SY210/211 Canopy System & Ejection System Flashcards

0
Q

The oil-filled struts bear the weight of the canopy and enable a single operator to move the entire assembly using about ____ pounds of force.

A

30

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1
Q

The Windscreen and Front Cockpit Transparency have been designed to withstand a ___-pound birdstrike at up to ____ KIAS

A

4 pound, up to 270 KIAS

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2
Q

What are the two sealing systems on the canopy?

A

Non-inflatable weather seal

Inflatable pressure seal

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3
Q

Which switch must be in the NORM or HI position for the canopy seal to operate?

A

BLEED AIR INFLOW

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4
Q

The canopy’s latch mechanism drives ____ over centering hooks through a continuous rod.

A

5

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5
Q

How can a pilot determine the canopy has been properly latched closed?

A

The mechanical green indicator is visible

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6
Q

What are the major systems of the T-6 canopy? (4)

A

Locking/latching, sealing, defog, fracturing

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7
Q

What two conditions are required for the pressurization seal to operate?

A

Bleed air inflow must be available

Weight must be off the right main landing gear

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8
Q

Each Martin-Baker ejection seat is fully automatic, designed to provide rapid escapee from ___ altitude and ___ airspeed, up to ________ feet and ____ KIAS

A

0, 0

35,000 feet, 370 KIAS

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9
Q

The MOR handle is used to manually initiate seat/pilot separation under what 2 circumstances?

A

Automatic System Failure

If seat/pilot separation is desired above 14,000 feet MSL, and should be used over mountainous terrain above 8,000 MSL

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10
Q

What is the purpose of the leg restraint system?

A

Prevent the feet from flailing during ejection.

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11
Q

The emergency oxygen cylinder is considered adequately charged if the pointer is anywhere in the black band (____-____ psi)

A

1800-2500 psi

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12
Q

The emergency oxygen cylinder will supply oxygen for approximately ____ minutes

A

10 minutes

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13
Q

If the ISS mode selector is set to BOTH, there is a _____ second delay after the rear seat ejects before front seat ejection.

A

0.37 seconds

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14
Q

When set to AUTO, the SSK is lowered automatically on a 12 foot line, ____ seconds after seat/pilot separation.

A

4 seconds

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15
Q

During the ejection process, movement of the seat is first initiated by _______________.

A

Detonated gas pressure

16
Q

What are 3 factors that affect the performance of the ejection system during an ejection sequence?

A

Dive Angle
Bank Angle
Sink Rate

17
Q

What are two types of ejections?

A

Controlled Ejection

Uncontrolled Ejection

18
Q

What is the recommended minimum altitude for a controlled ejection?

Uncontrolled ejection?

A

2000 AGL

6000 AGL

19
Q

Below 14,000 feet, the entire ejection process takes _____ seconds front/ _____ seconds rear from the pilot pulls the handle to the point the chute is fully deployed.

A
  1. 37 sec front

4. 00 sec rear

20
Q

During higher altitude ejections, the head box deployment, drogue chute release, seat separation, and parachute deployment are all delayed until below _______ to _______ feet MSL

A

14,000 to 16,000 feet