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Phenom 300 QRC > Limitations > Flashcards

Limitations Flashcards

1
Q

What are the crosswind Limits?

A

Takeoff - Static - 18 Knots; Rolling - 25 knots
Landing - 28 knots
Contaminated Runway Width: > or = to 150 ft: 15 kts; < or = 149 ft: 10 kts

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2
Q

What are the contaminated runway crosswind Limits?

A

Greater than or equal to 150’ width - 15 kts

Less than or equal to 149’ width - 10 kts

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3
Q

What is the max tailwind?

A

10 kts

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4
Q

What is the maximum ramp and taxi weight?

A

18497 lbs

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5
Q

What is the maximum takeoff weight?

A

18387 pounds

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6
Q

What is the maximum landing weight?

A

17042 lbs

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7
Q

What is the turbulence penetration airspeed (Vra/Mra)?

A

232 kts/ .65M

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8
Q

What is the min climb speed above FL180?

A

225 kts / .60M

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9
Q

What is maneuvering speed (Va)?

A

205 kts

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10
Q

What is the max landing gear operating/extended speed (Vlo/Vle)?

A

250 kts

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11
Q

What is the max Flaps 1 extended speed?

A

180 kts

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12
Q

What is the maximum speed for Flaps 2/3 extended?

A

170 kts

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13
Q

What is the maximum speed for Flaps Max extended?

A

160

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14
Q

What is the min speed in icing with WING STAB inhibited?

With WING STAB uninhibited?

A

165 kts

150 kts

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15
Q

What is the max speed in icing with YAW DAMP off?

A

180 kts

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16
Q

What is the max differential pressure for takeoff and landing?

A

.2 psi

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17
Q

What is the min two engine autopilot engagement height?

Min use height?

A

600’ to engage, do not use below 195’

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18
Q

What is the min engagement height for the autopilot with one engine inoperative (OEI)? Min use height?

A

1000’ to engage, don’t use below 220’

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19
Q

What is the min voltage for BATT start?

A

24 V

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20
Q

What is the min GPU voltage to charge the battery?

A

27V

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21
Q

What is the min temp for the WING STAB below 16000 ft?

A

-40 C

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22
Q

What is the min temp for the WING STAB at or above 16000 ft?

A

-45 C

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23
Q

What is the straight-in approach category for the Phenom 300?

A

CAT B or C (CAT B = 91 - 120 kts; CAT C = 121 - 140 kts)

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24
Q

What are the approach categories for a circling approach?

A

CAT C or D (CAT C = 121 - 140 kts; CAT D = 141 - 165 kts)

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25
Q

What is the time limit for maximum continuous thrust (MCT)?

A

10 min

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26
Q

What is the time limit for takeoff thrust?

A

5 min

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27
Q

What are the transient limits (20 sec) for N1, N2, ITT?

A

N1 - 102%, N2 - 103%, ITT - 765 C

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28
Q

What is the oil pressure transient (20 sec) limit?

A

0-20 psi

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29
Q

What is the low oil pressure limit?

A

20-270 psi for not longer than 400 sec

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30
Q

What are the engine starter cool down times?

A

1st and 2nd start - 1 min
3rd start - 15 min
4th start - 30 min

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31
Q

What is the max ZFW?

A

14220 lbs

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32
Q

What is the usable fuel on the aircraft?

A

5353 lbs

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33
Q

What is the maximum total fuel load?

A

5401 lbs

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34
Q

What is the Mmo/Vmo?

A

.78M / 320kts

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35
Q

How big a hangar would we need?

A

60x60x20

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36
Q

What checklist is not a “flow”?

A

Power on

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37
Q

How long would the battery last (approximately)?

A

11-12 min

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38
Q

What does it take to get the avail light from the GPU?

A

25-30v

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39
Q

Which light on the aircraft is not an LED light?

A

INSP light (left wing only)

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40
Q

What is the maximum weight in the forward baggage?

A

110 lbs

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41
Q

What is the maximum weight in the aft baggage?

A

463 lbs

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42
Q

How long does the courtesy light stay illuminated?

A

5 min

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43
Q

What is the engine on the Phenom?

A

Pratt & Whitney 535E

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44
Q

What is the minimum temp for a battery start of the engines?

A

-18 C

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45
Q

What is planned taxi fuel? What is normal reserve fuel?

A

110 lbs

1121 lbs

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46
Q

What is the maximum fuel imbalance?

A

220 lbs

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47
Q

When do you have to confirm the database for the Garmin 3000 under NJA rules?

A

Before the 1st flight of the day. (Garmin - 7 day delay?)

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48
Q

Where does the FADEC get its power?

