Cessna 208B Caravan Afms Blackhawk Pt6-42A

Front 1

Shaft Horsepower

Back 1

850

Front 2

Oil

Back 2

14.5 Quarts total capacity (9.2 Drain and refill Capacity)

Site gauge for reference only. When below green check stick.

Front 3

Max weights

Back 3

Landing 9,000
Ramp 9,100 (actually 9097)
Takeoff 9,062

Front 4

Max continuous power

Back 4

2232 ft/lbs @ 2,000 RPM 770 C or 101.6%np

Front 5

Takeoff power

Back 5

800 C for 5 minutes

Front 6

Total useable fuel

Back 6

332 Gal (166/side)

Front 7

Vne

Back 7

175

Front 8

Va

Back 8

112/143 min/max (basic speeds for Va during skydive ops)

Front 9

Vfe 0-10 degrees

Back 9

175

Front 10

Vfe 10-20 degrees

Back 10

150

Front 11

Vfe 20-full

Back 11

125

Front 12

Torque limitations

Back 12

2232 ft/lbs for most operations
2750 max transient (No more than 5 seconds)
1100 when < 1600 RPM
For "max" operations (max t/o, max climb, max cruise,) +/- 40 torque indication is allowed

Front 13

Np limitations

Back 13

2,000 most operations
1,050 idle
2,205 transient

Front 14

Ng limitations

Back 14

101.6 most operations
103.9 transient for 10 seconds

Front 15

Max idle T5

Back 15

750

Front 16

Max reverse T5 Ng Np

Back 16

750 88 1900

Front 17

Max start T5

Back 17

1000 (850-100 for no more than 5 seconds)

Front 18

Max takeoff T5

Back 18

800
770-800 no more than 5 minutes

Front 19

Oil temp limitations

Back 19

0-99 for most operations
55C min for takeoff

Front 20

Oil pressure limits

Back 20

Normal in flight = 100-135 @ 60-70C
Idle = min of 60
85 is min when at high power @ 60-70C
60-85 in flight = emergency and 1100 torque limited
< 60 = emergency, either use minimum power or shutdown and feather

Front 21

Recommended oil temp before takeoff

Back 21

55

Front 22

Max OAT for ground ops

Back 22

53C (Fuuck that ****!)

Front 23

Airspeed engine failure flaps up

Back 23

100

Front 24

Max fuel imbalance

Back 24

200 lbs

Front 25

Airspeed engine failure flaps full

Back 25

80

Front 26

Engine failure during takeoff

Back 26

1. POWERLever.......................... BETARANGE
2. Brakes...................................... APPLY

IF GOING TO OVERRUN
Condition lever OFF
Fuel Shutoff PULL
Fuel selectors OFF
Battery OFF

Front 27

Engine failure immediately after takeoff

Back 27

Airspeed 85
Prop FEATHER
Condition lever OFF
Fuel shutoff OFF
Fuel selectors OFF
Battery OFF

Front 28

Engine failure

Back 28

Airspeed 100 knots
Power IDLE
Prop FEATHER
Condition lever OFF

Boost pump OFF
Fuel shutoff OFF
Ignition NORMAL
Standby elec power OFF
Electrical load SHED

Front 29

Engine flameout

Back 29

> 50% Ng Power IDLE Ignition ON

<50% Ng Condition lever CUTOFF
(try air restart)

Front 30

Forced landing NO POWER

Back 30

1. Seats, Seat Belts, Shoulder Harnesses . . . . . . . SECURE
2. Airspeed........100KIAS(flapsUP) 80 KIAS (flaps FULL)
3. POWERLever .................................. IDLE
4. PROPRPMLever........................... FEATHER
5. FUELCONDITIONLever.......................CUTOFF
6. FUELBOOSTSwitch............................. OFF
7. IGNITIONSwitch .............................. NORM
8. STBYALTPWRSwitch ........................... OFF
9. NonessentialEquipment........................... OFF
10. FUELSHUTOFFKnob...................... PULLOFF
11. FUEL TANK SELECTORS . . . . . OFF (warning horn will sound)
12.WINGFLAPSHandle.. A/R (FULLrecommended)
13. CrewDoors...........UNLATCHPRIORTOTOUCHDOWN 14. GENERATOR Switch . . . . . . . . . . . . TRIP
15. BATTERYSwitch ........... OFF(whenlandingisassured) 16. Touchdown....................... SLIGHTLYTAILLOW
17. Brakes............................... APPLYHEAVILY

