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 Pitot - Static Systems Pitot - Static Systems

©PanAm International Flight Academy, Inc. 2001

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Pitot System•required for airspeed information

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Static System

•required for outside air pressure

•Altimeter

•ertical speed

•Pressuri!ation System

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Pitot "u#es

•left feeds $aptain%s airspeed

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•right upper feeds F&

airspeed

•right lo'er feeds AF$S (flight

director)

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Pitot "u#es are heated

•F& s*irt panel

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Stall ane + Pitot

•&"- stall ane and  

pitot heat

•/eft + ight

•& + &FF

Annunciators

•/eft 31 PI"&" &FF

PI"&"

1 &FF

•ight

•32 PI"&" &FF

•34 PI"&" &FF

PI"&"

2 &FF

PI"&"

4 &FF

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&"56

•o indication of stall ane heat failure

•PI"&" 34 &FF 'ired through 5ssential Aionics 7aster s'itch

PI"&"

1 &FF

PI"&"

2 &FF

PI"&"

4 &FF

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Filiment 8im

•$ontrols intensity of annunciator lights

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Static ent Plates

•rear of aircraft on #oth sides connected

•9 ents per plate

•&" heated

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Shape deflects airflo'

•proides static pressure area

•preents icing of ents

S1

S2S4

S:

S9

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Interior of the static ent plates

•#onus question6 'hich side is this;.the right or left side <

Flight $ontrol ca#les

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ent Plates

•

connected

•ia oerhead to coc*pit

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S1

•feeds $aptain instruments

S2

•feeds F& instruments

•note F& airspeed feedsoerspeed 'arning system

S4

•discharge ale

S:

•safety ale

S9

•ca#in differential, F8, F8 

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$aptain has an alternate

•S=

•ear Pressure ul*head

•$hangeoer coc* 

ote all the 'ater drains

•all in for'ard part of

aircraft at lo'est points

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S= Static ent Source

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Alternate Static S'itch

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If 'e are happy 'ith the pitot+static system

'e can get a closer loo* at the flight instruments that use this