Flight Deck Management

• PA.II.B.S1:

  Secure all items in the aircraft.
• PA.II.B.S2:

  Conduct an appropriate passenger briefing, including identifying the pilot-in-command (PIC), use of safety belts, shoulder harnesses, doors, passenger conduct, sterile aircraft, propeller blade avoidance, and emergency procedures.
• PA.II.B.S3:

  Properly program and manage the aircraft's automation, as applicable.
• PA.II.B.S4:

  Appropriately manage risks by utilizing ADM, including SRM/CRM.

• PH.II.B.S1:

  Secure all items in the aircraft.
• PH.II.B.S2:

  Conduct an appropriate passenger briefing, including identifying the pilot-in-command (PIC), use of safety belts, shoulder harnesses, doors, passenger conduct, rotor blade avoidance, and emergency procedures.
• PH.II.B.S3:

  Properly program and manage helicopter automation, as applicable.
• PH.II.B.S4:

  Appropriately manage risks by utilizing ADM, including SRM/CRM.

• CA.II.B.S1:

  Secure all items in the aircraft.
• CA.II.B.S2:

  Conduct an appropriate passenger briefing, including identifying the pilot-in-command (PIC), use of safety belts, shoulder harnesses, doors, passenger conduct, sterile aircraft, propeller blade avoidance, and emergency procedures.
• CA.II.B.S3:

  Properly program and manage the aircraft's automation, as applicable.
• CA.II.B.S4:

  Appropriately manage risks by utilizing ADM, including SRM/CRM.

• IR.II.C.S1:

  Perform preflight inspection by following the checklist appropriate to the aircraft and determine if the aircraft is in a condition for safe instrument flight.

• SP.1:

  Exhibits knowledge of the elements related to efficient flight deck management procedures and related safety factors.
• SP.2:

  Organizes and arranges material and equipment in a manner that makes the items readily available.
• SP.3:

  Briefs the occupant on the use of safety belts, shoulder harnesses, and any other required safety equipment, doors, and emergency procedures.

• SH.II.B.S1:

  Secure all items in the aircraft.
• SH.II.B.S2:

  Conduct an appropriate passenger briefing, including identifying the pilot-in-command (PIC), use of safety belts, shoulder harnesses, doors, passenger conduct, rotor blade avoidance, and emergency procedures, with the exception of single-seat aircraft.
• SH.II.B.S3:

  Properly program and manage helicopter-simplified flight controls automation, as applicable.
• SH.II.B.S4:

  Appropriately manage risks by utilizing ADM, including SRM/CRM.

• CA.III.B.S1:

  Identify and interpret airport/seaplane base runways, taxiways, markings, signs, and lighting.
• CA.III.B.S2:

  Comply with recommended traffic pattern procedures.
• CA.III.B.S3:

  Correct for wind drift to maintain the proper ground track.
• CA.III.B.S4:

  Maintain orientation with the runway/landing area in use.
• CA.III.B.S5:

  Maintain traffic pattern altitude, ±100 feet, and the appropriate airspeed, ±10 knots.
• CA.III.B.S6:

  Maintain situational awareness and proper spacing from other aircraft in the traffic pattern.

• CA.IX.G.S1:

  Promptly recognize an engine failure and maintain positive airplane control.
• CA.IX.G.S2:

  Set the engine controls, reduce drag, identify and verify the inoperative engine, and simulate feathering of the propeller on the inoperative engine (evaluator should then establish zero thrust on the inoperative engine).
• CA.IX.G.S3:

  Use flight controls in the proper combination as recommended by the manufacturer, or as required to maintain best performance, and trim as required.
• CA.IX.G.S4:

  Follow the manufacturer's recommended emergency procedures and complete the appropriate checklist.
• CA.IX.G.S5:

  Monitor the operating engine and make adjustments as necessary.
• CA.IX.G.S6:

  Maintain the manufacturer's recommended approach airspeed ±5 knots, in the landing configuration with a stabilized approach, until landing is assured.
• CA.IX.G.S7:

  Make smooth, timely, and correct control application before, during, and after touchdown.
• CA.IX.G.S8:

  Touch down on the first one-third of available runway/landing surface, with no drift, and the airplane's longitudinal axis aligned with and over the runway center or landing path.
• CA.IX.G.S9:

  Maintain directional control and appropriate crosswind correction throughout the approach and landing.
• CA.IX.G.S10:

  Complete the appropriate checklist(s).

• CA.IX.B.S1:

  Establish and maintain the recommended best glide airspeed, ±10 knots.
• CA.IX.B.S2:

  Configure the airplane in accordance with the Pilot's Operating Handbook (POH)\Airplane Flight Manual (AFM) and existing conditions.
• CA.IX.B.S3:

  Select a suitable landing area considering altitude, wind, terrain, obstructions, and available glide distance.
• CA.IX.B.S4:

  Plan and follow a flightpath to the selected landing area considering altitude, wind, terrain, and obstructions.
• CA.IX.B.S5:

  Prepare for landing as specified by the evaluator.
• CA.IX.B.S6:

  Complete the appropriate checklist(s).

• CA.IX.A.S1:

  Clear the area.
• CA.IX.A.S2:

  Establish and maintain the appropriate airspeed and configuration appropriate to the scenario specified by the evaluator and as covered in Pilot's Operating Handbook (POH)/Airplane Flight Manual (AFM) for the emergency descent.
• CA.IX.A.S3:

  Maintain orientation, divide attention appropriately, and plan and execute a smooth recovery.
• CA.IX.A.S4:

  Use bank angle between 30° and 45° to maintain positive load factors during the descent.
• CA.IX.A.S5:

  Maintain appropriate airspeed +0/-10 knots, and level off at a specified altitude ±100 feet.
• CA.IX.A.S6:

  Complete the appropriate checklist(s).
• CA.IX.A.S7:

  Use single-pilot resource management (SRM) or crew resource management (CRM), as appropriate.

• CA.IX.F.S1:

  Promptly recognize an engine failure, maintain control, and use appropriate emergency procedures.
• CA.IX.F.S2:

  Establish VYSE; if obstructions are present, establish best single-engine angle of climb speed (VXSE) or VMC +5 knots, whichever is greater, until obstructions are cleared. Then transition to VYSE.
• CA.IX.F.S3:

  Reduce drag by retracting landing gear and flaps in accordance with the manufacturer's guidance.
• CA.IX.F.S4:

  Simulate feathering the propeller on the inoperative engine (evaluator should then establish zero thrust on the inoperative engine).
• CA.IX.F.S5:

  Use flight controls in the proper combination as recommended by the manufacturer, or as required to maintain best performance, and trim as required.
• CA.IX.F.S6:

  Monitor the operating engine and aircraft systems and make adjustments as necessary.
• CA.IX.F.S7:

  Recognize the airplane's performance capabilities. If a climb is not possible at VYSE, maintain VYSE and return to the departure airport for landing, or initiate an approach to the most suitable landing area available.
• CA.IX.F.S8:

  Simulate securing the inoperative engine.
• CA.IX.F.S9:

  Maintain heading ±10° and airspeed ±5 knots.
• CA.IX.F.S10:

  Complete the appropriate checklist(s).

