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Kingair 350 > 350 > Flashcards

350 Flashcards

(66 cards)

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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
CABIN PRESSURIZATION LIMIT Maximum Cabin Pressure Differential.........._______
Maximum Cabin Pressure Differential ....... 6.6 psi
26
SYSTEMS AND EQUIPMENT LIMITS RUDDER BOOST Must be operational for ________
RUDDER BOOST Must be operational for all flights
27
SYSTEMS AND EQUIPMENT LIMITS LANDING GEAR CYCLE LIMITS Limited to _____ every ________ for a total of ________, followed by a ________ cool-down period.
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
SYSTEMS AND EQUIPMENT LIMITS BRAKE DEICE (IF INSTALLED) Is not to be operated above _____
BRAKE DEICE (IF INSTALLED) Is not to be operated above 15°C
29
ICING LIMITATIONS Min ambient temp for operation of deicing boots.... ________ Min airspeed for sustained icing flight....................... ________
Min ambient temp for operation of deicing boots............-40°C Min airspeed for sustained icing flight.......................140 knots
30
ICING LIMITATIONS [LENG ANTI-ICE] and [R ENG ANTI-ICE], shall be ___ for operation in ambient temperatures of _____ or below when ____________ _________ cannot be assured.
[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
ICING LIMITATIONS [LENG ANTI-ICE] and [R ENG ANTI-ICE], shall be ____ for ______ _________________ in ambient temperatures of above______.
[LENG ANTI-ICE] and [R ENG ANTI-ICE], shall be OFF for TAKE-OFF OPERATIONS in ambient temperatures of above +10 C.
32
AUTOPILOT Minimum engage height after takeoff Minimum use height during cruise Minimum use height during approach Minimum use height during steep approach
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
AUTOPILOT What are the maximum coupled intercept angles? Nav and Localizer ............. _____________ Back Course........................_____________
What are the maximum coupled intercept angles? Nav and Localizer .................Less than 90° Back Course...........................70°
34
WEIGHTS Maximum Ramp Weight..................................... _____________
Maximum Ramp Weight ......15,100 lbs
35
WEIGHTS Maximum Take-off Weight................................. _____________
Maximum Take-off Weight .......15,000 lbs
36
WEIGHTS Maximum Landing Weight................................. _____________
Maximum Landing Weight ......15,000 lbs
37
WEIGHTS Maximum Zero-Fuel Weight............................... _____________
Maximum Zero-Fuel Weigh .......12,500 lbs
38
WEIGHTS Maximum Weight in Baggage Compartment: ________
Maximum Weight in Baggage Compartment: 550 lbs
39
EMERGENCY AIRSPEEDS One-Engine-Inoperative Best-Angle-of-Climb (VXSE)...._____ Best-Rate-of-Climb (VYSE)...._____ Enroute Climb....______
Best-Angle-of-Climb (VXSE)..........................................125 Knots Best-Rate-of-Climb (VYSE)............................................125 Knots Enroute Climb..............................................................125 Knots
40
EMERGENCY AIRSPEEDS Air Minimum Control Speeds (VMCA) Flaps Up ....._____ Flaps Approach ....._____
Flaps Up ........................................................................94 Knots Flaps Approach ............................................................93 Knots
41
EMERGENCY AIRSPEEDS Emergency Descent ....._____ Maximum Range Glide ....._____
Emergency Descent .....................................184 Knots Maximum Range Glide .........…135 Knots
42
ENGINE FAILURE ENGINE FIRE OR FAILURE IN FLIGHT [ENG FIRE F/W PUSH CLOSED]
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
ENGINE FAILURE ENGINE FIRE ON GROUND [ENG FIRE F/W PUSH CLOSED]
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
ENGINE FAILURE EMERGENCY ENGINE SHUTDOWN ON THE GROUND
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
ENGINE FAILURE ENGINE FAILURE DURING TAKEOFF (AT OR BELOW V1) --- TAKEOFF ABORTED
1. Power Levers..................GROUND FINE 2. Brakes .............................MAXIMUM
