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PSA Training > PSA Limitations > Flashcards

PSA Limitations Flashcards

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0
Q

Max gear extension speed

200/700/900

A

220 KIA’S

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1
Q

Turbulence Penetration Speed

A

280 KIA’S / .75 M

whichever is lower

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2
Q

Max gear extended speed

A

220 KIAS

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3
Q

Max gear retraction speed

A

200 KIAS

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4
Q

V Wiper

A

220 KIAS

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5
Q

Max Tire speed

200/700

A

182 KIAS

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6
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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7
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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8
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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9
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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10
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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11
Q

EICAS Limit Markings
• Red
• Amber
• Green

A
  • Maximum and Minimum Limitations
  • Caution
  • Normal Operating Range
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12
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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13
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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15
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 (2 sec for 700)

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16
Q

Takeoff power oil pressure minimum

A

45psi

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16
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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17
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

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18
Q

Thrust Reversers

A

75 KIAS not more than 60% N1

60 KIAS reduced to idle not above 30% N1

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19
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 80’ AGL

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20
Q
  • Maximum slats/flaps altitude

* Enroute use of slats/flaps

A
  • 15,000

* Prohibited

21
Q

Max time with DC power to protect CRT displays

A

• 5 minutes

22
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

23
Q

Taxi Lights

A

Off when plane is stationary for more than 10 minutes

24
Q

Brake cooling limits

A

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

25
Q

Hydraulic 3b pump

A

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

26
Q

Dry motoring limitations

A

90sec-5 min off

30sec-5 min off

27
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

28
Q

Max altitude for engine start with APU bleed air

29
Q

Maximum 90 degree crosswind

for Takeoff and landing

A

27kts
Category II approach is 15kts
Category II approach headwind 17kts
Braking action fair - 15kts or less

30
Q

Crew Oxygen

A

2 Pilot - 1410

3 Pilot - based on temp in POH before start check

31
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
32
Q

Fuel crossflow

A

Powered crossflow and gravity crossflow must be OFF for takeoff

33
Q

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

A

4,600 lbs (200)

1 hr in cruise, still air, with one engine not working

34
Q

Fuel temperature?

A

Below 5c prohibited

35
Q

Min temp for cold-soaked APU starting on the ground:

36
Q

Max cruise in RVSM

37
Q

Oil Temp Limitations

A

Min Start -40c
Max Continuos +155c
Max Permissible +163c ( for 15 min)

38
Q

RVSM Required Equipment List

A

Autopilot - 1 working
Altitude Alerting System - 1 working
Transponder - (2) 1 working
ADC’s - (2) Two 2 working

39
Q

Maximum pressure altitude for takeoff and landing

40
Q

Maximum ambient temperature for takeoff and landing

A

ISA +35°C

41
Q

Minimum ambient temperature approved for takeoff

42
Q

Maximum runway slope approved for takeoff and landing

A

+2.0% (uphill)

-2.0% (downhill)

43
Q

Maneuvering Limit Load Factors

A

Clean -1.0/+2.5 G

Flaps 0.0/+2.0 G

44
Q

Max differential pressure:
Max negative differential pressure:
Max differential pressure for taxi, takeoff, and landing

A

8.7 psi
-0.5 psi
.1 psi

45
Q

Use of the EMER DEPRESS switch not permitted above

46
Q

Maximum headwind CAT II

47
Q

Max operating altitude 200

48
Q

Max operating altitude

700/900

49
Q

Max altitude for single pack operation 200

50
Q

Max altitude for single pack operation 700/900

51
Q

Max tire speed, 900

A

195 it’s

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