• CA.IX.E.S1:

  Close the throttles smoothly and promptly when a simulated engine failure occurs.
• CA.IX.E.S2:

  Maintain directional control and apply brakes (AMEL), or flight controls (AMES), as necessary.

• CA.IX.C.S1:

  Describe appropriate action for simulated emergencies specified by the evaluator, from at least three of the elements or sub-elements listed in K1 through K5 above.
• CA.IX.C.S2:

  Complete the appropriate checklist(s).

• CA.X.D.S1:

  Promptly recognize an engine failure and maintain positive aircraft control.
• CA.X.D.S2:

  Set the engine controls, reduce drag, identify and verify the inoperative engine, and simulate feathering of the propeller on the inoperative engine (evaluator should then establish zero thrust on the inoperative engine).
• CA.X.D.S3:

  Use flight controls in the proper combination as recommended by the manufacturer, or as required to .
• CA.X.D.S4:

  Follow the manufacturer's recommended emergency procedures and complete the appropriate checklist.
• CA.X.D.S5:

  Monitor the operating engine and aircraft systems and make adjustments as necessary.
• CA.X.D.S6:

  Request and follow an actual or a simulated air traffic control (ATC) clearance for an instrument approach.
• CA.X.D.S7:

  Maintain altitude ±100 feet or minimum sink rate if applicable, airspeed ±10 knots, and selected heading ±10°.
• CA.X.D.S8:

  Establish a rate of descent that ensures arrival at the minimum descent altitude (MDA) or decision altitude (DA)/decision height (DH) with the airplane in a position from which a descent to a landing on the intended runway or landing path can be made, either straight in or circling as appropriate.
• CA.X.D.S9:

  On final approach segment, maintain vertical (as applicable) and lateral guidance within 3/4-scale deflection.
• CA.X.D.S10:

  Avoid loss of airplane control or attempted flight contrary to the operating limitations of the airplane.
• CA.X.D.S11:

  Comply with the published criteria for the aircraft approach category if circling.
• CA.X.D.S12:

  Execute a landing.
• CA.X.D.S13:

  Complete the appropriate checklist(s).

• CA.X.A.S1:

  Recognize an engine failure, maintain control, use manufacturer's memory item procedures, and use appropriate emergency procedures.
• CA.X.A.S2:

  Set the engine controls, identify and verify the inoperative engine, and feather the appropriate propeller.
• CA.X.A.S3:

  Use flight controls in the proper combination as recommended by the manufacturer, or as required to maintain best performance, and trim as required.
• CA.X.A.S4:

  Attempt to determine and resolve the reason for the engine failure.
• CA.X.A.S5:

  Secure the inoperative engine and monitor the operating engine and make necessary adjustments.
• CA.X.A.S6:

  Restart the inoperative engine using manufacturer's restart procedures.
• CA.X.A.S7:

  Maintain altitude ±100 feet or a minimum sink rate if applicable, airspeed ±10 knots, and selected headings ±10°.
• CA.X.A.S8:

  Complete the appropriate checklist(s).

• CA.X.C.S1:

  Promptly recognize an engine failure and maintain positive airplane control.
• CA.X.C.S2:

  Set the engine controls, reduce drag, identify and verify the inoperative engine, and simulate feathering of the propeller on the inoperative engine (evaluator should then establish zero thrust on the inoperative engine).
• CA.X.C.S3:

  Establish the best engine-inoperative airspeed and trim the airplane.
• CA.X.C.S4:

  Use flight controls in the proper combination as recommended by the manufacturer, or as required to maintain best performance, and trim as required.
• CA.X.C.S5:

  Verify the prescribed checklist procedures used for securing the inoperative engine.
• CA.X.C.S6:

  Attempt to determine and resolve the reason for the engine failure.
• CA.X.C.S7:

  Monitor engine functions and make necessary adjustments.
• CA.X.C.S8:

  Maintain the specified altitude ±100 feet or minimum sink rate if applicable, airspeed ±10 knots, and the specified heading ±10°.
• CA.X.C.S9:

  Assess the airplane's performance capability and decide an appropriate action to ensure a safe landing.
• CA.X.C.S10:

  Avoid loss of airplane control or attempted flight contrary to the engine-inoperative operating limitationsof the airplane.
• CA.X.C.S11:

  Use single-pilot resource management (SRM) or crew resource management (CRM), as appropriate.

• CA.X.B.S1:

  Configure the airplane in accordance with the manufacturer's recommendations, in the absence of the manufacturer's recommendations, then at safe single-engine speed (VSSE/VYSE), as appropriate, and:

  • CA.X.B.S1a:

    Landing gear retracted.
  • CA.X.B.S1b:

    Flaps set for takeoff.
  • CA.X.B.S1c:

    Cowl flaps set for takeoff.
  • CA.X.B.S1d:

    Trim set for takeoff.
  • CA.X.B.S1e:

    Propellers set for high revolutions per minute (rpm).
  • CA.X.B.S1f:

    Power on critical engine reduced to idle and propeller windmilling.
  • CA.X.B.S1g:

    Power on operating engine set to takeoff or maximum available power.
• CA.X.B.S2:

  Establish a single-engine climb attitude with the airspeed at approximately 10 knots above VSSE.
• CA.X.B.S3:

  Establish a bank angle not to exceed 5° toward the operating engine, as required for best performance and controllability.
• CA.X.B.S4:

  Increase the pitch attitude slowly to reduce the airspeed at approximately 1 knot per second while applying increased rudder pressure as needed to maintain directional control.
• CA.X.B.S5:

  Recognize and recover at the first indication of loss of directional control, stall warning, or buffet.
• CA.X.B.S6:

  Recover promptly by simultaneously reducing power sufficiently on the operating engine, decreasing the angle of attack as necessary to regain airspeed and directional control, and without adding power on the simulated failed engine.
• CA.X.B.S7:

  Recover within 20° of entry heading.
• CA.X.B.S8:

  Advance power smoothly on the operating engine and accelerate to VSSE/VYSE, as appropriate, ±5 knots during recovery.

• CA.VI.C.S1:

  Select a suitable destination and route for diversion.
• CA.VI.C.S2:

  Make a reasonable estimate of heading, groundspeed, arrival time, and fuel required to the "divert to" destination.
• CA.VI.C.S3:

  Maintain the selected altitude ±100 feet and heading ±10°.
• CA.VI.C.S4:

  Update/interpret weather in flight.
• CA.VI.C.S5:

  Use displays of digital weather and aeronautical information, as applicable to maintain situational awareness.
• CA.VI.C.S6:

  Promptly divert toward the destination.

