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King Air > kingair_350_20121215045734 > Flashcards

kingair_350_20121215045734 Flashcards

2
Q

Engine Fire/Failure in Flight

A

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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3
Q

EMERGENCY ENGINE SHUTDOWN ON THE GROUND

A
  1. 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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4
Q

ENGINE FAILURE DURING TAKEOFF AT/BELOW V1 - TAKEOFF ABORTED

A
  1. Power Levers - GROUND FINE2. Brakes - MAXIMUM (or as required to achieve desired stopping distance)
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5
Q

ENGINE FAILURE DURING TAKEOFF AT/ABOVE V1 - TAKEOFF CONTINUED

A
  1. 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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6
Q

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

A

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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7
Q

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

A

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

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8
Q

ENGINE FAILURE IN FLIGHT BELOW Vmca

A
  1. Power - REDUCE AS REQUIRED TO MAINTAIN CONTROL2. Nose - LOWER TO ACCELERATE ABOVE Vmca
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9
Q

GLIDE (BOTH ENGINES INOPERATIVE)

A
  1. 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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10
Q

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

A
  1. 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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11
Q

UNSCHEDULED ELECTRIC PITCH TRIM ACTIVATION

A
  1. Aircraft attitude - MAINTAIN WITH ELEVATOR CONTROL2. AP/Trim disconnect - DEPRESS FULLY (Pitch Trim OFF) - ILLUMINATED
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12
Q

UNSCHEDULED RUDDER BOOST ACTIVATION

A
  1. AP/Trim disconnect - DEPRESS/HOLD (FIRST LEVEL)2. Rudder boost - OFFIf condition persists:3. Rudder boost circuit breaker - PULL
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13
Q

SPINS

A

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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14
Q

WINDSHIELD ELECTRICAL FAULT

A
  1. WSHLD ANTI-ICE switches - OFFIf smoke and/or fire does not cease:2. ELECTRICAL SMOKE OR FIRE Checklist - CONDUCT
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15
Q

ELECTRICAL SMOKE OR FIRE

A

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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16
Q

ENVIRONMENTAL SYSTEM SMOKE OR FUMES

A

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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17
Q

AIRSTAIR/CARGO DOOR UNLOCKED

A

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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18
Q

EMERGENCY DESCENT

A
  1. 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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19
Q

OXYGEN USE

A

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

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20
Q

PRESSURIZATION LOSS [CABIN ALT HI]

A
  1. 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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21
Q

HIGH DIFFERENTIAL PRESSURE

A
  1. Bleed air valve switches - ENVIR OFF2. Oxygen (crew and passengers) - AS REQUIRED3. Descend as required
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22
Q

AUTO-DEPLOYMENT OXYGEN SYSTEM FAILURE

A

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

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23
Q

BLEED AIR FAILURE

A

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

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24
Q

AUTOPILOT MISTRIM [E] or [A]

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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25
Q

AUTOPILOT TRIM FAIL [TRIM]

A
  1. Flight controls - HOLD FIRMLY2. AP - DISENGAGE
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26
Q

AUTOPILOT AUTOMATIC DISENGAGEMENT

A

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

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27
Q

EGPWS in IMC or NIGHT

A
  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
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28
Q

TAWS+ in IMC or NIGHT

A
  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
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74
Q

