1. Power levers - IDLE2. Prop levers - FULL FORWARD3. Flaps - APPROACH/202 KTS MAX4. Landing gear - DOWN/184 KTS MAX5. Airspeed - 184 KTS MAX

kingair_350_20121215045734 Flashcards by Abbie Crews

Engine Fire/Failure in Flight

Affected engine:1. Condition lever - FUEL CUTOFF2. Prop lever - FEATHER3. Firewall valve - CLOSE (EXTINGUISHER PUSH) and (CLOSED) - ILLUMINATED4. Fire extinguisher (if fire warning persists) - ACTUATE (DISCHARGED) - ILLUMINATED

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EMERGENCY ENGINE SHUTDOWN ON THE GROUND

Condition levers - FUEL CUTOFF2. Prop levers - FEATHER3. Firewall valves - CLOSE (EXTINGUISHER PUSH) and (CLOSED) - ILLUMINATED4. Master switch (gang bar) - OFF5. Battery bus switch - EMER OFF6. ESIS power - OFF

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ENGINE FAILURE DURING TAKEOFF AT/BELOW V1 - TAKEOFF ABORTED

Power Levers - GROUND FINE2. Brakes - MAXIMUM (or as required to achieve desired stopping distance)

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ENGINE FAILURE DURING TAKEOFF AT/ABOVE V1 - TAKEOFF CONTINUED

VR speed - ROTATE TO APPROXIMATELY 10° PITCH ATTITUDE2. Gear - UP (When positive climb established)3. Airspeed - MAINTAIN V2 TO 400 ft AGL AND CLEAR OF OBSTACLES4. Prop (inoperative engine) - VERIFY FEATHERED

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WARNING–ENGINE FAILURE DURING TAKEOFF AT/BELOW V1 - TAKEOFF ABORTED–WARNING

Do not use reverse thrust with an engine inoperative. Exercise care using single-engine GROUND FINE on surfaces with reduced traction.

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WARNING–ENGINE FAILURE DURING TAKEOFF AT/ABOVE V1 - TAKEOFF CONTINUED–WARNING

Do not retard failed engine power lever until auto feather system has completely stopped propeller rotation.

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ENGINE FAILURE IN FLIGHT BELOW Vmca

Power - REDUCE AS REQUIRED TO MAINTAIN CONTROL2. Nose - LOWER TO ACCELERATE ABOVE Vmca

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GLIDE (BOTH ENGINES INOPERATIVE)

Landing Gear - UP2. Flaps - UPWARNING: Do not feather second engine propeller if a No Starter Assist air start is to be conducted. Air starts with a windmilling propeller will result in lower starting temperatures. Refer to Abnormal Procedures for Air Start Procedures.3. Prop Levers - FEATHERED4. Airspeed - 135 KTS

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DUAL GENERATOR FAILURE [L DC GEN] and [R DC GEN]

Instrument emergency lights (if required) - ON2. Generator - RESET, THEN ON If either generator will reset:3. Operating generator loadmeter - MONITORIf neither generator resets:4. ECS mode - OFF5. Cockpit/Cabin blower - AUTO6. Non-essential equipment - OFF

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UNSCHEDULED ELECTRIC PITCH TRIM ACTIVATION

Aircraft attitude - MAINTAIN WITH ELEVATOR CONTROL2. AP/Trim disconnect - DEPRESS FULLY (Pitch Trim OFF) - ILLUMINATED

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UNSCHEDULED RUDDER BOOST ACTIVATION

AP/Trim disconnect - DEPRESS/HOLD (FIRST LEVEL)2. Rudder boost - OFFIf condition persists:3. Rudder boost circuit breaker - PULL

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SPINS

If a spin is entered inadvertently:1. Control column - FULL FORWARD - AILERONS NEUTRAL2. Rudder - APPLY FULL OPPOSITE SPIN DIRECTION3. Power levers - REDUCE TO IDLE ON BOTH ENGINESThese action should be accomplished as nearly simultaneously as possible4. RUDDER - NEUTRALIZE - HOLD UNTILE ROTATION STOPS5. Execute smooth pullout

