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PC-12/47 Voyager

PC12/47 Voyager SOP

Introduction

This document describes operation of the aircraft mimicking real operations as accurately as possible. They were collected using various sources online and filtered to keep the information coming from real pilots only.

Memory Flows

Most turbines are flown by following flows which are all from memory and using checklist to check that nothing was forgotten at the end of the flow.

Receiving Flow

Perform before passengers arrive. You will scan most thing from left to right then to the overhead panel.

  • Check that circuit breakers on left side are in.
  • Mask mic swich in mic position.
  • Make sure parking break is in. (IRL you need to apply break on the pedals and lock it with the parking break, generally not simulated).
  • ELT in armed position.
  • EFIS switch in norm.
  • EPS to test, validate that the green light is on. After 5s set to ARMED. Verify yellow light is on.
  • AHRS swithes all to slave.
  • Gear handle in down position.
  • Oxygen to on.
  • Trim interrupt switches to NORM.
  • Alternate stap trim to center postition (nose).
  • Manual override should be stowed.
  • PCL (power control) to idle
  • Condition lever to feather/cut-off position
  • Cabin lights to off except maybe for cabin reading light if you have passengers.
  • Emergency fuel and ECS (back of the center pedestal) are flush.
  • ECS to off.
  • Cabin pressure dump to auto and guarded
  • Tempearture as desired
  • Manual temp switch to center position and guarded.
  • Cabin pressure control switch to cruise altitude + 500ft.
  • Cabin rate of climb to the 12oclock position.
  • Copilot EFIS to norm
  • Copilot mic/mask switch to mic.
  • Copilot breaker switches in.
  • Battery 1 and 2 on.
  • Check voltage above 24V
  • Nav lights on. (they're usually always left on)
  • Push and hold the "test lamp" button, validate all the cockpit lights are on.
  • Press the fire test button. Validate master warning and aural fire.
  • Hit RH fuel pump. Validate Gren rh fuel pump CAWS message and hear pump sound. Back to auto.
  • Same with LH fuel pump.
  • Ignition to auto.
  • Gen 1 and 2 off.
  • External power off unless we have a gpu connected.
  • Avionics buses off.
  • Non essential override in auto.
  • Switch inverter. Gen1 or batt inverter work the same way. They are used alternatively for each flight to even the wear.
  • Turn on the standby bus to preprogram the avionics. This should power com1 and nav1.
  • Master power switch should be on and guarded. This only goes off in emergency to kill electricity in the airplane to prevent fires.
  • De-icing boots and prop are off.
  • Intert sep open.
  • LH and RH windshield on light, then off.
  • Probe heat off.
  • Cooling system off, but you can preselct how you want it.
  • Turn on no smoking and seatbelt signs.
  • Cabin heat is off.

Run Preflight Inspection checklist.

Before Start Flow

This is run after passengers and luggage are loaded in. Chocks pulled, door closed.

  • Seat belt fasten.
  • Shoulder harnesses are on.
  • Adjust pedal position.

One the Engine Indicating System (EIS):

  • Press test, validate all the leds turn on

Take off

  • FD- TO/GA
  • TO power
  • @80 kts lift off
  • positive rate- gear up
  • YD on
  • 400 feet AGL
  • flaps zero as long above 100 kias
  • 1000ft agl- separator closed
  • set climb power 36.9 psi. (with pax and pending ATC we set 1000-1200 fpm).
  • Run after takeoff checklist here.
  • we keep that climb rate till we either
    1. get high enough where my KIAS hits 150-160, then i hit IAS mode. (usually happens near FL 190)
    2. we hit our altitude. (keep below 750 ITT while climbing)
  • we let the plane speed up a bit on whatever power setting you had to climb.
  • Run Our cruise checklist.
  • Set power using the max performance chart.

Source/credits

  • CaptGamn on SWS discord
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