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psa 2 > CRJ-700 Limitations > Flashcards

CRJ-700 Limitations Flashcards

1
Q

RVSM Required Equipment List

A

Autopilot must be operational
Altitude Alerting System must be operational
Altitude Reporting Transponder(2) One must be operational
Air Data Computer(2) two must be operational

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2
Q

Maximum Ramp Weight (Important)

A

75,250 Lbs

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3
Q

Maximum Take Off Weight (Important)

A

75,000 Lbs

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4
Q

Maximum Landing Weight (Important)

A

67,000Lbs

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5
Q

Maximum Zero Fuel Weight (Important)

A

62,300Lbs

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6
Q

Minimum flight Weight (Less Important)

A

42,000Lbs

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6
Q

Maximum Airport Pressure Altitude for take off and landing

A

8,000 feet

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7
Q

Minimum Operating Empty Weight (Less Important)

A

39,835Lbs

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8
Q

Maximum operating altitude

A

41,000 feet

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9
Q

Maximum ambient air temperature for T/O and LDG

A

ISA +35 C

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10
Q

Minimum ambient air temperature for T/O

A

ISA -40 C

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12
Q

Cowl anti-ice system must be on, on the ground when OAT is ____ or below and:

A

Is 10 C or below;
When visible moisture is present (1 mile or less)
Operating on contaminated airport surface (runways taxiways ramps)

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13
Q

Cowl anti-ice must be on in flight when TAT is ____ or below and:

A

Is 10 C or below;
In icing conditions
Ice is annunciated

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14
Q

Wing anti-ice system must be ON for TAKEOFF when the OAT is ___ below and:

A

Is 5 C or below and;
Visible moisture is present (less than 1 mile)
Operating on contaminated runway
*When type II or IV anti-icing fluid has been applied
Wing anti-ice turned on just prior to thrust increase for T/O

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14
Q

Flying in supercooled large droplet icing

A
  • Prohibited
  • Wing and cowl icing systems must be on
  • Leave icing conditions immediately when side window icing occurs
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15
Q

Wing anti-ice must be on in FLIGHT when TAT is ____ or below and _________, except when SAT is _____ or below.

A

TAT of 10 C or below and;
Ice is annunciated
In icing conditions below 230 KIAS
Except when SAT is -40 or below

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16
Q

In cold weather operations, Take off is prohibited when?

A

Frost, ice or slush is adhering to any of the critical areas.
(Wing, upper fuselage, horizontal stabilizer, vertical stabilizer, control surfaces and engine inlets.)

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17
Q

T/O is______with frost, ice, snow or slush adhering to any critical areas (wing, upper fuselage, horizontal stabilizer, control surfaces and engine inlets.)

A

Prohibited
*T/O is permitted with frost adhering to the upper surface of the fuselage if it is possible to distinguish surface features
Max 1/8” layer of frost on underside of wing that is caused by cold soak fuel

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18
Q

Max slope for T/O and LDG

A

+2 uphill

-2 downhill

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19
Q

Flight must be within______ of a suitable airport if cargo is carried in either cargo compartment. Why?

A

60 mins.

Because aircrafts fire extinguishing system is only capable of providing 60 of fire supression.

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20
Q

Max tailwind component (Boxed Item)

A

10 knots

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21
Q

The CRJ 700 uses two___________engines

A

GE CF34-8C5B1

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22
Q

During all starts do not exceed______N1 for______mins.after start, or until all operating indications are in normal operating range, whichever is longer

A

75% N1

2 mins.

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23
Q

Engine must remain at _____ until oil pressure reaches________.

A

IDLE

Normal operating range

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24
Q

With engines running and bleeds configured for T/O, target N1 values must correspond to thrust settings charts_______.

A

+ or - 1%

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25
Q

With thrust levers set for T/O target and actual N1 values should______.

A

Match

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26
Q

Use of the engine High-Power Schedule Switch is_______.

