Fms
✈️ Flight Management System (FMS / FMGS) — Short Review
1. What the FMS Is
The FMS (Boeing) or FMGS (Airbus) is the central navigation and flight-path management system. It manages the aircraft’s lateral and vertical path from shortly after take-off to landing, with minimal crew input.
2. Main Purposes
The FMS:
Determines aircraft position (IRS + GNSS + radio updating)
Guides the aircraft in:
- LNAV (lateral navigation)
- VNAV (vertical navigation)
Optimises performance and fuel
Displays navigation/performance data on PFD/ND
Allows crew to:
- Build/modify routes (SID, STAR, approach, holds)
- Select automation modes
- Override with heading, speed, altitude, V/S via MCP/FCU
3. Main Components (Boeing / Airbus)
- FMC / FMGC – Flight management computer
- CDU / MCDU – Crew interface
- MCP / FCU – Mode selection (selected vs managed)
- AFDS – Autopilot + Flight Director
- A/T or A/THR – Speed/thrust control
- PFD / ND – Displays
Typical installation:
- Dual FMCs (mandatory for RNP)
- Cross-talk between FMCs
- Integrated with autopilot and autothrust
4. Inputs to the FMS
The FMS uses data from:
- IRS / ADIRS (position, attitude)
- ADCs (airspeed, altitude, temperature)
- GNSS
- Radio NAVAIDs
- Fuel & configuration sensors
- Aircraft clock (time accuracy for ACARS, FDR)
5. Pre-Flight Setup (Logic Flow)
Via CDU / MCDU:
Who am I? → IDENT (aircraft, engines, nav database)
Where am I? → POS INIT (alignment / GPS position)
Where am I going? → ROUTE INIT (departure, destination, alternate)
How will I get there? → SID, route, STAR, approach (DEP/ARR + ROUTE)
When will I get there? → PERF INIT (weights, CI, cruise FL, winds, TO data)
Then:
- ACTIVATE route
- EXEC to confirm
- Cross-check vs flight plan
6. In-Flight Operation
FMS computes:
- Optimum vertical profile
- Fuel and ETA predictions
LNAV/VNAV (or Airbus managed modes) can be engaged
Crew monitors and intervenes when required
7. Integration with Other Systems
FMS exchanges data with:
- Autopilot / Flight Director
- Autothrust
- EFIS (PFD/ND)
- EICAS / ECAM
- ACARS, FDR, maintenance systems
8. Automation & Human Factors
Advantages:
- Accurate navigation
- Reduced workload
- Precise SID/STAR and constraint compliance
- Enables RNP and autoland
Risks:
- Mode confusion
- Automation complacency
- Reduced situational awareness
Golden rule: 👉 Always know what the FMS is doing now and what it will do next.
The FMS computes and manages the aircraft’s lateral and vertical flight path, optimising performance while allowing crew supervision and intervention.
✈️ Boeing vs Airbus Automation Philosophy
Core Philosophy (Big Picture)
Boeing
👉 Pilot in command of the aircraft
- Automation is a tool to assist
- Pilot normally commands the aircraft
- Aircraft does what the pilot selects
Airbus
👉 Aircraft in command within limits
- Automation is a manager
- Pilot requests, aircraft decides
- Aircraft protects the flight envelope
Flight Path Control
Boeing
- Pilot selects targets (speed, altitude, heading)
- FMS advises and flies if commanded
- LNAV/VNAV are optional tools
- Vertical path can be overridden easily
Airbus
Managed modes follow FMGS
Pilot selects managed or selected
Aircraft maintains profile unless overridden
Clear distinction between:
- Managed (FMGS controls)
- Selected (pilot controls)
Mode Awareness & Indication
Boeing
- Mode logic is generally simpler
- Fewer mode transitions
- Pilot sets targets explicitly
Airbus
- More automation states
- Greater reliance on FMA monitoring
- Understanding what mode you’re in is critical
Flight Envelope Protection
Boeing
- Warnings only
- Pilot can exceed limits
- Pilot always has full authority
Airbus
Hard protections (normal law)
Prevents:
- Stall
- Overspeed
- Excessive bank / pitch
Pilot inputs are filtered
Autothrust / Autothrottle
Boeing
- Autothrottle moves thrust levers
- Pilot can see thrust changes physically
- Thrust mode changes are intuitive
Airbus
- Autothrust does not move levers
