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GoJet SOP > Memory Items SOP Chapter > Flashcards

Memory Items SOP Chapter Flashcards

1
Q

Memory Item - Double Boxed

3-2 STRUCTURAL WEIGHT LIMITATIONS

CRJ700 Structural Weight Limitations

CRJ900 Structural Weight Limitations

CRJ550 Structural Weight Limitations

A

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

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

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).

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2
Q

Memory Item - Double Boxed

3-5 OPERATION IN ICING CONDITIONS

3-5.1 Cowl Anti-Ice System

3-5.1.1 Ground Operations

A

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

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3
Q

Memory Item - Double Boxed

3-5 OPERATION IN ICING CONDITIONS

3-5.1 Cowl Anti-Ice System

3-5.1.3 Flight Operations

A

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

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4
Q

Memory Item - Double Boxed

3-5 OPERATION IN ICING CONDITIONS

3-5.3 Wing Anti-Ice System

3-5.3.1 Ground Operations

A

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

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5
Q

Memory Item - Double Boxed

3-5 OPERATION IN ICING CONDITIONS

3-5.3 Wing Anti-Ice System

3-5.3.3 Flight Operations

A

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

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6
Q

Memory Item - Double Boxed

3-5 OPERATION IN ICING CONDITIONS

3-5.5 Supercooled Large Droplet Icing

A

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

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7
Q

Memory Item - Double Boxed

3-6 COLD WEATHER OPERATIONS

A

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).

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8
Q

Memory Item - Double Boxed

3-8 TAILWIND CONDITIONS

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

A

10 knots.

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9
Q

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

3-13.5 Engines High-Power Schedule Switchlight

A

Use of the ENGINES HIGH PWR SCHEDULE switchlight is

prohibited.

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10
Q

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

3-13.7 Engine Operating Limits

ITT?

A
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11
Q

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

3-13.7 Engine Operating Limits

OIL Pressure?

A
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12
Q

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

3-13.7 Engine Operating Limits

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

A

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

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13
Q

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

3-13.7 Engine Operating Limits

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

A

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

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14
Q

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

3-13.7 Engine Operating Limits

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

A

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

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15
Q

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

3-13.11 Continuous Engine Ignition

A

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
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16
Q

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

3-13.12 Reduced (FLEX) Takeoff Thrust

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

????

A

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

17
Q

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

3-13.13.3 CRJ Starter Cranking Limits

All

A
18
Q

3-13.13.3 CRJ Starter Cranking Limits

Ground Start

A
19
Q

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

3-13.13.3 CRJ Starter Cranking Limits

Ground , Motoring

A
20
Q

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3-13.13.3 CRJ Starter Cranking Limits

Flight

Motoring & Starter

A
21
Q

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3-13.13.3 CRJ Starter Cranking Limits

All

A
22
Q

**** 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:

A

• during takeoff: 300 lbs (136 kg)

22
Q

**** 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:

A

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

23
Q

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

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

A

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
24
Q

**** 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 ?????

A

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.

25
Q

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

3-20 FLAPS EXTENDED SPEEDS

CRJ550/700 VFE CRJ900 VFE

Flaps 1??? KIAS ????? KIAS

A

CRJ550/700 VFE CRJ900 VFE

26
Q

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

3-20 FLAPS EXTENDED SPEEDS

CRJ550/700 VFE CRJ900 VFE

Flaps 8??? KIAS ????? KIAS

A

CRJ550/700 VFE CRJ900 VFE

27
Q

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

3-20 FLAPS EXTENDED SPEEDS

CRJ550/700 VFE CRJ900 VFE

Flaps 20??? KIAS ????? KIAS

A

CRJ550/700 VFE CRJ900 VFE

28
Q

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

3-20 FLAPS EXTENDED SPEEDS

CRJ550/700 VFE CRJ900 VFE

Flaps 45??? KIAS ????? KIAS

A

CRJ550/700 VFE CRJ900 VFE

29
Q

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

3-21 MAXIMUM LANDING GEAR OPERATING SPEEDS

Extension ?

Down and Locked ?

Retraction?

A

Extension 220 KIAS

Down and Locked 220 KIAS

Retraction 200 KIAS

30
Q

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3-24 TURBULENCE PENETRATION SPEED

Maximum airspeed for turbulence penetration is —– KIAS or ———- Mach, whichever is lower.

A

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

31
Q

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3-29 AUTOMATIC FLIGHT CONTROL SYSTEM

3-29.3 CRJ900 Automatic Flight Control System

A
32
Q

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3-29 AUTOMATIC FLIGHT CONTROL SYSTEM

3-29.1 CRJ550/700 Automatic Flight Control System

A
33
Q

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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 ??????

A

Ground Operation:

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

34
Q

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

3-31 FLIGHT CONTROLS – LIFT/DRAG DEVICES

3-31.1 Slats/Flaps

Is there any limitation?

A

1- Enroute use of Slats/Flaps is prohibited.

2- Flight with Slats/Flaps extended at altitudes above 15,000’ is prohibited.

35
Q

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

3-31.3 Flight Spoilers

Is there any limitation?

A

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.

GoJet SOP (13 decks)

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