Brainscape's Knowledge GenomeTM

Browse over 1 million classes created by top students, professors, publishers, and experts.


See full index

2FTS Basic Knowledge > Emergency Notes, Warnings and Cautions > Flashcards

Emergency Notes, Warnings and Cautions Flashcards

1
Q

Warning x 4 for EJECTION CHECKS

A
  1. The Canopy must be closed and locked before ejecting
  2. Notify the other occupant as soon as possible.
  3. Make a conscious effort to adopt the correct ejections posture
  4. Simultaneous ejection of both seats is inadvisable as seat entaglement could occur. The aircraft captain should order and wait for the other occupant to eject when operating with the ISS selector INDEPENDENT
How well did you know this?
1
Not at all
2
3
4
5
Perfectly
2
Q

Correct Ejection Posture

A
  1. Buttocks well back in seat
  2. Back pressed firmly against the seat back and sitting as straight as possible.
  3. Press head firmly against headpad
  4. Eyes closed.
  5. Legs forward with feet touching the rudder pedals to ensure optimum thigh support.
  6. Grip the ejection handle with the preferred hand. Use the other hand to grip the wrist of the pulling hand to prevent flailing at high speeds.
How well did you know this?
1
Not at all
2
3
4
5
Perfectly
3
Q

Ejection Checks

A

Carry out as many of the following checks as time permits.

  1. Seat Harness ….. Secured and Locked
  2. PSP …………………. Connected
  3. Helmet ……………. Visors down, chin strap secured.
  4. Seat Pin ………….. Removed
  5. Location …………. Suitable
  6. Height …………….. Ideally 2000ft AGL
  7. Airspeed …………. 150-250KIAS
  8. Trim …………………. 1/3 aileron trim
  9. Attitude …………… Wings Level, climbing
How well did you know this?
1
Not at all
2
3
4
5
Perfectly
4
Q

Note associated with Ejection Checks

A
  1. Leave the PCL at FUEL OFF if the engine has been shut down.
How well did you know this?
1
Not at all
2
3
4
5
Perfectly
5
Q

Warning Associated with Emergency Eggress on the ground

A

Eject if circumstances dictate; however, do not attempt to eject if:

  1. The occupants are not correctly strapped in.
  2. The canopy is not closed and locked
  3. The front cockpit CFS pin and seat pin, or rear cockpit seat pin when the seat is occupied is not removed.
How well did you know this?
1
Not at all
2
3
4
5
Perfectly
6
Q

Caution associated with Emergency Landing Checks

A

Anti-skid is inoperative when the main hydraulic system is nor operating. Apply brakes carefully with anti-skid inoperative.

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
7
Q

Notes x 3 associated with Emergency Landing Checks

A
  1. Do not check brakes after the emergency landing gear extension in order to preserve emergency hydraulic pressure for flaps extension and emergency powered braking after landing.
  2. Emergency powered braking may be limited after landing.
  3. The normal hydraulic system is disabled when the emergency landing gear handle is pulled. You will lose
    . Normal landing Gear Operation
    . Normal powered braking
    . Anti-skid
    . Normal flaps operation
    . Roll Spoilers
    . Powered aileron system
    . Airbrake
How well did you know this?
1
Not at all
2
3
4
5
Perfectly
8
Q

Note Associated with Engine Fire Or Smoke And Fumes - On Ground

A

The DWP and MFD FIRE warnings indicate engine fire. Smoke or fumes may exist without DWP and MFD FIRE indications.

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
9
Q

Warning Associated with Engine Fire Or Smoke And Fumes - On Ground

A

Activating the EO2 may lead to pure oxygen flowing into the cockpit during egress. However, operate the EO2 if incapacitation due to fumes is assessed to be a greater risk

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
10
Q

Caution x 2 Associated with Engine Fire Or Smoke And Fumes - On Ground

A
  1. Anti-skid is inoperative when the main hydraulic system is not operating (eg engine shutdown). Apply brakes carefully with anti-skid inoperative.
  2. Normal powered braking is not available when the main hydraulic system is not operating. Manual Braking requires higher than normal brake pedal pressure and travel for efficient braking.
How well did you know this?
1
Not at all
2
3
4
5
Perfectly
11
Q

Note associated with Engine Fire - In Flight

A

The DWP and MFD FIRE indcate engine fire. Smoke of fumes may exist without DWP and MFD FIRE indications

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
12
Q

Warning Associated with Engine Fire - In Flight

A

Monitor EO2 contents and descend to a safe altitude before EO2 is exhausted.

