BOMBARDIER DASH 8 Q400 STANDARD STANDARD OPERATING OPERATING PROCEDURES PROCEDURE S
REV 2 24/10/15 p.1
Pre-flight Preparation Befor Before e commen commencin cing g a fligh flight, t, thoro thoroug ugh h prepar preparati ation on shoul should d be compl complete eted d to ensure safe and efficient flying. Preparation for the flight includes checking of: • Route • Weather (Departure, destination, enroute, alternates! • "#$%&s • 'ompany notices • uel figure
Fuel preparation )t is *B++ policy for the - to uplift, in addition to the re/uired trip fuel, at least 01 contingency fuel (that is to say, an additional 01 of the calculated trip fuel! and a MINIMUM final reser2e figure of 400g! "o *B++ - flight should land 3ith less than -kg of fuel on board. "aturally, the final reser2e fuel and the contingency fuel can both be increased at the 'aptain4s discretion, taking into consideration any 3eather or operational limitations. $he standard ta5i fuel figure for the - is 6kg though once again, more can be added if the 'aptain anticipates a long ta5i (e.g. %&7 or 'D8!. $ankering fuel is acceptable, though it is company policy to land 3ith no "ore than 9,6kg of fuel on board unless in e5ceptional circumstances. +5planation for landing 3ith greater fuel /uantity may be re/uired. %lternate airports should be chosen on the basis of 3eather, "#$%&s and pro5imity. )t may also be prudent to choose lybe bases or destinations as alternates 3here possible for operational ease (for e5ample, Bristol or +5eter 3ould be good good alternates alternates for 7outhampton 7outhampton,, depending depending on 3eather"#$ 3eather"#$%&s!. %&s!.
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At the aircraft aircraft #n arri2al at the aircraft, the captain should ensure: ; Pins and co2ers are sto3ed ; Parking Brake set to P%R< ; "a2 =ights set to #"
External Inspection Described in a seperate document
First Flight Check )f it is the first flight of the cre34s day, or their first flight on a particular aircraft, then then a firs firstt flig flight ht chec check k must must be comp comple lete ted. d. $he $he safe safety ty chec check k incl includ udes es 2erification
of
the
presence
of
the
re/uisite
safety
e/uipment
and
documentation. $he circuit breaker panels must also bechecked thoroughly.
$he 'ockpit Preparation panel scan starts from the top left of the o2erhead panel (D' +lectrical panel! and mo2es in a W shape to the top right (%' +lectr +lectrica icall panel! panel!.. $her $hereaf eafter ter,, the scan scan starts starts from from the 'aptai 'aptain4 n4s s left lefthan hand d console, the glareshield, main instrument panel, pedestal and irst #fficer4s console, finishing at the o5ygen gauge.
$his is an e5panded checklist, checklist, but also includes all items found during the panel scan. 8reen items appear on the checklist, 3hilst blue items are ones that should be completed but do not appear on the checklist. $he scan should be done first, and then supplemented by the checklist (i.e. not readanddo!.
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#O#$PI% PREPARA%ION D#'>&+"$%$)#"........................................................'?+'< Check presence of aerodrome/enroute charts, OFP, checklist & manuals 7%+$@ +>)P&+"$....................................................'?+'< Goggles, extinguishers, axe, life ackets, escape hatch, flashlights, fire glo!es, h"draulic handpump =D8 8+%R A P)"7........................................................'?+'< Open #AI$ %A$I$G GEA' A%(E'$A(E 'E%EA)E OO' and check that #AI$ %G 'E%EA)E *A$%E in normal position+ Close the door+ Ensure %A$I$G GEA' E(E$)IO$ I$*I-I( ).I(C* set to $O'#A% and red guard closed+ Ensure %A$I$G GEA' A(E'$A(E E(E$)IO$ OO' on floor0 1 green lights are illuminated, then close+
O&ERHEAD PANE' +"8)"+ )"$%<+ D##R7.............................................#P+" Am2er OP$ %ights on o!erhead panel B%$$+R)+7...................................................................'?+'<+D -A(( #A)(E'/#AI$/A3/)(-4 should all 2e O$+ 5oltages need to 2e checked .ith E( P.' connected, -att should 6 7895 for engine start, or 885 if starting on 2atter" po:er onl"0+ (emperatures should not exceed 8; degrees+ &%)" B>7 $)+................................................................$)+ )'+ PR#$+'$)#" A W)"D7?)+=D..........................................................7+$ All s:itches should 2e OFF, I$(A
%A$I$G and (AI lights should 2e off+ +=$......................................................................................%>$# =)8?$ D%$% R'DR.........................................................8"D $+7$ Check that F%( A(A 'ECO'E' light on C.P goes out, then place s:itch 2ack to $O'#+ PD %=$)&+$+R >")$7..................................................%7 RD Altimeter units in Europe are in F(, though if operating in regions :ith metric altimetr", F( = # can 2e used+ )R+ D+$+'$)#" %"D 7&#<+....................................$+7$+D DO NOT TEST APU FIRE PROTECTION if the AP3 is running+ Press AP3 FI'E (E)(+ Ensure illumination of • AP3 F3E% 5A%5E C%O)E :hite light • AP3 -(% A'# am2er light • AP3 FA3%( am2er light • AP3 FI'E red light • AP3 caution light • AP3 E(G light • AP3 FAI% light • C*EC< FI'E E( :arning flashing0 • #A)(E' CA3(IO$ & #A)(E' .A'$I$G lights flashing0
Press E$GI$E > and su2se?uentl" E$GI$E 8 FI'E (E)( E(EC(IO$ s:itch+ Check for each@ • P3%% F3E%/*4 OFF handle illuminates • FA3%( A and FA3%( - ad!isor" lights illuminate • C*EC< FI'E E( :arning light illuminates • #A)(E' .A'$I$G light illuminates p.5