- Levers set to detents (CL, TOGA)
- FMGS controls thrust electronically
Pilot Interaction Style
Boeing
- “I fly the airplane”
- Automation supports pilot decisions
- Manual intervention is straightforward
Airbus
- “I manage the airplane”
- Automation flies the profile
- Pilot supervises and intervenes as needed
Failure Philosophy
Boeing
- Degradation leads toward manual flying
- Pilot authority remains unchanged
Airbus
Laws degrade:
- Normal → Alternate → Direct
Protections are gradually removed
Exam Comparison Table
| Feature | Boeing | Airbus |
|---|---|---|
| Philosophy | Pilot command | Aircraft management |
| Modes | Selected targets | Managed vs Selected |
| Envelope protection | Warnings only | Hard protections |
| Thrust control | Levers move | Detent logic |
| Override ease | Immediate | Requires mode change |
| Pilot role | Active controller | System manager |
One-Line Exam Memory Hooks
- Boeing: “Pilot flies, automation assists”
- Airbus: “Pilot manages, automation flies”
✈️ Boeing vs Airbus — FMS Pages Overview
Naming Convention
- Boeing: CDU pages (often multiple FMCs)
- Airbus: MCDU pages (FMGS-centric)
CORE PHILOSOPHY (Pages)
- Boeing: Pages are task-specific and more distributed
- Airbus: Pages are structured and sequential (INIT → F-PLN → PERF)
IDENTIFICATION & STATUS
Boeing
- IDENT – Aircraft model, engines, nav database
Airbus
- IDENT – Same purpose (aircraft & database)
👉 Same function, same exam meaning
POSITION INITIALISATION
Boeing
- POS INIT – IRS alignment and present position
Airbus
- INIT A – IRS alignment and initial position
👉 Different names, identical purpose
ROUTE CREATION
Boeing
- RTE – Origin, destination, en-route waypoints
- DEP/ARR – Runway, SID, STAR, approach
Airbus
- F-PLN – Full route displayed as one continuous plan
- DEP/ARR – Runway, SID, STAR, approach
👉 Boeing = route split across pages 👉 Airbus = route shown as a single flow
PERFORMANCE INITIALISATION
Boeing
- PERF INIT – Weights, reserves, CI, cruise level
- TAKEOFF / APPROACH REF – Speeds, flap settings
Airbus
- INIT B – Weights, fuel, reserves
- PERF – TO, CLB, CRZ, DES, APPR pages
👉 Airbus performance is phase-based 👉 Boeing performance is page-based
LEGS / WAYPOINT MANAGEMENT
Boeing
- LEGS – Waypoint-by-waypoint sequencing
- Manual intervention common (direct-to, deletes)
Airbus
F-PLN – Same page used for:
- Waypoints
- Constraints
- Direct-to
👉 Boeing: LEGS page = heart of navigation 👉 Airbus: F-PLN page = heart of navigation
PROGRESS & MONITORING
Boeing
- PROG – Position, ETA, fuel, waypoint progress
Airbus
- PROG – Same function
👉 Identical role
SECONDARY / SUPPORT PAGES
Boeing
- VNAV – Vertical profile details
- FIX – Radials, distance rings
- HOLD – Holding patterns
Airbus
- RAD NAV – Manual radio tuning
- FIX INFO – Fix rings, radials
- HOLD – Holding patterns
KEY EXAM COMPARISON TABLE
| Function | Boeing Page | Airbus Page |
|---|---|---|
| Aircraft / DB | IDENT | IDENT |
| Position init | POS INIT | INIT A |
| Route build | RTE | F-PLN |
| SID / STAR | DEP/ARR | DEP/ARR |
| Weights / fuel | PERF INIT | INIT B |
| Phase performance | TAKEOFF / APPR REF | PERF |
| Waypoints | LEGS | F-PLN |
| Progress | PROG | PROG |
ONE-LINE MEMORY HOOKS (EXAM GOLD)
- Boeing: “Many pages, pilot builds the route step by step”
- Airbus: “Few core pages, system manages the flight plan flow”
✈️ Boeing vs Airbus — Modes Overview
BIG PHILOSOPHY REMINDER
- Boeing: Pilot sets targets → aircraft follows
- Airbus: Pilot chooses managed or selected → aircraft decides
LATERAL MODES (Direction)
Boeing
- HDG SEL – Fly selected heading
- LNAV – Follow FMC lateral route
- LOC / VOR – Radio navigation
- ROL – Basic roll hold (fallback)
Airbus
- HDG (Selected) – Fly selected heading (knob pull)
- NAV (Managed) – Follow FMGS route (knob push)
- LOC – Localizer
- RWY / RWY TRK – Initial guidance after takeoff
VERTICAL MODES (Path)
Boeing
- VNAV – FMC vertical profile (climb/cruise/descent)
- FLCH – Pitch for speed, thrust for climb/descent
