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PSA Training > PSA Limitations > Flashcards

PSA Limitations Flashcards

This flashcard deck was created using Flashcardlet's card creator

1
Q

Ramp Weight

A

53,250 lbs.

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2
Q

Maximum Takeoff Weight

A

53,000

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3
Q

Maximum Landing Weight

A

47,000

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4
Q

Maximum Zero Fuel Weight

A

44,000 lbs.

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5
Q

Maximum Weight in Cargo Compartment

A

3,500 lbs.

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6
Q

Turbulence Penetration Speed

A

280 KIA’S / .75 M

whichever is lower

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7
Q

Max gear extension speed

A

220 KIA’S

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8
Q

Max gear extended speed

A

220 KIAS

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9
Q

Max gear retraction speed

A

200 KIAS

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10
Q

V Wiper

A

220 KIAS

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11
Q

Max Tire speed (200/700)

A

182 KIAS

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12
Q

Cargo in cargo compartment

A

Flight must be within 45 min of suitable airport

300 nautical miles

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13
Q

Flaps Vfe

A

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

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14
Q

Flaps Vfo

A

8 - 200 KIAS
20 - 200 KIAS
30 - 185 KIAS
45 - 170 KIAS

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15
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
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16
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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17
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
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18
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

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19
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

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20
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

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21
Q

EICAS Limit Markings
• Red
• Amber
• Green

A
  • Maximum and Minimum Limitations
  • Caution
  • Normal Operating Range
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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.
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23
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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24
Q

N2 split at ground idle power

A

Not greater than 2% N2

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25
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

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26
Q

Takeoff power oil pressure minimum

A

45psi

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27
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
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28
Q

Starter cranking limits

200

A

1 min……..10 secs off
1 min……..10 secs off
1 min……..5 minutes off

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29
Q

Starter cranking limits

700/900

A

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

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30
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

31
Q

Thrust Reversers

A

During landing maximum reverse thrust is prohibited below 75 KIAS
and reverse idle should be achieved by 60 KIAS

32
Q

Max fuel imbalance (200)

A

Takeoff 800 lbs
All other phases of flight
800 lbs.

33
Q

Pressure refueling

200

A

14,518 lbs.

34
Q

APU Start cycles (Battery)

A

30 seconds…..2 minutes off
30 seconds…..20 minutes off
30 seconds…..2 minutes off
30 seconds…..40 minutes off

35
Q

APU Start cycle (DC Ground Power)

A

15 seconds…..2 minutes off
15 seconds…..20 minutes off
15 seconds…..2 minutes off
15 seconds…..40 minutes off

36
Q

Why 2 minute delay observed between APU cranking attempts

A

Allow for the starter and starter contactor cooling and fuel drainage

37
Q

Bleed air extraction from APU
NOT permitted above
(200)

38
Q

APU Door not closed or position unknown (200)

A

300 KIAS

And APU must remain in operation

39
Q

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

A

The operating engines thrust must not exceed 70% N2

40
Q

APU Door not closed or position unknown (700/900)

A

220 Kts

Or APU must remain in operation

41
Q

• Max altitude for single pack operation (200)

A

• 25,000 ft

42
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
• Visual and non-precision approaches the minimum height is 400’
• For precision approaches (PAR/ILS), the minimum is 100’ AGL

43
Q
  • Max load on TRU

* Max time with DC power to protect CRT displays

A
  • 100 amps

* 5 minutes

44
Q
  • Maximum slats/flaps altitude

* Enroute use of slats/flaps

A
  • 15,000

* Prohibited

45
Q

Flaps can not be extended unless it is reasonably assured that

A
  • The visibility will remain above the required visibility

* An emergency condition exists

46
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

47
Q

Taxi Lights

A

Off when plane is stationary for more than 10 minutes

48
Q

Brake cooling limits

A

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

49
Q

Hydraulic 3b pump

A

Must be on instead of Auto from the before start checklist until the shutdown checklist

50
Q

Engine Type

Thrust Rating

A

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

51
Q

Dry motoring limitations

A

90sec-5 min off

30sec-5 min off

51
Q

Maximum 90 degree crosswind

for Takeoff and landing

A

27kts

15 kts for reduced landing minimum (RVR below 2400) to runways w/out TDZ or CL lights

52
Q

Max altitude for engine start with APU bleed air

53
Q

Crew Oxygen

A

2 Pilot - 1410

3 Pilot - based on temp in POH before start check

54
Q

No Reduced Thrust (Flex) when?

A 
Contaminated Runways
De-iced
Anti-ice in use
Windshear downdrafts forecast
APR not available
Special departure procedure specifies full thrust
55
Q

Min fuel for go-around (200)

A

450lbs per side (900lbs)

56
Q

Min fuel for T/O when with a T/O alternate

57
Q

Max fuel imbalance (700/900)

A

Takeoff 300lbs

All other phases of flight 800lbs

58
Q

T/O with fuel load in excess of_____in the center tank is not permitted unless each wing tank is above______

A

500lbs

4,400lbs

59
Q

Fuel crossflow

A

Powered crossflow and gravity crossflow must be OFF for takeoff

60
Q

Min fuel for go-around (700/900)

A

600 lbs per side

1200 lbs total

61
Q

Fuel temperature?

A

Below 5c prohibited

62
Q

Max cruise in RVSM

63
Q

A/C Generator loading

A

Main GEN 30kVA up to 350 then 25 kVA from 350-360

65
Q

Bleed air extraction from APU
NOT permitted above
(700) (900)

65
Q

Max 90 crosswind for takeoff and landing.

67
Q

Max 90 degree crosswind for landing from a cat II approach

68
Q

Max headwind for landing CAT II

69
Q

Max tailwind for takeoff and landing

70
Q

Max operating altitude

200

71
Q

• Max altitude for single pack operation (700/900)

72
Q

Max operating altitude

700/900

73
Q

Thrust reverser deployment

A

During landing, maximum reverse thrust is prohibited below 75 KIAS, and reverse idle should be achieved by 60 KIAS

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