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RJ Stuff > CRJ Limitations & Other Items > Flashcards

CRJ Limitations & Other Items Flashcards

0
Q

Maximum Taxi and Ramp weight

A

RJ200 - 53,250 lbs

RJ700 - 75,250 lbs

RJ900 - 85,000 lbs

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1
Q

Maximum Takeoff weight

A

RJ200 - 53,000 lbs

RJ700 - 75,000 lbs

RJ900 - 84,500 lbs

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2
Q

Maximum Landing Weight

A

RJ200 - 47,000 lbs

RJ700 - 67,000 lbs

RJ900 - 75,100 lbs

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3
Q

Maximum Zero Fuel Weight?

A

RJ200 - 44,000 lbs

RJ700 - 62,300 lbs

RJ900 - 70,750 lbs

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4
Q

Maximum Pressure Altitude for takeoff and landing?

A

8,000 ft

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5
Q

Maximum Operating Altitude?

A

RJ200 - 36,000 ft

RJ7-9 - 41,000 ft

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6
Q

Minimum Ambient Temperature for Takeoff?

A

-40 deg C

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7
Q

Definition of Icing Conditions:

COWL

A

Icing Conditions exist when the OAT or TAT is 10°C or below, and:
• Visible moisture in any form, is present in flight, or below 400 feet AGL for ground operations, or
• When operating on surfaces that are wet or contaminated

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8
Q

When must COWL ANTI-ICE be on?

A

Cowl Anti-Ice must be ON for all ground and flight operations when icing conditions exist except when the inflight SAT is -39°C or below, or ICE is annunciated by the ice detection system.

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9
Q

Definition of Icing Conditions:

Wing

A

Icing conditions exist when the OAT is 5°C or TAT is 10°C or below, and:
• Visible moisture in any form, is present in flight, or below 400 feet AGL for takeoff, or
• The runway is wet or contaminated.

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10
Q

When must WING ANTI-ICE be on?

A

Wing Anti-Ice must be ON for takeoff and flight operations when ICE is annunciated by the ice detection system, or when icing conditions exist and the airspeed is less than 230 KIAS except when the inflight SAT is -39°C or below.
RJ200
Wing Anti-Ice must be ON for the final two minutes prior to takeoff during all ground operations 5°C
OAT or below unless Type IV anti-icing fluid has been applied.

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11
Q

Do not hold in icing conditions with ________ and/ or _______ extended.

A

Slats ; Flaps

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12
Q

Continued operation in areas where SuperCooled Large Droplet icing conditions exist is _____________

A

Prohibited

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13
Q

All contaminated performance data will be for __________ takeoffs.

A

RJ200 - Static

RJ7-9 - Rolling

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14
Q

Maximum Tailwind for takeoff and landing _________

A

10 kts

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15
Q

Maximum Crosswind for takeoff and landing ________

A

27 kts

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16
Q

Maximum Crosswind for landing from a CAT II Approach

A

15 kts

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17
Q

Flights must be within _________ minutes of a suitable airport with cargo in the cargo compartment.

A

RJ200 - 45 min

RJ7-9 - 60 min

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18
Q

EICAS Limit Markings.
RED
AMBER
GREEN

A

Maximum and Minimum Limitations
Caution Range
Normal Operating Range

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19
Q

Maximum ITT for start

A

900 deg. C

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20
Q

Engine to engine N2 split at ground idle power should not be greater than___________ and If____________________________________, do not accelerate above idle.

A

2%

If N2 is 57% or less with an OAT of -20°C or warmer

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21
Q

Maximum ITT for all air starts

A

90 deg C

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22
Q

Maximum ITT allowed to advance the thrust levers to Idle for all ground starts

A

120 deg C

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23
Q

Oil Pressure Steady-state idle

A

25 psi

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24
Q

Oil Pressure Takeoff Power

A

45 psi

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25
Q

Minimum oil temperature for engine starting

A

-40 deg C

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26
Q

During ALL starts, do not exceed _______ N1 for _____ minutes after start, or until all operating indications are in the normal range, whichever is _________.

