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Q300 Limitations & SOP’s > Limitations & SOP’s > Flashcards

Limitations & SOP’s Flashcards

1
Q

Is the q300 rated to fly in severe icing?

A

No

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2
Q

Max ramp weight

A

19,595kg

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3
Q

Max takeoff weight

A

19,505kg

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4
Q

Max landing weight

A

19,051kg

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5
Q

Max zero fuel weight

A

17,917kg

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6
Q

Min structural design weight

A

11,204kg

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7
Q

Compartment 1a max weight

A

385kg

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8
Q

Compartment 2a max weight

A

227kg

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9
Q

Compartment 3 max weight

A

181kg

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10
Q

Compartment 1b max weight

A

454kg

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11
Q

Compartment 2 b max weight

A

227kg

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12
Q

Max baggage compartment weight

A

1134kg

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13
Q

Forward CofG limits

A

Up to 13,608kg - 15% MAC

From 13,608kg to 19,505kg - 15% to 21.5% MAC

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14
Q

Aft CofG limit

A

40% MAC

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15
Q

Flaps retracted load factor limit

A

+2.5g to -1g

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16
Q

Flaps extended load factor limit

A

+2g to 0g

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17
Q

Maximum fuel imbalance

A

272kg

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18
Q

Max operating altitude

A

25,000ft

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19
Q

Max operating altitude for takeoff and landing

A

10,000ft

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20
Q

Max altitude for extending gear or flap

A

15,000ft

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21
Q

Max altitude for air starting

A

20,000ft

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22
Q

Max runway slope for takeoff and landing

A

+2% (uphill)
-2% (downhill)

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23
Q

Max tailwind component

A

10kts (20kts air Nelson with limitations)

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24
Q

Max crosswind component

A

36kts

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25
Q

Ambient temperature limits

A

Max = 48.9C or ISA +35C

Min = -54C

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26
Q

VMO

A

0-17,000ft = 243kts
20,000ft = 232kts
25,000ft = 214kts

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27
Q

VFE

A

Flaps 5 = 163kts
Flaps 10 = 154kts
Flaps 15 = 150kts
Flaps 35 = 138kts

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28
Q

VA

A

177kts

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29
Q

VLO

A

163kts

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30
Q

VLE

A

173kts

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31
Q

VRA

A

190kts

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32
Q

Alternate gear extension speed

A

140kts

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33
Q

Max tyre speed

A

165kts

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34
Q

MTOP Tq%

A

105.6% (5mins)

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35
Q

NTOP Tq%

A

92%

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36
Q

Max continuous Tq%

A

90% @ 1200rpm
96% @ 1125rpm or lower

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37
Q

Transient Tq%

A

115% (20sec)

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38
Q

Max reverse Tq%

A

90%

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39
Q

MTOP ITT

A

800C (5mins max)

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40
Q

NTOP ITT

A

765C (can be exceeded by 5C for 30seconds)

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41
Q

Max continuous ITT

A

800C

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42
Q

Starting ITT

A

840-900C for 12 seconds
900-950C for 5 seconds

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43
Q

Transient ITT

A

840C (20 seconds)

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44
Q

Max reverse ITT

A

765C

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45
Q

MTOP NL%

A

104% (5mins)

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46
Q

NTOP NL%

A

101.7%

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47
Q

Max cont NL%

A

104%

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48
Q

Transient NL%

A

104.3% (20sec)

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49
Q

Max reverse NL%

A

101.7%

50
Q

Min flight idle NH%

A

66%

51
Q

MTOP NH%

A

102.7% (5mins)

52
Q

NTOP NH%

A

101%

53
Q

Max cont NH%

A

102.7%

54
Q

Transient NH%

A

103.7% (20sec)

55
Q

Max reverse Nh%

A

101%

56
Q

MTOP Np Prop RPM

A

1212rpm

57
Q

NTOP Np Prop RPM

A

1212rpm

58
Q

Max cont Np Prop RPM

A

1212 @ 90% Tq
1125 @ 96% Tq

59
Q

Transient Np Prop RPM

A

1320rpm (20sec)

