Memory items Flashcards

1
Q

what are the RVSM required equipment

A
#auto pilot must be operational 
#Altitude alerting system must be operational
#Altitude reporting transmitter 2 (1) one must be operational 
#Air data computers 2 must be operational
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2
Q

CRJ 700 Max ramp weight

A

75,250

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3
Q

CRJ 700 Take off weight

A

75,000

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4
Q

CRJ 700 Max landing weight

A

67,000

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5
Q

CRJ 700 Max zero fuel weight

A

62,300

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6
Q

CRJ 700 Min flight weight

A

42,000

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7
Q

CRJ 700 Min operational empty weight

A

39,835

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8
Q

CRJ 900Max ramp weight

A

85,000

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9
Q

CRJ 900 Take off weight

A

84,500

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10
Q

CRJ 900 Max landing weight

A

75,100

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11
Q

CRJ 900 Zero fuel weight

A

70,750

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12
Q

CRJ 900 Min flight weight

A

45,000

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13
Q

Max airport altitude for take off and landing

A

8,000

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14
Q

Max operating altitude

A

41,000

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15
Q

Max ambient temp for takeoff and landing

A

ISA +35C

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16
Q

Min ambient temp for takeoff and landing

A

-40C/-40F

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17
Q

When must Cowl anti ice be on

A

10C (50f) or below
visible moisture such as fog 1500meaters and 1 mile or rain , sleet ,and ice christals
When opporating on runways and ramp with or taxiway where there is surface snow,ice standing water or slush is preasent .

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18
Q

Icing condition is flight exist in flight at

A

Tat of 10C (50F) and visible moisture in any form is encountered (clouds ,rain ,snow,sleet or ice cristals ) except when the SAT is -40C (-40F)
In iceing conditions
ICE is announceaded by the ice detection system

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19
Q

When must the wing anti ice system be on

A

When outside air temp is 5C or (41 F)
Visible moisture such as fog with visibility 1500 meters or 1 mile or less with rain snow sleet or iced christals
When runways is contaminated with surface snow , slush or standing water .
When type ii or IV antiiceing fluid has been applied . Wing anti ice must be selected on if required just prior to trust increase for takeoff

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20
Q

When dees anti ice condition exist in flight ?

A

10 C or 50F or below visible moisture in any form is encountered such as

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21
Q

When does icing conditions exist in flight

A

TAT 10C 50F or below and visible moisture (such as rain,snow,sleet or ice crystals.

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22
Q

Engine cowl anti ice must be on when

A

In icing conditions

ICE is announced by the ice detection system

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23
Q

When is take off prohibited

A

When ice,snow or slush adhering to the critical areas of , wing ,upper fuselage horizontal stabilizer , vertical stabilizer , control surfaces ,and engine inlet .

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24
Q

Is take off permitted with frost adhering to aircraft surface

A

The upper surface if its possible to distinguish surface features
Max 1/8 in in (3.0mm) layer of frost on the underside of the wing if it is clouded by cold soak fuel

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25
Q

How far must you be from a suitable airport if the carriage is labeled cargo

A

60 min

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26
Q

CRJ 700 under seat

A

99 cu ft 12lbs per seat

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27
Q

CRJ 700 over head

A

97.8 cu ft 1180lbs

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28
Q

CRJ 700 forward cargo

A

109 cu ft 1000lbs

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29
Q

CRJ 700 Aft cargo

A

374 cu ft 3740 lds

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30
Q

Aft delta

A

2610 lbs

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31
Q

CRJ 900 under seat

A

99 cu ft. 12 lbs

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32
Q

CRJ 900 overhead

A

97.8 cu ft 1180 lbs

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33
Q

CRJ 900 FORWARD cargo

A

109 cu ft 850 lbs

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34
Q

CRJ 900 aft cargo

A

374 cu ft 3740 lbs

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35
Q

Max runway slope

A

+2. -2

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36
Q

Max tail wind component

A

10 knots

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37
Q

Min flight crew

A

I pilot one co pilot

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38
Q

When must the flight deck door be closed

A

At all times during flight except permitting access and egress

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39
Q

What are the ozone level restrictions

A

.25 parts per million , sea level equivalent and at any time above flight level 320

0.1 parts per million, sea level equivalent ,time weighted average during any three (3) hours interval above flight level 270

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40
Q

When does icing conditions exist in flight

A

TAT 10C 50F or below and visible moisture (such as rain,snow,sleet or ice crystals.

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41
Q

Engine cowl anti ice must be on when

A

In icing conditions

ICE is announced by the ice detection system

42
Q

When is take off prohibited

A

When ice,snow or slush adhering to the critical areas of , wing ,upper fuselage horizontal stabilizer , vertical stabilizer , control surfaces ,and engine inlet .

