Boxed Memory Items

Question 1

The airplane is certified in the transport category for day and night operations under what conditions?

Answer 1

VFR and IFR
Flight in icing conditions

Equipment and instruments must be approved, installed, and operable.

Question 2

What is the maximum taxi and ramp weight for the CRJ 550 airplane?

Answer 2

66,000 lbs

This weight limit is crucial for ground operations.

Question 3

What is the maximum takeoff weight for the CRJ 550 airplane?

Answer 3

65,000 lbs

Exceeding this weight can compromise safety during takeoff.

Question 4

What is the maximum landing weight for the CRJ 550 airplane?

Answer 4

61,000 lbs

This limit ensures safe landing performance.

Question 5

What is the maximum zero fuel weight for the CRJ 550 airplane?

Answer 5

59,000 lbs

This weight is critical for structural integrity.

Question 6

What is the minimum flight weight for the airplane?

Answer 6

42,000 lbs

This weight ensures proper flight characteristics.

Question 7

What is the maximum airport pressure altitude for takeoff and landing?

Answer 7

8,000’

This altitude limit is important for performance calculations.

Question 8

What is the maximum operating altitude for the airplane?

Answer 8

41,000’

This altitude is critical for flight planning.

Question 9

What is the maximum ambient air temperature approved for takeoff and landing?

Answer 9

ISA +35°C

Exceeding this temperature can affect aircraft performance.

Question 10

What is the minimum ambient temperature approved for takeoff?

Answer 10

-40°C (-40°F)

This temperature is crucial for engine performance.

Question 11

When must the cowl anti-ice system be ON during ground operations?

Answer 11

• OAT is 10°C (50°F) or below with:
  Visible moisture present and/or operating on contaminated surfaces

This prevents ice accumulation on the engines.

Question 12

When must the wing anti-ice system be ON for takeoff?

Answer 12

• OAT is 5°C (41°F) or below and:
• Visible moisture present and/or
  Runway contaminated with snow, slush, or water.
  If using type II or type IV anti-ice fluid, wing anti-ice should not be turned on until just prior to thrust increase for takeoff.

This is essential for safe takeoff in icy conditions.

Question 13

What is the maximum runway slope approved for takeoff and landing?

Answer 13

+2% (uphill)
-2% (downhill)

These limits ensure safe operations on sloped runways.

Question 14

What is the maximum tailwind component approved for takeoff and landing?

Answer 14

10 knots

Exceeding this can affect aircraft performance during takeoff and landing.

Question 15

What is the forward cargo weight limit?

Answer 15

1000 lbs

This limit is important for weight distribution.

Question 16

What is the aft cargo weight limit?

Answer 16

• 3740 lbs (with restrictions)
• 2710 lbs (without restrictions)

Proper weight distribution is critical for flight safety.

Question 17

What engines are used in the aircraft?

Answer 17

Two (2) General Electric CF34-8C5B1 engines

These engines are designed for regional jet performance.

Question 18

What is the maximum N1 for the engines?

Answer 18

99.5%

This is the maximum allowable engine speed.

Question 19

What is the normal N1 range for the engines?

Answer 19

0%-99.4%

Operating within this range ensures engine efficiency.

Question 20

What is the maximum oil temperature for the engines?

Answer 20

164 degrees Celsius

Exceeding this temperature can lead to engine damage.

Question 21

What is the normal oil temperature range for the engines?

Answer 21

-40-155 degrees Celsius

This range is essential for proper engine operation.

Question 22

What is the maximum ITT temperature for ground or assisted air start?

Answer 22

815 degrees Celsius

This limit is crucial for engine start procedures.

Question 23

What is the maximum ITT continuous temperature for the engines?

Answer 23

960 degrees Celsius

This temperature must not be exceeded during normal operations.

Question 24

What must be done during all starts regarding N1?

Answer 24

Do not exceed 75% N1 for two (2) minutes after start

This ensures engine stability during startup.

Question 25

Continuous engine ignition must be used during which conditions?

Answer 25

* Takeoffs and landings on contaminated runways * Flight through moderate or heavier rain * Flight through moderate or heavier turbulence * Flight in the vicinity of thunderstorms ## Footnote This enhances safety during critical flight phases.

