Pre Flight Flashcards

1
Q

When must the TSA access panel inspection be conducted?

A

Before the first flight of the day for that aircraft.
Before any flight departing the US to any foreign location (except Canada). Before any flight departing a foreign location to the US (except Canada). Upon arrival into the US from any foreign location (except Canada).
Reference: OM Vol. 1, Section 3, Exterior Inspection

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2
Q

Is there a requirement to open an access panel secured with a screw fastener during the aforementioned TSA inspection?

A

No, crewmembers are not required to open any panel that requires a screw driver in order to open the panel.
Reference: OM Vol.1, Section 3, Exterior Inspection

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3
Q

How can an RVSM critical area be identified?

A

RVSM critical areas may be identified by markings (four yellow corners) surrounding the areas of the fuselage adjacent to the primary static sources.
Reference: OM Vol.1, Section 3, Exterior Inspection

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4
Q

When inspecting RVSM critical areas, what conditions would preclude flight in RVSM

A

Creases, dents, deformations or bulges in the skin and/or deformations of the static sources. On the other hand, rub marks, dirt without obvious damage or deformation DO NOT preclude RVSM operations.
Reference: OM Vol.1, Section 3, Exterior Inspection

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5
Q

What requirement exists for the nose gear static discharger?

A

It must be touching the ground. Reference: OM Vol.1, Section 3, Exterior Inspection

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6
Q

How many static dischargers are found on EP/LR wings versus an XR aircraft?

A

5 static dischargers are installed on each EP/LR wing. 7 static dischargers (including winglets) are installed on each XR wing.
Reference: OM Vol.1, Section 3, Exterior Inspection

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7
Q

Can the aircraft be dispatched with missing static dischargers?

A

Yes, dispatch of an aircraft is permitted with missing static dischargers provided that they are deferred in accordance with the provisions of the CDL.
Reference: EMB-145 MEL Handbook, CDL, System 23.

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8
Q

Regarding tire wear, what is the minimum acceptable condition of an aircraft tire?

A

The tire should not be worn past the bottom of the tire grooves. Operating past the grooves will result in the loss of cut protection and penetration of the first ply will render the tire unsatisfactory for retread.
Reference: OM Vol.1, Section 3, Exterior Inspection.

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9
Q

How can brake wear be checked?

A

Brake wear can be checked by inspecting the brake wear indicators from a vantage point in front of and behind the aircraft tires. A fully worn-out brake exists when the brake wear indicator is flush with its housing. The parking brake must be set prior to checking the brake wear indicators.
Reference: OM Vol.1, Section 3, Exterior Inspection

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10
Q

If a gear uplock hook is in the locked position, what must be done?

A

Maintenance action is required. Reference OM Vol.1, Section 3, Exterior Inspection

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11
Q

When fluid is present within the nacelle drain sight glass, what else should be checked prior to notifying maintenance?

A

The six holes located around the sight glass must be inspected for presence of leaks, stains, or other evidence of fluid. If multiple indications of a leakage are present and/or the leakage appears to be excessive or consists of flammable fluids, Maintenance must be notified.
Reference: OM Vol.1, Section 3, Exterior Inspection

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12
Q

What would a missing safety disc next to the oxygen service panel indicate?

A

A missing disc indicates that the oxygen system has been over-pressurized during servicing.
Reference: OM Vol. 2, Section 2-16, Flight Crew Oxygen.

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13
Q

How many vortex generators are installed above each wing?

A

There are 12 vortex generators installed on the upper surface of each wing.
Reference: OM Vol.1, Section 3, Exterior Inspection

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14
Q

How many vortilons does each wing have?

A

There are 4 vortilons on the lower surface of each wing. Reference: OM Vol.1, Section 3, Exterior Inspection

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