Operating Limitations

Question 1

Runway Slope

Answer 1

+1.7% to -2.0%

Question 2

Maximum Operating Altitude

Answer 2

37,000 feet

Question 3

Maximum Takeoff and Landing Pressure Altitude

Answer 3

8,500 feet

Question 4

Maximum Takeoff and Landing Tailwind Component

Answer 4

10 knots, or as permitted by Company Pages

Question 5

Maneuvering Limit Load Factors

-Flaps/Slats retracted

Answer 5

+2.5g to -1.0g

Question 6

Maneuvering Limit Load Factors

-Flaps/Slats extended

Answer 6

+2.0g to 0.0g

Question 7

Wing landing light motors should be allowed to cool for

Answer 7

1 1/2 minutes after initial extension or retraction and 3 1/2 minutes after each subsequent extension or retraction.

Question 8

Lamps should not be operated in still air for

Answer 8

over 10 minutes

Question 9

Crosswind limit

Answer 9

38 knots for takeoff or landing, including gusts

Question 10

Severe turbulence air penetration speed

Answer 10

275KIAS/.75M

Question 11

Maximum Taxi Weight (MTW)

Answer 11

122,000#s

Question 12

Maximum Take Off Weight (MTOW)

Answer 12

121,000#s

Question 13

Maximum Landing Weight (MLW)

Answer 13

110,000#s

Question 14

Maximum Zero Fuel Weight (MZFW)

Answer 14

100,500#s

Question 15

Maximum cabin differential pressure is

Answer 15

7.86 psi

Question 16

Maximum emergency relief pressure is

Answer 16

8.27 psi

Question 17

For takeoff, the FLOW switch on the overhead panel must be in _____

Answer 17

NORM

Question 18

Do not exceed _______ KIAS below _______ feet when windshield heat is inoperative on any windshield.

Answer 18

315 KIAS; 10,000 feet

Question 19

Cracked captain, center, or first officer’s windshield operating limits below 10,000 feet:
Outer glass:
Inner glass:

Answer 19

Outer glass: 315 KIAS; Inner glass: 235 KIAS

Question 20

Wing Ice:

Do not take off with “_________” alert displayed

Answer 20

WING ICE DETECTED

Question 21

During takeoff, do not engage the _______ below ____ feet AGL

Answer 21

autopilot; 200’

Question 22

Do not conduct an auto coupled (ILS or autoland) approach if ________ alert illuminates for longer than ___ seconds after airplane is stabilized and tracking glideslope.

Answer 22

STAB OUT OF TRIM; 3 sec

Question 23

For non-ILS approaches, the autopilot must be disengaged no lower than the applicable minimums minus ___ feet.

Answer 23

50

Question 24

Maximum allowable wind component for autoland operations:
Headwind:
Crosswind:
Tailwind:

Answer 24

25, 15, 10

Question 25

Do not conduct autoland operations if:

Answer 25

* ALIGN mode is not annunciated on an FMA by 100 feet radio altitude. * Any unusual control position or other abnormal conditions exist in the flight control system. * RUDDER PWR OFF alert is displayed. * Airport field elevation exceeds 8,000 feet MSL. * Runway width is less than 145 feet

Question 26

Engine Starter Duty Cycle: _____ start attempts, with a minimum of ___ seconds between attempts. Maximum duration of each attempt is __ minutes. Allow __ minutes cooling time before further start attempts are made.

Answer 26

Three; 15 seconds; 3; 15 minutes

Question 27

Reduced thrust takeoffs are not authorized on runways contaminated with _____, _____, _____, _____, or _____.

Answer 27

standing water, loose snow, slush, compacted snow or wet ice.

Question 28

APU AIR switch must be _____ for takeoff and in flight operations

Answer 28

OFF

Question 29

APU starter motor duty cycle is limited to _____ consecutive start attempts. Wait ____ minutes prior to further start attempts.

Answer 29

three; 30

Question 30

Speedbrakes may not be used with flaps extended beyond

Answer 30

20°

Question 31

On the ground, the standby altimeter must be within +/- ____ feet of the Captain’s and First Officer’s altimeters

Answer 31

75

Question 32

The maximum allowable on the ground altimeter reading differences at a known field elevation for RVSM operations are:

Answer 32

Captain & F/O: 60' Captain or F/O & Field Elevation: 75' Captain and F/O (In Flight): 200'

Question 33

Do not operate the weather radar in a hangar or within ___ feet of any personnel or a fuel spill.

Answer 33

50'

Question 34

After takeoff, _____ fuel shall be emptied prior to using _____ fuel.

Answer 34

center tank; main tank

Question 35

Maximum permissible fuel imbalance is:

Answer 35

1500#'s

Question 36

The maximum fuel temperature is ___ for types: Jet A, Jet A1, JP-5, JP-8.

Answer 36

54°C

Question 37

The minimum fuel temperature is either the higher of the fuel freeze point, or the engine limits, as follows:

Answer 37

* -42°C for takeoff, climb, and go-around | * -48°C for flight above 15,000 feet

Question 38

Prior to engine start on any flight where _____ tank fuel is present and will be needed for that route segment, the _____ tank fuel pumps must be individually checked to verify pump operation.

Answer 38

center; center

Question 39

Do not reset any tripped _____ circuit breakers.

Answer 39

fuel pump

Question 40

Maximum landing gear retraction speed is:

Answer 40

250 KIAS

Question 41

Maximum landing gear extension speed is:

Answer 41

300 KIAS / 0.70M

Question 42

The certified maximum tire speed rating is:

Answer 42

195 knots

Question 43

Weather radar must be on for takeoff for _____ to be operable

Answer 43

predictive windshear