Question 26

The use of Reduced/FLEX thrust for takeoff is not authorized when?

Answer 26

* Wing and/or cowl anti-ice bleeds are in use * Runway is contaminated (FLEX is allowed if runway is just wet and crew selects "WET" on the MCDU (ACARS) PERF WT & BALANCE) * Warnings of windshear exist * Antiskid system is inoperative * Engine can’t achieve full rated thrust ## Footnote These conditions can affect aircraft performance.

Question 27

What is the maximum permissible fuel imbalance during takeoff?

Answer 27

300 lbs ## Footnote This limit is crucial for maintaining aircraft balance.

Question 28

What is the maximum permissible fuel imbalance during all other phases of flight?

Answer 28

800 lbs ## Footnote This ensures safe flight operations.

Question 29

Takeoff with a fuel load in excess of 500 lbs in the center tank is not permitted unless?

Answer 29

Each main wing tank is above 4,400 lbs of fuel ## Footnote Consult the AFM limitations section for further requirements.

Question 30

CRJ 700 Maximum Taxi and Ramp Weight

Answer 30

75,250 lbs

Question 31

CRJ 700 Maximum Takeoff Weight

Answer 31

75,000 lbs

Question 32

CRJ 700 Maximum Landing Weight

Answer 32

67,000 lbs

Question 33

CRJ 700 Maximum Zero Fuel Weight

Answer 33

62,300 lbs

Question 34

When must the cowl anti ice be on during flight operations?

Answer 34

When TAT is at or less than 10C and in visible moisture or when ice is annunciated. The exception is when SAT is -40C or below.

Question 35

When should wing anti-ice be turned on in flight?

Answer 35

With TAT at or below 10C in visible moisture (except when SAT is at or below -40C) and: Ice is annunciated by the ice detection system or in icing conditions below 230 KIAS. Note: Do not hold in icing conditions.

Question 36

How is SLD icing conditions detected? What anti-ice system(s) are required?

Answer 36

Ice begins to accumulate on the side windows. Both cowl and wing anti-ice should be turned on. Leave these icing conditions when ice begins to accumulate on the side windows.

Question 37

Max Forward Cargo Weight

Answer 37

1000 lbs

Question 38

Max Aft Cargo Weight

Answer 38

3740 (2710 69pax configuration)

Question 39

Max Oil Pressure During Ground Start

Answer 39

182 psi. 95 psi for no more than 10 minutes. (Oil pressure may peak beyond 182 psi during start and will be displayed as amber dashes if it does).

Question 40

Minimum Oil with Engine Off

Answer 40

40%

Question 41

Starter Limitation 1 & 2 attempts on the ground?

Answer 41

90 Seconds 10 Seconds Cool Down

Question 42

Starter Limitation Attempts 3-5 on the Ground?

Answer 42

90 seconds 5 minutes Cool Down

Question 43

Engine Start or Motoring in Flight 1st Attempt

Answer 43

120 Seconds 10 Second Cool Down

Question 44

Engine Start or Motoring in Flight 2-5 attempts:

