KA3 5 0 - MILVIZ · 2019-12-21 · MilViz KA350i 2-1 Product Features > Designed primarily for procedural flight training, the MilViz KA350i repre- sents the most advanced overall

KA3 5 0 iuser guide

End User License Agreement

By purchasing the MilViz KA350i you are consenting to be bound by and agree to the following:

COPYRIGHT: Copyright © 2019 Military Visualizations (MilViz). MilViz retains FULL copyright on the entire KA350i package.

DISTRIBUTION:You may NOT redistribute the KA350i package in whole or in part. Any such distribution is strictly prohibited.

GRANT OF LICENSE:A limited license is granted to use the MilViz KA350i for personal entertainment purposes only. Commercial, training or any other use without the express permission of Military Visualizations Inc. is expressly prohibited. Any such usage will be litigated to the full extent of the law. This does NOT give you the license to modify in anyway part or whole based on the designers original work ex-cept for your own personal use. You MAY of course use the Paintkit provided to create new liveries for public distribution, provided no charge is made for them!

Any inquiries regarding use of this product in a commercial or training capacity should be directed via e-mail to [email protected].

DISCLAIMER:MilViz and all associates shall NOT be held responsible for any damages arising from the use of the MilViz KA350i product.

Copyright © 2019 Military Visualizations, All Rights Reserved.

iMilViz KA350i

Table of Contents

Introduction 1-1

Product Features 2-1

System Requirements 3-1

Product Installation 4-1

Simulator Configuration 5-1

MVAMS Overview 6-1

In-Game Options 7-1

Specifications & Limitations 8-1

Systems Overview 9-1

Panel Overview 10-1

T/O Reference Chart 11-1

Normal Procedures 12-1

1-1MilViz KA350i

Introduction

Welcome!

We are extremely excited to introduce you to the MilViz KA350i. Recognizable throughout the world and with a pedigree as long as your arm, the 350 and it’s predecessors have been gracing the airways for many decades.

It’s hard not to get swept into an appreciation of flying when regarding the KA350i. It manages to exude a feeling of power, yet retains style and sophistication. It’s more than an airplane; it’s an icon, a status symbol, a reminder that air travel can still be something other than a massively commercialized commodity.

It’s no secret that our rendition of the KA350i has been a little while in the making. Our guarantee is that it’s been time well spent. We’ve endeavored to bring to the simulation environment the most accurate & realistic version of this aircraft that is currently possible with today’s technology.

From painstakingly researched and replicated avionics, beautiful hyper-realistic textures and modeling, to real-world-worthy flight response and handling characteristics, we’ve strived to make this aircraft a pinnacle of what can be achieved with flight simulation.

This user guide is designed to help you get ac-quainted with the MilViz KA350i. Divided into

sections, you’ll find information related to instal-lation, configuring the aircraft within the simula-tor, an overview of the aircraft itself, operating procedures, and much more.

The KA350i is not a simple aircraft, nor is it overly complex. It sits on that thin line where although it can be enjoyable to let the aircraft do the fly-ing, taking hold and hand flying it will also bring a wide grin to your face.

Regardless of how you approach it, it’s a wonder-ful aircraft to learn. We sincerely hope you en-joy every minute of your many exciting flights to come!

1-2MilViz KA350i

2-1MilViz KA350i

Product Features

> Designed primarily for procedural flight training, the MilViz KA350i repre-sents the most advanced overall aircraft simulation that currently exists for desktop simulator

> Exacting replication of the PL-21 integrated avionics system; includes the most advanced TAWS/EGPWS simulation available to date, an integrated WX radar display, and integrated checklist functionality

> P3D native obstacles database simulation (1:1 match for all obstacles in the simulator, including addons)

> A complete FMS-3000 integrated simulation providing en route, terminal and non-precision approach navigation, utilizing upgradable navdata

> Custom, highly realistic turboprop simulation, complete with an accurate fuel flow / propeller RPM relationship

> Persistent engine health, with both normal wear and accelerated wear through mishandling accumulating and capable of causing engine failures

> Flight characteristics and engine behavior through all stages of flight are carefully tuned & tested

> Exterior and interior rendered with exacting detail and precision, including high resolution PBR textures with realistic weathering effects

> Authentic Sound Environment featuring professionally created sounds matched to the aircraft and an immersive interior soundscape

> Configurable start-up options including ready-to-fly and cold n’ dark, with options for tie-downs & covers

> TFDi RealLight included; beautiful and adjustable night lighting

> TFDi TrueGlass included; advanced rain effects visible on the cabin windows

> 4 exceptionally detailed aircraft liveries included

> Downloadable paint kit for user creation of custom aircraft liveries

3-1MilViz KA350i

System Requirements

The following requirements apply as a general minimum to successfully install, configure and operate the MilViz KA350i.

Please note that your choice of scenery, location, simulator settings and 3rd party utilities may place additional demands on your simulation platform and may affect your simulator experience.

Supported Platforms:

Lockheed Martin Prepar3D, version 4.5 (Hotfix 1 required)

(Note: For compatibility with any future updates and hotfixes, please register for and visit our product forums. Compatibility with future versions of Prepar3D is not implied nor included.)

Supported Operating Systems: Windows 10

Processor (CPU):2.6 GHz CPU required (3.0 GHz, multiple core processor or better recommended.)

Video Card (GPU): DirectX 11 compliant video card with a minimum of 4 GB video RAM

System Memory (RAM): 8 GB RAM

Hard Drive Space: 3 GB (or greater) free hard drive space.

Gaming Controller:

Joystick, yoke, or other gaming controller (a means of controlling the aircraft rudder, either with twist joystick function or dedicated pedals, is additionally recommended).

(Note: All MilViz products require a minimum of one functioning gaming device such as a joystick for proper operation and control.)

Internet Connection: Please note that an active internet connection is required for successful activation of this product.

4-1MilViz KA350i

Product Installation

Pre-Installation Tasks

As with other flight simulator add-ons, pre-instal-lation precautions should involve closing any open applications, as well as temporarily disabling any active antivirus software.

Failure to temporarily disable antivirus software when installing may result in a non-functioning product and/or simulator!!!

Beginning Installation

After purchase, this product may be supplied as a compressed (.zip) file. This compressed file con-tains an executable (.exe) file, which is the installer for the MilViz KA350i.

Using the Windows File Explorer or file compres-sion utility of your choice, unzip this file to a loca-tion of your choosing.

Once unzipped, you may begin installation by right clicking on the executable (.exe) file, then select-ing “Run as administrator”. The installer will run, showing an initial welcome screen. Left click on the “Next” button to continue.

Prerequisites Setup Wizard

The installer will first run a process that checks for missing components that are needed for the KA350i to function.

Clicking ‘Next’ when prompted and following any prompts within the component installers will en-sure that these components are installed and cor-rectly configured for use.

KA350i Setup Wizard

After clicking ‘Next’ on the welcome screen, our installer will require the serial number you received at time of purchase. Entering this will then register your aircraft. This helps to ensure that only legiti-mately purchased copies of the KA350i are in use.

The setup wizard will then determine the cor-rect location for installation. If incorrect, this can changed. Please note that the MilViz KA350i only supports Prepar3D version 4.

Clicking ‘Install’ at the Ready to Install screen will proceed with the installation of the KA350i.

MVAMS Setup Wizard

Once the aircraft files are finished being installed, the installer will automatically run the MilViz Ad-don Management System (MVAMS) Setup Wizard.

The MVAMS application has been bundled with our new aircraft for the last few years, but this wizard ensures that it is properly installed for use with your aircraft.

Post-Installation Tasks

Please be sure to revert your antivirus program settings back to their previous state. Also please make sure that your P3D directory is off-limits to any automatic antivirus scanning. Failure to do this may result in a non-functioning simulator!

It may be worthwhile to back-up or save a copy of the downloaded installer. Please be aware that as new updates are released over time, we do not continue to offer older versions for download due

to support issues. Please also note that support is intended for the latest releases of our products only.

Uninstalling the KA350i

The MilViz KA350i must be uninstalled through the use of the Programs and Features window within the Windows operating system.

Note: Prior to uninstalling the aircraft, please be sure to back up any customized files or custom liv-eries you have installed if you wish to keep them.

Updating

The KA350i is updated by one of two methods, with minor update notifications delivered through the MVAMS application, and major update notifi-cation being provided by your vendor.

To check for a minor update, open the MVAMS application via the MVAMS icon which has been placed on your desktop. If a minor update is avail-able, a notification will appear here. Click yes to begin the update process, which largely mirrors the install process. Major updates may require a new version of the aircraft to be downloaded and installed.

Product Support

If you encounter any issues with your product or require assistance, we encourage you to visit our forums at http://milviz.com/forum/. Support fo-rums for our individual products are restricted to owners of that product. To register, please con-tact [email protected] for details. Please note that proof of purchase will be required.

5-1MilViz KA350i

Simulator Configuration

Options - RealismMilViz aircraft are developed with an overall goal of replicating a realistic level of accuracy in regards to operation and flight response. To this end, devel-opment and testing are generally carried out using the highest realism settings available within the simulator.

Overall, the realism settings within Prepar3D exist in order to make simulated flying less of a chore, as well as to remove some of the tasks which are nec-essary in real life to ensure a safe and proper flight.Our intent is not to discourage such use, but only to ensure that the user has the means to enjoy the aircraft to the level at which it was designed.

Flight ModelFor correct operation, all sliders in the flight model section should be set fully to the right.

Instruments and LightsThe MilViz KA350i has a sophisticated lighting sys-tem in place, so the “Pilot controls aircraft lights” should be checked. “Enable gyro drift” and “Display indicated airspeed” may be left to user preference.

Crashes and DamageThe choices in this section may left to user prefer-ence.

EnginesAll three checkboxes in this section must remain unchecked for correct operation.

Special EffectsThis may be left to user preference.

Flight ControlsFor the most realistic flight experience, “Autorud-der” should not be selected.

AttachmentsThese should remain unchecked.

Options - InformationThe only option of concern in this section is con-cerning ‘User Tips’. There exists an issue in Pre-par3D where if the aircraft uses custom code to handle fuel flow (as the KA350i does), then an in-

correct tip will display to the user that the fuel is low.