A

Prohibited

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28
Q

Engine operating limit ITT @ Ground Start (Boxed Item)

A

815 C (Both Ground and Air ASSISTED ONLY)

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29
Q

Engine operating limit ITT @ Assisted Air Start

A

815 C (Both Ground and Air ASSISTED ONLY)

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29
Q

Normal T/O and max power 2 eng is limited to______mins.

A

5 mins.

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30
Q

What are the normal oil pressure ranges while at IDLE?

A

25-65 PSI (oil temp below 60 C)

25-95 PSI (oil temp above 60 C)

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31
Q

APR power 1 eng is limited to_______mins.

A

10 mins.

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32
Q

ITT must be below______before attempting to air start engine

A

90 C

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33
Q

ITT must be below______before attempting to GROUND start engine. (Boxed Item)

A

120 C

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34
Q

Max oil pressure is limited to____psi when oil temp transient is less than_____C

A

156 PSI

60 C

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35
Q

Oil pressure above idle between_______psi require oil temp monitoring

A

25-45 PSI

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36
Q

Before the first flight of the day when the airplane has been cold-soaked at an ambient temp of_____C or below for more than_____hrs. Then engine and thrust reversers must

A
  • -30 C for 8 hours
  • Eng must be motored for 60 sec and fan rotation verified before an eng start is initiated.
  • Thrust reverses must be actuated until deploy and stode cycles are 2 sec or less
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37
Q

The starter must not be used if indicated N2 RPM exceeds

A

45%

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38
Q

Continuous engine ignition must be used during the following:

A

T/O and landing on contaminated runway
Flight through moderate or heavier intensity rain
Flight through moderate or heavier intensity turbulence
Flight in the vicinity of thunderstorm

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40
Q

Engine start (Ground) maximum time on (Boxed Item)

A

Start max time on followed by:
Starts 1&2 / 90 secs/ 10 sec cool down
Starts 3-5 / 90 secs/ 5 min cool down

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41
Q

Engine start or motoring in (flight) maximum time on (Boxed Item)

A

Start/motoring max time on followed by:
Start 1/ 120 sec/ 10sec cool down
Start 2-5/ 60 sec / 5 min cool down

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41
Q

Speed and N2% for engine relight starter assisted 21000-sea level

A

VREF up to VMO and 0-45% N2

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42
Q

Engine motoring on the (ground) max time on (Boxed Item)

A

Motoring max time on followed by:
Start1 /90 sec /5 min cool down
Start2-5 /30 sec/ 5 min cool down

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43
Q

All engines out rapid relight 10,000-sea level

FADEC rapid relight capability has been demonstrated at_____KIAS for up to______ secs.fuel interruption

A

200KIAS

15 Sec

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45
Q

Max permissible fuel imbalance between the content of the left/right wing tank;
During T/O______lbs
All phases of flight_____lbs
(Boxed Item)

A

300lbs

800lbs

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45
Q

Minimum fuel quantity for go-around is_______lbs per tank assuming a max climb attitude of________degrees pitch up

A

600lbs

10 degrees nose up

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46
Q

T/O with a fuel load in excess of____lbs in the center tank is not permitted unless;
*each main tank is above_______lbs
(Boxed Item)

A

500lbs

4,400lbs

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47
Q

Max fuel tank quantities for pressure fueling

A

Left wing-pressure 7,492lbs
Right wing-pressure 7,492lbs
Center tank-pressure 4,610
Total-pressure 19,594

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48
Q

Max fuel tank quantities for gravity fueling

A

Left wing-7,290lbs
Right wing-7,290lbs
Total-14,580

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49
Q

T/O with engine fuel temp indications below______is prohibited

A

5C

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50
Q

T/O with bulk fuel temp indications below_____or_____depending on fuel type is prohibited

A
  • 30 C

- 40 C

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51
Q

Power cross flow and gravity cross flow must be____for T/O

A

Off

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52
Q

Max duration without engine oil servicing is______operation hours

A

36 hours

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53
Q

Airplane operations in excess of______operation hours the engine oil level must be checked within_______mins up to_____hrs after every engine shutdown

