Psa Crj 200/700/900 Limitations

Front 1

What is the maximum allowable weight of the CR7/CR9 at the gate? Takeoff and Ramp

Back 1

CR7: 75,250 lbs.

CR9: 85,000 lbs.

Front 2

What is the maximum allowable takeoff weight of the CR7/CR9?

Back 2

CR7: 75,000 lbs.

CR9: 84,500 lbs.

Front 3

What is the maximum zero fuel weight of the CR7/CR9?

Back 3

CR7: 62,300 lbs.

CR9: 70,750 lbs.

Front 4

What is the maximum weight for landing for the CR7/CR9?

Back 4

CR7: 67,000 lbs.

CR9: 75,100 lbs.

Front 5

What is the maximum temperature for takeoff and landing?

Back 5

ISA + 35° C

Front 6

What is the minimum temperature for takeoff and dispatch?

Back 6

-40°C.

Front 7

What is the maximum takeoff and landing altitude?

Back 7

8,000 feet pressure altitude.

Front 8

What is the maximum Runway slope?

Back 8

±2% Uphill

±2% Downhill

Front 9

What is the maximum tailwind allowed for takeoff and landing?

Back 9

10 knots

Front 10

Assuming aircraft weight and OAT allow, what is the maximum altitude the aircraft may be

operated?

Back 10

CR2: FL360

CR7/CR9: FL410

Front 11

Your flight must be within 60 minutes for the CR7/CR9 of the nearest suitable airport under what

conditions?

Back 11

If cargo is carried in the cargo compartment.

Front 12

Assuming the BTMS system is operative, what is the minimum brake cooling time between

a landing stop or a rejected takeoff and the subsequent takeoff?

Back 12

15 minutes.

Front 13

What is the maximum crosswind?

Back 13

27 Knots

Front 14

What is the maximum speed to raise the landing gear?

Back 14

200 knots.

Front 15

What is the maximum speed with the landing gear extended?

Back 15

220 knots.

Front 16

What is the maximum speed for flaps 1°?

Back 16

230 knots.

Front 17

What is the maximum speed for flaps 8°?

Back 17

230 knots.

Front 18

What is the maximum speed for flaps 20°?

Back 18

220 knots

Front 19

What is the maximum speed for flaps 30?

Back 19

185 knots

Front 20

What is the maximum speed for flaps 45°?

Back 20

170 knots

Front 21

What is the maximum allowable tire speed for the CR7/CR9?

Back 21

182 knots ground speed

Front 22

What is the maximum airspeed for turbulent air penetration?

Back 22

280 knots or mach .75 whichever is lower

Front 23

What is the minimum altitude the autopilot may turned on after takeoff or go around?

Back 23

600 feet AGL.

Front 24

What is the minimum altitude the autopilot may be used while flying a visual approach?

Back 24

400 feet AGL.

Front 25

What is the minimum altitude the autopilot maybe used while flying a non-precision approach?

Back 25

400 feet AGL or 50 feet below the MDA (whichever is higher).

Front 26

By what altitude must the aircraft be configured for landing and on a stable approach prior

to commencing a Category II approach?

Back 26

By 1000 feet AGL

Front 27

In order to takeoff with more than 500 lbs. of fuel in the center tank, how much fuel needs

to be in the wing tanks?

Back 27

More than 4,400 lbs. in each wing tank.

Front 28

What is the maximum permissible fuel imbalance between the contents of the main left tank and the main right tank?

Back 28

300 lbs - During takeoff.

800 lbs - All other phases of flight.

Front 29

What is the minimum fuel quantity in each wing for a go around?

Back 29

600 lbs.

Front 30

What is the maximum engine ITT allowed during all ground starts

Back 30

120°C.

Front 31

How long must the engines stabilize at idle prior to shutdown?

Back 31

2 minutes.

Front 32

Does taxi time count towards the stabilization time and if so under what conditions?