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WINDSHIELD ELECTRICAL FAULT

WSHLD ANTI-ICE switches - OFFIf smoke and/or fire does not cease:2. ELECTRICAL SMOKE OR FIRE Checklist - CONDUCT

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ELECTRICAL SMOKE OR FIRE

WARNING: Dissipation of smoke is not sufficient evidence that a fire has been extinguished. If it cannot be visually confirmed that no fire exists, land at the nearest suitable airport.1. Oxygen mask(s) - DON2. Mask selector switch - EMERG3. Headset - DON/AUDIO SPEAKER ON4. Mic switch(es) - OXY

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ENVIRONMENTAL SYSTEM SMOKE OR FUMES

Oxygen: 1. Crew mask - DON 2. Mask selector switch - EMERG 3. Headset - DON/AUDIO SPEAKER ON 4. Mic selector - OXYGEN MASK

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AIRSTAIR/CARGO DOOR UNLOCKED

WARNING: Do not attempt to check the security of the airstair door or cargo door in flight. Remain as far from the door as possible with seat belts securely fastened. If the [DOOR UNLOCKED] Illuminates, of If An Unlatched Airstair Door/Cargo Door is Suspected:1. All occupants - SEATED WITH SEAT BELTS SECURELY FASTENED

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EMERGENCY DESCENT

Power levers - IDLE2. Prop levers - FULL FORWARD3. Flaps - APPROACH/202 KTS MAX4. Landing gear - DOWN/184 KTS MAX5. Airspeed - 184 KTS MAX

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OXYGEN USE

Crew System:1. Crew mask - DON2. Headsets - DON, AUDIO SPEAKER ON3. Mic Switches - OXYGEN MASK4. Oxygen duration - CONFIRM

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PRESSURIZATION LOSS [CABIN ALT HI]

Oxygen mask(s) - DON2. Headsets - DON or AUDIO SPEAKER ON3. Mic switch(es) - OXYGEN MASK4. Passenger manual drop out - PULL ON [PASS OXYGEN ON] - ILLUMINATED5. Descent - AS REQUREDWARNING: The highest recommended cabin altitude for sustained flight is 25,000 ft.

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HIGH DIFFERENTIAL PRESSURE

Bleed air valve switches - ENVIR OFF2. Oxygen (crew and passengers) - AS REQUIRED3. Descend as required

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AUTO-DEPLOYMENT OXYGEN SYSTEM FAILURE

CABIN ALT HI illuminated and PASS OXYGEN ON extinguished1. Passenger manual dropout - PULL ON

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BLEED AIR FAILURE

If illuminated during flight:1. Bleed air valve switch (affected engine) - PNEU/ENVIR OFF

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AUTOPILOT MISTRIM [E] or [A]

WARNING: Intentional or automatic disengagement of the autopilot without restraining the control wheel during mistrim condition will produce a significant airplane response in the direction of the mistrim force.If a Mistrim Indication continues for more than a few seconds:1. Flight controls - HOLD FIRMLY (Control forces may exceed 25 lbs)2. AP - DISENGAGE

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AUTOPILOT TRIM FAIL [TRIM]

Flight controls - HOLD FIRMLY2. AP - DISENGAGE

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AUTOPILOT AUTOMATIC DISENGAGEMENT

If an Automatic Disengagement occurs:1. Maintain airplane control2. AP/TRIM disconnect - DEPRESS TO 1st LEVEL TO CANCEL HORN

EGPWS in IMC or NIGHT

1. Wings - LEVEL2. Power - MAX ALLOWABLE3. Pitch - INCREASE- Promptly and smoothly increase pitch toward an initial pitch attitude of 20° to 25°- Adjust as required to avoid continuous buffeting and/or stall warning- Adjust to maintain 125 KIAS4. Gear and Flaps - UP

TAWS+ in IMC or NIGHT

1. Autopilot - DISENGAGE2. Wings - LEVEL3. Power - MAX ALLOWABLE4. Pitch - INCREASE- Promptly and smoothly increase pitch toward an initial pitch attitude of 20° to 25°- Adjust as required to avoid continuous buffeting and/or stall warning- Adjust to maintain 125 KIAS5. Gear and Flaps - UP

