STANDS Eval Flight Flashcards

1
Q

Stuck Droops

A

1- Shut sown one Engine to reduce %RPM R

2- If droops are still not in, accelerate rotor to 75% RPM R.

3- ENG PCL to IDLE and displace cyclic to attempt to dislodge droop.

4- If droop is still not in, clear area of personnel and shut down engine with cyclic in normal position.

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2
Q

Establish Single Engine Airspeed Definition

A

Maneuvering the aircraft to an appropriate airspeed that will allow continued flight under partial power conditions to a suitable landing area.

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3
Q

Establish Single Engine Airspeed EP

A
  1. Cyclic- Adjust as required
  2. Collective- Adjust as required to maintain % RPM R within normal operating range.
  3. Establish appropriate airspeed.
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4
Q

Lockout Definition

A

Manual control of Engine RPM while bypassing DEC functions.

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5
Q

Lockout EP

A
  1. ENG PCL- Pull down and advance full forward while maintaining downward pressure, then adjust to set % RPM R as required. (10% below other Engine.)
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6
Q

Single Engine Failure EP

A
  1. Establish Single Engine Airspeed
  2. External cargo/stores- Jettison (if required)

If continued flight IS NOT possible:

  1. Land As Soon As Possible

If continued flight IS possible:

  1. Land as Soon as Practicable.
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7
Q

1 Tail Rotor Servo Caution Appears with NO backup pump OR #2 Tail RTR Servo On does not appear.

A
  1. Tail Servo Switch- Backup
  2. Backup Hydraulic Pump Switch- ON
  3. Land as Soon as Practicable

Because of the limited yaw control range avail-able, a roll-on landing at approximately 40KIAS is required.

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8
Q

1 or #2 Hydraulic Pump Caution Appears WITHOUT Backup Pump ON Advisory does not appear.

A
  1. Airspeed- Adjust to a comfortable airspeed.
  2. BACKUP HYD PUMP switch- ON

If Backup Pump ON advisory does appear:
Refer to #1 or #2 HYD PUMP Caution Appears EP.

If Backup PUMP ON advisory does not appear:

  1. FPS and BOOST switches: OFF (For #2 HYD PUMP Caution.)
  2. Land as Soon as Possible
    (Turn off FPS and BOOST in case they come back on erratically. May cause loss of aircraft control.)
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9
Q

Stabilator Malfunction- Auto Mode Failure

A
  1. Cyclic Mounted Stabilator Slew Up switch- Adjust as required
  2. Auto Control Reset- Press ON once, after establishing a comfortable airspeed.
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10
Q

Slope Operation Prior Discussion

A
  1. Parking Brake Set
  2. Dynamic Rollover (Pivot Point, Rolling Motion, Exceeding the Critical Angle)
  3. Droop Stop Pounding
  4. Wind Speed and Direction
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11
Q

Autorotation Steady State Factors

A
  1. RPM R within limits.
  2. Airspeed not below 80 KIAS
  3. Torque, Trim, and aircraft in a position to land at desired touchdown point.
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12
Q

Unusual Attitude Recovery Procedures

A
  1. Attitude- Level the wings on the attitude indicator.
  2. Heading- Maintain heading; turn only to avoid known obstacles.
  3. Torque- Adjust torque as necessary.
  4. Trim- Trim aircraft as necessary.
  5. Airspeed- Adjust Airspeed as necessary.
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