Memory Items SOP Chapter

Question 1

Memory Item - Double Boxed

3-2 STRUCTURAL WEIGHT LIMITATIONS

CRJ700 Structural Weight Limitations

CRJ900 Structural Weight Limitations

CRJ550 Structural Weight Limitations

Answer 1

CRJ 900, 700, 550

Maximum Taxi and Ramp Weight 85,000 lbs==75250==66000

Maximum Takeoff Weight 84,500 lbs==75000===65000

Maximum Landing Weight 75,100 lbs==67000==61==

Maximum Zero Fuel Weight 70,750 lbs==62300==59000

Minimum Flight Weight 45,000 lbs==42000==42000

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Minimum Operating Empty Weight 39,835 lbs (only crj700)

===================================

Note: The maximum takeoff weight (MTOW) and/or maximum landing weight (MLW) may be further limited due to performance consideration(s).

Question 2

Memory Item - Double Boxed

3-5 OPERATION IN ICING CONDITIONS

3-5.1 Cowl Anti-Ice System

3-5.1.1 Ground Operations

Answer 2

Cowl anti-ice system must be ON when the OAT is 10°C (50°F) or below:

• and visible moisture in any form is present (such as fog with visibility of 1,500 meters [1 mile] or less, rain, snow, sleet and ice crystals)
• when operating on runways, ramps or taxiways where surface snow, ice, standing water, or slush is present

photo

Question 3

Memory Item - Double Boxed

3-5 OPERATION IN ICING CONDITIONS

3-5.1 Cowl Anti-Ice System

3-5.1.3 Flight Operations

Answer 3

Icing conditions exist in-flight at a TAT of 10°C (50°F) or below, and visible moisture in any form is encountered (such as clouds, rain, snow, sleet or ice crystals), except when the SAT is -40°C (-40°F) or below.

The engine cowl anti-ice system must be ON when:

• in icing conditions, or
• ICE is annunciated by the ice detection system

photo

Question 4

Memory Item - Double Boxed

3-5 OPERATION IN ICING CONDITIONS

3-5.3 Wing Anti-Ice System

3-5.3.1 Ground Operations

Answer 4

Wing anti-ice system must be ON for takeoff when the OAT is 5°C (41°F) or below and:

• visible moisture in any form is present (such as fog with visibility of 1,500 meters [1 mile] or less, rain ,snow, sleet and ice crystals)
• the runway is contaminated with surface snow, slush or standing water

When Type II or Type IV anti-icing fluids have been applied:

• wing anti-ice system must only be selected ON, if required, just prior to thrust increase for takeoff

photo

Question 5

Memory Item - Double Boxed

3-5 OPERATION IN ICING CONDITIONS

3-5.3 Wing Anti-Ice System

3-5.3.3 Flight Operations

Answer 5

Icing conditions exist in-flight at a TAT of 10°C (50°F) or below, and visible moisture in any form is encountered (such as clouds, rain, snow, sleet or ice crystals), except when the SAT is -40°C (-40°F) or below.

The wing anti-ice system must be ON when:

• ICE is annunciated by the ice detection system, or
• in icing conditions and the airspeed is less than 230 KIAS

NOTE Do not hold in icing conditions with Slats/Flaps extended.

photo

Question 6

Memory Item - Double Boxed

3-5 OPERATION IN ICING CONDITIONS

3-5.5 Supercooled Large Droplet Icing

Answer 6

Continued operation in areas where supercooled large droplet (SLD) icing conditions exist is prohibited.

SLD icing conditions are indicated by ice accretion on the flight deck side windows.

• wing and cowl anti-icing systems must be ON in SLD icing conditions
• leave icing conditions when side window icing occurs

photo

Question 7

Memory Item - Double Boxed

3-6 COLD WEATHER OPERATIONS

Answer 7

Take-off is prohibited with frost, ice, snow or slush adhering to any critical areas (wings, upper fuselage, horizontal stabilizer, vertical stabilizer, control surfaces, and engine inlets).