• E$GI$E FI'E lights flash • Fire :arning 2ell rings Ensure that the E$GI$E FI'E lights are depressed at least once during these tests, to ensure that the fire 2ell silences+
Press -AGGAGE )#O
............................................................#" GP3 should 2e used :here!er possi2le, as AP3 is expensi!e and nois"+ For AP3 )tart@ • Press P.' on AP3 CO$('O% panel+ Ensure AP3 F3E% 5A%5E OPE$ ad!isor" light illuminates • Press )(A'( on AP3 panel+ Ensure )(A'(E' am2er ad!isor" light illuminates, then extinguishes • .ait for green '3$ light and GE$ .A'$ light+ • Press GE$ ):itch and ensure GE$ O$ light illuminates+ Once running, check AP3 GE$ on #F Electrical page is at around +1 max >+0+ -us !oltage should read around 8B5+ +"8)"+ 7$%R$ P%"+=....................................................7+$ IG$I(IO$ ).I(C*E) should 2e in $O'# Engine selector should 2e centred and )tart p/2 2lank+ '%B)" %=$)$>D+ '#"$R#=7.........................................7+$ A3(O/#A$/3#P should 2e A3(O CA-I$ A%(I(3E FO'.A' O3(F%O. kno2 should 2e rotated full" anti p.6
clock:ise )et %anding Ele!ation of destination airport using %G A%( kno2
+$+R)#R =)8?$7 (C!....................................................7+$ a" 6 All off except PO)$ lights0 $ight 6 All on except anticollision light until 2efore engine start0 +&+R =)8?$7.................................................................%R& %7$+" B+=$7"# 7&#<)"8......................................%7 RD#" $O )#O$ %D*7R@ 73itch...........................................$+7$ (est caution and ad!isor" lights+ Particularl" important are@ = Fire and detection panel lights • eice and antiice lights • PO.E'E F%IG*( CO$('O% )*3(OFF lights • %A$I$G GEA' lights • AP I)E$G light • #A)(E' .A'$I$G & #A)(E' CA3(IO$ lights )ome lights :ill not illuminate during the test, including@ E$GI$E )E%EC(, E$GI$E )(A'(, CA-I$ A%(I(3E FA3%(, A%(E'$A(E PI%O( .IPE' O$+ Furthermore, the F3)E%AGE OO') light :ill not illuminate if the passenger or 2aggage doors are open+ B=++D %)R A C...............................................................# -%EE) > & 8 should 2e OFF and -%EE ):itch set to #I$+ %P> B=++D.......................................................................%7 RD p.7
O $O( use AP3 -%EE until 8 mins after AP3 '3$ green light illuminates+ B>7 *#=$%8+...................................................................'?+'< R+')R' %".......................................................................#"
PR+77P%'<7....................................................................7+$'?+'<+D Packs should 2e in A3(O (E#P CO$('O% for CA-I$ set to F/A and set for COC
#AP%AIN SIDE PANE' 8PW7 #*+RR)D+..............................................................."#R& Ensure s:itch is 2lank and guarded+ $# W%R" $+7$..................................................................$+7$ Check audio tone sounds %D' $+7$ A C...................................................................$+7$ Ensure A%( FAI%, IA) FAI% and I5)I FAI% flags remo!ed from PFs For each test,ensure@ • Altimeter sho:s >D,19ft on PF • Altimeter setting sho:s *pa • #aximum Operating )peed displa"s as 8BD kts • )A( 6 >; degrees and .(G8 FAI% legend appears on E • IA), IA) #I)#A(C* & A%( appear on PFs+ • PI(C* ('I# & E%E5A(O' FEE% caution lights illuminate • O!erspeed :arning tone sounds after ; seconds • (CA) FAI% legend appears momentaril" on PFs and #Fs+ 7$%== W%R")"8.................................................................$+7$ p.8
*old each test for at least > seconds+ Ensure@ • 'A increases to greater than ;ft • 'A decreases to ;ft • )tick shaker acti!ates • >80 )(A%% )4) FAI% and P3)*E' )4)( FAI% caution lights illuminate "#7+W?++= 7$++R)"8...................................................# $ose:heel #3)( remain off until push2ack is complete and the to: 2ar has 2een disconnected, so as to a!oid nose:heel unit damage+
('ARESHIE'D =)8?$$%)........................................................................$%) 7$)'< P>7?+R and +=+*%$#R $R)& 7?>$#.............."#R& (hese selectors should 2e 2lank '=#'<................................................................................7+$ Check chrono and E( reset, and that correct 3(C time sho:n 8PW7 $+7$.........................................................................$+7$ Check@ • P3%% 3P and -E%O. G/) ad!isor" lights illuminates • G%IE)%OPE and P3%% 3P aural :arnings sound If time permits, the GP.) (E)( p/2 can 2e depressed for longer than three seconds+ (his :ill test all GP.) associated aural tones+ If the test is not satisfactor", :ait 1 seconds 2efore repeating+ P'7................................................................................."#R&%= All PFC) s:itches should 2e 2lank and pushed out+ ?7) 7+=............................................................................#"7)D+ 7+=+'$+D *)I )E% p/2 should 2e pressed to toggle the fl"ing *)I+ If Captain is Pilot p.9
Fl"ing, there should 2e an 7*)I message on the First Officers PF+ If First Officer is PF, the *)IH message should 2e sho:n on Captains PF+ 7B@ '#&P%77...............................................................'?+'<+D
