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2026-2027
Minimum Flight Weight (CRJ-550 and CRJ-700)
ANSWERS: 42,000 LBS
Maximum Airport Pressure Altitude
ANSWERS: 8,000 Feet
Maximum Operating Altitude
ANSWERS: 41,000 Feet
Maximum Ambient Air Temperature Approved For Takeoff and Landing
ANSWERS: ISA +35C
, Minimum Ambient Temperature Approved For Takeoff
ANSWERS: -40C (-40F)
When Must Cowl Anti-Ice Be On For Ground Operations?
[BOXED]
ANSWERS:
• OAT Is 10C or Below
• Visible Moisture in any form
• When Operating on Runways, Ramps, or Taxiways where surface snow,
ice, standing water, or slush is present.
When Must Cowl Anti-Ice Be On For Flight Operations?
[BOXED]
ANSWERS: Flight in Visible Moisture in any form from TAT 10C or Below
(Except SAT
-40C or Below):
• Icing Conditions
• ICE Annunciated by Ice Detection System
,When Must Wing Anti-Ice Be On For Ground Operations?
[BOXED]
For Takeoff when the OAT is 5C or below and:
• Visible Moisture present in any form
• Runway Contaminated (Snow, Slush, Water)
When Type II or Type IV Anti-Icing have been applied:
• Wing Anti-Ice On, If Required, Just Prior to T/O Thrust
When Must Wing Anti-ice Be On For Flight Operations?
[BOXED]
Icing Conditions at TAT 10C or Below (Except Below SAT -40C) and
Visible Moisture is encountered:
Wing Anti-Ice Must Be ON When:
Ice Annunciated by Ice Detection System
Icing Conditions and A/S is less than 230 KIAS
(Don't Hold In Ice with Slats/Flaps Extended)
Can you continue a flight into an area where supercooled large droplet
icing conditions exist?
[BOXED]
No, It is Prohibited
, How can you tell you are in an area with supercooled large droplet
icing and what should you do?
[BOXED]
Ice Accretion on the flight deck side windows:
Wing and Cowl Anti-icing systems must be On
Leave icing conditions
Can you takeoff with frost, ice, snow, or slush adhering to any critical
areas (wings, upper fuselage, horizontal stabilizer, vertical stabilizer,
control surfaces, and engine inlets)?
No, It is Prohibited
Takeoff is permitted with frost adhering to:
Upper Fuselage if it is possible to distinguish surface features
Maximum 1/8 In of frost on the underside of the wing caused by cold
soaked fuel