Question 8

Memory Item - Double Boxed

3-8 TAILWIND CONDITIONS

The maximum tailwind component approved for takeoff and landing is ====== knots.

Answer 8

10 knots.

Question 9

**** Memory Item - Double Boxed *****

3-13.5 Engines High-Power Schedule Switchlight

Answer 9

Use of the ENGINES HIGH PWR SCHEDULE switchlight is

prohibited.

Question 10

**** Memory Item - Double Boxed *****

3-13.7 Engine Operating Limits

ITT?

Answer 10

Question 11

**** Memory Item - Double Boxed *****

3-13.7 Engine Operating Limits

OIL Pressure?

Answer 11

Question 12

**** Memory Item - Double Boxed *****

3-13.7 Engine Operating Limits

[1] Normal takeoff power and maximum power (two engines) is limited to ——– minutes.

Answer 12

[1] Normal takeoff power and maximum power (two engines) is limited to 5 minutes.

Question 13

**** Memory Item - Double Boxed *****

3-13.7 Engine Operating Limits

[2] APR power (one engine) is limited to————— minutes.

Answer 13

[2] APR power (one engine) is limited to 10 minutes.

Question 14

**** Memory Item - Double Boxed *****

3-13.7 Engine Operating Limits

[3] ITT must be below ———- before attempting to ground start engine.

Answer 14

[3] ITT must be below 120°C before attempting to ground start engine.

Question 15

**** Memory Item - Double Boxed *****

3-13.11 Continuous Engine Ignition

Answer 15

Continuous engine ignition must be used during the following:

• takeoffs and landings on contaminated runways
• flight through moderate or heavier intensity rain
• flight through moderate or heavier intensity turbulence
• flight in the vicinity of thunderstorms

Question 16

**** Memory Item - Double Boxed *****

3-13.12 Reduced (FLEX) Takeoff Thrust

Note: FLEX thrust may be used for takeoff on wet runways, ….

????

Answer 16

Note: FLEX thrust may be used for takeoff on wet runways, provided the flight crew selects “WET” runway performance data on the FMS MCDU (ACARS) PERF WT & BALANCE, CONDITIONS, page 1

Question 17

**** Memory Item - Double Boxed *****

3-13.13.3 CRJ Starter Cranking Limits

All

Answer 17

Question 18

3-13.13.3 CRJ Starter Cranking Limits

Ground Start

Answer 18

Question 19

**** Memory Item - Double Boxed *****

3-13.13.3 CRJ Starter Cranking Limits

Ground , Motoring

Answer 19

Question 20

**** Memory Item - Double Boxed *****

3-13.13.3 CRJ Starter Cranking Limits

Flight

Motoring & Starter

Answer 20

Question 21

**** Memory Item - Double Boxed *****

3-13.13.3 CRJ Starter Cranking Limits

All

Answer 21

Question 22

**** Memory Item - Double Boxed *****

3-15 FUEL

The maximum permissible fuel imbalance between the contents of the left wing tank and the right wing tank are given below:

during takeoff:

Answer 22

• during takeoff: 300 lbs (136 kg)

Question 22

**** Memory Item - Double Boxed *****

3-15 FUEL

The maximum permissible fuel imbalance between the contents of the left wing tank and the right wing tank are given below:

• all other phases of flight:

Answer 22

• all other phases of flight: 800 lbs (363 kg)

Question 23

**** Memory Item - Double Boxed *****

What is Takeoff with a fuel in the center tank limitation?

