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Emb 120 EP and Limitations > Emb 120 limitations > Flashcards

Emb 120 limitations Flashcards

1
Q

Ramp

A

26,609 lbs

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2
Q

Takeoff

A

26,433 lbs

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3
Q

Landing

A

25,794 lbs

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4
Q

Zero Fuel

A

24,030 lbs

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5
Q

Cargo

A

1,543 lbs

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6
Q

T6

T/O/Max continuous

A

800 C

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7
Q

T6

T/O/Emergency 5 min max

A

816 C

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8
Q

T6

Start: 816 C - 850 C

A

20 sec

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9
Q

T6

Start: 850 C - 950 C

A

5 sec

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10
Q

T6

Warning at

A

816 C

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11
Q

T6

SkyWest climb limit

A

720 C

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12
Q

Torque

T/O/Max continuous

A

100%

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13
Q

Torque

T/O/Emergency 5 min max

A

110%

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14
Q

Torque

Transient (up to 20 sec)

A

120%

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15
Q

NP

Max continuous

A

100%

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16
Q

NP

Max continuous tolerance.

A

100% to 101.0%

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17
Q

NP

Transient (up to 20 sec)

A

110%

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18
Q

NP

Max reverse

A

80.5%

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19
Q

NP

Max ground ops

A

65%

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20
Q

NP

Minimum NP for takeoff

A

99.5%

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21
Q

NP

Minimum NP in icing conditions

A

85%

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22
Q

NP

Aux gen energize at

A

70%

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23
Q

Cruise max torque

NP at 100%

A

72%

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24
Q

Cruise max torque

NP at 90%

A

80%

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25
Q

Cruise max torque

NP at 85%

A

84%

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26
Q

Cruise max torque

NP at 80%

A

84%

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27
Q

NH limits

T/O Max continuous (118A)

A

102%

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28
Q

NH limits Minimum

NH for operation of deice equipment

A

80%

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29
Q

Overspeed limited

oil presssure

A

103%

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30
Q

Overspeed limited

fuel flow

A

109%

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31
Q

EEC on

Condition Lever @ min

A

NH-62%, Np-50%

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32
Q

EEC on

Condition Lever @ max

A

NH-72%, Np-65%

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33
Q

Ground idle, EEC off

A

NH > 50%

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34
Q

VMO at 13,000 ft

A

272 KIAS

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35
Q

VA

A

200 KIAS

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36
Q

VB

A

175 KIAS

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37
Q

VLO/LE

A

200 KIAS

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38
Q

15 SKW

A

180 KIAS

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39
Q

25

A

150 KIAS

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40
Q

45

A

135 KIAS

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41
Q

Max wiper speed

A

160 KIAS

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42
Q

Max DV window open speed

A

140 KIAS

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43
Q

Max Tail Wind component

A

10 kts

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44
Q

Minimum single engine autopilot speed

A

120 KIAS

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45
Q

Max demonstrated crosswind

A

30 kts

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46
Q

Minimum ILS coupled autopilot altitude

A

200’ AGL

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47
Q

of emergency exits (+flt deck)

A

4 (6)

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48
Q

Oil temp

Min. start (red radial)

A

-40 C

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49
Q

Oil temp

Takeoff Max continuous (118A)

A

45 to 115 C

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50
Q

Oil temp

Transient (20 min) +(118A)

A

115 to 125 C

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51
Q

Oil temp

Minimum to unfeather prop

A

0 C

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52
Q

Oil temp

Minimum to feather prop

A

10 C

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53
Q

Oil Pres

Minimum ground idle (red radial)

A

40 psid

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54
Q

Oil Pres

Power flight idle and NH < 75%

A

40 to 55 psid

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55
Q

Oil Pres

Takeoff Max continuous

A

55 psid to 65 psid

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56
Q

Oil Pres

Electric feather pump duty cycle

A

20 sec / 6 consecutive cycles

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57
Q

Oil Pres

Prop tip clearance

A

18 in

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58
Q

Oil Pres

Prop feather before shutdown

A

20 sec

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59
Q

Power lever angle of

A

62

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60
Q

and torque of

A

62%

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61
Q

Autofeather activates when one torque drops below

A

22%

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62
Q

White ignition light on from

A

0% to 50%

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63
Q

Starter 1st Attempt: 30 sec ON

A

3 min OFF

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64
Q

Starter 2nd Attempt: 30 sec ON

A

3 min OFF

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65
Q

Starter 3rd Attempt: 30 sec ON

A

30 min OFF

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66
Q

Starter Cold weather (oil temp <10)

