How is the nose

cone heated?

Continously via P2.8 air

What is heated when you

select the engine anti-ice?

a) Inboard wing

b) Nacelle lip

c) First stage stator vanes

d) FADEC probes

e) Stabilizer leading edges

What must be on first for the outboard anti-ice to work?

Engine anti-ice must be on first

How is a pilot reminded to

turn engine anti-ice first before outboard anti-ice?

All associated wing, stab and engine anti-ice cold messages will appear in amber after 2.5 minutes

How does the X-flow fails

with loss of DC?

Fails closed

At what setting do you

have to set the power

to test the anti-ice?

70-75% N2

 How much power should you

set if the cyan message

are becoming amber

during ground test?

81% N2

How does bleed air monitor fail

and MAU 1-2-3-4 fail affects

the anti-ice system?

The EPIC system has lost ability

to display anti-ice messages

Leave icing conditions

What bleed air pressure is used for anti-ice above FL 250?

HP

What happens when you

select X-flow?

Wing anti-ice open

Stab anti-ice open

What problem is

a duct o'temp?

Environment problem due to a faulty TCV, bad controller, or bleed air just too hot

How can you tell the

temperature of the duct?

Select the appropriate supply

on the temp panel

Can a pilot select the nose cooling fan from the cockpit?

Turns automatically at 95F

Pilot can select HI

How can you turn off

windshield anti-ice?

L and R windshield anti-ice circuit breaker

How is the AOA

vane heated?

Pitot switches

(main DC)

How is the AOA

casing heated?

Avionics switch

How many ADC's

are there?

3 total:

Left, right, stby

What does the left

pitot turns on?

Left pitot

Left AOA

Stby system

What does the right

pitot turn on?

Right pitot

Right AOA

Stby system

What system use the

differential pressure gauge?

Stby system

On what bus is the

stby pitot static?

Emer bus

What does pitot/static cold

L-R stby mean?

Pitots are off while on the ground

What does pitot/static cold

L-R-stby mean?

Taking off with pitot switch off

Or malfunction

What does the pitot/static cold L-R-stby message monitor?

Current only

Not a temperature sensor

Is the AOA vane included

in the message pitot/static

cold L-R-stby?

Independent

Will get AOA heat fail L-R instead

What heats the stator vanes?

Same as nose cone: P2.8

What anti-ice valves are

normally closed in emer?

X-flow valves

How does the anti-ice system

fail on emer?

Fail safe

except X-flow

What is the stab

anti-ice limitation?

Must be on 1 minute prior to

descent at idle in icing condition

Is the trim on the

pylon heated?

No, cosmetic only

How long will a cold CAS

message remains cyan

once airborne?

 2.5 minutes

How long will a cold CAS

message remains cyan

when first turned on?

2.5 minutes

What does eng anti-ice

cold L-R mean in flight?

Either undertemp of engine inlet

Or stator anti-ice valve did not open

What happens to the

anti-ice system in o'temp?

Automatic shutoff

After surface has cooled, cycle on and off

When should wing

anti-ice be turned on?

Visible moisture +5 to - 35C RAT

When should engine

anti-ice be turned on?

Visible moisture +10 to -35C RAT

Can you use the anti-ice

system to deice the wings?

Prohibited

Why does the engine anti-ice

must be turned on first

before the wing anti-ice?

Need to open anti-ice engine stab valve

first to get through the wing

When do you get the cyan

cold messages in flight?

a) When you first turn it on

b) Whenever bleed air is shutoff

due to malfunction (result message)

Which of stab or wing

anti-ice X-flow valve is

monitored on EICAS?

Wing

When is "wing anti-ice

X-flow" cyan?

When the valve is open after

being selected open

When will you get wing

A/I crossflow open message?

When the valve remains open after

being selected closed

How would you know if

the X-flow valve did not open?

Would find out indirectly with

stab anti-ice cold messages

On what bus is the

bleed detection?

Main DC

What closes for

a wing bleed leak?

Wing anti-ice valve

What valves close

for a stab bleed leak?

left and right stab anti-ice valves

What valves close for

a supply bleed leak?

Left and right wing anti-ice

Left and right stab anti-ice

What cyan message come

as a result of a wing bleed leak?

Wing anti-ice cold L-R

What valve close during

an ACM bleed leak?

Left and right mass flow valves

BCV's (bleed control valve)

Max altitude to use anti-ice

FL 410

Min airspeed in icing

180 kts

Max OAT on the ground

to have anti-ice on

+20C (68F)

Except preflight test

What is recommended when

taxiing through slush and ice?

Leave flaps up until completing T/O checklist, to prevent ice contamination on the flaps surface

What is recommended with

the brakes taxiing through

slush and ice?

Heat them within the last mile of taxi to remove excess water that may freeze after T/O

What should you do with the

landing gear if you taxied

in ice and slush?

Leave gear down until 200 Kts to aid in clearing moisture and slush from gear

Minimum holding speed in icing

180 Kts

Max water/slush allowed on the runway for the Sovereign?

0.4 inches (1 cm)

(Advisory section)

At what temperature must

the cabin be at to be able

to deploy the masks, if cold soak?

56F by FL 250

On what bus are

the windshields?

Main DC

When are the windshields

heated?

With engine running

How can you check a failed

sensor on the windshields?

Rotary test

What is the normal

windshield temperature?

110F

What is the windshield o'temp?

140F

What comes on when you turn

on the engine anti-ice?

 a) Nacelle heat (bleed air)

b) 1st set of stator vanes (P2.8)

c) Stab anti-ice (bleed air)

d) Eng/stab anti-ice valve (bleed air)

e) Rat probes (electrical)

f) Allows cold messages

Can you get pitot/static cold

L-R-stby in flight?

No, this message would be amber instead

What monitors the case

around the AOA probe?

Not monitored

When is using X-flow

prohibited?

Wing or stab bleed leak

If the wing bleed leak message does not extinguish, the procedure is to turn off the opposite wing anti-ice. Why?

Since one wing can not be anti-iced,

the procedure is to match the condition

for asymmetry

What is a PRSOV?

a) Pressure regulator

b) Temperature regulator

c) Shutoff valve

How do you define

visible moisture?

Visibility less than 1 mile

Why is windshield heat

not available in emer?

Due to high amps loads, left and

right pitot/static are not on the emer bus either. (only stby is).

Since this require an exit from icing conditions, Cessna decided to leave the windshield heat off emer bus also

What do you turn on with the

PITOT/STATIC  switches?

Pitot tubes

Static ports

AOA vanes

When are the AOA cases heated?

When the avionics switch is ON

When are the RAT probes heated?

When you turn on the ENGINE/STAB

anti-ice switches ON

Does the crossflow shutoff valve

fail close or open with loss of DC?

Fails closed

Why does the AFM ask to heat the brakes

within the last mile of taxi in

cold weather and contaminated taxiway?

Short answer:

To remove excess water

Longer answer:

Carbon brakes are "hygroscopic",

meaning it absorbs liquids.

Once the still wet wheel assemblies get colder temperature, the liquids spread further apart between the rotors and stators and lock the brakes solidly.

How does Cessna defines severe icing on a Sovereign?

Accumulation standing more than 12 to 18 inches aft of heated leading edge.