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Kingair 350 > 350 > Flashcards

350 Flashcards

1
Q

Maneuvering Speed (Va)

A

184 KIAS

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2
Q

Maximum Flap Extension/Extended Speed (Vfe)

A

Approach (<APP (white)) ……………202 KIAS
Full Down (<DN (white)) …………….158 KIAS

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3
Q

Maximum Landing Gear Operating Speed (VLO)

A

Extension……….184 KIAS
Retraction………166 KIAS

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4
Q

Maximum Landing Gear Extended Speed (VLE)

A

184 KIAS

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5
Q

Maximum Operating Speed (VMO)
Sea Level to 21,000 feet….._____
21,000 to 35,000 feet………._____-_____

A

Seal Level to 21,000 feet ……….263 KIAS
21,000 to 35,000 feet …………….263-194*KIAS
*0.58 Mach

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6
Q

Airspeed Indicator Display
Solid Red Bar (at bottom of airspeed indicator scale)
Maximum weight, flaps down & idle power _________

A

81 KIAS

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7
Q

Airspeed Indicator Display

Solid Red Bar (Bottom of AI)

Max weight, flaps approach, idle power ….._______
Max weight, flaps up, idle power …………….._______

A

Max weight, flaps approach, idle power …..89 KIAS
Max weight, flaps up, idle power ……………..96 KIAS

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8
Q

AIRSPEED INDICATOR DISPLAY

Blue Line One-Engine-Inoperative Best Rate-of-Climb Speed
__________

A

Blue Line One-Engine-Inoperative Best Rate-of-Climb Speed
125 KIAS

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9
Q

ENGINE OPERATING LIMITS

Maximum ITT °C

Starting ………._____
Idle………………_____
Takeoff……….._____
Max Cruise…._____
Max Reverse.._____

A

Starting ……….1000 degrees for 5 seconds
Idle………………750 C
Takeoff………..820 C
Max Cruise….820 C
Max Reverse..760 C

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10
Q

ENGINE OPERATING LIMITS

Gas Generator RPM % N1

Max Cruise.._____
Takeoff………_____

A

Max Cruise..104
Takeoff……..104

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11
Q

ENGINE OPERATING LIMITS

Oil Temperature Limits

Minimum ………………………………………….._____
Maximum …………………………………………._____
Limited to a maximum of 10 minutes .._____

A

Minimum …………………………………………..-40 C
Maximum ………………………………………….+110 C
Limited to a maximum of 10 minutes ..between 99 C and 110 C

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12
Q

EXTERNAL POWER LIMITS

Set to ____ - ____ volts
minimum of ____ amps momentarily
and ____ amps continuously

A

Set to 28.0- 28.4 volts
minimum of 1000 amps momentarily
and 300 amps continuously

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13
Q

GENERATOR LIMITS

Maximum sustained generator load is limited as follows:
In Flight:
Sea Level to 34,000 feet altitude……______
Above 34,000 feet altitude…………….______

A

Sea Level to 34,000 feet altitude………………………………….100%
Above 34,000 feet altitude…………………………………………….95%

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14
Q

GENERATOR LIMITS

Maximum sustained generator load is limited as follows:
Ground Operation:
N1 MAXIMUM GENERATOR LOAD
62% to 70% ………………..______
70% to 100%……………….______

A

N1 MAXIMUM GENERATOR LOAD
62% to 70% ……………………………. 75%
70% to 100% ………………………….. 100%

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15
Q

STARTER LIMITS

_________ ON, __________ OFF,
_________ ON, __________ OFF,
_________ ON, __________ OFF

A

30 seconds ON, 5 minutes OFF,
30 seconds ON, 5 minutes OFF,
30 seconds ON, 30 minutes OFF

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16
Q

LIMITATIONS ON THE USE OF AVIATION GASOLINE

What are the limitations on the use of aviation gasoline (AVGAS)?

