Psa Crj-200 Limitations And Immediate Action Items Test

Front 1

Minimum flight crew

Back 1

One captain and one first officer

Front 2

Maximum Crosswind for takeoff and landing ________

Back 2

27 kts

Front 3

Maximum Crosswind for reduced landing minima to runways without TDZ lights and/ or CL lights

Back 3

15 kts

Front 4

Maximum crosswind for landing from a CAT II approach

Back 4

15 kts

Front 5

Maximum headwind for landing from a CAT II approach

Back 5

17 kts

Front 6

Maximum Tailwind for takeoff and landing _________

Back 6

10 kts

Front 7

Maximum runway slope for takeoff and landing

Back 7

2.0% uphill or downhill

Front 8

Maximum Operating Altitude?

Back 8

36,000 ft

Front 9

Maximum Pressure Altitude for takeoff and landing?

Back 9

8,000 ft

Front 10

Maximum ambient temperature for takeoff and landing

Back 10

ISA +35°C

Front 11

Minimum Ambient Temperature for Takeoff?

Back 11

-40° C

Front 12

Maneuvering Limit Load Factors - flaps retracted

Back 12

-1.0 to +2.5 G

Front 13

Maneuvering Limit Load Factors - flaps extended

Back 13

0.0 to +2.0 G

Front 14

Maximum Taxi and Ramp weight

Back 14

53,250 lbs

Front 15

Maximum Takeoff weight

Back 15

53,000 lbs

Front 16

Maximum Landing Weight

Back 16

47,000 lbs

Front 17

Maximum Zero Fuel Weight?

Back 17

44,000 lbs

Front 18

Minimum Operating Weight Empty

Back 18

25,480 lbs

Front 19

Flights must be within _________ minutes of a suitable airport with cargo in the cargo compartment.

Back 19

45

Front 20

Maximum weight in the cargo compartment

Back 20

3500 lbs.

Front 21

Maximum Turbulence Penetration Speed

Back 21

280 KIAS or .75 Mach, whichever is lower

Front 22

Gear Position and Operating Airspeed limitations?

Back 22

Extension - 220
Down and Locked - 220
Retraction - 200

Front 23

Maximum airspeed for windshield wiper operation

Back 23

220 KIAS

Front 24

Maximum airspeed for windshield wiper operation failed in the non-parked position

Back 24

200 - 220 KIAS

Front 25

Maximum Cruise Mach in RVSM Airspace

Back 25

0.82 Mach

Front 26

Maximum Tire Speed

Back 26

182 Knots

Front 27

Flap Positions 8, 20, 30, 45 Vfe & Vfo Speeds?

Back 27

Vfe Vfo

8 - 230 / 200
20 - 220 / 200
30 - 185
45 - 170

Front 28

Definition of Icing Conditions:
COWL

Back 28

Icing Conditions exist when the OAT or TAT is 10°C or below, and:
• Visible moisture in any form, is present in flight, or below 400 feet AGL for ground operations, or
• When operating on surfaces that are wet or contaminated

Front 29

Definition of Icing Conditions:
Wing

Back 29

Icing conditions exist when the OAT is 5°C or TAT is 10°C or below, and:
• Visible moisture in any form, is present in flight, or below 400 feet AGL for takeoff, or
• The runway is wet or contaminated.

Front 30

When must COWL ANTI-ICE be on

Back 30

Cowl Anti-Ice must be ON for all ground and flight operations when icing conditions exist except when the inflight SAT is -40°C or below, or ICE is annunciated by the ice detection system.

Front 31

When must WING ANTI-ICE be on

Back 31

Wing Anti-Ice must be ON for takeoff and flight operations when ICE is annunciated by the ice detection system, or when icing conditions exist and the airspeed is less than 230 KIAS except when the inflight SAT is -40°C or below.
Wing Anti-Ice must be ON for the final two minutes prior to takeoff during all ground operations 5°C
OAT or below unless Type III or IV anti-icing fluid has been applied.

Front 32

EICAS Limit Markings.
RED
AMBER
GREEN

Back 32

Maximum and Minimum Limitations
Cation Range
Normal Operating Range

Front 33

During ALL starts, do not exceed _____ N1 for _____ minutes after start, or until all operating indications are in the normal range, whichever is _____.

Back 33

75% ; 2 ; longer

Front 34

Start temperature

Back 34

900° C

Front 35

Maximum N2 split at idle

Back 35

2%

Front 36

If N2 is _____ or less with an OAT of _____ or warmer, do not accelerate above idle.

Back 36

57% ; -20° C

Front 37

Continuous Ignition must be used during

Back 37

• Takeoff and landing on contaminated runways
• Takeoff with high crosswind components (15 knots or greater)
• Flight through moderate or heavier intensity rain
• Flight through moderate or heavier intensity turbulence
• Flight in the vicinity of thunderstorms

Front 38

Starter Cranking Limits

Back 38

1 min on / 10 seconds off
1 min on / 10 seconds off
1 min on / 5 minutes off

Front 39

The starter must not be engaged if indicated N2 RPM exceeds _____.

Back 39

55%

Front 40

Maximum ITT allowed to advance the thrust levers to Idle for all ground starts

Back 40

120 deg C

Front 41

Maximum Fuel imbalance between the left and right wing tank?

Back 41

800 lbs

Front 42

Maximum total fuel for pressure Refueling ?

Back 42

14,518 lbs

Front 43

Takeoff with a fuel load in excess of __________ , in the center tank is not permitted unless each wing tank is above _____________

Back 43

500 lbs; 4,400 lbs

Front 44

Powered crossflow and gravity crossflow must be _________ for takeoff.

