Lear 1A Anti Ice and Environmental

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    L e a r j e t

    3 A

    P i l o t s

    Manual

    T BLEOFCONTENTS

    Wyfl om

    v

    NTI I CE

    ENV RONMENT L

    Ant i i ce

    Syst ems 6 - 1

    I c e

    Det ect L i ght s . 6 - 1

    Wng I nspect i on

    L i ght

    . 6 - 2

    Engi ne and

    Nacel l e

    I n l e t Ant i i ce

    . 6 - 2

    N CHE T

    Sw t ches

    . 6 - 2

    N CHTON

    L i ght

    6 3

    L

    and

    RN C

    HT

    Li ght s

    . 6 - 3

    WngAnt i i ce

    . 6 - 3

    ST BWNG

    HE TSw t ch

    WngHeat

    Funct i on

    6 3

    Wng

    Ant i i ce Syst em Fi gur e 6 - 1 6 4

    WNGTEMP

    I ndi cat or

    . 6 - 5

    WNG

    OV

    HT

    L i ght

    . 6 - 5

    Hor i zont al S t a bi l i z er Ant i i ce

    6 5

    ST B

    WNG

    HE T

    Sw t ch

    S t a bi l i z er

    Heat

    Funct i on

    6 6

    ST B

    HE T

    L i ght

    6 6

    W ndshi el d

    Ant i i ce

    6 6

    W ndshi el d

    Ant i i ce

    Syst em Fi gur e 6 - 2 6 7

    WSHLD

    HE TSw t ch . 6 - 8

    WSHLDHT

    L i ght

    6 8

    WSHLDOV

    HT

    Li ght

    . 6 - 8

    W ndshi el d

    Defog

    6 9

    WSHLD

    DEFOG

    Sw t ch

    . 6 - 9

    L

    and

    R

    WSDEFOG

    Annunci at or s

    . 6 - 1 0

    W ndshi el d

    Defog

    Syst em Fi gur e 6 - 3

    . 6 - 1 0

    W ndshi el d and

    RadomAnt i i ce

    Al cohol

    Syst em

    6 - 1 1

    LCOHOLSw t ch

    6 - 1 1

    LCLOW

    aut i on

    Li ght . 6 - 1 1

    Al cohol

    Ant i i ce Syst em

    Fi gur e 6 - 4 6 12

    P i t o t - s t a t i c andSt a l l

    Warni ng

    Ant i i ce 6 13

    PTTOTHE T

    Sw t ches

    . 6 - 1 3

    PTTOTHT

    Li ght . 6 - 1 3

    OxygenSyst em

    6 14

    OxygenSt or age andPressure

    Regul at or 6 14

    OxygenSyst emSchemat i c Fi gur e 6 - 5

    . 6 - 1 5

    OxygenPressure Gage 6 16

    OxygenSyst em

    Cockpi t

    Cont r ol s

    . 6 - 1 6

    PM 121

    VI 1

    Change

    4

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    P i l o t s Manual

    L ea r j e t

    3 A

    TABLE

    OFCONTENTSCont

    Passenger

    Masks

    6- 17

    Passenger

    Mask

    Fi gur e

    6 - 6 )

    6- 17

    Crew

    Masks

    6- 18

    CrewMask

    6600214 S e r i e s

    Fi gur e 6 - 7 )

    6- 18

    CrewMask

    Scott TOMC10- 15- 01 Fi gur e 6 - 8 ) 6- 19

    Pressur i zat i on Syst em

    6- 19

    Normal

    Pressur i zat i on 6- 20

    Emergency

    Pressur i zat i on 6- 20

    Pressur i zat i on Syst em

    Schemat i c

    Fi gur e

    6 - 9 )

    . 6- 21

    Pressur i zat i on

    Cont r ol s

    and

    I ndi cat ors

    6- 22

    BLEEDAIRSwi t ches

    6- 22

    BLEED

    AIRWarni ng

    Li ght s

    6- 22

    C BAIRSwi t ch

    6- 23

    CAB

    AIR

    Li ght

    6- 23

    Pressur i zat i on

    UTOM N

    Sw t c h 6- 23

    Cabi n

    Cont r ol l er 6- 23

    Pressur i zat i onManual

    Cont r ol

    Lever UP-DN

    6- 24

    CABI NALT/DFF PRESSGage

    6- 24

    CABI NCLI MB

    I ndi cat or

    6- 24

    EMER

    PRESS

    OVERRIDE

    Swi t ches 6- 24

    CABALT

    Li ght

    6- 25

    Cabi n

    Al t i t ude

    Warni ngHorn

    6- 25

    SYSTEM

    TEST

    Swi t ch

    CABI NALTFunct i on 6- 25

    Ai r Condi t i oni ng andHeat i ng 6- 25

    Pr i mar y Heat i ng andCool i ng

    Bl eed

    Ai r

    6- 26

    Tai l cone Bl eed- Ai r Di st r i but i on Fi gur e 6- 10

    6- 27

    CAB

    AIR

    Swi t ch

    6- 28

    UTOM N

    Sel ect or

    6- 28

    HOT-COLD

    Temper at ure S e l e c t o r 6- 28

    Ai r

    Di st r i but i on

    Schemat i c

    w t h R12 Freon Cool i ng Syst em Fi gur e

    6 - 1 1 )

    6- 29

    w t h R134ACool i ng Syst em Fi gure 6 - 1 2)

    6- 30

    TEMP

    CONTI ndi cat or

    6 - 3 1

    CABI NTEMP i ndi cat or

    6 - 3 1

    Temper at ure Cont r ol Schemat i c Fi gure

    6 - 1 3)

    6- 32

    R

    FreonCool i ng Syst em

    Ai r c r a f t

    wi t hout

    For war d

    Evapor at or

    and Bl ower

    Uni t 6 - 3 3

    R Freon

    Cool i ng

    Syst em

    St andar d

    Evapor at or

    Fi gur e

    6 - 1 4 )

    6- 33

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    L ea r j e t 31A

    P i l o t s Manual

    TABLEOF

    ONTENTS

    Cont

    COOL-OFF Swi t ch 6- 34

    CABINF NSwi t ch . 6- 34

    Cabi n Bl ower

    Di ver t er

    Cont r ol

    . 6- 34

    REWF N

    Swi t ch

    . 6- 34

    R12

    Freon

    Cool i ng

    Syst em

    A i r c r a f t wi t h Forward

    Evaporat or and

    Bower

    Uni t . 6 35

    COOL-OFFSwi t ch 6- 35

    CABIN

    F NSwi t ch 6- 35

    Cabi n

    Bl ower Di ver t er Cont rol . 6- 36

    R12

    Fr eon Cool i ng

    Syst em

    Opt i onal

    For ward

    Evaporat or

    Fi gure6- 15 . 6- 36

    REWF N

    Swi t ch

    . 6- 37

    R134ACool i ng Syst em

    . 6- 37

    COOL-OFFSwi t ch

    6- 38

    GASPERFAN

    . 6- 38

    FLOODFANCont rol

    . 6- 39

    REWF NCont r ol . 6- 39

    R134ACool i ng

    Syst em

    Fi gure 6 - 1 6 ) 6- 39

    Auxi l i ary

    Heat i ng Syst em

    . 6- 40

    CrewHeater 6- 40

    Cabi n Heater . 6 - 4 1

    UX

    HTSwi t ch

    . 6- 42

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    Lear j et 31A

    P i l o t s

    Manual

    ANTI ICE

    SYSTEMS

    SECDON

    ANTI ICE

    ENVIRONMENTAL

    Ai rcraf t

    a n t i - i c e protecti on i s provi ded through t he use of

    e l e c t r i c a l l y

    heat ed

    a n t i - i c e

    sys t ems,

    engi ne

    bl eed

    a i r heat ed a n t i - i c e

    syst ems, and

    anal cohol a n t i - i c e system E l e c t r i c a l l y heat ed s ys t ems

    i nc l ude

    t he

    pi -

    t o t - s t a t i c

    probes,

    t o t a l

    a i r

    t emper at ur e

    probe,

    engi ne

    i n l e t

    a i r

    t emper a-

    ture

    and

    pressure sensors,

    s t a l l war ni ng vanes, and

    hori zont al s t a b i -

    l i z e r l eadi ng

    edge

    E l e c t r i c a l l y heat ed w nds hi el ds pr ovi de

    w nds hi el d def oggi ng Engi ne

    bl eed

    a i r i s u t i l i z e d t o heat t he

    wng

    l eadi ng

    edge,

    w ndshi el d,

    andnacel l e i n l e t s Theal cohol systemi s i n -

    s t a l l e d t o

    pr ovi de a n t i - i c i n g

    f or t he

    nose radomeand

    backup

    a n t i - i c e

    protect i on

    f or t he p i l o t s

    w nds hi el d i n

    event

    of

    nor mal

    ant i - i c i ng s y s -

    temmal f unct i on

    ICE

    DETECT

    LIGHTS

    Two i c e

    detect

    l i g h t s are i n s t a l l e d

    on

    t he f or war d

    gl areshi el d t o

    i n d i -

    cate

    i c e

    or

    moi s t ur e

    f ormat i on ont he

    w nds hi el d dur i ng

    ni ght

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    t i ons These

    l i g h t s

    ar e

    i l l um nat ed whenever

    t he

    BATTERYsw t ches

    are On

    Wen

    part i c l es of

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    or moi s t ur e f or m

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    c o p i l o t s

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    posi t i oned

    out si de t he

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    i c e ai r st ream

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    t he c o p i l o t s w nds hi el d must be

