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PSA Training > Limitations 700 > Flashcards

Limitations 700 Flashcards

This deck is a copy of a Quizlet deck

0
Q

Fuel imbalance

A

Takeoff…..300 lbs.

Flight……..800 lbs.

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1
Q

Engine Type

Thrust Rating

A

GE CF34-3B1
• 8,729 lbs per engine
• 9,220 lbs per engine

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2
Q

V Wiper

A

220 KIAS

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3
Q

Dry motoring limitations

A

90sec-5 min off

30sec-5 min off

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4
Q

Pressure refueling

A

19,594 lbs.

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5
Q

Max Tire speed

A

182 KIAS

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6
Q

Automatic Flight Control System

A

Use of speed mode (DES or IAS), flight director or autopilot coupled, during approach is not permitted

  • Not permitted for approaches below 600’ AGL except for visual and non-precision approaches
  • For precision approaches (PAR/ILS), the minimum is 100’ AGL
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7
Q

APU Start cycle (DC Ground Power)

A

3 start attempts in one hour with 2 min between each

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8
Q

APU Start cycles (Battery)

A

3 start attempts in one hour with 2 min between each

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9
Q

Cargo in cargo compartment

A

Flight must be within 45 min of suitable airport

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10
Q

Maximum Weight in Cargo Compartment

A

1,000 lbs. (for)

3,300 lbs. (aft)

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11
Q
  • Max load on TRU

* Max time with DC power to protect CRT displays

A
  • 100 amps

* 5 minutes

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12
Q

WING ANTI-ICE Conditions

A
  • Icing conditions exist when the OAT (for takeoff) is 5c or TAT (inflight) is 10c or below, and;
  • Visible moisture in any form is present in flight or below 400’ AGL for ground operations
  • Runway surfaces are wet or contaminated
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13
Q

Ramp Weight

A

75,250 lbs.

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14
Q
  • Max altitude for single pack operation

* Max differential

A
  • 31,000’

* 8.7 psi

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15
Q

N2 split at ground idle power

A

Not greater than 2% N2

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16
Q

Turbulence Penetration Speed

A

280 KIA’S / .75 M

whichever is lower

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17
Q

Max ITT for start

Cold start

A

900c

Engine must be run at idle until oil pressure returns to normal range

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18
Q

Tactile check

A
  • OAT 5c or less
  • Wing fuel temp 0c or less
  • Atmospheric conditions conducive to frost formation
  • Ice and frost may contine to adhere to wing surfaces even at temps above 5c
19
Q
  • Maximum slats/flaps altitude

* Enroute use of slats/flaps

A
  • 15,000

* Prohibited

20
Q

Maximum Takeoff Weight

A

75,000

21
Q

APU Door not closed or position unknown

A

300 KIAS

And APU must remain in operation

22
Q

Engine start limit

Shutdown limit

A
  • During all starts do not exceed 75% N1 for 2 minutes after start or until all operating indications are in the normal range whichever is longer
  • Operate engines for 2 minutes prior to shutdown.
23
Q

Airplane cold soak

A

-30 for than 8 hrs, before first flight:
• engines motored for 60 sec and fan rotation verified
• thrust reverses actuated until the deploy stow cycles less than 5 sec

24
Q

Max gear extension speed

A

220 KIA’S

25
Q

Cowl Anti-ice system

A

Cowl anti-ice must be on for all ground and flight ops when icing conditions exist except when
• Inflight SAT is -40 or below or
• Ice is annunciated

26
Q

Maximum Landing Weight

A

67,000

27
Q

If both engines are to be started using the APU bleed air

A

The operating engines thrust must not exceed 70% N2

28
Q

EICAS Limit Markings
• Red
• Amber
• Green

A
  • Maximum and Minimum Limitations
  • Caution
  • Normal Operating Range
29
Q

COWL ANTI-ICE Conditons

A
  • Icing conditions exist when the OAT (on the ground and for takeoff) or TAT (inflight) is 10c or below, and;
  • Visible moisture in any form is present in flight or below 400’ AGL for ground operations
  • When operating on surfaces that are wet or contaminated
30
Q

Takeoff power oil pressure minimum

A

45psi

31
Q

Wing Anti-Ice System

A

Wing anti-ice must be ON for T/O and flight ops when
• Icing conditions exist and airspeed less than 230 KIAS
• ICE is annunciated by the ice detection system
• Except when inflight SAT is -40c or less

32
Q
  • Flight spoilers min altitude

* To ensure adequate maneuver margins, flight spoilers must not be deployed below

A
  • 1,000’ AGL

* Ref plus 17 KIAS

33
Q

Maximum Zero Fuel Weight

A

62,300 lbs.

34
Q

Bleed air extraction from APU

NOT permitted above

A

25,000’

35
Q

Continuous ignition

A
  • T/O and landing on Contaminated Runways
  • T/O with x wind components greater than 15 KIAS
  • Flight through moderate or heavier intensity rain
  • Flight through moderate or heavier intensity turbulence
  • Flight in the vicinity of thunderstorms
36
Q

Flaps Vfo

A

8 - 230 KIAS
20 - 230 KIAS
30 - 185 KIAS
45 - 170 KIAS

37
Q

Taxi Lights

A

Off when plane is stationary for more than 10 minutes

38
Q

When must the wing anti-ice be turned on

A

2 minutes prior to T/O during all ground ops 5c OAT or below unless type III or type IV anti-icing fluid has been applied

39
Q

Why 2 minute delay observed between APU cranking attempts

A

Allow for the starter and starter contactor cooling and fuel drainage

40
Q

Starter cranking limits

A

90 secs……..10 secs off
90 secs……..10 secs off
90 secs……..5 minutes off

41
Q

Flaps Vfe

A

8 - 230 KIAS
20 - 230 KIAS
30 -185 KIAS
45 -170 KIAS

42
Q

Brake cooling limits

A

Minimum is 15 minutes and all BTMS Indicators must be green and not increasing

43
Q

Initiation of thrust lever from SHUT OFF to IDLE

A

ITT must be 120c or less for all ground starts

90c or less for all air starts

44
Q

Max gear extended speed

A

220 KIAS

45
Q

Thrust Reversers

A

75 KIAS not more than 60% N1

60 KIAS reduced to idle not above 30% N1

46
Q

Max gear retraction speed

A

200 KIAS

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