King Air A100 Flashcards
EMER Engine Failure in Cruise
- Identify and verify failed engine
- Throttle of bad engine - idle
- Propellor lever - feather
- Condition Lever - cutoff
- Bleed Air - As required
- Fuel Pump - Off
- Fire Wall valve - Off
- Generator - Off
If a bleed air line breaks in flight what will happen?
What should the pilot do in response?
- Increase in ITT
- Decrease in Torque
- Increase in N1
Secure engine if conditions permit
How much weight is allowed in:
- The rear baggage compartment
- Couch
- Drawers
- On top of rear drink cabinet
- 410 lbs rear baggage
- 340 lbs on couch
- 30 lbs/drawers under couch
- 100 lbs on to of cabinet
What does the limiter unit do?
Limits the:
- Controls starting parameters
- reverse thrust
What does does the TSLM light stand for?
Turbine Start limiter module
If no ITT rise within 12 secs what should the pilot do?
- Cut off condition lever
- Allow 30 secs delay to drain fuel clear engine.
- In case of 3 unsuccessful starts fuel must be drained from drainage container.
Engine restarting is permitted up to ______ ft and up to ________ kts.
13,123 ft and 162 kts.
Severe icing is indicated by:
- Airspeed loss greater than 20 kts
- Decrease in rate of climb to 300 fpm
- Accumulation of ice on spinner more than normal
EMER: Engine fire on ground
- Condition lever cutoff
- Fuel firewall valve closed
- Starter switch - start only (push up)
EMER: Engine failure after takeoff
- Power max allowable
- Prop - Full Increase
- Airspeed - maintain speed at engine failure until obstacles are cleared
- Gear Up
- Identify/verify/Feather
- Airspeed - Vxse - 113 kts
- Flaps up
- Clean up
- Maintain at least blue line - 120 kts
What are the minimum weather requirements at an alternate airport?
Alternate with one approach - add 400 feet and 1 mile to minimums
Alternate with 2 approaches - add 200 ft and 1/2 mile to the highest of the two approaches
When is an alternate airport required?
- Forecast one hour before to one hour after landing time if the ceiling is (135.223):
a. at least 1500 ft above the lowest circling approach or
b. if no circling approach at least 1500 ft above the lowest published minimum or 2000 ft above the airport, whichever is higher
c. Visibility at least 3 miles or 2 miles above the lowest applicable minimums - whichever is greater for the instrument approach to be used at the destination.
EMER: What is the emergency descent procedure?
- Power levers - idle
- Propellor - full increase RPM
- Wing flaps - Approach only
- Landing Gear - Extend
- Airspeed - 156 kts maximum
EMER: Engine failure below rotation speed
- Power - IDLE
- Brake
If it looks like aircraft will go off end of rnwy: - Engine reverse if needed
- Condition levers to CUTOFF
- Firewall valves - OFF
- Electrical power - OFF
Describe electrical power distribution
Memorize the picture of power distribution in manual or picture on phone.
What is the quantity of fuel below which you cannot takeoff?
265 lbs/side or in the yellow arc
What are emergency squawk codes?
7500 -hijacking
7600 - no radio
7700 - emergency
How many starts are allowed on the Walter engines?
Five
2 minutes cooling time between each start
60 minutes after 5th attempt
A100 fuel capacity
- Wings
- Aux Tanks
- Wing - 388 useable gallons (2600 lbs)
2. Aux - 82 useable gallons (550 lbs)
A100 dimensions
Wingspan - 46 ft
Length - 40 ft
Top of Horizontal Stab - 15 ft
Main Gear - 13 ft wide
Max Torque Shaft Horse Power Max ITT Max RPM Max overshoot RPM Oil Pressure Oil Temperature
Torque - 1716 ft pounds
SHP - 680
Max ITT - 710
Max RPM - 1900 normal/ 2080 Takeoff - 2140 max overshoot during acceleration
Oil Pressure - 26 - 39 psi
Oil Temperature - 20 - 35 psi
How many fuel pumps are on the A100 with Walter engines and where are they?
Four on each side - (8 total)
- engine driven
- standy - electrical
- jet pump from auxiliary tank
- main electric pump
If ITT light illuminates what should be done after reducing power?
Controlling fuse must be replaced and logbook entry made
From which tank is fuel crossed when needed?
From one nacelle tank to the opposite nacelle tank.
Altitude limitation
25,000ft - set by Walter engine manual