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    PM121

    6-1

    Or i gi nal

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    P i l o t s Manual

    Leazj et 31A

    WNGNSPECTI ONLI GHT

    Thew ngi nspect i on l i g h t ,

    l ocat ed on

    t he r i ght

    f or war d

    f usel age, may

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    Theengi ne and

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    andpressure Pn

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    N HEAT

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    on

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    6

    PM121

    Or i gi nal

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    Lear j et 31A

    Pf l ot e Manual

    NAC

    HT

    ON

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    The

    gr een

    NACHT

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    i g h t

    on

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    Pi l ovs

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    ear j et 3 A

    WN NTI ICESYSTEM

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    Pi l ot s

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    WNGTEMPINDCATOR

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    poi nter

    i s

    i n t he r ed

    segment , t he

    w ng

    l eadi ng

    edge

    i s

    appr oachi ng

    an

    overheat condi t i on

    and

    cor recti ve

    act i on

    must be t aken

    The

    w ng

    a n t i i c e system

    shoul d

    be

    energi zed

    whenever

    f l y ing t hrough v i s i b l e

    moi st ur e

    and t he

    WNGTEMP

    i ndi cat or poi nter

    i s

    i n

    t he

    bl ue

    segment

    WNG

    HT

    LI GHT

    The r edWNGOVHT

    l i g h t on

    t he gl areshi el d

    annunci at or

    panel ,

    wi l l

    i l l umnate i n

    t he event

    t h a t

    t he

    wng

    l eadi ng

    edge

    heats

    t o

    215F

    102C The l i g h t i s ener gi zed by t he

    overheat

    want i ng l i g h t

    t hermo-

    swi t ch l ocat ed on

    t he

    i nner

    sur f ace of

    t he

    r i g h t w ng l eadi ng

    edge

    HORIZONTAL

    STABI LI ZER

    ANTI - I CE

    Thehor i zontal s t a b i l i z e r a n t i i c e syst emu t i l i z e s sequenced

    e l e c t r i c a l

    heat i ng el ement s al ong t he

    hor i zontal

    s t a b i l i z e r

    l eadi ng

    edge

    The

    systemconsi st s of

    an

    e l e c t r i c a l l y

    heat ed

    bl anket bonded t o each

    ha l f

    of t he

    hor i zontal

    s t a b i l i z e r l eadi ng

    edge,

    a sequence

    t i me r a caut i on

    l i g h t a

    system

    swi t ch,

    andassoci at ed a i r c r a f t

    wi r i ng Control c i r c u i t s

    oper ate on 28VDCsuppl i ed t hrough t he

    7S amp

    STAB

    HTc i r c u i t

    br eaker

    on

    t he

    copi l ot s

    c i r c u i t br eaker panel E l e c t r i c a l

    power f or t he

    heat i ng

    el ement s

    i s

    28

    VDC

    suppl i ed

    t hrough a 130- amp current

    l i m

    i t e r

    PM 2

    6

    Or i gi nal

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    STABWNGHEATSWTCH

    STABI LI ZER

    HEATFUNCTION

    Thehor i zont al s t abi l i zer ant i - i ce system s cont r ol l ed through t he

    STAB

    WNG

    HE Ts w t c h ont he

    cent er

    s w t c h panel Thes w t c hhas twopo-

    s i t i ons

    On

    STABWNG

    HEAT

    and

    OFF

    When

    t he

    a i r c r a f t

    i s

    i n

    f l i gh t

    and t he

    STAB

    WNG

    HE T

    s w t c h i s On, 28VD s suppl i ed through

    t he

    s t ab heat

    r e l a y box t o t he

    sequence t i mer

    The

    t i mer di s t r i but es

    i n-

    t e rmt ten t e lect r ica l power

    t o

    t he

    i ndi vi dual heat i ng el ement s i n a f or -

    war d- t o- af t sequence of 15 seconds dur at i on each

    Approximatel y

    3

    mnutes ar e

    r equi r ed t o

    compl ete a f u l l cyc l e The center,

    or

    par t i ng e l -

    ement s ,

    ar e

    suppl i ed

    wthcont i nuous el ect r i cal power

    Duri ngnormal

    s tab i l i ze r heat oper at i on, t he a i r c r a f t D

    MPS

    r eadout

    w l l

    r e f l ec t a

    pul sat i ng

    current

    dr ai n

    of

    appr oxi mat el y

    60-amps i n

    15

    second

    cycl es

    At

    l east one engi ne

    gener at or

    must be oper at i ng t o ener gi ze t he s t ab

    heat cont r ol ci r cui t s

    The cont r ol

    c i r c u i t s ar e r out ed through a st ar t

    cut -

    out r el ay

    and

    t he r i ght

    squat

    s w t c h

    t her ef or e,

    t he

    system

    s

    i noper at i ve

    when t he squat s w t c h i s i n t he groundmodeand dur i ng engi ne s ta r t

    STABHEAT LIGHT

    The

    amber STAB

    HT

    i g h t

    l ocat ed

    on

    t he

    gl ar eshi el d annunci at or panel

    w l l

    i l l umnat ewhenever t he STAB

    WNG

    HE Ts w t c h i s

    On

    and t he

    heat i ng bl anket par t i ng el ement s

    ar e not r ecei vi ng e lect r ica l power

    Duri ng f l i g h t i l l umnat i on of

    t he STAB

    HTl i ght

    i ndi cat es

    system a i l -

    ur e Duri ng ground oper at i on, t he STAB

    HT

    l i ght shoul d

    i l l umna t e

    whenever t he STAB

    WNG

    HE Ts w t c h s

    ON

    WNDSHIELDANTI- ICE

    Primary

    w ndshi el d

    an t i - i c i ng

    i s

    acc ompl i s hed

    by

    di r ec t i ng

    condi -

    t i oned engi ne bl eed

    ai r

    through

    duct i ng and

    cont r ol val ves

    toexternal

    out l et nozzl es f orward of

    t he

    w ndshi el d

    The

    wndshi el d an t i - i c e sys-

    temconsi st s

    of

    an an t i - i c e

    over heat

    shut of f val ve,

    a

    w ndshi el d

    an t i - i c e

    modul ati ng val ve, one l ow l i m t 215F

    [ 102C]

    and one

    h i gh - l im t

    250F

    [ 121C]

    thermoswtch f or ground

    oper at i ons,

    one l ow l i m t

    250F

    [ 121C]

    and one

    h i gh - l im t

    270F

    [ 132C]

    thermoswtch

    f or

    f l i g h t

    oper at i ons,

    a green

    WSHLD

    HT

    l i g h t a r ed

    WSHLD

    OV

    HT

    warni ng

    l i g h t

    a

    ram

    ai r

    modul ati ng

    val ve,

    an

    an t i - i c e

    duct

    t emper at ur e

    sensor, an

    an t i - i c e

    heat

    exchanger ,

    two

    out l et

    nozzl e ass embl i es, a sys-

    temcont r ol sw t ch, and associ at ed a i r c r a f t w r i ng and bl eed ai r duct -

