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HYD PUMPS · LIVEHYD PUMPS · LIVE

Hydraulics
LIVE
ConditionCondition
Overhead HYD PUMPS — systèmes A/B, voyants LOW PRESSURE / OVERHEAT, alimentations bus. SVG cockpit (zéro photo manuel).Overhead HYD PUMPS — systems A/B, LOW PRESSURE / OVERHEAT lights, bus feeds. Cockpit SVG (zero manual photos).
ObjectifObjective
Lire A/B, bus, voyants LOW PRESSURE / OVERHEAT — SVG cockpit seulement (photos derrière reveal si besoin).Read A/B, buses, LOW PRESSURE / OVERHEAT lights — cockpit SVG only (photos behind reveal if needed).
HYD PUMPS
HYD PUMPS SYSTEM A LOW PRESSURE ON OFF ENG 1 DC BUS 2 EDP OVERHEAT LOW PRESSURE ON OFF ELEC 2 GEN BUS 2 EMDP SYSTEM B OVERHEAT LOW PRESSURE ON OFF ELEC 1 GEN BUS 1 EMDP LOW PRESSURE ON OFF ENG 2 DC BUS 1 EDP ENG 1 + ELEC 2 = A (red) · ELEC 1 + ENG 2 = B (green) · EDP = LP only · EMDP = OH + LP
ENG 1 + ELEC 2 = A · ELEC 1 + ENG 2 = B. EDP : LOW PRESSURE seulement. EMDP : OVERHEAT + LOW PRESSURE. Canons switch (pas rectangles blancs).ENG 1 + ELEC 2 = A · ELEC 1 + ENG 2 = B. EDP: LOW PRESSURE only. EMDP: OVERHEAT + LOW PRESSURE. Switch barrels (not white rectangles).
DC BUS 2 · ENG 1 GEN BUS 2 · ELEC 2 GEN BUS 1 · ELEC 1 DC BUS 1 · ENG 2

ENG 1 · DC BUS 2

Solénoïde dépressurisation EDP système A. OFF = blocking valve, pas arrêt mécanique.EDP depressurization solenoid system A. OFF = blocking valve, not a mechanical stop.

ELEC 2 · GEN BUS 2

EMDP système A (OVERHEAT + LOW PRESSURE). Bus opposé au moteur de ce système.EMDP system A (OVERHEAT + LOW PRESSURE). Opposite generator bus to this system’s engine.

ELEC 1 · GEN BUS 1

EMDP système B (OVERHEAT + LOW PRESSURE).EMDP system B (OVERHEAT + LOW PRESSURE).

ENG 2 · DC BUS 1

Solénoïde dépressurisation EDP système B.EDP depressurization solenoid system B.

SYSTEM A SYSTEM B STANDBY PTU
Architecture A / B / StandbyArchitecture A / B / Standby
SYSTEM A ENG 1 EDP · ELEC 2 EMDP • Eng 1 Thrust Reverser • Inbd Flight Spoilers • Ground Spoilers • Autopilot A • Normal Brakes • NWS (normal) • LG Up/Down via LGTU • FLT CTL SOV (A) DC BUS 2 · GEN BUS 2 Full 4.80 · RFL 4.20 USG STANDBY EMDP · ram-air cooled • STBY Rudder (SOV) • LE Flaps / Slats (ALTN) • Eng 1 / 2 TR via STBY LOW QTY · LOW PRESSURE Full 2.80 · LQ @ 1.40 USG Fed from System B qty PTU ≈ 2,600 PSI → LED Motor A · Pump B · keel beam SYSTEM B ELEC 1 EMDP · ENG 2 EDP • Auto Slat / LE Flaps-Slats • TE Flaps (normal) • Eng 2 Thrust Reverser • Outbd Flight Spoilers • Yaw Damper · A/P B • Brakes + Accum · ALT NWS • FLT CTL SOV · ALTN Flaps GEN BUS 1 · DC BUS 1 Full 7.20 · RFL 6.40 USG SHARED FLIGHT CONTROLS (A + B) Rudder (+ FFM) · Ailerons · Elevator / Elevator Feel FEEL DIFF PRESS when TE Flaps UP Reservoirs 45–50 PSI pneumatic (max 65). No fluid transfer A↔B in normal ops. A STBY B PTU Catalog architecture — SVG recreation (no photos)
Architecture dense A (rouge) · B (vert) · Standby (jaune) · PTU · commandes partagées — catalog 5929–5932b.Dense architecture A (red) · B (green) · Standby (yellow) · PTU · shared controls — catalog 5929–5932b.

EDP : couplée N2 — tourne toujours moteur tournant. Débit 22–36 USG/min. Switch OFF = vanne dépressurisation (solénoïde DC Bus).EDP: N2-coupled — always runs with the engine. Flow 22–36 USG/min. Switch OFF = depressurization valve (DC Bus solenoid).

EMDP : ~6 USG/min — peut ne pas suffire seule (train, volets, reverse). OVERHEAT + LOW PRESSURE.EMDP: ~6 USG/min — may not meet high demand alone (gear, flaps, reverse). OVERHEAT + LOW PRESSURE.

Réservoirs : 45–50 PSI pneumatique (max 65). Pas de transfert A↔B en ops normales.Reservoirs: 45–50 PSI pneumatic (max 65). No fluid transfer A↔B in normal ops.