Front 31

Engine fire in flight

Back 31

1. POWERLever.................................. IDLE
2. PROPRPMLever........................... FEATHER
3. FUELCONDITIONLever ...................... CUTOFF
4. FUELSHUTOFFKnob...................... PULLOFF
5. CABIN HEAT...... OFF

6. ForwardSideVents ........................... CLOSE
7. OverheadVents................................ OPEN
8. VENTAIRFANS.................................. ON
9. WINGFLAPSHandle........................20°-FULL 10.Airspeed ................................ 80-85KIAS 11.ForcedLanding............................. EXECUTE

Front 32

Electrical fire in flight

Back 32

1. STBYALTPWRSwitch........................... OFF
2. GENERATORSwitch............................ TRIP
3. BATTERYSwitch................................ OFF
4. Vents ........................ CLOSED(toavoiddrafts)
a. ForwardSideVents ....................... CLOSE
b. OverheadVents........................... CLOSE
c. VENTAIRFANS............................. OFF
5. BLEEDAIRHEATSwitch ......................... OFF
6. FireExtinguisher ................................ USE

Front 33

Cabin fire

Back 33

1. STBYALTPWRSwitch...........................OFF
2. GENERATORSwitch............................ TRIP
3. BATTERYSwitch................................OFF
4. Vents......................... CLOSED(toavoiddrafts)
a. ForwardSideVents ........................ CLOSE
b. OverheadVents........................... CLOSE
c. VENTAIRFANS .............................OFF
5. BLEEDAIRHEATSwitch..........................OFF
6. FireExtinguisher................. ACTIVATE(ifavailable)

Front 34

Wing fire

Back 34

1. PITOT/STATICHEATSwitch....................... OFF
2. STALLHEATSwitch ............................. OFF
3. STROBESwitch................................. OFF
4. NAVSwitch .................................... OFF
5. LDGandTAXI/RECOGSwitches................... OFF
6. FUELQUANTITYCircuitBreakers .................. OFF
(second row, third breaker from front and third row third breaker from front)
7. RADARR/TCircuitBreaker(ifinstalled)............. PULL (AVN BUS 1, second row, sixth breaker from left side)
8. VENTAIRFANS ................................ OFF
9. AIRCONDITIONING(ifinstalled) ................... OFF

Front 35

Engine fire during start

Back 35

Condition lever OFF
Boost pump OFF
MOTOR>>>>>>>
IF FIRE CONTINUES
Starter OFF
Fuel shutoff PULL
Battery OFF
EVACUATE AND EXTINGUISH

Front 36

Pitch trim failure

Back 36

1. ControlWheel........................... GRIPFIRMLY
2. AP/TRIMDISCButton.......................... PRESS
(high elevator control forces possible)
3. ELEVATOR TRIM . . . . . . . . RETRIM (using manual trim wheel)
NOTE
Actuate each half of the pilot and copilot Manual Electric Pitch Trim Switches separately to make sure trim does not actuate with only one half switch.
IF Red PTRIM CAS MESSAGE CLEARS
Procedure complete
IF Red PTRM MESSAGE REMAINS
4. Autopilot ........................ DONOTRE-ENGAGE

Front 37

Fuel flow interruption to reservoir

Back 37

1. FUELTANKSELECTORS.................... BOTHON
2. IGNITIONSwitch............................. ON
3. FUELBOOSTSwitch............................. ON
4.
If Red RSVR FUEL LOW CAS MSG remains and there is usable fuel in the wing tanks:
a. Carefully monitor engine indications and Amber FUEL PRESS LOW CAS MSG for signs of fuel starvation.
b. Land as soon as possible and determine cause of Red RSVR FUEL LOW warning.