• CA.VI.D.S1:

  Use an appropriate method to determine position.
• CA.VI.D.S2:

  Maintain an appropriate heading and climb as necessary.
• CA.VI.D.S3:

  Identify prominent landmarks.
• CA.VI.D.S4:

  Use navigation systems/facilities or contact an ATC facility for assistance.
• CA.VI.D.S5:

  Select an appropriate course of action.

• CA.VI.B.S1:

  Use an airborne electronic navigation system.
• CA.VI.B.S2:

  Determine the airplane's position using the navigation system.
• CA.VI.B.S3:

  Intercept and track a given course, radial, or bearing.
• CA.VI.B.S4:

  Recognize and describe the indication of station or waypoint passage.
• CA.VI.B.S5:

  Recognize signal loss or interference and take appropriate action, if applicable.
• CA.VI.B.S6:

  Use proper communication procedures when utilizing radar services.
• CA.VI.B.S7:

  Maintain the selected altitude ±100 feet and heading ±10°.

• CA.VI.A.S1:

  Prepare and use a flight log.
• CA.VI.A.S2:

  Navigate by pilotage.
• CA.VI.A.S3:

  Navigate by means of pre-computed headings, groundspeeds, elapsed time, and reference to landmarks or checkpoints.
• CA.VI.A.S4:

  Use the magnetic direction indicator in navigation, including turns to headings.
• CA.VI.A.S5:

  Verify position within three nautical miles of the flight-planned route.
• CA.VI.A.S6:

  Arrive at the en route checkpoints within five minutes of the initial or revised estimated time of arrival (ETA) and provide a destination estimate.
• CA.VI.A.S7:

  Maintain the selected altitude ±100 feet and heading ±10°.

• CA.V.C.S1:

  Clear the area.
• CA.V.C.S2:

  Select an altitude that will allow the maneuver to be performed no lower than 1,500 feet above ground level (AGL).
• CA.V.C.S3:

  Establish the appropriate entry configuration, power, and airspeed.
• CA.V.C.S4:

  Establish the angle of bank at approximately 30°.
• CA.V.C.S5:

  Simultaneously apply power and pitch to maintain a smooth, coordinated climbing turn, in either direction, to the 90° point, with a constant bank and continuously decreasing airspeed.
• CA.V.C.S6:

  Begin a coordinated constant rate rollout from the 90° point to the 180° point maintaining power and a constant pitch attitude.
• CA.V.C.S7:

  Complete rollout at the 180° point, ±10° just above a stall airspeed, and maintaining that airspeed momentarily avoiding a stall.
• CA.V.C.S8:

  Resume a straight-and-level flight with minimum loss of altitude.

• CA.V.D.S1:

  Clear the area.
• CA.V.D.S2:

  Select an altitude that will allow the maneuver to be performed no lower than 1,500 feet above ground level (AGL).
• CA.V.D.S3:

  Establish the appropriate entry configuration, power, and airspeed.
• CA.V.D.S4:

  Maintain coordinated flight throughout the maneuver.
• CA.V.D.S5:

  Complete the maneuver in accordance with the following:

  • CA.V.D.S5a:

    Approximately 30° bank at the steepest point.
  • CA.V.D.S5b:

    Constant change of pitch and roll rate and airspeed.
  • CA.V.D.S5c:

    Altitude at 180° point, ±100 feet from entry altitude.
  • CA.V.D.S5d:

    Airspeed at the 180° point, ±10 knots from entry airspeed.
  • CA.V.D.S5e:

    Heading at the 180° point, ±10°.
• CA.V.D.S6:

  Continue the maneuver through the number of symmetrical loops specified, then resume straight-andlevel flight.

• CA.XII.A.S1:

  [Archived].
• CA.XII.A.S2:

  Park in an appropriate area, considering the safety of nearby persons and property.
• CA.XII.A.S3:

  Complete the appropriate checklist(s).
• CA.XII.A.S4:

  Conduct a postflight inspection and document discrepancies and servicing requirements, if any.
• CA.XII.A.S5:

  Secure the airplane.

• CA.XII.B.S1:

  If anchoring, select a suitable area considering seaplane movement, water depth, tide, wind, and weather changes. Use an adequate number of anchors and lines of sufficient strength and length to ensure the seaplane's security.
• CA.XII.B.S2:

  If not anchoring, approach the dock/mooring buoy or beach/ramp in the proper direction and at a safe speed, considering water depth, tide, current, and wind.
• CA.XII.B.S3:

  Complete the appropriate checklist.
• CA.XII.B.S4:

  Conduct a postflight inspection and document discrepancies and servicing requirements, if any.
• CA.XII.B.S5:

  Secure the seaplane considering the effect of wind, waves, and changes in water level, or comply with applicable after landing, parking, and securing procedures if operating an amphibious airplane on land.

• CA.I.H.S1:

  Associate the symptoms and effects for at least three of the conditions listed in K1a through K1l with the cause(s) and corrective action(s).
• CA.I.H.S2:

  Perform self-assessment, including fitness for flight and personal minimums, for actual flight or a scenario given by the evaluator.

• CA.II.E.S1:

  Receive and correctly read back clearances/instructions, if applicable.
• CA.II.E.S2:

  Use an Airport diagram or taxi chart during taxi, if published.
• CA.II.E.S3:

  Comply with seaplane base/airport/taxiway markings, signals, and signs.
• CA.II.E.S4:

  Depart the dock/mooring buoy or beach/ramp in a safe manner, considering wind, current, traffic, and hazards.
• CA.II.E.S5:

  Complete the appropriate checklist(s).
• CA.II.E.S6:

  Position the flight controls, flaps, doors, water rudders, and power correctly for the existing conditions to follow the desired course while sailing and to prevent or correct for porpoising and skipping during step taxi.
• CA.II.E.S7:

  Exhibit procedures for steering and maneuvering while maintaining proper situational awareness and desired orientation, path, and position while taxiing using idle, plow, or step taxi technique, as appropriate.
• CA.II.E.S8:

  Plan and follow the most favorable taxi or sailing course for current conditions.
• CA.II.E.S9:

  Abide by right-of-way rules, maintain positive airplane control, proper speed, and separation between other aircraft, vessels, and persons.
• CA.II.E.S10:

  Comply with applicable taxi elements in Task D if the practical test is conducted in an amphibious airplane.

