Upgrade Knowledge Prep - Ground and Takeoff Flashcards
When is the Originating Check required to be accomplished? (SOPM 04-01.2)
- Accepting an aircraft,
- Aircraft was left unattended by the flight deck crew,
- Aircraft was completely powered down.
During the Safety Check flow, after a crew swap where the aircraft remains powered, are you required to reset the hydraulic pumps to the OFF position? (SOPM 04-01.8)
- No
- Hydraulic pump 3A is off because of shutdown check.
- Rest of the pumps are set to Auto in order to provide brake accumulator pressure
When is the minimum oxygen pressure level required to be at or above 1650 psi? (SOPM 04-01.58)
• The minimum is 1650 psi for dispatch from the United States to an international destination.
During the Originating Check, the captain can select the windshield heat to OFF above what temperature? (SOPM 04-01.58)
When ambient temperatures are above 30°C. The selection of windshield heat to LOW may be delayed until the After Takeoff Check.
What is the procedure when a CARGO OVHT caution message is displayed during the preflight phase? Prior to takeoff? In flight? (SOPM 04-02.13)
• During the preflight stage, keep the CARGO Switch in the COND AIR position.
• Just prior to takeoff, move the CARGO Switch from COND AIR to FAN. Ensure the
CARGO OVHT caution message extinguishes. Approximately 30 minutes after takeoff, return the CARGO Switch to the COND AIR position. When the CARGO OVHT caution illuminates, comply with the QRH procedures.
Are you prohibited from carrying animals in the cargo bin with a CARGO OVHT message? (SOPM 04-02.13)
• No.
- When are you required to calculate the fuel load using FliteView – Manifest? (SOPM 04-02.13)
• When there is fuel in the center tank and the two main tanks are not full, the allowable fuel load must be calculated using the manifest application in FlightView.
The APU must be started how many minutes prior to pushback? (SOPM 04-16.5)
• The APU start is delayed until 10 minutes prior to pushback, unless required for AC power or for passenger comfort.
Prior to closing the MCD, what must the crew check? (SOPM 04-03.6)
• When ground air condition was being used, ensure low-pressure air has been disconnected.
Before the first flight of the day, prior to starting a cold soaked engine, what is required? (SOPM 04-03.16)
Prior to starting, the engines must be motored for 60 seconds and fan rotation verified before the engine start is initiated.
- Cold soaked: Aircraft has been parked in -30°C or colder for more than 8 hours.
Prior to departure in a cold soaked airplane, the thrust reverser deploy and stow cycles must be less than how many seconds in the CRJ 200? (SOPM 04-03.16)
- CRJ200: Below 5 seconds
* CRJ7/900: Below 2 seconds
Where is the CRJ 200 cross bleed engine start procedure located? How is it accomplished?
(QRH SUPP 2-1)
• The procedure is located in QRH Volume 1 Engine Start – Cross Bleed o APU LCV: Close,
o 10th Stage Bleed Valve (on operating engine): OPEN,
o ECS Page: Select and Monitor,
o Thrust Lever (for operating engine): Advance as required to achieve a minimum
of 60 PSI bleed air pressure (approx. 85% N2),
o LorRENG–Start
o If thrust lever was advanced to achieve 60 psi, reduce to idle after starter cutout
When is a two-engine taxi required? (SOPM 04-04.1)
- Conducting FFOD checks
- Operating on a contaminated or congested ramp or taxiway(s)
- Short taxi out (<5 min)
- Captain’s discretion
When is cowl anti-ice required for taxi? (SOPM 04-04.18)
• When OAT is ≤ 10°C and:
o Visible moisture is present, or
o Visibility is ≤ 1mile, or
o When operating on surfaces where ice, snow, standing water, or slush is present.
When is wing anti-ice required for taxi? How many minutes prior to takeoff must they be selected on? (SOPM 04-04.18)
• In the CRJ200:
o When OAT ≤ 5° C, with or without visible moisture, and
o Aircraft has not been anti-iced with Type II or IV fluid
o After second engine start and at least two minutes prior to takeoff