To prevent this from showing, please deselect this option, located in General/Information/Miscella-neous Text.

6-1MilViz KA350i

MVAMS Overview

MVAMS stands for MilViz Addon Management Sys-tem. It is a standalone application used by many of our product releases which represents our us-er-friendly solution to the growing complexity of options and choices available within our aircraft. It provides a central location to manage your air-craft, as well as providing incremental update ca-pabilities.

If not already present, the MilViz KA350i installs, and fully integrates with, the MVAMS application. This allows the user access to a range of configu-ration utilities specific to this aircraft.

Starting MVAMS

If this is your first MilViz product that includes the MVAMS application, the KA350i installer will have ran the installer for MVAMS, which will place a shortcut icon on your desktop. If this is not your first MVAMS equipped MilViz product, the shortcut icon may already exist on your desktop. This icon will open the MVAMS application. In addition, the installer will open automatically run MVAMS once installation is complete.

MVAMS Location

The installer places the MVAMS application folder and related files within the AppData\Local\MVAMS folder. If your desktop shortcut is deleted or is oth-erwise missing, the application may be launched from this folder.

Selecting Your Aircraft

When you open the MVAMS application, you are presented with a pictorial view of all MVAMS-compatible aircraft installed on your computer. The configuration details for any aircraft may be

shown by clicking its image with the left mouse button. Your newly installed KA350i will be avail-able in this list for selection.

If it is desired to set the configuration options for more than one aircraft, the aircraft selection menu can be accessed by clicking the logo/icon at the top left corner. Note that leaving the current air-craft configuration page without saving will result in the loss of any options changed or selected.

The aircraft selection overview is not available if

there is only a single MilViz aircraft installed.

Aircraft Specific Details

Each individual aircraft represented within MVAMS has it’s own unique set of configuration options available which determine how the aircraft loads within the simulator. If there are many configura-tion options available, the options are organized into a series of tabs to group similar or related op-tions together. Tabs may be moved between with-out loss of selections or changes made.

6-2MilViz KA350i‘Load’ Tab

The KA350i has a configurable loadout for passengers, fuel, and cargo/bag-gage, configured on the ‘Load’ tab. A series of textboxes are displayed where a desired weight may be input, as well as a pictorial representation of the aircraft cabin to assist the user in making choices about how the aircraft is loaded.

‘Options’ Tab

The ‘Options’ tab for the KA350i consists of configuration for the state of the aircraft systems when the simulator is loaded, allowing the user to tailor the start-up experience to their liking.

The sound levels are customizable; the option exists to sync the KA350i sound with the simulator, or to manually adjust volume of the cockpit, internal en-gine, or external engine sounds.

The MilViz KA350i also tracks the health of the aircraft engines. Engines may be harmed through mishandling, as well as accumulate normal wear. Such damage and wear is persistent across simulator sessions, and can be reset here while the simulator is not running.

‘Show/Hide Items’ Tab

This tab contains initial display settings for the wheel chocks, the engine cov-ers, and the pitot covers. Selecting these allows for these items to be visible when the aircraft is loaded.

Saving and Closing MVAMS

To save any changes or selections made, click the ‘Save Defaults’ button lo-cated at the bottom of the screen (Note: If the aircraft is loaded while you access MVAMS, it will be required to reload the aircraft before most changes made will be present in the simulator.)

To close the MVAMS application, click on the ‘X’ in the top right corner. Note that closing MVAMS without saving will result in the loss of any options changed or selected.

6-3MilViz KA350iEngine State: Explained

As previously mentioned, the KA350i tracks and saves the health of the en-gine. This information is displayed to the user in the form of a pair of status bars in the ‘Options’ tab in the MVAMS application, as shown to the right.

It’s important to note that this bar decreases through wear accumulated dur-ing normal operation. From perfect condition, a full bar depleting to an empty bar represents approximately 100 hours of operation. After that point, the air-craft engine is extremely likely to fail during the next session. At any point prior to this, the aircraft may be ‘serviced’ by pressing the ‘Restore’ button to bring the aircraft to perfect condition. Please note that the simulator must be closed before the engine can be restored.

In addition to normal wear accumulating during regular use, engine wear can be accelerated by operator error and general mishandling of the aircraft engine. Exceeding any of the engine instrumentation limits will reduce the hours-to-service, with ITT over-temperature being one of the most serious.

This increased engine wear, if not monitored and acted upon, is capable of causing an unexpected engine failure. Should an engine failure occur, the only method for ‘fixing’ the failed engine is by closing the simulator and using the option within MVAMS to restore the engine to good condition.

Some of the situations that can cause greatly accelerated engine wear are:

» ITT exceedance at startup (30 or more seconds until failure) » Engine overtorque, such as full power with a feathered propeller (6 or 7

seconds until failure)

Remember, when in doubt, stay within the limitations indicated on the instru-mentation!

7-1MilViz KA350i

In-Game Options

Visual Options

The ability to hide or show the visual options available for the KA350i while the simulator is loaded is performed through the Prepar3D menu bar, under the Add-ons menu. The entries update depending on the current visibility of the item.

Disable/Enable TrueGlass Also found under the Add-Ons menu is the ability to enable or disable the TrueGlass effect.

Showing/Hiding 2D Aircraft Panels

While not technically a configuration item, also present in the KA350i is the ability to display 2D panels for many of the systems and avionics displays available in the product.

These panels can be viewed and selected through the Vehicle > Instrument Panel menu on the Prepar3D menu bar (pictured to the right).

8-1MilViz KA350i

Number of Engines Two

Engine Model PT6A-60A

Engine Type Turboprop

Number of Drive Shafts Two

Engine Shaft Horsepower Rating 1050 SHP

Number of Propellers Two

Number of Blades Four

Propeller TypeConstant-speed, Full-feathering, Reversing, Counter-weighted, Hydraulically Actuated

Usable Fuel Main Fuel System 2546 lbs (380 gal)

Auxiliary Fuel System 1065 lbs (159 gal)

Maximum Weights Maximum Ramp Weight 15,100 lbs

Maximum Take-off Weight 15,000 lbs

Maximum Landing Weight 15,000 lbs

Maximum Zero Fuel Weight 12,500 lbs

Wing Loading 48.4 pounds per square foot

Power Loading 7.14 pounds per shaft horsepower

KA350i Specifications & Limitations

8-2MilViz KA350i

Aircraft & Cabin Dimensions Cabin Width (Maximum) 54 inches

Cabin Length (Between pressure bulkheads) 24 feet, 10 inches

Cabin Height (Maximum) 57 inches

Pressure Vessel Volume 443 cubic feet

Wing Span 57.9 feet

Airplane Length 46.7 feet

Airplane Height 14.33 feet

Cargo Area Volume (Maximum potential) 303 cubic feet

Turning Radius Inside Gear 4 feet

Nose Wheel 20 feet, 6 inches

Outside Gear 21 feet, 2 inches

Wing Tip 41 feet, 7 inches

Airspeed Limitations Maneuvering Speed (VA) 184 KIAS

Maximum Flap Extension/Extended Speed (VFE) 202 KIAS (Approach)

158 KIAS (Full Down)

Maximum Landing Gear Operating Speed (VLO) 184 KIAS (Extension)

166 KIAS (Retraction)

8-3MilViz KA350i

Airspeed Limitations (continued) Maximum Landing Gear Extended Speed (VLE) 184 KIAS

Air Minimum Control Speed (VMCA)

Inoperative Engine Propeller Feathered - Flaps Up 94 KIAS

Inoperative Engine Propeller Feathered - Flaps Approach 93 KIAS

Maximum Operating Speed (VMO)

Sea Level to 21,000 feet 263 KIAS

21,000 to 35,000 feet 163 - 194 KIAS (0.58 Mach)

Stalling Speed (VSO) at maximum weight with flaps down and idle power

81 KIAS

Stalling Speed (VS1) at maximum weight with flaps ap-proach and idle power

89 KIAS

Stalling speed (VS1) at maximum weight with flaps up and idle power

96 KIAS

One-Engine-Inoperative Best Rate-of-Climb Speed 125 KIAS

Flight Load Factor Limits Flaps Up 3.1 G + to 1.24 G -

Flaps Down 2.0 G + to 0.0 G -

Steep Approach Limitations Maximum Approved Approach Angle 5.5°

One-Engine-Inoperative Steep Approaches Not Approved

Flaps Up Steep Approaches Not Approved

8-4MilViz KA350i

Engine Operating Limits

OPERATInG COnDITIOn TORqUE %

MAxIMUM ITT °C

GAS GEnERATOR RPM% n1

PROP RPMn2

OIL PRESSPSI

OIL TEMP°C

STARTInG 1000 0 - 200 -40

IDLE 750 62 1050 60 -40 to +110

TAKEOFF 100 820 104 1700 90 - 135 0 TO 110

MAx COnT. 100 820 104 1700 90 - 135 0 TO 110

CRUISE / CLIMB 785 104 1700 90 - 135 0 TO 110

MAx CRUISE 820 104 1700 90 - 135 0 TO 110

MAx REVERSE 760 1650 90 - 135 0 TO 99

TRAnSIEnT 156 850 104 1870 200 0 TO 110

> Torque limit applies within range of 1000 - 1700 propeller rpm (N2). Below 1000 propeller rpm, torque is limited to 62%.

> Cruise torque values vary with altitude and temperature.

> Inadvertent torque excursions up to 102% are time limited to 7 minutes.

> Transient values are time limited to 20 seconds.

> High ITT at ground idle may be corrected by reducing accessory load and/or increasing N1 rpm

9-1MilViz KA350i

Systems & Controls Overview

General Overview

The KA350i is a twin-engine, all-metal, low-wing monoplane, with fully canti-levered wings and a T-tail empennage.

Seating may be provided for up to 17 persons, including crew.

Control Surfaces

The airplane is equipped with conventional ailerons and rudder, and utilizes a T-tail horizontal stabilizer and elevators mounted at the top of the vertical stabilizer.

The ailerons and elevators are operated through interconnected convention-al control wheels. The rudder pedals are interconnected via linkage located below the floor. Elevator, aileron, and rudder trim are adjustable via controls mounted on the center pedestal.