MIN CREW

A

ONE PILOT

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75
Q

PAX SEATING LIMITATIONS

A

15 PAX MAX

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76
Q

LOAD FACTOR FLAPS DOWN NEGATIVE

A

0 Gs

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77
Q

LOAD FACTOR FLAPS DOWN POSITIVE

A

1.1 Gs

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78
Q

LOAD FACTOR FLAPS UP NEGATIVE

A

-1.24 Gs

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79
Q

LOAD FACTOR FLAPS UP POSITIVE

A

3.1 Gs

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80
Q

MAX OPERATING ALTITUDE WITH AVGAS AND BOTH STBY BOOST PUMPS OPERATIVE

A

35,000 FT

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81
Q

MAX OPERATING ALTITUDE

A

35,000 FT

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82
Q

MAX OPERATING ALTITUDE AVGAS EITHER STBY BOOST PUMT INOP

A

FLIGHT PROHIBITED

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83
Q

MAX ALLOWABLE TAKEOFF WEIGHT

A

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

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84
Q

MAX LANDING WEIGHT

A

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

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85
Q

MAX RAMP WEIGHT

A

15,100 LBS

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86
Q

MAX ZERO FUEL WEIGHT

A

12,500 LBS

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87
Q

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

A

125 KIAS

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88
Q

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

A

125 KIAS

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89
Q

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

A

125 KIAS

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90
Q

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

A

94 KIAS

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91
Q

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

A

93 KIAS

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92
Q

EMERGENCY AIRSPEEDS (15,000 LBS)EMERGENCY DESCENT SPEED

A

184 KIAS

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93
Q

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

A

135 KIAS

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94
Q

MAX DEMO’D CROSSWIND

A

20 KTS

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95
Q

MAX TAILWIND

A

10 KTS

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96
Q

SINGLE ENGINE ENROUTE CLIMB

A

125 KIAS

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97
Q

MANEUVERING SPEED (VA)

A

184 KTS

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98
Q

MAX FLAP EXTENSION/EXTENDED SPEED (VFE) APPROACH

A

202 KIAS

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99
Q

MAX FLAP EXTENSION/EXTENDED SPEED (VFE) FULL

A

158 KIAS

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100
Q

MAX LANDING GEAR EXTENDED SPEED (VLE)

A

184 KIAS

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101
Q

MAX LANDING GEAR OPERATING SPEED (VLO) EXTENSION

A

184 KIAS

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102
Q

MAX LANDING GEAR OPERATING SPEED (VLO) RETRACTION

A

166 KIAS

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103
Q

AIR MIN CONTROL SPEED (VMCA) PROP FEATHERED FLAPS UP

A

96 KIAS

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104
Q

AIR MIN CONTROL SPEED (VMCA) PROP FEATHERED FLAPS APPROACH

A

94 KIAS

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105
Q

MAX OPERATING SPEED (VMO)

A

263 KIAS/0.58 MACH

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106
Q

AIRCRAFT HEIGHT

A

14’ 4”

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107
Q

AIRCRAFT LENGTH

A

46’ 8”

108
Q

AIRCRAFT WINGSPAN

A

57’ 11”

109
Q

AFT FACING SEATS TAKEOFF RESTRICTION

A

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

110
Q

AUTOPILOT MAX COUPLED INTERCEPT ANGLE FOR BACK COURSE

A

70°

111
Q

AUTOPILOT MAX COUPLED INTERCEPT ANGLE FOR NAV/LOC

A

LESS THAN 90°

112
Q

AUTOPILOT MIN ALT FOR APPROACH

A

200 FT AGL

113
Q

AUTOPILOT MIN ALT FOR CRUISE

A

1,000 FT AGL

114
Q

AUTOPILOT MIN ALT FOR STEEP APPROACH

A

160 FT AGL

115
Q

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

A

20 VDC

116
Q

EXTERNAL POWER AMPS LIMITS: MOMENTARY

A

1,000 AMPS

117
Q

EXTERNAL POWER AMPS LIMITS: CONTINUOUS

A

300 AMPS

118
Q

EXTERNAL POWER VOLTAGE RANGE

A

28 TO 28.4 VOLTS

119
Q

GENERATOR LOAD LIMITS ABOVE 34,000 FT

A

95%

120
Q

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

A

75%

121
Q

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

A

100%

122
Q

GENERATOR LOAD LIMITS SL TO 34,000 FT

A

100%

123
Q

MIN BATTERY VOLTS FOR BATTERY START

A

23 VDC

124
Q

STARTER DUTY CYCLE

A

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

125
Q

For fuel system, fill the _______ tanks first.

