Installing the hydraulic power unit
Preliminary requirements
Required Conditions
Remove the right transmission fairing (432BR).
Remove the left transmission fairing (432AL).
Support equipment
Hydraulic Power Unit (HPU)
Local supply
1
600 PSI (4137 kPa) operating pressure, 1.7 gallons per minute (6.44 L/min) maximum flow, 5-micron pressure filter.
Union
AS5174W0505
1
Or equivalent.
Consumables, materials and expendables
Caps or plugs
C-428
AR
Safety conditions
Make sure that the Hydraulic Power Unit (HPU) is serviced only with an approved hydraulic fluid. If you do not obey this precaution, there is a risk of contamination of the hydraulic system.
Make sure that the Hydraulic Power Unit delivery pressure is less than 400 PSI (2757.9 kPa) before you apply hydraulic power to the aircraft. If you do not obey this precaution, there is a risk of damage to the hydraulic system and/or the Hydraulic Filter Reservoir Module (HRFM).
Do not apply more than 400 PSI (2757.9 kPa) to the hydraulic system or damage to the Hydraulic Reservoir Filter Module (HRFM) can occur.
If Hydraulic Power Unit pressure exceeds 800 PSI (5515.8 kPa), inspect rupture disk for leaks or damage.
Procedure
Put the Hydraulic Power Unit (HPU) on the right side of the helicopter, near the Hydraulic Reservoir Filter Module (HRFM).
Connect the pressure hose of the Hydraulic Power Unit (HPU) to the tee fitting.
Disconnect the elbow fitting from the check valve at the return port (FROM ACT) of the HRFM.
Connect the Union (AS5174W0505) to the elbow fitting.
Connect the return hose of the Hydraulic Power Unit (HPU) to the Union (AS5174W0505).7Install Caps or plugs (C-428) on the open port of the check valve.
Last updated