A

36 hours

3 min - 2 hours

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54
Q

The CRJ-700 Auxiliary power unit

A

Allied signal RE 220 RJ

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55
Q

Minimum temp for starting a cold soaked APU on the ground is______

A

-40 C

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57
Q

The APU starter motor duty cycle is limited to not more than_______ (Boxed Item)

A

3 Start attempts in 1 hour with 2 min cool down in between

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57
Q

APU max RPM

A

106%

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58
Q

The APU must observe_____mins.cool down between start attempts (Boxed Item)

A

2 mins

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59
Q

APU generator may be used up to______

A

41,000 feet

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60
Q

APU may not be started above_________

A

37,000 feet

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61
Q

APU bleed extraction is not permitted above_________

A

25,000 feet

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62
Q

Max permissible load on the APU generator

A

40 KVA

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63
Q

APU Indications Red

A

RED
APU EGT 807 C
APU RPM 107%

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64
Q

What is the absolute max APU EGT?

A

1038 C or lesser value indicated on the ICAS display.

65
Q

MMO/VMO

A

.85 Mach 335 KIAS

66
Q

Max cruising Mach # in RVSM airspace (Boxed Item)

A

.83

68
Q

Flap extension speeds (Boxed Item)

A 
VFE
Flaps 1 230 KIAS
Flaps 8 230 KIAS
Flaps 20 230 KIAS
Flaps 30 185 KIAS
Flaps 45 170 KIAS
68
Q

Max tire limit speed is______

A

182 KIAS

69
Q

Max landing gear operating speeds (Boxed Item)

A

Gear position max operating speed
Extention 220 KIAS
Down and locked 220 KIAS
Retraction 200 KIAS

70
Q

Max speed for ADG operations is_____

A

VMO/MMO

71
Q

Max airspeed for windshield operations is____

A

250 KIAS

72
Q

Max airspeed for turbulence penetration is_____ (Boxed Item)

A

280 KIAS or .75 mach

73
Q

Maneuvering limit load factors

A

Flaps retracted -1.0 to 2.5 G

Flaps extended 0.0 to 2.0 G

74
Q

Max relief differential pressure is_____

A

8.7 psi

75
Q

Max negative differential pressure is_____

A

-0.5 psi

76
Q

During taxi, T/O and LDG the max differential pressure is______

A

0.1 psi

77
Q

The use of the EMERG DEPRESS switch above______is prohibited

A

15,000 feet

78
Q

Max altitude for single pack operation is_____

A

31,000 feet

79
Q

Max generator loading

A

40 KVA

80
Q

Minimum height use of the autopilot is____ (Boxed Item)

A

Take off 600 feet AGL
Non-precision Approach 400 feet AGL
Precision approach > 3.5 glide slope 120 feet AGL
Precision approach < or = 3.5 glide slope 80 feet AGL

81
Q

Max permissible continuous load on the TRU’s is____

A

120 Amps

83
Q

Max permissible time for ground operations with DC power is_____to protect the CRT display. (Boxed Item)

A

5 mins.

84
Q

Enroute use of slats/flaps is_____ (Boxed item)

A

Prohibited

85
Q

Flights with slats/flaps extended at altitudes above_____is prohibited (Boxed item)

A

15,000 feet

86
Q

Flight spoilers must not be extended in flight below an altitude of_____ (Boxed Item)

A

300 feet AGL

86
Q

Both stall protection system switches must remain_____for_____

A

On

All phases of flight

87
Q

To ensure adequate maneuver margin, flight spoilers must not be extended in-flight at air speeds below the recommended approach speed plus_____KIAS (Boxed Item)

A

10

88
Q

Do not attempt a_____after deployment of the______

A

Go-around

Thrust reversers

89
Q

Thrust reversers must be reduced to below_____%at ______KIAS

A

60%

75 KIAS

90
Q

Backing up with thrust reversers is_____

A

Prohibited

91
Q

Minimum flight crew consists of

A

One pilot and one co-pilot

92
Q

Taxi lights must be switched off whenever the airplane is stationary in excess of______mins. (Boxed Item

A

10 mins.

