SOP Notes Flashcards
The autopilot perfectly trims the airplane in pitch, but does not trim
for roll and yaw.
“Holding” the checklist:
— When the Captain elects not to accomplish an item on the checklist when it is called, s/he will state,
“Stop checklist”.
Continuing the checklist:
— When the Captain desires to continue the checklist, s/he will state,
“Continue the checklist”. The checklist will then resume with the item at which it was held.
Use of TCS, or disregarding flight director commands while operating in FLCH (SPD E),
may result in speed deviations.
To read the battery voltage, the GPU pushbutton must be
disconnected (pushed OUT).
BATT1 / BATT 2 . . . . . . . . . 1-ON / 2-AUTO
— Ensure aircraft is not moved until IESS is initialized. Initialization occurs within
90 seconds after power-up.
Prior to performing the FIRE Panel Test ensure that
no ‘FAIL’ fire detection / extinguishing system messages are displayed on the EICAS.
If the APU is running, pressing and holding the Fire Detection TEST button for more than
10 seconds will result in APU shutdown.
For E1 airplanes, to allow for the flight controls built-in-test (BIT), wait
three (3) minutes after AC power is applied or for the FLT CTL TEST IN PROG message to clear before turning any hydraulic pump on.
3 seconds after APU speed has reached 95%,
electrical and pneumatic loading are available. If the APU does not reach proper speed or acceleration rate within the starting cycle time, the APU will automatically shut down.
During the Power-up, wait
30 seconds after EICAS has been energized prior to start the APU.
If FLT CRTL BIT EXPIRED message is displayed,
refer to the QRH.
The action of reading and checking the OEBs must be performed by both pilots at the same time. The PF will read the OEBs and the PM will
cross check the information.
To allow for the flight controls built-in-test (BIT), wait three (3) minutes after AC power is applied, or
wait for the FLT CTL TEST IN PROG EICAS message to disappear before accomplishing the TRIMS check.
For all of the following trim checks, push and hold for more then
three (3) seconds to verify automatic stop:
NAV lights: During day time NAV lights must be turned ON prior to the inspection and
turned OFF once the inspection is accomplished. At night NAV light must be turned ON and remain ON after the inspection.
- Inspection lights: At night inspection lights must be turned ON prior to commencing the inspection and turned OFF once the inspection is accomplished
Check engine for leaks and obstructions in the air inlets. Oil puddles in exhaust nozzle exceeding
23 cm by 15 cm require logbook entry and maintenance action
Static Wicks (number) . . . . . . . . . Check
— Ensure four (4) on the rudder, one on the vertical stabilizer,
three (3) on each elevator and three (3) on each horizontal stabilizer.
Static Wicks (number) . . . .Check
— Ensure
three (3) on the aileron and six (6) on the winglet.
After the software calculates the takeoff performance the
Captain will read the ePerf results card on his EFB while the First Officer will cross check the information on the results card of his EFB.
Use CG 22% for E190, CG
25% for E195 and 29% for E195-E2.
Low pressure external (pre-conditioned) air in combination with APU BLEED air is acceptable. The use of HP air in combination with the
APU BLEED air is prohibited.
Normal limits are ± _______ between PFD 1 and 2. If a difference above the tolerance is noticed, report on technical logbook.
20 feet
Hydraulic Synoptic page . . . . . . Check
— Ensure hydraulic fluid quantity is
“green.”