GOJET SOP chapter 3 limitations and memory
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CRJ700 Structural Weight Limitations Answer: Weights Maximum
Taxi and Ramp Weight 75,250 Ibs
Maximum Takeoff Weight 75,000 lbs.
Maximum Landing Weight 67,000 lbs.
Maximum Zero Fuel Weight 62,300 lbs.
Minimum flight weight 42,000 lbs.
Minimum operating weight 39,835 lbs.
CRJ550 Structural Weight Limitations Answer: Maximum Taxi and
Ramp Weight 66,000 lbs
Maximum Takeoff Weight 65,000 lbs.
Maximum Landing Weight 61,000 lbs.
Maximum Zero Fuel Weight 59,000 Ibs.
Minimum Flight Weight 42,000 lbs.
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CRJ900 Structural Weight Limitations Answer: Maximum Taxi and
Ramp Weight 85,000 lbs Maximum Takeoff Weight 84,500 lbs.
Maximum Landing Weight 75,100 lbs. Maximum Zero Fuel Weight
70,750 Ibs. Minimum Flight Weight 45,000 Ibs.
Weight Limitations Note: Answer: The maximum takeoff weight
(MTOW) and/or maximum landing weight (MLW) may be further
limited due to performance consideration(s).
RVSM REQUIRED EQUIPMENT LIST Answer: EQUIPMENT
AUTOPILOT (1)
ALTITUDE ALERTING SYSTEM (1)
ALTITUDE REPORTING TRANSPONDER (2)
AIR DATA COMPUTERS (2)
Kinds of Airplane Operation Answer: VFR and IFR Flight in icing
conditions
Maximum airport pressure altitude for takeoff and landing Answer:
8,000'
Maximum operating altitude is Answer: Maximum 41,000'
The maximum ambient air temperature approved for takeoff and
landing Answer: ISA +35°C
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The minimum ambient temperature approved for takeoff Answer: -
40°C (-40°F)
Ground Cowl anti-ice system must be ON when Answer: 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
The engine cowl anti-ice system must be ON in flight when:
Answer: in icing conditions, or ICE is annunciated by the ice
detection system
Cowl Anti-Ice System Icing conditions in flight Answer: exist in-
flight at a TAT of 10°C (50°F) or below, and visible moisture in any
form is encountered (such as douds, rain, snow, sleet or ice crystals),
except when the SAT is -40°C (-40°F) or below.
Wing anti-ice system must be ON for takeoff when Answer: 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
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