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GoJet > SOP Limitations > Flashcards

SOP Limitations Flashcards

1
Q

What must be operational for RVSM?

A

Autopilot (1)
Altitude alerting system
Altitude reporting transponder (we have 2, need only 1)
Air data computers (2)

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2
Q

Max pressure altitude for takeoff

A

8,000

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3
Q

Max operating altitude

A

41,000

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4
Q

Max air temp for takeoff and landing ISA?

A

+35°C

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5
Q

Minimum temp approved for takeoff

A

-40° F or C. They’re the same here

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6
Q

On the ground, when, and at what temp must cowl anti ice be on

A

OAT 10°C
Contaminated runway
Visible moisture/fog with vis 1 mile or less

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7
Q

For ground ops, wing anti ice must be on for takeoff at what temperature?

A

OAT 5°C
visible moisture/fog with vis 1 mile or less

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8
Q

For flight ops, at what TAT must the wing anti-ice be on

A

10°C TAT
when Ice is annunciated
If you’re in ice and airspeed less than 230

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9
Q

Max slope approved for takeoff and landing

A

+2% uphill
-2% downhill

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10
Q

Max tailwind for takeoff and landing

A

10 knots

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11
Q

What kind of engines do we have

A

Two General Electric CF34-8C5B1 turbofans

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12
Q

ITT must be below what temperature to ground start an engine?

A

120°C

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13
Q

ITT must be below what temp to air start an engine?

A

90°C

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14
Q

When can you NOT use reduced (FLEX) takeoff thrust?

A

-Wing/cowl anti ice bleeds in use
- contaminated runway
- wind shear warnings/forecast
- anti skid system inop

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15
Q

Max fuel imbalance during takeoff

A

300 pounds

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16
Q

Max fuel imbalance in all other phases of flight except takeoff

A

800 pounds

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17
Q

Max useable fuel in each tank for pressure refuel

A

-Left tank: 7,492
-Right tank: 7,492
-Center tank: 4,610
-Total fuel: 19,594

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18
Q

Can we use automatic fuel cross flow on takeoff?

A

No; must be in manual

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19
Q

Min temp for starting a cold soaked APU on the ground

A

-40° F or C

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20
Q

At what altitude is APU bleed air extraction not authorized?

A

FL250

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21
Q

Vfe speeds

A

Flaps 1: 230
Flaps 8: 230
Flaps 20: 230
Flaps 30: 185
Flaps 45: 170

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22
Q

Vle extension

A

220

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23
Q

Vle retraction

A

200

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24
Q

Max tire limit speed

A

182

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25
Q

Windshield wiper ops speed

A

250 or below

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26
Q

At what altitude can you activate autopilot?

A

600’ AGL

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27
Q

For non precision approaches, what altitude must the autopilot be deactivated?

A

400’ AGL

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28
Q

For precision approaches, what altitude must the autopilot be deactivated?

A

Less than 3.5° glide slope angle: 80’ AGL
3.5° and 4° glide slope angle: 120’ AGL

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29
Q

APU service ceiling

A

41,000

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30
Q

Flight spoilers must not be extended below what altitude and speed

A

300; Vref +10

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31
Q

Max flap/slats deployment altitude

A

15,000

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32
Q

When to use continuous ignition

A

Contaminated runway
Rain moderate or heavier
Turbulence moderate or heavier
Vicinity of thunderstorms

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33
Q

Engine Start limits on ground

A

Starts 1/2 - 90 seconds, 10 second cooldown

Starts 3-5 - 90 seconds, 5 minute cooldown

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34
Q

Motoring limits on the ground

A

1 - 90 seconds, 5 minute cool down

2-5 - 30 seconds 5 minute cooldown

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35
Q

Engine motoring in flight: time and cooldown

A

1 - 120 seconds, 10 second cooldown

2-5 - 60 seconds, 5 minute cooldown

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36
Q

Relight (restart) in flight altitudes, windmilling and using the starter

A

Windmilling: 25,000
Using the starter: 21,000

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37
Q

How high can we start the APU

A

37,000

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38
Q

How high can we take electricity out of the APU

A

41,000

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39
Q

Time limit with battery master on

A

5 minutes

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40
Q

Flaps/slats prohibited when

A

En route and above 15,000

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41
Q

Spoilers prohibited below what altitude

A

300 feet

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42
Q

Reversers need to be off and stowed by

A

Off by 75
Stowed by 60

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43
Q

Under what flight conditions (not temperature) must the cowl anti Ice be on?