• CA.II.D.S1:

  Receive and correctly read back clearances/instructions, if applicable.
• CA.II.D.S2:

  Use an airport diagram or taxi chart during taxi, if published, and maintain situational awareness.
• CA.II.D.S3:

  Position the flight controls for the existing wind, if applicable.
• CA.II.D.S4:

  Complete the appropriate checklist(s).
• CA.II.D.S5:

  Perform a brake check immediately after the airplane begins moving.
• CA.II.D.S6:

  Maintain positive control of the airplane during ground operations by controlling direction and speed without excessive use of brakes.
• CA.II.D.S7:

  Comply with airport/taxiway markings, signals, and air traffic control (ATC) clearances and instructions.
• CA.II.D.S8:

  Position the airplane properly relative to hold lines.

• CA.VII.D.S1:

  Clear the area.
• CA.VII.D.S2:

  Select an entry altitude that allows the Task to be completed no lower than 3,000 feet above ground level (AGL).
• CA.VII.D.S3:

  Establish the configuration as specified by the evaluator.
• CA.VII.D.S4:

  Set power appropriate for the configuration, such that the airspeed does not exceed the maneuvering speed (VA) or any other applicable Pilot's Operating Handbook (POH)/Airplane Flight Manual (AFM) limitation.
• CA.VII.D.S5:

  Establish and maintain a coordinated turn in a 45° bank, increasing elevator back pressure smoothly and firmly until an impending stall is reached.
• CA.VII.D.S6:

  Acknowledge the cues at the first indication of a stall (e.g., aircraft buffet, stall horn, etc.).
• CA.VII.D.S7:

  Acknowledge cues of the impending stall and then recover promptly after a full stall occurs.
• CA.VII.D.S8:

  Configure the airplane as recommended by the manufacturer, and accelerate to best angle of climb speed (VX) or best rate of climb speed (VY).
• CA.VII.D.S9:

  Return to the altitude, heading, and airspeed specified by the evaluator.

• CA.VII.A.S1:

  Clear the area.
• CA.VII.A.S2:

  Select an entry altitude that allows the Task to be completed no lower than 1,500 feet above ground level (AGL) (ASEL, ASES) or 3,000 feet AGL (AMEL, AMES).
• CA.VII.A.S3:

  Establish and maintain an airspeed at which any further increase in angle of attack, increase in load factor, or reduction in power, would result in a stall warning (e.g., aircraft buffet, stall horn, etc.).
• CA.VII.A.S4:

  Accomplish coordinated straight-and-level flight, turns, climbs, and descents with the aircraft configured as specified by the evaluator without a stall warning (e.g., aircraft buffet, stall horn, etc.).
• CA.VII.A.S5:

  Maintain the specified altitude, ±50 feet; specified heading, ±10°; airspeed, +5/-0 knots; and specified angle of bank, ±5°.

• CA.VII.B.S1:

  Clear the area.
• CA.VII.B.S2:

  Select an entry altitude that allows the Task to be completed no lower than 1,500 feet above ground level (AGL) (ASEL, ASES) or 3,000 feet AGL (AMEL, AMES).
• CA.VII.B.S3:

  Configure the airplane in the approach or landing configuration, as specified by the evaluator, and maintain coordinated flight throughout the maneuver.
• CA.VII.B.S4:

  Establish a stabilized descent.
• CA.VII.B.S5:

  Transition smoothly from the approach or landing attitude to a pitch attitude that induces a stall.
• CA.VII.B.S6:

  Maintain a specified heading ±10°° if in straight flight; maintain a specified angle of bank not to exceed 20°, ±5° if in turning flight, until an impending or full stall occurs, as specified by the evaluator.
• CA.VII.B.S7:

  Acknowledge cues of the impending stall and then recover promptly after a full stall occurs.
• CA.VII.B.S8:

  Execute a stall recovery in accordance with procedures set forth in the Pilot's Operating Handbook (POH) or Airplane Flight Manual (AFM).
• CA.VII.B.S9:

  Configure the airplane as recommended by the manufacturer, and accelerate to best angle of climb speed (V_x) or best rate of climb speed (V_y).
• CA.VII.B.S10:

  Return to the altitude, heading, and airspeed specified by the evaluator.

• CA.VII.C.S1:

  Clear the area.
• CA.VII.C.S2:

  Select an entry altitude that allows the Task to be completed no lower than 1,500 feet above ground level (AGL) (ASEL, ASES) or 3,000 feet AGL (AMEL, AMES).
• CA.VII.C.S3:

  Establish the takeoff, departure, or cruise configuration, as specified by the evaluator, and maintain coordinated flight throughout the maneuver.
• CA.VII.C.S4:

  Set power (as assigned by the evaluator) to no less than 65 percent power.
• CA.VII.C.S5:

  Transition smoothly from the takeoff or departure attitude to the pitch attitude that induces a stall.
• CA.VII.C.S6:

  Maintain a specified heading ±10°° if in straight flight; maintain a specified angle of bank not to exceed 20°, ±10° if in turning flight, while inducing the stall.
• CA.VII.C.S7:

  Acknowledge cues of the impending stall and then recover promptly after a full stall occurs.
• CA.VII.C.S8:

  Recover at the first indication of a stall or after a full stall has occurred, as specified by the evaluator.
• CA.VII.C.S9:

  Configure the airplane as recommended by the manufacturer, and accelerate to best angle of climb speed (V_X) or best rate of climb speed (V_Y).
• CA.VII.C.S10:

  Return to the altitude, heading, and airspeed specified by the evaluator.

N/A

• CA.IV.H.S1:

  Complete the appropriate checklist(s).
• CA.IV.H.S2:

  Make radio calls as appropriate.
• CA.IV.H.S3:

  Ensure the airplane is aligned for an approach to the correct/assigned landing surface.
• CA.IV.H.S4:

  Scan the landing area for traffic and obstructions.
• CA.IV.H.S5:

  Select and aim for a suitable touchdown point considering the wind, landing surface, and obstructions.
• CA.IV.H.S6:

  Establish the recommended approach and landing configuration, airspeed, and trim, and adjust pitch attitude and power as required to maintain a stabilized approach.
• CA.IV.H.S7:

  Maintain manufacturer's published approach airspeed or in its absence not more than 1.3 V_SO, +10/-5 knots with gust factor applied.
• CA.IV.H.S8:

  Maintain directional control and appropriate crosswind correction throughout the approach and landing.
• CA.IV.H.S9:

  Make smooth, timely, and correct control application before, during, and after touchdown.
• CA.IV.H.S10:

  Contact the water at the recommended airspeed with a proper pitch attitude for the surface conditions
• CA.IV.H.S11:

  Touch down at a proper pitch attitude, within 200 feet beyond or on the specified point, with no side drift, minimum float, and with the airplane's longitudinal axis aligned with the projected landing path.
• CA.IV.H.S12:

  Execute a timely go-around if the approach cannot be made within the tolerances specified above or for any other condition that may result in an unsafe approach or landing.
• CA.IV.H.S13:

  Apply elevator control as necessary to stop in the shortest distance consistent with safety.