Back 32

Yes, taxi time at a stabilized 80% N2 or below may be counted towards the two-minute cool down period.

Front 33

For how long must the engine starter cool after the third start attempt?

Back 33

5 minutes.

Front 34

How long may the starter remain on during a start attempt CR2/CR7/CR9?

Back 34

CR2- 60 seconds

CR7/CR9 - 90 seconds.

Front 35

During Landing, Max Reverse Thrust is prohibited below what speed?

Back 35

75 knots.

Front 36

Reverse idle must be achieved by what speed?

Back 36

60 knots.

Front 37

Under what conditions do icing conditions exist on ground and for takeoff?

Back 37

OAT 10°C or lower with visible moisture present in any form with visibility 1 mile or less.

Front 38

When must cowl anti-ice only be used?

Back 38

• Taxi - Ground Contamination or Visible Moisture and OAT is 10c or Below
  
• Takeoff - Ground Contamination or Visible Moisture and OAT is 10c or Below
• In Flight - Visible Moisture, TAT 10c to SAT -40c, and Airspeed is equal to or greater than 230 knots

Front 39

When must Wing ice be used as well at Cowl Ice

Back 39

• Takeoff - Ground Contamination or Visible Moisture and OAT is 5c or Below.
• In Flight - Visible Moisture, TAT 10c to SAT -40c, and airspeed is less than 230 knots.
  
• Ice annunciated in flight.

Front 40

What is the maximum 90 degree crosswind for takeoff and landing?

Back 40

27 knots

Front 41

What is the maximum 90 degree crosswind for landing from a Category II Approach?

Back 41

15 knots

Front 42

Maximum headwind for a landing from a Category II approach?

Back 42

16 knots

Front 43

Maximum direct tailwind for takeoff and landing?

Back 43

10 knots

Front 44

What is the minimum operating weight empty of the CR7/CR9?

Back 44

CR7: 42,000 lbs.

CR9: 45,000 lbs.

Front 45

Minimum flight crew?

Back 45

One Captain

One First Officer

Front 46

Maximum gear extended speed

Back 46

220 knots

Front 47

Maximum airspeed for windshield wiper operation

Back 47

220 knots

Front 48

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

Back 48

CR2: 220 knots

CR7/CR9: 250 knots

Front 49

In the CR7/CR9 Vfe and Vfo are?

Back 49

Equal

Front 50

Ground Contamination Definition

Back 50

Runways, ramps, or taxiways with surface snow, ice, slush or standing water.

Front 51

Visible Moisture Definition

Back 51

Visible moisture or precipitation in any form (such as clouds, fog with visibility of one mile or less, mist, rain, snow, sleet or ice crystals) is present inflight, or below 400' AGL for takeoff.

Front 52

Continuous engine ignition must be used during the following: (5 items)

Back 52

• 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 53

EICAS Indicating Red mean?

Back 53

Maximum and minimum limitations

Front 54

EICAS Indicating Yellow mean?

Back 54

Caution Range

Front 55

EICAS Indicating Green mean?

Back 55

Normal Operating Range

Front 56

ENGINE OPERATING LIMITS DUE TO WIND DIRECTION

Within 30° on either direction of the airplane nose-no windspeed limit

-OR-

>30° in either direction of the airplane nose- <5 knots windspeed

Back 56

No limitations - TOGA thrust may be applied before brakes released.

Front 57

ENGINE OPERATING LIMITS DUE TO WIND DIRECTION

>30° in either direction of the airplane nose and between 5 and 30 knots windspeed

Back 57

Apply maximum of 75% N1 before brake release, then TOGA thrust.

Front 58

ENGINE OPERATING LIMITS DUE TO WIND DIRECTION

>30° in either direction of the airplane nose >30 knots windspeed

Back 58

Apply maximum of idle/taxi thrust before brake release, then TOGA thrust

Front 59

ENGINE STARTER CRANKING LIMITS

CR7/CR9 - Ground only

Back 59

Start 1 - 90 seconds on 10 seconds off

Start 2 - 90 seconds on 10 seconds off

Start 3 and subsequent - 90 seconds on 5 minutes off.