MAIN INS%RUMEN% PANE' 7P++D B>87.................................................................7+$ *, *R, *C, *R) and *'=)&B bugs should be set according to tables%urasim calculation. %=$)&+$+R7.................................................................7+$ )et local $* and crosscheck altimeter indication :ith pu2lished airfield ele!ation+ D?&D%.....................................................................7+$ $?R>7$ R+D>'$)#" )et #A 2ug for the thrust reduction, :hich is >ft AA% default0+ >Ft = aerodrome ele!ation+ PD.................................................................................'?+'< #ake sure no red flags are present and that all necessar" na!igation aids are presented on E*)I+ &D................................................................................'?+'< Check all pages to test for functionalit"+ )tandard prestart presentation is E%EC('ICA% page on Captains #F and OO') page on First Officers page+ 7$%"DB@ )"7$R>&+"$..............................................'?+'< Ensure correct $* and altitude sho:n on stand2" instrument+ +D.................................................................................'?+'< Check fuel ?uantit" and temperature and all maintenance messages are 2lank+ =%"D)"8 8+%R...........................................................'?+'< Ensure le!er do:n and %EF(/$O)E/'IG*( green lights indicated+ %/' & $ p.10
OO' am2er lights ma" also 2e sho:ing+ *old (E)( s:itch and listen for gear :arning horn+ 8PW7 =%P..................................................................%7 R+>)R+D )et for destination landing flap >; or 1;0+ 7$B@ ?@D PR+77P$> ?@D E9 )7#= *%=*+..................."#R&%= #ake sure all s:itches are off and 2lank+
PEDES%A' &7.......................................................................................#"'?+'<+D (urn 2oth F#) computers on+ Check data2ase !alidit" and press ACCEP(+ P)$'? %"D R#== D)7'#""+'$.........................................)" -oth "ello: handles should 2e pushed in+ $%"< %>)=)%R@ P>&P7...................................................# -oth 2uttons should 2e off and 2lank+ Confirm on the #F Fuel page+ >+=....................................................................................'?+'<+D $ransfer should be #. uantity should be crosschecked 3ith light Plan. )mbalance bet3een tanks should be no greater than C6Ckg. 7$B@ *? P%"+=...............................................................# '*R.....................................................................................'?+'<+D %>$#+%$?+R..................................................................$+7$ • CO$ %E5E') 6 F3E% OFF • PO.E' %E5E') 6 I)C epress A3(OFEA(*E' s:itch+ #essages on E@ • A/F )E%EC( • 3P('I# • I(( and $* increase • $(OP changes to $(OP p.11
• (or?ue rating increases • A/F A'# increases • 3P('I# disappears • #(OP changes to $(OP and tor?ue ratings decrease+ • A/F (E)( PA)) message After test complete, deselect A3(OFEA(*E' p/2+ If the test fails, maintenance must 2e carried out and the flight #3)( $O( CO$(I$3E + +&+R8+"'@ BR%<+..........................................................7+$ A '?+'<+D -rake le!er should 2e set to park and sufficient pressure should 2e !erified on *4'A3%IC page+ At least ; P)I is re?uired+ '#"$R#= =#'<.................................................................. #" P#W+R =+*+R7..................................................................D)7' '#"D =+*+R7.....................................................................>+= # %R'D> A C..............................................................................#" A 7+$ )et na!igation and A(C fre?uencies re?uired for departure+ (CA) test must 2e carried out first flight of the da"+ (o do this, select (CA)+ Press EP and line select against (E)(+ .ait for (CA) )4)(E# (E)( O< aural tone+ $R)&7....................................................................................'?+'<+D (est ele!ator trim for full and free tra!el+ 'eturn to (/O range+ Ele!ator trim needs to 2e set as follo:s@ (A1+BBJ+++++++++++++++++++++++++3)E AF( E$ of (/O 'ange (A
Aileron@ -riefl" release control lock and c"cle through range+ (hen set needle to centre and engage control lock+ 'udder@ C"cle through range+ (hen reset to one needle :idth to the right to p.12
counteract "a:ing motion from propeller :ash on takeoff0 R%D%R..................................................................................#
)IRS% O))I#ER*S ('ARESHIE'D '=#'<..................................................................................7+$ 7$)'< P>7?+R+=+*%$#R $R)& 7?>$#....................."#R& ):itches should 2e off and 2lank %"$)7<)D.............................................................................#" ):itching the Anti)kid to O$ :ill start a selftest process+ Ensure that the I$- A$(I)
)IRS% O))I#ER*S SIDE PANE' #RW%RD #>$=#W *%=*+............................................."#R&%= #@8+" PR+77..................................................................'?+'< Ox"gen should 2e in the green gauge+ #inimum dispatch is >1 P)I+
BE)ORE S%AR% F#) )etup $he route stipulated on the #perational light Plan should be inserted into the &7, along 3ith published 7)D and 7$%R procedures 3here applicable. When filling the &7 fuel plan, the P%77+"8+R7 section should remain at Fero and the correct +&P$@ W+)8?$ should be inserted. $raffic load for the flight should be inserted in the '%R8# section. )nsert the alternate fuel for the selected alternate aerodrome, and the final reser2e fuel (usually e/ui2alent to 9 minutes flying time! should be inserted in the ?#=D section.