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
13
Q

Caution Associated with Engine Fire - In Flight

A

Observe engine limits manually and avoid rapid power changes with the PMS in manual mode.

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
14
Q

Warning x 3 Associated with Smoke Or Fumes In The Cockpit - In Flight

A
  1. Monitor EO2 contents and descent to a safe altitude before EO2 is exhausted
  2. Land as soon as possible following smoke or fumes in the cockpit
  3. Ensure the occupants are wearing gloves, and mask and visors are down prior to operating the MDC handle.
How well did you know this?
1
Not at all
2
3
4
5
Perfectly
15
Q

Note x 4 Associated with Smoke or Fumes in the cockpit - In Flight

A
  1. The overpressure of breathing gas in the
    oxygen mask should not permit cockpit air
    to contaminate the breathing gas. Conduct
    the Smoke Or Fumes In The Cockpit – In
    Flight procedure if fumes are present in the
    oxygen mask.
  2. As engine bleed air is used to pressurise
    the cockpit (P2.5 and P3 air) and to supply
    the OBOGS (P3 air), fumes in the engine
    compartment may be present as fumes in
    the cockpit or mask.
  3. If the source of the smoke or fumes can
    be identified positively originating from a
    specific cockpit system (eg smoking FMS or
    HUD), consider selecting the specific system
    to off and cabin pressure to RAM, to ensure
    continuing oxygen supply from the OBOGS
    and preserve EO2 contents. Conduct the
    full Smoke Or Fumes In The Cockpit – In
    Flight checklist if there is any doubt as to the
    source of the smoke or fumes.
  4. The SFD will be the only remaining functional
    electrical service with the batteries and
    generators off. It will operate for at least
    30 minutes on a fully charged emergency
    battery. NAV 1 will not operate.
How well did you know this?
1
Not at all
2
3
4
5
Perfectly
16
Q

Warning x1 Associated with Aborted Take-Off

A

Eject if there is likely risk of collision

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
17
Q

Caution x2 Associated with Aborted Take-Off

A
  1. Anti-skid is inoperative when the main
    hydraulic system is not operating (eg
    following engine shutdown or failure). Apply
    brakes carefully with anti-skid inoperative.
  2. Normal powered braking is not available
    when the main hydraulic system is not
    operating:
    • Manual braking requires higher than
    normal brake pedal pressure and travel
    for efficient braking
    • Release the brakes and pull the
    emergency landing gear handle if
    emergency powered braking is required
How well did you know this?
1
Not at all
2
3
4
5
Perfectly
18
Q

Warning x1 Associated with Engine Failure After Take-off

A

Delaying ejection in a futile attempt to restart
the engine, recover controlled flight or reach
an aerodrome may place the aircraft in
marginal conditions for safe ejection. Eject
if unable to carry out a forced landing safely

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
19
Q

Warning Associated with Engine Mechanical Failure

A

Monitor EO2 contents and descend to safe

altitude before EO2 is exhausted.

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
20
Q

Warning Associated with Engine Flamout

A

Monitor EO2 contents and descend to safe

altitude before EO2 is exhausted.

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
21
Q

Caution Associated with Engine Flameout

A

Minimise power changes following engine

flameout.

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
22
Q

Indiciations of an Engine Flameout

A 
• Loss of power
• ITT below 400°C
• NG decreasing below 80% with PMS
in automatic mode and 70% with PMS
in manual mode
23
Q

Warning Associated with Engine Surge

A

Monitor EO2 contents and descend to safe

altitude before EO2 is exhausted

24
Q

Caution x2 Associated with Engine Surge

A
  1. Minimize power cvhanges following engine surge.