    i ng

    El ect r i cal

    power

    t o

    t he cont r ol c i r c u i t s i s 28

    VD suppl i ed

    through

    t he 7 5 amp

    WSHLD

    HT

    c i r c u i t br eaker

    on

    t he pi l o t s c i r c u i t br eaker

    panel

    6- 6

    PM121

    Change

    3

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    P i l o t s Manual

    Change2

    WNDSHELD

    ANTI ICE

    SYSTEM

    Fi gure

    6

    NOTE Thi s f i gur e i s

    i nt ended

    t o r e f l e c t t he

    system l o g i c

    nd not

    necessar i l y l l of t he act ual

    component s used t o

    accompl i sh

    that

    l o g i c

    ONFUGHTTEMPERATURE

    UMTTHERMOSIMTCH

    RAMAI R

    MODaannNG

    VALVE

    Overheat An t i - I c e

    Shut of f l ve

    i s

    nor mal l y

    c l osed

    must

    be

    energi zed

    open

    ROUNDTEMPERATURE

    l e c t r i c a l ground on t h i s

    w r e tu rns

    UMTTHERMOSWTCH

    WSHLD

    HTl i g h t

    on

    SQUATSWTCHRELAY

    l e c t r i c a l ground

    on

    t h i s

    wi r e tu rns

    makes connect i onwhen

    a i r c r a f t

    s

    on

    the

    gr ound

    WSHLDOVHTl i g h t on

    i nput i s power

    or

    open

    c i r c u i t

    the

    out put

    i s

    an

    e l e c t r i c a l ground

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    WSHLD

    HEATSWTCH

    The

    wi ndshi el d a n t i - i c e

    system cont r ol l ed t hr ough

    t he

    WSHLD

    HE Tsw t ch i n

    t he

    ANTI - I CE

    gr oup

    on

    t he cent er sw t c h

    panel

    The

    sw t ch

    has

    thr ee posi t i ons

    On

    WHLD

    HEAT

    HOLD and

    OFF

    Whent heBATTERYsw t ches

    ar e

    s e t ON

    t he wi ndshi el d a n t i - i c e over-

    heat shut of f

    val ve

    i s ener gi zed

    t o

    t he open posi t i on When

    open,

    t he

    over heat

    shut of f val ve al l ows engi ne

    bl eed

    a i r

    t o

    f l o wdownstreamt o

    t he a n t i - i c e

    modul at i ng

    val ve

    When t he

    WSHLDHE T

    swi t ch

    i s

    pl aced i n

    t he

    On

    posi t i on,

    a c i r c u i t i s compl et ed t o

    t he a n t i - i c e modu-

    l a t i n g

    val ve and

    WSHLDHT

    i ndi cat or

    l i g h t

    The

    a n t i - i c e modul at i ng

    val ve

    wi l l

    movet owar d f u l l open u n t i l t he

    val ve

    i s

    f u l l y

    open or

    t he

    WSHLDHE T

    swi t ch i s s e t t o HOLDWhen

    t he

    sw t c h i s

    i n

    t he

    HOLD

    p o s i t i o n ,

    t he

    a n t i - i c e

    modul at i ng

    val ve

    wi l l

    r emai n

    i n

    i t s

    l a s t

    at tai ned

    p o s i t i o n , and

    al l owbl eed

    a i r

    t o t he

    a n t i - i c e

    heat exchanger When t he

    WSHLD

    HE Tswi t ch

    i s

    set t o OFF,

    t he

    a n t i - i c e

    modul at i ng

    val ve

    wi l l

    move

    t owar ds

    t he cl osed posi t i on

    u n t i l

    t he val ve

    i s

    f u l l y

    cl osed

    or t he

    WSHLDHE Tswi t ch i s s e t t o HOLDThe

    a n t i - i c e

    modul at i ng val ve

    wi l l

    f u l l y open

    or

    c l ose i n

    appr oxi mat el y

    15 seconds The

    a n t i - i c e

    heat

    exchanger cool s the

    bl eed

    a i r

    w t h rami r r egul at edby a

    ram

    i r

    mod-

    ul at i ng

    val ve

    Thi s

    val ve

    i s cont r ol l ed by t hedownstreama n t i - i c e

    duct

    t emper at ur e

    sensor

    and

    r egul at es t he

    a n t i - i c e

    bl eed

    a i r

    t emper at ur e

    by

    var yi ng t he

    amount

    of

    ram

    i r

    al l owed

    i n t o

    t heheat exchanger

    WHLD

    HT LI GHT

    The

    gr een

    WSHLD

    HT l i g h t , l ocat ed

    on

    t he gl ar eshi el d

    annunc i at or

    panel ,

    pr ovi des

    t he c rew wi t h

    a

    vi sual i ndi cat i on o f

    wi ndshi el d

    heat

    oper at i on

    The i ght

    wi l l

    i l l umnate

    whent he

    a n t i - i c e modul at i ng val ve

    i n

    any

    posi t i on

    except

    f u l l y

    cl osed

    and

    r emai n

    i l l um nat ed

    u n t i l

    t he

    appl i cabl e

    gr ound

    or

    i n f l i g h t

    l ow- l i mt

    t her moswi t ch

    t r i p s

    or t he

    WSHLD

    HE T

    swi t ch i s

    s e t

    t o

    OFF

    WHLD

    OV

    HTLIGHT

    I l l umnat i on of t he r ed

    WSHLD

    OVHT war ni ng l i g h t , on t he

    gl ar eshi el d annunci at or panel ,

    i n di c a t e s t h a t

    t he bl eed

    a i r

    t emper at ur e

    i n t he

    wi ndshi el d out l et nozzl es has r eached t he

    appl i cabl e

    gr ound

    o r

    i n f l i g h t

    hi gh- l i mt

    t her moswi t ch

    s e t t i n g

    and

    t he

    wi ndshi el d

    a n t i - i c e

    systemhas been

    shut down I f t he

    o ut l e t

    nozzl e bl eed

    a i r

    t emper at ur e

    r eaches 250F

    121C

    dur i ng

    gr ound oper at i on, t he gr ound hi gh- l i mt

    over heat

    t her moswi t ch wi l l

    c l o s e

    t he

    a n t i - i c e over heat

    shut of f

    val ve

    and

    i l l umnate the

    WSHLD

    OV

    HT

    war ni ng l i g h t

    I f t he

    o ut l e t

    nozzl e

    bl eed

    ai r t emper at ur e

    r eaches

    270F

    132C i n f l i g h t , t he i n f l i g h t

    hi gh-

    l i m t over heat

    t her moswi t ch wi l l per f o rm

    t he

    samef unct i on When

    t he

    PM 2 6- g

    Change

    3

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    P i l o t s

    Manual

    nozzl e

    bl eed

    a i r

    t emperat ur e

    cool s s u f f i c i e n t l y

    t he

    overheat

    t h e r -

    moswi t ches

    wi l l r e s e t and

    al l ow

    t he a n t i - i c e over heat

    shut of f val ve

    t o

    open,

    ext i ngui shi ng

    t he

    WSHLD

    OV

    HTwar ni ng l i g h t

    To avoi d

    a

    f a l s e

    WSHLD

    OVHT

    i ndi cat i on upon

    l andi ng, t he gr ound

    over heat t h e r -

    moswi t ch

    c i r c u i t r y

    i s

    di sabl ed

    f o r

    10

    seconds

    a f t e r

    t ouchdown,

    a f t e r

    whi ch

    nor mal

    f unct i oni ng wi l l

    r esume

    WNDSHELD

    DEFOG

    W ndshi el d

    i nt ernal

    def oggi ng

    i s accompl i shed

    usi ng e l e c t r i c a l l y heat -

    ed

    w ndshi el d

    panel s The

    system desi gned t o

    be

    acti vat ed bef or e

    t akeof f

    and

    r emai n

    on u n t i l

    shutdown

    The system

    consi st s

    of two

    w ndshi el d

    panel s w t h i n t e g r a l

    h e a t e r s

    w ndshi el d heat

    control

    u n i t

    system

    sw t ch,

    L

    and

    R

    WS

    DEFOG

    annunci at ors,

    and

    associ at ed

    a i r -

    c r a f t

    w r i ng

    Thesystem

    u t i l i z e s a

    163

    VACout put

    f r om t he

    i nver t er

    system t o power t he

    i n t e g r a l

    heaters

    The

    control c i r c u i t r ecei ves

    28

    VDCthrough t he5 amp

    LWSHLD

    DEFOG

    and

    RWSHLDDEFOGi r -

    c u i t breakers on t he

    p i l o t s

    and c o p i l o t s c i r c u i t

    breaker panel s

    WSHLDDEFOGSWTCH

    The

    w ndshi el d

    def og system

    i s

    cont r ol l ed

    through

    t he

    WSHLD

    DE

    FOG

    sw t ch

    i n t he

    ANTI ICE

    gr oup

    on t he

    cent er

    sw t ch panel

    The

    sw t ch

    has

    two

    posi t i ons

    OFF

    andOn

    WSHLD

    DEFOG

    Wen t he

    WSHLDDEFOG

    sw t ch

    i s s e t

    t o t he On

    p o s i t i o n

    t he

    i n t e g r a l heaters

    wi l l be suppl i ed

    163

    v o l t s

    ACpower f r omt he

    i n v e r t e r

    systemv ia t he

    w ndshi el d

    heat

    control

    uni t

    NOTE

    The

    i nver t er

    power i ng

    t he l e f t C

    bus

    wi l l power t he l e f t

    w ndshi el d

    panel

    whi l e

    t he

    i nver t er

    power i ng

    t he

    r i ght

    AC

    buswi l l

    power t he

    r i g h t

    w ndshi el d

    panel

    Normal system

    oper at i on

    i s

    i ndi cat ed

    by

    i l l umnat i on of

    t he L andR

    WSDEFOG

    annunci at or s when t he system

    i s

    act i vat ed w ndshi el d

    t emper at ur ebel ow8 F

    [27C Wen

    t he w ndshi el d

    i s heat ed above

    80F

    27C , t he annunci at ors

    wi l l

    exti ngui sh

    PM121

    6 9

    Change

    3

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    Lear j et A

    LNDRWS

    DEFOG

    ANNUNCIATORS

    I l l umna t i on

    of

    a

    WS

    DEFOG

    annunci at or ,

    l ocat ed on t he

    gl ar eshi el d

    annunci at or panel , i ndi cat es an over - t emper at ur e condi t i on, under

    t emper at ur e

    condi t i on

    or

    l oss

    of

    or

    D

    power

    Normal

    oper at i ng

    t emper at ur e

    of

    t he wndshi el d i s between 105F 41C and 120F

    49C

    Temperature sensor s ar e

    attached t o

    each wndshi el d

    panel

    whi ch pr ovi de t emper at ur e

    dat a

    t o

    t he

    w ndshi el d

    heat cont r ol

    uni t

    Shoul d t he t emper at ur e

    of

    t he w ndshi el ddropbel ow80F

    27C ,

    t he

    appl i cabl eWS

    DEFOG

    annunci at or w l l i l l umna t e t o al er t t he crew

    Shoul d

    t he t emper at ur e

    of

    t he w ndshi el d

    i ncr ease

    above150F 66C ,

    t he

    appl i cabl eWS

    DEFOG

    annunci at or w l l i l l umna t e and

    t he

    affected

    w ndshi el d w l l bedeact i vat ed

    When

    t he wndshi el d

    cool s

    t o t he nor -

    mal oper at i ng r ange, t he systemw l l r eact i vat e andt he

    WS

    DEFOG

    an-

    nunci at or

    w l l ext i ngui sh El ect r i cal f aul t s det ect ed

    by t he system

    moni tor w l l cause t he affectedWS

    DEFOG

    annunci at or t o

    i l l umna t e

    LWSHLD

    R

    WSHLD

    DEFOG

    DEFOG

    WSHLD

    DEFOG

    83

    V

    I N

    OFF

    WNDSHIELDDEFOGSYSTEM

    Fi gur e 6 3

    6-10

    PM 2

    Change

    3

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    WNDSH ELD

    NDR DOME

    ANTI I CE L OHOLSYSTEM

    The

    al cohol

    a n t i - i c e

    system i s

    u t i l i z e d

    f or radome a n t i - i c e pr ot ecti on

    and f o r w ndshi el d a n t i - i c i n g i n

    t he event of

    a w ndshi el d heat i ng s y s -

    tem

    mal f unct i on

    Al cohol

    a n t i - i c i n g

    i s

    accompl i shed

    by

    di r ect i ng

    met h-

    y l

    al cohol

    over

    t he

    p i l o t s

    w ndshi el d sur f ace

    through

    anext er nal

    o ut l e t

    i n t he

    w ndshi el d heat o ut l e t

    nozzl e

    assembl y

    and

    through an o ut l e t

    nozzl e assembl y on t he radome Thesystemconsi sts o f a 1

    . 7 5

    gal l on

    6 6 l i t e r )

