Checked Limitations Flashcards

1
Q

Circle to land minimums

A

1000 foot ceiling and 3 miles visibility, unless stated higher on the approach plate.

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2
Q

Circle to land minimum descent altitude

A

1000 AFE feet unless restricted to higher altitude in the circle to land minimums.

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3
Q

Max operating Altitude

A

41,000 feet

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4
Q

With engine bleed air switches ON, do not operate the air conditioning packs on HIGH for:

A

Takeoff, approach or landing unless otherwise directed by the QRH

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5
Q

Holding in icing conditions with flaps extended is…

A

Prohibited

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6
Q

MAX - Do not operate wing anti-ice on the ground when OAT is above…

A

10 C or 50 F

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7
Q

MAX - do not use wing anti-ice as a substitute for:

A

Ground de-icing/anti-icing and inspection procedures required to comply with operating rules.

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8
Q

Do not operate weather radar during:

A

Fueling, near fuel spills, or near people.

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9
Q

Electrical Power

On the ground, limit one generator operation (engine driven) to a maximum of:

A

215 AMPS

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10
Q

Do not remove AC power from aircraft for at least _____ seconds for IRS shutdown.

A

30 Seconds

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11
Q

Max EGT ground start (NG)

A

725 C

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12
Q

After Engine start roll back, delay takeoff power for ____ minutes (NG), and ______ minutes for (MAX)

A

2 minutes NG

3 minutes MAX

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13
Q

Operate engines at or near idle for ____ minutes NG and ____ minutes MAX before shutdown.

A

1 minute NG

3 minutes MAX

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14
Q

Reverse Thrust is limited to:

A

Ground use only

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15
Q

APU

Max Altitude for operation

A

41,000 feet

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16
Q

APU

Max Altitude for Electric Only

A

41,000 feet

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17
Q

APU

Max Altitude Bleed Air Only

A

17,000 feet

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18
Q

APU

Max Altitude Bleed and Electric

A

10,000 feet

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19
Q

Do not extend flaps above ________ feet pressure Altitude.

A

20,000 feet

20
Q

Alternate flap duty cycle in flight is one complete cycle, then _____ minutes off.

A

5 minutes

21
Q

A complete Alternate flap cycle is movement from _____ to _____ and back to _____.

A

0° to 15° and back to 0°.

22
Q

ALTERNATE FLAP position switch must be in the OFF position for ____ seconds before reversing the direction of the flap movement.

A

15 seconds

23
Q

In flight, do not extend the speedbrake lever beyond the _____ ________.

A

FLIGHT DETENT

24
Q

Do not use speed brakes in flight below ____________ AGL.

A

1,000 AGL

25
Q

NG and MAX

In flight, do not use speed brakes with greater than flaps ______.

A

Flaps 10

26
Q

7W

Do not operate the aircraft at speeds in excess of _____ knots at weights over __________ lbs if the speed brake wing load alleviation system is inoperative.

A

320 knots

143,000 lbs

27
Q

Max Fuel Tank Temperature

A

+ 49°C

28
Q

Min Fuel Tank Temperature

A

-37°C

29
Q

Jet A Fuel freeze point is _____.

A

-40°C

30
Q

Fuel Distribution

Main tanks must be full if the center tank quantity is greater than ______

A

1,000 lbs

Note 7-
*Some MEL items can override this limitation

31
Q

Fuel Distribution
Note 5

________ pounds may be retained in the center Tank provided the effects of balance have been considered.

A

1,000 lbs

32
Q

Fuel Distribution
Note 6

Center Tank fuel pumps must be _____ for takeoff with more than _______ pounds of fuel in the center Tank.

A

ON

1,000 pounds

33
Q

Corresponding center tank fuel pump must be switched to _____ when a center tank LOW PRESSURE light illuminates.

A

OFF

34
Q

Max Range (NG)

A

~3000 NM

35
Q

Normal Cruise Speed Mach

A

.785 Mach

36
Q

Max Certified Mach

A

.82 Mach

37
Q

Max Takeoff weight 700NG

A

154,500 lbs

38
Q

Max Landing Weight 700NG

A

128,000 lbs

39
Q

Max Takeoff and Landing Altitude

A

8,400 feet MSL

40
Q

Max Taxi weight NG

A

155,000 lbs

41
Q

Max zero fuel weight

A

120,500 lbs

42
Q

Wing Tank Fuel Capacity

737-700 NG

A

8,630 lbs

43
Q

Center Fuel Tank Capacity

737-700 NG

A

28,803 lbs

44
Q

Total Aircraft Fuel Capacity 737-700 NG

A

46,063 lbs

45
Q

Wing Span 737-700 NG

A

117 FT 5 IN

46
Q

Aircraft Length 737-700 NG

A

110 FT 4 IN