A

PMA (Permanent Magnet Alternator) or 28vdc ships power, whichever provides more

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49
Q

When you do the after start electrical emergency start, what is the minimum voltage?

A

23.5 v

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50
Q

How many passengers can a NJA Phenom carry by its rules? How many seats are there?

A

8, 7

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51
Q

What lights should you see during ANN test on the TEST panel?

A

2 on CVR, EMER ELEC, PUSHER, PARKING BRAKE, DUMP, G/S INHIB, FLAP OVRD, TERR INHIB

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52
Q

How many tests and how many switches get moved during the cockpit preparation flow?

A

4 tests - O2, CVR, TEST PANEL, TRIM

2 switches - O2 knob, Seat Belt switch

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53
Q

What is on the hydraulic system?

A

Landing gear, main brakes, EMER/parking brakes, spoilers, pusher, rudder spring actuator

54
Q

What does the TO CONFIG button check?

A

Parking brake, flaps, spoilers, and pitch trim all set for takeoff.

55
Q

What is the normal F-R-A AEO?

A

400’

56
Q

What is the approximate pitch during initial climb to get a V2+10 to 180 speed?

A

15-18 degrees

57
Q

As the PF what should you say pretty darn quick after calling for “Flaps zero, after takeoff checklist” and hearing “flaps zero”? (Use 737 technique - flaps and gear are up)

A

“Select FLC and set speed 160”

58
Q

What is the maximum takeoff altitude? And in icing?

A

14000’ normal, 10000’ in icing

59
Q

What documents are “paper” and required to be on board the aircraft?

A

Airworthiness cert, registration, radio station authorization, checklist cards, QRH, compass card.

60
Q

How are the circuit breakers numbered?

A

Rows A-D on all four panels, columns 1-16 on the LP lower panel, 17-32 on the RP lower panel, and 33 - 40 behind the LP. Running clockwise.

61
Q

What do you have to do after removing the gust lock pin?

A

Press the rudder pedals full travel to fully unlock the gust lock

62
Q

When should you turn on the NAV light?

A

As soon as you hit the battery switch.

63
Q

What are the steps for the RP on flight guidance programming?

A

Flight Plan
LFE
Database (first flight)
Profile/Display option

64
Q

How much does NJ require to make a 180 degree turn?

A

65 feet

65
Q

What happens when the ENG 1 / 2 START SWITCH is set to run?

A

Boost pump is powered

Red beacon is on

66
Q

What is the max demonstrated crosswind?

A

25 kts TO

28 kts LDG

67
Q

When does the CAS message for fuel imbalance illuminate? Extinguish?

A

220 lbs on and off at 88 lbs

68
Q

When does the FUEL EQUAL advisory light illuminate?

A

44 lbs

69
Q

How many messages can be displayed on the CAS without scrolling?

A

14

70
Q

When do the speed brakes automatically stow?

A

< 125 kts
Any flaps selected
Thrust lever at MAX CRZ or >

71
Q

When do I need windshield heat?

A

5 degrees or below

Fogging up

72
Q

What is Vap typically?

A

VRef+10 for a straight in approach, Vref+20 for a circling approach

73
Q

What happens when you hit TOGA?

A

Sequences FP (to MA routing)
F/D goes to ROL/GA for guidance
Disconnects AP (but not yaw damper)
CDI reverts to FMS (pink lines)

74
Q

When can I do a CFDA (controlled flight descent angle)?

A

3.77 degrees of less GP
Straight in approach
Have a local altimeter setting

75
Q

What is powered on a cold dark airplane?

A

Refuel panel
Gust lock pin
Baggage lights (aka courtesy also)
Courtesy lights (stairs and entry way)

76
Q

How long do the courtesy lights and baggage lights stay illuminated?

A

5 min

77
Q

How are the circuit breakers marked?

A

“Alphanumerically”

78
Q

What is needed for the CVR test?

A

Parking brake set and powered on for more than 60 sec

79
Q

What doors are monitored on the status panel? How is the refueling door monitored?

A

2 nose baggage doors, main entry door, emergency exit door, and aft baggage door. Refueling door will give warning if the switches are on.

80
Q

When do you get both igniters?

A

In flight start or a start below O C

81
Q

When doing a battery start, what happens when you start the second engine?

A

The operating engine will automatically spool up to approximately 72% N2 to give enough power to the engine.

82
Q

What do you ”get” when testing the fire system?

A

Two red CAS messages, the master warning, “FIRE” “FIRE”, the chime, red lights on the ITT gages, and red lines in the fire shutoff switches

83
Q

What is the max operating altitude?

A

45,000 ft

84
Q

What is the maximum flaps extended altitude?

