DQ30

Question 1

1. Concerning TASK 1102 Perform Manual Throttle Operation - Emergency Mode:
   a. Maximum FLI deviation is ________
   b. WARNING: It is critical to ensure that when the number ______ thottle is placed into the emergency (EMER) area, that the __________ does not fall into position __________.
   c. After landing the _______ will rotate the _______ (affected engine) to _______ prior to reducing the collective lever to the full down position.
   d. During training of this task, any movement of ______ switch will be ________ when completing appropriate emergency procedures steps.

Answer 1

1. Concerning TASK 1102 Perform Manual Throttle Operation - Emergency Mode:
   a. Maximum FLI deviation is +1/-2
   b. WARNING: It is critical to ensure that when the number 2 thottle is placed into the emergency (EMER) area, that the limiting stop does not fall into position inadvertently.
   c. After landing the P* will rotate the twist grip (affected engine) to idle prior to reducing the collective lever to the full down position.
   d. During training of this task, any movement of N2 switch will be simulated when completing appropriate emergency procedures steps.

Question 2

ENGINE OVERSPEED - GOVERNOR FAILURE

Procedure:

1. Collective lever - _________

2. VAR NR system NORM/MAN sw - ___________

3. N2 TRIM sw - ___________

If step 3 is not possible:

4. Affected engine - __________

5. Twist grip (affected engine) - __________

6. LAND AS SOON AS __________

Answer 2

ENGINE OVERSPEED - GOVERNOR FAILURE

Procedure:

1. Collective lever - Raise as necessary to maintain N2 and NRO within limits

2. VAR NR system NORM/MAN sw - Check MAN

3. N2 TRIM sw - Try to trim NRO to 101% with matched torque

If step 3 is not possible:

4. Affected engine - Identify

5. Twist grip (affected engine) - Rotate towards IDLE until N2 and NRO stabilize in normal range and FLI needles match

6. LAND AS SOON AS PRACTICABLE

Question 3

ENGINE UNDERSPEED - GOVERNOR FAILURE

Procedure:

1. OEI flight condition - _________

2. Bleed air consumers - ________

3. VAR NR system NORM/MAN pb - _________

4. Affected engine - ___________

5. N2 TRIM sw - ___________

If torque match is not possible:

6 Twist grip (affected engine) - __________

7. LAND AS SOON AS __________

If no residual torque (affected engine is available

8. Single engine emergency shutdown - ________

Answer 3

ENGINE UNDERSPEED - GOVERNOR FAILURE

Procedure:

1. OEI flight condition - Establish

2. Bleed air consumers - OFF

3. VAR NR system NORM/MAN pb - Check MAN

4. Affected engine - Identify

5. N2 TRIM sw - Compensate N2/NRO drop and try to match torque

If torque match is not possible:

6 Twist grip (affected engine) - Release stop plate and rotate towards FLIGHT until N2 and NRO stabilize in normal range and FLI needles match

7. LAND AS SOON AS PRACTICABLE

If no residual torque (affected engine is available

8. Single engine emergency shutdown - Perform

Question 4

During a practice autorotation, before reaching _____ feet AGL, ensure that a steady - state autorotation is attained. If it is not, _______ the maneuver or execute a ________. A steady-state autorotation means that-

a.

b.

c.

d.

Answer 4

During a practice autorotation, before reaching 200 feet AGL, ensure that a steady - state autorotation is attained. If it is not, abort the maneuver or execute a go-around. A steady-state autorotation means that-

a. Rotor RPM is within limits
b. Aircraft is at the correct airspeed
c. Aircraft in trim
d. Aircraft is in a position to terminate at the intended landing area

Question 5

WARNING LIGHT INDICATIONS —- ROTOR RPM

Conditions/Indications

NRO low

• NRO ______ or less - ___________
• Audio signal - __________

NRO high

• NRO ______ or above - ____________
• Audio signal at ________ or above - ___________

Answer 5

WARNING LIGHT INDICATIONS —- ROTOR RPM

Conditions/Indications

NRO low

• NRO 95% or less - Steady light
• Audio signal - Low pitch beeping tone

NRO high

• NRO 106% or above - Flashing light and warning gong
• Audio signal at 110% or above - Flashing light and steady high pitch tone

Question 6

Autorotation

Procedure

1._______________

2.______________

NOTE Maximum range airspeed ……. _______ KIAS

minimum rate of descent airspeed …._______ KIAS

3.________________

AT APPROXIMATELY ________ FT AGL:

4. Flare attitude - Establish (approx.____ to ____) to reduce forward speed and rate of descent; control NRO

AT APPROXIMATELY ____ to ____ FT AGL: (Note: ____ in ATM)

5. Flare attitude - Reduce to approx ______
6. Heading - Maintain
7. Collective lever - _________

8. _________

NOTE The appropriate values must be adjusted according to prevailing conditions of gross mass, wind and terrain.

Answer 6

Autorotation

Procedure

1. Collective lever - Reduce to maintain NRO within limits

2. Airspeed - 75 KIAS recommended

NOTE Maximum range airspeed ……. 90 KIAS

minimum rate of descent airspeed ….. 60KIAS

3. Dual engine emergency shutdown - Perform

AT APPROXIMATELY 100 FT AGL:

4. Flare attitude - Establish (approx 15 to 20) to reduce forward speed and rate of descent; control NRO

AT APPROXIMATELY 8 to 12 FT AGL: (Note: 10-15 in ATM)

5. Flare attitude - Reduce to approx 7
6. Heading - Maintain
7. Collective lever - Raise to stop descent and cushion landing

8. BAT MSTR sw - OFF

NOTE The appropriate values must be adjusted according to prevailing conditions of gross mass, wind and terrain.