FINNAIR
CARAVELLE III .2
MI : Magnetic Indicator.
Transition altitude = when altitude unit change from feet (8000ft)
to flight level (FL 80) (defined by ATC or maps)
Transition Level = when altitude unit change from flight level (FL 80)
to feet (8000ft) (defined by ATC or maps)
_________________________________________________
Plane in cold start configuration.
COCKPIT PREPARATION
·
Parking
brake..........................................................On ( Ctrl + ;)
· Gear lever..........................................................DOWN
·
Speedbrakes
lever.....................................RETRACT
· TADG IIS..................................................................OFF
Electrical panel
:
· GENERATORS POWER SOURCE SEL..............PLANE BAT
· ALTERNATORS POWER SOURCE SEL.............PLANE ALT
- To power with
Ground Power Unit–
·
ASK FOR CONNECTION
(Click onto area)
· GENERATORS POWER SOURCE SEL..............DC GND PWR
· ALTERNATORS POWER SOURCE SEL.............AC GND PWR
Main panel (inverters) :
· EMERG INVERT.....TEST ...................................MI WHITE
......switch back to OFF.....MI BLACK....then switch to....ON
· MAIN INVERT..............................................................NORM
·
·
·
·
Upper panel UP2 :
· AIR INTAKE LIGHTS........................................As req.
· TRANSPONDER....................................................ON
Hydraulic panel :
· RED circuit
pressure..................................Checked (2500 psi)
· RED (red) pump switch......................................OFF
· YELLOW pumps tests................................Checked
Servo Controls :
· YELLOW SELECTOR ..............................NEUTRAL (center)
·
PRINCIPAL SELECTOR...............BLUE & GREEN(center)
·
ARTIFICIAL FEEL
SELECTOR............................ON
Pedestal :
· Flight Director Selector......................................... SB (Stand By)
Main panel :
· Flight controls....................Follow up..........Checked
· MARKER HI-LOW selector......................................HI
· IAS & Machmeter...................................................Zero
·
PDI...................................................................Flag OFF
· ADI......................FD (Flight Director)..G (Gyro) Flags
· Turn indicator............................................All centered
·
Altimeter..........................................................Checked (QNH
baro)
·
Vertical Speed
indicator.......................................Zero
·
OIL
TEMP........................................................Checked
·
OIL
PRESS.............................................................Zero
·
TEMP
indicator..............................................Checked
·
RPM.........................................................................Zero
· ENGINE TEMP C°(EGT)...............................Checked
·
FLAPS
indicator.....................................................Zero
· SYNCHRO...............................................................OFF
· JPT REG switch......................................................OFF
·
FUEL
FLOW............................................................Zero
· FUEL
USED ...........................................................Zero
·
FUEL
QUANTITY.............................................Checked
· Gear position indicators................................Checked
Upper panel UP2
· NAV LIGHTS......................................................STEADY
Upper panel UP3 :
· WINDSHIELD DE ICING........................................OFF
·
STATIC
HEATER.....................................................OFF
· PITOTS HEATERS..................................................OFF
· ENGINE DE ICING..................................................OFF
·
AIRFOIL DE
ICING..................................................OFF
TADG IIS :
·
POWER
SUPPLY....................................................ON
Pedestal :
· Flaps lever.................................................................UP
·
AP..............................................................................OFF
·
HP-throttle
levers...........................................CLOSED
· Speedbrakes...............................................RETRACT
Upper panel (UP2 ) :
·
NAV1
frequency.......................................................Set
(N1 + +)
·
Course
1...................................................................Set
(V
+
1 + +)
·
NAV2
freqeuncy........................................................Set
(N2 + +)
· ADF1 & 2 frequencies............................................Set (A + +)
_________________________________________________
BEFORE ENGINE START
·
Clearance.................................................................OK
· Engine area..........................................................Clear
·
CABIN & BELLY
DOORS................................Closed
· ANTI COLL LIGHT...................................................ON
· NO SMOKING...........................................................ON
· FASTEN BELT..........................................................ON
_________________________________________________
ENGINE START
Start eng 2 first and eng1
- ENGINE START PROCEDURE:
Fuel pumps (main panel) :
· 1 - MAIN 1 & 2 RH.................................................ON
·
2 - AUX 1
RH....................................................NORM
Pedestal :
·
3 - Throttle
lever 2................................HP CLOSED
-If starting with batteries:
·
3bis - Battery
switch.........................................112V
Engine start panel :
· 4 - ENG selector.......................................................2
· 5 - START-CRANK selector..........................START
·
6 - START
button..........................................pushed
·
7 - RPM....700........HP-throttle
lever.............OPEN
· 8 - LH OIL LOW PR light (UP5)..........................Off
· 10 - Engine parameters.............................Checked
· ENG 1 same procedure Steps 1 to 10
· 11 - ENG selector.................................................OFF
· 12 - START-CRANK selector.......................CRANK
-If starting with batteries:
· 13 - Battery switch...............................................28V
Electrical panel
:
· GENERATORS POWER SOURCE SEL..............PLANE BAT
· ALTERNATORS POWER SOURCE SEL.............PLANE ALT
_________________________________________________
AFTER ENGINE START
Main panel :
· JPT REG switch.......................................................ON
Upper panel (UP3):
·
AIR COND MASTER
VALVES..........................OPEN
·
PITOTS HEATERS....................CAPT & FO..........ON
· STATIC HEATER.....................................................ON
· FD................(Test).....................................................VL (Vor Loc)
· FD................(Test).....................................................FI (Flight Instruments = heading)
· AUTOPILOT READY TO ENGAGE............NORMAL (green light on)
· Speed Index (bugs)...............................................Set
(V2 & 150kts)
_________________________________________________
TAXI
·
Taxi
clearance.................................................Cleared
· TAXI LIGHTS.......................................................As req.
