Cockpit & Avionics
Flight Deck
Six-screen Common Display System with conventional control columns and the dual-FMC flight management system.
How it works
- 01Control columns and wheels move cables to hydraulic power control units (PCUs) — no fly-by-wire on the NG; manual reversion if hydraulics are lost.
- 02Autopilot Flight Director System (AFDS) with two FCCs; Mode Control Panel (MCP) on the glareshield.
- 03Two Air Data Inertial Reference Units (ADIRUs) provide attitude and air data.
- 04Master Caution with system annunciator 'six-pack' panels; failures are handled with the paper/electronic QRH.
Key data & limitations
- Displays
- 6 × LCD (CDS)
- Hydraulics
- A, B & Standby (3000 psi)
- FMC
- Smiths/GE dual FMC
Maintenance guidelines
- ADIRU and FCC BITE tests per AMM Chapter 22/34.
- Pitot-static leak checks and probe heat tests.
- CDS software part numbers verified against configuration.
REF: FCOM Vol. 2 — Ch. 4 (Automatic Flight), Ch. 9 (Flight Controls), Ch. 10 (Flight Instruments)
