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Exam (elaborations)

FAM3102 Practice Test Questions and Answers All Correct

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  • FAM3102

FAM3102 Practice Test Questions and Answers All Correct When should you use the OIL SYSTEM MALFUNCTION OR LOW OIL PRESSURE? - Answer- 1. Red OIL PX annunciator illuminated 2. Amber OIL PX annunciator illuminated 3. Oil Pressure Fluctuations 4. Oil Temperature out of limits 5. Visibly confirm...

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  • September 28, 2024
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  • 2024/2025
  • Exam (elaborations)
  • Questions & answers
  • FAM3102
  • FAM3102
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Scholarsstudyguide
FAM3102 Practice Test Questions
and Answers All Correct
When should you use the OIL SYSTEM MALFUNCTION OR LOW OIL PRESSURE? -
Answer- 1. Red OIL PX annunciator illuminated
2. Amber OIL PX annunciator illuminated
3. Oil Pressure Fluctuations
4. Oil Temperature out of limits
5. Visibly confirmed leaking oil

What does the FUEL PX annunciator indicate? - Answer- The engine driven high
pressure fuel pump is suction feeding; Engine operation with the pump suction feeding
is limited to 10 hours

Should we reset the boost pump circuit breaker? - Answer- Unless a greater emergency
exists, DO NOT RESET

What equipment will be operative in the event of a Generator Bus Failure? - Answer- -
Battery buses w/ bus tie closed
- Backup UHF control panel
- EADI/EHSI composite mode only
- EFIS control panel (F.CP)
- GPS (F.CP)
- UHF Comm
- Audio (ICS)

Will the generator still be able to charge the battery in the event of a Generator Bus
Failure? - Answer- With an operating generator and the bus tie switch in NORM, the
generator will continue to charge the battery and power the battery buses

How long will the battery last after shedding the generator bus? - Answer- 30 Minutes

If GEN annunciator is illuminated, what is the first thing you should check? - Answer-
Verify starter switch position is NORM; the generator will be inoperative if in any other
position

Max Effective Braking? - Answer- Smooth, single application, increasing as airspeed
decreases

Max braking speed? - Answer- 80 KTS

, Max Abort Speed? - Answer- - When the abort speed is above rotation speed, rotation
speed becomes the abort speed.
- Calculated in charts A3-3 to A3-5; based on winds, runway conditions, air temperature,
weight, runway length, and runway gradient, and flap configuration

Battery Bus Failure considerations - Answer- - OBOGS will be inoperative once the
main battery is depleted or fails
- If the standby attitude gyro off flag appears after the battery bus has failed, the
indicator will continue to operate for at least 9 minutes
- Cockpit will depressurize when power to the battery bus is lost
- Place the bus tie switch to OPEN to isolate the generator bus from any potential
battery or battery bus faults
- Plan to extend the landing gear using the emergency extension system; indicators will
not be powered

If the situation requires immediate ground egress? - Answer- Eject; the ejection system
has the capability for 0/0 ejection

Precautionary Emergency Landing (PEL) - Answer- 1. TURN TO NEAREST SUITABLE
FIELD
2. CLIMB OR ACCELERATE TO INTERCEPT ELP
3. GEAR, FLAPS, SPEED BRAKE - UP
4. NON-BOLDFACE ITEMS

If Engine is vibrating excessively or if indications of failure are imminent during PEL,
what should you do? - Answer- SET PCL - OFF

What may diminish your visibility out of the canopy with an engine failure or
malfunction? - Answer- 1. It will disable the bleed air system and may cause canopy
icing and or fogging depending on the environmental conditions
2. Spray oil leakage on the windshield

What should you do if the rate of descent is greater than 1500 ft/min - Answer- Increase
torque as necessary (up to 131%) to achieve 1350 to 1500 ft/min rate of descent; Set
PCL to OFF if engine power is not sufficient to produce a rate of descent less than 1500
ft/min

Forced Landing Procedure - Answer- AIRSPEED - 125 KIAS PRIOR TO EXTENDING
LANDING GEAR
EMERGENCY LANDING GEAR HANDLE - PULL, AS REQUIRED
AIRSPEED - 120 KIAS MINIMUM UNTIL INTERCEPTING FINAL; 110 KIAS MINIMUM
ON FINAL
FLAPS - AS REQUIRED

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