Day 10 - Hydraulic/Pneumatic Systems Flashcards
The T-1 hydraulic system controls
Flaps, landing gear, speed brakes, and normal braking
What types of hydraulic pumps are utilized in the T-1
Variable displacement, rotary plunger type pumps
The hydraulic pumps delivery and pressure varies from __ gpm at __ psi to __ gpm at __ psi
0, 1500, 3.9, 1400
Hydraulic reservoir capacity is
1.2 gallons
The hydraulic reservoir is pressurized by what and at what psi
Engine bleed air, 15 psi
Why is the hydraulic reservoir pressurized
To prevent frothing
The hydraulic system normally stabilizes at __ psi
1500
The hydraulic pressure relief valve begins to open at __ psi
1650
The hydraulic pressure relief valve is fully open at __ psi
1850
Hydraulic pressures above 1850 can only be relieved by doing what
By activating the hydraulic pressure relief switch on the flightdeck
The HYD PUMP PRESS LO annunciator illuminates when pressure falls below
750 psi
The HYD LEVEL LO annunciator illuminates when
The fluid level in the reservoir falls below 0.6 gallons
When landing without normal hydraulic pressure, increase __ flap landing distance by __
30, 90%
The systems that require bleed air are
Engine anti-ice, wing anti-ice, hydraulic reservoir pressurization, entrance door seal inflation, cabin pressurization, and environmental system (ACU)
When does CABIN PRESSURE LO annunciator illuminate
Cabin altitude 9500 +/- 500 feet