Ch7 Normal Procedures Flashcards
When is the climb checklist performed?
1000 AGL or when entering the VFR pattern
If possible, propeller levers should be moved out of reverse above ____ to prevent prop blad erosion.
40 knots
The propeller levers must be placed ___ to ensure proper reversing characteristics.
Full forward
Max wind beyond which structural damage can occur.
75 knots
During start, if N1 stabilizes at less than ___ anticipate a hotter than normal start.
17 percent
During start, if N1 stabilizes below ___ consider a GPU start to prevent the possiblity of an overtemp on start.
15 percent
Minimum strut extension
Main: 5.56 “
Nose: 3.77”
After start generator voltage should be indicated on both buses. If this is not the case, then a ___ may have failed.
Current limiter
Time for alignment of the ESIS
2-3 minutes
If windshield temperature is greater than ___ windshield antiice may not operate.
32 C
Maximum takeoff weight may be restricted by the following:
Accelerate stop within runway length
100 fpm climb with gear down and failed engine
Achieve obstacle clearanace climb gradient
2 engine minimum N1’s to maintain pressurization schedule on descent
75%
1 engine minimum N1 to maintain pressurization schedule on descent
85%
Approach speed
120 KIAS or Vref whichever is greater
What is considered a short field landing
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.
Waveoff procedures
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
How long must ITT be stabilized prior to engine shutdown
1 minute
How many static wicks are required
5, 1 on rudder, 1 on outboard ends of each elevator, 1 on each outboard ends of the ailerons
Prop rpm range for overspeed governor check
1830 to 1910 rpm
Minimum flight deck oxygen pressure
500 psi
Reserve fuel requirements
10 percent or 45 minutes of flight at endurance (10K) whichever is greater
How often should a flight fuel log be kept
Every flight a fuel log should be prepared on cross checked with actual fuel consumption for every flight
Takeoff power must be applied ___ to obtain the normal takeoff distances from performance charts
Prior to releasing brakes
When is cruise checklist performed
Extended cruise operation, not normally below 10,000 ft or in pilot training environment
Overspeed governor and rudder boost engine runup procedure
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
Primary governor engine runup procedure
Props full forward
Set 1800 rpm using power levers
Retard props to detent and check 1600-1640 rpm
Pressurization test engine runup procedure
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
Auto feather/ auto ignition engine runup procedure
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
Prop manual feather engine runup procedure
Power levers idle and props full forward
Manually feather both propellers
Note that N1 does not decrease by more than 1 percent