43
Q

Is take off permitted with frost adhering to aircraft surface

A

The upper surface if its possible to distinguish surface features
Max 1/8 in in (3.0mm) layer of frost on the underside of the wing if it is clouded by cold soak fuel

44
Q

How far must you be from a suitable airport if the carriage is labeled cargo

A

60 min

45
Q

CRJ 700 under seat

A

99 cu ft 12lbs per seat

46
Q

CRJ 700 over head

A

97.8 cu ft 1180lbs

47
Q

CRJ 700 forward cargo

A

109 cu ft 1000lbs

48
Q

CRJ 700 Aft cargo

A

374 cu ft 3740 lds

49
Q

Aft delta

A

2610 lbs

50
Q

CRJ 900 under seat

A

99 cu ft. 12 lbs

51
Q

CRJ 900 overhead

A

97.8 cu ft 1180 lbs

52
Q

CRJ 900 FORWARD cargo

A

109 cu ft 850 lbs

53
Q

CRJ 900 aft cargo

A

374 cu ft 3740 lbs

54
Q

Max runway slope

A

+2. -2

55
Q

Max tail wind component

A

10 knots

56
Q

Min flight crew

A

I pilot one co pilot

57
Q

When must the flight deck door be closed

A

At all times during flight except permitting access and egress

58
Q

What are the ozone level restrictions

A

.25 parts per million , sea level equivalent and at any time above flight level 320

0.1 parts per million, sea level equivalent ,time weighted average during any three (3) hours interval above flight level 270

59
Q

N1 %

A

red 99.5 Green 0 to 99.4

60
Q

N2 %

A

Red 99.4 Green 0 to 99.3

61
Q

ITT C

A

Variable

62
Q

Ool temp C

A

Red 164 Amber 156 to 165 Green -40 to 155

63
Q

Oil pressure psi

A

RED 0 to 24 variable

64
Q

CRJ 700 oil pressure ground start

A

182 psi 95 psi after 10 min

65
Q

CRJ 700 N 1

A

815

66
Q

CRJ 700 Normal take off power two engines is limited to

A

5 min

67
Q

CRJ 700 Apr power one engine is limited to

A

10 min

68
Q

CRJ 700 ITT must be below ______ before attempting to ground start engine

A

12O

69
Q

continuous engine ignition

A

take off and landings on contaminated runway

Flight through moderate or heavy intensity icing
Flight through moderate or heavy intensity turbulence
Flight in the vicinity of thunderstorm

70
Q

The use of flex is not recommended

A

wing or cowl anti ice bleeds are in use
Runway is contaminated with standing water ,slush ,show and ice
warning of forecast wind shear and down draft
Anti skid system is inoperative
The engine cannot achieve full rated trust

71
Q

CRJ 700 Engine start on the ground 1 & 2

A

Max time 90 sec 10 sec cool down

72
Q

CRJ 700 Engine start on the ground 3 to 5

A

Max time 90 sec 5 min cool down

73
Q

CRJ 700 start monitoring in flight 1

A

Max time 120 sec 10 sec cool down

74
Q

CRJ 700 start monitoring in flight 2 through 5

A

Max time 60 sec 5 min cool down

75
Q

Motoring on ground 1

A

Max time 90 sec 5 min cool down

76
Q

Motoring on ground 2 through 5

A

Max time 30 sec 5 min cool down

77
Q

CRJ 700 Windmilling

A

Alt from 21,000 to 10,000

speed 290 knots to Vmo and 7.2% N2 minimum

78
Q

CRJ 700 Windmilling

A

Alt from 10,000 to Sea leavel

speed 250 knots to Vmo and 7.2% N2 minimum

79
Q

CRJ 700 Starter assisted

A

Alt from 21,000 to sea leavel

speed Vref to Vmo and from 0 to 45 %

80
Q

CRJ 700 All engine out rapid realign

A

Alt from 10,000 to sea level

FADEC rapid relight capability has been demonstrated at 200 KIAS for up to 15 second fuel interruptions

81
Q

CRJ 900 Windmilling

A

Alt from 21,000 to Sea leavel

speed 250 knots to Vmo and 7.2% N2 minimum

82
Q

CRJ 900 Starter assisted

A

Alt from 21,000 to sea leavel

speed Vref to Vmo and from 0 to 45 %

83
Q

CRJ 900 All engine out AOE rapid realign

A

Alt from 10,000 to sea level

FADEC rapid relight capability has been demonstrated at 200 KIAS for up to 15 second fuel interruptions

84
Q

Note 1 30 deg ether direction aircraft nose , no wind speed limit and < 5 knots windspeed

A

No limit - TOGA trust may be applied before brake release but must set by 60 KIAS

85
Q

NOTE 2 .30 deg in either direction of nose between 5 and 30 knots wind speed

A

Apply up to 75% N1 before break released , then set toga trust by 60 knots

86
Q

NOTE 3 > in either direction of aircraft nose

A

Apply maximum of idle/taxi thrust before brakes released , then set TOGA thrust by 60 KIAS

87
Q

Max permissible fuel imbalance between left and right wing

A

during take off 300 lbs all other phases of flight 800 lbs

88
Q

left / right wing tank

A

pressure 74,920 Gravity (700) 7,290 lbs

900 7,405

89
Q

Center tank

A

Pressure 4,610

90
Q

Total Fuel

A

Pressure 19,594 Gravity (700) 14,580 (900

) 14,810

91
Q

take off with fuel load in excess of 500 lbs in center tank is not prohibited

A

Each main tank is above 4,400 ibs

92
Q

The min fuel quantity for go around is

A

600 lbs assuming clime angle 10 deg nose up

93
Q

The max consumption of oil for each engine

A

189 cubic centiliters per hour 6.4 us unces or .05 gallons per hour

94
Q

max duration without oil servicing

A

36 hours

95
Q

Min ambient temperature for starting a cold soak APU

A

-40 C /-40F

96
Q

APU starting motor is limited to

A

3 starts in 1 hour A two min delay must be given between starting attempts

97
Q

Max APU rpm

A

106%

98
Q

Max APU EGT

A

1038 C

99
Q

APU Bleed air Extraction

A

Not permitted above 25,000

100
Q

APU engine start during ground opp-orations

A

No bleed air extraction limitation Each engine may be started using the APU bleed air source .

101
Q

APU EGT

A

RED 807 Green 0 to 806