A

Icing conditions or ICE is annunciation by the ice detection system

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44
Q

What are considered critical areas of the aircraft?

A

Wings
upper fuselage
horizontal stab
vert. Stab
control surfaces
engine inlet

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45
Q

Is takeoff with frost permitted? If so when?

A

Yes, only if it adheres to the upper fuselage and it’s possible to distinguish surface features or with 1/8 inch of frost on the underside of the wing

46
Q

What is the Minimum flight crew

A

1 pilot
1 copilot

47
Q

CRJ550 cargo dimensions

A

Fwd: 1,000 lbs
Aft: 374 cu ft - 3740 lbs
OR
Aft: 296 cu ft - 271 lbs

48
Q

At what altitude is APU bleed air extraction not permitted?

A

25,000 feet

49
Q

Max turbulence penetration speed in knots and Mach?

A

280 knots
0.75 Mach

50
Q

Minimum and maximum pressure differential?

A

-0.5 psi - 8.7 psi

51
Q

Single pack operation max altitude

A

31,000

52
Q

Max useable fuel in each tank for gravity refuel

A

Right wing: 7,290
Left wing: 7,290
Center tank: none
Total: 14,580

53
Q

Minimum oxygen required for dispatch

A

2 cockpit crew members - 810psi
3 cockpit crew members - 1110psi

54
Q

Min fuel required for go around

A

600 pounds per wing, max 10° pitch up

55
Q

Underseat storage weight

A

12 pounds

56
Q

Overhead storage

A

1,180 pounds

57
Q

Forward cargo weight

A

1,000 pounds

58
Q

Aft cargo weight

A

3740 pounds

59
Q

Engine limits green and red for N1, N2, oil temp

A

N1: Green: 0-99.4 Red: 99.5
N2: Green: 0-99.3 Red: 99.4
Oil temp: Green: -40-155 Red: 164

60
Q

Engine warmup: don’t exceed 75% N1 for…

A

2 mins after start or till all indications are normal

61
Q

How would you know if you are getting SLD Ice and what kind of precip is it

A

Ice on flight deck side window, it’s freezing rain

62
Q

Engine relight limitations - windmilling/starter assisted

A

Windmilling - SL-25,000, 250kts - Vmo and N2 7.2%

Starter assisted SL-21,000. Vref - Vmo and 0-45% N2

63
Q

Mmo, RVSM Mmo

A

Mmo: 0.85
RVSM Mmo: 0.83

64
Q

Fuel temp limits

A

Jet A takeoff limit -30, flight limit -40

65
Q

When can an FO with less than 100 hrs not takeoff/land

A

Breaking action is 4 or less (good-medium)
SUA
RVR less than 4,000 or 3/4 mile vis
Crosswind more than 15 knots
Widndshear
Contaminated runway

66
Q

APU min temp, how many starts in an hour

A

-40C
3 starts in an hour with 2 mins in between

67
Q

FO with more than 100 hrs limitations

A

No takeoff on runway shorter than 4500
Less than cat 1 mins (less than 1800 rvr)
Brake action less than poor (code of 2)
Pic determines

68
Q

Load factor limits with flaps up and down

A

Up: -1.0 - +2.5
Down: 0.0 - 2.0

69
Q

Can you do an emergency depress above 15,000?

A

NO

70
Q

Max/min differential pressure

A

Max 8.7
Min -0.5

71
Q

Max APU and IDG Kva

A

40 for both

72
Q

Max APU RPM and EGT

A

106%
1038°C

73
Q

FO limitations more than 100 hrs

A

No takeoff if wx below landing mins for dep airport

Below 4500

Braking less than poor

74
Q

What is Marginal weather

A

1,000ft and 3 miles at destination, 600 ft and 2 miles at alternate

75
Q

O2 reqs for 2 ppl vs 3 with 77 cu ft vs 50

A

77 - 810/1110
50 - 1180/1630

76
Q

How many jackscrews we got?

A

1 - moves horizontal stabilizer, powered by 2 electric motors , one at a time

77
Q

What connects the aielerons

A

Torque tube. Ailerons mechanically connected via a torque tube

78
Q

What’s RAP and what’s the max time

A

Reserve availability period (short call) up to 14 hours,

79
Q

If you call in fatigued how much rest do you get?

A

12 hours

80
Q

How long is long call reserve

A

12 hours

81
Q

The ice detection probe - is it heated?

