15.1.6 Airplane Limits and Specifications Flashcards

1
Q
  1. You are ready to taxi in N741CK. What is the maximum the aircraft can weigh?
A

(AOM Vol I, Ch L)

• 873,000

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2
Q
  1. You are in N745CK and have just received your weight and balance form. The zero fuel weight shows 612,754. Is any action required?
A

(AOM Vol I, Ch L)

• You must remove enough payload to return the ZFW within limits.

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3
Q
  1. You are in Europe. It is a grey and rainy day. Your intended landing runway is not shown as grooved on the 10-9A airport chart. Braking action is reported as a “.30” on a Tapley report. What is your maximum recommended crosswind component?
A

(AOM Vol I, Ch L) (QRH, Ch AP)

• 20 knots

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4
Q
  1. You are conducting a Category III approach. The approach chart indicates a threshold crossing height of 39 feet. What is the significance?
A

(AOM Vol I, Ch L)

• The minimum autoland threshold crossing height is 40 feet

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5
Q
  1. You are conducting an RNAV approach, using VNAV as the pitch mode. When must the autopilot be isconnected?
A

(AOM Vol I, Ch L)

• 50 feet below MDA

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6
Q
  1. What is the maximum permitted depth of dry snow for takeoff? For landing?
A

(AOM Vol I, Ch L)
• Takeoff – 2.4 inches
• Landing – 4.0 inches

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7
Q
  1. You are in Amsterdam on a grey and rainy day. The runway is wet and the breaking action has been reported as “4”. What is the maximum crosswind component for landing?
A

(AOM Vol I, Ch L)

• 30 knots

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8
Q
  1. You are conducting an ILS approach to a runway with a prevailing visibility of ¾ nautical miles. Is the flight director required to be on?
A

(AOM Vol I, Ch L)

• No

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9
Q
  1. What must a person do to enter the main deck in flight?
A

(AOM Vol I, Ch L)

• He or she must carry a portable oxygen bottle to enter the main deck in flight.

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10
Q
  1. You are conducting a flight with a payload that requires ballast fuel to bring the zero fuel weight CG within limits. What is the maximum amount of required fuel that can be shown on the flight release?
A

(AOM Vol I, Ch L) (AOM Vol II, Ch 12)

• Approximately 244,000 pounds (244,416 @ 6.7 lb.gal)

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