A
  1. Operation is limited to 150 hours between engine overhauls.
  2. Operation is prohibited if either standby fuel pump is inoperative.
  3. Crossfeed capability is required for flight above 20,000 feet pressure altitude (FL200).
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17
Q

FUEL MANAGEMENT

USABLE FUEL (GALLONS X 6.7 = POUNDS)

Total Quantity…..___ gallons ( ____ pounds)
* Each Main Fuel Tank
System….………….___ gallons ( ____ pounds)
* Each Auxiliary Fuel Tank………………………………….___ gallons ( ___ pounds)

A

Total Quantity…539 gallons ( 3611 pounds)
* Each Main Fuel Tank

System….…………190 gallons ( 1273 pounds)
* Each Auxiliary Fuel Tank.……79.5 gallons ( 533 pounds)

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18
Q

FUEL MANAGEMENT

FUEL IMBALANCE
Maximum allowable fuel imbalance between the wing fuel system?

FUEL CROSSFEED
Permitted only for what circumstance?

A

FUEL IMBALANCE
Fuel imbalance between wing fuel systems is 300 pounds

FUEL CROSSFEED
Permitted only when one engine is inoperative

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19
Q

FUEL MANAGEMENT

FUEL GAGES IN THE YELLOW ARC

Do not take off if fuel quantity gauges indicate in yellow arc
or indicate less than ___ lbs of fuel in each wing system.

A

Do not take off if fuel quantity gages indicate in yellow arc
or indicate less than 265 lbs of fuel in each wing system.

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20
Q

FUEL MANAGEMENT

OPERATING WITH LOW FUEL PRESSURE

Operation with the [L FUEL PRES LO] /
[R FUEL PRES LO] illuminated is limited to _____ hours.

A

Operation with the [L FUEL PRES LO] / [R FUEL PRES LO] illuminated is limited to 10 hours.

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21
Q

PROPELLERS

PROPELLER ROTATIONAL SPEED LIMITS
Minimum idle speed……………………………………. _____________

PROPELLER AUTOFEATHER
Must be operable for ______ and must be armed for _______, _______, _______, and _______.

A

Minimum idle speed…………………………………………….. 1050 rpm

PROPELLER AUTOFEATHER - Must be operable for all flights and must be armed for
takeoff, climb, approach, and landing.

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22
Q

MISCELLANEOUS INSTRUMENT MARKINGS

PNEUMATIC PRESSURE GAUGE Green Arc (Normal Operating Range)

A

Green Arc (Normal Operating Range)…………………12 to 20 psi

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23
Q

MAXIMUM OPERATING ALTITUDE LIMITS

Normal Operation ….______

A

Normal Operation ………………35,000 feet

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24
Q

MAXIMUM OUTSIDE AIR TEMPERATURE LIMITS

Sea Level to 25,000 feet pressure altitude …… _____________

A

Sea Level to 25,000 feet pressure altitude ………….. ISA + 37°C

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25
Q

CABIN PRESSURIZATION LIMIT

Maximum Cabin Pressure Differential………._______

A

Maximum Cabin Pressure Differential ……. 6.6 psi

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26
Q

SYSTEMS AND EQUIPMENT LIMITS

RUDDER BOOST Must be operational for ________

A

RUDDER BOOST Must be operational for all flights

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27
Q

SYSTEMS AND EQUIPMENT LIMITS

LANDING GEAR CYCLE LIMITS

Limited to _____ every ________ for a total of ________, followed by a ________ cool-down period.

A

LANDING GEAR CYCLE LIMITS

Limited to one every 5 minutes for a total of 6 cycles, followed by a 15-minute cool-down period.