A

75% ; 2 ; longer

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27
Q

Operate engines at or near idle for _______ prior to shutdown.

A

2 minutes

  • Taxi time at a stabilized 80% N2 or below may be credited towards the 2 minutes cool down period
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28
Q

Define Airplane Cold Soaked

A

Before the first flight of the day, when the airplane is cold-soaked at an ambient temperature of -30°C (-22°F) or below for more than 8 hours:
• The engines must be motored for 60 seconds and fan rotation must be verified before an engine start is initiated

• Thrust reversers must be actuated until the deploy and stow cycles are less than 5 seconds
2 seconds

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29
Q

Continuous Ignition must be used during

A
  • Takeoff and landing on contaminated runways
  • Takeoff with high crosswind components (15 knots or greater)
  • Flight through moderate or heavier intensity rain
  • Flight through moderate or heavier intensity turbulence
  • Flight in the vicinity of thunderstorms
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30
Q

Starter Cranking Limits - RJ200

A

1 min on / 10 seconds off
1 min on / 10 seconds off
1 min on / 5 minutes off

The starter must not be engaged if the indicated N2 RPM exceeds 55%

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31
Q

Dry Motoring Cycle for engines

A

90 sec on / 5 min off

30 sec on / 5 min off

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32
Q

Maximum Fuel imbalance between the left and right wing tank?

A

RJ200

800lbs - At all times

RJ7-9

Take off - 300 lbs

All Phases of Flight - 800lbs

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33
Q

Maximum total fuel for pressure Refueling?

A

RJ200 - 14,518 lbs

RJ7-9 - 19,594 lbs

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34
Q

Takeoff with a fuel load in excess of __________ , in the center tank is not permitted unless each wing tank is above _____________

A

500 lbs; 4,400 lbs

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35
Q

Powered Crossflow and gravity Crossflow must be _________ for takeoff.

A

OFF

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36
Q

Takeoff with engine fuel temperature indications below __________ is prohibited.

A

5 Degrees C

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37
Q

Minimum Fuel Quantity for a go-around per wing tank, assuming 10 degrees pitch up ___________

A

RJ200 - 450 lbs

RJ7-9 - 600lbs

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38
Q

APU Start cycles on Battery - RJ200

A

30 secs / 2 min
30 secs / 20 min
30 secs / 2 min
30 secs / 40 min

The 2 minute delay between cranking attempts is to allow for cooling of the starter, start contractor and APU fuel drainage

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39
Q

APU Start cycles on DC ground Power - RJ200

A

15 secs / 2 min
15 secs / 20 min
15 secs / 2 min
15 secs / 40 min

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40
Q

APU Maximum starting altitude

A

RJ200 - 30,000 ft.

RJ7-9 - 37,000 ft.

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41
Q

APU Maximum Operating altitude

A

RJ200 - 36,000 ft.

RJ7-9 - 41,000 ft.

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42
Q

Maximum APU RPM

A

RJ200 - 107 %

RJ7-9 - 106%

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43
Q

With the APU door not closed, or the door position is unknown: The airplane must be limited to _________, or _______________________________________ .

A

RJ200 - 300 KIAS

RJ7-9 - 220 KIAS

The APU must remain in operation

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44
Q

Maximum Bleed air extraction altitude for Air Conditioning from the APU is _________________ .

A

RJ200 - 15,000 ft.

RJ7-9 - 25,000 ft.

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45
Q

Maximum engine start altitude with APU bleed air ___________

A

RJ200 - 13,000 ft.

RJ7-9 - Starter Assisted Main Engine Start (MES) Limitation of 21,000 ft. Not an APU limitation

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46
Q

Minimum Engine Oil Pressure for Takeoff __________ .

A

45 psi.

47
Q

Flaps extended and operating Speeds?

RJ200

A

8 - 230 / 200
20 - 220 / 200
30 - 185
45 - 170

48
Q

Gear Position and Operating Airspeed limitations?