    al cohol

    r e s er v o i r , a

    f l o a t

    sw tch,

    af i l t e r a

    r e l i e f

    val ve, at h r e e -

    waycontrol val ve,

    a

    bl eed

    a i r

    shut of f and

    pressure

    r egul at or val ve,

    a

    systemsw t ch,

    an

    amberL LOWaut i on l i g h t ,

    and

    associ at ed a i r -

    c r a f t w r i ng The pressure

    r e l i e f

    val ve i s i n s t a l l e d t o pr event system

    over pr essur i zat i on

    by

    vent i ng system

    pressure

    gr eat er

    than 2 6

    psi

    17

    9

    kPa

    above

    ambi ent ,

    and

    bl eed

    system

    pressure whent he

    system

    i s o f f Thesystem

    control

    c i r c u i t s oper at e on28VD suppl i ed t hr ough

    t he

    5 amp

    ALC SYS

    c i r c u i t

    br eaker

    on

    t he

    c o p i l o t s

    c i r c u i t

    breaker

    panel

    L OHOL

    SWTCH

    The

    al cohol

    a n t i - i c e systemi s

    cont r ol l ed

    by

    t he

    three

    posi t i on

    ALCO

    HOLsw t ch

    on

    t he cent er sw t ch

    panel

    When t he sw t ch i s

    s e t

    t o WS/

    RAD

    c i r c u i t s

    ar e

    compl et ed

    t o

    open

    t he

    shut of f

    and

    pressure

    r egul at or

    val ve

    and

    posi t i on t he t hr ee- way

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    t he

    w ndshi el d andradome Theal cohol

    r e s er v o i r ,

    pr essur i zed

    t o

    appr oxi -

    mat el y

    2

    4 psi 16 . 5 kPa above ambi ent t hr ough

    t he shut of f

    and

    pres-

    sure

    r egul at or val ve, suppl i es al cohol t o t he

    w ndshi el d

    out l et and

    radomenozzl es through

    a

    f i l t e r

    and

    t he t hr ee- way control

    val ve

    When

    t hesw t ch

    i s s e t t o

    RAD t he t hr ee- way val ve

    wi l l

    posi t i on

    t o suppl y

    a l -

    cohol

    f l o w

    t o t he

    radome onl y

    When t he sw t ch i s

    s e t

    t o

    OFF,

    t he shut -

    o f f

    and

    pressure

    r egul at or

    val ve

    wi l l

    c l o s e,

    t he

    t hr ee- way

    val ve wi l l

    r eposi t i on

    t o cut

    o f f f l o wandsystempressure wi l l

    bl eed

    o f f t hr ough

    t he

    pressure r e l i e f val ve

    L

    LOW

    AUTI ON

    LI GHT

    I l l umnat i on of t he amberL LOWi ght , l ocat ed on t he gl ar eshi el d

    annunci at or

    panel , i n d i c a t e s

    t he

    al cohol

    suppl y i n t h e r eser voi r

    i s l ow

    The

    r eser voi r

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    wi l l

    i l l umnate t he

    l i g h t t hr ougha

    r el aywhen

    i n t he f u l l down

    posi t i on

    When t he r e l a y i s ener gi zed, ahol di ng

    c i r c u i t

    i s

    a l s o

    ener gi zed

    t o

    pr event

    t he

    l i g h t

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    f l i c k e r i n g

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    t o

    t he

    bobbi ng

    mot i on o f t he

    f l o a t

    Thehol di ng

    c i r c u i t i s

    deener gi zed

    when

    t he

    BAT-

    TERYsw t ches a r e s e t t o OFFand t he

    al cohol

    r eser voi r

    i s

    f i l l e d

    com

    pl et el y f i l l e d

    r eser voi r

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    t he

    al cohol a n t i - i c e

    syst em w th

    appr oxi mat el y 45 m nut es

    o f al cohol

    f l o w

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    pr ot ecti on

    f o r

    both

    t he

    w ndshi el d

    and radome

    or

    appr oxi mat el y 2hour s

    f or

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    dome onl y

    PM121

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    P i l o t s

    Manual

    ear j et

    3 A

    PNEUMATIC

    I R PRESSURE

    ALCOHOLSUPPLY

    OVERBOARDVENT

    ELECTRCAL

    CHECKVALVE

    PRESSURE

    RELIEF

    VALVE

    ALCOHOL PRESSUREREGULATOR

    8

    SHUTOFF VALVE

    L OHOL

    ANTI -ICESYSTEM

    Roar

    6 4

    THREE WAY VALVE

    FILTER

    FLOAT

    SWTCH

    J

    Q

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    Z

    O

    >2W

    W

    O>

    m

    6

    2

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    Or i gi nal

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    Lear j et

    3 A

    Pi l ot s Manual

    PITOT STATIC

    N

    TALLW RNNGNTI ICE

    Ant i - i ce

    pr ot ec t i on f or t he

    p i t o t - s t a t i c probes,

    t o t a l

    t emper at ur e probe,

    and s t a l l war ni ng

    vanes,

    i s acc ompl i shed

    by

    ener gi zi ng

    i n t e gr a l e l e c -

    t r i c a l heat i ng

    el ement s

    i n

    each

    component

    The

    i ndependent

    p i t o t -

    s t a t i c

    probe, t o t a l t emper at ur e probe,

    ands t a l l war ni ng vane

    a n t i - i c e

    s yst ems consi st

    of cont r ol sw t ches, probe

    h e a t e r s

    wane

    h e a t e r s and

    p i t o t heat moni t or s Bot h l e f t

    and

    r i g ht

    syst ems u t i l i z e t he

    same

    PI -

    TOT

    HT

    l i g h t The

    p i t o t - s t a t i c

    probe

    heat i ng

    el ement s r ecei ve

    28 VDC

    t hr ough

    t he r espect i ve 15- amp

    L

    andRPTTO

    T

    HTc i r c u i t

    breakers on

    t he p i l o t s and

    c o p i l o t s

    c i r c u i t br eaker panel s

    Mot

    heat systemi s op-

    erat i ve

    dur i ng

    EMERBUSmode The

    t o t a l t emper at ur e

    probe

    heat i ng

    el ement

    r ecei ves

    28 VDC

    hr ough

    t he

    5 amp

    T T

    PROBE

    HT

    c i r c u i t

    breaker

    on

    t he

    p i l o t s c i r c u i t

    breaker

    panel

    The

    s t a l l

    warni ng

    vane

    heat i ng

    el ement s r ecei ve

    28

    VDC

    t hr ough

    t he r espect i ve 10- amp L

    andR

    STALLV NEHTc i r c u i t

    breakers

    ont he

    p i l o t s

    and c o p i l o t s

    c i r c u i t

    br eaker panel s

    PI TOT

    HEAT

    SWTCHES

    The

    p i t o t - s t a t i c

    heat s yst ems

    are i ndi vi dual l y

    cont rol l ed t hr ough t he

    MOTHEAT

    sw t ches

    i n t he

    ANTI ICE

    gr oup ont he center

    s w t c h

    panel

    Each

    s w t c h

    has

    twoposi t i ons

    On

    L or R) and

    OFF

    When

    t he

    LandRMOT

    HEATsw t ches ar e

    s e t

    t o On LandR) , power

    i s

    sup-

    p l i e d t o each

    p i t o t - s t a t i c

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    heater, each s t a l l warni ngvaneheater,

    andt he t o t a l t emper at ur e

    probe

    heater

    PI TOT HTLI GHT

    dual p i t o t heat moni t or

    systemi s

    i n s t a l l e d

    t o a l e r t t he

    p i l o t

    i f i nsuf -

    f i c i e n t

    current

    i s

    bei ng

    appl i ed

    t o

    t he

    p i t o t - s t a t i c

    probe

    heat i ng

    el e-

    ments The moni t or s

    ar e

    w r ed t o t he

    ground

    s i de of t he p i t o t - s t a t i c

    probe

    heat i ngel ement s

    Each

    moni t or

    i s basi cal l y

    a

    rel ay

    whi ch

    mai n-

    t ai ns

    an

    open

    c i r c u i t

    f o r t he PITOTHT l i g h t as l ong as s u f f i c i e n t cur-

    rent i s

    bei ng

    appl i ed t o t he

    associ at ed

    p i t o t - s t a t i c

    probe

    heat i ng el e-

    ment

    I n t he

    event

    of a

    mal f unct i on

    i n or l o s s of power t o t he

    associ at ed

    p i t o t - s t a t i c

    probe heat i ng

    el ement ,

    t he

    rel ay wi l l r el ease

    and

    compl et e

    t he

    PITOTHT

    l i g h t

    c i r c u i t

    I l l um nat i on

    of t he amber

    PI TOTHTl i g h t i n

    t he gl ar eshi el d annunci at or panel , i ndi cat es

    amal -

    f unct i on

    i n

    e i t he r

    t he

    l e f t

    or

    r i ght

    p i t o t - s t a t i c

    heat

    system

    or

    that at

    l e a s t onePITOTHE T

    s w t c h

    i s

    OFF

    PM 2

    6 3

    Change l

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    Lear j et

    31A

    OXYGEN

    SYST M

    The ai r c r af t oxygen system

    pr ovi des

    oxygen ser vi ce f or

    t he

    crewand

    passenger s Thesystemconsi st s of t he crewand

    passenger

    di st r i but i on

    syst ems,

    a

    hi gh- pr essur e

    oxygen

    st or age

    cyl i nder,

    a

    shut of f

    val ve

    and

    pressure

    r egul at or

    assembl y, an

    oxygen pr essur e gage,

    an overboard

    di schar ge r e l i e f val ve and i ndi cat or , an oxygen aner oi d sw t ch, a pas-