Back 44

OFF

Front 45

APU Start cycles on Battery

Back 45

30 secs / 2 min
30 secs / 20 min
30 secs / 2 min
30 secs / 40 min

Front 46

APU Start cycles on DC ground Power

Back 46

15 secs / 2 min
15 secs / 20 min
15 secs / 2 min
15 secs / 40 min

Front 47

APU Maximum starting altitude

Back 47

30,000 ft.

Front 48

APU Maximum Operating altitude

Back 48

36,000 ft.

Front 49

APU bleed air extraction for Air Conditioning is not permitted above _____ .

Back 49

15,000 ft.

Front 50

if both engines are to be started using the APU bleed air, the operating engine's thrust must not exceed _____ N2.

Back 50

70%

Front 51

With the APU door not closed, or the door position is unknown: The airplane must be limited to _____, or _____.

Back 51

300 KIAS; the APU must remain in operation

Front 52

Use of SPEED MODE (DES or IAS), flight director, or autopilot coupled during approach is _____.

Back 52

not permitted.

Front 53

Minimum Auto Pilot Engagement altitude __________ , except when performing:
Non-Precision Approach ___________
Precision Approach __________

Back 53

600 ; 400 ; 80

Front 54

RVSM Required Equipment List?

Back 54

Autopilot - Must be operational
Altitude Alerting System - Must be operational
2 Transponders with Altitude Reporting - 1 Must be Op
2 Air Data Computers - Both must be operational

Front 55

To protect flight compartment CRT displays, maximum permissible time on the ground with only DC power ___________

Back 55

5 minutes

Front 56

Enroute use of slats/flaps is

Back 56

prohibited

Front 57

Maximum Slat/Flaps extended altitude

Back 57

15,000 ft

Front 58

Minimum altitude for flight spoiler deployment __________

Back 58

1,000 ft.

Front 59

Minimum airspeed for flight spoiler use ________________

Back 59

approach speed + 17 KIAS

Front 60

During landing application of thrust reverse above ________ is not permitted at air speeds below __________ . Below ___________ , reverse thrust must be reduced to idle, not above _____________ .

Back 60

60% N1 ; 75 KIAS
60 KIAS ; 30% N1

Front 61

Minimum brake cooling time _____

Back 61

15 minutes

Front 62

Name all the Boldfaced Emergency Procedures

Back 62

Braking Loss/ Asymmetry

Cabin Alt Msg or Emergency Descent Procedure

Double Engine Failure

Smoke/Fumes

Stab Trim Runaway

Eng Oil Press Msg or Oil Pressure Low

Aileron Jam, Elevator Jam, Rudder Jam

Un-commanded Yaw

Front 63

Braking Loss / Asymmetry

Back 63

1. Wheel brakes ....... Release Momentarily
2. PM will switch ANTI-SKID OFF
3. Wheel brakes ....... Re-Apply as required
4. Reverse Thrust . Apply maximum until stopping assured

Front 64

Cabin Alt / Emergency Descent Procedure

Back 64

1. Oxygen Mask ......... Don and 100%
2. Crew Communication ...... Establish
3. CAPT assumes PF Duties

Front 65

Double Engine Failure

Back 65

1. CONT IGNITION ........ ON
2. Airspeed ....... 240 KIAS minimum

Front 66

Smoke / Fumes

Back 66

1. Oxygen Mask ...... Don and 100%
2. Crew Communication ...... Establish

Front 67

Stab Trim Runaway

Back 67

1. Control Wheel........ Assume Manual Control and override runaway
2. BOTH STAB DISCs ....... PUSH, HOLD and RELEASE
3. CAPT assumes PF duties
4. STAB CH. 1 cb (2F5) ...... OPEN
5. STAB CH. 2 cb (4A1) ...... OPEN

Front 68

Tactile Check - when, why, how

Back 68

tactile inspection of the wing leading edge, wing upper forward and rear surfaces during the walkaround. determines the wing is free of frost, ice, snow, or slush. needed when OAT is 5°C or less, or wing fuel temp is 0°C or less, or atmospheric conditions are conducive to frost formation.

Front 69

Continued operation in areas where SLD icing conditions exist is _____.

Back 69

prohibited

Front 70

all contaminated performance data will be for _____ takeoffs.

Back 70

static

Front 71

maximum ITT for all air starts

Back 71

90°C

Front 72

oil pressure steady-state idle

Back 72

25 PSI minimum

Front 73

oil pressure takeoff power

Back 73

45 PSI minimum

Front 74

minimum oil temperature for engine starting

Back 74

-40°C

Front 75

operate engines at or near idle for _____ minutes prior to shutdown

Back 75

2

Front 76

airplane cold soak definition

Back 76

before the first flight of the day, when the airplane is cold soaked at an ambient temperature of -30°C or below for more than 8 hours

Front 77

airplane cold soak operational

Back 77

engines must be motored for 60 seconds and fan rotation must be verified before initiating engine start.

thrust reversers must be actuated until the deploy & stow cycles are less than 5 seconds

Front 78

dry motoring cycle for engines

Back 78

90 seconds on, 5 minutes off

30 seconds on, 5 minutes off for all subsequent attemps

Front 79

takeoff with engine fuel temperature indications below _____ is prohibited

Back 79

5°C

Front 80

minimum fuel quantity for a go-around per wing tank, assuming 10 degrees pitch up:

Back 80

450 lbs

Front 81

maximum APU RPM

Back 81

107%

Front 82

use of the EMER DEPRESS switch above _____ is prohibited

Back 82

15,000

Front 83

max altitude for single pack operations

Back 83

25,000

Front 84

max differential pressure for taxi, takeoff, and landing

Back 84

.1 psi

Front 85

maximum relief differential pressure

Back 85

8.7 psi