A

Extension - 220
Down and Locked - 220
Retraction - 200

49
Q

Tire limit ground speed

A

RJ200 and 700 - 182 Knots

RJ900 - 195 knots

50
Q

Maximum airspeed for windshield wiper operation failed in the non-parked position.

A

RJ200 - 220 KIAS

RJ7-9 - 250 KIAS

51
Q

Maximum Turbulence Penetration Speed

A

280 KIAS or .75 Mach whichever is lower

52
Q

Maximum Cruise Mach in RVSM Airspace

A

0.82 Mach

53
Q

RVSM Required Equipment List?

A

Autopilot - Must be operational
Altitude Alerting System - Must be operational
2 Transponders with Altitude Reporting - 1 Must be Operational
2 Air Data Computers - Both must be operational

54
Q

Minimum Auto Pilot Engagement altitude __________ , except when performing:
Non-Precision Approach ___________
Precision Approach __________

A

600 ; 400 ; 80 AGL

Glide path greater than 3.5 < 4.0 degrees with airport elevation is < 4000 ft minimum height for autopilot use is 120 AGL

55
Q

Maximum Slat/Flaps extension altitude _____________

A

15,000 ft

56
Q

Maximum permissible time on the ground with only DC power ___________

A

5 minutes

57
Q

Minimum altitude for flight spoiler deployment

A

1,000 ft. AGL

58
Q

Minimum airspeed for flight spoiler use ________________

A

VREF + 17 KIAS

59
Q

Minimum brake cooling time _____

A

15 minutes, and all BTMS indicators must be green and not increasing

60
Q

During landing, maximum reverse thrust is prohibited below__________, and reverse idle should be achieved by____________

A

75 KIAS

60 KIAS

61
Q

Use of the EMER DEPRESS switch above ___________ is prohibited.

A

15,000 ft.

62
Q

Max altitude for single pack operations _______________.

A

RJ200 - 25,000 ft.

RJ700, 900 - 31, 000 ft

63
Q

Max differential pressure during ground maneuvering__________

A

0.1 psi

64
Q

Maximum relief differential pressure ___________ .

A

8.7 psi

65
Q

Braking Loss / Asymmetry

A
  1. Wheel brakes ……. Release Momentarily
  2. PM will switch ANTI-SKID OFF
  3. Wheel brakes ……. Re-Apply as required
  4. Reverse Thrust . Apply maximum until stopping assured
66
Q

Cabin Alt

A
  1. Oxygen Mask ……… Don and 100%
  2. Crew Communication …… Establish
  3. CAPT assumes PF Duties
67
Q

Double Engine Failure

A
  1. CONT IGNITION …….. ON

2. Airspeed ……. 240 KIAS minimum

68
Q

Smoke / Fumes

A
  1. Oxygen Mask (If Required)…… Don and 100%

2. Crew Communication …… Establish

69
Q

Stab Trim Runaway

A
  1. Control Wheel…….. Assume Manual Control and override runaway
  2. BOTH STAB TRIM DISCONNECT ……. PUSH, HOLD and RELEASE
  3. CAPT assumes PF duties
  4. STAB CH. 1 cb (2F5) …… OPEN
  5. STAB CH. 2 cb (4A1) …… OPEN
70
Q

What is the Tactile Check?

A

In addition to a visual check a Tactile Check of the Wing Leading Edge, Forward Upper, and Rear Upper Surfaces. Conducted during walk around to determine they are free of frost, ice, snow, or slush when…

  • OAT is 10 deg C or below, or
  • Bulk Fuel Temp is 0 deg C or below, or
  • Atmospheric conditions have been conducive to frost formation
  • Ice and Frost may adhere for sometime even at OAT higher than 10 deg C
71
Q