A

Yes. Heats for 5 seconds every 60 second period

82
Q

How long can we be at max power or takeoff power with 2 engines?

A

5 mins

83
Q

How long can we be at apr thrust with 1 engine?

A

10 mins

84
Q

When type 2 or 4 anti-ice fluids are applied, when do you turn on wing anti ice

A

Just prior to thrust increase

85
Q

Normal N1 idle range?

A

20-25%

86
Q

Normal N2 idle range?

A

55-65%

87
Q

Max ITT for engine start on ground? (Red line)

A

815°

88
Q

Max ITT for windmill engine start? (Red line)

A

927°

89
Q

Minimum oil pressure?

A

25 psi

90
Q

Normal oil pressure ranges below 60 and above 60

A

Below 60 - 25-65 psi
Above 60 - 25-95 psi

91
Q

Normal thrust rating vs APR thrust rating?

A

12,670 pounds
13,790 pounds (APR)

92
Q

What’s on the accessory gearbox?

A

O - oil pump
F - fuel pump
F - FADEC alternator
H - hydraulic pump
I - integrated drive generator
A - air turbine starter

93
Q

How many amps is the main battery vs APU battery

A

Main 17
APU 43

94
Q

What powers the FADEC?

A

Airplane electrical system until N2 reaches 50%, then the FADEC alternator powers the FADEC

95
Q

Oil pressure normal range?

A

26-116psi

96
Q

When will we get a green “takeoff config ok”

A

Flaps set 8-20
Aileron trim
Rudder trim
Stabilizer trim
Parking brake off
Flight spoilers stowed
Autopilot off

97
Q

When will continuous ignition fire automatically?

A

FADEC senses flameout
Approaching a stickshaker during a stall
Disruption of airflow through engine

98
Q

How many different idles are there and what are they?

A

Five - FLAG R
F - flight idle
L - landing idle
A - approach idle
G - ground idle
R - reverse idle

99
Q

What conditions must be met for TO/TO to activate in the FMA?

A

Parking brake off
Flaps 8-20°
V-speeds set
Stabilizer trim in takeoff range
Both engines running

100
Q

How many AC and DC busses are there

A

AC - 4
DC - 9

101
Q

What’s attatched to ADG

A

SAFE H

S - stab trim channel 2
A - ADG bus
F - flaps/slats 1/2 speed
E - essential AC bus
H - hydraulic pump 3B

102
Q

Difference between tat and sat

A

Tat accounts for compressibility. All the ram air coming at you. Sat is air temp outside

103
Q

Min rpm on apu on ground vs in flight

A

5 on ground 12 in flight

104
Q

When do you remember BIGHAF and what is it?

A

Engine fire push buttons pressed

B - bleed prsov close
I - igniters inhibited
G - generators (IDG) disconnected
H - hydraulic sov closed
A - arms engine fire bottles
F - fuel sov closed

105
Q

When do you remember GASPL and what does it stand for?

A

When the APU fire button is pressed

G - generator, APU generator trips offline
A - arms the fire bottle
S - sov, fuel sov closed
P - pump, fuel pump off
L - load control valve (LCV) closed

106
Q

What is PHCHRCWT for and what does it stand for?

A

For the flow of air through PACK components

P - precooler
H - heat exchanger (primary)
C - compressor
H - heat exchanger (secondary)
R - reheater
C - condenser
W - water extractor
T - turbine (expansion turbine)

This air then goes to a mixing manifold then into the cabin

107
Q

What’s the function of the PRSOVs?

A

Pressure regulating shutoff valves, they regulate pressure in the bleed air manifolds to 45 PSI +/- 3.

The ACSCs (air conditioning system controllers) command the PRSOVs

108
Q

Hot start memory/non memory item

A

ITT goes super hot: Thrust lever shut off, reference QRH

109
Q

Hung start non memory/memory item

A

N2 hangs below 50% and stays there: thrust lever shut off, reference QRH

110
Q

No starter cutout memory/non memory item

A

When N2 is above 50%, the start message on ED2 should go away and the start light should extinguish, if it doesn’t: press stop button. Reference QRH

111
Q

550 weights

A

Max ramp: 66,000
Max takeoff: 65,000
Max landing: 61,000
Zero fuel: 59,000
Min flight: 42,000

112
Q

700 weights

A

Max ramp: 75,250
Max takeoff: 75,000
Max landing: 67,000
Zero fuel: 62,300
Min flight: 42,000
Min operating: 39,835

GoJet (3 decks)

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