60
Q

Max reverse Np Prop RPM

A

1212rpm

61
Q

Oil Px limits

A

55-65psi
40-55psi at engine speeds below 75% NH
200psi during starting

62
Q

Oil temp limits

A

45-115C
Transient 115-125C (20min)
Starting -40C
Un-feathering and power setting above flight idle min 0C
For adequate inlet splitter anti-icing min 45C

63
Q

Fuel capacity

A

Total 2574kg
Individual 1287kg

64
Q

Do the aux fuel pumps need to be on for takeoff and landing?

A

Yes

65
Q

Is continuous ops with fuel heater outlet temp outside 11-57C allowed?

A

No

66
Q

Starter cranking limits

A
  1. 1min. 2min off
  2. 1min. 2min off
  3. 1min. 30min off
67
Q

Prop prohibited range

A

500-780rpm

68
Q

Max loads - DC Gen

A

0.7 - ground
1.0 - flight

69
Q

Max loads - L & R TRU’s

A

Ground - 1.0
Flight - 1.0

70
Q

Max loads - AC Gen’s

A

Ground up to +10C - 1.0
Ground above +10C - 0.33
Flight - 1.0

71
Q

Max load - inverter

A

Ground - 1.0
Flight - 1.0

72
Q

Normal cabin px differential

A

5.5psi

73
Q

Max cabin px differential

A

5.95psi

74
Q

Max cabin px differential during taxi, takeoff, landing

A

0.5psi

75
Q

Max cabin altitude (pressurised flight)

A

8,000ft

76
Q

Can bleed air be on for takeoff and landing?

A

No

77
Q

Icing conditions in flight

A

SAT below +5C & visible moisture (clouds, fog, rain, snow, sleet, ice crystals)

78
Q

Icing conditions on ground

A

SAT below +10C & visible moisture or if snow, ice, standing water, or slush may be ingested into engine nacelles on the ground

79
Q

What needs to be switched in icing conditions

A

Engine intake bypass doors open, engine ignition switch on auto

If ice is detected airframe auto selector needs to be on either fast or slow

80
Q

What category is the AFCS (automatic flight control system)

A

Cat 1

81
Q

On approach what height does the autopilot need to be disengaged

A

200ft

Or

100ft provided:

Xw less than 15kts
Tailwind less than 10kts
And afcs dual mode and nav sel illuminates on both sides at 1200ft RA

82
Q

Can autopilot be used for an approach with an engine inop?

A

No

83
Q

APP mode cannot be used with what flap setting?

A

35 (glideslope angles greater than 3 degrees cannot use flap 35)
5 below 1500ft and a/p engaged
0 below 500ft and a/p engaged

84
Q

After takeoff or go-around min a/p engagement height

A

1000ft

85
Q

Stable gate policy?

A

C onfig for landing
R OD below 1000 fpm
A irspeed vref + 20
P rofile correct

500ft visual approach
1000ft instrument approach

86
Q

Circuit met minima on take-off

A

Day - 1100ft ceiling, 5km viz
Night - 1500ft ceiling, 8km viz

87
Q

Class c & d speed restriction

A

200kts below 3000ft and within 5nm

88
Q

Speed restrictions class g

A

Below 9500ft - 200kts
Below 5000ft - 160kts

89
Q

When is an alternate required?

A

1hr either side of eta:

Ceiling less than 1000ft above app minima
Viz less than 5km or 2km above app minima whichever is higher

90
Q

Alternate minima

A

Precision app - ceiling 600ft or 200ft above minima whichever is higher
- viz 3000m or 1000m above minima
Non-precision app - ceiling 800ft or 200ft above
- viz 4000m or 1500m above

91
Q

Take off minima when no minima is prescribed

A

300ft ceiling
1500m viz

92
Q

RVR take-off

A

0ft ceiling
800m viz

Or

400-350m viz if crew trained in last 13 months

93
Q

Max Torque during ground ops

A

92.5%

94
Q

Max torque with props feathered during ground ops

A

48%

95
Q

Min fuel in #1 tank for apu start

A

225kg

96
Q

Distance fuel truck needs to be from apu to refuel with apu running?

