CJ3 - Oral Questions Flashcards

(53 cards)

0
Q

During volts/amps check, when battery is selected to OFF, voltmeter shows 29 volts. Is this normal? What is the problem? May we depart?

A

No this is not normal. Battery relay is stuck closed. Can’t takeoff until the problem is fixed.

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1
Q

After engine start, start, start button remains illuminated. Is this normal?

A

No. Proceed to abnormal/emergency procedures checklist.

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2
Q

Before takeoff checklist item #14 is “Takeoff Data.” Where is it found?

A

AFM; FMS (w/takeoff datebase); checklist.

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3
Q

We are cleared to “line up and wait” when do we turn on pitot/static heat?

A

Wait to ensure we do not exceed two minutes of ground operation.

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4
Q

After takeoff, we notice that the “HYD PRESS ON” and “GEAR UNLOCKED” lights remain on. Is this normal? What problem do we suspect? What do we do?

A

No this is not normal. A gear uplock switch malfunction is likely. Proceed to the abnormal/emergency checklist procedures checklist.

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5
Q

During a battery overtemp, if placing the battery switch to “EMER” does not result in volts/amps decrease, the checklist calls for placing the switch back in the “BATT” why?

A

Battery relay is stuck. For the battery disconnect switch to work, the battery switch must be in “BATT” to power the disconnect relay.

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6
Q

After a dual generator failure, we go to operation on the emergency buses. In that configuration, describe the condition of the following systems: Flight guidance, EFIS, FADEC, Fuel, Ice protection, pressurization, landing gear, flaps, rudder bias, antiskid.

A

Flight guidance is inop; EFIS inop; FADEC normal (permanent magnet alternators); NO boost pumps, transfer valve or quantity indication; NO tail de-ice; bleed anti-ice fails on; Pressurization fails to MAX diff with manual control only; Gear and flaps are normal; NO rudder bias; NO antiskid.

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7
Q

After a decompression, emergency pressurization activates but we show no differential pressure. What is the likely problem?

A

Windshield bleed manual valves are open.

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8
Q

The “CABIN ALT” light illuminates. The rising cabin altitude will stop where?

A

14,500 when emergency pressurization activates.

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9
Q

A complete hydraulic failure requires a manual gear extension. How are the brakes affected?

A

They are NOT affected. The brakes, while hydraulic, are completely independent of the main hydraulic system.

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10
Q

On final, the cabin altitude selector shows a red light. Is this a problem?

A

Automatic pressurization control has failed; ensure cabin pressure differential is zero before landing.

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11
Q

Can we access SIDs and STARs on the MFD? Will they show the magenta geo-ref airplane? Why/why not?

A

SIDs and STARs are available on the MFD. They will NOT show geo-ref, as they are not drawn to scale.

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12
Q

We receive a “direct” routing from ATC sector, which we execute; next sector wants us back on the previous routing. How do we retrieve it?

A

Press “DIRECT” then “PREV.” The history page will then show up to 15 previous waypoints.

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13
Q

Holding in position for takeoff, we notice the FMS showing a “CHK POS” message. What can we do?

A

Select the departure runway with the DEP/ARR button, if we have not already done so. On the “LEGS” page, select “Runway Update.”

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14
Q

What are the steps to transition to a missed approach?

A
  • Press the “GA BUTTON”
  • Pitch to the command bars
  • Add power
  • Flaps to 15
  • Gear up
  • Flaps 0
  • Ensure navigation source is FMS
  • Select “NAV”
  • Autopilot ON
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15
Q

How may we depart a missed approach hold?

A

“EXIT HOLD,” with the next flight segment beyond the discontinuity; “DIRECT” to any subsequent fix; a heading to intercept any subsequent course, ensuring an intercept turn in the correct direction by placing on the “from” line of the “LEGS” page whichever fix will be behind us after the intercept.

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16
Q

Generally speaking what are the differences between the red, amber and white annunciators?

A

Annunciators are classified as warning, caution and advisory. Red annunciators indicate a warning, cause the master warning to flash and require immediate corrective action. Amber annunciators are caution and require immediate attention, but not necessarily immediate action. White annunciators are advisory but may require action. (i.e. stuck HYD PRESS ON).

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17
Q

Will the engine fire annunciator trigger a master warning?

A

No

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18
Q

What happens when the fire switch-light is pressed?

A

The fuel and hydraulic firewall shutoff valves close, the associated F/W SHUT OFF annunciator illuminates, the generator field relay open, the two fire bottle armed switch-lights illuminate.

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19
Q

What is the likely cause if a fire switch light fails to illuminate during the rotary test?

A

Bad fire loop or sensor.

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20
Q

Will the generator field relay reset automatically when the fire switch light is pressed a second time?

A

No

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21
Q

If the master warning annunciator flashes in the fire detection test position on the rotary test knob, what does it indicate?

A

A baggage smoke detection system is installed.

