Hydraulics Flashcards
Hydraulic System Description
- number of systems
- names
- minimum dispatch quantity for systems 1, 2, and 3
• (4) hydraulic systems:
o #1 and #2 Main systems
o #3 Backup system
o Auxiliary system
NOTE: The minimum dispatch quantity for the #1, 2, and 3 systems is 40% of their normal volume
1 Hydraulic System
- number of reservoirs and quarts
- number of pumps
- when will the AC standby pump activate
- describe the PTU and when it activates
- min parking brake pressure prior to starting the left engne
- 1 reservoir (8 quarts)
- 1 Engine Driven Pump (EDP)
- 1 AC Standby Motor Pump (ACMP) used as a back-up for the EDP
- AC Standby pump will automatically activate when the No. 1 engine fails, or whenever the flaps are selected to any position greater than 0° (the parking brake must be released)
- PTU (Power Transfer Unit) uses hydraulic POWER from system 1 to provide hydraulic PRESSURE to system 2
- PTU will automatically turn ON when the #2 engine fails or whenever the flaps selected to any position greater than 0° (the parking brake released)
NOTE: Minimum indicated parking brake pressure prior to starting the LEFT Engine first is 1000 psi
1 Hydraulic Abnormal Operation
- A “Hydraulic System Isolation Valve” remains open for all normal operations
- If inadequate fluid quantity or loss is detected in the system, #1 Hydraulic system HYD ISO valve CLOSES, hydraulic power is only AVAILABLE to the following #1 services: (4)
- PTU
- Rudder (lower pcu)
- Elevators (outboard pcu)
- Flaps
#1 Hydraulic Abnormal Operation - "priority valve" remains open for normal ops: at what pressure will it close and shuts of power to what (2)
- A “Priority Valve” remains open for all normal operations
- If the hydraulic pressure in #1 system decreases below 2100 psi, the “Priority Valve” automatically closes
- Closing of the “Priority Valve” shuts off hydraulic power to the Flaps and PTU
1 Hydraulic Abnormal Operation
- when must the standby hydraulic pump be manually activated
- when will the standby hydraulic pump automatically be activated
- Standby hydraulic pump must be manually activated in the event of a #1 EDP failure to maintain pressure to the system
- Standby hydraulic pump will automatically activate in response to a #1 engine failure
1 Hydraulic Abnormal Operation
- If the #1 and/or #2 Main hydraulic systems fail, #3 hydraulic system will automatically activate to supply pressure to the
- If automatic activation does not take place, #3 system can be activated manually by pressing the
- If the #1 and/or #2 Main hydraulic systems fail, #3 hydraulic system will automatically activate to supply pressure to the left and right elevator (inboard PCUs) to maintain pitch control
- If automatic activation does not take place, #3 system can be activated manually by pressing the “HYD #3 ISOL VLV” switchlight on the HYDRAULIC CONTROL panel
2 Main Hydraulic System
- number of reservoirs and quantity
- number of pumps
- what valves does it/does not have
- min parking brake pressure prior to starting the right engine
- 1 Reservoir (12 quarts)
- 1 Engine Driven Pump (EDP)
- Has no PTU
- A “Hydraulic System Isolation Valve” remains open for all normal operations
- “Priority Valve” does not exist on the #2 Hydraulic System because it is assisted from the #1 Hydraulic System PTU
NOTE: Minimum indicated parking brake pressure prior to starting the RIGHT engine first is 500 psi
2 Hydraulic Abnormal Operation
- A “Hydraulic System Isolation Valve” remains open for all normal operations
- If inadequate fluid quantity or loss is detected in the system, #2 Hydraulic system HYD ISO valve CLOSES, hydraulic power is only AVAILABLE to the following #2 services:
- Rudder (upper pcu)
- Elevators (center pcu)
2 Hydraulic Abnormal Operation
- when must the PTU be manually activate
- when will the PTU automatically activate
- PTU must be manually activated in the event of a #2 EDP failure to maintain pressure to the system
- PTU will automatically activate in response to a #2 engine failure
2 Hydraulic Abnormal Operation
- If the #1 and/or #2 Main hydraulic systems fail, #3 hydraulic system will automatically activate to supply pressure to the
- If automatic activation does not take place, #3 system can be activated manually by pressing the
- If the #1 and/or #2 Main hydraulic systems fail, #3 hydraulic system will automatically activate to supply pressure to the left and right elevator (inboard PCUs) to maintain pitch control
• If automatic activation does not take place, #3 system can be activated manually by pressing the “HYD #3 ISOL VLV” switchlight on the HYDRAULIC CONTROL panel
3 Backup Hydraulic System
- number of reservoirs and quarts
- powered by
- accumulator pressure maintained by and kept between what psi
- If Both EDPs, Standby Hydraulic Pump, and the PTU FAIL, the DCMP in the #3 hydraulic system will provide hydraulic power to the
- 1 Reservoir (2.6 quarts)
- Powered by a gas charged accumulator
- Accumulator pressure is maintained by a DC Motor-Driven-Pump (DCMP)
- DCMP operation is to maintain the accumulator pressure within 2600 to 3250 psi
- If Both EDPs, Standby Hydraulic Pump, and the PTU FAIL, the DCMP in the #3 hydraulic system will provide hydraulic power to the left and right elevator for pitch control
#3 Hydraulic Abnormal Operations - If the #3 Hydraulic system accumulator pressure falls to \_\_ psi, or if the DCMP has been running for longer than \_\_ seconds while on the ground, it results in the illumination of the #3 \_\_ caution light
- 900, 60, STBY HYD PUMP
#3 Hydraulic Abnormal Operations - If the #3 Hydraulic system isolation valve fails OPEN during normal operations, it results in
- all three hydraulic systems supplying pressure to the elevator actuators and the illumination of a “ELEVATOR PRESS” caution light
4 Auxiliary Hydraulic System
- reservoir and quantity
- quantity indication
- purpose of the system
- 1 reservoir (1.2 quarts) located in the right forward lower compartment, aft of the crew O2 bottle
- There is NO quantity indication in the cockpit
- Manually operated system and serves as an alternate means of extending the main landing gear
- This manual system is used to ensure the main landing gear is completely extended