A

2 start attempts

67
Q

EEC ON, ENGINE BLEED OPEN

A

FL320

68
Q

EEC ON, ENGINE BLEED CLSD

A

FL250

69
Q

EEC OFF, ENGINE BLEED OPEN

A

FL250

70
Q

EEC OFF, ENGINE BLEED CLSD

A

FL200

71
Q

PA

EEC off

A

10,000’

72
Q

PA

EEC on

A

8,000’

73
Q

RVSM restriction

A

FL280

74
Q

Temp

MINIMUM

A

-54 C

75
Q

Temp

MAXIMUM EFIS

A

ISA + 35 C

76
Q

Temp

MAXIMUM FIS

A

ISA + 38 C

77
Q

Total per tank

A

2,866 lbs

78
Q

Max fuel imbalance

A

600 lbs

79
Q

Unusable fuel per wing

A

24 lbs

80
Q

Dripless sticks per wing

A

4

81
Q

Add__ to unusable fuel per wing when main ejector pump inop

A

79.6 lbs

82
Q

Anti-skid disabled below

A

6 knots

83
Q

Braking not possible on landing until wheel speed

A

is 50 knots or 3 sec. after touchdown, whichever occurs first

84
Q

After T/O, landing gear warning inhibited for

A

1 minute

85
Q

Pusher inhibited for

A

5 sec after T/O and again above 173 KIAS

86
Q

Pusher armed slowing below

A

153 KIAS

87
Q

NWS tiller steering

A

50

88
Q

NWS rudder pedal steer

A

7

89
Q

Rudder green system disabled

A

> 120 KIAS

90
Q

Green Hydraulic system

A 
outboard brakes
outboard flaps
rudder
landing gear
cabin door
steering
91
Q

Blue Hydraulic System

A 
inboard brakes
inboard flaps
nacelle flaps
emergency brakes
rudder
92
Q

Norm. battery voltage

A

24 V

93
Q

Min batt. volts for APU start

A

22 V

94
Q

Hot battery bus items:

A 
Door
Courtesy lights
Auto transfer
DC indicator
Fire extinguisher
Fuel Shut Off Valve
Hydraulic Shut Off Valve
95
Q

Gen Main

A

400 A

96
Q

> 27,000 ft or ISA +27 C

A

380 C

97
Q

Auxiliary

A

150 A

98
Q

> 18,000 ft

A

140 C

99
Q

Battery temp warning

A

70 C

100
Q

GPU power overrides

A

APU power

101
Q

Main generator power overrides

A

GPU power

102
Q

Backup battery

A

24 V 5 A

103
Q

Backup battery powers standby attitude indicator when emergency bus drops to less than __ volts

A

19 volts

104
Q

Functions of backup batter

A

stabilizes current

105
Q

Powers standby gyro after emergency bus drops below

A

19 volts

106
Q

Generators parallel within

A

10% of each other

107
Q

Max speed, nose tires

A

183 Kts

108
Q

Max speed, main tires

A

165 Kts

109
Q

Hydroplane, nose tires

A

80 Kts

110
Q

Hydroplane, main tires

A

103 Kts

111
Q

FIRE PROTECTION Fire handle activates

A 
Fuel Shut Off Valve
Hyd Shut Off Valve
Bleed Shut Off Valve
Electric feather system
Engine deice valves
112
Q

P3 Bleed air used for

A 
Pressurization/environmental
Pneumatic deice
Hydraulic reservoir pressurization
Engine labyrinth seals
109% overspeed protection
Vacuum for pressurization
113
Q