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Fuel Crosscheck )n >+= #" B#%RD, insert ramp fuel minus the ta5i fuel (usually 6kg!. 'rosscheck that the 8R#77 W+)8?$ section automatically sho3s aircraft takeoff 3eight. #nce this check is complete, reinsert actual ramp fuel figure into >+= #" B#%RD section. 8R#77 W+)8?$ should no3 sho3 the aircraft4s ramp 3eight. &7 routeing can be crosschecked using the P=%" display on the &D. $his is optional but can be useful for spotting erroneous flight plan points.
'adio $a!igation -ackup )f flying a prescribed 7)D routeing, pilots should back up the &7 flight plan by tuning the radio aids stipulated on the departure charts.
Instrument )etting P)D • lags not present • ?eading matches 7B@ compass • ?D8 B>8 matches departure run3ay heading • 7peed bugs set *, *R, *C, *R) and *'=)&B • *#R A %D set and displayed on ?7) (as re/uired! • D? blank • &D% should display acceleration altitude (default G ft %%= unless other3ise stated on aerodrome chartscompany procedures • %ltimeters should be set to local "? and ele2ation should be checked 3ith published aerodrome ele2ation M)D • $oggle through the 2arious pages checking for functionality p.14
• 'aptain4s &D should be set to +=+' • irst #fficer4s &D should be set to D##R7 ED • 'onfirm fuel figure agrees 3ith #P • 'heck sensible engine parameters and indications • 'heck "$#P set A(I) %$)7 for the local aerodrome should be recorded and re2ie3ed
(akeoff ata $akeoff data can be obtained using the published *B++ - charts or by using the +B pro2ided by %urasim. Weights and 3eather information inserted into the +B should be crosschecked thoroughly, as 3ell as po3er and flap settings. >se the 7P++D B>8 selector to set *, *R, *C, *R) and *'=)&B. $he filled in triangle represents *R) (flap retraction speed!, 3hilst the hollo3 triangle represents *'=)&B. %l3ays crosscheck all data for accuracy before departure. "$#P 3ill be used for all departures and bleeds 3ill usually be left in the &)"#" position for takeoff, unless performance tables do not permit this.
eparture clearance #btain departure clearance from %$'. #nce obtained, set the altitude selector and transponder appropriately. )f %$' are not a2ailable ()*%#*%$7)&!, announce departure intentions on >")'#& using format H('%==7)8"! $rafficI. KEGP* ('FC, -EE95A, *B, )tand 88, Push2ack and )tart for EGAC, (%A9C departure r:" 8DL+
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BE)ORE S%AR% #HE#$'IS% '#'+=.............................................................................+R #, $@JJJJJJ Check fuel transfer s:itch centred+ Ensure fuel im2alance does not exceed 8M8kg and that 5A%5E OPE$ lights on F3E% )4) page are not sho:ing+ Ensure sufficient fuel ?uantit" for the flight+ BR%<+PR+77>R+.........................................................#",PR+77 '?+'<+D Ensure E#E'GE$C4/PA'+= # %"$)7<)D............................................................................#" %=$)&+$+R7........................................................................"?JJJ 7+$ '?+'<=)7$ '#&P=+$+
)tarting :ith AP3 )f using the %P> for electrical po3er on startup, ensure %P> 8+" is selected #" and B= %)R selected # (%P> Bleed must "#$ be operating during engine start!.
)tarting :ith External Po:er )t is preferable to start 3ith 8P> connected 3here possible. $his can be done by starting the first engine on stand. Pushback can the commence and, 3ith the use of the &%)" B>7 $)+, the running engine generator can be used to pro2ide po3er for the second engine start.
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)ingle Engine (axi )f a single engine ta5iout is anticipated, engine C should be started first.
Clearance %l3ays ensure start clearance from %$' has been obtained. %lso make a 2isual confirmation out of side 3indo3s that the engine areas are clear before engine start.
-atter" )tart 7tarting on batteries is not an appro2ed standard procedure, but may be performed in e5ceptional circumstances 3here neither %P> or 8P> are a2ailable. $here must be at least CC* bus 2oltage for battery start.
------------#'EAR %O S%AR%------------$R)&7................................................................................7+$ Ensure Ele!ator trim is set in takeoff range and according to the aircrafts CG+ Aileron trim should 2e neutral 'udder trim should 2e > needles :idth to the right to counteract "a:ing motion :hen takeoff po:er is applied+ D##R7...............................................................................'=#7+D Confirm on OO') )4) page that all fuselage doors are closed+ Flight deck door should 2e closed+ "#7+W?++= 7$++R)"8...............................................# (his #3)( 2e selected off prior to push2ack to a!oid structural damage+ B>87...................................................................................7+$ 'ead out 2ugged 5>, 5', 58, 5F'I and 5C%I#-+ Ensure set correctl" on 2oth sides+ p.17
Crosscheck 2ugged acceleration altitude on #A 2ug+ P%77+"8+R 7)8"7...........................................................#" %"$)'#==)7)#".................................................................R+D %P> B=++D..........................................................................# B>7 *#=$7........................................CK* (CC* for Battery 7tart! '?+'<=)7$ '#&P=+$+
S%AR% PRO#EDURE • +ngine areas confirmed clear and bus 2oltages checked • 7elect start s3itch to EC (E! • 7$%R$ light illuminates • Depress 7$%R$ s3itch • %t first indication of "? on +D, set condition le2er to 7$%R$+%$?+R • &onitor )$$ and oil pressures (should increase to green!
