Minimum dispatch hydraulic fluid quantity levels are:
The standby hydraulic pumps:
The purpose of the PTU is to:
-Retract the gear in the event of a #1 engine failure.
-Retract the gear in the event of a #2 engine failure.
-To power the #2 hydraulic system in the event of fluid loss from the #2
system.
-Transfer hydraulic fluid from #1 hydraulic system to #2 hydraulic system in the event of a fluid loss.
The subsystems actuated by the No. 1 hydraulic system are:
- Landing gear, nosewheel steering, outboard roll spoilers, and upper rudder actuator.
- Flaps, brakes and antiskid, inboard roll spoilers, lower rudder actuator, and the power transfer unit.
- Flaps, landing gear, brakes and antiskid, and ground spoilers.
- Power transfer unit, alternate gear extension, and outboard and inboard
roll spoilers.
Illumination of a STBY HYD PUMP HOT caution light indicates:
- Fluid over temperature in the standby system.
- Over temperature of the windings in the electric motor driving the standby
pump.
- The engine driven pump is overheating
- The standby pump is hot.
The main system reservoirs are pressurized by:
The ENG HYD PUMP caution light illuminates when:
The main source of pressure for the No. 1 and No. 2 hydraulic systems is:
The number of hydraulic systems on the Dash 8 aircraft is: