PA34 · Normal Procedures · 15 of 16
VMCA Demonstration and VSSE
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- 03 · LOCKEDBefore Starting and the Normal Engine Start
- 04 · LOCKEDStarting with the Optional Primer System
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- 12 · LOCKEDApproach, Landing and Go-Around
- 13 · LOCKEDAfter Landing, Shutdown and Mooring
- 14 · LOCKEDTurbulence, Doors-Off Flight and Stalls
15 · Reading now
VMCA Demonstration and VSSE
Single-engine training revolves around two speeds: VSSE, the floor for intentional one engine flight, and VMCA, which the demonstration approaches at a safe height. The danger is where the stall and VMCA arrive together.
At a glance
- VSSE85 KIAS
- VMCA66 KIAS
- Minimum altitude for the demonstration3500 ft above the ground
- Rate of slowingapproximately 1 knot per second
- Bank toward the operative engine5°
The two speeds
VSSE, the intentional one engine inoperative speed, is 85 KIAS for the Seneca III. VMCA has been determined to be 66 KIAS. In training or in an emergency on one engine, keep the indicated airspeed above 85 KIAS.
Setting up the demonstration
Never below 3500 feet above the ground.
Landing gear — UP
Flaps — UP
Airspeed — at or above 85 KIAS (VSSE)
Propeller controls — HIGH RPM
Throttle (simulated inoperative engine) — IDLE
Throttle (other engine) — MAX ALLOWABLE
Airspeed — reduce about 1 knot per second until either VMCA or the STALL WARNING is reached
CAUTION — Use rudder to hold the heading and ailerons to keep a 5° bank toward the operative engine.
Recovery
Immediately reduce power on the operating engine and lower the nose to accelerate to VSSE.
The most critical case is where the stall speed and VMCA coincide: directional control is lost at the stall, and a spin could result.
Check yourself
What are VSSE and VMCA?
What is the minimum height for a VMCA demonstration?
How are the throttles set, and how quickly is the airspeed reduced?
What ends the slowdown?
Describe the recovery, and the most critical situation.
Study aid — always fly your aircraft's current AFM/POH.
Source: Piper PA-34-220T Seneca III Pilot's Operating Handbook and FAA Approved Airplane Flight Manual, Report VB-1150, p. 4-36..4-37, Rev. 16 (15 May 1998)
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