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
How far must you be from a suitable airport if the carriage is labeled cargo
60 min
26
CRJ 700 under seat
99 cu ft 12lbs per seat
27
CRJ 700 over head
97.8 cu ft 1180lbs
28
CRJ 700 forward cargo
109 cu ft 1000lbs
29
CRJ 700 Aft cargo
374 cu ft 3740 lds
30
Aft delta
2610 lbs
31
CRJ 900 under seat
99 cu ft. 12 lbs
32
CRJ 900 overhead
97.8 cu ft 1180 lbs
33
CRJ 900 FORWARD cargo
109 cu ft 850 lbs
34
CRJ 900 aft cargo
374 cu ft 3740 lbs
35
Max runway slope
+2. -2
36
Max tail wind component
10 knots
37
Min flight crew
I pilot one co pilot
38
When must the flight deck door be closed
At all times during flight except permitting access and egress
39
What are the ozone level restrictions
.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
40
When does icing conditions exist in flight
TAT 10C 50F or below and visible moisture (such as rain,snow,sleet or ice crystals.
41
Engine cowl anti ice must be on when
In icing conditions | ICE is announced by the ice detection system
42
When is take off prohibited
When ice,snow or slush adhering to the critical areas of , wing ,upper fuselage horizontal stabilizer , vertical stabilizer , control surfaces ,and engine inlet .
43
Is take off permitted with frost adhering to aircraft surface
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
How far must you be from a suitable airport if the carriage is labeled cargo
60 min
45
CRJ 700 under seat
99 cu ft 12lbs per seat
46
CRJ 700 over head
97.8 cu ft 1180lbs
47
CRJ 700 forward cargo
109 cu ft 1000lbs
48
CRJ 700 Aft cargo
374 cu ft 3740 lds
49
Aft delta
2610 lbs
50
CRJ 900 under seat
99 cu ft. 12 lbs
51
CRJ 900 overhead
97.8 cu ft 1180 lbs
52
CRJ 900 FORWARD cargo
109 cu ft 850 lbs
53
CRJ 900 aft cargo
374 cu ft 3740 lbs
54
Max runway slope
+2. -2
55
Max tail wind component
10 knots
56
Min flight crew
I pilot one co pilot
57
When must the flight deck door be closed
At all times during flight except permitting access and egress
58
What are the ozone level restrictions
.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
N1 %
red 99.5 Green 0 to 99.4
60
N2 %
Red 99.4 Green 0 to 99.3
61
ITT C
Variable
62
Ool temp C
Red 164 Amber 156 to 165 Green -40 to 155
63
Oil pressure psi
RED 0 to 24 variable
64
CRJ 700 oil pressure ground start
182 psi 95 psi after 10 min
65
CRJ 700 N 1
815
66
CRJ 700 Normal take off power two engines is limited to
5 min
67
CRJ 700 Apr power one engine is limited to
10 min
68
CRJ 700 ITT must be below ______ before attempting to ground start engine
12O
69
continuous engine ignition
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
The use of flex is not recommended
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
CRJ 700 Engine start on the ground 1 & 2
Max time 90 sec 10 sec cool down
72
CRJ 700 Engine start on the ground 3 to 5
Max time 90 sec 5 min cool down
73
CRJ 700 start monitoring in flight 1
Max time 120 sec 10 sec cool down
74
CRJ 700 start monitoring in flight 2 through 5
Max time 60 sec 5 min cool down
75
Motoring on ground 1
Max time 90 sec 5 min cool down
76
Motoring on ground 2 through 5
Max time 30 sec 5 min cool down
77
CRJ 700 Windmilling
Alt from 21,000 to 10,000 | speed 290 knots to Vmo and 7.2% N2 minimum
78
CRJ 700 Windmilling
Alt from 10,000 to Sea leavel | speed 250 knots to Vmo and 7.2% N2 minimum
79
CRJ 700 Starter assisted
Alt from 21,000 to sea leavel | speed Vref to Vmo and from 0 to 45 %
80
CRJ 700 All engine out rapid realign
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
CRJ 900 Windmilling
Alt from 21,000 to Sea leavel | speed 250 knots to Vmo and 7.2% N2 minimum
82
CRJ 900 Starter assisted
Alt from 21,000 to sea leavel | speed Vref to Vmo and from 0 to 45 %
83
CRJ 900 All engine out AOE rapid realign
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
Note 1 30 deg ether direction aircraft nose , no wind speed limit and < 5 knots windspeed
No limit - TOGA trust may be applied before brake release but must set by 60 KIAS
85
NOTE 2 .30 deg in either direction of nose between 5 and 30 knots wind speed
Apply up to 75% N1 before break released , then set toga trust by 60 knots
86
NOTE 3 > in either direction of aircraft nose
Apply maximum of idle/taxi thrust before brakes released , then set TOGA thrust by 60 KIAS
87
Max permissible fuel imbalance between left and right wing
during take off 300 lbs all other phases of flight 800 lbs
88
left / right wing tank
pressure 74,920 Gravity (700) 7,290 lbs | 900 7,405
89
Center tank
Pressure 4,610
90
Total Fuel
Pressure 19,594 Gravity (700) 14,580 (900 | ) 14,810
91
take off with fuel load in excess of 500 lbs in center tank is not prohibited
Each main tank is above 4,400 ibs
92
The min fuel quantity for go around is
600 lbs assuming clime angle 10 deg nose up
93
The max consumption of oil for each engine
189 cubic centiliters per hour 6.4 us unces or .05 gallons per hour
94
max duration without oil servicing
36 hours
95
Min ambient temperature for starting a cold soak APU
-40 C /-40F
96
APU starting motor is limited to
3 starts in 1 hour A two min delay must be given between starting attempts
97
Max APU rpm
106%
98
Max APU EGT
1038 C
99
APU Bleed air Extraction
Not permitted above 25,000
100
APU engine start during ground opp-orations
No bleed air extraction limitation Each engine may be started using the APU bleed air source .
101
APU EGT
RED 807 Green 0 to 806