Control of the elevator trim is accomplished manually by rotating forward (nose-down trim) and aft (nose-up trim) the trim control wheel located on the left side of the pedestal. Electric control of the elevator trim is done through a thumb switch on each control wheel along with a trim disconnect switch on each control wheel.

Rudder Boost

Rudder boost is enabled by setting the pedestal mounted control switch to the RUDDER BOOST position and the AP/YD DISC bar in the up position.

This system senses engine torque from both engines; if the difference in torque exceeds a certain level, the electric servo is activated in order to assist the pilot. An amber caution annunciator, RUD BOOST OFF, is provided on the Caution/Status annunciator panel to indicate that the system is not operat-ing due to the control switch being in the OFF position or the trim disconnect switch being pressed.

Annunciator System

The annunciator system consists of a warning annunciator panel located in the center of the glareshield, and a caution/status annunciator panel locat-ed on the center subpanel. The indicators on the warning annunciator panel are red, while the indicators on the caution/status panel are amber (caution), green (advisory), and white (status).

Also part of the system are the pairs of red MASTER WARNING and amber MASTER CAUTION flashers located on the glareshield, as well as a PRESS TO TEST button located to the right of the warning annunciator panel.

If any triggering fault requires immediate attention and a reaction by the pilot, the appropriate red warning annunciator will illuminate and both red MASTER WARNING flashers will begin flashing. The flashers may be extinguished by pressing the face of either flasher. They will then stop flashing until an addi-tional warning annunciator illuminates.

When a triggering fault requires pilot attention and possible future action, an appropriate amber caution annunciator will illuminate and both amber MAS-TER CAUTION flashers will begin flashing. The flashers may be extinguished by pressing the face of either flasher. They will then stop flashing until an ad-ditional caution annunciator illuminates.

Green advisory annunciators signal that an operation initiated by the pilot was successful and do not require immediate pilot alerting or action. White status annunciators indicate the presence of a normal or abnormal condition and also do not require immediate pilot alerting or action. Green and white annun-ciators do not have a corresponding master flasher.

Flaps

The flaps are operated through the use of a sliding handle on the center ped-estal located below the condition levers. Flap travel is shown on an indicator located on the top of the center pedestal. The flap switch has three positions: UP, TAKEOFF AND APPROACH, and DOWN. The flaps are not able to be stopped in any other position than the three indicated.

9-2MilViz KA350iLanding Gear

Landing gear on the KA350i is extended and retracted hydraulically by means of a switch placarded LDG GEAR CONTROL- UP - DN located on the pilot’s right subpanel.

Safety switches prevent the LDG GEAR CONTROL from being raised while the airplane is on the ground. This safety mechanism can be overridden by use of the red DOWN LOCK REL button located to the left of the LDG GEAR CONTROL. If the LDG GEAR CONTROL is moved out of DN while the airplane is on the ground is, the landing gear warning horn will sound intermittently and a red indicator light located in the LDG GEAR CONTROL will illuminate.

Visual indication of landing gear position is provided by individual green GEARDOWN annunciators NOSE - L - R on the pilot’s right subpanel. These green annunciators may be checked by pressing the annunciator.

Landing Gear Warning System

The landing gear warning system warns the pilot that the landing gear is not down and locked during specific flight regimes. Depending upon the position of the flaps, various warning modes will occur.

With the FLAPS in either the UP or APPROACH position and either or both power levers are retarded below approximately 85% N1, the warning horn will sound and the LDG GEAR CONTROL lights will illuminate. The horn can be muted by pressing the GEAR WARN SILENCE button located on the left power lever. The lights in the LDG GEAR CONTROL cannot be extinguished. If the power lever(s) are advanced above approximately 85% N1, the warning system is rearmed.

With the FLAPS beyond APPROACH position, the warning horn and LDG GEARCONTROL lights will be activated regardless of the power settings, and neither can be cancelled.

Brakes

Dual hydraulic brakes are operated by depressing the toe portion of either the pilot’s or copilot’s rudder pedals. The parking brake control is located below the pilot’s left subpanel. The parking brake is applied by pulling out the park-ing brake handle, and may be released by pushing the parking brake handle in.

Propulsion System

The propulsion system is operated by three sets of controls; twin power levers twin propeller levers, and twin condition levers, with each lever corresponding to the engine on that side of the airplane.

Power Levers

The power levers enable control of engine power from idle through take-off power via the gas generator (N1) governor in the fuel control unit. Increasing gas generator (N1) RPM increases engine power.

Propeller Levers

Each propeller lever directly adjusts the propeller governor of the respective engine in order to increase or decrease propeller RPM. While in flight, the op-erating range of the propellers is 1450 to 1700 rpm.

Condition Levers

The condition levers control the fuel cutoff function of the fuel control unit, along with limiting idle speed at 62% N1 for low idle and 70% N1 for high idle. Each control lever has three positions; FUEL CUTOFF, LOW IDLE and HIGHIDLE.

Propeller Ground Fine Operation

Propeller ground fine operation provides optimum deceleration wile the air-plane is on the ground during landing by utilizing the maximum available pro-peller drag. Operation is achieved through a gate position for the power levers, retarded past IDLE into the GROUND FINE gate.

Propeller ReversingThe power levers, when retarded past the IDLE and GROUND FINE positions, provide engine power in the REVERSE range. Setting the condition levers at HIGH IDLE (70% N1 minimum) provides for maximum reversing performance.

9-3MilViz KA350iEngine Instrumentation

Engine instruments are displayed in the upper area of the MFD. Along with in-corporated green, yellow, and red operating ranges and time limit monitoring of each range, these give the pilot a visual indication of engine parameters. The following engine instrumentation is displayed:

» ITT indicators » Torquemeters » N2 (propeller) tachometers » N1 (gas generator) tachometers » Fuel Flow indicators » Oil Temperature & Pressure indicators

Propeller Synchrophaser

The propeller synchrophaser system serves to match the RPM of both propel-lers at a preset phase relationship in order to reduce cabin noise. It may be used in all flight operations.

To engage the synchrophaser system, manually set each propeller RPM to within 10 RPM of each other, then turn the prop sync switch to ON.

Starting & Ignition System

The engines are started through the use of a three position switch located on the pilot’s left subpanel placarded, IGNITION AND ENGINE START - LEFT - RIGHT - ON - OFF -STARTER ONLY. Moving the switch to the ON position activates both the starter and ignition, and the appropriate IGNITION ON an-nunciator will illuminate. The starter is stopped by moving the switch to the center OFF position. The STARTER ONLY position is used to motor the engine without ignition.

Auto Ignition

The auto ignition system is used to prevent engine loss in the case of com-bustion failure. This ensures constant ignition during turbulence or flight in icing or precipitation conditions.

Electronic Flight Instrument System (EFIS)

The electronic flight instrument system consists of three 8” x 10” adaptive flight displays (AFD), provided as two primary flight displays (PFD) and one multifunction display (MFD). Each PFD displays airplane attitude, heading, airspeed, altitude, vertical speed, flight guidance system annunciations and navigation data. The PFD may also provide engine monitoring information when placed in reversionary mode.

The upper area of the PFD displays the Attitude Director Indicator (ADI), alti-tude scale, airspeed scale and vertical speed scale. Flight guidance system mode information shows directly above the ADI.

The lower area of the PFD presents a Horizontal Situation Indicator (HSI); Weather radar or EGPWS information can be overlaid on the partial arc format or map format. The space to either side of the HSI format is used to display lateral navigation data, weather radar mode, EGPWS mode, system messages and selected menus.

Along the bottom of the PFD is shown radio tuning, time and temperature displays.

The MFD is used to show information such as: Present Position Map, TCAS, and FMS based textual data, navigation data, engine data, and the electronic checklist.

Basic display formats are controlled through the line select keys that are pro-vided as bezel mounted line select keys. These, along with the display control panel and the flight guidance panel, provide a primary pilot interface to the PFD and the MFD. Radar, NAV sources, and bearing pointers are controlled through the display control panel and the line select keys, while the course, preselect heading, altitude and speed references are controlled through the flight guidance panel.

Display Control Panel (DCP)

Two display control panels handle the menu and display functions of the PFDs and the MFD, located adjacent to the PFD or MFD they normally control. When combined with the line select keys on the PFD, control is provided for the weather radar, NAV sources, bearing pointers, V speeds, BARO minimums and RA minimums.

9-4MilViz KA350iControl Display Unit (CDU)

A color LCD-based Control Display Unit (CDU) is located on the center pedes-tal. It includes an integrated keyboard, an alphanumeric keypad, and six line select keys located in the bezel of the color LCD display.

The CDU provides integrated control of various combinations of airplane com-munications and navigation, including the Flight Management System (FMS).

Flight Management System (FMS)

The Flight Management System (FMS) serves to provide flight plan manage-ment, airplane navigation, and radio tuning. The system consists of a Flight Management Computer (FMC), a Control Display Unit (CDU) and a Data Base Unit (DBU).

The FMC is used by the autopilot to fly a programmed flight plan. It processes coupled VNAV, NAV-to-NAV capture, navaid database storage and several control/planning functions. The FMS will provide navigation solutions if it is receiving suitable navigation information from one or more of the following:

» One VOR/DME » Two DMEs » One GPS

Radio Tuning System

The Radio Tuning System provides the control, displays, and sensors for VHF & HF voice communication, VOR/ILS/DME, ADF, transponder tuning, and TCAS II. The system consists of a primary Radio Tuning Unit (RTU) located in the center of the instrument panel, and a secondary radio tuning unit contained in the CDU on the pedestal.