A

18,000 feet

85
Q

What is the maximum OEI in icing altitude?

A

15,000 feet

86
Q

What is the minimum altitude for start, takeoff and landing?

A

-1000 feet

87
Q

What is the maximum differential pressure?

A

9.4 psi

88
Q

What is the maximum differential overpressure?

A

9.6 psi

89
Q

What is the maximum differential negative pressure?

A
  • 0.3 psi
90
Q

What is the maximum generator load in flight?

A

390 Amp

91
Q

What is the maximum generator load on the ground?

A

330 Amp

92
Q

When do icing conditions exist?

A

OAT is 10 degrees C or below and visible moisture exists or operating on contaminated surfaces

93
Q

When is flight prohibited?

A

In freezing drizzle or freezing rain

94
Q

What is the aircraft’s certificated approach category?

A

Category B

95
Q

Is there an altitude restriction for Baro-VNAV approaches?

A

Baro-VNAV is not authorized at an airport elevation above 5000 feet

96
Q

What is the time limit for maximum thrust?

A

10 minutes

97
Q

What is the time limit for takeoff thrust?

A

5 minutes

98
Q

What is the time limit for max cont or max climb thrust?

A

5 minutes when in level flight

99
Q

What are the transient engine limits and for how long?

A

102% N1, 103%N2, 765C ITT for no more than 20 sec

100
Q

What are the transient oil limits?

A

0-20 psi for no more than 20 sec

20 -270 for no more than 400 sec

101
Q

What is the trigger for the steps of the climb flow? Who does it? What are the steps?

A

Passing 10,000 ft, LP,
SIGNS/OUTLET….as required (no turbulence OFF/ON, Turbulence BELTS/ON)
WSHLD 1 & 2….as required

102
Q

What is the transition flow trigger and steps?

A

Climbing through transition - altimeters

103
Q

What is the cruise flow?

A

When leveling at final cruise altitude - fuel and altimeters

104
Q

What busses are on GEN 1? What busses are on GEN 2?

A

DC Bus 1
Shed Bus 1
EMER Bus
Hot Bus 1

105
Q

What busses are on Gen 2?

A

DC Bus 2
Shed Bus 2
Hot Bus 2
Central Bus

106
Q

When can I not crossfeed?

A

Takeoff & Landing

107
Q

When do the fuel boost pumps automatically activate?

A

Engine Start
Low Fuel Pressure
Crossfeed operation

108
Q

What does the hydraulic priority valve do?

A

Guarantees hydraulic power to the spoilers, stick pusher, rudder spring and brakes by restricting flow to landing gear as necessary during simultaneous operation

109
Q

When do the passenger masks deploy?

A

14,700 +/- 300 feet

110
Q

How many AHRS are there? How many ADCs?

A

2 AHRS and 3 ADCs

111
Q

What does the “green donut” on the airspeed indicator signify?

A

1.3 Vs

112
Q

What is the maximum airspeed for structural damage?

A

170 KIAS max

113
Q

What is the max tire groundspeed?

A

182 kts

114
Q

When does the landing gear aural warning go off?

A

700 ft AGL and airspeed below 160, Flaps 0-1-2

115
Q

How long do the brakes need to cool in the event of an aborted TO?

A

20 min

116
Q

What is the minimum tank temperature?

A

-37

117
Q

What is the maximum fuel tank temperature?

A

52 on the ground and 80 in flight

118
Q

When does the fuel gage indicate “min fuel”?

A

310 lbs

119
Q

How much fuel is unusable?

A

Approximately 25 lbs in each tank/50 lbs total

120
Q

Above what airspeed will the stick pusher not actuate?

A

205 kts

121
Q

When does the ventral rudder begin damping?

A

Above 60 kts

122
Q

Above what speed does the antiskid protection kick in?

A

30 kts

123
Q

When does the push to talk button cut out?

A

35 s

124
Q

When is the anti-ice system inhibited on the ground?

A

Below 40 kts

125
Q

With the ADS probe switch in AUTO when do the probes heat?

A

One engine operating or the airplane is not weight on wheels

126
Q

What is the max thrust of the PW 535E?

A

3360 lbs

127
Q

What happens when you press the fire shutoff button?

A

Hydraulic, fuel and bleed air are cutoff

Extinguisher is armed

128
Q

The masks dropping in the back of the airplane for the passengers also does what?

A

Cuts out the power to the outlets

129
Q

When does the ATR activate?

A

20% difference on the N1s

130
Q

How does the automatic thrust reserve get the airplane an extra thrust if activated during TO or GA?

A

Closes the ECS valves

Phenom 300 QRC (3 decks)

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