A

9.2m

97
Q

Apu fuel burn

A

55kg per hr

98
Q

Er oute fuel burn

A

660kg/hr

99
Q

Holding fuel burn

A

480kg/hr

100
Q

Missed app and second app fuel burn

A

150kg

101
Q

Does the cabin need to be evacuated if we get a fire or smoke warning?

A

Yes

102
Q

Evacuation pa?

A

Attention attention this is the captain, evacuate evacuate evacuate, use ……. Exits

Land: all Exits or specify which exits
Water: use window exits

103
Q

Precautionary evacuation communication order?

A

F/a
ATC
Passengers

104
Q

Precautionary evacuation pa

A

Attention attention, this is the captain speaking, disembark immediately, use the main door

105
Q

Responsibility for f/o and captain during evacuation

A

F/o Exit Aircraft either using main exit or front right emergency exit in an emergency evacuation. Gather all passengers

Captain completes cockpit drills, helps passenger leave aircraft, is last person to gather outside aircraft using the main exit

106
Q

Wind shear procedure

A

“Wind shear, set max power”

Apply MTOP power and
Raise nose to 9 degrees

If needed

“Firewall the power levers”

Raise nose further but don’t slow below v2/vga

107
Q

What defines wind shear

A

Airspeed +/- 15kts
Abnormal pitch attitude
Vertical speed outside normal parameters
Abnormal pl position

108
Q

Egpws procedure

A

Select G/A and advance pl towards MTOP

“Going around set max power”

Roll wings level
Climb aggressively respecting stick shaker
Target vga

“Go around drills”

109
Q

Emergency descent pa

A

“Attention attention, this is the captain, emergency descent”

110
Q

PM’s role during emergency descent

A

Advise atc

Set alt alerter with altsel
“10,000 set altsel”

Set transponder

Contact f/a that cabin is below 10,000’

111
Q

Pf’s role during emergency descent

A

Seatbelt signs on

“Emergency descent”
Potentially make pa

Set ias vmo
Levers flight idle
Condition levers max
Airspeed vmo

112
Q

Bomb threat pa

A

Attention attention, this is the captain, disembark immediately, use main door, take all hand luggage.

113
Q

What would the flight attendant say during a hijacking?

A

“This is mike Nolan, crew number 69420 7500, I must come to the flight deck”

114
Q

Brace pa

A

Attention attention, this is the captain, brace for impact

115
Q

Impact drill

A

Pic “I have control”

F/o:
cabin signs on
Emergency lights on

Condition levers fuel off (if no longer required)

116
Q

Hijacking pa

A

Attention attention, this is the captain, seventee five hundred

117
Q

Severe turbulence p/a

A

“Flight attendant take your seat”

118
Q

Pa if evacuation isn’t necessary

A

Attention attention, this is the captain, remain seated

119
Q

Hijacking

A

Don’t let anyone into flight deck
ATC
Descend, depressurise, divert
Continuous comms with f/a

If terrorist enters cockpit maintain passive role
No rapid movements
Ask if you can tell pax to fasten seat belts and remain seated
Advise of aircraft limitations

After landing
Evacuate a/c at same time as pax
Pull cvr circuit breaker
Turn on interior light and turn off all exterior lights if at night

120
Q

Bomb threat

A

Evacuate, take all hand luggage

Or if in flight move pax away from bomb and de pressurise cabin. Slow down and extend landing gear to reduce airframe stress

121
Q

Take-off and landing reqs (first 200hrs)

A

Runway not contaminated
Crosswind component of no more than 50% company xw limit
Wx above alternate minima
No reported wind shear
Cat a or b airport

122
Q

What are the critical phases of flight

A

Off blocks to 10,000ft
Within 1000ft from transition or level off
TOD or anticipating a clearance
10,000ft to on blocks

Q300 Limitations & SOP’s (1 decks)

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