IF NO LIGHT UP WITHIN 10 SECONDS '#"D le2ers to >+= #
ABNORMAL START $his includes: L "o )$$ indication after fuel selected #" • ?ot start ()$$ goes abo2e MC degrees! • "? decreasesdoes not increase • "o oil pressure or oil pressure belo3 -- P7) )n these circumstances, abandon engine start )&&+D)%$+=@ by selected '#"D le2ers to >+= # and deselecting start s3itch.
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$ormal Engine )tart #nce "? stable abo2e K-1, +"8 #)= PR+77 3arning, +"8 >+= PR+77 and +"8 ?@D P>&P cautions all e5tinguished, call 47$%B=+ 7$%R$4. Repeat process for ne5t engine.
DO NO% pla+e #OND le,er to MA. /hilt on or near tan area! All peronnel an e12ip"ent MUS% 3e +lear 3efore MA. i ele+te!
A)%ER S%AR% EN( 56 +$ PWR%P>.................................................................# Ensure external po:er s:itch OFF and AP3 is deselected+ (o deselect AP3, first s:itch off GE$ s:itch+ Green GE$ O$ light should extinguish+ (hen press P.' s:itch and ensure ad!isor" lights extinguish and F3E% 5A%5E C%O)E ad!isor" illuminates+ R%D%R..............................................................................7B@ o not select radar to O$ until :ell clear of ramp area & personnel+ >+= P>&P7....................................................................#" R>DD+R............................................................................'?+'<+D Ensure full and free tra!el on the rudder+ For first flight of the da", make a full and free check+ (hen s:itch '3 > P3)* OFF s:itch O$+ Check full and free+ eselect '3 > P3)* OFF s:itch+ 'epeat :ith '3 8 P3)* OFF s:itch+ Ensure all PFC) s:itches are 2lank 2efore taxiing+ "#7+ 7$++R)"8...............................................................#" Once to: 2ar disconnected, select steering to O$ ?@DR%>=)'7.....................................................................'?+'<+D Pressures should 2e checked sufficient 8B1 )tand2", 81> #ain > p.19
& 80 uantities should 2e at least ;J epress *4 1 I)O% 5A%5E+ Ensure am2er ad!isor" illuminates+ $o+1 s"stem should sho: 8D1> P)I+ E%E5 P'E)) caution should appear+ Check ele!ator for full and free tra!el+ eselect *4 1 I)O% 5A%5E and place small ele!ator input to depressurise s"stem 1+ =%P7..................................................................................JJJ 7+$ Ensure flap position set for takeoff+ D+)'+ PR+77>R+.............................................................'?+'<+D Check pressure on First Officers side panel+ )elect (E)( on P'OP ICI$G s:itch and ensure 2oth green lights illuminate+ Once complete, return to OFF position+
Singl Engin T!"i Do not ta5i single engine o2er an acti2e run3ay. +nsure both engines are started before crossing acti2e run3ays. +ngine C should be started first to supply hydraulic pressure. +nsure +ngine C '#"D le2er set to &% before ta5i. Rudder inputs can be used to augment nose3heel steering to stop un3anted mo2ements to the left 3ith +ngine C started. +ngine should be started in good time for takeoff and should be stabilised and running for at least t3o minutes before takeoff po3er is applied. +ngine should be run in 7$%R$+%$?+R for at least 9 seconds before running '#"D le2er to &%.
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A)%ER S%AR% EN( 76 #HE#$'IS% +=+'$R)'%= P%"+=...........................................................'?+'<+D -atteries should all 2e on+ E( P.' should 2e OFF #AI$ -3) (IE should 2e OFF+ '#"D)$)#" =+*+R7..........................................................&% %>$#+%$?+R...................................................................7+=+'$ Ensure :hite )E%EC( light illuminates+ PD&D+D........................................................................'?+'<+D A 7+$ Check for failure messages+ Captain and F/O #Fs should no: 2e selected to $A5+ B=++D7.............................................................................#"&)" (#R %7 RD! Ensure 2leeds set as per takeoff data calculations+ $ormall" O$/#I$ should 2e set+ '?+'<=)7$ '#&P=+$+
%A.I $a5iing should al3ays be performed 3ith $%) light selected #". %ny re2erse ta5iing or pushback is 7$R)'$=@ prohibited. Wing inspection lights should also be used at night or in conditions of poor 2isibility. $a5i speed should not e5ceed 9 kts straight line and 0 kts in turns. $ight turns (M degrees or more! should be performed at &% kts. $ry not to 4ride4 the brakes against po3er, as this increases 3ear and brake temperatures.