22
Q

What is the meaning of the red BATT O’TEMP (BATT FAULT) annunciator?

A

The NiCad or Lead acid battery has reached an internal temperature of 145°F (63°C)

23
Q

What are the memory items for the red BATT O’TEMP (BATT FAULT) annunciator procedure?

A

Volts/amps - Note.
Battery switch - EMER.
Volts/amps - Note decrease.

24
What is the meaning if the red >160° (BATT FAIL) annunciator illuminates and flashes?
The NiCad or Lead acid battery has exceeded an internal temperature of 160°F (71°C)
25
What altitude doe the red CABIN ALT annunciator illuminate?
Cabin altitudes 9500' in normal mode, 14,500' in high-altitude mode.
26
What is the meaning of the red BAGGAGE SMOKE annunciator?
Smoke has been detected in either the nose or aft baggage compartments.
27
What is the procedure for the illuminateion of the BAGGAGE SMOKE annunciator?
Land as soon as possible.
28
What are the minimum altitudes for autopilot use after takeoff, during an ILS approach, non-precision approach and cruise phase of flight?
Takeoff - 350' AGL ILS - 180' AGL Non-precision - 350' AGL Cruise - 1000' AGL
29
Can a coupled VOR approaches be conducted in NAV mode?
No. Must be in APPR mode or manually tracked in HDG mode. Applies to coupled and FD use.
30
What is the limitation on coupled VOR approaches as it relates to VOR location?
Coupled VOR approaches are prohibited if the VOR is located more than 15 miles behind the aircraft.
31
What is the maximum ramp weight of the CJ3? Takeoff weight? Landing weight? ZFW?
Max ramp weight =14,070 Max T/O weight = 13,870 Max Landing weight = 12,750 Max ZFW = 10,510
32
What is the maximum takeoff altitude limit?
14,000
33
For engine start, what is the maximum tailwind component/ Crosswind component? Maximum time to light-off?
Max tailwind = 10 Max crosswind = 10 Max light off = 10 seconds
34
What is the minimum voltage for a battery start?
24 volts.
35
What is the amperage range for a ground power start?
800-1000 amps
36
What is the maximum time to run the wing/eng/windshield heat on the ground above 75%N2?
Two minutes.
37
What is the maximum time to run the pilot-static heater on the ground?
Two minutes.
38
What are the maximum gear, flap 15, flap 34, and flap 55 speeds?
Max gear = 200 Flaps 15 = 200 Flaps 35 = 161 Flaps 55 = 140
39
What is MMO and VMO?
MMO = .737 VMO = 260 IAS below 8000' 278 IAS above 8000'-29,300
40
What is the maximum operating altitude limit?
FL450
41
What is the maximum cabin differential limit?
8.9 psid +/- .1 psid
42
Why are the windshield air manual valves normally left in the closed position?
To allow proper operation of the pressure switch and allow full airflow during emergency pressurization operation.
43
What is the meaning of the illumination of the W/S AIR O'HEAT annunciator on the ground with the switch in the off position?
The shutoff valve has failed in the open position or is leaking at least 5 psi into the system.
44
What is the de-powered position of the windshield air shutoff valve?
It is de-powered open.
45
When is the most likely time to experience a WING O'HEAT annunciation?
When checking the wing anti-ice system on the ground when ambient temps are warm and the power is kept too high for too long during the test. It occurs from the lack of cooling airflow over the wind leading edge.
46
What is the meaning of the RUDDER BIAS annunciator illumination in flight?
The valve is in bypass. The system does not function when the light is illuminated.
47
If the PWR BRK LOW PRESS annunciator illuminates, will the anti-skid system still be operational?
No. The antiskid inop annunciator will also be illuminated with a power brake failure.
48
What is the meaning of the FUEL LOW PRESS annunciator?
The fuel pressure to the engine-driven fuel pump is below normal (falling through 4.4 psi).
49
When will the white FUEL BOOST ON annunciator illuminate?
When the switch is placed in the ON position; during fuel transfer; during start with the pump in the NORM position; a failed motive flow pump.
50
When does the FUEL LOW LEVEL annunciator illuminate and why is there a 4 second delay in the master caution light illumination?
When fuel quantity decreases below 190 lbs +/-20 in either tank. The time delay avoids nuisance trips of the mater caution light in turbulence.
51
What are the meanings of the VIDEO FAIL (ANNUN PNL FAULT 1) and AUDIO FAIL (ANNUN PNL FAULT 2) annunciators?
A level of redundancy is inoperative (no loss of annunciator lights) and a level of redundancy is inoperative for the audio annunciation system. There will be no loss of sounds warnings.
52
What are the three conditions that may cause the TAIL DECICE FAIL annunciator to illuminate?
Either low voltage to the tail device bleed air valve or low pressure to the boots during a cycle; deice timer failure; tail deice circuit breaker is open.