    senger

    oxygen

    cont r ol val ve,

    l anyar d actuated passenger

    mask

    oxygen

    val ves, andcrewandpassenger oxygenmasks El ec t r i cal power t o

    op-

    e ra te t he

    passenger

    oxygen cont r ol val ve i s suppl i ed through t he 75

    ampOXYVALVE

    ci r c ui t

    br eaker

    on t he pi l o t s c i r c ui t

    br eaker

    panel

    Oxygen

    i s avai l abl e

    t o

    t he

    crewat a l l t i mes and

    canbe

    made

    avai l abl e

    t o

    t he

    passenger s

    ei t her

    aut omat i cal l y

    above

    14, 000

    750

    f eet

    cabi n

    a l

    t i t ude,

    or

    manual l y at

    any al t i t ude

    through t he use

    of

    t he cockpi t con-

    t r o l s

    on

    t he p i l o t s

    si dewal l

    The

    oxygen

    system

    s desi gned

    f or

    use

    duri ng

    emergencydescent t o a cabi n al t i t ude

    not r equi r i ng

    oxygen

    and

    i s not t o

    be

    used f or

    extended

    per i ods of f l i g h t at cabi n al t i t udes r equi r -

    i ngoxygen

    or as

    a subst i t ut e f or t he normal

    pr essur i zat i on

    system

    Pas-

    senger masks

    w l l

    not

    pr ovi de suf f i c i ent oxygen

    f or prol onged

    oper at i on

    above

    34, 000 f e e t cabi n al t i t ude

    Prol onged

    oper at i on

    above

    25, 000

    feet cabi n al t i t ude wth passenger s onboard i s not recommend

    ed Smoki ng

    i s

    pr ohi bi t ed

    when

    oxygen

    i s

    i n

    use

    Ref er

    t o

    t he

    F

    Ap

    proved

    Ai r pl ane

    Fl i ght Manual f or l i m t at i ons and oper at i ng

    pr ocedur es

    OXYGENSTOR G N R SSUR

    R GUL TOR

    Theoxygenst or age

    cyl i nder

    has

    a

    st or age

    capaci t y of 4 cubi c f eet 1. 13

    cubi c met er s at

    1800 psi

    12, 411

    kPa The

    cyl i nder

    i s l ocat ed i n t he dor -

    sal f i n

    or

    t he

    r i ght

    si de

    of

    t he

    nose

    compartment

    The

    shut of f

    and

    pr es-

    sure

    r egul at or assembl y forms an i nt egr al

    par t of

    t he st or age

    cyl i nder

    and

    pr ovi des

    f or pr essur e r egul at i on, pressure i ndi cat i on, and servi c-

    i ng Oxygen pr essur e i s avai l abl e t o t he passenger andcrewdi st r i bu-

    t i on

    systems and i s r egul at ed

    t o

    a

    pressure

    of 6 t o 8 psi 418 t o 552

    kPa when t he oxygen cyl i nder shut of f val ve

    i s open The shut of f

    and

    pr essur e

    r egul at or assembl y

    al so i ncor por at es

    a

    bur st

    di sc pressure r e

    l i e f

    val ve t o

    di schar ge t he

    oxygen cyl i nder cont ent s

    overboard

    i n

    t he

    event that cyl i nder pr essur e r eaches 2700 t o psi 18, 617 t o 20, 685

    kPa Shoul d t he

    cyl i nder cont ent s

    be di schar ged over boar d, t he gr een

    overboard di schar ge

    i ndi cat or ,

    on t he

    out si de

    sur f ace

    of

    t he a i r c r a f t

    near t he st or age cyl i nder , w l l be ruptured or m ssi ng

    6- 14

    PM121

    Change

    3

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    ear j et

    3 A

    i l o t s

    Manual

    REW

    M SK

    OXYGENSYSTEM

    S HEM TI

    Fi gure

    6 5

    PM 2 6 5

    r i gi nal

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    Lear j et 31A

    OXYG NPRESSUREG G

    The

    oxygen pressure gage

    i s

    l ocat ed

    on

    t he

    p i l o t s

    si dewal l

    Thegage

    i s

    cal i br at ed

    from

    0t o

    2000

    psi Thegage

    i s

    a

    di r ect - r eadi ng t ype t h a t

    i s

    pl umbed

    t o

    t he

    hi gh- pr essur e

    si de of t he

    r egul at or

    and

    i ndi cat es

    oxygen

    cyl i nder

    pressure

    onl y

    OXYG NSYSTEM

    COCKPI T

    CONTROLS

    The

    oxygen

    systemcockpi t

    cont r ol s

    consi st

    of

    one

    cont r ol val ve, l a-

    bel ed

    PASSENGEROXYG NOFF AUTODEPLOY l ocat ed

    on

    t he

    p i l o t s

    si dewal l

    above

    t he

    armest

    Thecont r ol

    val ve

    cont r ol s

    oxygen

    a v a i l a b i l i t y

    t o t h e passenger

    oxygen

    di st r i but i on systemandpr ovi des

    aut omat i c

    or manual mode s e l e c t i o n

    Oxygen

    i s

    avai l abl e t o t he c rew

    oxygen

    di st r i but i on systemat al l

    t i mes

    when t he

    oxygen

    cyl i nder

    shut of f

    val ve

    i s open

    Cont r ol posi t i ons

    and

    system f unct i ons ar e

    as

    f ol l ows

    1

    Wth

    t he

    PASSENGER

    OXYGEN

    val ve

    i n t he UTOposi t i on,

    oxygeni s

    avai l abl e

    t o t he passenger di st r i but i on systemandt he

    aneroi d- cont r ol l ed

    sol enoi d

    val ve

    wi l l

    depl oy

    t he

    masks

    aut o-

    mat i cal l y

    Shoul d

    t he cabi n

    a l t i t u d e

    reach

    14, 000 750

    f e e t t he

    aner oi d swi t ch

    wi l l

    open t he

    sol enoi d

    val ve, t he passenger

    oxy-

    genmasks

    wi l l

    depl oy,

    and

    t he

    upper cent er panel

    l i g h t s wi l l l

    l um nat e

    t o

    pr ovi de

    maxi mum

    v i s i b i l i t y

    f or

    donni ng masks

    Nor mal l y, t he cont r ol shoul d

    be

    i n t h i s posi t i on

    2 Wth

    t he PASSENGEROXYG Nal ve i n t h e

    DEPLOY

    p o s i t i o n

    oxygen i s

    avai l abl e

    t o t he passenger di st r i but i on

    system

    and

    t he

    passenger

    masks

    wi l l

    depl oy

    The sol enoi d

    val ve wi l l be

    by-

    passed andal l ow

    oxygen

    systempressure t o depl oy

    t he

    passen-

    ger

    masks

    Thi s posi t i on can

    be

    used t o depl oy t he passenger

    masks

    at

    any

    cabi n

    a l t i t u d e andmust be

    used

    i f el ec t r i c al power

    i s unavai l abl e

    3 Wth t he PASSENGER

    OXYG Nal ve

    i n t he

    OFF

    p o s i t i o n oxy-

    gen

    i s not avai l abl e t o t he passenger di st r i but i on systemregard-

    l e s s

    of cabi n

    a l t i t u d e Thi s

    posi t i on

    can be used when

    oxygen i s

    r equi r ed f or t he c rewonl y

    6 16

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    Or i gi nal

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    A

    P i l o t s Manual

    PASSENGERMASKS

    Passenger

    oxygen

    masks

    ar e st owed i n compar tment s i n the cabi n

    c e i l i n g

    upper - cent er panel

    Whenever

    t he

    compartment

    door s

    open

    automat i cal l y

    PASSENGER

    OXYGEN

    AUTO

    or

    manual l y

    PAS-

    SENGER

    OXYGEN

    DEPLOY ,

    oxygen

    i s

    avai l abl e

    f or

    passenger

    use

    Passengers shoul d donmasks andmust

    pul l

    l anyard

    to

    i n i t i a t e

    oxy-

    gen

    f l ow

    An

    o r i f i c e i s i ncorporat ed

    i n t hemask to

    pr ovi de aconstant

    f l owof 4 1 l i t e r s per

    mnute

    The

    rebreather

    bagwi l l

    i n f l a t e at

    a

    seem

    i ngl y

    s l ow

    r a t e whenoxygen

    i s

    f l ow ng Thi s

    i s

    normal

    Shoul d t he

    compartment door be i nadver t ent l y

    opened

    from

    t he

    c o c kp i t pres-

    suremust be bl ed from

    t he systemby

    pul l i ng

    one

    of

    t he l anyar ds be-

    f o r e

    t he

    masks

    can

    be r est owed The

    compartment

    door s can

    be

    opened

    manual l y

    f or

    mask

    cl eani ng

    and

    ser vi ci ng

    by

    rel easi ng

    t he

    l a t c h

    l abel ed

    OXYGEN

    adj acent t o each

    door

    When t he

    door s

    ar e

    openedusi ng t h i s met hod

    nooxygen

    f l ow

    i s avai l abl e t o t he

    masks

    PASSENGER

    MASK

    Fi gure

    6 6

    PM 121

    6-17

    Or i gi nal

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    Lear j et

    31A

    REW

    M SKS

    The

    s t andar d

    6600214 s e r i e s ) f l i g h t

    crew

    masks

    ar e s t owed

    on

    straps

    behi nd t he p i l o t s andc o p i l o t s

    s e a t s

    Opt i onal

    S c o t t

    ATO

    M

    10- 15-

    0 1 ) f l i g h t crewmas ks , s t owed i n access i bl e

    storage r ecept acl es

    on

    t he

    p i l o t s

    and

    c o p i l o t s

    si dewal l s, may

    r epl ace

    t he s t andar d

    crew

    masks

    Thepressure

    demandmask

    r egul at ors pr ovi de f o r

    nor mal , 100

    96 oxy-

    gen and

    emer gency

    oper at i on r e f e r

    t o t he FAA

    Approved

    Ai r pl ane

    F l i ght Manual f or det ai l ed oper at i onal

    procedures)

    Each

    mask

    i n c o r -

    por at es a

    m cr ophone

    cont rol l ed

    byt he

    MCSELECT

    s w t c h ont he

    au-

    di o cont r ol panel s

    Ane l e c t r i c a l cord

    ext ends

    f r o meach mask and i s

    pl ugged i nt o t heOXYMC ack

    on

    t he j a c k

    panel

    Communi cati on

    be-

    tweencrew

    members

    can beaccompl i s hed by

    us i ng t heOXYf unct i on

    of

    t he

    MC

    SELECTs w t c h

    on

    t he

    audi o

    cont r ol

    panel s

    ressure de-

    t e c t o r i s i n s t a l l e d

    i n

    each

    maskoxygen s uppl y l i n e t o show

    v i s i b l e v e r -

    i f i c a t i o n of

    oxygen

    pressure

    t o t he mask

    qui ck- di s connect

    i s

    provi ded

    f or

    each

    crewmember When t he mask bayonet

    i nsert ed

    i nt o t he

    qui ck- di sconnect , aspr i ng l oaded

    poppet moves

    of f

    i t s

    seat

    and

    al l ows

    oxygenf l o w

    i nt o t hemask

    suppl y

    l i n e

    REWM SK66 214SERIES

    Fi gure

    6 7

    6 18

    PM121

    Change

    4

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    L ea r j e t

    A

    P i l o t s Manual

    PRESSURIZ TION

    SYSTEM

    Cabi n

    pr essur i zat i on i s

    pr ovi ded by

    condi t i oned

    a i r ent er i ng

    t he cabi n

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    di st r i but i on

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    and cont r ol l ed

    by modul at i ng

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    amount of a i r exhaust ed f r o mt he

