paint is not available with the PWS switch in auto below

Answer 93

2300’ AGL

Question 94

If freezing precipitation is present a final physical check of the surfaces should be made within ___ of takeoff

Answer 94

5 min.

Question 95

From the control cabin it is difficult to see a coating of clear ice on the wings of as much as

Answer 95

¼”

Question 96

In either ACCL or MAX the command bars display initial climb commands of

Answer 96

8. 5 for 20 flaps | 8. 0 for 30 flaps

Question 97

Call “pickle” at

Answer 97

VROT -10 knots

Question 98

Abort the takeoff if the engines don’t reach charted N1 between

Answer 98

40 and 80 knots