A

MAIN

126
Q

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

A

YELLOW265

127
Q

FUEL CROSSFEED PERMITTED ONLY WHEN

A

ONE ENGINE INOP

128
Q

MAX FUEL IMBALANCE

A

300 LBS

129
Q

AUX SYSTEM FUEL QUANTITY

A

79.5 U.S. GAL / 533 LBS

130
Q

MAIN SYSTEM FUEL QUANTITY

A

190 U.S. GAL / 1,273 LBS

131
Q

TOTAL USABLE FUEL QUANTITY

A

539 U.S. GAL / 3,611 LBS

132
Q

WHEN IS ENGINE ANTI-ICE REQUIRED?

A

+5° C IN VISIBLE MOISTURE

133
Q

MIN TEMP FOR DEICING BOOTS OPERATIONS

A

-40° C

134
Q

MIN AIRSPEED FOR SUSTAINED OPS IN ICING

A

140 KTS

135
Q

MAIN LANDING GEAR STRUT EXTENSION (INCHES)

A

3.23 TO 3.49 INCHES

136
Q

NOSE LANDING GEAR STRUT EXTENSION (INCHES)

A

3.77 TO 4.06 INCHES

137
Q

BRAKES DEICE TEMP OPERATION LIMITE

A

NOT ABOVE 15° C

138
Q

LANDING GEAR CYCLE LIMITS

A

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

139
Q

MAX CABIN PRESSURE DIFFERENTIAL

A

6.6 PSI

140
Q

CABIN DIFFERENTIAL PRESSURE (GREEN ARC)

A

0 TO 6.6 PSI

141
Q

CABIN DIFFERENTIAL PRESSURE (RED ARC)

A

6.6 PSI AND UP

142
Q

When does the “CABIN ALTITUDE” light illuminate?

A

ABOVE 10,000 FT CABIN ALT

143
Q

When does the “CABIN ALTITUDE HI” light illuminate?

A

ABOVE 12,000 FT CABIN ALT

144
Q

When do the passenger mask automatically deploy?

A

ABOVE 12,500 FT CABIN ALT

145
Q

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

A

13,000 FT

146
Q

The “CABIN DIFF HI” light illuminates at what PSID?