Front 38

Trim tabs

Back 38

Aileron- 1 tab on right side (servo)
Elevator- 2 tabs

Front 39

Spoilers

Back 39

Disrupt airflow over corresponding flap for increased maneuverability at slow speeds. Spoilers are extended after 5 degrees of aileron travel has been reached.

Front 40

OIL PRESS LOW (RED)

Back 40

Indicates engine oil pressure is less than 40 psi.

Front 41

VOLTAGE LOW (RED)

Back 41

Indicates electrical system bus voltage is less than 24.5 volts and power is being supplied from the battery.

Front 42

VOLTAGE HIGH (RED)

Back 42

Indicates electrical system bus voltage is greater than 32.0 volts.

Front 43

RSVR FUEL LOW (RED)

Back 43

reservoir is less than 1/2 full and 3-9 minutes of fuel is left

Front 44

FUEL SELECT OFF (RED)

Back 44

Indicates left and right fuel selectors are both OFF at any time, or left fuel selector is OFF when right tank is low, or right fuel selector is OFF when the left tank is low; or that either left or right selectors are OFF when starter switch is ON. It can also indicate that the FUEL SEL WARN circuit breaker has been pulled.

Front 45

FUEL PRESS LOW (AMBER)

Back 45

<4.75 psi

Front 46

ITT sensing

Back 46

Done by 8 Chromel/alumel probes located near the power turbine stator vanes.

Front 47

Chip detectors

Back 47

1 under reduction gear case
1 under accessory gear case

Front 48

Battery start procedure (abridged)

Back 48

Bat - On

Bus volts - 24 min

E power lev - norm

Boost pump on- looking for Aux pump light on and low pressure light off.

Starter switch on- observe start light on, Ng 14% min, oil pressure up

Condition lever - Low idle (min FF 50pph) 1000C max temp (850-1000 for 5 seconds) Ng 50% min

Start switch off - Check light off

Fuel boost switch normal

Avionics etc. - On

Front 49

Aux start procedure (abridged)

Back 49

External power switch - BUS

Voltmeter - 24-28.5

Bat switch - On

External power switch - Starter

Boost pump - On and observe necessary lights

Starter switch on - lights, 14% min, oil...

Con lever - Low Idle observe 50pph min, 1000C max Ng 50% stabilized

Start switch - Off / lights off

External power switch - Off

Boost switch - Norm / lights off

Avionics etc. ..

Front 50

Condition lever

Back 50

Low idle = 58-61%
High idle = 68-71%

Front 51

Engine instruments

Back 51

LED's
None = Normal
Constant red = exceeding limit
Flashing red fast = Transducer signal failed
Flashing red slow = Instrument has failed

Front 52

Torque indicator

Back 52

Electrically powered 28VDC

Measures torque difference between different sides of the gearbox and transmits electrically in ft/lbs

Front 53

Oil pressure gauge

Back 53

Electrically powered 28VDC

Measured at upper right truss tube and signal sent and converted to psi

Front 54

Torque limiter

Back 54

At 2410 ft/lbs Py air is bled off to reduce fuel flow and reduce torque

Front 55

Starter/generator time limitations

Back 55

Batt: 30 on 30 off, 30 on 30 off, 30 on 30 min.
Ext: 20 on 120 off, 20 on 120 off, 20 on 60 min.

Front 56

Prop overspeed governor

Back 56

TEST = 1750 +- 50

Front 57

Aux fuel pump

Back 57

In 'normal' will turn on when fuel manifold pressure drops below 4.75 psi

Front 58

Stby power rating

Back 58

75 amps

Front 59

Stby power setup

Back 59

Gen fail/off
stby power on
stby avionics power on
avionics bus tie on
avionics 1 & 2 off
maintain @ or below 75 amps

Front 60

starter/generator output and cutoff start-gen

Back 60

28V 200 amp
Cuts out during start after 47%

Front 61

Fuel quantity transmitters

Back 61

8
4 in each tank
float

Front 62

When does standby power come on?

Back 62

When bus voltage drops below 27.5V

Front 63

Prop overspeed governor tests @

Back 63

1750 +- 50