Name all the Boldfaced Emergency Procedures

A 
Double Engine Failure
Stab Trim Runaway
Braking Asymmetry / Loss of Brakes
Cabin Alt Message or Emergency Descent
Smoke/Fumes in the Cockpit
Aileron Jam, 
Elevator Jam
Rudder Jam
Un-commanded Yaw
Low Engine Oil Psi.
72
Q

Maximum ambient temperature for takeoff and landing

A

ISA +35C

73
Q

RJ200

If both engines are to be started using the APU bleed air, the operating engine’s thrust must not exceed

A

70% N2

74
Q

Taxi lights must be switched off whenever the airplane is stationary for

A

10 minutes

75
Q

T
E
S
T

A

T - Type of Emergency
E - Estimated Time of Arrival
S - Signal for Brace
T - Take Special Instructions

76
Q

The Pilot Flying (PF) MUST confirm the following

A 
T - Thrust Levers
E - Engine Fire Push Switchlights
G - GEN Switchlights
A - All Other Guarded Switchlights
F - Fuel Boost Switchlights
77
Q

APU will auto shutdown in flight for the following:

A 
F – FIRE (Bottle will not discharge)
O - OVERSPEED
D – DC Power loss
E – ECU Failure
R – RPM Signal loss
S – SLOW/Abnormal Start
78
Q

Different ways to disconnect the Auto Pilot

A
  • Stick Pusher
  • Trim use while AP engaged
  • AP yoke button
  • AP button on the FCP
  • AP Disengage Bar on the FCP
  • Disconnection of both Yaw Dampers
79
Q

Items that have to be on a release to make it legal:

A 
D – Departure and Destination Airports
A – Alternate Airport (if required)
M – Minimum Takeoff Fuel (MINTO)
I – IFR or VFR
T – Tail Number of A/C
T – Trip Number
80
Q

Ram Air is used for the following:

A
  • Cool Packs and Heat Exchangers
  • Cool HYD Systems 1 and 2
  • Used for takeoff/landing with Anti-Ice on and APU deferred
  • Used to evacuate the cockpit of smoke and fumes
  • On ground a small electric fan is used to draw in air to assist in cooling
81
Q

FLEX T/O IS PROHIBITED WHEN:

A

A – ANTI-SKID is Inop
B – BLEEDS – 14th Stage wing and/or cowl anti-ice is on
C – Contaminated Runway
D – Aircraft has been DE-ICED
E – ENGINE is unable to produce full thrust
F – The aircraft is FIELD limited as per the TLR
G – GUSTS – Windshear warnings or forecasts are present

82
Q

MINIMUM REDUCED FLEX POWER

A

83.5% N1

83
Q

What 2 MEL categories are extendable?

A

B (3 day period)
C (10 day period)

Excluding the day it was written

84
Q

Where are CDL Stickers found?

A

Under the standby instruments.

85
Q

Maximum headwind for landing from a Category II Approach

A

16 kts

86
Q

Flaps extended and operating Speeds?

RJ7-9

A 
1 - 230
8 - 230 
20 - 220 
30 - 185
45 - 170
87
Q

APU START CYCLES - RJ7-9

A

Limited to not more than three (3) starts/start attempts in one (1) hour with a two (2) minute delay between cranking attempts.

88
Q

Starter Cranking Limits - RJ7-9

A

90 seconds on / 10 seconds off
90 seconds on / 10 seconds off
90 seconds on / 5 minutes off

89
Q

RJ900
For precision approaches (PAR/ILS) or approach procedures with vertical guidance, the minimum height for autopilot use with one engine operating is____________

A

110 ft. AGL

90
Q

RJ200

If both engines are to be started using the APU bleed air, the operating engine’s thrust must not exceed__________

A

70% N2

91
Q

Max differential pressure during initial landing________

A

1.0 psi

92
Q

Low Pressure Air must be______prior to the main cabin door being closed and secure

A

OFF

93
Q

The 10th stage bleed air valves must be______for takeoff and landing if the anti-ice systems have been selected ON

A

Closed

94
Q

Cabin Pressurization must not be operated to a cabin altitude of__________when the system is manual mode