2. Observe engine limitations manually and avoid rapid power changes with the PMS in manual mode.

25
Q

Note Associated with Engine Surge

A

The maximum permitted torque is 2850 ft lb

(67.5%) with the PMS in manual mode.

26
Q

indications of an Engine Surge

A

• Loss of power
• ITT excessively high or fluctuating
• Unusual engine noise (popping or
rumbling)

27
Q

Caution x2 Associate with PMS Failure

A
  1. Observe engine limits manually and avoid rapid power changes with the PMS in manual mode.
  2. Attempt PMS reset once only.
28
Q

Caution x3 Associated with Propeller Speed

A
  1. Continue flight at low speed using minimum practical power.
  2. Monitor the engine for indications of mechanical failure.
  3. Maximum torque is 2000 ft lb with NP < 1000 RPM
29
Q

Caution Associated with Engine Temp - In Flight

A

Low ITT may indicate engine flameout

30
Q

Warning Associated with Engine Temp - In Flight

A

Monitor EO2 contents and descend to safe altitude before EO2 is exhausted

31
Q

Caution Associated with Engine Speed Checklist

A

Low NG may indicate engine flameout

32
Q

Warning Associated with Engine Speed Checklist

A

Monitor EO2 contents and descend to safe altitude before EO2 is exhausted

33
Q

Note x 3 Associated with oil Pressure Out of Limits

A
  1. oil pressure may be as low as 40psi during aerobatics if recovery is within 20second.
  2. Manoeuvres which cause the oil pressure to exceed permitted limits should be avoided.
  3. Verify oil pressure under positive g.
34
Q

Note Associated with Oil Temp High - On Ground

A

Increasing engine NG above IDLE setting may reduce oil temperature by increasing the airflow through the oil cooler.

35
Q

Caution x3 Associated with Metal Particles detected in gearbox

A
  1. Minimise power changes with CHIP indicated.
  2. Monitor the engine for signs of mechnical failure.
  3. Shut down the engine as soon as possible after landing.
36
Q

Caution Associated with Uncommanded power changes

A

Observe engine limitations manually and avoid rapid power changes with the PMS in manual mode

37
Q

Note Associated with Uncommanded power changes

A

The maximum permitted torque is 2850 ft-lb (67.5%) with the PMS in manual mode.

38
Q

General Oxygen System Warning

A

Monitor EO2 contents and descend to safe altitude before EO2 is exhausted

39
Q

General Oxygen System Note x 2

A
  1. Control rate and depth of breathing when using EO2 to maximise during and avoid hyperventilating when using 100% oxygen
  2. Monitor the MFD ECS page cockpit pressuration status with OBOGS inoperative.
40
Q

Note Associated with OXYGEN OFF (BOTH COCKPITS)

A

Consider aircraft fuel state, fuel required to reach a landing aerodrome, and EO2 remaining.

41
Q

Note x 2 Associated with OBOGS Failure

A
  1. OBOGS excessive pressure supply to the pilot mask may occur without any DWP or MFD alerts. Perform the OBOGS FAILURE checks if excessive pressure is making it difficult to breathe.
  2. Consider aircraft fuel state, fuel required to reach a landing aerodrome, and EO2 remaining.
42
Q

Note Associated with OXYGEN PRESSURE OR OXYGEN CONCENTRATION LOW

A

Consider aircraft fuel state, fuel required to reach a landing aerodrome, and EO2 remaining.

43
Q

Note x 3 Associated with OXY FLOW WARNING

A
  1. Check the flow indicators to identify the affected cockpit
  2. EO2 activation will isolate OBOGS oxygen flow in the affected cockpit, causing an OXY FLOW warning until the EO2 is depleted or reset.
  3. Consider aircraft fuel state, fuel required to reach a landing aerodrome, and EO2 remaining.
44
Q

Caution Associated with FUEL PRESSURE LOW

A

Operating below 0°C OAT without fuel icing
inhibitor may cause filter blockage due to ice
formation.