10-1MilViz KA350i

Panel Overview - Front

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1. PFD2. MFD3. FLIGHT GUIDANCE PANEL4. RADIO TUNING UNIT5. COMM/RADIO SWITCH PANEL6. CAUTION/STATUS ANNUNCIATOR PANEL7. WARNING ANNUNCIATOR PANEL

8. MASTER CAUTION/WARNING LIGHTS9. BACKUP ATTITUDE INDICATOR10. PARKING BRAKE CONTROL11. PILOT’S LEFT LOWER PANEL12. PILOT’S RIGHT LOWER PANEL13. CO-PILOT’S LEFT LOWER PANEL14. CO-PILOT’S RIGHT LOWER PANEL

15. FLAP INDICATOR16. CABIN VERTICAL SPEED INDICATOR17. CABIN PRESSURE INDICATOR18. CENTER SWITCH PANEL19. DISPLAY CONTROL PANEL20. TAWS INHIBIT LAMPS21. FIRE / EMERGENCY LAMPS

10-2MilViz KA350i

Panel Overview - Pilot’s Left Lower Panel

ExTPWR

AVIOnICSMASTERPOWER

EGnAUTO

IGn

EnGInE AnTI-ICE

ACTUATORSMAIn

STAnDBY

On

OFF

LEFT RIGHT

ARM

OFFLEFT RIGHT

PROP TEST

OFF

GOVGnD IDLE

STOP

AUTOFEATHER

ARM

TEST

OFF

EnGInE AnDIGnITIOn START

LEFT RIGHTOn

OFF

STARTER OnLY

BUS SEnSERESET

TEST

GEn TIESMAn CLOSE

OPEn

nORM

On

TEST

OFF

ESIS

BAT BUS

nORM

EMEROFF R GEnL GEnBAT

GEnRESET

On

OFF

PARKInG BRAKE

10-3MilViz KA350i

Panel Overview - Pilot’s Right Lower Panel

SURFACEDEICE

SInGLE

MAnUAL

UP

DOWn

STROBEBEACOnLAnDInG

TAILFLOOD

STALLWARn

LIGHTS

LIGHTS

TAxI ICE nAV RECOG

LEFT RIGHTOFF

ICE PROTECTIOnPROPWSHLD AnTI-ICE

nORMALOFF

HIGH PILOT CO-PILOT

AUTO MAnUAL FUEL VEnT

LEFT RIGHT

LEFT RIGHTOFF

OFF

BRAKEDEICE LAnDInG

GEAR

RELAY

OFF

DOWnLOCKREL

HD LTTEST

GEARDOWn

nOSE

L R

HYD FLUIDSEnSOR

TEST

PITOT

10-4MilViz KA350i

Panel Overview - Co-pilot’s Left Lower Panel

MAnHEAT

AUTO InCR

EnVIROnMEnTAL

OFF

BLEEDLEFT

OFF

BLOWER TEMP MAn COOL MAn TEMPInCR

InCR

AUTO

ELECHEAT

MODE

COCKPIT

DECR

EnG

BLOWER

PnEU & EnVIR OFF

OFF

AUTO

TEST

WARnSILEnCE

LOW

LEFT RIGHT

EnVIRBLEED AIR

nORMAL

EnVIROFF

OFF

TEMP

AUTO InCR InCR

CABIn

AIROPEn

VALVESRIGHT

FIREDET

ExT

OFF

ALTCABInTEST

CABIn DIFFWARn TEST

WInDOWDEFOG

OFF

OVERSPEEDWARn TEST

OFF

STALLWARn TEST

LFG GEARWARn TEST

10-5MilViz KA350i

Panel Overview - Overhead Control Panel

DI

M

OFF

OFF

MASTERPAnELLIGHTS

On

PILOTInSTR

PnLOFF

BRT

PILOTDISPLAYS

BRT

WInDSHIELD WIPEROFF

PARK SLOW

FAST

PILOTOVHD

FLOODOFF

BRT BRT BRT

BRT BRT BRT

OVHD PED& SUBPAnEL

OFF

SIDEPAnEL

OFFCOPILOT

DISPLAYS

COPILOTInSTR

PnLOFF

AnnUnPUSH BRT

DIM

BRT

CABInLIGHT

PAx

OFF

nO SMKFSB

FSB

InTERIORMASTER

On

OFF

EnTRYLIGHTS

On

L GEn R GEn

CTR TPL FED

ExTPWR

BAT

VOLT METERBUS SELECT

DC%LOAD DC%LOAD

DC

VOLT

BAT

AMP

PROP AMPS

MAXIMUMIAS KNOTS

GR EXTENSIONGR RETRACTGR EXTENDEDAPPROACH FLAPFULL ON FLAPMANEUVERING

184166184202158184

InSTRUMEnTEMERG LIGHTS

On

OFF

10-6MilViz KA350i

nOMEnCLATURE COLOR CAUSE FOR ILLUMInATIOn

DOOR UnLOCKED RED Airstair /Cargo Door open or not secure

L FUEL PRES LOW RED Fuel pressure failure on left side

CABIn ALT HI RED Cabin pressure altitude exceeds 12,000 ft

CABIn DIFF HI RED Cabin differential pressure exceeds 6.9 psi

R FUEL PRES LO RED Fuel pressure failure on right side

L OIL PRES LO RED Low oil pressure left engine

R OIL PRES LO RED Low oil pressure right engine

L BLEED AIR RED Melted or failed plastic left bleed air failure line

R BLEED AIR RED Melted or failed plastic right bleed air failure line

Panel Overview - Warning Annunciator Panel

-- -- DOOR UnLOCKED -- --

L FUEL PRES LOW -- CABIn ALT HI CABIn DIFF HI R FUEL PRES LO

L OIL PRES LO -- -- -- R OIL PRES LO

-- L BLEED AIR -- R BLEED AIR --

10-7MilViz KA350i

L DC GEn L GEn TIE OPEn HYD FLUID LOW RVS nOT READY R GEn TIE OPEn R DC GEn

L CHIP DETECT L nO FUEL xFR BAT TIE OPEn DUCT OVERTEMP R nO FUEL xFER R CHIP DETECT

L EnG ICE FAIL L FUEL qTY ELEC HEAT On ExT PWR R FUEL qTY R EnG ICE FAIL

L BL AIR OFF AUTOFTHR OFF -- OxY nOT ARMED RUD BOOST OFF R BL AIR OFF

L PITOT HEAT -- -- PROP GnD SOL -- R PITOT HEAT

L IGnITIOn On l Eng Anti-icE FUEL CROSSFEED -- r Eng Anti-icE R IGnITIOn On

WInG DEICE L BK DEICE On MAn TIES CLOSE -- R BK DEICE On TAIL DEICE

L PROP PITCH CABIn ALTITUDE LDG/TAxI LIGHT PASS OxY On AIR COnD n1 LOW R PROP PITCH

Panel Overview - Caution / Advisory / Status Annunciator Panel


L DC GEn AMBER Left generator offline

L GEn TIE OPEn AMBER Left generator bus isolated from center bus

HYD FLUID LOW AMBER Hydraulic fluid in the power pack is low

RVS nOT READY AMBER Propeller levers are not in the high rpm, low pitch position with landing gear extended

R GEn TIE OPEn AMBER Right generator bus isolated from center bus

R DC GEn AMBER Right generator offline

10-8MilViz KA350i


L CHIP DETECT AMBER Metal contamination detected in left engine oil

L nO FUEL xFR AMBER No left auxiliary fuel transfer

BAT TIE OPEn AMBER Battery isolated from generator buses

DUCT OVERTEMP AMBER Duct air too hot

R nO FUEL xFR AMBER No right auxiliary fuel transfer

R CHIP DETECT AMBER Metal contamination detected in right engine oil

L EnG ICE FAIL AMBER Left engine selected anti-ice system is inoperative

L FUEL qTY AMBER Left fuel quantity has less than 30 minutes remaining at maximum continuous power

ELEC HEAT On AMBER Electric heat is on

ExT PWR AMBER External power is connected

R FUEL qTY AMBER Right fuel quantity has less than 30 minutes remaining at maximum continuous power

R EnG ICE FAIL AMBER Right engine selected anti-ice system is inoperative

L BL AIR OFF AMBER Left bleed air flow control valve is closed

AUTOFTHER OFF AMBER Autofeather switch is not armed and landing gear is extended

OxY nOT ARMED AMBER Oxygen arming handle not pulled or system failed to charge

RUD BOOST OFF AMBER Rudder Boost Switch is OFF

10-9MilViz KA350i


R BL AIR OFF AMBER Right bleed air flow control valve is closed

L PITOT HEAT AMBER Left Pitot Heat inoperative or switch is in the OFF position

PROP GnD SOL AMBER 28v is being delivered to one or both ground idle low pitch stop solenoids.

R PITOT HEAT AMBER Right Pitot Heat inoperative or switch is in the OFF position

L IGnITIOn On GREEn Left ignition & engine start switch is on, or left auto ignition is armed and left engine torque is below 17%

l Eng Anti-icE GREEn Left engine anti-ice vanes in position for icing conditions

FUEL CROSSFEED GREEn Crossfeed valve is open

r Eng Anti-icE GREEn Right engine anti-ice vanes in position for icing conditions

R IGnITIOn On GREEn Right ignition & engine start switch is on, or right auto ignition is armed and left engine torque is below 17%

WInG DEICE GREEn Wing surface deice system in operation

L BK DEICE On GREEn Left brake deice system in operation

MAn TIES CLOSE GREEn Manually closed generator bus ties

R BK DEICE On GREEn Right brake deice system in operation

TAIL DEICE GREEn Horizontal stabilizer surface deice system in operation

L PROP PITCH WHITE Left propeller is below the flight idle stop

CABIn ALTITUDE WHITE Cabin Altitude exceeds 10,000 feet

10-10MilViz KA350i


LDG/TAxI LIGHT WHITE Landing light(s) or taxi light on with landing gear up

PASS OxYGEn On WHITE Passenger oxygen system charged

AIR COnD n1 LOW WHITE Right engine N1 too low for air conditioning load

R PROP PITCH WHITE Right propeller is below the flight idle stop

11-1MilViz KA350i

TAKEOFF WEIGHT ITEM

OUTSIDE AIR TEMPERATURE °C

-35 -15 -5 5 15 25 35 45 52

15,000 LBS

v1 (KiAS)vr (KiAS)v2 (KiAS)toFl (Ft)

106109117

3085

106110117

3505

106110117

3716

106110117

3949

106110117

4192

106110117

4541

108111117

5181

110111117

5919

111112117

6493

14,000 lbS


103106114

2682

102106114

3057

102106114

3255

102107114

3459

102107114

3654

102107114

3955

104107114

4504

106108114

5129

107108114

5607

13,000 LBS


101104112

2373

99104111

2692

99104111

2857

99104111

3026

99104111

3203

99104111

3458

100104111

3910

102105110

4430

103105110

4843

12,000 LBS


99104112

2199

98104112

2489

98104112

2646

98104111

2799

97104111

2960

97104111

3193

99104110

3602

100104110

4037

101104110

4361

11,000 LBS


98104112

2028

97104112

2290

97104112

2431

96104112

2577

96104112

2722

96104111

2931

97104111

3301

99104110

3733

99104110

4021

10,500 LBS AnD UnDER


97104112

1943

97104112

2192

96104112

2326

96104112

2465

95104112

2606

95104111

2803

96104111

3155

98104110

3562

99104110

3681

Takeoff Speeds & Field Length Reference (Sea Level)

