Checked Limitations Flashcards
Circle to land minimums
1000 foot ceiling and 3 miles visibility, unless stated higher on the approach plate.
Circle to land minimum descent altitude
1000 AFE feet unless restricted to higher altitude in the circle to land minimums.
Max operating Altitude
41,000 feet
With engine bleed air switches ON, do not operate the air conditioning packs on HIGH for:
Takeoff, approach or landing unless otherwise directed by the QRH
Holding in icing conditions with flaps extended is…
Prohibited
MAX - Do not operate wing anti-ice on the ground when OAT is above…
10 C or 50 F
MAX - do not use wing anti-ice as a substitute for:
Ground de-icing/anti-icing and inspection procedures required to comply with operating rules.
Do not operate weather radar during:
Fueling, near fuel spills, or near people.
Electrical Power
On the ground, limit one generator operation (engine driven) to a maximum of:
215 AMPS
Do not remove AC power from aircraft for at least _____ seconds for IRS shutdown.
30 Seconds
Max EGT ground start (NG)
725 C
After Engine start roll back, delay takeoff power for ____ minutes (NG), and ______ minutes for (MAX)
2 minutes NG
3 minutes MAX
Operate engines at or near idle for ____ minutes NG and ____ minutes MAX before shutdown.
1 minute NG
3 minutes MAX
Reverse Thrust is limited to:
Ground use only
APU
Max Altitude for operation
41,000 feet
APU
Max Altitude for Electric Only
41,000 feet
APU
Max Altitude Bleed Air Only
17,000 feet
APU
Max Altitude Bleed and Electric
10,000 feet
Do not extend flaps above ________ feet pressure Altitude.
20,000 feet
Alternate flap duty cycle in flight is one complete cycle, then _____ minutes off.
5 minutes
A complete Alternate flap cycle is movement from _____ to _____ and back to _____.
0° to 15° and back to 0°.
ALTERNATE FLAP position switch must be in the OFF position for ____ seconds before reversing the direction of the flap movement.
15 seconds
In flight, do not extend the speedbrake lever beyond the _____ ________.
FLIGHT DETENT
Do not use speed brakes in flight below ____________ AGL.
1,000 AGL
NG and MAX
In flight, do not use speed brakes with greater than flaps ______.
Flaps 10
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
Max Fuel Tank Temperature
+ 49°C
Min Fuel Tank Temperature
-37°C
Jet A Fuel freeze point is _____.
-40°C
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
Fuel Distribution
Note 5
________ pounds may be retained in the center Tank provided the effects of balance have been considered.
1,000 lbs
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
Corresponding center tank fuel pump must be switched to _____ when a center tank LOW PRESSURE light illuminates.
OFF
Max Range (NG)
~3000 NM
Normal Cruise Speed Mach
.785 Mach
Max Certified Mach
.82 Mach
Max Takeoff weight 700NG
154,500 lbs
Max Landing Weight 700NG
128,000 lbs
Max Takeoff and Landing Altitude
8,400 feet MSL
Max Taxi weight NG
155,000 lbs
Max zero fuel weight
120,500 lbs
Wing Tank Fuel Capacity
737-700 NG
8,630 lbs
Center Fuel Tank Capacity
737-700 NG
28,803 lbs
Total Aircraft Fuel Capacity 737-700 NG
46,063 lbs
Wing Span 737-700 NG
117 FT 5 IN
Aircraft Length 737-700 NG
110 FT 4 IN
