ATA29747-400P0

Hydraulics

Overview

The 747-400 has four independent hydraulic systems (1, 2, 3, 4) operating at 3,000 psi. Each engine drives one Engine-Driven Pump (EDP); systems 1 and 4 also have Air-Driven Pumps (ADPs) powered by bleed air, and systems 2 and 3 add Electric Demand Pumps. A Ram Air Turbine (RAT) deploys automatically on loss of all AC power to provide backup pressure to system 1.

Architecture

Failure sim:
BOEING 747-400 HYDRAULIC SYSTEM SCHEMATICSYSTEM 1SYSTEM 2SYSTEM 3SYSTEM 4ENGINE DRIVENPUMPELEC MTRPUMP(AUX)AIR DRIVENPUMP(DEMAND)ENGINE DRIVENPUMPELEC MTRPUMP(DEMAND)ENGINE DRIVENPUMPELEC MTRPUMP(DEMAND)ENGINE DRIVENPUMPELEC MTRPUMP(AUX)AIR DRIVENPUMP(DEMAND)PSI3000PSI3000PSI3000PSI3000NOSE GEAR STEERINGBODY GEAR STEERINGCENTRE AUTOPILOTRIGHT AUTOPILOTLEFT AUTOPILOTNORMAL BRAKESBRAKE ACCMTRSPOILERS 2, 3, 10, 11SPOILERS 1, 4, 9, 12SPOILERS 5, 6, 7, 8NOSE GEAR ACTUATIONBODY GEAR ACTUATIONWING GEAR ACTUATIONLEFT OUTBD ELEVATORLEFT INBD ELEVATORELEVATOR FEELRIGHT INBD ELEVATORRIGHT OUTBD ELEVATORINBD TE FLAPSOUTBD TE FLAPSSTABILISER TRIMLEFT OUTBD AILERONLEFT INBD AILERONRIGHT INBD AILERONRIGHT OUTBD AILERONUPPER RUDDERLOWER RUDDERALTERNATE BRAKES (1)ALTERNATE BRAKES (2)Toggle SYS 1-4 above to simulate failure · Multi-source rows show secondary supply dot
EDP = Engine-Driven Pump
ELEC MTR PUMP = Electric Motor Pump
ADP = Air-Driven Pump
RAT = Ram Air Turbine (Sys 1 backup)
Aircraft Zones — Side View
FLIGHT DECKUPPER DECK / CREW RESTFWD E/E BAYFWD MAIN DECKAFT MAIN DECKFWD CARGO LOBEAFT CARGO LOBECWTWING TANKSMAIN GEAR BAYNLG4 × ENGINE NACELLES (pylons under wings)VSTAB / RUDDERHSTAB / ELEVATORSTAIL CONEAPU
Overhead Panel — Controls
OVERHEAD — HYDRAULIC PANELSYSTEM 1EDPONAIRAUTOAUXOFFRES OKSYSTEM 2EDPONDEMAUTO——RES OKSYSTEM 3EDPONDEMAUTO——RES OKSYSTEM 4EDPONAIRAUTOAUXOFFRES OKEDP normally ON · DEM pumps AUTO · RES indicator goes amber on low qty

Components

Hydraulic Systems4 independent (Sys 1, 2, 3, 4)
System Pressure3,000 psi nominal
Engine-Driven Pumps (EDPs)4 (one per engine)
Air-Driven Pumps (ADPs)2 (Sys 1 and Sys 4) — pneumatic
Electric Demand Pumps2 (Sys 2 and Sys 3) — AC
Auxiliary PumpSys 4 has an aux electric pump for parking brake
RATRam Air Turbine — deploys on all-engine flameout or loss of AC; powers Sys 1
Reservoirs4 (pressurized by bleed air)
FluidSkydrol — phosphate ester (BMS 3-11)

System Usage

| System | Primary Users | |---|---| | Sys 1 | Lower rudder, inboard ailerons, inboard elevator, body gear steering, lower outboard elev, normal brakes, autopilot L | | Sys 2 | Outboard ailerons, outboard elevators, flaps (normal), autopilot R | | Sys 3 | Inboard ailerons, inboard elevator, lower rudder, nose gear steering, normal brakes, autopilot C | | Sys 4 | Upper rudder, outboard ailerons, outboard elevators, slats, alternate brakes |

STUB — REWRITE
Cross-check distribution above against FCOM — derived from public ATA-29 summaries.

Normal Operation

  • All four EDPs ON during normal flight (each engine driving its pump)
  • ADPs/Demand pumps in AUTO — supplement EDPs at low engine speed or on engine loss
  • System pressure monitored on EICAS HYD page

Failures & Abnormals

CAUTION — Single System Loss

Loss of one hydraulic system results in degraded redundancy on shared surfaces but full flight control retained. Plan for alternate landing distance per QRH if Sys 1 (normal brakes) lost.

WARNING — All AC Bus Loss / RAT Deployment

RAT deploys automatically and provides pressure to Sys 1 only. Many surfaces lose redundancy. Land at nearest suitable airport per QRH.

Limits

  • System pressure: 3,000 psi nominal, EICAS alert below ~2,400 psi
  • Reservoir quantity: monitor on EICAS — low quantity triggers EICAS message
  • Hydraulic fluid temp: max ≈ 215 °F (varies by system)

Notes / Personal

STUB — REWRITE
User to add notes on demand pump behavior at low engine RPM, etc.