Systems - Windows and Doors Flashcards

1
Q

Flight deck door description

A

*Penetration resistant door.
*Locked by 3 electronic locking strikes.
*Keypad in cabin, code required to request entry, pilots then use cockpit door panel to allow or deny.
*If denied, won’t buzz again for 15 minutes (switching to unlock shortly with revert to normal)
*If ignored, door will unlock for 5 seconds after 45 seconds
*buzzing for more than 45 seconds means emergency code has been entered
*flap for escape from cockpit side only
*manual d handle for flight crew to unlock
*unlocks if power is locked, or rapid de pressurisation

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2
Q

Cabin doors

A

4
1L, 1R
2L, 2R

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3
Q

Cockpit widow features

A

Handle to unlock, uncovers a locking pin in the slide - this must be flipped before closing, can only be opened from the inside

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4
Q

With the aircraft on the ground and shut down, a red light on an exit door indicates?

A

The slide is disarmed, and a cabin pressurisation differential exists

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5
Q

An amber door indication on the DOOR/OXY page means?

A

The door is open

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6
Q

An amber EMER EXIT indication on the DOOR/OXY page means?

A

The emergency exit handle is not in its position OR the emergency exit has been opened and the slide has been deployed

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7
Q

Maximum speed the cockpit windows can be opened?

A

200kt

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8
Q

Maximum wind for:
Passenger door operation?
FWD and AFT cargo doors?

A

Pax doors - 65dkt

Cargo doors - 40k
(unless AC nose into wind, or doors on leeward side then 50kt) doors must be closed before wind reaches 65kt

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9
Q

Is it possible to open the Cockpit sliding windows from outside?

A

No

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10
Q

What does the red indicator light on the inside of the cabin doors indicate when flashing?

A

The slide is disarmed and a pressurisation differential exists with the AC on the ground and the engines shut down

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11
Q

Max wind speed for a cabin door and cargo door?

A

65kt
40kt (must be closed by 65kt) - **CHECK

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12
Q

Max airspeed for opening a cockpit window?

A

200kt

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13
Q

How are you going to check cockpit windshield crack?

A

Fasten shoulder harness, touch the crack with a pen or gently with nail to determine which side of the windshield it’s on

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14
Q

What is the altitude limitation if there is no crack on Cockpit side (inner ply) in
event of windshield crack? And Why?

A

NO LIMITATION
The inner ply is not affected. Therefore, the window/windshield is still able to sustain the differential pressure up to the maximum flight level.

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15
Q

What actions are you going to take if there’s a crack on the cockpit side of the windscreen and why?

A

Oxy masks on, max alt FL230 /MEA/MORA
The inner ply is affected. The flight crew is not able to easily determine if other plies are
affected. Descend to FL 230/MEA and reduce differential pressure to 5 PSI .
Note: The maximum flight level is restricted to FL 230/MEA to obtain ΔP 5 PSI , without
resulting in an excessive cabin altitude and an EXCESS CAB ALT warning.

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