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CRJ900 Mesa CL-65 Study Cards > Recurrent Written Exam > Flashcards

Recurrent Written Exam Flashcards

1
Q

What is the maximum takeoff weight of the CRJ 900?

A

82,500 lbs

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2
Q

What is the maximum landing weight of the CRJ 900?

A

73,500 lbs

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3
Q

The maximum total weight in the forward and center cargo compartments is

A

1,700 lbs

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4
Q

What is the maximum weight that can be supported by the main passenger door?

A

1,000 lbs

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5
Q

The DC service switch on the overhead panel “ON” is the primary service configuration used on line.

A

False

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6
Q

The DC service switch, in the “ON” position, will power the

A

DC Service Bus

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7
Q

The AC external power “AVAIL” switchlight indicates that:

A

AC external power is connected to the aircraft.
AC external power is at the correct voltage, frequency, and phase.
AC external power is not currently in use.

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8
Q

What does the illumination of the FAULT portion of an IDG switchlight indicate?

A

High oil temperature or low oil pressure in the IDG

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9
Q

With the hydraulic pumps in the AUTO/ON position, which pumps are running during a normal takeoff?

A

All 6 hydraulic pumps

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10
Q

When will a hydraulic B pump turn on with the switch in the AUTO position?

A

When the bus is powered, any generator is online, and flaps are out of 0

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11
Q

What methods are available to close the hydraulic SOV?

A

A guarded switchlight on the overhead panel.
Pressing the RH or LH ENG FIRE PUSH switchlight.

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12
Q

How many DC motors are installed to control the outflow valve?

A

3

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13
Q

At what cabin altitude do passenger oxygen masks automatically deploy?

A

14,000 ft

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14
Q

What is Ram Air used for in the CRJ 900?

A

Pack pre-cooling

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15
Q

Illumination of the FAULT portion of a pack switchlight indicates

A

An overpressure or overtemperature condition in the pack

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16
Q

When in manual pressurization mode, placing the MAN ALT switch in the UP position

A

Opens the outflow valve

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17
Q

With a red windshear warning displayed on the PFD, the airplane is experiencing:

A

A decrease in performance

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18
Q

What is the maximum altitude for slat/flap extension?

A

15,000 ft

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19
Q

Selecting the EMER FLAP switch to DEPLOY at 250 KIAS would not result in slat/flap movement.

A

True

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20
Q

What flap position would deploying the EMER FLAP switch result in?

A

20 degrees

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21
Q

Which hydraulic system is used for normal landing gear extension?

A

3

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22
Q

If hydraulic system 3 failed, what amount of nosewheel steering movement would be available?

A

8 degrees with the rudder pedals

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23
Q

If the ADG deploys, we must place hydraulic pump 3B switch into the ON position in order to power the pump

A

False

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24
Q

While single-engine taxiing on the first flight of the day (left engine running), with flaps set for takeoff, how much braking will be available?

A

Full braking

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25
Q

How would we conduct a bleeds closed takeoff?

A

Turn the APU on for takeoff

26
Q

If the APU is not operating and the APU door position is unknown or open, what is the maximum airspeed?

A

220 KIAS

27
Q

When must continuous ignition be selected ON?

A

Takeoffs and landings on contaminated runways

28
Q

What is the maximum speed landing gear can be retracted?

A

200 KIAS

29
Q

If we discharge the cargo fire bottles into the aft cargo compartment, we still have an additional bottle to discharge into the forward/center compartments.

A

False

30
Q

At what amount of imbalance does the EICAS display a FUEL IMBALANCE caution message?

A

800 lbs

31
Q

When will the fuel system computer automatically balance fuel?

A

200 lbs

32
Q

What is maximum fuel capacity for a gravity refuel?

A

14,810 lbs

33
Q

The refuel/defuel panel can be powered when the aircraft is not connected to any source of AC electrical power

A

True

34
Q

What is the maximum pressure differential for the aircraft?

A

8.7 PSI

35
Q

Pressing the EMER DEPRESS switchlight in flight will cause

A

The outflow valve to open.
Cabin altitude to be limited to 14,500 ft +/- 500 ft.

36
Q

What does pressing the ENG START switchlight do?

A

Closes the ISOL valve.
Closes the pack valves.
Closes the bleed air valves (PRSOVs).

37
Q

FADEC provides protection for hot starts only

A

False

38
Q

What is the danger area in front of the aircraf with the weather radar operating?

A

2 ft

39
Q

Pressing the TOGA buttons on the ground causes:

A

TO lateral mode, which will maintain heading at weight-off-wheels with a maximum 5 degree bank angle.
TO vertical mode which results in an optimized pitch-up attitude on the flight director.
Updates the FMS position to the end of the runway.

40
Q

Pressing the TOGA buttons in the air results in:

A

A 10 degree pitch up on the flight director

41
Q

A set of _____ rechargeable batteries powers the emergency lights for ___ minutes in the event of a loss of electrical power.

A

5, 10

42
Q

How often must the emergency equipment in the aircraft be inspected?

A

Every 12 calendar months

43
Q

Caution and status messages can be boxed, while warning and advisory messages cannot.

A

True

44
Q

An advisory message indicates:

A

That a safe condition exists

45
Q

What is the rating of the TRUs?

A

120 A

46
Q

The primary flight controls in the CRJ900 are:

A

Controlled by a system of cables and pulleys

47
Q

After pulling the ROLL DISC handle, an amber ROLL SEL switchlight will illuminate on the glareshield. Selecting that swtichlight will:

A

Provide cross-side MFS panel control to assist in roll

48
Q

The thrust reverser translating cowls are actuated by:

A

The on-side hydraulic system

49
Q

Thrust reversers must be idle or stowed by:

A

60 KIAS

50
Q

When flying a visual approach, the autopilot must be disengaged by:

A

400 ft AGL

51
Q

An engine fire on the ground will cause both engine fire bottles to discharge automatically into the affected engine.

A

False

52
Q

The engine core and turbine sections are equipped with a dual-loop overheat detection system.

A

True

53
Q

What causes the AC ESS XFER switchlight to illuminate?

A

AC ESS bus is being powered by a source other than AC bus 1

54
Q

NAV 2 can be tuned using:

A

Either RTU.
The FMS radio page.
FMS auto tuning.

55
Q

What is the minimum battery voltage required on both batteries to start the APU?

A

22V

56
Q

What causes the illumination of the ICE caution message and associated switchlight?

A

Icing conditions detected with wing and/or cowl anti-ice selected off

57
Q

How long after turning the battery master on must we wait prior to completing a fire detection test?

A

30 seconds

58
Q

The pilot is authorized to reset any circuit breaker that may have popped without authorization from maintenance control or a specific procedure.

A

False

59
Q

At what point does the crew oxygen blowout disc blowout?

A

2,800 PSI

60
Q

How long will the chemical oxygen generators for passengers generate oxygen after activation?

A

13 minutes

CRJ900 Mesa CL-65 Study Cards (9 decks)

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