93
Q

Flight deck door

A

Closed and locked at all times during flight except in accordance with the approved procedures for opening, closing and locking the door

94
Q

Any time one of the flight crew leaves the flight deck

A

Another crew member must be present to ensure the required crew member is not locked out of the flight deck.

95
Q

Max N1% RPM

A

99.4 RPM

96
Q

Max N2% RPM

A

99.3% RPM

97
Q

Engine oil green temp range

A

-40 C to 155 C

98
Q

Engine oil Amber temp range

A

156 C to 163 C

99
Q

What is the max oil temperature for normal or APR power?

A

163 C limited to 15 mins.

100
Q

What is the minimum oil pressure?

A

25psi

101
Q

Reduced (FLEX) Takeoff Thrust is not authorized when

WEWAR

A

Wing and or cowl anti ice is on
Engine cannot achieve full rated thrust
Warnings or forecast of windshear or down drafts exists
Anti-skid system inoperative
Runway is contaminated with standing water, slush, snow or ice

102
Q

Flex thrust may be used for takeoff on wet runways provided the flight crew selects

A

“WET” runway performance data on the FMS (ACARS) PERF WT & BALANCE CONDITIONS

103
Q

Speed and N2% for engine relight windmilling from 21,000 to 10,000 feet

A

290 KIAS to VMO and 7.2% N2 minimum

104
Q

Speed and N2% for engine relight windmilling 10,000 to sea level

A

250 KIAS to VMO and 7.2% N2 minimum

105
Q

Wind within 30 degrees of aircraft nose or greater than 30 degrees but wind less than 5 Kts

A

No limitations-TOGA thrust may be applied before brakes released, but must be set by 60KIAS

106
Q

Wind > 30 degrees of aircraft nose between 5 and 30 Kts wind speed

A

Apply up to a max of 75% N1 before brakes released, then set TOGA thrust by 60KIAS

107
Q

Wind > 30 degrees of aircraft nose in either direction and or > 30 Kts wind speed

A

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

108
Q

Takeoff with engine fuel temp indications below 5 C is.

A

Prohibited

109
Q

Takeoff with bulk fuel temp indications below the limits stated is

A

Prohibited

110
Q

During flight, bulk fuel temp must remain?

A

Above the applicable bulk fuel freezing point.

111
Q

If use of oil replenishment system is required, how long after shutdown should the engine(s) be replenished?

A

Engine(s) should be replenished within 15 mins to 2 hours after engine shutdown

112
Q

Max refill allowable for oil replenishment system is____ without dry motoring the engine

A

2 US Quarts

113
Q

If the oil replenishment system has to be replenished to max capacity and the replenishment period has been exceeded the engine(s) must be

A

Dry-motored

114
Q

APU max EGT

A

1038 C

115
Q

APU EGT normal operating temp range is

A

0-806 C

116
Q

APU RPM normal operating range is

A

0-106% RPM

117
Q

Name all “8” pressurized doors

FLAGCRAM

A 
F orward cargo bay door
L eft over wing Emergency door
A vionics bay door
G alley service door 
C rew escape hatch
R ight over wing emergency door
A ft cargo bay
M ain passenger door
117
Q

What pressurized door is not displayed on ED2

A

Crew escape hatch

117
Q

What other major exterior door is not displayed, and is it pressurized?

A

Aft equipment bay door

No

118
Q

How many people can the main cabin door stairs support at once?

A

4 or 1000 lbs.

119
Q

Aside from the doors page on ED2, how can the main cabin door be verified closed?

A

By verifying all the green alignment pins on the inside of door are aligned.

120
Q

How many emergency light battery packs are there?

A

4- 6volts ea. wired in series

121
Q

How many mins of light will the emergency lights provide?

A

10 mins.

122
Q

What will cause the emergency lights to illuminate when the switch is in the armed position?

A

A loss of either A/C or D/C essential bus

123
Q

How long must the photo luminescent strips in the cabin be exposed to light prior to passenger boarding?

A

15 mins.

