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B-717 > Limitations > Flashcards

Limitations Flashcards

1
Q

Max starting altitude for APU

A

FL 370

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2
Q

Max gear extension/extended speed

A

300 KIAS/M.70

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3
Q

Max gear retraction speed

A

250 KIAS

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4
Q

Landing gear load limit at Max landing weight

A

600 FPM

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5
Q

Max landing gear load limit at Max Takeoff weight

A

360 FPM

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6
Q

Min brake pressure for at least 8 hrs parking time

A

2000 PSI

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7
Q

When should you never set the parking brake

A

When BRAKE OVERHEAT displayed on EAD

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8
Q

Which circuit breakers must never be reset?

A

Hydraulic Aux Pump, Fuel Pump, Fuel Quantity Indicating System, Lavatory Flush Monitor, Galley Power

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9
Q

Max fuel lateral imbalance

A

1500 lbs

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10
Q

Center fuel tank ballast fuel limitations (2)

A
  1. Ballast fuel not required to complete the flight

2. Zero fuel weight and CG includes the weight of the ballast fuel.

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11
Q

Fuel density range limitation

A

6.3 to 7.1 lbs/gal

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12
Q

Max fuel temperature

A

54°C

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13
Q

Jet A minimum fuel temperature

A

-40°C

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14
Q

If main wing fuel tanks are full, how can you get to max ramp weight?

A

Fuel may be added to the center fuel tank

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15
Q

If main wing tanks are NOT full, can we fill the center fuel tank?

A

Yes, but only if the ZFW and CG plus the weight of the center fuel tank do not exceed MaxZFW (100,500 lbs) and CG limitations

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16
Q

How to burn center tank fuel?

A

Center tank shall be emptied first. If center tank being used for ballast, burn center first to the ballast value, then burn main wing tanks.

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17
Q

Rudder hydraulic power limitation

A

Must be on for takeoff

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18
Q

RUDDER POWER OFF airspeed limitation

A

144 KIAS

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19
Q

Speed brake - flaps limitation

A

Speed brakes must not be used w/flaps extended beyond 20°

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20
Q

What should you never do with spoiler/speedbrake lever in flight?

A

Never move it to ground spoiler position in flight.

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21
Q

Max airspeed

A

340 KIAS up to FL260

MMO = .82 up to FL370

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22
Q

Max slat extend speed

A

M .57 / 280 KIAS

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23
Q

Takeoff configuration limitation - flaps/slats

A

Slats must be extended for takeoff. Flaps must be set no less than 5°

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24
Q

Max flap speeds

A

0-10° - 280 KIAS/M.57
10.1-20° - 240 KIAS/M.57
25° - 220 KIAS/M.57
40° - 200 KIAS/M.57

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25
Q

Max tire speed

A

195 KIAS

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26
Q

Time limit for Takeoff Thrust

A

5 minutes (10 minutes if engine failed or go-around)

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27
Q

Max TGT @ Max Continuous Thrust

A

Amber Line

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28
Q

Normal engine oil pressure

A

45 psi and greater

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29
Q

Engine Starter Duty Cycle

A

3 minutes - 15 seconds
3 minutes - 15 seconds
3 minutes - 15 minutes

30
Q

Time limit for Go-Around Thrust

A

None

31
Q

APU starter motor duty cycle

A

3 consecutive, then wait 30 minutes (wait until APU parameters on Secondary Engine synoptic are no longer displayed before another start attempt)

32
Q

APU air limitation

A

Must be OFF for takeoff and inflight ops

33
Q

Max latitude for IRS ground alignment

A

78.25°N - 60°S

34
Q

Latitude restriction for IRS only navigation

A

North of 80°N or South of 60°S

35
Q

Flight director wind shear guidance

A

Prohibited with one engine inoperative

36
Q

PROF mode restrictions on approaches

A

Use is prohibited below MDA or DA

37
Q

ILS approach with inop glideslope: FMS PROF mode & Vertical Descent Indicator (VDI) limitation

A

VDI must not be used for descent after the FAF

38
Q

RNP value for GPS approaches

A

0.3

39
Q

Speed limit with inoperative Mach Trim

A

M .78

40
Q

Minimum altitude for autopilot use on instrument approaches

A

Minimums minus 50 ft

41
Q

Auto coupled ILS restriction

A

Disconnect A/P if STAB OUT OF TRIM alert is displayed for more than 3 seconds after aircraft is stabilized and tracking the glide slope

42
Q

Lowest altitude to engage autopilot

A

200 ft AGL (HAL restriction is 500 AGL)

43
Q

Max operating temperature at Sea Level

A

50°C

44
Q

Minimum operating temperature at Sea Level

A

-54°C

45
Q

FLOW switch limitation

A

If AIR CONDITIONING is on for takeoff, then FLOW switch must be in NORM position

46
Q

Manual mode cabin pressurization limitation

A

Takeoff and land UNpressurized

47
Q

Max emergency relief pressure

A

8.2 psi

48
Q

Max cabin differential pressure

A

7.8 psi

49
Q

Cracked CAPT, center, or FO windshield - speed limits below 10,000ft

A

Outer glass- under 315 KIAS

Inner glass- under 235 KIAS

50
Q

Limitation when windshield heat is inop?

A

Do not exceed 315 KIAS below 10,000 ft

51
Q

Cracked window limitation

A

Do not use windshield anti-ice or anti-fog

52
Q

Max certified altitude

A

FL 370

53
Q

Engine Takeoff Wind limitation

A

Engine Crosswind limit is 40 kts (can taxi but limited to 50% N1)

54
Q

Max tailwind for takeoff and landing

A

10 kts

55
Q

Runway slope limitations for takeoff and landing

A

+1.7% to -2.0%

56
Q

Maneuvering load factor limit — flaps/slats retracted

A

+2.5 g to -1.0 g

57
Q

Maneuvering load factor limit — flaps and slats extended

A

+2.0 g to 0 g

58
Q

Maneuvering load factor limit — flaps retracted and slats extended

A

+2.0 g to 0 g

59
Q

Max ramp/taxi weight

A

115,000 lbs

119,000 lbs (488, 489, 490)

60
Q

Max takeoff weight

A

114,000 lbs

118,000 lbs (488, 489, 490)

61
Q

Max landing weight

A

110,000 lbs

62
Q

Max zero fuel weight

A

100,500 lbs

63
Q

Emergency lights limitation

A

Must be armed for all flight operations

64
Q

Wing landing light motor cooling limitations

A
  1. 5 minutes after initial extension or retraction,

3. 5 minutes after each subsequent extension or retraction

65
Q

Landing lights still, ambient air limitation

A

Must not be on for more than 10 minutes (heat build up)

66
Q

Forward entry and service door girt bar limitations

A

Girt bars must be inserted in floor fittings prior to departure and in position until arrival

67
Q

Emergency operating handle on aft pressure bulkhead door limitations

A

Must be exposed and normal operating handle covered prior to departure

68
Q

Can use reduced thrust for takeoff on wet runway?

A

Yes - when using wet runway takeoff performance

69
Q

When can we NOT use reduced thrust on takeoff?

A
  1. Contaminated runway with standing water, loose snow, slush, compacted snow or wet ice.
  2. When items affecting performance cause a significant increase in crew workload (inop equipment, non-std takeoff technique)
70
Q

When is reinforced cockpit door checked?

A

Must be checked each flight day (Mx overnight check)

B-717 (4 decks)

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