• CA.IV.G.S1:

  Complete the appropriate checklist(s).
• CA.IV.G.S2:

  Make radio calls as appropriate.
• CA.IV.G.S3:

  Verify assigned/correct takeoff path.
• CA.IV.G.S4:

  Determine wind direction with or without visible wind direction indicators.
• CA.IV.G.S5:

  Position the flight controls for the existing wind, if applicable.
• CA.IV.G.S6:

  Clear the area, taxi into takeoff position utilizing maximum available takeoff area, and align the airplane on the takeoff path.

  • CA.IV.G.S6a:

    Retract the water rudders, as appropriate.
• CA.IV.G.S7:

  Advance the throttle smoothly to takeoff power and confirm proper engine and flight instrument indications prior to rotation.
• CA.IV.G.S8:

  Establish a pitch attitude that maintains the most efficient planing/lift-off attitude and correct for porpoising and skipping.
• CA.IV.G.S9:

  Avoid excessive water spray on the propeller(s).
• CA.IV.G.S10:

  Rotate and lift off at the recommended airspeed, and accelerate to the recommended obstacle clearance airspeed or V_x.
• CA.IV.G.S11:

  Establish a pitch attitude to maintain the recommended obstacle clearance airspeed or V_x, ±5 knots until the obstacle is cleared or until the airplane is 50 feet above the surface.
• CA.IV.G.S12:

  Establish a pitch attitude for V_y and accelerate to V_y ±5 knots after clearing the obstacle or at 50 feet AGL if simulating an obstacle.
• CA.IV.G.S13:

  Retract flaps, if extended, after a positive rate of climb has been verified or in accordance with airplane manufacturer's guidance.
• CA.IV.G.S14:

  Maintain V_y ±5 knots to a safe maneuvering altitude.
• CA.IV.G.S15:

  Maintain directional control and proper wind-drift correction throughout takeoff and climb.
• CA.IV.G.S16:

  Comply with noise abatement procedures, as applicable.

• CA.IV.J.S1:

  Complete the appropriate checklist(s).
• CA.IV.J.S2:

  Make radio calls as appropriate.
• CA.IV.J.S3:

  Scan the landing area for traffic and obstructions.
• CA.IV.J.S4:

  Select a proper approach and landing path considering the landing surface, visual attitude references, water depth, and Collision hazards.
• CA.IV.J.S5:

  Establish the recommended approach and landing configuration, airspeed, and trim, and adjust pitch attitude and power as required to maintain a stabilized approach.
• CA.IV.J.S6:

  Maintain manufacturer's published approach airspeed or in its absence not more than 1.3 V_SO, ±5 knots.
• CA.IV.J.S7:

  Make smooth, timely, and correct power and control adjustments to maintain proper pitch attitude and rate of descent to touchdown.
• CA.IV.J.S8:

  Contact the water in a proper pitch attitude, and slow to idle taxi speed.
• CA.IV.J.S9:

  Maintain directional control throughout the approach and landing.

• CA.IV.I.S1:

  Complete the appropriate checklist(s).
• CA.IV.I.S2:

  Make radio calls as appropriate.
• CA.IV.I.S3:

  Position flight controls and configure the aircraft for the existing conditions.
• CA.IV.I.S4:

  Clear the area; select appropriate takeoff path considering surface hazards or vessels and surface conditions.

  • CA.IV.I.S4a:

    Retract the water rudders, as appropriate.
  • CA.IV.I.S4b:

    Advance the throttle smoothly to takeoff power and confirm proper engine and flight instrument indications prior to rotation.
• CA.IV.I.S5:

  [Archived].
• CA.IV.I.S6:

  Establish and maintain an appropriate planing attitude, directional control, and correct for porpoising, skipping, and increase in water drag.
• CA.IV.I.S7:

  Avoid excessive water spray on the propeller(s).
• CA.IV.I.S8:

  Use appropriate techniques to lift seaplane from the water considering surface conditions.
• CA.IV.I.S9:

  Establish proper attitude/airspeed and accelerate to V_y ±5 knots during the climb.
• CA.IV.I.S10:

  Configure the airplane after a positive rate of climb has been verified or in accordance with airplane manufacturer's instructions.
• CA.IV.I.S11:

  Maintain Vy ±5 knots to a safe maneuvering altitude.
• CA.IV.I.S12:

  Maintain directional control throughout takeoff and climb.

• CA.IV.N.S1:

  Complete the appropriate checklist(s).
• CA.IV.N.S2:

  Make radio calls as appropriate.
• CA.IV.N.S3:

  Make a timely decision to discontinue the approach to landing.
• CA.IV.N.S4:

  Apply takeoff power immediately and transition to climb pitch attitude for V_x or V_y as appropriate ±5 knots.
• CA.IV.N.S5:

  Configure the airplane after a positive rate of climb has been verified or in accordance with airplane manufacturer's instructions.
• CA.IV.N.S6:

  Maneuver to the side of the runway/landing area when necessary to clear and avoid conflicting traffic.
• CA.IV.N.S7:

  Maintain V_Y ±5 knots to a safe maneuvering altitude.
• CA.IV.N.S8:

  Maintain directional control and proper wind-drift correction throughout the climb.
• CA.IV.N.S9:

  Use runway incursion avoidance procedures, if applicable.

• CA.IV.A.S1:

  Complete the appropriate checklist(s).
• CA.IV.A.S2:

  Make radio calls as appropriate.
• CA.IV.A.S3:

  Verify assigned/correct runway or takeoff path.
• CA.IV.A.S4:

  Determine wind direction with or without visible wind direction indicators.
• CA.IV.A.S5:

  Position the flight controls for the existing wind, if applicable.
• CA.IV.A.S6:

  Clear the area, taxi into takeoff position, and align the airplane on the runway centerline (ASEL, AMEL) or takeoff path (ASES, AMES).

  • CA.IV.A.S6a:

    Retract the water rudders, as appropriate (ASES, AMES).
• CA.IV.A.S7:

  Advance the throttle smoothly to takeoff power and confirm proper engine and flight instrument indications prior to rotation.

  • CA.IV.A.S7a:

    Establish and maintain the most efficient planing/lift-off attitude, and correct for porpoising or skipping (ASES, AMES).
• CA.IV.A.S8:

  Avoid excessive water spray on the propeller(s) (ASES, AMES).
• CA.IV.A.S9:

  Rotate and lift off at the recommended airspeed and accelerate to V_Y.
• CA.IV.A.S10:

  [Archived].
• CA.IV.A.S11:

  Establish a pitch attitude to maintain the manufacturer's recommended speed or V_Y, ±5 knots.
• CA.IV.A.S12:

  Configure the airplane in accordance with manufacturer's guidance.
• CA.IV.A.S13:

  Maintain V_Y ± knots to a safe maneuvering altitude.
• CA.IV.A.S14:

  Maintain directional control and proper wind-drift correction throughout takeoff and climb.
• CA.IV.A.S15:

  Comply with noise abatement procedures, as applicable.

