PSA Limitations

Question 0

Max gear extension speed

200/700/900

Answer 0

220 KIA’S

Question 1

Turbulence Penetration Speed

Answer 1

280 KIA’S / .75 M

whichever is lower

Question 2

Max gear extended speed

Answer 2

220 KIAS

Question 3

Max gear retraction speed

Answer 3

200 KIAS

Question 4

V Wiper

Answer 4

220 KIAS

Question 5

Max Tire speed

200/700

Answer 5

182 KIAS

Question 6

COWL ANTI-ICE Conditons

Answer 6

• 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

Question 7

WING ANTI-ICE Conditions

Answer 7

• 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

Question 8

Tactile check

Answer 8

• 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

Question 9

Cowl Anti-ice system

Answer 9

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

Question 10

Wing Anti-Ice System

Answer 10

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

Question 11

EICAS Limit Markings
• Red
• Amber
• Green

Answer 11

• Maximum and Minimum Limitations
• Caution
• Normal Operating Range

Question 12

Engine start limit

Shutdown limit

Answer 12

• 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.

Question 13

Max ITT for start

Cold start

Answer 13

900c

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

Question 15

Airplane cold soak

Answer 15

-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)

Question 16

Takeoff power oil pressure minimum

Answer 16

45psi

Question 16

Continuous ignition

Answer 16

• 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

Question 17

Initiation of thrust lever from SHUT OFF to IDLE

Answer 17

ITT must be 120c or less for all ground starts

90c or less for all air starts

Question 18

Thrust Reversers

Answer 18

75 KIAS not more than 60% N1

60 KIAS reduced to idle not above 30% N1

Question 19

Automatic Flight Control System

Answer 19

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

Question 20

• Maximum slats/flaps altitude

* Enroute use of slats/flaps

Answer 20

• 15,000

* Prohibited

Question 21

Max time with DC power to protect CRT displays

Answer 21

• 5 minutes

Question 22

• Flight spoilers min altitude

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

Answer 22

• 1,000’ AGL

* Ref plus 17 KIAS

Question 23

Taxi Lights

Answer 23

Off when plane is stationary for more than 10 minutes

Question 24

Brake cooling limits

Answer 24

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

Question 25

Hydraulic 3b pump

Answer 25

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

Question 26

Dry motoring limitations

Answer 26

90sec-5 min off | 30sec-5 min off

Question 27

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

Answer 27

500lbs | 4,400lbs

Question 28

Max altitude for engine start with APU bleed air

Answer 28

13,000'

Question 29

Maximum 90 degree crosswind | for Takeoff and landing

Answer 29

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

Question 30

Crew Oxygen

Answer 30

2 Pilot - 1410 | 3 Pilot - based on temp in POH before start check

Question 31

No Reduced Thrust (Flex) when?

Answer 31

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

Question 32

Fuel crossflow

Answer 32

Powered crossflow and gravity crossflow must be OFF for takeoff

Question 33

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

Answer 33

4,600 lbs (200) | 1 hr in cruise, still air, with one engine not working

Question 34

Fuel temperature?

Answer 34

Below 5c prohibited

Question 35

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

Answer 35

-40°C

Question 36

Max cruise in RVSM

Answer 36

.82M

Question 37

Oil Temp Limitations

Answer 37

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

Question 38

RVSM Required Equipment List

Answer 38

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

Question 39

Maximum pressure altitude for takeoff and landing

Answer 39

8,000 ft.

Question 40

Maximum ambient temperature for takeoff and landing

Answer 40

ISA +35°C

Question 41

Minimum ambient temperature approved for takeoff

Answer 41

-40°C

Question 42

Maximum runway slope approved for takeoff and landing

Answer 42

+2.0% (uphill) | -2.0% (downhill)

Question 43

Maneuvering Limit Load Factors

Answer 43

Clean -1.0/+2.5 G | Flaps 0.0/+2.0 G

Question 44

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

Answer 44

8.7 psi -0.5 psi .1 psi

Question 45

Use of the EMER DEPRESS switch not permitted above

Answer 45

15,000 ft

Question 46

Maximum headwind CAT II

Answer 46

16 kits

Question 47

Max operating altitude 200

Answer 47

36,000 ft

Question 48

Max operating altitude | 700/900

Answer 48

41,000 ft

Question 49

Max altitude for single pack operation 200

Answer 49

25,000 ft

Question 50

Max altitude for single pack operation 700/900

Answer 50

31,000 ft

Question 51

Max tire speed, 900

Answer 51

195 it's