TD 13 Flashcards

1
Q

To properly maintain airspace surveillance the PC will brief airspace surveillance procedures ______ to flight and assign ______. The crew will announce ______ or ______ changes, ______ the aircraft, and immediately inform other crew members of all _______ or ______ that pose a threat to the aircraft and announce when attention is focused _______ the aircraft and when attention is focused back _______.

A

prior, responsibilities, drift, attitude, clear, traffic, obstacles, inside, outside

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2
Q

The main purpose of the hover power check is to determine whether the aircraft is _____ of completing the assigned mission and ensure that aircraft _____ will not be exceeded. The ______ will be focused outside the aircraft during the hover power check using _____ foot stationary hover the direction of _____, preferably into the wind. _____ will compare the ______ hover TQ to the _____ hover TQ on the PPC and announce the results to the ______.

A

capable, limitations, pilot on the controls, 3, takeoff, pilot, actual, predicted, pilot on the controls

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3
Q

Initiate an in-flight fuel consumption check within ______ after leveling off or within ______ of entering into mission profile. Compute the fuel consumption rate _______ and complete the fuel check within ______ after taking the initial readings. Fuel quantities should be checked with the aircraft in a ______.

A

10 mins, 10 mins, +- 50 lbs, 15-30 mins, level attitude

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4
Q

White Line Limits

A

TOT Starting Range

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5
Q

Yellow Line

A

AEO takeoff power range
FLI: 8.5-10
Time Limited: 5 mins
% TRQ: 71-88%

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6
Q

Red Line

A

AEO Max Takeoff Power
FLI: 10
Time Limited: 12 cont. sec
%TQ: 2x88%

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7
Q

Yellow Broken Line

A

OEI Max Continuous power
FLI: 11
%TQ: 91.5%

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8
Q

Red Broken Line

A

OEI 2.5 min power
FLI: 12
Time Limited: 2.5 continuous min
%TQ: 125%

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9
Q

Red Full Circle

A

AEO Transient
FLI: 10.5
Time Limited: Max 12 seconds
%TQ: 2x97%

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10
Q

Red Broken Circle

A

OEI transient max
FLI: 14
Time Limited: Max 12 seconds
%TQ: 107.5%

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11
Q

Hover Turns
For gross mass up to 3200kg…..
Maximum _____ •/s ( _____ seconds for a 360• turn)

A

45, 8

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12
Q

Hover Turns
For gross mass above 3200kg….
maximum ____•/s ( ____ seconds for a 360• turn)

A

30, 12

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13
Q

MASTER caution light

The master caution light ____ comes on in conjunction with ____ caution indication on the CAD

A

Always, any

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14
Q

Master Caution Light

Procedure:

  1. Caution Indication (CAD):_________
  2. RESET switch (cyclic stick) ______
A

Check and perform corresponding procedure(s)

Press

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15
Q

CAUTION INDICATION - ENG CHIP
(SYSTEM 1 or 2)

ON GROUND

  1. Affected engine —
  2. Single engine emergency shutdown —

IN FLIGHT

  1. OEI flight condition —
  2. Affected engine —
  3. Alternative:
  4. Single engine emergency shutdown—
  5. Alternative
  6. Twist grip (affected engine) —

CAUTION THE SECOND ALTERNATIVE ENABLES THE CREW TO USE THE AFFECTED ENGINE FOR LANDING IF NECESSARY. BE PREPARED FOR ENGINE FAILURE…..
4. LAND AS SOON AS ________

A

ON GROUND

  1. Affected engine — Identify
  2. Single engine emergency shutdown — Perform

IN FLIGHT

  1. OEI flight condition — Establish
  2. Affected engine — Identify
  3. Alternative:
  4. Single engine emergency shutdown— Perform
  5. Alternative
  6. Twist grip (affected engine) — Rotate slowly to IDLE, check indications
  7. LAND AS SOON AS PRACTICABLE
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16
Q

Dynamic rollover can occur on _______ as well as during a _______ or ________ ________ and ______

A

Level ground, slope, crosswind, landing, takeoff

17
Q

What are the conditions required for Dynamic Rollover to occur?

A
  1. Pivot point
  2. Rolling Motion
  3. Exceed Critical Angle
18
Q
Human factors considered in the prevention of dynamic rollover include:
1.
2.
3.
4.
5.
A
  1. Inattention
  2. Inexperience
  3. Failure to take timely corrective action
  4. Inappropriate control point
  5. Loss of visual reference
19
Q

Red unfilled Triangle

A

Max TOT Starting
FLI: 8.5
TOT: 785 degrees

20
Q

Red filled triangle

A

TOT Starting Transient
FLI: 11
Time Limited: 5 secs
TOT: 865 degrees