MIN CREW

ONE PILOT

PAX SEATING LIMITATIONS

15 PAX MAX

LOAD FACTOR FLAPS DOWN NEGATIVE

0 Gs

LOAD FACTOR FLAPS DOWN POSITIVE

1.1 Gs

LOAD FACTOR FLAPS UP NEGATIVE

-1.24 Gs

LOAD FACTOR FLAPS UP POSITIVE

3.1 Gs

MAX OPERATING ALTITUDE WITH *AVGAS* AND BOTH STBY BOOST PUMPS OPERATIVE

35,000 FT

MAX OPERATING ALTITUDE

35,000 FT

MAX OPERATING ALTITUDE AVGAS EITHER STBY BOOST PUMT INOP

FLIGHT PROHIBITED

MAX ALLOWABLE TAKEOFF WEIGHT

15,000 LBSOR AS LIMITED BY:-TAKEOFF CLIMB REQUIREMENTS-TIRE SPEED-BRAKE ENERGY-TAKEOFF FIELD LENGTH

MAX LANDING WEIGHT

15,000 LBSOR AS LIMITED BY:-MAX LANDING WIEGHT TO ACHIEVE CLIMB GRADIENTS-MAX LANDING DISTANCE - FLAPS DOWN

MAX RAMP WEIGHT

15,100 LBS

MAX ZERO FUEL WEIGHT

12,500 LBS

EMERGENCY AIRSPEEDS (15,000 LBS)ONE ENGINE INOP BEST ANGLE OF CLIMB (VXSE)

125 KIAS

EMERGENCY AIRSPEEDS (15,000 LBS)ONE ENGINE INOP BEST RATE OF CLIMB (VYSE)

125 KIAS

EMERGENCY AIRSPEEDS (15,000 LBS)ONE ENGINE INOP ENROUTE CLIMB

125 KIAS

EMERGENCY AIRSPEEDS (15,000 LBS)AIR MIN CONTROL SPEED (VMCA): FLAPS UP

94 KIAS

EMERGENCY AIRSPEEDS (15,000 LBS)AIR MIN CONTROL SPEED (VMCA): FLAPS APPROACH

93 KIAS

EMERGENCY AIRSPEEDS (15,000 LBS)EMERGENCY DESCENT SPEED

184 KIAS

EMERGENCY AIRSPEEDS (15,000 LBS)MAX RANGE GLIDE SPEED

135 KIAS

MAX DEMO'D CROSSWIND

20 KTS

MAX TAILWIND

10 KTS

SINGLE ENGINE ENROUTE CLIMB

125 KIAS

MANEUVERING SPEED (VA)

184 KTS

MAX FLAP EXTENSION/EXTENDED SPEED (VFE) APPROACH

202 KIAS

MAX FLAP EXTENSION/EXTENDED SPEED (VFE) FULL

158 KIAS

MAX LANDING GEAR EXTENDED SPEED (VLE)

184 KIAS

MAX LANDING GEAR OPERATING SPEED (VLO) EXTENSION

184 KIAS

MAX LANDING GEAR OPERATING SPEED (VLO) RETRACTION

166 KIAS

AIR MIN CONTROL SPEED (VMCA) PROP FEATHERED FLAPS UP

96 KIAS

AIR MIN CONTROL SPEED (VMCA) PROP FEATHERED FLAPS APPROACH

94 KIAS

MAX OPERATING SPEED (VMO)

263 KIAS/0.58 MACH

AIRCRAFT HEIGHT

14' 4"

AIRCRAFT LENGTH

46' 8"

AIRCRAFT WINGSPAN

57' 11"

AFT FACING SEATS TAKEOFF RESTRICTION

IF OCCUPIED FOR T/O, HEADRESTS MUST BE FULLY EXTENDED

AUTOPILOT MAX COUPLED INTERCEPT ANGLE FOR BACK COURSE

70°

AUTOPILOT MAX COUPLED INTERCEPT ANGLE FOR NAV/LOC

LESS THAN 90°

AUTOPILOT MIN ALT FOR APPROACH

200 FT AGL

AUTOPILOT MIN ALT FOR CRUISE

1,000 FT AGL

AUTOPILOT MIN ALT FOR STEEP APPROACH

160 FT AGL

Below ______ volts, battery must be recharged prior to attempting engine start.