• CA.IV.M.S1:

  Complete the appropriate checklist(s).
• CA.IV.M.S2:

  Make radio calls as appropriate.
• CA.IV.M.S3:

  Plan and follow a flightpath to the selected landing area considering altitude, wind, terrain, and obstructions.
• CA.IV.M.S4:

  Select the most suitable touchdown point based on wind, landing surface, obstructions, and aircraft limitations.
• CA.IV.M.S5:

  Position airplane on downwind leg, parallel to landing runway.
• CA.IV.M.S6:

  Correctly configure the airplane.
• CA.IV.M.S7:

  As necessary, correlate crosswind with direction of forward slip and transition to side slip before touchdown.
• CA.IV.M.S8:

  Touch down at a proper pitch attitude, within 200 feet beyond or on the specified point with no side drift and with the airplane's longitudinal axis aligned with and over the runway centerline or landing path, as applicable.

• CA.IV.L.S1:

  Complete the appropriate checklist(s).
• CA.IV.L.S2:

  Make radio calls as appropriate.
• CA.IV.L.S3:

  Ensure the airplane is aligned with the correct/assigned waterway.
• CA.IV.L.S4:

  Scan the landing area for traffic and obstructions.
• CA.IV.L.S5:

  Select and aim for a suitable touchdown point considering the wind conditions, landing surface, and obstructions.
• CA.IV.L.S6:

  Establish the recommended approach and landing configuration, airspeed, and trim, and adjust pitch attitude and power as required to maintain a stabilized approach.
• CA.IV.L.S7:

  Maintain manufacturer's published approach airspeed or in its absence not more than 1.3 V_SO, ±5 knots with gust factor applied.
• CA.IV.L.S8:

  Maintain directional control and appropriate crosswind correction throughout the approach and landing.
• CA.IV.L.S9:

  Make smooth, timely, and correct power and control adjustments to maintain proper pitch attitude and rate of descent to touchdown.
• CA.IV.L.S10:

  Contact the water in a proper pitch attitude, considering the type of rough water.

• CA.IV.K.S1:

  Complete the appropriate checklist(s).
• CA.IV.K.S2:

  Make radio calls as appropriate.
• CA.IV.K.S3:

  Verify assigned/correct takeoff path.
• CA.IV.K.S4:

  Determine wind direction with or without visible wind direction indicators.
• CA.IV.K.S5:

  Position flight controls and configure the airplane for the existing conditions.
• CA.IV.K.S6:

  Clear the area, select an appropriate takeoff path considering wind, swells, surface hazards, or vessels.

  • CA.IV.K.S6a:

    Retract the water rudders as appropriate; advance the throttle smoothly to takeoff power.
  • CA.IV.K.S6b:

    Advance the throttle smoothly to takeoff power and confirm proper engine and flight instrument indications prior to rotationr.
• CA.IV.K.S7:

  [Archived].
• CA.IV.K.S8:

  Establish and maintain an appropriate planing attitude, directional control, and correct for porpoising, skipping, and increase in water drag.
• CA.IV.K.S9:

  Avoid excessive water spray on the propeller(s).
• CA.IV.K.S10:

  Lift off at minimum airspeed and accelerate to VY ±5 knots before leaving ground effect.
• CA.IV.K.S11:

  Configure the airplane after a positive rate of climb has been verified or in accordance with airplane manufacturer's instructions.
• CA.IV.K.S12:

  Maintain VY ± knots to a safe maneuvering altitude.
• CA.IV.K.S13:

  Maintain directional control and proper wind-drift correction throughout takeoff and climb.

• CA.IV.F.S1:

  Complete the appropriate checklist(s).
• CA.IV.F.S2:

  Make radio calls as appropriate.
• CA.IV.F.S3:

  Ensure the airplane is aligned with the correct/assigned runway.
• CA.IV.F.S4:

  Scan the landing runway and adjoining area for traffic and obstructions.
• CA.IV.F.S5:

  Select and aim for a suitable touchdown point considering the wind conditions, landing surface, and obstructions.
• CA.IV.F.S6:

  Establish the recommended approach and landing configuration, airspeed, and trim, and adjust pitch attitude and power as required to maintain a stabilized approach.
• CA.IV.F.S7:

  Maintain manufacturer's published approach airspeed or in its absence not more than 1.3 V_SO, ±5 knots with gust factor applied.
• CA.IV.F.S8:

  Maintain directional control and appropriate crosswind correction throughout the approach and landing.
• CA.IV.F.S9:

  Make smooth, timely, and correct control application before, during, and after touchdown.
• CA.IV.F.S10:

  Touch down at a proper pitch attitude within 100 feet beyond or on the specified point, threshold markings, or runway numbers, with no side drift, minimum float, and with the airplane's longitudinal axis aligned with and over the runway centerline.
• CA.IV.F.S11:

  Use manufacturer's recommended procedures for airplane configuration and braking.
• CA.IV.F.S12:

  Execute a timely go-around if the approach cannot be made within the tolerances specified above or for any other condition that may result in an unsafe approach or landing.
• CA.IV.F.S13:

  Use runway incursion avoidance procedures, if applicable.

• CA.IV.E.S1:

  Complete the appropriate checklist(s).
• CA.IV.E.S2:

  Make radio calls as appropriate.
• CA.IV.E.S3:

  Verify assigned/correct runway.
• CA.IV.E.S4:

  Determine wind direction with or without visible wind direction indicators.
• CA.IV.E.S5:

  Position the flight controls for the existing wind, if applicable.
• CA.IV.E.S6:

  Clear the area, taxi into takeoff position, and align the airplane on the runway centerline utilizing maximum available takeoff area.
• CA.IV.E.S7:

  Apply brakes while setting engine power to achieve maximum performance.
• CA.IV.E.S8:

  Confirm takeoff power prior to brake release and verify proper engine and flight instrument indications prior to rotation.
• CA.IV.E.S9:

  Rotate and lift off at the recommended airspeed and accelerate to the recommended obstacle clearance airspeed or V_x, ±5 knots.
• CA.IV.E.S10:

  Establish a pitch attitude to maintain the recommended obstacle clearance airspeed or V_X, ±5 knots until the obstacle is cleared or until the airplane is 50 feet above the surface.
• CA.IV.E.S11:

  Establish a pitch attitude for V_y and accelerate to V_y, ±5 knots after clearing the obstacle or at 50 feet AGL if simulating an obstacle.
• CA.IV.E.S12:

  Configure the airplane in accordance with the manufacturer's guidance after a positive rate of climb has been verified.
• CA.IV.E.S13:

  Maintain V_y ±5 knots to a safe maneuvering altitude.
• CA.IV.E.S14:

  Maintain directional control and proper wind-drift correction throughout takeoff and climb.
• CA.IV.E.S15:

  Comply with Comply with noise abatement procedures, as applicable.