> Flaps in UP position > A/C and Bleed Air ON

11-2MilViz KA350i

TAKEOFF WEIGHT ITEM


-35 -15 -5 5 15 25 35 45 52

15,000 LBS


106110117

3458

106110117

3931

106110117

4191

106110117

4443

106110117

4713

107111117

5324

109111117

6109

111112117

7017

--------

14,000 lbS


103106114

3014

102107114

3443

102107114

3654

102107114

3878

102107114

4108

103107114

4637

105108114

5295

107108114

6068

--------

13,000 LBS


100104111

2655

99104111

3014

99104111

3204

98104111

3397

98104111

3586

99104111

4028

101105110

4585

103105110

5233

--------

12,000 LBS


98104112

2455

98104111

2788

97104111

2960

97104111

3139

97104111

3313

98104110

3709

99104110

4169

100104109

4693

--------

11,000 LBS


97104112

2259

96104112

2566

96104112

2722

96104111

2883

95104111

3044

96104111

3400

98104110

3855

99104110

4348

--------



97104112

2163

96104112

2455

95104112

2606

95104112

2759

95104111

2910

96104111

3250

97104110

3679

98104110

4161

--------

Takeoff Speeds & Field Length Reference (2000 ft)


11-3MilViz KA350i

TAKEOFF WEIGHT ITEM


-35 -15 -5 5 15 25 35 45 52

15,000 LBS


106110117

3879

106110117

4429

106110117

4719

106110117

5016

107111117

5531

108111117

6300

110112117

7219

--------

--------

14,000 lbS


102107114

3399

102107114

3866

102107114

4114

102107114

4370

103107114

4819

104108114

5454

106108114

6244

--------

--------

13,000 LBS


99104111

2977

98104111

3387

98104111

3600

98104111

3821

99104111

4191

100105110

4728

102105110

5388

--------

--------

12,000 LBS


98104111

2755

97104111

3130

97104111

3325

97104111

3526

97104110

3860

98104110

4316

100104110

4853

--------

--------

11,000 LBS


96104112

2535

96104111

2875

95104111

3056

95104111

3239

96104111

3538

97104110

3978

98104110

4477

--------

--------



96104112

2424

95104112

2751

95104111

2922

94104111

3099

95104111

3381

96104110

3797

98104110

4297

--------

--------



11-4MilViz KA350i

TAKEOFF WEIGHT ITEM


-35 -15 -5 5 15 25 35 45 52

15,000 LBS


106110117

4378

106110117

5007

106110117

5332

106111117

5795

108111117

6535

110112117

7448

111112117

8599

--------

--------

14,000 lbS


102107114

3823

102107114

4363

102107114

4664

102107114

5050

104108114

5674

105108114

6448

107109114

7419

--------

--------

13,000 LBS


98104111

3351

98104111

3815

98104110

4053

98104111

4397

100104110

4921

101105110

5572

103106110

6381

--------

--------

12,000 LBS


97104111

3095

97104111

3521

97104111

3749

97104110

4049

98104110

4499

99104110

5029

100104109

5667

--------

--------

11,000 LBS


96104111

2844

95104111

3235

95104111

3440

95104111

3713

96104110

4144

98104110

4642

99104109

5235

--------

--------



95104112

2722

94104111

3094

94104111

3290

94104111

3548

96104110

3955

97104110

4449

98104109

5023

--------

--------



11-5MilViz KA350i

TAKEOFF WEIGHT ITEM


-35 -15 -5 5 15 25 35 45 52

15,000 LBS


105110117

4956

106111117

5689

106111117

6127

107111117

6850

109112117

7761

111112117

8926

--------

--------

--------

14,000 lbS


102107114

4317

102107114

4955

102107114

5341

103108114

5956

105108114

6723

107109114

7673

109109114

8913

--------

--------

13,000 LBS


98104111

3778

98104110

4314

98104110

4641

99105110

5166

101105110

5811

102106110

6616

104106110

7634

--------

--------

12,000 LBS


97104111

3487

97104111

3987

97104110

4286

97104110

4721

98104110

5250

100104109

5893

101104108

6683

--------

--------

11,000 LBS


95104111

3204

95104111

3658

95104111

3926

96104110

4350

97104110

4842

98104109

5442

100104109

6167

--------

--------



94104111

3065

94104111

3497

94104111

3751

95104110

4153

96104110

4652

98104110

5231

99104109

5916

--------

--------



11-6MilViz KA350i

TAKEOFF WEIGHT ITEM


-35 -15 -5 5 15 25 35 45 52

15,000 LBS


106111117

5693

106111117

6599

107111117

7329

109112117

8242

110112117

9437

--------

--------

--------

--------

14,000 lbS


102107114

4962

102108114

5756

103108114

6360

104108114

7134

106109114

8117

108109114

9379

--------

--------

--------

13,000 LBS


98104110

4320

98104110

5007

99105110

5523

100105110

6168

102106110

6996

104106110

8030

--------

--------

--------

12,000 LBS


96104111

3993

97104110

4613

97104110

5041

98104110

5575

99104109

6224

101104109

7032

--------

--------

--------

11,000 LBS


95104111

3664

95104111

4226

96104110

4646

97104110

5140

98104109

5751

99104109

6487

--------

--------

--------



94104111

3502

94104111

4036

95104110

4436

96104110

4936

97104110

5521

99104109

6234

--------

--------

--------

Takeoff Speeds & Field Length Reference (10,000 ft)


12-1MilViz KA350i

Normal Procedures

Preflight Inspection 12-1

Before Engine Starting 12-7

Engine Starting (Battery) 12-9

Engine Starting (External Power) 12-11

Before Taxi 12-13

Before Takeoff - Runup 12-17

Before Takeoff - Final Items 12-22

Takeoff 12-23

Climb & Cruise 12-24

Descent & Before Landing 12-25

Landing & After Landing 12-26

Shutdown & Securing 12-28

Emergency and Abnormal procedures are not listed.

References to details obviously unavailable within a simulation environment have been in-cluded for those interested, but should not be taken literally.

12-2MilViz KA350i

Preflight Inspection

Cabin

1. Baggage secure

2. Aft exit signON-TEST

chEck illumiNaTiONOff-rESET

3. Forward exit signSTOw ON-TEST

chEck illumiNaTiONOff-rESET

4. emergency exits secure & unlocked

5. control locks remove

6. Parking Brake SET

7. landing Gear dOwN

8. condition levers fuEl cuTOff

9. Elevator Trim 2 uNiTS NOSE up

10. rudder Trim 0 uNiTS

11. aileron Trim 0 uNiTS

12. Battery Bus norm

13. Voltmeter - BaT position 23 VOlTS miN

14. Battery on

15. Landing Gear Indicators ILLUMINATED

16. Fuel Quantity CHECK

17. Voltmeter - TPL FED 22 VOLTS MIN

18. Voltmeter - L GEN & R GEN 0 VOLTS

19. Voltmeter - CTR 23 VOLTS MIN

20. Voltmeter - EXT PWR 0 VOLTS

21. GEN TIES MAN CLOSE

22. Flaps CHECK

23. Battery OFF

(Preflight (Cabin) Inspection complete)

12-3MilViz KA350i

Preflight Inspection [continued]

LEFT WING & ENGINE NACELLE

1. Cabin Door Seal CheCk

2. handrails CheCk

3. Left Side Windows CheCk

4. Flaps CheCk

5. Aileron & Trim Tab CheCk

6. Static Wicks CheCk

7. Siphon Break Vent CheCk

8. Lights CheCk

9. Main Fuel Tank Cap SeCure

10. Stall Warning Vane CheCk

11. Tie-Down reMoVe

12. outboard Fuel Drain DrAin

13. outboard Deice Boot & Stall Strip CheCk

14. Wing Panels SeCure

15. Leading-edge Fuel Tank & Gravity-Line Drains DrAin

16. Inverter Cooling Louvers CLEAR

17. Flush Fuel Vent & Heated Fuel Vent CLEAR

18. Landing Gear CHECK

19. Engine Oil Vent CLEAR

20. Brake Line CHECK

21. Brakes CHECK

22. Wheel Chocks REMOVE

23. Fuel Strainer & Fuel Filter Drains DRAIN

24. Ice Vane & Oil Radiator Exhaust CLEAR

25. Ice Light CHECK

26. Engine Oil CHECK, SECURE CAP

27. Cowling Air Exhaust CLEAR

28. Left Side Engine Cowling, Doors, & Panels SECURE

29. Left Side Exhaust Stack CHECK

30. Left Side Top Cowling Camlocks SECURE

31. Propeller CHECK , ROTATE

12-4MilViz KA350i


lEFt Wing & EnginE nAcEllE (continued)

32. Top Cowling Air Intakes CLEAR

33. Engine & Oil Radiator Air Intakes CLEAR

34. Right Side Top Cowling Camlocks SECURE

35. Right Side Exhaust Stack CHECK

36. Swing Check Valve Exhaust CLEAR

37. Generator Air Intake CLEAR

38. Right Side Engine Cowling, Doors, & Panels SECURE

39. Auxiliary Fuel Tank Cap SECURE

40. Hydraulic Gear Service Door SECURE

41. Inboard Deice Boot CHECK

42. Heat Exchanger Air Intake & Exhaust CLEAR

43. Hydraulic Gear Overfill & Vent Lines CLEAR

44. Auxiliary Fuel Tank Drain DRAIN

45. Lower Antennas & Panels SECURE

(Preflight (Left Wing & Engine Nacelle) Inspection complete)

nOSE

1. OAT Probe & Relief Tube Vent CHECK

2. Brake Reservoir Vent CLEAR

3. Left Avionics Access Panel SECURE

4. Air Conditioner Condenser Exhaust Duct CLEAR

5. Windshield & Windshield Wipers CHECK

6. Radome CHECK

7. Pitot Masts CLEAR

8. Landing & Taxi Lights CHECK

9. Nose Gear CHECK


11. Nose Gear Doors & Wheel Well CHECK

12. Air Conditioner Condenser Intake Duct CLEAR

13. Right Avionics Access Panel SECURE

(Preflight (Nose) Inspection complete)