Normal cabin diff press

A

7.0 psi

114
Q

Max cabin differential pressure

A

7.2 psi

115
Q

Inward press relief at

A

-.3 psi

116
Q

Electric controller dump limit

A

13,000 ft

117
Q

Climb

A

650 FPM

118
Q

Descent

A

450 FPM

119
Q

Cabin alt light

A

10,000 ft

120
Q

Cabin pressurizes to __ feet below field elevation on T/O

A

-300 feet

121
Q

Boot Cycles On/off

A

6 sec/ 54 sec

122
Q

Prop cycles COLD on/off

A

20 Sec/ 60 sec

123
Q

Prop cycles NORM on\/off

A

10 sec/ 60 sec

124
Q

Intake boot cycle on/off

A

6 sec/174 sec

125
Q

APU 1st attempt 30 sec ON

A

3 min OFF

126
Q

APU 2nd attempt 30 sec ON

A

3 min OFF

127
Q

APU 3rd attempt 30 sec ON

A

3 min OFF

128
Q

APU 4th attempt 30 sec ON

A

30 min OFF

129
Q

Auto shutdown in flight

A

a) Gen overvoltage

b) Overspeed

130
Q

Max start EGT

A

<50% 974 C

131
Q

Max EGT

A

> 90% 732 C

132
Q

Altitude Garrett

A

-1,000 to 20,000 ft

133
Q

Airspeed Garrett

A

135 to 200 KIAS

134
Q

APU start contact engaged from

A

0% to 50%

135
Q

Garrett Up to 16,000 ft

A

ISA + 38 C

136
Q

Garrett above 16,000 ft

A

ISA +35 C

137
Q

Garett APU
Up to ISA +35 C
<16,000 ft

A

400A

138
Q

Garett APU
Up to ISA +35 C
>16,000 ft

A

290 A

139
Q

Garrett APU
Greater than ISA + 35 C
<15,000 ft

A

400A

140
Q

Garrett APU Greater than ISA + 35 C

15,000 ft

A

280 A

141
Q

Dry Snow

A

MORE THAN 6500 FEET 4 INCHES

6500 FEET OR LESS 2 INCHES

142
Q

WET SNOW

A

MORE THAN 6500 FEET 2 INCHEs

6500 FEET OR LESS 1 INCH

143
Q

SLUSH/STANDING WATER

A

MORE THAN 6500 FEET 1 INCH

6500 FEET OR LESS 1/2 INCH

144
Q

Normal Passenger Oxygen pressure

A

1850 PSI @ 21 C

145
Q

Main bottle with Passengers

A

1400 PSI

146
Q

Main bottle without Passengers

A

800 PSI

147
Q

Cabin portable bottle

A

1200 PSI

148
Q

Passenger O2 mask drop at

A

14,000 CPA

149
Q

QRH

A

A

Cabin Fire or Smoke

  1. Crew oxygen masks… DON, SELECT 100%
  2. Recirculation and gasper fans… OFF
  3. Smoke goggles… DON
  4. Crew communication… ESTABLISH
150
Q

QRH

B.

A

Rapid Depressurization

  1. Crew oxygen masks… DON, SELECT 100%
  2. Crew communication… ESTABLISH
151
Q

QRH

C.

A

Propeller Overspeed - Np Above 103%
Identify the affected engine and proceed:
1. Power lever… FLT IDLE
2. Condition lever… FEATHER, THEN CHECK
3. Airspeed… BELOW 180 KIAS
4. Flaps… 15
5. Airspeed… 125 KIAS MIMIMUM
In case no feathering is observed:
6. Electric feather switch… ON, THEN CHECK FEATHER

152
Q

QRH

D.

A 
Emergency Evacuation
1. Parking brake... ON
2. Pressurization system... DUMP
3. Condition levers... FUEL CUT OFF
4. Fire handles... SQUEEZE AND PULL
5. Agent A and B (if necessary)... DISCHARGE
6. APU SHUTOFF/EXTG switch... CLOSE
7.APU SHUTOFF/EXTG switch (if necessary)... EXTG
8. Emergency lights... ON
9. Evacuation... INITIATE
"EVACUATE! EVACUATE! EVACUATE!"
10. Power select switch, backup battery... OFF
Pull CVR circuit breaker H14
153
Q

QRH

E.

A

Engine Failure, Propeller Did Not Feather
Identify the affected engine and proceed
1. Power lever… FLT IDLE
2. Condition lever… Feather, THEN CHECK
In case no feathering is observed:
3. Electric feather switch, ON, THEN CHECK FEATHER

154
Q

QRH

F.

A

Electric Trim Runaway

  1. Elevator trim wheel… HOLD
  2. AP/TRIM/PUSHER DISC switch… PRESS AND HOLD
  3. Autopilot transfer switch… PRESS
155
Q

QRC

A

A

Engine Fire on the Ground

156
Q

QRC

B

A

Engine Fire in Flight

157
Q

QRC

C

A

Auxiliary Power Unit Fire

158
Q

QRC

D

A

Class-C Baggage Compartment Fire or Smoke

159
Q

QRC

E

A

Inadvertent Propeller Feather

160
Q

QRC

F

A

Battery Overheat

161
Q

QRC

G

A

Emergency Descent

162
Q

QRC

H

A

Windshield Overheat

163
Q

NP

Max speed for setting NP to 100%

A

200 KIAS

Emb 120 EP and Limitations (1 decks)

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