Answer 44

60 Seconds 5 Minute Cool Down

Question 45

Engine Motoring on the Ground 1st Attempt

Answer 45

90 Seconds 5 Minute Cool Down

Question 46

Engine Motoring on the Ground 2-5 Attempts

Answer 46

30 Seconds 5 Minute Cool Down

Question 47

Max Altitude for Windmill Start. Min Speed and N2

Answer 47

25,000' 250 KIAS 7.2% N2

Question 48

Max Altitude for Starter Assisted Engine Start and Minimum Speed and Minimum N2

Answer 48

21,000' Vref 45% N2

Question 49

Max Altitude for Rapid Relight and Speed

Answer 49

10,000' and 200 KIAS

Question 50

Max Fuel in Main Tanks with Pressure Fueling

Answer 50

7492 lbs

Question 51

Max Fuel in Main Tanks with Gravity Fueling

Answer 51

7290 lbs

Question 52

Max Fuel in Center Tank with Pressure Fueling

Answer 52

4610 lbs

Question 53

Max Total Fuel with Pressure Fueling

Answer 53

19594 lbs

Question 54

Minimum Fuel Temp for Takeoff

Answer 54

5C

Question 55

Minimum Jet A Bulk Fuel Temperature for Takeoff

Answer 55

-30C

Question 56

Minimum Jet A Bulk Fuel Temperature During Cruise

Answer 56

-40C

Question 57

Max Oil Consumption

Answer 57

.05 Gallons per Hour

Question 58

Minimum Time to Wait After Engine Shutdown Before Checking Oil Level

Answer 58

5 Minutes

Question 59

Minimum Time to Wait After Engine Shutdown Before Oil Servicing

Answer 59

15 Minutes

Question 60

What Kind of APU Does the Aircraft Have?

Answer 60

Allied Signal RE 220

Question 61

Minimum Ambient Temp To Start APU

Answer 61

-40C

Question 62

Max APU Start Temperature

Answer 62

692C

Question 63

Max APU Temperature

Answer 63

1038C

Question 64

APU Starter Limitations

Answer 64

3 Start Attempts Within One Hour with 2 Minute Cooldown Between Attempts

Question 65

Max Altitude for APU Bleed Air Extraction

Answer 65

25,000'

Question 66

Max Load on APU

Answer 66

40 KVA

Question 67

Max Altitude for APU Start

Answer 67

37,000'

Question 68

Max Altitude for APU Use

Answer 68

41,000'

Question 69

Max Speed in RVSM Airspace

Answer 69

Mach .83

Question 70

Flap Speeds

Answer 70

Flap 1: 230 Flap 8: 230 Flap 20: 230 Flap 30: 185 Flap 45: 170

Question 71

Max Speed for Gear Extension, Down & Locked

Answer 71

220 KIAS

Question 72

Max Speed for Gear Retraction

Answer 72

200 KIAS

Question 73

Max Tire Speed

Answer 73

182 KIAS

Question 74

Max Speed for ADG Use

Answer 74

Vmo/Mmo

Question 75

Max Turbulent Air Penetration Speed

Answer 75

280 KIAS or Mach .75 Whichever is Lower

Question 76

Max Speed for Windshield Wipers

Answer 76

250 KIAS

Question 77

Max Load with Flaps Retracted

Answer 77

-1.0 to 2.5 G

Question 78

Max Load with Flaps Extended

Answer 78

0.0-2.0 G

Question 79

Max Pressure Relief Differential

Answer 79

8.7 psi

Question 80

Max Negative Pressure Differential

Answer 80

-.5 psi

Question 81

Max Pressure Differential During Taxi, Takeoff, and Landing

Answer 81

.1 psi

Question 82

Max Altitude to Use "EMERG DEPRESS":

Answer 82

15,000'

Question 83

Max Altitude for Single Pack Operation

Answer 83

31,000'

Question 84

Minimum 02 2 Crew Members

Answer 84

810 psi

Question 85

Minimum 02 With Jump Seat

Answer 85

1110 psi

Question 86

Miniumum Auto Pilot Altitude During Takeoff

Answer 86

600' AGL

Question 87

Minimum Altitude for Auto Pilot Use During Non-Precision Approach

Answer 87

400' AGL

Question 88

Minimum Altitude for Autopilot Use During Precision Approach with Pitch Up To 3.5 Degrees

Answer 88

80' AGL

Question 89

Minimum Altitude for Autopilot Use During Precision Approach with Pitch Between 3.5-4.0 Degrees

Answer 89

120' AGL

Question 90

Max Load for IDG's

Answer 90

40KVA

Question 91

Max TRU Load

Answer 91

120 Amps

Question 92

Max Time on DC Power on Ground

Answer 92

5 Minutes (To Protect CRT Screens)

Question 93

Max Altitude for Slats/Flaps

Answer 93

15,000'

Question 94

Spoilierons Min Altitude

Answer 94

300' AGL

Question 95

Spoilerons Minimum Speed

Answer 95

No Less Than Vref plus 10 KIAS

Question 96

Max Speed with Full Reverse Thrust

Answer 96

75 KIAS

Question 97

Max Reverse Idle Speed

Answer 97

60 KIAS

Question 98

Max Time with Taxi Lights On After A/C is Stopped

Answer 98

10 Minutes