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    Thepr essur i zat i on systemcon

    s i s t s

    of

    a

    cabi n

    pr i mar y

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    d i f f e r e n t i a l

    pressure r e l i e f val ves cabi n

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    a

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    aner oi d swi t ch

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    Power

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    CREWM SK SCOTT

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    P i l o t s

    Manual

    L ea r j e t

    3 A

    NORM L

    PRESSURI ZATI ON

    Normal pr essur i zat i on i s cont r ol l ed by

    r egul at i ng cont r ol

    pressure t o

    t he

    cabi npr i mar y

    out f l ow

    val ve

    The

    control

    pressure

    may

    be r e gu l a t -

    ed

    aut omat i cal l y by t he CABI NCONTROLLERor manual l y

    by

    t he

    manual

    UP DN

    control

    l ever

    r essur i zat i on

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    r egul at ed vacuum

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    pressure to

    operate

    t he

    val ve

    W t h t he

    squat

    s w t c h

    i n

    a i r mode and

    t he pr essur i zat i on AUTO

    M N

    w t c h

    i n AUTO t he

    a i r c r a f t

    pr essur i zat i on

    system s compl et el y

    i ndependent o f t he a i r c r a f t

    e l e c t r i c a l system I f

    t he

    a i r c r a f t i s

    i nadver t -

    ent l y

    al l owed t o ascend andexceed t he

    cont r ol l i ng

    l i m t s

    of t he pres-

    sur i zat i on c o nt r o l s

    t he nor mal d i f f e r e n t i a l

    pressure

    r e l i e f

    val ve

    wi l l

    cause

    t he

    pr i mar y

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    t o open

    and

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    a

    9 . 4

    psi 64

    . 8

    kPa d i f f e r e n t i a l

    Shoul d t he

    nor mal d i f f e r e n t i a l pressure r e l i e f

    val ve

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    7 psi 67 kPa d i f f e r e n t i a l Cabi n

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    servo

    pressure vacuum i ne s

    t o

    t he p r i -

    mary out f l ow val ve and

    cabi n safety

    val ve t o l i m t

    cabi n

    af t i t ude t o

    11, 500

    f e e t shoul d a d i f f e r e n t i a l

    r e l i e f

    val ve

    f a i l

    and

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    t he

    pr i mar y

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    s a f e t y

    val ve t o r emai n

    open

    Shoul d

    t he cabi n

    al -

    t i t ude

    reach

    11, 500 f e e t t he

    a l t i t u d e l i m t e r s wi l l

    vent

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    pressure

    t o

    t he

    pr i mar y out f l ow

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    and cabi n s a f e t y

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    chamber s

    causi ng

    t he

    val ves

    t o

    c l o s e

    Shoul d

    a

    r api d descent

    cause

    a

    negat i ve

    pressure i n t he cabi n, both t he

    pr i mar y

    out f l ow

    val ve

    and

    cabi n

    safety

    val ve

    w i l l open t o vent ambi ent at mospher i c pressure t o

    t he

    cabi n

    EMERGEN YPRESSURI ZATI ON

    I n t he event of nor mal cabi n a i r f l ow

    mal f unct i on,

    emer gency pressur-

    i zat i on i s pr ovi ded by r out i ng

    engi ne bl eed a i r

    d i r e c t l y

    i n t o t he

    cabi n

    t hr ough

    t he emer gency pr essur i zat i on val ves

    Emergency

    pr essur i za-

    t i o n

    i s accompl i shed aut omat i cal l yby

    pr essur i zat i on

    aner oi d sw t ches

    whent hecabi n

    a l t i t u d e i ncr eases

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    9500

    250

    f e e t

    or

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    s e t -

    t i ng t he BLEED

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    val ves wi l l

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    r egul at or val ve

    wi l l go

    t o t he l ow- pr essur e s e t t i n g duct i ng

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    l ow- pr essur e

    bl eed

    a i r d i -

    r e c t l y i n t o t he cabi n a i r

    si dewal l

    andf l o o r d i f f u s er s

    Thi s bypasses t he

    condi t i oned

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    t a i l c o n e

    areato maxi m ze

    t he

    i nf l ow

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    Theemer gency pr essur i zat i on val ves ar e deener -

    gi zed

    t o t he open

    pos i t i on f or

    emer gency a i r f l ow, andener gi zed

    cl osed

    f or

    nor mal

    bl eed- ai r

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    Each

    val ve

    i s

    i ndependent

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    t he ot her and,

    whenever

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    t emper at ur e control and

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    w ng, andw ndshi el d a nt i - i c e wi l l be unavai l abl e Oper at i ng power f o r

    emer gency

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    act uat i on

    i s

    28

    VD uppl i ed t hr ough

    ei t her t he

    7 5 -

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    and

    REMERPRESSc i r c u i t br eaker s on t he p i l o t s

    and c o p i l o t s

    c i r c u i t

    br eaker panel s Power f o r emer gency

    val ve act uat i on

    i s a v a i l -

    abl e dur i ng EMER

    BUS

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    6-20

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    e a r j e t

    3 A

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    P i l o t s Manual

    L ea r j e t

    A

    PRESSURI Z TI ON

    ONTROLS

    N

    NDC TORS

    BLEED I RSWTCHES

    The

    L

    and

    R

    BLEED

    IR

    swi t ches, l ocat ed

    on

    t he

    c o p i l o t s

    swi t ch panel ,

    cont r ol t he respect i ve l e f t and

    r i ght

    bl eed- ai r shut of f

    /pressure

    r egul a-

    t o r

    val ves

    on t he engi ne and l e f t and

    r i g ht

    emer gency pr essur i zat i on

    val ves i n t he

    bl eed a i r duct i ng

    Each BLEED

    I R

    swi t ch has t hr ee pos i -

    t i ons

    EMER ON and

    OFFWen

    a

    BLEEDIRswi t ch i s

    i n t h e

    ONo-

    s i t i o n ,

    t he r espect i ve bl eed- ai r

    shut of f / pr essur e

    r egul at or val ve wi l l

    openandt he emer gency

    pr essur i zat i on

    val ve

    wi l l

    r emai n cl osed unl ess

    t he 9500- f oot

    emergency

    pr essur i zat i on

    aner oi d swi t ches

    ar e act i vat ed

    WenaBLEED

    IR

    swi t ch

    i s s e t

    t o

    OFF,

    t he r espect i ve bl eed- ai r shut -

    of f /p ressure r egul at or

    val ve

    wi l l

    be

    ener gi zed

    t o

    t he

    cl osed

    pos i t i on

    Wen

    aBLEED IRswi t ch i s s e t t o

    EMER

    t he

    r espect i ve

    bl eed- ai r

    shut of f / pr essur e

    r egul at or

    val ve

    wi l l suppl y

    l ow- pr essur e

    bl eed

    a i r

    and

    emer gency pr essur i zat i on

    val ve wi l l

    be de- ener gi zed

    open The

    bl eed- ai r

    shut of f / pr essur e

    r egul at or

    val ves

    control

    bl eed

    a i r f l o w

    t o t h e

    cabi n a i r d i s t r i b u t i o n and t emper at ur e

    control

    system

    wng

    a n t i - i c e

    system

    and

    wi ndshi el d a n t i - i c e syst em

    The

    bl eed- ai r shut of f /pressure

    r egul at or

    val ves wi l l c l o s e

    aut omat i cal l ywhenever

    t he r espect i ve

    ENG

    FI RE

    PULL

    T

    handl e

    i s

    pul l ed

    Bl eed- ai r f or

    wi ndshi el d

    al cohol

    t ank

    pr essur i zat i on i s

    s t l l

    avai l abl e

    wi t h

    t he

    shut of f / pr essur e

    r egul at or

    val ves

    cl osed

    TheBLEED IRswi t ches

    r emai n

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    dur i ng

    EMER

    BUS

    mode

    BLEED I R

    W RNNG

    LI GHTS

    RedBLEEDI R

    L

    and

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    IR

    Rwar ni ng l i g h t s

    on

    t he gl ar eshi el d

    annunci at or

    panel ,

    pr ovi de

    t he

    cr ew wi t h

    vi sual

    i ndi cat i on of a

    pyl on

    over heat

    condi t i onor

    pyl onbl eed

    a i r

    duct i ng

    over heat condi t i on

    Each

    l i g h t i s

    oper at ed by

    a t her mal swi t ch i n t he associ at ed

    pyl on

    bl eed- ai r

    duct i ng or

    a

    t her mal swi t ch i n t he associ at ed

    pyl on

    j u s t

    af t of t he f o r -

    ward engi ne

    mount

    The

    duct i ng t her mal

    swi t ches

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    t emper at ur e shoul d

    reach

    645 10 F 34 1 [S 5 ] C ) The

    pyl on

    t her mal

    swi t ches

    wi l l

    i l l umnat e the

    r espect i ve l i g h t i f

    t he t emper at ur e i n

    a

    py-

    l on exceeds

    250 5 F

    121

    [ 2. 7 ] C )

