BoredAviator
Automatic Flight
AFDS
ConditionCondition
Modes LNAV / VNAV — latéral et vertical FMC via AFDS ; interaction MCP, FMA et A/T.LNAV / VNAV modes — FMC lateral and vertical via AFDS; MCP, FMA and A/T interaction.
ObjectifObjective
Distinguer LNAV vs HDG SEL vs VOR LOC, VNAV PTH/SPD vs LVL CHG/V/S, et le plafond ALT MCP.Distinguish LNAV vs HDG SEL vs VOR LOC, VNAV PTH/SPD vs LVL CHG/V/S, and the MCP ALT ceiling.
LIVE Push LNAV / VNAV · lire FMAPush LNAV / VNAV · read FMA
Schéma modes FMC ↔ AFDSFMC ↔ AFDS mode schematic
FMC / CDU MCP FCC → LNAV FCC → VNAV LAT · LNAV active route legs FMA ROLL column VERT · VNAV PTH / SPD · MCP ALT FMA PITCH column Valid RTE + performance / constraints — else LNAV/VNAV will not arm or will drop.
FMC fournit la trajectoire ; MCP arme ; FCC vole ; FMA confirme.FMC supplies path; MCP arms; FCC flies; FMA confirms.
LNAV
VNAV

VNAV PTH

  • Suit le path vertical FMC (contraintes, idle path, etc.).Follows FMC vertical path (constraints, idle path, etc.).
  • Altitude MCP reste le plafond / contrainte sélectionnée équipage.MCP altitude remains the crew-selected ceiling / constraint.

VNAV SPD

  • Priorise la vitesse (souvent montée) plutôt que le path exact.Prioritizes speed (often climb) over exact path.
  • Lire la colonne pitch — ne pas assumer PTH.Read the pitch column — do not assume PTH.
Interactions A/TA/T interactions
ModeA/T typiqueNoteNote
VNAV climbN1Limite N1 FMC (sauf A/T LIM)FMC N1 limit (unless A/T LIM)
VNAV cruiseN1 / SPEEDSelon thrust mode / economyPer thrust mode / economy
VNAV descentARM / SPEEDSouvent idle path + speed windowOften idle path + speed window
LVL CHG climbN1Vers ALT MCPToward MCP ALT
LVL CHG descSPEED / idleSurveille underspeedWatch underspeed
Checks équipageCrew checks
  1. CDU : RTE active, pas de discontinuity non voulue, perf OK.CDU: active RTE, no unwanted discontinuity, perf OK.
  2. MCP : ALT correct (contrainte / clearance) ; IAS cohérent.MCP: correct ALT (constraint / clearance); coherent IAS.
  3. Push LNAV / VNAV → FMA armé puis capturé.Push LNAV / VNAV → FMA armed then captured.
  4. Si A/T LIM + symptômes TAT → croiser sonde température.If A/T LIM + TAT symptoms → cross-check temp probe.
LNAV vs HDG SEL vs VOR LOCLNAV vs HDG SEL vs VOR LOC
ModeSourceSourceQuand l’utiliserWhen to use
LNAVFMC legsSID/STAR/RTE, approche LNAV, RNAVSID/STAR/RTE, LNAV approach, RNAV
HDG SELMCP headingVecteurs ATC, recovery perte LNAVATC vectors, LNAV-loss recovery
VOR/LOCNav radioVOR track / LOC avant APP completVOR track / LOC before full APP
LOCILSAprès APP — capture localizerAfter APP — localizer capture
VNAV vs LVL CHG vs V/SVNAV vs LVL CHG vs V/S
ModePilotageGuidancePlafondCeiling
VNAV PTH/SPDFMCMCP ALT + contraintes
LVL CHGThrust/speed vers ALTThrust/speed toward ALTMCP ALT
V/SThumbwheelMCP ALT (capture)
ALT HOLDMaintienHoldAltitude actuelle

Scénarios teachingTeaching scenarios

MCP ALT = CREW CEILING SELECTED ALT VNAV / LVL CHG / V/S will not climb through MCP window Set clearance / constraint before arming vertical mode
Fenêtre altitude MCP = plafond — toujours avant le mode vertical.MCP altitude window = ceiling — always before vertical mode.
LNAV/VNAV = teaching AFDS. Pour switches LIVE → simulateur MCP. FMC détail → chapitre FMC/CDU.LNAV/VNAV = AFDS teaching. For LIVE switches → MCP simulator. FMC detail → FMC/CDU chapter.
FMA · MCP · Système · Course / MEL 34-17FMA · MCP · System · Course / MEL 34-17