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B717 Limitations > Operating Limitations > Flashcards

Operating Limitations Flashcards

1
Q

Runway Slope

A

+1.7% to -2.0%

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2
Q

Maximum Operating Altitude

A

37,000 feet

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3
Q

Maximum Takeoff and Landing Pressure Altitude

A

8,500 feet

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4
Q

Maximum Takeoff and Landing Tailwind Component

A

10 knots, or as permitted by Company Pages

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5
Q

Maneuvering Limit Load Factors

-Flaps/Slats retracted

A

+2.5g to -1.0g

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6
Q

Maneuvering Limit Load Factors

-Flaps/Slats extended

A

+2.0g to 0.0g

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7
Q

Wing landing light motors should be allowed to cool for

A

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

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8
Q

Lamps should not be operated in still air for

A

over 10 minutes

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9
Q

Crosswind limit

A

38 knots for takeoff or landing, including gusts

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10
Q

Severe turbulence air penetration speed

A

275KIAS/.75M

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11
Q

Maximum Taxi Weight (MTW)

A

122,000#s

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12
Q

Maximum Take Off Weight (MTOW)

A

121,000#s

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13
Q

Maximum Landing Weight (MLW)

A

110,000#s

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14
Q

Maximum Zero Fuel Weight (MZFW)

A

100,500#s

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15
Q

Maximum cabin differential pressure is

A

7.86 psi

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16
Q

Maximum emergency relief pressure is

A

8.27 psi

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17
Q

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

A

NORM

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18
Q

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

A

315 KIAS; 10,000 feet

19
Q

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

A

Outer glass: 315 KIAS; Inner glass: 235 KIAS

20
Q

Wing Ice:

Do not take off with “_________” alert displayed

A

WING ICE DETECTED

21
Q

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

A

autopilot; 200’

22
Q

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

A

STAB OUT OF TRIM; 3 sec

23
Q

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

A

50

24
Q

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

A

25, 15, 10

25
Q

Do not conduct autoland operations if:

A
  • 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
26
Q

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.

A

Three; 15 seconds; 3; 15 minutes

27
Q

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

A

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

28
Q

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

A

OFF

29
Q

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

A

three; 30

30
Q

Speedbrakes may not be used with flaps extended beyond

A

20°

31
Q

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

A

75

32
Q

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

A

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

33
Q

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

A

50’

34
Q

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

A

center tank; main tank

35
Q

Maximum permissible fuel imbalance is:

A

1500#’s

36
Q

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

A

54°C

37
Q

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

A
  • -42°C for takeoff, climb, and go-around

* -48°C for flight above 15,000 feet

38
Q

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.

A

center; center

39
Q

Do not reset any tripped _____ circuit breakers.

A

fuel pump

40
Q

Maximum landing gear retraction speed is:

A

250 KIAS

41
Q

Maximum landing gear extension speed is:

A

300 KIAS / 0.70M

42
Q

The certified maximum tire speed rating is:

A

195 knots

43
Q

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

A

predictive windshear

B717 Limitations (1 decks)

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