·
Plane
area............................................................Clear
·
Parking
brake................................................released
· Brakes test Right and Left (F11 and F12)
· Brakes indicators (hydraulic panel)..........Checked
· Gyro instruments..........................................Checked
· Flaps.........................................................................10.° (F7)
· Speed Index (bugs)......................................Checked
(V2 & 150kts)
· Flight controls................................................Checked
_________________________________________________
RUNWAY LINEUP
·
Pitch
trim..................................................................1.5°
·
PITOTS HEATERS......................CAPT & FO.......ON
·
STATIC HEATER....................................................ON
·
ENGINE DE ICE....................................................OFF
· AIRFOIL DE ICE....................................................OFF
· Heading vs Runway axis............................Checked
·
NAV
LIGHTS.....................................................FLASH
· LANDING LIGHTS.............................EXTEND & ON
· Flight Director....................................................As req
_________________________________________________
TAKE-OFF
· Brakes..........................................................Released
·
RPM
TO....................................................................Set
· VR = V2 ..............................................................Rotate (10° to 15° max)
-
positive rate of climb–
·
Gear...........................................................................UP (G)
· ENGINE DE ICE................................................As req.
· AIRFOIL DE ICE................................................As req.
· WINDSHIELD DE ICING.................................As req.
- IAS
= V2 + 10–
·
Flaps..........................................................................UP (F5)
_________________________________________________
CLIMB (alt > 1000 ft)
· Climb RPM.............................................................Set
·
IAS..................................V2 + 10 Kt (15° max pitch)
- 3000 ft–
·
IAS......................................................................250
Kt
· TAXI LIGHTS.........................................................OFF
· LANDING LIGHTS........................OFF & RETRACT
· CABIN ALT..............................................................Set
· AUTOPILOT READY TO ENGAGE............NORMAL
· SYNCHRO...............................................................ON
TRANSITION
ALTITUDE
·
Altimeter......................................1013mb /
29.92hg
_________________________________________________
CRUISE
Upper panel (UP2):
· NAV LIGHTS..................................................STEADY
Pressu panel :
· Cabin altimeter..............................Altitude checked
Main panel :
·
Altimeter......................1013mb /
29.92hg checked
·
Cruising
thrust......................................................Set
_________________________________________________
DESCENT
·
Landing
weight.........................................computed
· Minimum Decision Altitude...........................known
· CABIN ALT.............................................................Set
·
Speed
Index..........................................................Set
(VRF & VRF + 25)
·
·
·
·
·
_________________________________________________
HOLDING
·
IAS.................................................................VRF
+ 60
_________________________________________________
APPROACH or DOWN WIND (manual or ATT CAT I)
·
Flaps.........................................................................20.°
(F7)
·
Gear...................................................................DOWN (G)
· IAS..................................................................VRF + 30
APPROACH or DOWN WIND (ATT CAT II)
· Flaps........................................................................20.° (F7)
· IAS..................................................................VRF + 25
_________________________________________________
FINAL APPROACH (manual or ATT CAT I)
·
LANDING
LIGHTS......................EXTENDED & ON
· Flaps........................................................................35° (F8)
·
Speed
Index.................................................Checked
(Vref & Vref + 25)
· IAS.........................................................................VAPP
- if ATT CAT I –
· Height < 400 ft ............................AP HEADING OFF
· Height < 200 ft ..............................AUTOPILOT OFF
FINAL APPROACH (ATT CAT II)
· AUTOPILOT....................................................VOR LOC
· FD.................................................................................V/L
·
LANDING
LIGHTS..........................EXTENDED & ON
- 2 pts before glide –
· Gear......................................................................DOWN (G)
· FD...............................................................................APP
· AUTOPILOT...............................................................GS
- 1 pt before glide –
· IAS....................................................................VRF + 15
· Flaps..........................................................................35° (F8)
- glide slope –
· IAS..........................................................Vapp = VRF + 5
· SPEEDBRAKES.........................................EXTENDED ( :)