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13 Cards in this Set

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Icing conditions

1. OAT on ground or for t/o is 5C or blw and visible moisture or vis < 1sm


2. 5C or blw with surface snow, ice, standing water, or slush

Bleed air from single engine

Sufficient for either:


1. Both ESC packs OR


2. 1 ESC pack & ice protection

Pitot and AoA sensors

LH pitot probe & LH AoA sensor (ESS BUS)


- probes 1 PB


RH pitot probe & RH AoA sensor (NON ESS Bus 2)


- probes 2 PB


TAT sensor (ESS) & Stdby pitot probe (DC bus 2)


- STBY PB



Static ports


- ice free design (aerodynamically protected)

Windshield

Wipers


- separate 28V DC motors



Heat


2 independent systems:


- WSHLD 1 = Capt front & FOs side


- WSHLD 2 = FOs front & Capts side


System applies soft heat for first 5 mins to prevent thermal shock


Airfoil deice & sequence of de-icing cycle (5)

Inflated (energized condition)


- P3 air regulated to 21psi to boots


Non-inflated condition


- ejector flow control valve applies suction pressure to boots


* bleed PBs must be ON to operate



Cycle:


Outer section wing


Outer section stab & upper vert stab


Inner section stab & lwr vert stab


Middle section wing


Inner section wing



4 sec dwell time btwn sections


EFCV energized for 6 secs (=46s)

Airfoil cycle selector

Single - 1 deicing cycle only (46secs)


Slow - deicing cycle (46secs) w/ dwell period of 134 secs btwn cycle = 3min


Fast - decing cycle (46s) w/ dwell period of 14 secs btwn cycle = 1min

Engine air intake de-ice cycle

3 inflatable boots ea inlet



Engine intake boots: 6secs


Deflate period: 54 secs

Horn heat ON on t/o

LH = Left elevator and rudder horns


RH = right elevator horn


Blue numbers (Higher V1/Vr/V2)


Otherwise could get stall horn


- when selected ON, stick shaker/pusher thresholds adjusted

Prop heat electric pwr automatically removed

If prop < 650 RPM


= Np < 50%

Prop heat ab -10C

De-icer mats heated for 7 secs seperated by 29 sec interval


Blades 1/3/5 begin heating, 36 secs later other blades begin heat


72 secs total

Prop heat blw -10C

Mats heated for 25 secs seperated by 17.5 sec interval


Blades 1/3/5 begin heating, 42.5 secs later other blades begin heating


85 secs total


*system auto shutdown ab 5C

Ice detection system

Ice builds changing weight and resonance fqz



ICE signal activated for 60 secs then heaters auto switched ON clear probe



EICAS msg stay on for 5 mins

Representative surface

O/b LE of wing AND/OR


Prop spinner