- V/S – Selected vertical speed
- ALT HOLD / ALT ACQ – Level-off modes
Airbus
- CLB / DES (Managed) – FMGS vertical profile
- OP CLB / OP DES (Selected) – Pitch for speed, ignore constraints
- V/S – FPA – Vertical speed or flight path angle
- ALT / ALT* – Altitude hold/acquire
SPEED / ENERGY MODES
Boeing
Speed set by:
- MCP window or
- FMC (VNAV)
Autothrottle moves thrust levers
Thrust modes shown on FMA
Airbus
- Managed speed (FMGS) or Selected speed
- Autothrust active in detents
- Thrust levers do not move
APPROACH MODES
Boeing
- APP – Arms LOC + GS
- VNAV PATH – For non-precision approaches
- FLARE / ROLLOUT – Autoland (if equipped)
Airbus
- APPR – Arms LOC + GS
- FINAL APP – Managed non-precision
- FLARE / ROLLOUT – Autoland
MODE SELECTION INTERFACE
Boeing (MCP)
Windows always active
Pilot selects:
- Heading
- Speed
- Altitude
Then selects the mode
Airbus (FCU)
- Push = Managed
- Pull = Selected
- Windows may be dashed (managed)
PROTECTION PHILOSOPHY
Boeing
- No hard limits
- System warns
- Pilot can override everything
Airbus
- Envelope protections (Normal Law)
- Inputs are limited for safety
- Protections degrade with failures
QUICK EXAM COMPARISON TABLE
| Area | Boeing | Airbus |
|---|---|---|
| Lateral nav | LNAV | NAV (managed) |
| Vertical nav | VNAV | CLB / DES (managed) |
| Immediate climb/descent | FLCH | OP CLB / OP DES |
| Speed control | Window or FMC | Managed or selected |
| Thrust levers | Move | Fixed detents |
| Pilot role | Fly the airplane | Manage the airplane |
ONE-LINE MEMORY HOOKS (EXAM GOLD)
- Boeing: “Select a target, then choose a mode”
- Airbus: “Push to manage, pull to command”
✈️ Boeing vs Airbus — FMS Components Overview
Core Philosophy Reminder
- Boeing: Pilot commands the system
- Airbus: Pilot manages the system
CENTRAL COMPUTERS (Brains)
Boeing
FMC – Flight Management Computer
Calculates:
- lateral route (LNAV)
- vertical profile (VNAV)
- fuel & performance
Usually dual FMCs with cross-talk
Airbus
FMGC – Flight Management & Guidance Computer
Combines:
- flight management
- guidance laws
Usually dual FMGCs
👉 Same role, Airbus integrates guidance more tightly
PILOT INTERFACE (Input)
Boeing
CDU – Control Display Unit
Used to:
- enter route
- enter performance
- modify waypoints
Works with FMC logic
Airbus
MCDU – Multi-function Control Display Unit
Used to:
- initialise FMGS
- manage F-PLN and PERF
Strongly structured workflow
👉 CDU = pilot-driven 👉 MCDU = system-driven
MODE SELECTION (Autoflight Control)
Boeing
MCP – Mode Control Panel
Pilot sets:
- speed
- heading
- altitude
Then selects mode (LNAV, VNAV, FLCH)
Airbus
FCU – Flight Control Unit
Pilot:
- push = managed
- pull = selected
Windows may be dashed (managed)
👉 Boeing: windows always command 👉 Airbus: windows may be advisory
AUTOPILOT & GUIDANCE
Boeing
- AFDS (Autopilot + Flight Director)
- Executes FMC commands if selected
- Pilot can override instantly
Airbus
- AP / FD integrated with FMGC
- Guidance laws apply protections
- Degrades through flight control laws
SPEED & THRUST CONTROL
Boeing
- Autothrottle (A/T)
- Moves thrust levers
- Speed controlled via MCP or FMC
Airbus
- Autothrust (A/THR)
- Thrust levers fixed in detents
- Speed controlled electronically
DISPLAY SYSTEMS
Both
- PFD – attitude, speed, altitude, FMA
- ND – route, waypoints, constraints, weather
👉 FMA is critical on both — more so on Airbus
SUPPORTING INPUT SYSTEMS (Both)
- IRS / ADIRS – position & attitude
- ADCs – airspeed & altitude
- GNSS
- Radio NAVAIDs
- Fuel & configuration sensors
- Aircraft clock (time reference)
EXAM COMPARISON TABLE (Components)
| Function | Boeing | Airbus |
|---|---|---|
| FMS computer | FMC | FMGC |
| Pilot interface | CDU | MCDU |
| Mode panel | MCP | FCU |
| Autoflight | AFDS | AP/FD |
| Thrust system | A/T | A/THR |
| Guidance logic | Pilot-led | System-managed |
ONE-LINE MEMORY HOOKS (EXAM GOLD)
- Boeing: “Pilot commands computers”
- Airbus: “Pilot manages computers”