20 VDC

EXTERNAL POWER AMPS LIMITS: MOMENTARY

1,000 AMPS

EXTERNAL POWER AMPS LIMITS: CONTINUOUS

300 AMPS

EXTERNAL POWER VOLTAGE RANGE

28 TO 28.4 VOLTS

GENERATOR LOAD LIMITS ABOVE 34,000 FT

95%

GENERATOR LOAD LIMITS IN GROUND AT 62%-70% N1

75%

GENERATOR LOAD LIMITS IN GROUND AT 70%-100% N1

100%

GENERATOR LOAD LIMITS SL TO 34,000 FT

100%

MIN BATTERY VOLTS FOR BATTERY START

23 VDC

STARTER DUTY CYCLE

-30 SEC ON/5 MIN OFF-30 SEC ON/5 MIN OFF-30 SEC ON/30 MIN OFF

For fuel system, fill the _______ tanks first.

MAIN

For fuel system, do not takeoff if fuel gauges in the ______ arc or indicate less than _____ lbs in each wing system.

YELLOW265

FUEL CROSSFEED PERMITTED ONLY WHEN

ONE ENGINE INOP

MAX FUEL IMBALANCE

300 LBS

AUX SYSTEM FUEL QUANTITY

79.5 U.S. GAL / 533 LBS

MAIN SYSTEM FUEL QUANTITY

190 U.S. GAL / 1,273 LBS

TOTAL USABLE FUEL QUANTITY

539 U.S. GAL / 3,611 LBS

WHEN IS ENGINE ANTI-ICE REQUIRED?

+5° C IN VISIBLE MOISTURE

MIN TEMP FOR DEICING BOOTS OPERATIONS

-40° C

MIN AIRSPEED FOR SUSTAINED OPS IN ICING

140 KTS

MAIN LANDING GEAR STRUT EXTENSION (INCHES)

3.23 TO 3.49 INCHES

NOSE LANDING GEAR STRUT EXTENSION (INCHES)

3.77 TO 4.06 INCHES

BRAKES DEICE TEMP OPERATION LIMITE

NOT ABOVE 15° C

LANDING GEAR CYCLE LIMITS

1 CYCLE (UP/DOWN) EVERY 5 MIN FOR TOTAL OF 6 FOLLOWED BY 15 MIN COOL-DOWN

MAX CABIN PRESSURE DIFFERENTIAL

6.6 PSI

CABIN DIFFERENTIAL PRESSURE (GREEN ARC)

0 TO 6.6 PSI

CABIN DIFFERENTIAL PRESSURE (RED ARC)

6.6 PSI AND UP

When does the "CABIN ALTITUDE" light illuminate?

ABOVE 10,000 FT CABIN ALT

When does the "CABIN ALTITUDE HI" light illuminate?

ABOVE 12,000 FT CABIN ALT

When do the passenger mask automatically deploy?

ABOVE 12,500 FT CABIN ALT

Cabin altitude is limited to _____ Ft as long as air is coming into pressure vessel.

13,000 FT

The "CABIN DIFF HI" light illuminates at what PSID?