A

-1500ft below sea level

95
Q

Full application of rudder and aileron controls, as well as maneuvers that involve angles of attack near the stall, must be confined to speeds________

A

Below Va

96
Q

Maximum continuous load on each TRU

A

RJ200 - 100 amps

RJ700 and 900 - 120 amps

97
Q

After cold start, engine must remain at_______until oil pressure returns to normal range

A

Idle

98
Q

Ground contamination definition

A

Runways, ramps or taxiways with surface snow, ice, slush, or standing water

99
Q

Visible moisture definition

A

Visible moisture of any form such as clouds, fog with visibility of one mile or less, mist, rain snow, sleet, ice crystals or clouds in flight

100
Q

L(R) Engine Oil Pressure
Or
Oil Pressure Low

A
  1. (L/R) Engine oil pressure…….Check

2. (L/R) Thrust Lever ……..Confirm and retard to idle

101
Q

Aileron System Jammed

A
  1. Autopilot………………………….Disconnect
  2. Both Aileron controls………….Release pressure
  3. ROLL DISC handle …………PULL, TURN 90° to lock
  4. Airplane control…………..Reference Flight Control synoptic and transfer to pilot with operative aileron
102
Q

Elevator System Jammed

A
  1. Autopilot……………………………Disconnect
  2. Both Elevator controls………….Release pressure
  3. PITCH DISC handle……….. PULL, TURN 90° to lock
  4. Airplane control……………….Reference Flight Control synoptic and transfer to pilot with operative elevator
103
Q

Rudder System Jammed

A
  1. Yaw Damper……………………DISC

2. Rudder pedals…………………Overpower

104
Q

Uncommanded Yaw Motion

A
  1. Controls ………….Assume manual control and counter aircraft motion using control wheel
  2. YAW DAMPER, DISC button …………..Push
105
Q

Unreliable Airspeed In-Flight

A

If above minimum safe altitude:

1.Autopilot …………………………..DISENGAGE
2. FDs………………………………….DESELECT
3. Use standby attitude indicator / ISI.

If below minimum safe altitude:

  1. Autopilot …………………..DISENGAGE
  2. FDs…………………………..DESELECT
  3. Use standby attitude indicator / ISI.
  4. Pitch/N1…………………….10 degrees/TO
  5. Airplane …………………Go-around, clean up and climb above minimum safe altitude

Above 15,000 feet:

  1. Pitch/N1………………….5 degrees/CLB

Caution Respect stall warning/stick shaker.

106
Q

The order in which to deal with multiple failures

A

E - Electric
H - Hydraulic
P - Pneumatic
O - Other

107
Q

Use of Speed Mode (DES or IAS) flight director or autopilot coupled, during Approach is__________

A

Not Permitted

108
Q

Use of VNAV, flight director or autopilot coupled, during the climb and approach phases of flight is__________

A

Not Permitted

109
Q

What is the normal range for the hydraulic System pressure and fluid?

A

3000 psi +/- 200

45-85%

110
Q

Maximum weight in the cargo compartment

A

RJ200 - 3500 lbs

RJ700 - FWD - 1000 lbs / AFT - Varies

RJ900 - FWD - 1000 lbs / AFT - 3470 lbs

111
Q

What is significant about Flight Abort Mode?

A

Alleviates the pilot from having to reset the landing elevation when aborting a flight to return to the takeoff airfield by reverting cabin altitude to the prepressurization altitude

  • Armed during the first 10 minutes after takeoff
  • Aircraft altitude is less than 6,000 feet
  • A descent of 1,000 fpm is initiated in this window
112
Q

Except in an emergency, Takeoff or landing will not be attempted whenever peak wind value exceeds

A

50 kts

113
Q

The bleed air 10th-Stage Valves must be closed for takeoff and landing if the anti-ice systems have been selected

200 only

A

ON

114
Q

CAT II approaches are prohibited when the braking action is reported as

A

Less than “Medium”

RJ Stuff (4 decks)

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