ATP Piper Seminole Training Supplement - ATP Flight Piper Seminole Training Supplement - ATP Flight School

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  • 800-255-2877 904-595-7940

    T h e M o s t R e s p e c t e d N a m e i n P i l o t C e r t i f i c a t i o n

    Piper SeminoleTraining Supplement

    $29.95Revised 2015-06-03

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  • Introduction

    Thank you for choosing ATP for your flight program.

    ATP flies over 11,000 hours per month to provide over 4,500 FAA certificates each year. ATP is committed to providing you low prices; efficient, standardized, and effective flight programs; andmost importantlythe highest level of safety.

    To maximize the effectiveness of your flight program, ATPs Piper Seminole Training Supplement contains a condensed overview of multi-engine aerodynamics, portions of the Piper Seminole POH, and flight procedures. You must have a complete knowledge of all information contained in this supplement prior to the start of your program. This information will assist you with your training and flight check.

    It is critical that you memorize the following:

    Emergency Engine Failure Checklists. V-Speeds. Answers to all questions contained in the Oral Review section in the

    back of the supplement.

    The information in this supplement is highly condensed and serves as a good quick reference, but it must not be used as a substitute for the FAA-approved pilot's operating handbook required for safe operation of the airplane.

    Thank you for giving ATP an opportunity to serve you.

  • Contents Revised 2015-06-03Engine-Out Aerodynamics ............... 1

    Aerodynamic Effects of an Engine Failure .. 1Approximate Drag Factors .......................... 2Airspeeds for Max SE Performance ............. 2Sideslip Versus Zero Sideslip ...................... 3Single-Engine Service Ceiling ...................... 4Single-Engine Absolute Ceiling .................... 4Climb Performance Factors ......................... 4Critical Engine .............................................. 4VMC ............................................................... 6

    Aircraft Systems .................................. 8Engines ........................................................ 8Propellers .................................................... 9Landing Gear ............................................. 10Brakes ....................................................... 11Flaps .......................................................... 11Vacuum Pumps .......................................... 11Pitot Static ................................................. 11Fuel System ............................................... 12Electrical System .......................................12Heater ....................................................... 13Stall Warning Horn.....................................13Emergency Exit .......................................... 14Inoperative Instruments & Equipment ......14Garmin G500 ............................................. 14Standby Instruments .................................17G500 Failures & Partial-Panel ...................18Differences in '79 & '00 Seminoles ...........21

    Performance / Weight & Balance ...22Piper Seminole V-Speeds ..........................22Performance Charts ..................................23Sample Weight & Balance Problem ...........23Formulas ................................................... 24CG Envelope Graph ....................................24

    Flight Check Tasks & Procedures ...25Passenger Briefing ....................................25Pre-Takeoff Briefing ..................................25Normal Takeoff (Flaps 0) ........................26Engine Failure Procedure ..........................27Approach Briefing .....................................28Announced Calls on Approach ..................28

    Stabilized Approach Corridor ....................28Go Around Philosophy ...............................29Normal Landing ......................................... 29Normal Visual Approach & Landing ..........30ILS Approach One or Two Engines ............32Non-Precision Straight-In Approach .........33Circle to Land Approaches Two Engines ...34Go Around / Missed Approach ..................35Holding ...................................................... 35Approach, PT & Holding Power Settings ...35In-Flight Maneuvers ...................................35Clearing Turns for In-Flight Maneuvers .....36VMC Demonstration ....................................36Maneuvering with One Engine Inop ...........37In-Flight Engine Failure Demo ...................37Example SE Drift Down Scenario ...............39Airstart Procedure ....................................39Emergency Descent...................................40Recovery from Unusual Attitudes ..............40Spin Awareness ......................................... 41

    Private Pilot Multi-Engine Add-On .42Steep Turns ............................................... 42Maneuvering During Slow Flight ................42Stall Recovery ............................................ 43Power-Off Stall .......................................... 44Power-On Stall ........................................... 44

    Commercial Multi-Engine Add-On .46Steep Turns ............................................... 46Maneuvering During Slow Flight ................46Power-Off Stall .......................................... 47Power-On Stall ........................................... 48Accelerated Stall ........................................48Short Field Takeoff & Climb (Flaps 0) .....49Short Field Visual Approach & Landing ....50

    CFI Multi-Engine Add-On ................51Airspeed Drag Demonstration ..................51

    Airline Transport Pilot ......................52Steep Turns ............................................... 52Approach to Stall in Approach Config .......52Approach to Stall in Landing Config ..........53

    Oral Review ........................................54Sample Oral Questions ..............................55

  • Engine-Out Aerodynamics 1

    SECTION 1

    Engine-Out Aerodynamics

    Aerodynamic Effects of an Engine FailureWhen an engine failure occurs in a multi-engine aircraft, asymmetric thrust and drag cause the following effects on the aircrafts axes of rotation:

    Pitch Down (Lateral Axis)Loss of accelerated slipstream over the horizontal stabilizer causes it to produce less negative lift, causing the aircraft to pitch down. To compensate for the pitch down effect, additional back pressure is required.

    The Seminole has a lesser pitch-down effect than most light twins because the T-tail configuration removes the horizontal stabilator from the accelerated slipstream.

    Roll Toward the Failed Engine (Longitudinal Axis)The wing produces less lift on the side of the failed engine due to the loss of accelerated slipstream. Reduced lift causes a roll toward the failed engine and requires additional aileron deflection into the operating engine.

    Yaw Toward the Dead Engine (Vertical Axis)Loss of thrust and increased drag from the windmilling propeller cause the aircraft to yaw toward the failed engine. This requires additional rudder pressure on the side of the operating engine. Dead foot, dead engine.

    e-learning

    VIDEO: Visit ATPFlightSchool.com/students for an interactive multi-engine aerodynamics presentation. Requires Flash Player.

  • 2 Engine-Out Aerodynamics

    Engine Inoperative Climb PerformanceClimb performance depends on the excess power needed to overcome drag. When a multi-engine airplane loses an engine, the airplane loses 50% of its available power. This power loss results in a loss of approximately 80% of the aircrafts excess power and climb performance. Drag is a major factor relative to the amount of excess power available. An increase in drag (such as the loss of one engine) must be offset by additional power. This additional power is now taken from the excess power, making it unavailable to aid the aircraft in climb. When an engine is lost, maximize thrust (full power) and minimize drag (flaps and gear up, prop feathered, etc.) in order to achieve optimum single-engine climb performance.

    Approximate Drag Factors per the Piper Seminole POH1. Flaps 25 ................................. -240 FPM2. Flaps 40 ................................. -275 FPM3. Windmilling Prop ................ -200 FPM4. Gear Extended ..................... -250 FPM

    ATPs experience indicates more than -200 FPM drag from the windmilling prop.

    Under FAR Part 23:The FAA does not require multi-engine airplanes that weigh less than 6,000 pounds or have a VSO speed under 61 knots to meet any specified single-engine performance criteria. No single engine climb performance is required. Actual climb performance is documented by the manufacturer.

    The Seminoles max TOW is 3,800 pounds and VSO speed is 55 KIAS. Review the POH for single-engine climb performance for specific conditions.

    Airspeeds for Max Single-Engine PerformanceVXSEThe airspeed for the steepest angle of climb on single-engine.

    VYSEThe airspeed for the best rate of climb on single-engine. (Or for the slowest loss of altitude on drift-down.) Blueline is the markin

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