Front 60

ENGINE STARTER CRANKING LIMITS

CR7/CR9 - Flight only

Back 60

Start 1 - 2 minutes on 10 seconds off

Start 2 and subsequent - 1 minute on 5 minutes off.

Front 61

Associated Conditions.

At initiation of thrust lever movement from

SHUT OFF to IDLE:

Back 61

• ITT must be 120°C or less for all ground starts

Front 62

Dry-Motoring Cycle.

Back 62

A dry-motoring cycle (with thrust levers at SHUT OFF) may be used for engine ground starts and engine air starts.

Start 1 - 90 Seconds on 5 minutes off

Start 2 and subsequent - 30 seconds on 5 minutes off.

Front 63

Oil Pressure

Steady-State Idle

Back 63

25 psi minimum

Front 64

Oil Pressure

Takeoff Power

Back 64

45 psi minimum

Front 65

Oil Pressure

Maximum Continuous

Back 65

95 psi maximum

Front 66

Oil Pressure

Maximum Transient

Back 66

156 psi when oil temp is <60°C

Front 67

Oil Pressure

Maximum transient after cold start(10 minutes maximum)

Back 67

182 psi or amber dashes

Front 68

After cold start engine must?

Back 68

Remain at idle until oil pressure returns to normal range.

Front 69

Fuel Quantity Pressure Refueling

Back 69

Left Tank - 7,492 lbs.

Right Tank - 7,492 lbs.

Center Tank - 4,610 lbs.

Total - 19,594 lbs.

Front 70

Fuel Crossflow

Powered crossflow and gravity crossflow must be OFF for what phase of flight?

Back 70

Takeoff

Front 71

APU Starter Limits

The APU starter motor duty cycle is limited to not more than _______ (1) attempts in one _______(2) with a _______(3) delay between cranking attempts.

Back 71

1. three (3) starts/start
2. one (1) hour
3. two (2) minute delay
   

Front 72

APU Bleed Air

Air Conditioning

Bleed air extraction from the APU is not permitted above what altitude? CR2/CR7/CR9

Back 72

CR2 - 15,000ft.

CR7/CR9 - 25,000ft.

Front 73

APU Bleed Air

Engine start during ground operations

Back 73

Each engine may be started using the APU as a bleed air source.

Front 74

APU Door Open Limitation.

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

Back 74

220 knots, or the APU must remain in operation

Front 75

Taxi Light

The taxi lights must be switched OFF whenever the airplane is stationary in excess of

Back 75

10 Minutes

Front 76

Flight Spoilers.

Minimum altitude for flight spoilers deployment:

Back 76

1000 ft. AGL

Front 77

Flight spoilers

To ensure adequate maneuver margins, flight spoilers must not be extended inflight at airspeeds below the

Back 77

Vr + 17 knots

Front 78

Thrust Reversers

During landing, maximum reverse thrust is not permitted at airspeeds below?

Back 78

75 knots, and reverse idle should be achieved by 60 knots.

Front 79

Wheel Brake Cooling Limitations.

Minimum brake cooling time is_____(1)? and All BTMS indicators must be _____(2)?and are not______(3)?

Back 79

1. 15 minutes,
   
2. Green
   
3. Not increasing.
   

Front 80

Automatic Flight Control System

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

Permitted or Not Permitted

Back 80

Not Permitted.

Front 81

Automatic Flight Control System

CR9 Use of VNAV, flight director or autopilot coupled, during the climb and approach phases of flight is?

Permitted or Not Permitted

Back 81

Not Permitted.