p.21
BE)ORE %A$EO)) #HE#$'IS% BR%<+7.................................................................................'?+'<+D Ensure 2rakes appl" efficientl" and s"mmetricall"+ $# W%R")"8........................................................................$+7$+D )elect (/O .A'$ s:itch and ensure aural tone does not sound+ $# P#W+R..........................................................................."$#P =$ )"7$R>&+"$7.............................................................'?+'<+D Ensure correct indications and no flags #ake sure 2ugs set correctl" .hilst turning, check '#I, E*)I, magnetic compass and turn/slip indicators for correct indications+ )lip indicator should mo!e in OPPO)I(E direction to turn+ EAI and stand2" artificial horiNon should remain erect+ =)8?$ '#"$R#=7...........................................................'?+'<+DR++ isengage control lock+ Check ailerons and spoilers mo!e through full tra!el+ SIM NOTE # T$ M%C &400 n'()$l (*+ing i( ,'n*+'ll- . *$ ,'n*+'l ,'ln '+ !il+'n !"i( A ,'n*+'l ,$,3 )ill l!- *' n)!n*- 'n*( 'n *$ *!"i)! (' i* i( +,'n-- *' 6+7'+ 7ll !n- 7+ ,$,3 !* '+ n!+ (*!*i'n!+ @%W D%&P+R..................................................................#" '%B)"...............................................................................7+'>R+ '?+'<=)7$ '#&P=+$+
p.22
----------#'EARED %O 'INE UP--------=)8?$7.............................................................................7+$ %anding lights should 2e O$ Anticollision should 2e .*I(E $R%"7P#"D+R...............................................................7+$ Ensure correct s?ua:k code and A%(/O$ set '%B)" 'R+W....................................................................W%R"+D C"cle FA)(E$ -E%() sign to :arn ca2in cre: of pending departures P)$#$ 7$%$)'..................................................................#" Ensure PI(O( )(A(IC s:itches are on and C.P cautions are extinguished+ &%..............................................................8%, ?D8, %=$ 7+= 'WP..................................................................................B=%"< '?+'<=)7$ '#&P=+$+
%A$EO)) $he takeoff should be commenced 3ith the 3ind in mind (check 3indsock, sim 3eather indications or listen to 3ind 2ectors gi2en by %$'!. $his is to ensure proper directional control during takeoff. )t also ser2es as a reminder for a reNected takeoff in the e2ent of a fire, as fires should al3ays be kept do3n3ind of the fuselage 3here possible. %d2ance po3er le2ers smoothly and note that takeoff po3er is set. "ote that % %R& annunciation appears on +D. If thi oe not o++2r R+O+'$ $%<+# )&&+D)%$+=@. %t *R, rotate gently and follo3 flight director bars. When positi2e climb is established, select landing gear >P and note that gear lights e5tinguish. $he initial climbout should be performed at a &)")&>& speed of *CL kts. *C p.23
is only the minimum speed during single engine climb. %t 0ft %%=, lateral modes may be selected on the light 8uidance Panel.
INI%IA' #'IMB %t acceleration altitude: • 7elect lap ero (ensure abo2e *R)! • +ngage autopilot (if re/uired ; hand flying is acceptable but %P greatly reduces 3orkload! • Bleeds should be set to #""#R& (or &% if re/uired!. 'heck amber B=++D indication on +D • '#"D =+*+R7 set to M. %fter flap retraction, engage )%7 mode and climb at C kts (or as re/uired ; standard profile is C kts!.
%$+R $%<+# '?+'<=)7$ =%"D)"8 8+%R....................................................................>P =%P7...................................................................................+R# B=++D7................................................................................#"A"#R&&% Onl" select #A :ith full passenger load+ (his setting increases fuel consumption+ '=)&B P#W+R.....................................................................7+$ '?+'<=)7$ '#&P=+$+
p.24
#'IMB "ote 3hen passing &inimum 7afe %ltitude. #nce transition altitude is reached, set 9 on both PDs. 7tandby altimeter remains 9 until passing ,ft (=!. 'heck both altimeter indications correct and synchronised. 'abin cre3 are released, once aircraft has climbed abo2e &7%, using the %R'D> '?)&+ button. Pressurisation system should be checked for normal operation. $his check must also be performed e2ery ,ft in climb and descent.
)tep clim2s )f aircraft le2els off before reaching cruise altitude, speed can be allo3ed to increase to *&# C kts. When cleared to a higher le2el, use small and gradual changes to allo3 aircraft to climb 3ithout making Nolting mo2ements or rapid, uncomfortable pitch changes. (+.g. 3hen le2el at K, and cleared to =0 3hilst aircraft flying at *&# C, set ne3 altitude and )%7 &ode for *&# 9 initially, rather than reducing )%7 selection immediately to C knots. $his 3ould cause rapid and uncomfortable pitch mo2ements.! 'limb in *7 mode is NO% PERMI%%ED.
p.25
'=)&B '?+'<=)7$ %=$)&+$+R7..................................................................7$D 9 PR+77>R)7%$)#".........................................................'?+'<+D 7$B@ ?@D A P$> '"$R=..............................................B=%"< Ensure 2oth s:itches are pushed out and off >+= P>&P7..................................................................B=%"< Ensure 2oth s:itches are pushed out and off %>$#+%$?+R..............................................................# Ensure A3(OFEA(*E' push2utton 2lank '?+'<=)7$ '#&P=+$+
#RUISE >se &7 estimations on >+= or P+R page to establish 3hether the aircraft 3ill reach destination on time, late or early. )f late, use *&# kts as the cruise speed. )f time is not a problem for the flight, *&# C can be used to sa2e fuel.