28
Q

SYSTEMS AND EQUIPMENT LIMITS

BRAKE DEICE (IF INSTALLED) Is not to be operated above _____

A

BRAKE DEICE (IF INSTALLED) Is not to be operated above 15°C

29
Q

ICING LIMITATIONS

Min ambient temp for operation of deicing boots…. ________
Min airspeed for sustained icing flight………………….. ________

A

Min ambient temp for operation of deicing boots…………-40°C
Min airspeed for sustained icing flight…………………..140 knots

30
Q

ICING LIMITATIONS

[LENG ANTI-ICE] and [R ENG ANTI-ICE],
shall be ___ for operation in ambient temperatures of _____ or below
when ____________ _________ cannot be assured.

A

[LENG ANTI-ICE] and [R ENG ANTI-ICE],
shall be ON for operation in ambient temperatures of +5 C or below
when FLIGHT FREE OF VISIBLE MOISTURE cannot be assured.

31
Q

ICING LIMITATIONS

[LENG ANTI-ICE] and [R ENG ANTI-ICE], shall be ____ for ______ _________________
in ambient temperatures of above______.

A

[LENG ANTI-ICE] and [R ENG ANTI-ICE], shall be OFF for TAKE-OFF OPERATIONS
in ambient temperatures of above +10 C.

32
Q

AUTOPILOT

Minimum engage height after takeoff
Minimum use height during cruise
Minimum use height during approach
Minimum use height during steep approach

A

Minimum engage height after takeoff………………….. 400 ft AGL
Minimum use height during cruise……………………. 1000 ft AGL
Minimum use height during approach………………….. 79 ft AGL
Minimum use height during steep approach……….. 160 ft AGL

33
Q

AUTOPILOT

What are the maximum coupled intercept angles?

Nav and Localizer …………. _____________

Back Course……………………_____________

A

What are the maximum coupled intercept angles?

Nav and Localizer ……………..Less than 90°

Back Course………………………70°

34
Q

WEIGHTS

Maximum Ramp Weight………………………………. _____________

A

Maximum Ramp Weight ……15,100 lbs

35
Q

WEIGHTS

Maximum Take-off Weight…………………………… _____________

A

Maximum Take-off Weight …….15,000 lbs

36
Q

WEIGHTS

Maximum Landing Weight…………………………… _____________

A

Maximum Landing Weight ……15,000 lbs

37
Q

WEIGHTS

Maximum Zero-Fuel Weight…………………………. _____________

A

Maximum Zero-Fuel Weigh …….12,500 lbs

38
Q

WEIGHTS

Maximum Weight in Baggage Compartment: ________

A

Maximum Weight in Baggage Compartment: 550 lbs

39
Q

EMERGENCY AIRSPEEDS

One-Engine-Inoperative

Best-Angle-of-Climb (VXSE)…._____
Best-Rate-of-Climb (VYSE)…._____
Enroute Climb….______

A

Best-Angle-of-Climb (VXSE)……………………………………125 Knots
Best-Rate-of-Climb (VYSE)……………………………………..125 Knots
Enroute Climb……………………………………………………..125 Knots

40
Q

EMERGENCY AIRSPEEDS

Air Minimum Control Speeds (VMCA)

Flaps Up ….._____
Flaps Approach ….._____

A

Flaps Up ………………………………………………………………94 Knots
Flaps Approach ……………………………………………………93 Knots

41
Q

EMERGENCY AIRSPEEDS

Emergency Descent ….._____
Maximum Range Glide ….._____

A

Emergency Descent ……………………………….184 Knots
Maximum Range Glide …………135 Knots

42
Q

ENGINE FAILURE

ENGINE FIRE OR FAILURE IN FLIGHT
[ENG FIRE F/W PUSH CLOSED]

A

Affected Engine:
1. Condition Lever ………….. FUEL CUTOFF
2. Prop Lever …………………. FEATHER
3. Firewall Fuel Valve ……….CLOSE
4. Fire Extinguisher
(if fire warning persists) …ACTUATE

43
Q

ENGINE FAILURE

ENGINE FIRE ON GROUND
[ENG FIRE F/W PUSH CLOSED]