6.9 PSID

ENGINE MODEL NUMBER AND TYPE

PT6A-60A, TURBOPROP

PROPELLER TYPE

CONSTANT-SPEED, FULL-FEATHERING, REVERSING, COUNTER-WEIGHTED, AND HYDRAULICALLY ACTUATED

MAX N1 CRUISE CLIMB

104%

62% MIN

MAX N1 MAX CRUISE

104%

MAX TRANSIENT N1

104%

MAX ITT CRUISE

820° C

MAX ITT CRUISE CLIMB

785° C

MAX ITT IDLE

750° C

MAX CONTINUOUS ITT

820° C

MAX ITT REVERSE

760° C

ENGINE STARTING MAX TRANSIENT ITT

1,000° C FOR 5 SEC

MAX TAKEOFF ITT

820° C

ENGINE MAX ITT TRANSIENT

850° C FOR 20 SEC

NORMAL OIL PRESSURE FOR CRUISE CLIMB

90 TO 135 PSI

ENGINE OIL PRESSURE IDLE

60 PSI MIN

MAX CONTINUOUS OIL PRESSURE

90 TO 135 PSI

MAX CRUISE OIL PRESSURE

90 TO 135 PSI

MAX REVERSE OIL PRESSURE

90 TO 135 PSI

ENGINE OIL PRESSURE STARTING

0 TO 200 PSI

NORMAL TAKEOFF OIL PRESSURE

90 TO 135 PSI

ENGINE OIL PRESSURE TRANSIENT

200 PSI

ENGINE OIL TEMP CRUISE CLIMB

0° TO 110° C

ENGINE OIL TEMP IDLE

-40° TO 110° C

MAX CONTINUOUS OIL TEMP

0 TO 110° C

ENGINE OIL TEMP MAX CRUISE

0 TO 110° C

ENGINE OIL TEMP MAX REVERSE

0 TO 99° C

ENGINE OIL TEMP MIN FOR FUEL HEAT AT T/O

55° C (RECOMMENDED)

ENGINE PROP RPM (N2) CRUISE CLIMB

1,700 (UP TO 1,735 FOR 7 MINUTES)

ENGINE PROP RPM (N2) IDLE

1,050 MIN

ENGINE PROP RPM (N2) MAX CONTINUOUS

1,700 RPM (UP TO 1,735 FOR 7 MINUTES)

MAX CRUISE N2

1,700 RPM (UP TO 1,735 FOR 7 MINUTES)

MAX REVERSE N2

1,650 RPM

MAX TAKEOFF N2

1,700 RPM (UP TO 1,735 FOR 7 MINUTES)

MAX TRANSIENT N2

1,870 RPM FOR 20 SEC

ENGINE TORQUE% MAX CONTINUOUS

100% (UP TO 102% FOR 7 MINUTES)

MAX TORQUE% FOR TAKEOFF

100% (UP TO 102% FOR 7 MINUTES)

ENGINE TORQUE LIMITE BELOW 1,000 RPM N2

62%

If the shaft to the primary governor were to shear, what would happen to the propeller?

It would feather

What is the range of the primary governor?

1,450 to 1,700 RPM

The overspeed governor governs to \_\_\_\_\_.

1,768 RPM

TERMINAL AREA (TWO ENG)

* 180 KIAS * 40% TORQUE * 1,500 RPM * GEAR UP * FLAPS 0

APPROACH (TWO ENG)

* 180 KIAS * 25% TORQUE * 1,500 RPM * GEAR UP * FLAPS APPR

ILS OM INBOUND (GEAR @ G/S, 650 FPM) (TWO ENG)

* 130 KIAS * 25 % TORQUE * 1,700 RPM * GEAR DOWN * FLAPS APPR

NON-PRECISION FAF INBOUND (TWO ENGINE)

* 130 KIAS * 25% TORQUE * 1,700 RPM * GEAR DOWN * FLAPS APPR

CIRCLE TO LAND / MDA (TWO ENG)

* 130 KIAS * 40% TORQUE * 1,700 RPM * GEAR DOWN * FLAPS APPR

STEEP TURNS

* 180 KIAS * 52% TORQUE * 1,500 RPM * GEAR UP * FLAPS 0

TERMINAL AREA (SINGLE ENG)

* 180 KIAS * 80% TORQUE * 1,700 RPM * GEAR UP * FLAPS 0

APPROACH (SINGLE ENG)

* 130 KIAS * 60% TORQUE * 1,700 RPM * GEAR UP * FLAPS APPR

ILS-OM INBOUND (GEAR @ G/S, 650 FPM) (SINGLE ENG)

* 130 KIAS * 50% TORQUE * 1,700 RPM * GEAR DOWN * FLAPS APPR

NON-PRECISION FAF INBOUND ( SINGLE ENG)

* 130 KIAS * 50% TORQUE * 1,700 RPM * GEAR DOWN * FLAPS APPR

CIRCLE TO LAND/MDA (SINGLE ENG)

* 130 KIAS * 80% TORQUE * 1,700 RPM * GEAR DOWN * FLAPS APPR

kingair_350_20121215045734 Flashcards

(152 cards)