REMEMBER9 *&# ; kts is the &%)&>& permissible cruise speed.
7elect cruise po3er 3ith condition le2ers *+R@ '%R+>==@ to a2oid inad2ertent feathering. #ne &D should al3ays ha2e $+RR selected, and the &7% of the flight plan route printed on the #P should al3ays be considered. &onitoring C.0 from time to time on *?C is good airmanship. % fuel check should be made against #P predictions at least e2ery C minutes. )n addition, the &D system pages should be re2ie3ed for correct indications. Pressurisation system indications, hydraulic system, ice protection and o5ygen indications must also be checked at least e2ery C minutes in the cruise. p.26
DES#EN% Descent planning can be made by using the &7 *"%* page. %ll descents should be planned to be continuous or nearly continuous, 3ith po3er as close to idle as possible. 7et the *"%* page using altitude restrictions published on the 7$%R. )f there is no published 7$%R or altitude restrictions, the *"%* page should be used to plan to be at 0ft 3ith 0 track miles remaining. $he *$# page 3ill sho3 the descent rate from present position to each *"%* 3aypoint. %pproach radio aids should be tuned, 7$%R routeing set in the &7, $#D point calculated and approach charts re2ie3ed and briefed before descent if possible.
• 7et &D% (or D? for '%$ )) approach! • 7et arri2al "? on standby instruments • Re2ie3 safety and transition altitudes for arri2al • 'heck fuel and crosscheck 3ith #P for alternate re/uirements • 'rosscheck landing 3eight on #P 3ith prediction on &7 >+= page • >se %urasim or performance charts to calculate *R+ (solid triangle! A *'=)&B (hollo3 triangle! • 7et aerodrome ele2ation on pressurisation panel • 7et radio aids and applicable inbound course for each • Re2ie3 missed approach procedure and ta5i procedure for arri2al • Re2ie3 goaround acceleration altitude (ft %%= dual engine!
p.27
DES#EN% #HE#$'IS% PR+77>R)7%$)#".....................................................7+$ Aerodrome ele!ation set on ca2in altitude selector+ =;ft if landing :ith 2leeds off+ 8PW7 =%P P#7)$)#"..............................................JJJ 7+$ )et s:itch to Flap >; or 1;+ 7%+$@$R%"7)$)#" %=$7.......................................R+*)+W+D BR)+)"8B>87.................................................R+*)+W+D7+$ '?+'<=)7$ '#&P=+$+
Descent should be flo3n at C9 )%7 3ith po3er as near to idle as possible. Do not forget to use %=$7+= mode for e2ery altitude or le2el change.
*olding ?olding procedures should be completed at a minimum of 6 kts.
APPROA#H #nce cleared to an altitude, set the local "? on both altimeters and crosscheck. %t this point, au5iliary fuel pumps should be turned on (green!, 7$B@ ?@D A P$> '"$R= turned on, %>$#+%$?+R should be selected. =anding lights must be s3itched on belo3 ,ft (=!. Passenger signs must be on by =.
p.28
APPROA#H #HE#$'IS% %=$)&+$+R7.............................................."? JJJJ 7+$ >+= P>&P7.............................................#" 7$B@ ?@DP$> '"$R=.............................#" P%77+"8+R 7)8"7..................................#" Passenger signs must 2e on 2" >,ft F%>0 '%B)"..........................................................7+'>R+ '?+'<=)7$ '#&P=+$+
'ANDIN( =anding is completed using lap 0 or 90. Because lap 90 produces cumbersome flight control beha2iours, and also increases fuel consumption during final approach, it should only be used 3hen operating into short run3ays (i.e. belo3 Qm =D%!. Reduced "P should be used 3hene2er practicable. $his is achie2ed by selecting RD' "P push button on pedestal and then selecting '#"D le2ers to &% 3ithin C seconds. $his should be completed after landing gear e5tension. Do not use reduced "P if: • %ntiskid inoperati2e • "ose3heel steering inoperati2e • 8round spoilers inoperati2e • Performing a steep approach • Performing a single engine approach • Performing a '%$ )) approach • =anding on ,er: 3et or contaminated p.29
%anding )chedule Q <$7 (CQ miles!.....................=%P 0 6 <$7 (Q0 miles!.......................8+%R D#W" (9 greens! .......................R+D>'+D "P'#"D =+*+R7 &% .......................B=++D7 #"&)" ......................%7$+" B+=$7 7)8" '@'=+D ......................&)77+D %PPR#%'? ?D8%=$ B>87 7+$ K <$7 (0- miles!.......................=%P 0 ......................=%"D)"8 '?+'<7 9 miles G Reduce to *R+.
%pproach should be flo3n at *R+, or *R+ L in turbulence.