12-5MilViz KA350i


RIGHT WInG & EnGInE nACELLE

1. Ejector Exhaust CLEAR

2. Auxiliary Fuel Tank Drain DRAIN

3. Battery Box Drain CLEAR

4. Lower Panels SECURE

5. Heat Exchanger Air Intake & Exhaust CLEAR

6. Inboard Deice Boot CHECK

7. Battery Access Panel SECURE

8. Auxiliary Fuel Tank Cap SECURE

9. Engine Oil CHECK, SECURE CAP

10. Cowling Air Exhaust CLEAR

11. Left Side Engine Cowling, Doors, & Panels SECURE

12. Collector Drain CLEAR

13. Left Side Exhaust Stack CHECK

14. Left Side Top Cowling Camlocks SECURE

15. Propeller CHECK , ROTATE

16. Top Cowling Air Intakes CLEAR

17. Engine & Oil Radiator Air Intakes CHECK

18. Right Side Top Cowling Camlocks SECURE

19. Right Side Exhaust Stack CHECK

20. Swing Check Valve Exhaust CLEAR

21. Generator Air Intake CLEAR

22. Right Side Engine Cowling, Doors, & Panels SECURE

23. Ice Light CHECK

24. Oil Radiator & Ice Vane Exhaust CLEAR

25. Fuel Filter & Fuel Strainer Drains DRAIN

26. Landing Gear CHECK

27. Engine Oil Vent CLEAR

28. Brake Line CHECK

29. Brakes CHECK


31. Flush Fuel Vent & Heated Fuel Vent CLEAR

12-6MilViz KA350i


right Wing & EnginE nAcEllE (continued)

32. Inverter Cooling Louvers CLEAR

33. Leading-Edge Fuel Tank & Gravity-Line Drains DRAIN

34. External Power Door SECURE

35. Wing Panels SECURE

36. Outboard Deice Boot & Stall Strip CHECK

37. Outboard Fuel Drain DRAIN

38. Tie-Down REMOVE

39. Main Fuel Tank Cap SECURE

40. Lights CHECK

41. Static Wicks CHECK

42. Siphon Break Vent CLEAR

43. Aileron CHECK

44. Flaps CHECK

45. Right Side Windows CHECK

(Preflight (Right Wing & Engine Nacelle) Inspection complete)

RIGHT AFT FUSELAGE

1. Lower Antennas & Beacon CHECK

2. Oxygen Service Access Door SECURE

3. Static Ports CLEAR

4. ELT Antenna CHECK

5. Aft Compartment Lower Access Door SECURE

6. Tie-down REMOVE

7. Ventral Fin Drain Holes CLEAR

8. Cabin Air Exhaust CLEAR

9. Access Panel SECURE

(Preflight (Right Aft Fuselage) Inspection complete)

12-7MilViz KA350i


TAIL

1. Ventral Fin & Static Wick CHECK

2. VOR Antennas CHECK

3. Rudder & Trim Tab CHECK

4. Horizontal Stabilizer CHECK

5. Elevator & Trim Tab CHECK

6. Trim Tabs in Neutral Position VERIFY

7. Lights CHECK

(Preflight (Tail) Inspection complete)

LEFT AFT FUSELAGE

1. Access Panels SECURE

2. Static Ports CLEAR

3. Oxygen Discharge & Aft Drain Tubes CLEAR

4. Relief Tube CLEAR

(Preflight (Left Aft Fuselage) Inspection complete)

(Preflight Inspection checklist complete)

12-8MilViz KA350i

Before Engine Starting

1. Weight, CG, Performance, & V-Speeds CHECKED

2. Doors LOCKED

3. Load & Baggage CONFIRM SECURED

4. Passenger Briefing COMPLETE

5. Cabin Equipment POSITIONED

6. Parking Brake CONFIRM SET

7. Control Locks CONFIRM REMOVED

8. Oxygen System Preflight CONFIRM COMPLETE

9. ELT Switch ARM

10. Fuel Panel CHECK

a. Standby Pumps OFF

b. Crossfeed OFF

c. Aux Transfer Switches AUTO

d. Circuit Breakers IN

11. Pilot’s Instrument Panel & Subpanel CHECK

a. ESIS Power ON

b. Battery Bus CONFIRM NORM

c. Engine Anti-ice ON & MAIN

d. Landing Gear Relay Circuit Breaker IN

e. Landing Gear Control DOWN

12. Power Console & Pedestal CHECK

a. Power Levers IDLE

b. Prop Levers FULL FORWARD

c. Condition Levers FUEL CUTOFF

d. Oxygen Controls SET

e. Landing Gear Alternate Extension Handle STOWED

13. Reversionary Switch Panel CHECK

a. DG FREE/NORM NORM

b. SLEW +/- CENTER

c. ATC Select STBY

d. PILOT DISPLAY NORM

e. AHRS NORM

12-9MilViz KA350i

Before Engine Starting [continued]

f. ADC NORM

g. TUNE NORM

h. RMT TUNE NORM

i. GND COM EXTINGUISHED

14. Copilot’s Subpanel & Instrument Panel CHECK

a. Window Defog OFF

b. ECS Mode OFF

c. Cabin Blower AUTO

d. Env. Bleed Air AS REQUIRED

15. Electric Heat AS REQUIRED

16. Right Panel Circuit Breakers IN

17. Pilot’s Static Air Source NORMAL

18. Interior Master Switch OFF

19. Battery ON

20. Annunciators TEST

21. Fuel System CHECK

a. Firewall Fuel Valves OPEN

b. Standby Pumps OFF

c. Crossfeed OFF

d. Fuel Quantity TEST


23. Pilot’s Subpanel CHECK

a. Landing Gear Control Lights TEST

b. Hydraulic Fluid Sensor TEST

c. Beacon ON

24. Copilot’s Subpanel CHECK

a. Cabin Altitude Warning TEST

b. Cabin Differential Warning TEST

c. Stall & Landing Gear Warning TEST

d. Fire Detector & Extinguisher TEST

(Before Engine Starting checklist complete)

12-10MilViz KA350i

Engine Starting (Battery)


2. Propeller Area CLEAR

3. Right Ignition & Engine Start ON

�observee] � [R IGNITION ON] ILLUMINATED

�observee] � [R FUEL PRES LO] EXTINGUISHED

�waite]� After N1 reaches 12% (minimum):

4. Right Condition Lever LOW IDLE

5. Right ITT & N1 MONITOR

6. Right Oil Pressure CHECK

�waite]� After N1 reaches 50%:

7. Right Ignition & Engine Start OFF

8. Right Condition Lever HIGH IDLE

9. Right Generator RESET, THEN ON

�observee] � [R DC GEN] EXTINGUISHED

�observee] � [L GEN TIE OPEN] EXTINGUISHED

�observee] � [R GEN TIE OPEN] EXTINGUISHED

10. Battery CHARGE

11. Left Ignition & Engine Start ON

�observee] � [L IGNITION ON] ILLUMINATED

�observee] � [L FUEL PRES LO] EXTINGUISHED


12. Left Condition Lever LOW IDLE

13. Left ITT & N1 MONITOR

14. Left Oil Pressure CHECK


15. Left Ignition & Engine Start OFF


17. Left and Right Prop RPM 1050 MINIMUM

�observee] � [L PROP PITCH] ILLUMINATED

�observee] � [R PROP PITCH] ILLUMINATED

12-11MilViz KA350i

Engine Starting (Battery) [continued]

18. Voltmeter - L GEN 27.5 - 29.0 VOLTS

19. Left Generator RESET, THEN ON

�observee] � [L DC GEN] EXTINGUISHED

20. Right Generator RESET



21. Right Generator ON

(Engine Starting (Battery) checklist complete)

12-12MilViz KA350i

Engine Starting (External Power)

1. Battery VERIFY ON


3. Voltmeter - BAT 20.0 VOLTS MINIMUM

4. External Power VERIFY OFF

5. Avionics Master VERIFY OFF

6. Left and Right Generators VERIFY OFF

7. Interior Master Switch VERIFY OFF

8. Battery Bus VERIFY NORM

9. Beacon VERIFY ON

10. External Power Source TURN OFF

CONNECT TO AIRPLANE

TURN ON

11. Voltmeter - EXT PWR 28.0 - 28.4 VOLTS

12. External Power ON

�observee] � [EXT PWR] ILLUMINATED

13. Prop Levers FEATHER

14. Propeller Area CLEAR

15. Right Ignition & Engine Start ON


�observee] � [R FUEL PRES LO] EXTINGUISHED



17. Right ITT & N1 MONITOR

18. Right Oil Pressure CHECK


19. Right Ignition & Engine Start OFF

20. Left Ignition & Engine Start ON


�observee] � [L FUEL PRES LO] EXTINGUISHED


21. Left Condition Lever LOW IDLE

22. Left ITT & N1 MONITOR

12-13MilViz KA350i

Engine Starting (External Power) [continued]

23. Left Oil Pressure CHECK


24. Left Ignition & Engine Start OFF

25. External Power OFF

26. External Power Source TURN OFF

DISCONNECT FROM AIRPLANE

SECURE DOOR

�observee] � [EXT PWR] EXTINGUISHED

27. Right Generator RESET, THEN ON

�observee] � [R DC GEN] EXTINGUISHED



28. Voltmeter - L GEN 27.5 TO 29.0 VOLTS

29. Left Generator RESET, THEN ON

�observee] � [L DC GEN] EXTINGUISHED

30. Right Generator .RESET, THEN ON



31. Prop Levers FULL FORWARD

32. Left & Right Prop RPM 1050 MINIMUM



(Engine Starting (External Power) checklist complete)

