Fms Autoflight Flows
βοΈ How FMS, Autoflight, Modes & Panels Work Together
Big Picture (one sentence)
The FMS plans the flight, the panels select authority, the autoflight flies the airplane, and autoland is the fully automatic end-state of that cooperation.
1. FMS (FMC / FMGS) β Planner
- Stores route, constraints, performance
- Computes LNAV / VNAV / speed targets
- Sends guidance commands to autoflight
- Does not move control surfaces itself
π FMS = brain
2. Panels (MCP / FCU) β Authority Selector
Pilot interface between FMS and autoflight
Determines who is in control:
- Boeing MCP: pilot sets targets (windows rule)
- Airbus FCU: pilot chooses managed vs selected
Mode changes happen only via the panel
π Panels = permission gate
3. Modes (LNAV, VNAV, CLB, DES, FLCH, etc.) β Rules
Modes define how the aircraft flies:
- lateral
- vertical
- speed
Displayed on FMA
If a mode is not on the FMA, it is not active
π Modes = rules of flight
4. Autoflight (AP / FD / A-T or A-THR) β Executor
Takes commands from:
- FMS (managed), or
- Panel selections (selected)
Moves:
- control surfaces (pitch/roll)
- thrust (speed/path control)
FD shows what AP is commanding
π Autoflight = muscles
5. Autoland β Full Automation Outcome
Special case where:
- FMS guidance
- ILS data
- Multiple autopilots
- Autothrust all work together automatically
Modes progress:
- APP β LAND β FLARE β ROLLOUT
Pilot monitors system integrity (AH, status)
π Autoland = autoflight at maximum authority
End-to-End Flow (exam perfect)
FMS plans path
β
Panel selects authority (managed / selected)
β
Modes define how to fly
β
Autoflight executes pitch, roll, thrust
β
Autoland = full automatic landing using same logic
One-Line Exam Answer
The FMS plans the flight path, the MCP/FCU selects authority and modes, the autoflight system executes the commands, and autoland is the fully automated landing using the same systems at maximum redundancy.
βοΈ PF / PM Operational Flow (Short & Clear)
1. Departure (Take-off & Climb)
Pilot Flying (PF)
- Flies manually or monitors autopilot
- Follows FD guidance
- Requests mode changes as needed
- Maintains aircraft control at all times
Pilot Monitoring (PM)
Sets modes on MCP / FCU
Verifies:
- FMS route active
- Correct thrust, LNAV/NAV, VNAV/CLB
Calls out FMA mode changes
Monitors flight path, speed, altitude
System Flow
FMS β computes SID & climb profile
Panel β modes selected (LNAV/NAV, VNAV/CLB)
Autoflight β flies pitch, roll, thrust
2. En-Route (Brief Context)
- PF: monitors automation, manages flight path
- PM: monitors modes, handles radios & systems
- Both verify FMA after any clearance or change
3. Approach & Landing
Pilot Flying (PF)
- Flies manually or supervises autopilot
- Ensures stable approach
- Takes over if required
Pilot Monitoring (PM)
Arms APP mode
Confirms:
- LOC / GS capture
- Autoland status (if used)
Calls out:
- modes
- deviations
- minima
System Flow
FMS β provides approach data
ILS β provides LOC / GS
Panel β APP selected
Autoflight β LOC, GS, FLARE, ROLLOUT
4. Autoland (If Used)
- PF: monitors, ready to take over
- PM: monitors system status (LAND 3 / CAT 3)
- Both monitor Alert Height / DH logic
Key Exam Lines (Memorise)
- PF flies or supervises
- PM manages modes and monitors FMA
- Every mode change is verified on the FMA
- Autoflight flies β pilots decide
One-Line Exam Answer
During departure and approach, the PF flies or supervises the aircraft while the PM manages modes and monitors automation, with the FMS planning the path and the autoflight system executing it.
βοΈ Panels, Mode Selectors & Annunciators
(FMS β Autopilot β Autoland)
1. FMS (Flight Management System)
Panels / Interfaces
- Boeing: CDU (Control Display Unit)
- Airbus: MCDU (Multi-function CDU)
What they do
- Enter route, SID/STAR, performance
- Modify flight plan
- Monitor predictions (fuel, ETA)
Annunciators / Displays
- ND β route, waypoints, constraints
- PFD (FMA) β shows if FMS guidance is being used (LNAV/VNAV, NAV/CLB/DES)
2. Autopilot / Autoflight
Panels (Mode Selection)
Boeing
MCP (Mode Control Panel)
- ALT window
- SPD window
- HDG window
- Buttons: LNAV, VNAV, FLCH, V/S, APP
- AP engagement: CMD A / CMD B
- A/T ARM switch
Airbus
FCU (Flight Control Unit)
- ALT, SPD, HDG knobs
- Push = managed
- Pull = selected
- AP buttons: AP1 / AP2
- A/THR button
Annunciators (Both β Critical)
FMA (Flight Mode Annunciator) on PFD Shows:
- Lateral mode (LNAV / NAV / LOC)
- Vertical mode (VNAV / CLB / DES / GS)
- Speed/thrust mode
- Armed modes
π If itβs not on the FMA, itβs not active
3. Autoland
Panels Used
Same panels as autopilot:
- MCP / FCU
APP mode selector
Dual autopilot engagement
- Boeing: CMD A + CMD B
- Airbus: AP1 + AP2
Annunciators (Autoland Status)
Boeing (PFD)
- LAND 3 β Fail-operational
- LAND 2 β Fail-passive
- NO AUTOLAND
Airbus (FMA)
- CAT 3 DUAL β Fail-operational
- CAT 3 SINGLE β Fail-passive
- CAT 2
Autoland Mode Sequence (FMA)
- APP armed
- LOC / GS
- LAND
- FLARE
- ROLLOUT
4. Quick Exam Table
| Function | Boeing | Airbus | Annunciator |
|---|---|---|---|
| FMS input | CDU | MCDU | ND / FMA |
| Mode selection | MCP | FCU | FMA |
| AP engagement | CMD A/B | AP1 / AP2 | FMA |
| Thrust | A/T | A/THR | FMA |
| Autoland status | LAND 2 / 3 | CAT 3 SINGLE / DUAL | PFD / FMA |
One-Line Exam Answer
The CDU/MCDU programs the FMS, the MCP/FCU selects modes and authority, the FMA announces what the aircraft is doing, and autoland uses the same panels with dual autopilots and dedicated LAND/CAT annunciations.