A

Affected Engine:
1. Condition Lever…………FUEL CUTOFF
2. Firewall Fuel Valve…….CLOSE
3. Starter Switch………….. STARTER ONLY
4. Fire Extinguisher
(if fire warning persists) ….. ACTUATE

44
Q

ENGINE FAILURE

EMERGENCY ENGINE SHUTDOWN ON THE GROUND

A
  1. Condition Levers………….FUEL CUTOFF
  2. Prop Levers ………………. FEATHER
  3. Firewall Fuel Valves …….CLOSE
  4. Master Switch (gang bar) ….OFF
  5. Battery Bus ………………..EMERG OFF
  6. ESIS Power ………………….OFF
45
Q

ENGINE FAILURE

ENGINE FAILURE DURING TAKEOFF (AT OR BELOW V1) — TAKEOFF ABORTED

A
  1. Power Levers………………GROUND FINE
  2. Brakes ………………………..MAXIMUM
46
Q

ENGINE FAILURE

ENGINE FAILURE DURING TAKEOFF (AT OR ABOVE V1) — TAKEOFF CONTINUED

A
  1. VR Speed
    ROTATE TO APPROX. 10° PITCH ATTITUDE
  2. Landing Gear (when positive climb established)……..UP
  3. Airspeed…..MAINTAIN V2 TO 400 FT AGL
  4. Propeller (inoperative engine)
    VERIFY FEATHERED
47
Q

ENGINE FAILURE

ENGINE FAILURE IN FLIGHT — BELOW AIR MINIMUM CONTROL SPEED (VMCA)

A
  1. Power ……………..REDUCE AS REQUIRED TO MAINTAIN CONTROL
  2. Nose ………………..LOWER TO ACCELERATE ABOVE VMCA
48
Q

ENGINE FAILURE

ELECTRICAL SMOKE OR FIRE

A
  1. Oxygen Mask(s) ……………………DON
  2. Mask Selector Switch ……………EMERG
  3. Mic Switch(es)……………………….OXY
49
Q

ENGINE FAILURE

ENVIRONMENTAL SYSTEM — SMOKE OR FUMES

A
  1. Oxygen Mask(s)……………………DON
  2. Mask Selector Switch ………..…EMERG
  3. Mic Switch(es) ……………………..OXY
50
Q

AIRSTAIR DOOR/CARGO DOOR UNLOCKED [DOOR UNLOCKED]

If the [DOOR UNLOCKED] illuminates, or if an unlatched airstair door / cargo door is suspected:

A
  1. All Occupants……………………SEATED WITH SEAT BELTS SECURELY FASTENED
51
Q

EMERGENCY DESCENT CHECKLIST

A
  1. Power Levers …………..IDLE
  2. Prop Levers ……………..FULL FORWARD
  3. Flaps (202 knots maximum)..APPROACH
  4. Landing Gear (184 knots maximum) DOWN
  5. Airspeed……….184 KNOTS MAXIMUM
52
Q

GLIDE CHECKLIST

A
  1. Landing Gear ……………………UP
  2. Flaps…………………………………UP
  3. Prop Levers ……………………. FEATHERED
  4. Airspeed ………………………….135 KNOTS
53
Q

ELECTRICAL

DUAL GENERATOR FAILURE
[L DC GEN] & [R DC GEN]
(yellow annunciator)

A
  1. Instrument Emergency Lights
    (if required)…………………..ON
  2. Generators …………….. RESET, THEN ON

If Either Generator Will Reset:

  1. Operating Generator Loadmeter ……………………………………..MONITOR
54
Q

ELECTRICAL

DUAL GENERATOR FAILURE
[L DC GEN] & [R DC GEN]
(yellow annunciator)

(continued)

If Neither Generator Will Reset:

A
  1. ECS Mode…………………………..OFF
  2. Cockpit/Cabin Blower…………AUTO
  3. Non-essential Equipment…..OFF
55
Q

