Ch7 Normal Procedures

Question 1

When is the climb checklist performed?

Answer 1

1000 AGL or when entering the VFR pattern

Question 2

If possible, propeller levers should be moved out of reverse above ____ to prevent prop blad erosion.

Answer 2

40 knots

Question 3

The propeller levers must be placed ___ to ensure proper reversing characteristics.

Answer 3

Full forward

Question 4

Max wind beyond which structural damage can occur.

Answer 4

75 knots

Question 5

During start, if N1 stabilizes at less than ___ anticipate a hotter than normal start.

Answer 5

17 percent

Question 6

During start, if N1 stabilizes below ___ consider a GPU start to prevent the possiblity of an overtemp on start.

Answer 6

15 percent

Question 7

Minimum strut extension

Answer 7

Main: 5.56 “
Nose: 3.77”

Question 8

After start generator voltage should be indicated on both buses. If this is not the case, then a ___ may have failed.

Answer 8

Current limiter

Question 9

Time for alignment of the ESIS

Answer 9

2-3 minutes

Question 10

If windshield temperature is greater than ___ windshield antiice may not operate.

Answer 10

32 C

Question 11

Maximum takeoff weight may be restricted by the following:

Answer 11

Accelerate stop within runway length
100 fpm climb with gear down and failed engine
Achieve obstacle clearanace climb gradient

Question 12

2 engine minimum N1’s to maintain pressurization schedule on descent

Answer 12

75%

Question 13

1 engine minimum N1 to maintain pressurization schedule on descent

Answer 13

85%

Question 14

Approach speed

Answer 14

120 KIAS or Vref whichever is greater

Question 15

What is considered a short field landing

Answer 15

Landing on a runway where the usable surface is equal to or less than 150% of the minimum runway required based on the landing distance calculated.

Question 16

Waveoff procedures

Answer 16

Power- max allowable 
Props- full forward
Attitude- sufficient to stop descent rate
Airspeed- as required (Vx or Vy)
Flaps- approach
Establish positive rate of climb
Gear - up
Flaps - up

Question 17

How long must ITT be stabilized prior to engine shutdown

Answer 17

1 minute

Question 18

How many static wicks are required

Answer 18

5, 1 on rudder, 1 on outboard ends of each elevator, 1 on each outboard ends of the ailerons

Question 19

Prop rpm range for overspeed governor check

Answer 19

1830 to 1910 rpm

Question 20

Minimum flight deck oxygen pressure

Answer 20

500 psi

Question 21

Reserve fuel requirements

Answer 21

10 percent or 45 minutes of flight at endurance (10K) whichever is greater

Question 22

How often should a flight fuel log be kept

Answer 22

Every flight a fuel log should be prepared on cross checked with actual fuel consumption for every flight

Question 23

Takeoff power must be applied ___ to obtain the normal takeoff distances from performance charts

Answer 23

Prior to releasing brakes

Question 24

When is cruise checklist performed

Answer 24

Extended cruise operation, not normally below 10,000 ft or in pilot training environment

Question 25

Overspeed governor and rudder boost engine runup procedure

Answer 25

Power levers idle, props full forward
Prop Gov - TEST
Increase power on left engine until prop rpm stabilizes at 1830-1910 rpm then advance power until rudder displaces left.
Power lever idle and repeat on right engine

Question 26

Primary governor engine runup procedure

Answer 26

Props full forward
Set 1800 rpm using power levers
Retard props to detent and check 1600-1640 rpm

Question 27

Pressurization test engine runup procedure

Answer 27

Props full forward set 70% N1 on power levers
Turn off bleed air and note associated warning lights
Set pressure controller 500 ft below field elevation and rate knob to max
Hold cabin press switch to TEST
Open left bleed air valve, note 12-20 psi pneumatic pressure, bleed air warning extinguish, and decrease in cabin rate
Close left bleed air valve and repeat on the right
Reset cabin to 500 above field elevation, rate knob to 10 o’clock, and bleed air valves to enviro off

Question 28

Auto feather/ auto ignition engine runup procedure

Answer 28

Props full forward
Autoignition ON
Power levers set 25% torque
Hold AUTOFEATER to TEST and not both annunciator lights
Retard to left power lever to 18+/-2: opposite autofeather extinguishes and same side ignitor light illuminates
Retart left power lever to 11 +/-2: both autofeather lights extinguish and prop begins to feather
Repeat on right power lever
After both power levers are checked retard both to IDLE, both autofeather lights will extinguish and autoignition lights illuminate
Release test switch and turn autoignitors OFF

Question 29

Prop manual feather engine runup procedure

Answer 29

Power levers idle and props full forward
Manually feather both propellers
Note that N1 does not decrease by more than 1 percent