• CA.IV.D.S1:

  Complete the appropriate checklist(s).
• CA.IV.D.S2:

  Make radio calls as appropriate.
• CA.IV.D.S3:

  Ensure the airplane is aligned with the correct/assigned runway.
• CA.IV.D.S4:

  Scan the landing runway and adjoining area for traffic and obstructions.
• CA.IV.D.S5:

  Select and aim for a suitable touchdown point considering the wind, landing surface, and obstructions.
• CA.IV.D.S6:

  Establish the recommended approach and landing configuration, airspeed, and trim, and adjust pitch attitude and power as required to maintain a stabilized approach.
• CA.IV.D.S7:

  Maintain manufacturer's published approach airspeed or in its absence not more than 1.3 V_SO, ±5 knots with gust factor applied.
• CA.IV.D.S8:

  Maintain directional control and appropriate crosswind correction throughout the approach and landing.
• CA.IV.D.S9:

  Make smooth, timely, and correct control inputs during the round out and touchdown, and, for tricycle gear airplanes, keep the nose wheel off the surface until loss of elevator effectiveness.
• CA.IV.D.S10:

  Touch down at a proper pitch attitude with minimum sink rate, no side drift, and with the airplane's longitudinal axis aligned with the center of the runway.
• CA.IV.D.S11:

  Maintain elevator as recommended by manufacturer during rollout and exit the "soft" area at a speed that would preclude sinking into the surface.
• CA.IV.D.S12:

  Execute a timely go-around if the approach cannot be made within the tolerances specified above or for any other condition that may result in an unsafe approach or landing.
• CA.IV.D.S13:

  Maintain proper position of the flight controls and sufficient speed to taxi while on the soft surface.

• CA.IV.C.S1:

  Complete the appropriate checklist(s).
• CA.IV.C.S2:

  Make radio calls as appropriate.
• CA.IV.C.S3:

  Verify assigned/correct runway.
• CA.IV.C.S4:

  Determine wind direction with or without visible wind direction indicators.
• CA.IV.C.S5:

  Position the flight controls for the existing wind, if applicable.
• CA.IV.C.S6:

  Clear the area, maintain necessary flight control inputs, taxi into takeoff position and align the airplane on the runway centerline without stopping, while advancing the throttle smoothly to takeoff power.
• CA.IV.C.S7:

  Confirm takeoff power and proper engine and flight instrument indications.
• CA.IV.C.S8:

  Establish and maintain a pitch attitude that transfers the weight of the airplane from the wheels to the wings as rapidly as possible.
• CA.IV.C.S9:

  Lift off at the lowest possible airspeed and remain in ground effect while accelerating to V_x or V_y, as appropriate.
• CA.IV.C.S10:

  Establish a pitch attitude for V_x or V_y, as appropriate, and maintain selected airspeed ±5 knots during the climb.
• CA.IV.C.S11:

  Configure the airplane after a positive rate of climb has been verified or in accordance with airplane manufacturer's instructions.
• CA.IV.C.S12:

  Maintain V_x or V_y, as appropriate, ±5 knots to a safe maneuvering altitude.
• CA.IV.C.S13:

  Maintain directional control and proper wind-drift correction throughout takeoff and climb.
• CA.IV.C.S14:

  noise abatement procedures, as applicable.

• IR.VII.D.S1:

  Advise ATC or the evaluator if unable to comply with a clearance.
• IR.VII.D.S2:

  Complete a non-precision instrument approach without the use of the primary flight instruments using the skill elements of the non-precision approach Task (see Area of Operation VI, Task A).
• IR.VII.D.S3:

  Use single-pilot resource management (SRM) or crew resource management (CRM), as appropriate.

• IR.VII.C.S1:

  Promptly recognize an engine failure and maintain positive aircraft control.
• IR.VII.C.S2:

  Set the engine controls, reduce drag, identify and verify the inoperative engine, and simulate feathering of the propeller on the inoperative engine (evaluator should then establish zero thrust on the inoperative engine).
• IR.VII.C.S3:

  Use flight controls in the proper combination as recommended by the manufacturer, or as required to maintain best performance, and trim as required.
• IR.VII.C.S4:

  Follow the manufacturer's recommended emergency procedures and complete the appropriate checklist.
• IR.VII.C.S5:

  Monitor the operating engine and aircraft systems and make adjustments as necessary.
• IR.VII.C.S6:

  Request and follow an actual or a simulated air traffic control (ATC) clearance for an instrument approach.
• IR.VII.C.S7:

  Maintain altitude ±100 feet or minimum sink rate if applicable, airspeed ±10 knots, and selected heading ±10°.
• IR.VII.C.S8:

  Establish a rate of descent that ensures arrival at the minimum descent altitude (MDA) or decision altitude (DA)/decision height (DH) with the airplane in a position from which a descent to a landing on the intended runway can be made, either straight in or circling as appropriate.
• IR.VII.C.S9:

  On final approach segment, maintain vertical (as applicable) and lateral guidance within 3/4-scale deflection.
• IR.VII.C.S10:

  Maintain control and fly within the aircraft's operating limitations.
• IR.VII.C.S11:

  Comply with the published criteria for the aircraft approach category if circling.
• IR.VII.C.S12:

  Execute a landing.
• IR.VII.C.S13:

  Complete the appropriate checklist(s).
• IR.VII.C.S14:

  Use single-pilot resource management (SRM) or crew resource management (CRM), as appropriate.

• IR.VII.B.S1:

  Promptly recognize an engine failure and maintain positive aircraft control.
• IR.VII.B.S2:

  Set the engine controls, reduce drag, identify and verify the inoperative engine, and simulate feathering of the propeller on the inoperative engine (evaluator should then establish zero thrust on the inoperative engine).
• IR.VII.B.S3:

  Establish the best engine-inoperative airspeed and trim the airplane.
• IR.VII.B.S4:

  Use flight controls in the proper combination as recommended by the manufacturer, or as required to maintain best performance, and trim as required.
• IR.VII.B.S5:

  Verify the prescribed checklist procedures used for securing the inoperative engine.
• IR.VII.B.S6:

  Attempt to determine and resolve the reason for the engine failure.
• IR.VII.B.S7:

  Monitor engine functions and make necessary adjustments.
• IR.VII.B.S8:

  Maintain the specified altitude ±100 feet or minimum sink rate if applicable, airspeed ±10 knots, and the specified heading ±10°.
• IR.VII.B.S9:

  Assess the aircraft's performance capability and decide an appropriate action to ensure a safe landing.
• IR.VII.B.S10:

  Maintain control and fly within the aircraft's operating limitations.
• IR.VII.B.S11:

  Use single-pilot resource management (SRM) or crew resource management (CRM), as appropriate.