46
ENGINE FAILURE ENGINE FAILURE DURING TAKEOFF (AT OR ABOVE V1) --- TAKEOFF CONTINUED
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
ENGINE FAILURE ENGINE FAILURE IN FLIGHT --- BELOW AIR MINIMUM CONTROL SPEED (VMCA)
1. Power .................REDUCE AS REQUIRED TO MAINTAIN CONTROL 2. Nose ....................LOWER TO ACCELERATE ABOVE VMCA
48
ENGINE FAILURE ELECTRICAL SMOKE OR FIRE
1. Oxygen Mask(s) ........................DON 2. Mask Selector Switch ...............EMERG 3. Mic Switch(es)............................OXY
49
ENGINE FAILURE ENVIRONMENTAL SYSTEM --- SMOKE OR FUMES
1. Oxygen Mask(s)........................DON 2. Mask Selector Switch ...........…EMERG 3. Mic Switch(es) ..........................OXY
50
AIRSTAIR DOOR/CARGO DOOR UNLOCKED [DOOR UNLOCKED] If the [DOOR UNLOCKED] illuminates, or if an unlatched airstair door / cargo door is suspected:
1. All Occupants........................SEATED WITH SEAT BELTS SECURELY FASTENED
51
EMERGENCY DESCENT CHECKLIST
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
GLIDE CHECKLIST
1. Landing Gear ........................UP 2. Flaps.......................................UP 3. Prop Levers ......................... FEATHERED 4. Airspeed ...............................135 KNOTS
53
ELECTRICAL DUAL GENERATOR FAILURE [L DC GEN] & [R DC GEN] (yellow annunciator)
1. Instrument Emergency Lights (if required)......……………..ON 2. Generators ................. RESET, THEN ON If Either Generator Will Reset: 3. Operating Generator Loadmeter ……………………………………..MONITOR
54
ELECTRICAL DUAL GENERATOR FAILURE [L DC GEN] & [R DC GEN] (yellow annunciator) (continued) If Neither Generator Will Reset:
4. ECS Mode................................OFF 5. Cockpit/Cabin Blower............AUTO 6. Non-essential Equipment.....OFF
55
ENVIRONMENTAL SYSTEMS USE OF OXYGEN CREW
1. Oxygen Mask(s).........................DON 2. Mic Switch(es)............................OXY
56
ENVIRONMENTAL SYSTEMS PRESSURIZATION LOSS [CABIN ALT HI] (red annunciator)
1. Oxygen Mask(s)..........................DON 2. Mic Switch(es).............................OXY 3. Passenger Manual Drop Out....PULL ON 4. Descend..........................…AS REQUIRED
57
ENVIRONMENTAL SYSTEMS HIGH DIFFERENTIAL PRESSURE [CABIN DIFF HI] (red annunciator)
1. Bleed Air Valves................ENVIR OFF 2. Oxygen (crew and passengers)................. AS REQUIRED 3. Descend ........................... AS REQUIRED
58
ENVIRONMENTAL SYSTEMS AUTO-DEPLOYMENT OXYGEN SYSTEM FAILURE [CABIN ALT HI] (red) ILLUMINATED, [PASS OXYGEN ON] (white) EXTINGUISHED
1. Passenger Manual Drop Out....................PULL ON
59
ENVIRONMENTAL SYSTEMS BLEED AIR FAIL [L BLEED FAIL] OR [R BLEED FAIL] (red)
1. Bleed Air Valve (affected engine)............ PNEU & ENVIR OFF
60
SPINS
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
FLIGHT CONTROLS UNSCHEDULED ELECTRIC PITCH TRIM ACTIVATION
1. Airplane Attitude MAINTAIN USING ELEVATOR CONTROL 2. AP/Trim Disconnect DEPRESS FULLY & HOLD
62
FLIGHT CONTROLS UNSCHEDULED RUDDER BOOST ACTIVATION
1. AP/Trim Disconnect DEPRESS TO 1ST LEVEL AND HOLD 2. Rudder Boost .............OFF If Condition Persists: 3. YD/AP DISC (on Flight Guidance Panel).....PULL DOWN
63
AVIONICS AUTOPILOT FAILURES AUTOPILOT MISTRIM [E] OR [A] If A Mistrim Indication Continues For More Than A Few Seconds
1. Flight Controls....................HOLD FIRMLY 2. AP .....................................…DISENGAGE
64
AVIONICS AUTOPILOT TRIM FAIL [TRIM]
1. Flight Controls...................HOLD FIRMLY 2. AP .......................................DISENGAGE
65
AVIONICS AUTOPILOT AUTOMATIC DISENGAGEMENT If An Automatic Disengagement Occurs:
1. Maintain airplane control. 2. AP /TRIM Disconnect DEPRESS TO 1ST LEVEL TO CANCEL HORN
66
AVIONICS ENHANCED GROUND PROXIMITY WARNING SYSTEM (EGPWS) (IF INSTALLED) In IMC Or At Night:
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. 4. Gear and Flaps.......................UP

Kingair 350 (2 decks)

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