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Page | 16/43 | Date | 20.10.2016 | Size | 2.65 Mb. | | #6810 |
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Maintenance and Operational Procedures
for Federal Aviation Administration Master Minimum Equipment List - No: 8a - 08/01/2008
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1. SYSTEM,
Sequence Numbers & Item
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Repair Category
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2. Number Installed
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3. Number Required for Dispatch
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MAINTENANCE
PROCEDURES
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OPERATIONAL
PROCEDURES
| 29 – Hydraulic Power |
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4. Remarks and Exceptions
| 30-1 | L/R HYD LO FLOW Annunciators (Viper Engines, Only) |
C
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2
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1
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(O) One may be inoperative provided:
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Associated hydraulic pump is operative,
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Main hydraulic supply pressure indicator is operative,
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EMRG HYD LO PRESS annunciator is operative,
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Associated engine is started first to verify pressure buildup before each departure.
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Confirm HYD LO PRESS indicator is operative.
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Prior to each departure, start the engine on the affected side first and confirm a pressure increase on the main hydraulic pressure indicator.
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If HYD LP lamp illuminates in flight, follow EMERGENCY BRAKE SUPPLY FAILURE drill.
| 30-2 | HYD LO PRESS 1 or 2 Annunciators (TFE-731 Engines, Only) |
C
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2
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1
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(O) One may be inoperative provided:
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Associated hydraulic pump is operative,
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Main hydraulic supply pressure indicator is operative.
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EMRG BRK LO PRESS annunciator is operative, and
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Associated engine is started first to verify pressure buildup before each departure.
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Prior to each departure,
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Prior to engine start, select Emergency Brake and operate brake pedals until EMER BRK LO PRESS annunciator illuminates.
Caution
Airplane must be chocked during engine start.
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Start the associated engine first and observe pressure build up on the main hydraulic pressure indicator.
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Observe EMER BRK LO PRESS annunciator OFF at 2250 to 2450 psi.
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Series 1 thru 700: If brake EMERG BRK LO PRESS warning light illuminates in flight, follow EMERGENCY BRAKE SUPPLY FAILURE drill.
| 30-3 | Combined Brakes and SUPPLY Pressure Gauge |
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1)
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BRAKE Pressure Indicators
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C
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2
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1
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(O) One may be inoperative provided before each departure:
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Main hydraulic SUPPLY indication is within normal limits,
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Emergency Brake Pressure Indicators/Annunciators are verified operative, and
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Normal braking is confirmed independently for left and right brakes.
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Prior to each departure:
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Confirm Supply Pressure indication is normal.
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Prior to taxi, select EMRGY wheel brake and confirm both 1 and 2 WHEEL BRAKE EMRGY annunciators illuminate.
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Confirm normal braking independently for left and right brakes.
| 30-4 | Accumulator Pressure Indicators |
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Deleted, Rev. 3.
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| 30-5 | AUX HYD LO LEVEL Annunciator (Series 3 Through 900XP, Only) |
C
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1
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0
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(O) May be inoperative provided fluid quantity is visually verified to be adequate before each departure.
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Gain access to Nose Landing Gear (NLG) wheel well.
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Visually confirm Auxiliary AUX HYD Reservoir has adequate quantity prior to each departure.
| 30-6 | Accumulator Pressure Indicators (Main and Emergency Brake Only) |
C
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2
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1
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(O) One may be inoperative provided:
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Combined BRAKES and SUPPLY Pressure Gauge is operative, and
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Associated accumulator pre-charge is verified adequate before the first flight of each day.
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Perform the following prior to the first flight of each day:
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With engines not operating, check hydraulic pressure indicator pressure to be ~2,300 PSI.
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Operate brakes five (5) times and confirm negligible change in hydraulic pressure.
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Select WHEEL BRAKE lever to EMERGY and operate brakes 5 times. Confirm EMERG BRAKE annunciators illuminate.
| 30-7 | Thrust Reverser Accumulator Pressure Indicator (Series 800, if installed, and 750, 800XP, 850XP and 900XP) |
C
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1
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0
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(O) May be inoperative provided before each departure:
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Thrust Reversers are verified operative, and
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Main Hydraulic Accumulator pressure is verified normal.
Note
Thrust Reversers may be inoperative with loss of main hydraulic system pressure.
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Prior to each departure, confirm Thrust Reversers are operative, and
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Confirm Main Hydraulic Accumulator pressure is normal.
Note
Thrust Reversers may be inoperative with loss of main hydraulic system pressure.
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