SOP Flashcards
Standard Operating Procedures consist of
inspections, preparations, and normal procedures. All items of a given procedure are listed in a sequence that follows a standardized scan of the cockpit panels, unless that sequence goes against the action priority logic, to ensure that all actions are performed in the most efficient way.
PRO-NOR-SOP-01 P 1/2
The flight crew must also verify ISA deviations and
enroute icing conditions, and must consider the possibility of holding due to weather at the destination.
PRO-NOR-SOP-02 P 1/4
Do not pressurize the green hydraulic system without.
clearance from ground personnel if any gear door is open.
PRO-NOR-SOP-03 P 1/2
During walkaround, observe any possible abnormalities on the landing gear status: • Wheels and tires status (cut, wear, cracks) • Safety pins are removed • Brakes status (brake wear pin length with parking brake ON) and:
Length of oleo. Any difference between the two main landing gears must be reported. Typically, a 10 bar low pressure in oleo, leading to 60 mm oleo reduction, decreases the tail clearance by approximately 1 ft.
PR-NP-SOP-50 P 1/2
To observe any possible abnormalities on the engines:
‐ Fan blades, turbine exhaust, engine cowl and pylon status ‐ Access door closed ‐ Correct closure/latching condition of the fan cowl doors
PR-NP-SOP-50 P 1/2
4,000 ft < optimum flight level =
5 % fuel penalty
PRO NOR SOP 02 p 2/4
If flight above optimum (up to ceiling) is intended, the increase in consumption may reach
3 %.
PRO NOR SOP 02
The aircraft is: ‐ in TRANSIT STOP when the last check list
‐ in SECURED STOP when the last check list
performed by the flight crew is the PARKING C/L
performed by the flight crew is the SECURING THE AIRCRAFTC/L
FCTM PR-NP-GEN P 2/4
Check that the oil quantity is : ‐ At or above——- for flight time below 10 h, or ‐ At or above ——— for ETOPS flights or for flight time at or above 10 h.
18 QT
19 QT
PRO-NOR-SOP-04 P 9/12
Minimum Bottle Pressure to Cover: ‐ Preflight checks ‐ The use of oxygen, when only one flight crewmember is in the cockpit ‐ Unusable quantity (to ensure regulator operation with minimum pressure) ‐ Normal system leakage ‐ The most demanding case among the following:
• Protection after loss of cabin pressure, with mask regulator on NORMAL (diluted oxygen): ▪ During emergency descent for all crewmembers and observers for 15 min , ▪ During cruise at FL 100 for two crewmembers for 105 min. • Protection against smoke with 100 % oxygen for all flight crewmembers and observers during 15 min at 8 000 ft cabin altitude.
LIM-OXY P 1/4
If the aircraft has been electrically supplied during the last 6 h
BAT 1 pb-sw, BAT 2 pb-sw and APU BAT pb-sw………………………………………………………..AUTO Note: In case of APU start on battery only, perform the following check: BAT 1 pb-sw, BAT 2 pb-sw and APU BAT pb-sw…………………………………………..AUTO BAT 1 and 2 and APU BAT………………………………………………..CHECK ABOVE 23.5 V If one battery voltage is lower than 23.5 V, there is a risk that APU start aborts. A charging cycle of the battery is required.
PRO-NOR-SOP-04 P 2/12
APU START - In cold weather conditions (below approx. 10 °C), the flight crew may observe a bleed pressure up to
12 PSI with possible fluctuations on the APU SD page and BLEED SD page.
PRO-NOR-SOP-04 P 4/12
At electrical power-up, the FMGSs and FCU run through various internal tests. Allow enough time
(3 min) for tests’ completion, and do not start to press pushbuttons until the tests are over. If the “PLEASE WAIT” message appears, do not press any MCDU key until the message clears.
PRO-NOR-SOP-04 P 5/12
The parking brake must be set to ON during the exterior walkaround, in order to
enable the flight crew to check brake wear indicators.
PRO-NOR-SOP-05 P 1/14
COMPLETE IRS ALIGNMENT
The IR mode selectors must be OFF for more than 5 s. Then, the flight crew sets
the IR mode selectors to the NAV mode
PR-NP-SOP-60 P 1/8