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.

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.

25
NG and MAX In flight, do not use speed brakes with greater than flaps ______.
Flaps 10
26
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.
320 knots | 143,000 lbs
27
Max Fuel Tank Temperature
+ 49°C
28
Min Fuel Tank Temperature
-37°C
29
Jet A Fuel freeze point is _____.
-40°C
30
Fuel Distribution Main tanks must be full if the center tank quantity is greater than ______
1,000 lbs Note 7- *Some MEL items can override this limitation
31
Fuel Distribution Note 5 ________ pounds may be retained in the center Tank provided the effects of balance have been considered.
1,000 lbs
32
Fuel Distribution Note 6 Center Tank fuel pumps must be _____ for takeoff with more than _______ pounds of fuel in the center Tank.
ON | 1,000 pounds
33
Corresponding center tank fuel pump must be switched to _____ when a center tank LOW PRESSURE light illuminates.
OFF
34
Max Range (NG)
~3000 NM
35
Normal Cruise Speed Mach
.785 Mach
36
Max Certified Mach
.82 Mach
37
Max Takeoff weight 700NG
154,500 lbs
38
Max Landing Weight 700NG
128,000 lbs
39
Max Takeoff and Landing Altitude
8,400 feet MSL
40
Max Taxi weight NG
155,000 lbs
41
Max zero fuel weight
120,500 lbs
42
Wing Tank Fuel Capacity | 737-700 NG
8,630 lbs
43
Center Fuel Tank Capacity | 737-700 NG
28,803 lbs
44
Total Aircraft Fuel Capacity 737-700 NG
46,063 lbs
45
Wing Span 737-700 NG
117 FT 5 IN
46
Aircraft Length 737-700 NG
110 FT 4 IN