ENVIRONMENTAL SYSTEMS

USE OF OXYGEN

CREW

A
  1. Oxygen Mask(s)…………………….DON
  2. Mic Switch(es)……………………….OXY
56
Q

ENVIRONMENTAL SYSTEMS

PRESSURIZATION LOSS
[CABIN ALT HI] (red annunciator)

A
  1. Oxygen Mask(s)……………………..DON
  2. Mic Switch(es)………………………..OXY
  3. Passenger Manual Drop Out….PULL ON
  4. Descend……………………..…AS REQUIRED
57
Q

ENVIRONMENTAL SYSTEMS

HIGH DIFFERENTIAL PRESSURE
[CABIN DIFF HI] (red annunciator)

A
  1. Bleed Air Valves…………….ENVIR OFF
  2. Oxygen (crew and passengers)…………….. AS REQUIRED
  3. Descend ……………………… AS REQUIRED
58
Q

ENVIRONMENTAL SYSTEMS

AUTO-DEPLOYMENT OXYGEN SYSTEM FAILURE
[CABIN ALT HI] (red) ILLUMINATED,
[PASS OXYGEN ON] (white) EXTINGUISHED

A
  1. Passenger Manual Drop Out………………..PULL ON
59
Q

ENVIRONMENTAL SYSTEMS

BLEED AIR FAIL
[L BLEED FAIL] OR [R BLEED FAIL] (red)

A
  1. Bleed Air Valve (affected engine)………… PNEU & ENVIR OFF
60
Q

SPINS

A
  1. Control Column………….. FULL FORWARD, AILERONS NEUTRAL
  2. Full Rudder………………… OPPOSITE THE DIRECTION OF SPIN
  3. Power Levers……………….IDLE
  4. Rudder………………………..NEUTRALIZE WHEN ROTATION STOPS
  5. Execute a smooth pullout.
61
Q

FLIGHT CONTROLS

UNSCHEDULED ELECTRIC PITCH TRIM ACTIVATION

A
  1. Airplane Attitude
    MAINTAIN USING ELEVATOR CONTROL
  2. AP/Trim Disconnect
    DEPRESS FULLY & HOLD
62
Q

FLIGHT CONTROLS

UNSCHEDULED RUDDER BOOST ACTIVATION

A
  1. AP/Trim Disconnect
    DEPRESS TO 1ST LEVEL AND HOLD
  2. Rudder Boost ………….OFF

If Condition Persists:

  1. YD/AP DISC
    (on Flight Guidance Panel)…..PULL DOWN
63
Q

AVIONICS

AUTOPILOT FAILURES AUTOPILOT MISTRIM [E] OR [A]
If A Mistrim Indication Continues For More Than A Few Seconds

A
  1. Flight Controls………………..HOLD FIRMLY
  2. AP ……………………………….…DISENGAGE
64
Q

AVIONICS

AUTOPILOT TRIM FAIL [TRIM]

A
  1. Flight Controls……………….HOLD FIRMLY
  2. AP …………………………………DISENGAGE
65
Q

AVIONICS

AUTOPILOT AUTOMATIC DISENGAGEMENT
If An Automatic Disengagement Occurs:

A
  1. Maintain airplane control.
  2. AP /TRIM Disconnect
    DEPRESS TO 1ST LEVEL TO CANCEL HORN
66
Q

AVIONICS

ENHANCED GROUND PROXIMITY WARNING SYSTEM
(EGPWS) (IF INSTALLED) In IMC Or At Night:

A
  1. Wings……………………………..LEVEL
  2. Power……………………….MAX ALLOWABLE
  3. Pitch………………………….INCREASE
    * Promptly and smoothly increase pitch towards an initial pitch attitude of 20º to 25º.
  • Adjust as required to avoid continuous buffeting and/or stall warning.
  • Adjust to maintain 125 KIAS.
  1. Gear and Flaps…………………..UP

Kingair 350 (2 decks)

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