Front 82

Automatic Flight Control System

Operation with the autopilot engaged is prohibited at altitudes below 600 ft. AGL, except when performing thefollowing:

3 Things

Back 82

1. For visual and non-precision approaches, the minimum height for autopilot use is 400 ft. AGL.
   
2. For precision approaches (PAR/ILS), the minimum height for autopilot use is 80 ft. AGL.
   
3. CR9 For precision approaches (PAR/ILS) or approach procedures with vertical guidance, the minimum height for autopilot use with one engine operating is 110 ft. AGL
   

Front 83

Automatic Flight Control System

Category II Approach must be flown with the autopilot.

Engaged or Not Engaged

Back 83

Engaged.

Front 84

RVSM Airspace.

Maximum cruise speed in RVSM airspace is?

Back 84

0.82M.

Front 85

RVSM Airspace.

In flight, prior to entering RVSM airspace all required equipment for operation in RVSM airspace must be.

Back 85

Operational.

Front 86

The ADC source coupled to the active FCC must be the same as that coupled to the ATC transponder during flight in?

Back 86

RVSM airspace.

Front 87

RVSM Airspace.

RVSM Required Equipment List

Autopilot with Altitude Hold

Back 87

Must Be Operational

Front 88

RVSM Airspace.

RVSM Required Equipment List

Altitude Alerting System

Back 88

Must Be Operational

Front 89

RVSM Airspace.

RVSM Required Equipment List

Altitude Reporting Transponder (2)

Back 89

One Must Be Operational

Front 90

RVSM Airspace.

RVSM Required Equipment List

Air Data Computers (2)

Back 90

Two Must Be Operational

Front 91

Permissible DC Electrical System Loads.

Ground Operations

To protect the flight compartment CRT displays, the maximum permissible time for ground operations with DCpower only is?

Back 91

5 Minutes.

Front 92

Slats/Flaps.

Enroute use of slats/flaps is?

Prohibited or Not Prohibited

Back 92

Prohibited.

Front 93

Slats/Flaps.

Maximum slats and/or flaps extended altitude:

Back 93

15,000 ft.

Front 94

Taxi time at a stabilized _____% N____ or below may be credited towards the two-minute cool down period.

Back 94

80%

N2

Front 95

During all starts, do not exceed _____%(1) N____ (2) for ____ (3) minutes after start, or until all operating indications are in the _____ (4) range, whichever is longer.

Back 95

1. 75%
2. N1
3. 2 minutes
4. Normal Range

Front 96

What is the maximum engine ITT allowed during all air starts.

Back 96

90°C.

Front 97

Immediate Action Items

Braking Loss/Asymmetry

Back 97

1. Wheel brakes - Release momentarily
   
2. PM will select ANTI-SKID to OFF
   
3. Wheel brakes - Re-apply as required
   
4. Reverse Thrust - Apply maximumuntil stopping assured
   

Front 98

Immediate Action Items

CABIN ALT Msg or EMERGENCY DESCENT

PROCEDURE

Back 98

1. Oxygen masks - Don and 100%
2. Crew communication - Establish
3. Captain assumes PF duties
   

Front 99

Immediate Action Items

DOUBLE-ENGINE FAILURE

Back 99

1. CONT IGNITION - ON
   
2. Airspeed - 240 knots minimum

Front 100

Immediate Action Items

SMOKE/FUMES

Back 100

1. Oxygen masks - Don and 100%
2. Crew communication - Establish
   

Front 101

Immediate Action Items

CR7/CR9 STAB TRIM RUNAWAY

Back 101

1. Control wheel - Assume manual control and override runaway

2. STAB TRIM DISC - Push, hold and release

Front 102

EMERGENCIES WITH IMMEDIATE ACTION ITEMS THAT ARE NOT MEMORY ITEMS

6 EMERGENCIES

Back 102

1. Rudder System Jam
2. Aileron System Jam
3. Elevator System Jam
4. L (R) ENGINE OIL PRESSURE Msg or Oil Pressure Low
5. Uncommanded Yaw Motion
6. Unreliable Airspeed In-Flight

Front 103

Maneuvering Limit Load Factors

Flaps Retracted/Extended

Back 103

Flaps Retracted -1.0 to +2.5G

Flaps Extended 0.0 to + 2.0G

Front 104

When does the Auto Fuel X-Flow turn on?

