Define V1, Vr, V2 for FAR 121 ops. Why does V1 vary with runway and weight?
What they are really probing: Standard FAR/121 frame.
Model answer
V1 (Decision Speed): max speed to abort, min speed to continue. Defined by balanced field or limited by ASD/AGD. Vr (Rotation Speed): speed at which the pilot pulls back to initiate rotation. V2 (Safety Speed): min single-engine climb speed, achieved by 35 ft AGL after liftoff, required for second-segment climb gradient (FAR 25.121 — 2.4% for two-engine). V1 is bounded: above Vmcg (else can't maintain centerline if engine fails after V1), below Vr (else committed to abort with no room to take off). Runway length: shorter = lower V1 (must stop within ASDA), but cannot go below Vmcg. Weight: heavier = higher Vmcg, Vr, V2; longer ASD; V1 increases to balance. Slope: upslope helps stop, hurts go; downslope opposite. Tie to ATL: at 1000 ft elevation, V1 typically +5 kts vs sea level for same weight.
What fails this question
- — Vague definitions
- — Forgetting Vmcg constraint
- — Not knowing 2.4% second-segment gradient
Follow-ups they ask next
- — What's Vmcg?
- — Define second-segment climb.
- — Define ASDA.