By 0ft R?, the aircraft &>7$ be stabilised. $his includes: • 'orrect flight path • #n run3ay centreline • %t *R+ (no more than L0kts! • *7 less than ftmin • 8ear do3n • =anding flap set • =anding checklist complete • Po3er setting )f these conditions are not met, the missed approach must be carried out. #nce established on the glidepath, aircraft must not de2iate more than one dot on localiser or glidepath. % nonprecision approach must be flo3n 3ithin 0 degrees of published inbound course. p.30
)t has been pro2en that closing the throttles 3hilst flaring on the - 3ill cause a 2iolent touchdo3n. Po3er 3ill be needed throughout the flare until main 3heels touch do3n, at 3hich point =)8?$ )D=+ should be used. 'heck PR#P+==+R 8R#>"D R%"8+ ad2isories illuminate. Do not flare too high and do not forget that a missed approach is al3ays an option, e2en at 2ery lo3 heights. #n nose gear touchdo3n, po3er le2ers into D)7'. 'heck 7P#)=+R7 ad2isory lights illuminate. %t K kts, engage control locks. Re2erse thrust is certainly not to be used in ordinary circumstances, as placing po3er le2ers into D)7' 3ill pro2ide enough drag for deceleration. )n emergency situations, ho3e2er, re2erse thrust can be used to slo3 the aircraft as /uickly as possible. 'ANDIN( #HE#$'IS% =%"D)"8 8+%R..........................................D#W" 9 8R++"7 '#"D)$)#" =+*+R7..................................&% )elect #A+ If using reduced $P, select 'C $P 2efore selecting #A+ B=++D7......................................................%7 RD 3suall" O$/#I$+ =%P7........................................................JJJ 7+$ '?+'<=)7$ '#&P=+$+
or diagrams of specific approach types, refer to pilot library page on the *B++ 3ebsite.
p.31
(O-AROUND 8oarounds can be tricky in this aircraft, so it is important to re2ie3 the missed approach procedure thoroughly before commencing the approach. )t should be completed smoothly and carefully, 3ithout huge pitch changes or 2iolent control mo2ements. $o initiate a goaround, press the goaround s3itches on the po3er le2ers. $his sets the flight director bars to a pitch of M degrees nose up. 7moothly apply full po3er and retract the flaps by one stage. %t confirmation of positi2e rate of climb, select the landing gear up. 7elect heading and %=$7+=. DO NO% e5ceed flap limiting speeds. %t acceleration altitude, select laps ero, autopilot, Bleeds #n"orm and set 'limb Po3er to M. 'arry out the %$+R $%<+# '?+'<=)7$.
A)%ER 'ANDIN( %s soon as aircraft lea2es the run3ay, select anticollision lights to R+D and landing lights #. =)8?$$%) s3itch is set to $%). When appropriate, deselect fuel pumps, %>$#+%$?+R and 3eather radar. Retract the flaps and select &%)" B>7 $)+ to #". )f re2erse thrust 3as not used for landing, +ngine E can be shutdo3n immediately. 7elect E po3er le2er to 7$%R$ A +%$?+R for 9 seconds and then to >+= #. E bleed can then be selected #. +ngine shutdo3n 3ill cause cautions and 3arnings 3hich should be checked for anomalies. $he #78 test should be carried out according to the procedure stipulated on the p.32
"#R&%= '?+'<=)7$. $his only needs to be done after the last flight on 7aturday night or if re/uested by technical personnel. %$+R =%"D)"8 '?+'<=)7$ '#"$R#= =#'<7...........................................................#" =)8?$7.............................................................................7+$ Anticollision to 'E, landing lights OFF+ =%P7..............................................................................+R# &%)" B>7 $)+..................................................................$)+ =)8?$$%).....................................................................$%) )'+ PR#$+'$)#"............................................................# .indshield heat off+ All fuselage, tail, :ing and propeller icing protection should 2e deselected+ P)$#$ 7$%$)'...................................................................# (his :ill pro!oke cautions :hich should 2e checked+ @%W D%&P+R...................................................................# W+%$?+R R%D%R............................................................7$B@
SHU%DO;N %s the aircraft approaches the stand, s3itch off the $%) light. 'heck hydraulic pressures and note any failures. #nce parked, set +&+R8 BR%<+ to P%R< and carry out shutdo3n checks. 8P> can be re/uested and connected once '#"D le2ers are set to 7$%R$+%$?+R. +nsure 8P> connected on +=+' 7@7 page and then select +$ PWR s3itch to #". Propellers should be set to 7$%R$+%$?+R for 9 seconds before selecting >+= #. p.33
7?>$D#W" '?+'<=)7$ BR%<+..............................................................................7+$ >+= P>&P7...................................................................# ?@D P>&P A P$> '"$R=..............................................# PWR'#"D =+*+R7...............D)7'7$R$ A $?R (9 seconds! "#7+W?++= 7$++R)"8...............................................# R%D%R............................................................................# $R%"7P#"D+R$'%7..................................................C 7B@ +"8)"+ B=++D7..........................................................# A &)" %P>8P>......................................................................#" Ensure AP3 started O' GP3 connected+
1 )ECO$) )(A-I%I)(A(IO$ CO#P%E(E
'#"D =+*+R7...........................................................>+= # P%77+"8+R 7)8"7..................................................# %"$)'#==)7)#"........................................................# '?+'<=)7$ '#&P=+$+
SE#URE When lea2ing the aircraft, the secure checklist should be used. )"$%<+ D##R7.........................................................'=#7+D R+')R' %"..............................................................# +&+R8+"'@ =)8?$7..............................................# B%$$+R)+7...............................................................# )R7.............................................................................# %"$)7<)D.................................................................# Don4t forget to submit the P)R+P using 7&%R$'%R7 before ending the flight. or reference to specific approach type diagrams, lo3 2isibility procedures, icing p.34