Back 104

200lbs low and shuts off when wing is 50lbs above.

Front 105

When do the Transfer Injectors come on?

Back 105

94% and they shut off at 97%

Front 106

What is the minimum fuel temp for takeoff?

Back 106

5C

Front 107

What has to be confirmed in the plane?

Back 107

1. Hydraulic SOV
   
2. Fuel Pumps
   
3. Generators
   
4. Fire Push Switches
   
5. Thrust Levers Shutoff
   
6. Guarded Switches

Front 108

What altitude and airspeed do you get the "Too Low Gear" warning on the EGPWS?

Back 108

500ft on the radio altimeter and less than 190kts.

Front 109

Which Hydraulic System operates the manual gear release?

Back 109

Hydraulic System 2.

Front 110

If we lose Hydraulic System 2, will we have the NLG?

Back 110

No

Front 111

What are the maximum steering degrees for the Nose Wheel

Back 111

80 degrees with the tiller and 8 degrees with the rudder peddles.

Front 112

What are the hydraulic systems of the 700?

Back 112

• Primary and Secondary Flight Controls
• Wheel Brakes
• Nosewheel Steering
• Landing Gear Extension and Retraction
• Thrust Reversers
  

Front 113

Which Pumps are EDP and Which are ACMP

Back 113

EDP (Engine Driven Pump)

1a, 2a

ACMP (AC Motor Pump)

3a, 3b, 1b, 2b.

Front 114

When Does the Hydraulic Pressure Relief Valve open and close

Back 114

Opens at 3600psi and closes at 3200psi.

Front 115

What is Normal operating range for Hydraulic Pressure

Back 115

3000psi +/- 200psi

Front 116

What is Normal operating range for the Hydraulic reservoirs?

Back 116

45% - 85%

If lower than 45% refer to the chart in the POH.

Front 117

How do we close the Hydraulic SOV (L/R)

Back 117

1. Engine Fire Push Switch

or

2. Hydraulic SOV Shutoff Switch

Front 118

What conditions must be met before the Auto Pilot can be engaged?

(5 Items)

Back 118

1. AP DISC bar/switch is up
2. At least one yaw damper engaged
3. No unusual aircraft attitudes or rates
4. No FCC faults exist
5. AP Pitch Trim fault will prohibit AP engagement but will not cause an AP disconnect if failure occurs after the AP isengaged

Front 119

What conditions will cause Auto Pilot to be manually disconnected?

(7 Items)

Back 119

1. AP/SP DISC switch pressed
2. TO/GA switch pressed
3. A manual trim switch is moved
4. The AP DISC bar/switch is lowered
5. AP ENG switch is pressed a second time
6. YD DISC is pressed
7. STAB TRIM DISC pressed

Front 120

What conditions will cause Auto Pilot to be automatically disconnected?

Back 120

1. FCC detects a fault
2. Stick pusher is activated
3. Stall condition
4. Both yaw dampers are disconnected
5. Decreasing performance Windshear annunciation
   

Front 121

Do not hold in icing conditions with _____________ extended?

Back 121

Slats or Flaps

Front 122

Immediate Action Items

CR2 STAB TRIM RUNAWAY

Back 122

1. Control wheel - Assume manual control and override runaway

2. Both STAB TRIM DISC - Push, hold and release

3. Captain Assumes PF Duties

4. STAB Trim CH1 cb (2F5) - Open

5. STAB Trim CH2 cb (4A1) - Open

Front 123

Single Pack Operation is limited to?

Back 123

CR2 - 25,000ft

CR7/CR9 - 31,000ft