124
Q

If primary wing nav light burns out how is the secondary bulb selected?

A

Automatically

125
Q

When the seatbelt sign switch is in the auto position, when will the seatbelt sign illuminate automatically?

A

When the landing gear or flaps extend, or when the cabin altitude exceeds 10,000 feet.

126
Q

What sends the signal for the seatbelt to illuminate when the cabin altitude exceeds 10,000 feet?

A

CPAM

127
Q

What is the engine cool down limitation?

A

After landing the engine must be at or near idle thrust for two mins. Prior to shutdown.

128
Q

What is the normal N1 idle range?

A

20-25%

129
Q

What is the normal N2 idle range?

A

55-65%

130
Q

What is max continuous N2 %?

A

98%

131
Q

Max oil temp for max continuos thrust?

A

155 C

132
Q

How many fire extinguishers and PBE’s are there inboard the aircraft?

A

4 of each located within three feet of each other

133
Q

How many gallons do the forward and aft potable water tanks hold?

A
  1. 5 gallons forward

10. 1 gallons aft

134
Q

What provides pressure for the potable water inflight and on the ground?

A

Bleed air inflight

Electrical motor on ground

135
Q

Are the drain masts of the potable water heated

A

Yes

136
Q

The forward potable water shutoff valve is located?

A

In the flight deck coat compartment just above the floor.

137
Q

The aft potable water shutoff valve is located?

A

In the compartment located behind the toilet paper in the lav.

138
Q

What is the APU max RPM?

A

106%

139
Q

APU normal operating range for EGT?

A

0 to 806 C

140
Q

APU RPM normal operating range

A

0 to 106%

141
Q

How many life preservers are inboard the airplane?

A

There is one life preserver for each crew member and one additional life preserver for the flight deck jumps seat. Limited number of inflatable infant life vests and each seat cushion can be used as a floatations device.

142
Q

When does the cockpit voice recorder (CVR) begin recording?

A

As soon as the battery bus is energized.

143
Q

When does the flight data recorder (FDR) start recording?

A

When the strobes or beacon is on, or when aircraft is in flight.

144
Q

What is the length of the aircraft?

A

106’8” feet

145
Q

What is the wingspan?

A

76’3” feet

146
Q

What is the height of the aircraft at it’s tail?

A

24’10”

147
Q

How much room is required for an 180 degree turn?

A

75’ feet

149
Q

What is the minimum oil quantity for flight?

A

40% while shutdown.

149
Q

Why is the max differential pressure 0.1 psi for taxi, take-off and landing?

A

To allow the doors to easily open in the event of an emergency evacuation.

150
Q

What’s the minimum oxygen pressure for three crew members verses two crew members?

A

Three crew members requires 1110 psi and two crew members requires 810 psi

151
Q

What is the FRD event button used for on the center pedestal?

A

When the pilot what’s to record an event during flight, the pilot presses and holds the FDR button for two seconds.

152
Q

What is the max ITT for windmilling start? (Not assisted)

A

927 C

153
Q

Max continuous N1

A

99.5%

154
Q

The maximum ITT is _____ at APR MAX POWER for ____ minutes.

A

1006 for 2 minutes

155
Q

Maximum weight in the FORWARD cargo compartment?

A

1000

156
Q

Maximum weight in the AFT cargo compartment?

A

3740

157
Q

Engine Red Line Indications for N1, N2, Oil Temp and Oil Pressure.

A

N1 99.5
N2 99.4
Oil Temp 164
Oil Pressure 0-24

158
Q

Maximum Oil Pressure during Ground Start is ______ initially, and may be greater than _____ for a maximum of ___ minutes (Boxed Item)

A

182 and may peak beyond this value to amber dashes

95 psi for a maximum of 10 minutes.

159
Q

How much thrust do the engines produce at APR thrust and normal take-off thrust?

A

Max takeoff APR thrust 14,510
Normal take-off thrust 13,600
(Max continuous thrust is 13,386 when high power schedule is selected. Never used)

psa 2 (12 decks)

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