• IR.IV.B.S1:

  Use proper instrument cross-check and interpretation to identify an unusual attitude (including both nose-high and nose-low) in flight, and apply the appropriate flight control, power input, and aircraft configuration in the correct sequence, to return to a stabilized level flight attitude.
• IR.IV.B.S2:

  Use single-pilot resource management (SRM) or crew resource management (CRM), as appropriate.

• IR.V.A.S1:

  Tune and identify the navigation facility/program the navigation system and verify system accuracy as appropriate for the equipment installed in the aircraft.
• IR.V.A.S2:

  Determine aircraft position relative to the navigational facility or waypoint.
• IR.V.A.S3:

  Set and orient to the course to be intercepted.
• IR.V.A.S4:

  Intercept the specified course at appropriate angle, inbound to or outbound from a navigational facility or waypoint.
• IR.V.A.S5:

  Maintain airspeed ±10 knots, altitude ±100 feet, and selected headings ±5°.
• IR.V.A.S6:

  Apply proper correction to maintain a course, allowing no more than 3/4-scale deflection of the course deviation indicator (CDI). If a distance measuring equipment (DME) arc is selected, maintain that arc ±1 nautical mile.
• IR.V.A.S7:

  Recognize navigational system or facility failure, and when required, report the failure to air traffic control (ATC).
• IR.V.A.S8:

  Use a multi-function display (MFD) and other graphical navigation displays, if installed, to monitor position, track wind drift, and to maintain situational awareness.
• IR.V.A.S9:

  At the discretion of the evaluator, use the autopilot to make appropriate course intercepts, if installed.
• IR.V.A.S10:

  Use single-pilot resource management (SRM) or crew resource management (CRM), as appropriate.

• PA.III.B.S1:

  Identify and interpret airport/seaplane base runways, taxiways, markings, signs, and lighting.
• PA.III.B.S2:

  Comply with recommended traffic pattern procedures.
• PA.III.B.S3:

  Correct for wind drift to maintain the proper ground track.
• PA.III.B.S4:

  Maintain orientation with the runway/landing area in use.
• PA.III.B.S5:

  Maintain traffic pattern altitude, ±100 feet, and the appropriate airspeed, ±10 knots.
• PA.III.B.S6:

  Maintain situational awareness and proper spacing from other aircraft in the traffic pattern.

• PA.VIII.B.S1:

  Transition to the climb pitch attitude and power setting on an assigned heading using proper instrument cross-check and interpretation, and coordinated flight control application.
• PA.VIII.B.S2:

  Climb at a constant airspeed to specific altitudes in straight flight and turns.
• PA.VIII.B.S3:

  Maintain altitude ±200 feet, heading ±20°, and airspeed ±10 knots.

• PA.VIII.C.S1:

  Transition to the descent pitch attitude and power setting on an assigned heading using proper instrument cross-check and interpretation, and coordinated flight control application.
• PA.VIII.C.S2:

  Descend at a constant airspeed to specific altitudes in straight flight and turns.
• PA.VIII.C.S3:

  Level off at the assigned altitude and maintain altitude ±200 feet, heading ±20°, and airspeed ±10 knots.

• PA.VIII.E.S1:

  Use proper instrument cross-check and interpretation to identify an unusual attitude (including both nose-high and nose-low) in flight, and apply the appropriate flight control, power input, and aircraft configuration in the correct sequence, to return to a stabilized level flight attitude.
• PA.VIII.E.S2:

  Use single-pilot resource management (SRM) or crew resource management (CRM), as appropriate.

• PA.VIII.A.S1:

  Maintain straight-and-level flight using proper instrument cross-check and interpretation, and coordinated control application.
• PA.VIII.A.S2:

  Maintain altitude ±200 feet, heading ±20°, and airspeed ±10 knots.

• PA.VIII.D.S1:

  Turn to headings, maintain altitude ±200 feet, maintain a standard rate turn, roll out on the assigned heading ±10 degrees, and maintain airspeed ±10 knots.

• PA.IX.G.S1:

  Promptly recognize an engine failure and maintain positive airplane control.
• PA.IX.G.S2:

  Set the engine controls, reduce drag, identify and verify the inoperative engine, and simulate feathering of the propeller on the inoperative engine (evaluator should then establish zero thrust on the inoperative engine).
• PA.IX.G.S3:

  Use flight controls in the proper combination as recommended by the manufacturer, or as required to maintain best performance, and trim as required.
• PA.IX.G.S4:

  Follow the manufacturer's recommended emergency procedures and complete the appropriate checklist.
• PA.IX.G.S5:

  Monitor the operating engine and make adjustments as necessary.
• PA.IX.G.S6:

  Maintain the manufacturer's recommended approach airspeed +10/-5 knots, in the landing configuration with a stabilized approach, until landing is assured.
• PA.IX.G.S7:

  Make smooth, timely, and correct control application before, during, and after touchdown.
• PA.IX.G.S8:

  Touch down on the first one-third of available runway/landing surface, with no drift, and the airplane's longitudinal axis aligned with and over the runway center or landing path.
• PA.IX.G.S9:

  Maintain directional control and appropriate crosswind correction throughout the approach and landing.
• PA.IX.G.S10:

  Complete the appropriate checklist(s).

• PA.IX.B.S1:

  Establish and maintain the recommended best glide airspeed, ±10 knots.
• PA.IX.B.S2:

  Configure the airplane in accordance with the Pilot's Operating Handbook (POH)\Airplane Flight Manual (AFM) and existing conditions.
• PA.IX.B.S3:

  Select a suitable landing area considering altitude, wind, terrain, obstructions, and available glide distance.
• PA.IX.B.S4:

  Plan and follow a flightpath to the selected landing area considering altitude, wind, terrain, and obstructions.
• PA.IX.B.S5:

  Prepare for landing as specified by the evaluator.
• PA.IX.B.S6:

  Complete the appropriate checklist.

• PA.IX.A.S1:

  Clear the area.
• PA.IX.A.S2:

  Establish and maintain the appropriate airspeed and configuration appropriate to the scenario specified by the evaluator and as covered in Pilot's Operating Handbook (POH)/Airplane Flight Manual (AFM) for the emergency descent.
• PA.IX.A.S3:

  Maintain orientation, divide attention appropriately, and plan and execute a smooth recovery.
• PA.IX.A.S4:

  Use bank angle between 30° and 45° to maintain positive load factors during the descent.
• PA.IX.A.S5:

  Maintain appropriate airspeed +0/-10 knots, and level off at a specified altitude ±100 feet.
• PA.IX.A.S6:

  Complete the appropriate checklist(s).
• PA.IX.A.S7:

  Make radio calls as appropriate.
• PA.IX.A.S8:

  Use single-pilot resource management (SRM) or crew resource management (CRM), as appropriate.