    The

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    wi l l openand

    t he a f -

    fected BLEEDIR

    Li ght

    wi l l ext i ngui sh as t he

    pyl on

    cool s

    6- 22

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    L ea r j e t

    A

    P i l o t s

    Manual

    C BAI R

    SWTCH

    TheC B

    AIRswi t ch on t he

    pr essur i zat i on cont r ol panel cont r ol s

    t he

    c abi n a i r

    f l o w

    control val ve

    and

    t he

    pr essur i zat i on system

    cabi n

    safety

    val ve

    Dur i ng gr ound

    oper at i on

    when

    t he

    CAB

    AIRswi t ch

    i n

    t he

    OFF

    p o s i t i o n

    t he nor mal l y cl osed

    vacuumshut of f sol enoi d ener

    gi zed

    open

    t hr ough

    r el ays

    i n t he squat swi t ch

    r e l a y

    panel

    andr egul at ed

    vacuum r om

    t he

    pr essur i zat i onvacuum

    egul at or

    w i l l open

    t he

    cabi n

    safety

    val ve When

    t he C BAIRswi t ch i s s et ON

    t he vacuumshut of f

    sol enoi d de ener gi zed

    al l owi ng t he

    safety val ve

    t o dr i ve cl osed un

    der

    i ncr easi ng cabi n

    pressure

    C B

    AI R

    LIGHTOPTIONAL

    Anamber

    CABAIR i ght

    may

    be

    i n s t a l l e d on t he gl ar eshi el d

    annunci

    a t o r panel whi ch

    i l l umnat es when t he C B

    AIRswi t ch i s

    i n t he

    OFF

    pos i t i on Thi s l i g h t

    serves

    t o

    r e mnd

    c re w

    members t o swi t ch C B

    AIR

    on

    pr i or t o t akeof f

    PRESSURIZATION

    UTOM NSWTCH

    The

    UTOM N

    swi t ch

    on

    t he pr essur i zat i on cont r ol panel

    pr ovi des

    aut omat i c

    andmanual

    mode

    s e l e c t i o n

    f or nor mal pr essur i zat i on When

    t he swi t ch

    i s s e t t oMAN, sol enoi d val ves

    i n t h e r egul at edvacuumi ne s

    ar e ener gi zed

    t o

    remove

    r egul at ed vacuum

    f r o m

    t he

    CABINCON-

    TROLLERandappl y

    r egul at ed

    vacuum o t he

    manual

    control

    val ve

    The

    control

    val ve

    i s manual l y oper at ed by

    t he

    r edUP-DN

    cont r ol l ever

    When t he UTOM N

    swi t ch i s s e t

    t oAUTO t he

    sol enoi d

    val ves

    de

    ener gi ze and a l l o w

    r egul at ed

    vacuum o t he CABINCONTROLLER

    f o r

    aut omat i c pr essur i zat i on

    control

    Nor mal l y

    t he

    UTOM N

    swi t ch

    r emai ns

    i n

    t he

    UTO

    pos i t i on

    CABIN

    CONTROLLER

    W t h t he

    C BAIR swi t ch ONand

    t he pr essur i zat i on

    UTOM N

    swi t ch AUTO

    t he

    CABIN

    CONTROLLER, l ocat ed

    on

    t he

    pr essur i za

    t i o n

    control

    panel w i l l aut omat i cal l y control

    cabi n a l t i t u d e

    The

    con

    t r o l l e r

    senses cabi n

    a l t i t u d e and r at e of cl i mb and aut omat i cal l y

    modul at es

    t he

    pr i mar y

    out f l ow

    val ve

    by

    r egul at i ng cont r ol

    servo

    vac

    uumpressure

    Pr i or

    t o t a k eo f f t he

    a l t i t u de s el e c t o r

    knob

    on

    t he

    f a c e

    of

    t he c o n t r o l l e r shoul d

    be s e t

    t o s e l e c t e d

    crui s i ng

    a l t i t u d e

    or

    desi r ed

    cab

    i n

    a l t i t u d e

    TheRATE

    knob

    may

    be

    rotated t o s e l ec t

    and

    mai nt ai n

    a

    com or t abl e

    pr essur i zat i on

    r a t e f o r

    ascent or descent For descent

    and

    l andi ng

    t he

    a l t i t u d e s e l e c t o r

    shoul d

    be s e t t o l andi ng f i e l d

    el evat i on

    PM 121

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    P i l o t s

    Manual

    L ea r j e t

    31A

    PRESSURI ZATI ON

    M NU L

    CONTROLLEVER

    UP-DN

    Wth

    t he C B

    AI R

    swi t ch ON

    and

    t he pr essur i zat i on UTOM N

    swi t ch

    i n

    MAN

    cabi n

    pr essur i zat i on i s

    cont r ol l ed

    by

    t he r ed UP DN

    manual

    control l ever

    on

    t he pr essur i zat i on cont r ol panel The l ever

    cont r ol s servo vacuum

    pressure

    t o

    t hepr i mar y

    out f l owval ve

    t hr ough

    amanual

    control

    val ve

    As t he l ever i s moved t owar ds UP out si de

    s t a t i c a i r

    pressure

    i s vent ed

    t o

    t he out f l ow val ve control

    chamber

    causi ng t he

    val ve

    t o

    open

    Whent he l ever i s movedt owar ds

    DN

    cab-

    i n

    pressure i s vent ed

    t o t he

    out f l ow val ve control

    chamber

    causi ng

    t he val ve t odose

    CABIN

    ALT/ DI FF PRESSG GE

    The

    cabi n

    a l t i me t e r / d i f f e r e nt i a l pressure

    gage,

    ont he

    pr essur i zat i on

    cont r ol panel ,

    i s vent ed

    t o

    both out si de a i r pressure

    and

    cabi n

    a i r

    pressure The

    i ndi cat or

    has two

    poi nt er s,

    each t r a v e l s over a separ at e

    cal i br at ed

    scal e Thel ar ge

    poi nt er sweeps over

    t he

    out si de

    scal e t o

    i n-

    di cat e

    cabi n a l t i t u d e

    The

    CABI NALT

    s c a l e

    i s

    marked f r o m0 t o

    50, 000 f e e t

    i n 1000- f oot i ncr ement s

    The

    smal l poi nt er

    sweeps

    over t he

    i nsi de

    s c a l e

    t o i ndi cat e

    d i f f e r e n t i a l pressure

    i n psi

    TheD FF

    PRESS

    scal e i s

    marked

    f r o m

    0

    t o

    10

    psi i n02- psi i ncr ement s

    CABINCLIMBI NDCATOR

    The

    r a t e

    of

    change i n

    cabi n

    pressure al t i t ude i s i ndi cat ed i n f e e t per

    m nut e

    ont heCABI NCLI MB

    i ndi cat or l ocat ed

    on t he

    pr essur i zat i on

    control panel

    The i ndi cat or f ace i s

    marked

    f r o m

    0

    t o 6000 f e e t per

    m nut e

    i n both UPandDOWNdi r ecti ons The i nst r ument

    f unct i ons

    si m l ar l y t o t he a i r c r a f t

    v e r t i c a l speed

    i ndi cat or but i s

    vent ed t o

    cabi n

    pressure

    onl y

    EMER

    PRESS

    OVERRDESWTCHES

    Emergency pr essur i zat i on

    over r i de swi t ches

    ar e

    pr ovi ded

    t o al l ow

    takeoffs and

    l andi ngs

    a t f i e l d el evat i ons hi gher t han t he emer gency

    pr essur i zat i onaner oi d swi t ch

    s e t t i n gs 9500

    [ 15 0 ]

