Memory Items SOP Chapter Flashcards
Memory Item - Double Boxed
3-2 STRUCTURAL WEIGHT LIMITATIONS
CRJ700 Structural Weight Limitations
CRJ900 Structural Weight Limitations
CRJ550 Structural Weight Limitations
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)
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Note: The maximum takeoff weight (MTOW) and/or maximum landing weight (MLW) may be further limited due to performance consideration(s).
Memory Item - Double Boxed
3-5 OPERATION IN ICING CONDITIONS
3-5.1 Cowl Anti-Ice System
3-5.1.1 Ground Operations
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
Memory Item - Double Boxed
3-5 OPERATION IN ICING CONDITIONS
3-5.1 Cowl Anti-Ice System
3-5.1.3 Flight Operations
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
Memory Item - Double Boxed
3-5 OPERATION IN ICING CONDITIONS
3-5.3 Wing Anti-Ice System
3-5.3.1 Ground Operations
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
Memory Item - Double Boxed
3-5 OPERATION IN ICING CONDITIONS
3-5.3 Wing Anti-Ice System
3-5.3.3 Flight Operations
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.
Memory Item - Double Boxed
3-5 OPERATION IN ICING CONDITIONS
3-5.5 Supercooled Large Droplet Icing
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
Memory Item - Double Boxed
3-6 COLD WEATHER OPERATIONS
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).
Memory Item - Double Boxed
3-8 TAILWIND CONDITIONS
The maximum tailwind component approved for takeoff and landing is ====== knots.
10 knots.
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3-13.5 Engines High-Power Schedule Switchlight
Use of the ENGINES HIGH PWR SCHEDULE switchlight is
prohibited.
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3-13.7 Engine Operating Limits
ITT?
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3-13.7 Engine Operating Limits
OIL Pressure?
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3-13.7 Engine Operating Limits
[1] Normal takeoff power and maximum power (two engines) is limited to ——– minutes.
[1] Normal takeoff power and maximum power (two engines) is limited to 5 minutes.
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3-13.7 Engine Operating Limits
[2] APR power (one engine) is limited to————— minutes.
[2] APR power (one engine) is limited to 10 minutes.
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3-13.7 Engine Operating Limits
[3] ITT must be below ———- before attempting to ground start engine.
[3] ITT must be below 120°C before attempting to ground start engine.
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3-13.11 Continuous Engine Ignition
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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3-13.12 Reduced (FLEX) Takeoff Thrust
Note: FLEX thrust may be used for takeoff on wet runways, ….
????
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
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3-13.13.3 CRJ Starter Cranking Limits
All
3-13.13.3 CRJ Starter Cranking Limits
Ground Start
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3-13.13.3 CRJ Starter Cranking Limits
Ground , Motoring
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3-13.13.3 CRJ Starter Cranking Limits
Flight
Motoring & Starter
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3-13.13.3 CRJ Starter Cranking Limits
All
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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:
• during takeoff: 300 lbs (136 kg)
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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:
• all other phases of flight: 800 lbs (363 kg)
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What is Takeoff with a fuel in the center tank limitation?
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
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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 ?????
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.
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3-20 FLAPS EXTENDED SPEEDS
CRJ550/700 VFE CRJ900 VFE
Flaps 1??? KIAS ????? KIAS
CRJ550/700 VFE CRJ900 VFE
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3-20 FLAPS EXTENDED SPEEDS
CRJ550/700 VFE CRJ900 VFE
Flaps 8??? KIAS ????? KIAS
CRJ550/700 VFE CRJ900 VFE
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3-20 FLAPS EXTENDED SPEEDS
CRJ550/700 VFE CRJ900 VFE
Flaps 20??? KIAS ????? KIAS
CRJ550/700 VFE CRJ900 VFE
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3-20 FLAPS EXTENDED SPEEDS
CRJ550/700 VFE CRJ900 VFE
Flaps 45??? KIAS ????? KIAS
CRJ550/700 VFE CRJ900 VFE
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3-21 MAXIMUM LANDING GEAR OPERATING SPEEDS
Extension ?
Down and Locked ?
Retraction?
Extension 220 KIAS
Down and Locked 220 KIAS
Retraction 200 KIAS
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3-24 TURBULENCE PENETRATION SPEED
Maximum airspeed for turbulence penetration is —– KIAS or ———- Mach, whichever is lower.
Maximum airspeed for turbulence penetration is 280 KIAS or 0.75 Mach, whichever is lower.
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3-29 AUTOMATIC FLIGHT CONTROL SYSTEM
3-29.3 CRJ900 Automatic Flight Control System
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3-29 AUTOMATIC FLIGHT CONTROL SYSTEM
3-29.1 CRJ550/700 Automatic Flight Control System
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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 ??????
Ground Operation:
• to protect the CRT displays, the maximum permissible time for ground operations with DC power is 5 minutes.
**** Memory Item - Double Boxed *****
3-31 FLIGHT CONTROLS – LIFT/DRAG DEVICES
3-31.1 Slats/Flaps
Is there any limitation?
1- Enroute use of Slats/Flaps is prohibited.
2- Flight with Slats/Flaps extended at altitudes above 15,000’ is prohibited.
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3-31.3 Flight Spoilers
Is there any limitation?
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.
