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why am i saying what what way > So You’re Flying Along… > Flashcards

So You’re Flying Along… Flashcards

1
Q

Single Engine Conditions

A

Collective - ADJUST
Airspeed - ADJUST
Engine anti-ice, cabin heater, and cockpit heater - OFF
Fuel/external cargo - DUMP or JETTISON

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2
Q

WARNING
If AC power is not available, what compartments will have fire protection?
With what fire bottle?

A

Only the No. 1 engine compartment or the APU compartment has fire protection.
Reserve fire bottle.

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3
Q

WARNING
Suspected Engine Compartment Fire

A

Visually confirm fire before engine shutdown

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4
Q

NOTE
Airspeed for discharging the fire extinguishers

A

Airspeed should be reduced to 100 KIAS or below before discharging fire extinguishers due to the airflow through the engine compartment at higher speeds

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5
Q

Dual Generator Failure Indications

A

CONV 1 FAIL and CONV 2 FAIL cautions
and
AC REF BUS DEGRAD advisory illuminate

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6
Q

WARNING
Loss of DC primary power in regards to power and advisory lights

A

Will result in the engine anti-ice and engine inlet anti-ice valves failing to the open position. This will reduce power available up to 20% Q per engine.
Respective ENG ANTI ICE advisory lights will not illuminate due to the loss of electrical power.

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7
Q

Battery Life

A

17 minutes

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8
Q

CONV 1 FAIL or CONV 2 FAIL caution illuminates checklist

A

There is none lol
Electrical power will be provided by the remaining system.

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9
Q

Post Engine Shutdown Fire Indications

A

Rise in TGT above 500 degree C after shutdown
and/or
excessive smoke from the engine exhaust

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10
Q

PTO - 1
BOOST SERVO OFF CAUTION ILLUMINATES indicates what?

A

A pilot valve jam in either the collective or yaw boost servo.

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11
Q

NOTE
During electrical malfunctions, even though it’s not listed as a checklist step, what should we be looking for?

A

Popped circuit breakers

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12
Q

NOTE
There isn’t a checklist for a single converter failure, but what can’t we do?

A

Turn off corresponding battery switch. It will cause the battery bus tie connector to close resulting in loss of all associated batter bus and DC essential bus.

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13
Q

WARNING with engine out audio

A

ENG OUT audio is not the sole indication of an engine failure and should be confirmed by verifying TGT, NG, and NP

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14
Q

T/R Quad Fail Caution
What will happen with one cable failure vs two?

A

one: if helicopter is shut down and or hydraulic power is removed, there’s no spring tension so quadrant spring will displace enough to unlatch the quadrant cable
two: a centering spring will position the tail rotor servo linkage to provide 10.5 degrees of pitch

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15
Q

Yaw Controllability Check
-CAUTION with airspeeds
-recommended type of landing

A

-airspeeds below target touchdown will result in right yaw
-shallow approach to rolling landing

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16
Q

NR decreasing from 100-96% with an increase in Q during steady flight with no engine malfunction, what’s happening?

A

main transmission planetary carrier may have failed

17
Q

Main Transmission Failure WARNING
-what is primary consideration?

A

land helicopter before failure progresses to gear box seizure or loss of drive to main and or tail rotor.

18
Q

Load Demand System Malfunctions
What positions can it fail to?

A

Full open or partial/stuck

19
Q

Basic Rules that apply to all aircraft emergencies

A
  1. Maintain aircraft control
  2. Analyze the situation
  3. Take proper action
  4. Refer to the checklist if time permits
20
Q

Land As Soon as Possible

A

A landing be made at the first available area which will assure minimal injury to crew/damage to the aircraft.

21
Q

Land as Soon as Practical

A

No injury to the crew or damage to the aircraft and acceptable access for corrective actions.

22
Q

PTO -1
WARNING Going to EDECU lockout does not remove what?

A

NG limiting or max fuel flow.

23
Q

PTO -1
What is the minimum egress with munitions and flares onboard?

A

600’

24
Q

PTO -1
When will FUEL 1 LOW or FUEL 2 LOW cautions illuminate?

A

Fuel level decreases to 250lbs in each tank.
Indicates a low fuel condition exists.

25
Q

PTO -1
What indication is there when a main fuel quantity status is failed?

A

Black text on red background, digital readout is displayed as three red dashes.

26
Q

PTO -1
What indication is there that a miscompare condition existsin the fuel system?

A

MAIN FUEL tape label will display as black text on a yellow background.

27
Q

PTO -1
When will the MAIN FUEL tape and digital readout (along with the TOTAL digital readout) turn yellow?

A

Below 300lbs

28
Q

What equipment will we have battery only? (no AC)

A
  • Pilots inboard MFD, FMS, FD/DCP
  • No 2 ADC
  • No 2 DCU
  • No 2 EGI
  • No 1 stabilator
  • LPCAPs
  • Coms 1-5
  • RADALT
  • digital clock
  • IFF/SIF
  • VOR/ILS
  • searchlight
  • IVHMS
29
Q

PTO -1
WARNING Associated with losing DC Primary power?

A

It will result in the engine anti-ice and engine inlet anti ice failing to the open position. This will result in reduced power up to 20% Q per engine. The advisory lights will not illuminate due to the loss of electrical power.

30
Q

PTO -1
How long will the auxiliary bearing operate for?

A

10 additional hours of operation after the caution illuminates.

31
Q

PTO -1
How is emergency electrical power provided?

A

A generator driven by the APU

32
Q

ENG OUT audio

A

NG below 55%

33
Q

Low Rotor RPM

A

NR is below approximately 96%

34
Q

FUEL DUMP FAIL caution condition

A

FUEL DUMP switch is in the DUMP position and no fuel dump flow has been detected within 25 seconds

35
Q

FUEL DUMP ON caution condition

A

FUEL DUMP switch is in the OFF position and fuel dump flow has been detected.

36
Q

FUEL 1/2 LOW caution condition

A

Tank is below approximately 250lbs

37
Q

FUEL PROBE FAIL caution conditions

A

Fuel probe has been in the unlocked state for more than 60 seconds.

why am i saying what what way (19 decks)

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