A

6.9 PSID

147
Q

ENGINE MODEL NUMBER AND TYPE

A

PT6A-60A, TURBOPROP

148
Q

PROPELLER TYPE

A

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

149
Q

MAX N1 CRUISE CLIMB

A

104%

150
Q

N1

A

62% MIN

151
Q

MAX N1 MAX CRUISE

A

104%

152
Q

MAX TRANSIENT N1

A

104%

153
Q

MAX ITT CRUISE

A

820° C

154
Q

MAX ITT CRUISE CLIMB

A

785° C

155
Q

MAX ITT IDLE

A

750° C

156
Q

MAX CONTINUOUS ITT

A

820° C

157
Q

MAX ITT REVERSE

A

760° C

158
Q

ENGINE STARTING MAX TRANSIENT ITT

A

1,000° C FOR 5 SEC

159
Q

MAX TAKEOFF ITT

A

820° C

160
Q

ENGINE MAX ITT TRANSIENT

A

850° C FOR 20 SEC

161
Q

NORMAL OIL PRESSURE FOR CRUISE CLIMB

A

90 TO 135 PSI

162
Q

ENGINE OIL PRESSURE IDLE

A

60 PSI MIN

163
Q

MAX CONTINUOUS OIL PRESSURE

A

90 TO 135 PSI

164
Q

MAX CRUISE OIL PRESSURE

A

90 TO 135 PSI

165
Q

MAX REVERSE OIL PRESSURE

A

90 TO 135 PSI

166
Q

ENGINE OIL PRESSURE STARTING

A

0 TO 200 PSI

167
Q

NORMAL TAKEOFF OIL PRESSURE

A

90 TO 135 PSI

168
Q

ENGINE OIL PRESSURE TRANSIENT

A

200 PSI

169
Q

ENGINE OIL TEMP CRUISE CLIMB

A

0° TO 110° C

170
Q

ENGINE OIL TEMP IDLE

A

-40° TO 110° C

171
Q

MAX CONTINUOUS OIL TEMP

A

0 TO 110° C

172
Q

ENGINE OIL TEMP MAX CRUISE

A

0 TO 110° C

173
Q

ENGINE OIL TEMP MAX REVERSE

A

0 TO 99° C

174
Q

ENGINE OIL TEMP MIN FOR FUEL HEAT AT T/O

A

55° C (RECOMMENDED)

175
Q

ENGINE PROP RPM (N2) CRUISE CLIMB

A

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

176
Q

ENGINE PROP RPM (N2) IDLE

A

1,050 MIN

177
Q

ENGINE PROP RPM (N2) MAX CONTINUOUS

A

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

178
Q

MAX CRUISE N2

A

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

179
Q

MAX REVERSE N2

A

1,650 RPM

180
Q

MAX TAKEOFF N2

A

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

181
Q

MAX TRANSIENT N2

A

1,870 RPM FOR 20 SEC

182
Q

ENGINE TORQUE% MAX CONTINUOUS

A

100% (UP TO 102% FOR 7 MINUTES)

183
Q

MAX TORQUE% FOR TAKEOFF

A

100% (UP TO 102% FOR 7 MINUTES)

184
Q

ENGINE TORQUE LIMITE BELOW 1,000 RPM N2

A

62%

185
Q

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

A

It would feather

186
Q

What is the range of the primary governor?

A

1,450 to 1,700 RPM

187
Q

The overspeed governor governs to _____.

A

1,768 RPM

190
Q

TERMINAL AREA (TWO ENG)

A
  • 180 KIAS
  • 40% TORQUE
  • 1,500 RPM
  • GEAR UP
  • FLAPS 0
191
Q

APPROACH (TWO ENG)

A
  • 180 KIAS
  • 25% TORQUE
  • 1,500 RPM
  • GEAR UP
  • FLAPS APPR
192
Q

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

A
  • 130 KIAS
  • 25 % TORQUE
  • 1,700 RPM
  • GEAR DOWN
  • FLAPS APPR
193
Q

NON-PRECISION FAF INBOUND (TWO ENGINE)

A
  • 130 KIAS
  • 25% TORQUE
  • 1,700 RPM
  • GEAR DOWN
  • FLAPS APPR
194
Q

CIRCLE TO LAND / MDA (TWO ENG)

A
  • 130 KIAS
  • 40% TORQUE
  • 1,700 RPM
  • GEAR DOWN
  • FLAPS APPR
195
Q

STEEP TURNS

A
  • 180 KIAS
  • 52% TORQUE
  • 1,500 RPM
  • GEAR UP
  • FLAPS 0
196
Q

TERMINAL AREA (SINGLE ENG)

A
  • 180 KIAS
  • 80% TORQUE
  • 1,700 RPM
  • GEAR UP
  • FLAPS 0
197
Q

APPROACH (SINGLE ENG)

A
  • 130 KIAS
  • 60% TORQUE
  • 1,700 RPM
  • GEAR UP
  • FLAPS APPR
198
Q

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

A
  • 130 KIAS
  • 50% TORQUE
  • 1,700 RPM
  • GEAR DOWN
  • FLAPS APPR
199
Q

NON-PRECISION FAF INBOUND ( SINGLE ENG)

A
  • 130 KIAS
  • 50% TORQUE
  • 1,700 RPM
  • GEAR DOWN
  • FLAPS APPR
200
Q

CIRCLE TO LAND/MDA (SINGLE ENG)

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

King Air (1 decks)

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