45
Q

Note X 2 associated with FUEL PRESSURE LOW

A
  1. Change altitude to find warmer OAT if possible.

2. Ensure positive g.

46
Q

Caution Associated with TRIM RUNAWAY

A
  1. Selecting TRIM/AIL PWR off de-energises
    the electric trim systems, and the hydraulic
    aileron servo, roll spoilers and normal
    powered braking systems are inoperative.
  2. Aileron force increases and roll rate
    decreases
3. Normal powered braking is not available
with TRIM/AIL PWR off:
- Manual braking requires higher than
normal brake pedal pressure and
travel for efficient braking
- Landing ground roll distance is 8%
longer with manual braking
- Pull the emergency landing gear
handle if emergency powered
braking is required
  1. Anti-skid is inoperative with TRIM/AIL
    PWR off. Apply brakes carefully with
    anti-skid inoperative.
  2. Flight control trims are inoperative
47
Q

Note x 2 Associated with TRIM RUNAWAY

A
  1. To avoid leg fatigue, the aircraft may be
    flown with the slip indicator not centred.
    High sideslip angles are acceptable at and
    below 220 KIAS.
  2. The fuel quantity indications can be
    unreliable when the slip indicator is not
    centred for a prolonged period:
    • Restore centred slip indicator to obtain
    the correct fuel quantity indications
    • A reset of the fuel low level indication
    can take up to 2 minutes
48
Q

Caution Associated with AILERON CONTROL SYSTEM MALFUNCTION

A 
Selecting TRIM/AIL PWR off de-energises
the electric trim systems, and the hydraulic
aileron servo, roll spoilers and normal
powered braking systems are inoperative:
• Aileron force increases and roll rate
decreases
• Normal powered braking is not available
with TRIM/AIL PWR off:
- Manual braking requires higher than
normal brake pedal pressure and
travel for efficient braking
- Landing ground roll distance is 8%
longer with manual braking
- Pull the emergency landing gear
handle if emergency powered
braking is required
• Anti-skid is inoperative with TRIM/AIL
PWR off. Apply brakes carefully with
anti-skid inoperative.
• Flight control trims are inoperative
49
Q

Caution Associated with Flap Failure

A

Observe flaps extended airspeed and g limitations if flaps cannot be confirmed up.

50
Q

Note x 2 Associated with FLAP FAILURE

A
  1. Consider aircraft fuel state and fuel required to reach a suitable landing aerodrome.
  2. Use flapless approach and landing speed
    (E-12) or AOA indexer for approach and
    landing if flaps are not at LDG position.
51
Q

Note x 4 Associated with Gear Retraction Failure

A
  1. Do not recycle the landing gear.
  2. Landing gear cannot be retracted following emergency landing gear extension.
  3. Do not check brakes after emergency landing gear extension in order to preserve emergency hydraulic pressure for flaps extension and emergency powered breaking after landing.
  4. Emergency powered braking may be limited after landing.
52
Q

Caution Associated with GEAR RETRACTION FAILURE

A

Anti-skid is inoperative when the main
hydraulic system is not operating following
emergency landing gear extension. Apply
brakes carefully with anti-skid inoperative.

53
Q

Caution Associated with GEAR LOWERING FAILURE

A

Anti-skid is inoperative when the main
hydraulic system is not operating following
emergency landing gear extension. Apply
brakes carefully with anti-skid inoperative.

54
Q

Note x 3 Associated with GEAR LOWERING FAILURE

A
  1. Landing gear cannot be retracted following emergency landing gear extension.
  2. Do not check brakes after emergency landing gear extension in order to preserve emergency hydraulic pressure for flaps extension and emergency powered breaking after landing.
  3. Emergency powered braking may be limited after landing.
  4. Do not recycle the landing gear
  5. Attempt to extend the landing gear while applying positive g, varying between zero and +2g

2FTS Basic Knowledge (3 decks)

Brainscape helps you reach your goals faster, through stronger study habits.
© 2024 Bold Learning Solutions. Terms and Conditions