12-14MilViz KA350i

Before Taxi

1. Electrical System CHECK

a. GEN TIES OPEN

�observee] � [L GEN TIE OPEN] ILLUMINATED

�observee] � [R GEN TIE OPEN] ILLUMINATED

b. Voltmeter CHECK

1) TPL FED 26.5 TO 28.0 VOLTS

2) R GEN 27.5 TO 29.0 VOLTS

3) L GEN 27.5 TO 29.0 VOLTS

4) CTR 23 VOLTS MINIMUM

c. GEN TIES NORM



d. Bus Sense TEST

�observee] � [L GEN TIE OPEN] ILLUMINATED

�observee] � [R GEN TIE OPEN] ILLUMINATED

�observee] � [BAT TIE OPEN] ILLUMINATED

e. Voltmeter - CTR 0 VOLTS

f. Bus Sense RESET



�observee] � [BAT TIE OPEN] EXTINGUISHED

g. Voltmeter - CTR 27.5 TO 29.0 VOLTS

h. Generator Load CHECK

�observee] � Observe Parallel Loads - Within 10%

2. Avionics Master ON

3. Interior Master Switch AS REQUIRED

4. Master Panel & Cockpit Lights AS REQUIRED

5. Mic Switches NORMAL

6. Cabin Lights AS REQUIRED

7. Cabin Sign NO SMK/FSB

8. ESIS Display CHECK

�observee] � INITIALIZATION COMPLETE

12-15MilViz KA350i

Before Taxi [continued]

9. Exterior Lights AS REQUIRED

10. Overspeed Warning TEST

11. Environmental System Controls SET

a. Automatic Climate Control AS REQUIRED

1) ECS Mode AUTO

2) Cockpit/Cabin Temp AS REQUIRED

3) Cockpit/Cabin Blower AUTO

4) Environmental Bleed Air AUTO

5) Bleed Air Valves OPEN

b. Manual Control Cooling AS REQUIRED

1) ECS Mode MAN COOL


3) Cockpit/Cabin Blower AS REQUIRED

4) Environmental Bleed Air AS REQUIRED


c. Manual Control Heating AS REQUIRED

1) ECS Mode MAN HEAT



4) Environmental Bleed Air AS REQUIRED


6) Man Temp Incr/Decr AS REQUIRED

d. Recirculation Blowers AS REQUIRED

1) ECS Mode OFF


e. Electric Heat Control AS REQUIRED

1) ECS Mode ELEC HEAT

�observee] � [ELEC HEAT ON] ILLUMINATED

12. Brake Deice AS REQUIRED

13. Prop Sync ON

14. TCAS II TEST

a. MFD - PRESS TFC KEY FOR > 1 SEC TO SELECT TCAS ONLY MAP

12-16MilViz KA350i


b. RTU - PRESS LSK R3 THREE TIMES TO ACTIVATE TEST

�observee] � TCAS II test pattern will display on MFD

�observee] � TCAS TEST message will be displayed on PFDs and MFD

�observee] � The red TRAFFIC message will be displayed on PFDs

�observee] � TCAS II vertical speed test pattern will be displayed on IVSIs

15. EMER FREQ EXTINGUISHED

16. TAWS+ PREFLIGHT

a. Verify avionics on and the following is functioning:

» Radio Altimeter

» ADC 1 and 2

» AHRS 1 and 2

» GPS 1

» Gear and Flap Indicating System

» Display System (PFD and MFD)

» FMS

b. Ensure all TAWS+ inhibit switches (G/S INHIB, TERR INHIB, and FLAP OVRD) are deselected

c. Verify no TAWS+ inoperative mode messages (amber GPWS or TERR)are displayed on the PFD

d. Select present position map and TERR for display on the MFD. Verify no TERRAIN FAIL message is present

e. Conduct a self test of the system by depressing the G/S INHIB an-nunciator switch and releasing. The following annunciations and alerts should be issued:

» Amber GPWS and TERR annunciators on the PFD and TERRAIN FAIL on the MFD

» A momentary illumination of the G/S INHIB and FLAP OVRD annun-ciator switches (ACTIVE)

» Amber GND PROX message on the PFD

» A red PULL UP message on the PFD

» Test pattern on the MFD terrain display

» Terrain display test pattern removed and all TAWS+ messages and annunciator switches extinguished

17. Flight and Engine Instruments CHECK

a. Altimeters SET

b. ESIS Altimeter SET

18. Flaps UP

12-17MilViz KA350i


19. Flight Controls CHECK

» FULL FREEDOM OF MOVEMENT

» PROPER DIRECTION OF TRAVEL

20. Brakes RELEASE, CHECK

(Before Taxi checklist complete)

12-18MilViz KA350i

Before Takeoff - Runup

1. Avionics & Radar CHECK

2. Pressurization CHECK, SET

a. Environmental Bleed Air NORMAL

b. Bleed Air Valves OPEN

c. Pressurization Controller SET

1) Adjust cabin altitude knob to indicate 1,000 ft below pressure altitude

2) Set rate knob to 12-o’clock position.

d. Cabin Pressure Switch HOLD AT TEST POSITION

e. Cabin Altimeter and VSI CHECK FOR DESCENT INDICATION

f. Cabin Pressure Switch RELEASE

g. Pressurization Controller SET

�observee] � Inner scale (ACFT ALT) should indicate planned cruise altitude + 1,000 ft

3. Autopilot CHECK

a. Pitch Trim TAKEOFF POSITION

b. Elevator FORWARD POSITION

c. Autopilot ENGAGE

�observee] � [AP] ILLUMINATED (PFD)

d. Electric Pitch Trim OPERATE BOTH DIRECTIONS

�observee] � Autopilot disengages with each operation; YD remains engaged

e. Elevator CENTERED

f. Autopilot ENGAGE

1) Apply rearward pressure on the elevator; observe pitch trim travel nose-down

2) Apply forward pressure on the elevator; observe pitch trim travel nose-up

g. AP/Trim Disconnect DEPRESS TO 1ST LEVEL

�observee] � MOMENTARY RED [AP] ILLUMINATED (PFD), THEN EXTINGUISHED

�observee] � AMBER [YD] ILLUMINATED (PFD), THEN EXTINGUISHED

h. Repeat items a through g for copilot’s side

4. Yaw Damper CHECK

a. Yaw Damper ON

�observee] � Green [YD] ILLUMINATED (PFD)

12-19MilViz KA350i

Before Takeoff - Runup [continued]

» AP/Trim Disconnect DEPRESS TO 1ST LEVEL

�observee] � Yellow [YD] FLASHES

5. Electric Pitch Trim CHECK

a. Pilot’s and Copilot’s Trim Switches CHECK

b. AP/Trim Disconnect DEPRESS TO 2ND LEVEL

�observee] � Red [TRIM] ILLUMINATED (PFD)

c. AP/Trim Disconnect RELEASE

�observee] � Red [TRIM] EXTINGUISHED

6. Trim Tabs SET

7. Engine Controls Friction Locks SET

8. Flaps CHECK, SET

9. Overspeed Governors & Rudder Boost CHECK

a. Rudder Boost Switch OFF

�observee] � [RUD BOOST OFF] ILLUMINATED

b. Rudder Boost Switch RUDDER BOOST

�observee] � [RUD BOOST OFF] EXTINGUISHED

c. Prop Levers FULL FORWARD

d. Prop Governor Test Switch HOLD TO GOV

e. Power Levers (individually)

