PA44 · Emergency Procedures · 03 of 24

One-Engine Speeds, Identification and Bank

  1. 01 · LOCKEDWarnings: CAS and Engine Display
  2. 02 · LOCKEDCautions, Advisories and How Soon to Land
  3. 03 · READING NOW

    One-Engine Speeds, Identification and Bank

    Every engine-failure drill leans on three speeds, one identification rule and two bank angles. These belong together: the speed keeps the airplane controllable and climbing, the rule finds the dead engine, and the bank angle depends on whether you are fighting for control or for climb.

    At a glance

    • VMCA56 KIAS
    • VYSE (one engine inop best rate)88 KIAS
    • VXSE (one engine inop best angle)82 KIAS
    • Maneuvering speed, 3800 lb135 KIAS
    • Maneuvering speed, 2870 lb115 KIAS
    • Never exceed202 KIAS
    • Bank for control (near/below VMC)about 5° toward the operating engine
    • Bank for climb (secured)2° to 3° toward the operating engine

    Airspeeds for safe operation

    • One engine inoperative air minimum control (VMCA) — 56 KIAS.

    • One engine inoperative best rate of climb — 88 KIAS.

    • One engine inoperative best angle of climb — 82 KIAS.

    • Maneuvering — 135 KIAS at 3800 lb, 115 KIAS at 2870 lb.

    • Never exceed — 202 KIAS.

    Do not let the airspeed fall below VXSE, 82 KIAS: any slower and climb performance is significantly reduced. Once the obstacles are cleared, accelerate to the single-engine best rate of climb speed.

    Finding the dead engine

    The failed engine is identified by the rudder you need to hold direction: pressure is required toward the operating engine — dead foot, dead engine. EGT and oil pressure indications help confirm it. Then verify complete power loss by retarding that engine's throttle and noting no change in the engine or the airplane.

    Two bank angles, two jobs

    • Maximum controllability, near or below VMC — bank about 5° into the operating engine; the slip-indicator trapezoid sits 1/2 to 3/4 of a width toward the operating engine.

    • Maximum climb performance, under control and secured — hold 2° to 3° of bank toward the operating engine, about 1/2 trapezoid.

    Continue or discontinue?

    After an engine failure on takeoff, discontinuing is advisable under most circumstances. Continuing the takeoff is not advisable if the engine fails before obstacle speed is reached and the gear is retracted.

    Check yourself

    • What are VMCA, VYSE and VXSE on this airplane?

    • Below which speed does single-engine climb performance drop significantly?

    • How is the inoperative engine identified, and how is the failure verified?

    • How much bank do you use for maximum control, and how much for maximum climb?

    • When is continuing a takeoff after an engine failure not advisable?


    Study aid — always fly your aircraft's current AFM/POH.

    Source: Piper PA-44-180 Seminole Pilot's Operating Handbook and FAA Approved Airplane Flight Manual, Report VB-2636, p. 3-7, 3-17, Rev. 7 (26 February 2021)

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  4. 04 · LOCKEDThe Engine Securing Procedure
  5. 05 · LOCKEDEngine Failure During Takeoff
  6. 06 · LOCKEDEngine Failure in the Climb and Below VMCA
  7. 07 · LOCKEDEngine Failure in Flight Above VMCA
  8. 08 · LOCKEDOne Engine Inoperative Landing and Go-Around
  9. 09 · LOCKEDAir Starts
  10. 10 · LOCKEDEngine Roughness, Oil Problems and Propeller Overspeed
  11. 11 · LOCKEDFuel Flow and Fuel Quantity
  12. 12 · LOCKEDEngine and Electrical Fires
  13. 13 · LOCKEDLanding Gear Unsafe and Manual Extension
  14. 14 · LOCKEDCircuit Breakers and Alternator Failures
  15. 15 · LOCKEDEmergency Battery and Complete Electrical Failure
  16. 16 · LOCKEDPFD and MFD Failures
  17. 17 · LOCKEDAHRS, ADC, Engine Display and CAS Failures
  18. 18 · LOCKEDCOM and GPS Failures
  19. 19 · LOCKEDAutopilot and Trim Malfunctions
  20. 20 · LOCKEDAutopilot Speed Recovery and Loss of Navigation
  21. 21 · LOCKEDCooling Fans, Pitot Heat and Starter Engaged
  22. 22 · LOCKEDSpin Recovery and Emergency Descent
  23. 23 · LOCKEDOpen Door and Emergency Exit
  24. 24 · LOCKEDHeater Overheat and CO Detector