Answer 23

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

• each main wing tank is above 4,400 lbs, or
• if each main wing tank is less than 4,400 lbs consult the Aircraft Flight Manual’s Limitations section for additional requirements

Question 24

\*\*\*\* Memory Item - Double Boxed \*\*\*\*\* 3-18 MAXIMUM OPERATING SPEED AND MACH NUMBER The **CRJ550/700** Maximum cruise Mach number during flight in RVSM airspace is **????** The **CRJ900** Maximum cruise Mach number during flight in RVSM airspace is **?????**

Answer 24

The CRJ550/700 Maximum cruise Mach number during flight in RVSM airspace is **0.83.** The CRJ900 Maximum cruise Mach number during flight in RVSM airspace is **0.82.**

Question 25

**\*\*\*\* Memory Item - Double Boxed \*\*\*\*\*** 3-20 FLAPS EXTENDED SPEEDS **CRJ550/700** VFE **CRJ900** VFE **Flaps 1**??? KIAS ????? KIAS

Answer 25

**CRJ550/700** VFE **CRJ900** VFE

Question 26

**\*\*\*\* Memory Item - Double Boxed \*\*\*\*\*** 3-20 FLAPS EXTENDED SPEEDS **CRJ550/700** VFE **CRJ900** VFE **Flaps 8**??? KIAS ????? KIAS

Answer 26

**CRJ550/700** VFE **CRJ900** VFE

Question 27

**\*\*\*\* Memory Item - Double Boxed \*\*\*\*\*** 3-20 FLAPS EXTENDED SPEEDS **CRJ550/700** VFE **CRJ900** VFE **Flaps 20**??? KIAS ????? KIAS

Answer 27

**CRJ550/700** VFE **CRJ900** VFE

Question 28

**\*\*\*\* Memory Item - Double Boxed \*\*\*\*\*** 3-20 FLAPS EXTENDED SPEEDS **CRJ550/700** VFE **CRJ900** VFE **Flaps 45**??? KIAS ????? KIAS

Answer 28

**CRJ550/700** VFE **CRJ900** VFE

Question 29

**\*\*\*\* Memory Item - Double Boxed \*\*\*\*\*** 3-21 MAXIMUM LANDING GEAR OPERATING SPEEDS **Extension ?** **Down and Locked ?** **Retraction**?

Answer 29

Extension **220** KIAS Down and Locked **220** KIAS Retraction **200** KIAS

Question 30

**\*\*\*\* Memory Item - Double Boxed \*\*\*\*\*** 3-24 TURBULENCE PENETRATION SPEED Maximum airspeed for turbulence penetration is ----- KIAS or ---------- Mach, whichever is lower.

Answer 30

Maximum airspeed for turbulence penetration is **280** KIAS or **0.75** Mach, whichever is **lower**.

Question 31

**\*\*\*\* Memory Item - Double Boxed \*\*\*\*\*** 3-29 AUTOMATIC FLIGHT CONTROL SYSTEM 3-29.3 **CRJ900** Automatic Flight Control System

Answer 31

Question 32

**\*\*\*\* Memory Item - Double Boxed \*\*\*\*\*** 3-29 AUTOMATIC FLIGHT CONTROL SYSTEM 3-29.1 CRJ550/700 Automatic Flight Control System

Answer 32

Question 33

**\*\*\*\* Memory Item - Double Boxed \*\*\*\*\*** 3-30.3 Permissible DC Electrical System Loads **Ground Operation:** • to protect the CRT displays, the maximum permissible time for ground operations with DC power is **??????**

Answer 33

**Ground Operation:** • to protect the CRT displays, the maximum permissible time for ground operations with DC power is **5 minutes.**

Question 34

**\*\*\*\* Memory Item - Double Boxed \*\*\*\*\*** 3-31 FLIGHT CONTROLS – LIFT/DRAG DEVICES **3-31.1 Slats/Flaps** Is there any limitation?

Answer 34

1- **_Enroute_** use of Slats/Flaps is **prohibited**. 2- Flight with Slats/Flaps **_extended_** at **altitudes above 15,000’** is **prohibited**.

Question 35

**\*\*\*\* Memory Item - Double Boxed \*\*\*\*\*** **3-31.3 Flight Spoilers** Is there any limitation?

Answer 35

1- Flight spoilers must not be extended in-flight **below an altitude of 300’** AGL 2- To ensure adequate maneuver margins, flight spoilers must not be extended in-flight at airspeeds below the recommended approach speed plus **10 KIAS.**