» INCREASE UNTIL PROP IS STABILIZED AT 1500 TO 1610 RPM

f. AP/Trim Disconnect DEPRESS TO 1ST LEVEL

�observee] � [RUD BOOST OFF] ILLUMINATED

g. AP/Trim Disconnect RELEASE

�observee] � [RUD BOOST OFF] EXTINGUISHED

h. Power Lever IDLE

i. Repeat steps e through h on the opposite engine

j. Prop Governor Test Switch RELEASE

10. Low Pitch Stops & Primary Governors CHECK

a. Prop Levers FULL FORWARD

b. Low Pitch Stop Switch HOLD TO GND IDLE STOP

12-20MilViz KA350i




c. Power Levers SET 1500 RPM

d. Prop Levers CYCLE TO LOW AND HIGH RPM

e. Low Pitch Stop Switch RELEASE

�observee] � [L PROP PITCH] EXTINGUISHED

�observee] � [R PROP PITCH] EXTINGUISHED

f. Prop RPM STABILIZED AT 1150 TO 1250 RPM

11. Autofeather CHECK

a. Autofeather Switch HOLD TO TEST

b. Power Levers APPROX. 22% TORQUE

�observee] � [L AFX] ILLUMINATED

�observee] � [R AFX] ILLUMINATED

c. Power Levers RETARD INDIVIDUALLY

» At approximately 17% torque: OPPOSITE ANNUNCIATOR - EXTINGUISHED

» At approximately 10% torque: BOTH ANNUNCIATORS - EXTINGUISHED

d. Power Levers IDLE

�observee] � [L AFX] EXTINGUISHED

�observee] � [R AFX] EXTINGUISHED

e. Autofeather Switch RELEASE

12. Autofeather ARM

�observee] � [AUTOFTHER OFF] EXTINGUISHED

13. Manual Propeller Feathering CHECK

14. Vacuum & Deice Pressure CHECK

a. Left Bleed Air Switch PNEU & ENVIR OFF

�observee] � Pneumatic pressure and vacuum gages

NORMAL PRESSURE

�observee] � [L BLEED FAIL] EXTINGUISHED

�observee] � [R BLEED FAIL] EXTINGUISHED

b. Right Bleed Air Switch PNEU & ENVIR OFF


ZERO PRESSURE

12-21MilViz KA350i


�observee] � [L BLEED FAIL] ILLUMINATED

�observee] � [R BLEED FAIL] ILLUMINATED

c. Left Bleed Air Switch OPEN OR ENVIR OFF


NORMAL PRESSURE

�observee] � [L BLEED FAIL] EXTINGUISHED

�observee] � [R BLEED FAIL] EXTINGUISHED

d. Right Bleed Air Switch OPEN OR ENVIR OFF

15. Engine Anti-ice CHECK

a. Engine Anti-ice Actuators STANDBY

b. Engine Anti-ice OFF

�observee] � [L ENG ANTI-ICE] EXTINGUISHED

�observee] � [R ENG ANTI-ICE] EXTINGUISHED

c. Engine Anti-ice Actuators MAIN

d. Engine Anti-ice ON

�observee] � [L ENG ANTI-ICE] ILLUMINATED

�observee] � [R ENG ANTI-ICE] ILLUMINATED

16. Ice Protection Equipment (If Required) CHECK

a. Engine Auto-Ignition CHECK

1) Power Levers IDLE

2) Engine Auto-Ignition Switches ARM



3) Power Levers ADVANCE TO ABOVE 17% TORQUE

�observee] � [L IGNITION ON] EXTINGUISHED

�observee] � [R IGNITION ON] EXTINGUISHED

4) Power Levers IDLE



5) Engine Auto-Ignition Switches OFF

�observee] � [L IGNITION ON] EXTINGUISHED

12-22MilViz KA350i


�observee] � [R IGNITION ON] EXTINGUISHED

b. Windshield Anti-ice CHECK

1) Windshield Anti-ice HI

�observee] � Increase on left & right loadmeters

2) Windshield Anti-ice OFF, THEN NORMAL

�observee] � Increase on left & right loadmeters

3) Windshield Anti-ice OFF

c. Electrothermal Propeller Deice CHECK

1) Automatic Prop Deice ON

�observee] � Deice Ammeter 26 TO 32 AMPS

2) Manual Prop Deice HOLD IN MANUAL

�observee] � Deice Ammeter 0 AMPS

3) Manual Prop Deice RELEASE

�observee] � Deice Ammeter 26 TO 32 AMPS

4) Automatic Prop Deice OFF

d. Surface Deice CHECK

1) Condition Levers HIGH IDLE

2) Pneumatic Pressure CHECK

3) Surface Deice Switch SINGLE, RELEASE

�observee] � Pneumatic Pressure MOMENTARY DECREASE

�observee] � [WING DEICE] ILLUMINATED,THEN EXTINGUISHED

�observee] � [TAIL DEICE] ILLUMINATED,THEN EXTINGUISHED

4) Condition Levers LOW IDLE


18. Flight & Engine Instruments CHECK

19. Static Take-Off Power CONFIRM

20. V1, VR, V2 SET

(Before Takeoff - Runup checklist complete)

12-23MilViz KA350i

Before Takeoff - Final Items

1. Engine Auto-Ignition ARM (IF REqUIRED)

�observee] � [L IGNITION ON] ILLUMINATED (IF ARMED)

�observee] � [R IGNITION ON] ILLUMINATED (IF ARMED)

2. Engine Anti-ice AS REQUIRED

�observee] � [L ENG ANTI-ICE] ILLUMINATED (IF ON)

�observee] � [R ENG ANTI-ICE] ILLUMINATED (IF ON)

3. Exterior Lights AS REQUIRED

4. Ice Protection AS REQUIRED

a. Windshield Anti-ice NORMAL/HI (IF REqUIRED)

b. Prop Deice AUTO (IF REqUIRED)

c. Left & Right Fuel Vent Heat ON

d. Stall Warning Heat ON

e. Left & Right Pitot Heat ON

�observee] � [L PITOT HEAT] EXTINGUISHED

�observee] � [R PITOT HEAT] EXTINGUISHED

5. Transponder SELECT 1 OR 2


7. Trim CONFIRM SET

8. Flaps CONFIRM SET

9. Environmental Bleed Air SET

a. OAT above 10°C AUTO OR LOW

b. OAT at or below 10°C AUTO OR NORMAL

10. Bleed Air Valves AS REQUIRED

11. ECS Mode AS REQUIRED

12. Cockpit/Cabin Blower AS REQUIRED

13. Cockpit/Cabin Temp AS REQUIRED

14. Interior Lights AS REQUIRED

15. Generator Load CHECK

16. Battery Ammeter CHECK

17. Annunciators OFF / CONSIDERED

(Before Takeoff - Final Items checklist complete)

12-24MilViz KA350i

Takeoff

nORMAL TAKEOFF

1. Brakes HOLD

2. Power Levers SET STATIC TAKE-OFF POWER



3. Brakes RELEASE

�waite]� Upon reaching VR:

4. ROTATE TO APPROXIMATELY 10°

�waite]� When positive climb established:

5. Landing Gear UP

6. AirspeedMAINTAIN V35 UNTIL

CLEAR OF OBSTACLES

�waite]� At 125 knots, minimum:

7. Flaps UP

(Normal Takeoff checklist complete)

ROLLInG TAKEOFF

1. Brakes RELEASE

2. Power Levers SET STATIC TAKE-OFF POWER



�waite]� Upon reaching VR:

3. ROTATE TO APPROXIMATELY 10°

�waite]� When positive climb established:

4. Landing Gear UP

5. AirspeedMAINTAIN V35 UNTIL

CLEAR OF OBSTACLES


6. Flaps UP

(Rolling Takeoff checklist complete)

12-25MilViz KA350i

Climb & Cruise

CLIMB

1. Bleed Air Valves OPEN

2. Environmental Bleed Air AS REQUIRED

3. Yaw Damper ON

4. Climb Power SET

5. Props 1600 RPM, OR AS DESIRED

6. Windshield Anti-Ice NORMAL

7. Engine Instruments MONITOR

8. Cabin Sign AS REQUIRED

9. Pressurization CHECK

10. Lights AS REQUIRED

(Climb checklist complete)

CRUISE

1. Cruise Power SET AS DESIRED

2. Autofeather OFF

3. ECS Mode AS REQUIRED

4. Engine Instruments MONITOR

5. Fuel Gauges MONITOR

6. Cabin Pressurization

If revised flight plan calls for an altitude change of 1000 feet or more, select the new cruise altitude plus 1000 feet on the ACFT ALT dial of the cabin pressurization controller.

(Cruise checklist complete)

12-26MilViz KA350i

Descent & Before Landing

DESCEnT

1. Pressurization SET

a. Cabin Altitude SET

b. Rate Control AS DESIRED

2. Altimeter SET

3. Cabin Sign AS REQUIRED

4. Windshield Anti-ice AS REQUIRED

5. Brake Deice AS REQUIRED

�observee] � [L BK DEICE ON] ILLUMINATED, IF ON

�observee] � [R BK DEICE ON] ILLUMINATED, IF ON

6. Window Defog AS REQUIRED

7. Fuel Balance CHECK

8. Cabin Equipment POSITIONED

(Descent checklist complete)

BEFORE LAnDInG

1. Approach Speeds CONFIRM

2. Autofeather ARM

3. Environmental Bleed Air LOW

4. Cabin Lights AS REQUIRED

5. Cabin Sign NO SMK/FSB

6. Flaps APPROACH

7. Landing Gear DOWN

8. Exterior and Interior Lights AS REQUIRED

9. Radar AS REQUIRED

10. Surface Deice AS REQUIRED

(Before Landing checklist complete)

12-27MilViz KA350i

Landing & After Landing

nORMAL LAnDInG

1. Flaps DOWN

2. Airspeed VREF

3. Yaw Damper OFF

4. Power Levers IDLE


�waite]� After Touchdown:

6. Power Levers SELECT GROUND FINE

7. Brakes AS REQUIRED

(Normal Landing checklist complete)

MAxIMUM REVERSE THRUST LAnDInG

1. Flaps DOWN

2. Airspeed VREF

3. Yaw Damper OFF

4. Condition Levers HIGH IDLE

5. Power Levers IDLE


�waite]� After Touchdown:

7. Power Levers REVERSE

8. Brakes AS REQUIRED

9. Condition Levers LOW IDLE

(Maximum Reverse Thrust Landing checklist complete)

12-28MilViz KA350i

Landing & After Landing [continued]

BALKED LAnDInG

1. Power MAXIMUM ALLOWABLE

2. Airspeed MAINTAIN VREF

�waite]� Clear of obstacles:

3. Establish normal climb

�waite]� VREF + 10 knots:

4. Flaps APPROACH

5. Landing Gear UP


6. Flaps UP

(Balked Landing checklist complete)

AFTER LAnDInG

1. Engine Auto-Ignition OFF

2. Engine Anti-ice ON

3. Exterior and Interior Lights AS REQUIRED

4. Ice Protection OFF

5. Transponder STANDBY

6. Radar STANDBY OR OFF

7. Trim SET

8. Flaps UP

9. Pressurization Differential VERIFY 0

10. Bleed Air Valves OPEN OR ENVIR OFF

(After Landing checklist complete)

12-29MilViz KA350i

SHUTDOWN & SECURING

1. Parking Brake SET

2. Avionics Master OFF

3. ESIS Power OFF

4. Autofeather OFF

5. Exterior Lights OFF

6. ECS Mode OFF

7. Cockpit/Cabin Blower AUTO

8. Oxygen Controls OFF

9. Battery CHARGED

10. Interior Master Switch OFF

11. ITT STABILIZED

12. Instrument Emergency Lights ON, IF DESIRED

13. Condition Levers FUEL CUTOFF

14. Prop Levers FEATHER

15. Overhead Panel Switches OFF

16. Cabin Entry Lights AS REQUIRED

�waite]� Below 15% N1:

17. Battery & Generator Switches OFF

18. Control Locks INSTALL

19. Instrument Emergency Lights OFF

20. Tie-downs & Chocks INSTALL

21. External Covers INSTALL

22. Parking Brake OFF

23. Baggage Compartment Lights OFF

24. Cabin Entry Lights OFF

(Shutdown & Securing checklist complete)

MV Team Collin Biedenkapp Tomas Aguiló Jon Bleeker Henry Chen Sandra Yoo Ricardo Ramos Bill Leaming Brandon Filer Chuck Jodry MacFarland Masterson Oisin Little Jim Stewart Colin Pearson

Special Code Bits FSSI Engineering Modeling & Textures Dmi Usatyi - 3DReach

Sound Environment Mike Maarse - SimAcoustics

RealLight & TrueGlass TFDi Design

Product Testers Steve McNitt John M Marlon Carter Zach Alcantar Mike Cameron Ryan Butterworth Tom Stovall Sergio S Jaroslaw Kowalczyk Greg Morin Daniel Faas Asid [D.O.W.] Jerome Zimmermann John White

Project Consultant Ken (King Air 200/300 Instructor)

Cre

dit

s

Documents

KA3 5 0 - MILVIZ · 2019-12-21 · MilViz KA350i 2-1 Product Features > Designed primarily for procedural flight training, the MilViz KA350i repre- sents the most advanced overall