Weeks 1-2 Flashcards

1
Q

Land Immediately

A

The urgency of landing is paramount. Primary considerations is to assure survival of the occupants. Landing in water, trees, or other area should be considered only as a last resort

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2
Q

Land As Soon As Possible

A

Land without delay at the nearest adequate site (i .e. open field) at which a safe approach and landing can be made

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3
Q

Land As Soon As Practicable

A

The landing site and duration of flight are at the discretion of the pilot. Extended flight beyond the nearest landing area where appropriate assistance can be expected is not recommended

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4
Q

OGE

A

Out of ground effect

Above 1 rotor diameter above the ground

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5
Q

IGE

A

In ground effect

downwash reacts with hard surface (ground)

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6
Q

A caution indication on the blank and ….

A

Two yellow master caution lights on the instrument panel indicate malfunction or failure conditions which do not require immediate crew action but the possible need for future corrective action

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7
Q

A red warning light ……

A

on the warning panel coming on together with a gong signal or dedicated audio signal indicates an emergency condition requiring immediate corrective action

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8
Q

Single Engine Emergency Action Notes

A

The Var NR system will revert to the manual mode automatically.

Before performing an in-flight single engine emergency shutdown, determine if the situation will allow for OEI flight

Make certain that:
The controls of the effected engine are selected, and the collective lever is adjusted to maintain the normal engine within the OEI limits

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9
Q

Single Engine Emergency Shutdown Procedure

A
  1. Twist grip (affected engine) - rotate slowly to idle, check indications, then to OFF
  2. Rotor speed - trim to maximum
    Bleed air heating (if installed) will be shutdown automatically, however, depending on power margin of remaining engine, may be re-engaged as follows:
  3. BLD HTG EMER/NORM SW - EMER
  4. BLD HTG Rheostat - ON
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10
Q

Double Engine Emergency Shutdown

ON GROUND

A
  1. Both twist grips - OFF
  2. Both FUEL PRIME PUMP sw - OFF
  3. BAT MSTR sw - OFF
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11
Q

Double Engine Emergency Shutdown

IN FLIGHT

A
  1. Both twist grips - OFF

If there is an indication that the engines are still running

  1. Both EMER OFF sw - Press
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12
Q

Emergency Response Method

A
F ly the aircraft
A lert the crew 
D iagnose the emergency condition
E xecute the emergency procedure
C ommunicate 
-
F ly the aircraft
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13
Q

Acceleration

A

Rate of change of velocity with respect to time

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14
Q

Inertial Force

A

An object’s resistance in a state of rest or motion

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15
Q

Back, Left, Down

A

Gx+, Gy+, Gz+

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16
Q

Speed

A

An object’s magnitude of motion and rate of change

17
Q

Velocity

A

An object’s speed in a given direction

18
Q

Autorotate

A

Adjusting the flight controls as necessary to establish an auto rotational descent and landing

19
Q

Will

A

Used only to indicate futurity, never to express or indicate a mandatory requirement

20
Q

May

A

Used to express permissiveness (an application of a procedure is optional)

21
Q

Should

A

Used to express non-mandatory permissions (an application of procedure is recommended)

22
Q

Shall and Must

A

Used to express a mandatory requirement

23
Q

Note

A

An operating procedure, technique, etc., which is essential to emphasize

24
Q

Caution

A

An operating procedure, technique, etc., which if not strictly observed, could result in damage to or description of equipment

25
Q

Warning

A

An operating procedure, technique, etc., which if not strictly observed, could result in personal injury or loss of life

26
Q

Basic Rules

A
  1. Operate the aircraft
  2. Analyze the situation
  3. Take proper action
27
Q

VNE for OEI Operation

A

110 kts or as shown in VNE-tables.

Whichever is less

28
Q

VNE for steady Autorotation

A

90 kts or as shown in VNE-tables

Whichever is first