    f e e t Theswi t ches

    ar e l ocat ed

    on

    t he

    c o p i l o t s

    swi t ch panel

    and

    ar e

    l abel ed EMER

    PRESS

    OVERR DE -

    NORM L

    LandRWth

    t he

    swi t ches

    i n OVERR DE po-

    s i t i o n ,

    t he

    emer gency

    pr essur i zat i on

    aner oi d swi t ches ar e

    e l e c t r i c a l l y

    i sol at ed f r o m t he

    emer gency

    pr essur i zat i on

    val ves

    t hus pr event i ng

    t he

    val ves f r o mopeni ng when t he aner oi d swi t ches a c t i v a t e When

    t he

    over r i de swi t ches

    ar e i n t he NORM L

    p o s i t i o n ,

    act uat i on of t he

    aner oi d swi t ches wi l l open

    t he

    emer gency

    pr essur i zat i on

    val ves The

    swi t ches wi l l

    have

    no

    e f f e c t

    t he BLEED

    AIRswi t ches

    ar e i n t he OFF

    or

    EMER

    pos i t i on

    6- 24

    PM 121

    Or i gi nal

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    L ea r j e t

    3 A

    P i l o t s Manual

    CASALT

    LI GHT

    Shoul d t he

    cabi n

    a l t i t u d e exceed 8750 250

    f e e t , an

    aneroi d swi t ch

    wi l l

    cl ose

    t o

    i l l um nat e t he

    amber

    C

    ALTl i g h t

    on

    t he

    gl ar eshi el d

    an-

    nunci at or panel

    The

    aneroi d

    swi t ch wi l l a l s o deact i vat e t he

    UTO

    pr essur i zat i on

    mode

    t o

    stop t he cabi n

    a l t i t u d e

    f rom

    r i s i n g

    any

    hi gher

    t he

    mal f unct i on

    was i n

    t h a t

    cont rol

    system The

    aneroi d swi t chw l l

    r e -

    s e t a t a l ower

    cabi n a l t i t u de ,

    r eener gi zi ng t he aut omat i c cont r ol system

    andext i ngui shi ng

    t he

    CABALTl i g h t

    CABN

    ALTI TUDE

    WRNNGHORN

    cabi n

    a l t i t u d e

    aur al

    war ni ng hor n wi l l sound t o a l e r t t he crewshoul d

    t he cabi n

    a l t i t u d e

    reach

    10, 100 250

    f e e t

    The

    hom

    s

    cont r ol l ed

    by

    an

    aneroi d swi t ch

    whi chwi l l appl y a

    gr ound t o t he

    warni nghorn

    c i r c u i t

    when act uat ed The

    cabi n

    a l t i t u d e

    war ni ng

    horn

    c i r c u i t

    i s tested

    t hr ough

    t he syst em t e s t swi t ch

    on

    t he

    p i l o t s

    i nst r ument

    panel

    The

    MUTE

    swi t ch on t he

    r i g h t

    t hrust

    l ever

    maybe used

    t o i nt er r upt t he

    hor n

    f or

    appr oxi mat el y 60

    seconds

    i n t he

    event

    t he hor n sounds

    The

    cabi n

    a l t i t u d e

    war ni ng hor n i s

    operat i ve

    dur i ng EMERBUSmode

    SYSTEM

    TEST

    SWTCHC IN

    ALT

    FUNCTION

    The

    rotary-type

    system t e s t swi t ch on

    t he

    p i l o t s i nst r ument

    panel

    i s

    used

    t o t e s t t he cabi n

    a l t i t u d e

    war ni ng

    system Rot at i ng

    t he swi t ch t o

    CABNALTanddepr essi ng t he swi t ch PRESSTESTbut t on

    wi l l pr o-

    vi de a

    gr ound

    si mul at i ng

    t he

    10, 100- f oot aneroi d swi t ch

    act uat i on

    Dur i ng t he t e s t sequence,MUTE

    swi t ch

    operat i onmay

    a l s o be

    checked

    ARCONDTIONNGND

    HE TING

    Pr i mar y heat i ng and

    cool i ng i s accompl i shed by cont r ol l i ng

    t he

    t em-

    perat ur e

    of

    t he

    bl eed

    a i r

    ent er i ng t he

    cabi n

    a i r di str i but i on

    syst ems

    On

    a i r c r a f t 31- 035

    thru

    31- 190, an R f r eon- based cool i ng syst em i s i n -

    s t a l l e d t o

    pr ovi de

    addi t i onal

    cool i ng

    a t

    a l t i t u de s bel ow

    35, 000

    f e e t

    and

    dur i ng ground

    operat i ons Ona i r c r a f t

    31- 191

    and

    subsequent , an

    R 4A

    r ef r i ger ant - t ype cool i ng system i s i n s t a l l e d

    t o

    pr ovi de

    addi t i onal cool -

    i ng

    An

    auxi l i ar y

    e l e c t r i c a l )

    cabi n

    heat i ng systemi s

    i n s t a l l e d

    t o

    pr ovi de

    addi t i onal

    cabi n

    heat i ng,

    i f

    r equi r ed

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    Lear j et 31A

    PRM RY

    HE TINGNDOOLNGBLEED R

    Cockpi t

    andcabi n t emper at ur e i s

    r egul at ed

    bycont r ol l i ng t he

    t emper -

    ature of

    t he pr essur i zat i on

    bl eed

    a i r

    ent er i ng t he

    cabi n

    a i r di st r i but i on

    system

    Wth

    t he

    BLEED

    AI Rswi t ches ON

    and

    t he

    CAB

    AI Rswi t ch

    ON engi ne

    bl eed

    a i r i s

    a d m t t e d

    t o t he rama i r heat exchanger

    t hr ough

    a f l o w

    cont r ol

    val ve

    The

    bl eed

    a i r

    i s

    cool ed

    i n

    t he

    heat

    ex-

    changer by ram

    i r

    ent er i ng t he

    dorsal

    i n l e t passi ng t hr ough t he

    ex-

    changer ,

    and

    then e x i t i n g i n t o t he

    t a i l c o n e

    The

    condi t i oned bl eed

    a i r

    then

    passes out

    of t he exchanger i n t o t he

    cabi n

    a i r di st r i but i on duct s

    The

    t emper at ur e o f t he

    condi t i oned

    ai r

    i s

    cont r ol l ed by t he hot

    a i r

    by-

    pass

    H)

    val ve Thi s

    val ve bypasses

    some

    of

    t he

    bl eed ai r ar ound

    t he

    heat exchanger and

    mxes

    d i r e c t l y wi t h

    t he condi t i oned

    a i r

    exi t i ng

    t he

    heat

    exchanger

    H- val ve

    p o s i t i o n

    t hus,

    t emper at ur e

    r egul at i on,

    i s

    cont r ol l ed byt he

    pneumat i cal l y oper at ed

    t emper at ur e

    cont r ol

    system

    Whenever t he cabi n

    t emper at ur e

    UTOM Ne l e c t o r knob i s r ot at -

    ed

    t o AUTO

    t he t emper at ur e cont r ol l er wi l l

    aut omat i cal l y

    mai nt ai n

    t he

    t emper at ur e

    set wi t h

    t he t emper at ur e

    s e l e ct o r

    Wth

    t he

    mode

    se-

    l e c t o r i n

    UTO

    andt he HOT COLDt emper at ur e s e l e c t o r knob s e t

    t o

    COLD he t emper at ur e

    s e l e c t o r

    needl e val ve

    opens

    and r educes t he

    pressure t o

    t he cabi n

    t emper at ur e sensor The

    decreased pressure

    causes t he

    cabi n

    t emper at ur e

    sensor

    bl eed

    pat h

    t o

    open

    and

    al l ows

    t he

    sensor t o vent more

    of t he pressure t o

    ambi ent

    The

    decr eased

    pressure

    al l ows

    t he H

    val ve t o cl os e andr out es bl eed

    a i r t hr ough

    t he

    heat exchanger ,

    then

    i n t o

    t he

    cabi n

    at a l ower t emper at ur e When t he

    t emper at ur e s e l e c t o r

    i s

    s e t

    t o HOTt he

    t emper at ur e

    s e l e c t o r needl e

    val ve

    cl oses and

    r a i s e s t he pressure t o t he

    cabi n

    t emper at ur e sensor

    The

    i ncr eased pr essur e

    caus es t he cabi n

    t emper at ur e

    s ens or bl eed

    pat h

    t o cl ose

    and i ncr eases pressure t o t he

    al ve

    The i ncr eased

    pr es s ur e al l ows t he

    H- val ve

    t o

    openand

    bypass

    more

    hot

    a i r

    i n t o t he

    cabi n

    di st r i but i on

    system

    The

    cabi n

    t emper at ur e

    sensor s

    f an

    bl ows

    cabi n

    a i r

    acr oss t he sensor, and causes t he sensor t o

    met er

    more or

    l e s s

    pressure,

    dependi ng

    on t he t emper at ur e

    of

    t he

    cabi n

    a i r and t he

    sel ect ed t emper at ur e The

    t emper at ur e sensor

    f an

    i s

    i noper at i ve

    when

    t he

    COOL OFFswi t ch i s s e t t o COOL When t he mode s e l e c t o r i s s e t

    t o MAN t he

    cabi n

    t emper at ur e

    sensor and

    duct t emper at ur e sensor

    ar e

    removed

    from he system and

    t he

    pressure

    t o

    t he H- val ve

    i s con-

    t r o l l e d

    d i r e c t l y by

    t he

    HOT COLDt emper at ur e s e l e ct o r

    Set t i ng t he

    t emper at ur e s e l e c t o r t o

    COLD

    bl eeds of f

    a

    greater amount of t he reg-

    ul at ed

    pressure

    and

    al l ows

    t he

    H- val ve

    t o

    route

    more

    bl eed

    a i r

    t hr ough

    t he

    heat

    exchanger

    Set t i ng t he t emper at ur e

    s e l e c t o r

    t o HOT

    cl oses t he

    bl eed

    pat h and

    i ncr eases t he

    pressure

    at t he

    H- val ve

    The

    val ve

    opens

    and

    bypasses more bl eed

    a i r d i r e c t l y

    i n t o t he

    cabi n

    a i r

    di st r i but i on

    duct s

    6 26

    PM 2

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    31A

    i l o t s Manual

    CA N

    DSTRWION

    BLEED

    AIR

    TALCONEBLEEDARDSTRIBUTION

    Fi gure 6 10

    CABIN

    OBTIBBuno

    CONDTONED

    AIR

    PM 121

    6 27

    r i gi nal

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    Lear j et 31A

    C BAI R

    SWTCH

    The

    C BAI Rs wi t c h, l oc at ed

    on

    t he pr es sur i z at i on c ont r ol panel ,

    con-

    t r o l s

    t he f l o w

    control val ve

    Wth t he

    BLEEDAI R

    swi t ches ON s e t -

    t i n g

    t he

    C B

    AI R

    s wi t c h

    ON

    wi l l

    de- ener gi ze t he

    f l o w

    control

    val ve

    cont r ol l i ng

    s ol enoi d and

    al l ow

    systempressure t o

    t he val ve s cont r ol -

    l i n g chamber s I n t e r n a l

    pressures

    w i l l pos i t i on t he

    val ve

    b u t t e r f l y

    cont r ol l i ng bl eed

    ai r f l o w t o

    t he

    heat exchanger

    Set t i ng t he

    C B

    AI R

    s wi t c h ONal s o ener gi zes

    t he c abi n

    t emper at ur e

    sensor bl ower

    S e t -

    t i n g

    t he

    C B

    AI R

    s wi t ch OFF

    wi l l

    ener gi ze

    t he val ve control

    s ol enoi d

    whi ch wi l l

    shutoff control pressure

    and a l l o w

    t he val ve

    b u t t e r f l y

    t o

    bl ock

    bl eed ai r

    f l o w

    UTOM N

    SELECTOR

    An AU PO-MANmode

    s e l e c t o r

    l ocat ed on t he c o p i l o t s s wi t c h panel ,

    pr ovi des

    f or aut omat i c

    or

    manual

    mode oper at i on

    of t he c abi n

    t em

    perature

    control

    system

    Wen

    i n

    UTO

    mode

    t he

    system

    t emper a-

    t ur e cont r ol l er s

    aut omat i cal l y

    posi t i on t he

    H- val ve

    but t er f l y I n t he

    M Nmode t he HOT- COLD

    s el e c t o r d i r e c t l y

    r egul at es t he

    H- val ve

    cont r ol l i ng

    pressure

    HOT- COLD

    TEMPERATURE

    SELECTOR

    The HOT- COLD t emper at ur e s e l e c t o r l ocat ed

    on

    t he

    c o p i l o t s

    s wi t c h

    panel

    I n

    systemUTOmode

    t he

    t emper at ur e s e l e c t o r i s used

    t o

    s e l e c t t he desi r ed

    cabi n

    t emper at ur e t o be mai nt ai ned

    aut omat i cal -

    l y

    by

    t he

    t emper at ur e

    control

    system

    I n M N

    mode

    t he t e