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
nOMEnCLATURE COLOR CAUSE FOR ILLUMInATIOn
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
nOMEnCLATURE COLOR CAUSE FOR ILLUMInATIOn
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
nOMEnCLATURE COLOR CAUSE FOR ILLUMInATIOn
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
nOMEnCLATURE COLOR CAUSE FOR ILLUMInATIOn
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
v1 (KiAS)vr (KiAS)v2 (KiAS)toFl (Ft)
103106114
2682
102106114
3057
102106114
3255
102107114
3459
102107114
3654
102107114
3955
104107114
4504
106108114
5129
107108114
5607
13,000 LBS
v1 (KiAS)vr (KiAS)v2 (KiAS)toFl (Ft)
101104112
2373
99104111
2692
99104111
2857
99104111
3026
99104111
3203
99104111
3458
100104111
3910
102105110
4430
103105110
4843
12,000 LBS
v1 (KiAS)vr (KiAS)v2 (KiAS)toFl (Ft)
99104112
2199
98104112
2489
98104112
2646
98104111
2799
97104111
2960
97104111
3193
99104110
3602
100104110
4037
101104110
4361
11,000 LBS
v1 (KiAS)vr (KiAS)v2 (KiAS)toFl (Ft)
98104112
2028
97104112
2290
97104112
2431
96104112
2577
96104112
2722
96104111
2931
97104111
3301
99104110
3733
99104110
4021
10,500 LBS AnD UnDER
v1 (KiAS)vr (KiAS)v2 (KiAS)toFl (Ft)
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
OUTSIDE AIR TEMPERATURE °C
-35 -15 -5 5 15 25 35 45 52
15,000 LBS
v1 (KiAS)vr (KiAS)v2 (KiAS)toFl (Ft)
106110117
3458
106110117
3931
106110117
4191
106110117
4443
106110117
4713
107111117
5324
109111117
6109
111112117
7017
--------
14,000 lbS
v1 (KiAS)vr (KiAS)v2 (KiAS)toFl (Ft)
103106114
3014
102107114
3443
102107114
3654
102107114
3878
102107114
4108
103107114
4637
105108114
5295
107108114
6068
--------
13,000 LBS
v1 (KiAS)vr (KiAS)v2 (KiAS)toFl (Ft)
100104111
2655
99104111
3014
99104111
3204
98104111
3397
98104111
3586
99104111
4028
101105110
4585
103105110
5233
--------
12,000 LBS
v1 (KiAS)vr (KiAS)v2 (KiAS)toFl (Ft)
98104112
2455
98104111
2788
97104111
2960
97104111
3139
97104111
3313
98104110
3709
99104110
4169
100104109
4693
--------
11,000 LBS
v1 (KiAS)vr (KiAS)v2 (KiAS)toFl (Ft)
97104112
2259
96104112
2566
96104112
2722
96104111
2883
95104111
3044
96104111
3400
98104110
3855
99104110
4348
--------
10,500 LBS AnD UnDER
v1 (KiAS)vr (KiAS)v2 (KiAS)toFl (Ft)
97104112
2163
96104112
2455
95104112
2606
95104112
2759
95104111
2910
96104111
3250
97104110
3679
98104110
4161
--------
Takeoff Speeds & Field Length Reference (2000 ft)
> Flaps in UP position > A/C and Bleed Air ON
11-3MilViz 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)
106110117
3879
106110117
4429
106110117
4719
106110117
5016
107111117
5531
108111117
6300
110112117
7219
--------
--------
14,000 lbS
v1 (KiAS)vr (KiAS)v2 (KiAS)toFl (Ft)
102107114
3399
102107114
3866
102107114
4114
102107114
4370
103107114
4819
104108114
5454
106108114
6244
--------
--------
13,000 LBS
v1 (KiAS)vr (KiAS)v2 (KiAS)toFl (Ft)
99104111
2977
98104111
3387
98104111
3600
98104111
3821
99104111
4191
100105110
4728
102105110
5388
--------
--------
12,000 LBS
v1 (KiAS)vr (KiAS)v2 (KiAS)toFl (Ft)
98104111
2755
97104111
3130
97104111
3325
97104111
3526
97104110
3860
98104110
4316
100104110
4853
--------
--------
11,000 LBS
v1 (KiAS)vr (KiAS)v2 (KiAS)toFl (Ft)
96104112
2535
96104111
2875
95104111
3056
95104111
3239
96104111
3538
97104110
3978
98104110
4477
--------
--------
10,500 LBS AnD UnDER
v1 (KiAS)vr (KiAS)v2 (KiAS)toFl (Ft)
96104112
2424
95104112
2751
95104111
2922
94104111
3099
95104111
3381
96104110
3797
98104110
4297
--------
--------
Takeoff Speeds & Field Length Reference (4000 ft)
> Flaps in UP position > A/C and Bleed Air ON
11-4MilViz 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)
106110117
4378
106110117
5007
106110117
5332
106111117
5795
108111117
6535
110112117
7448
111112117
8599
--------
--------
14,000 lbS
v1 (KiAS)vr (KiAS)v2 (KiAS)toFl (Ft)
102107114
3823
102107114
4363
102107114
4664
102107114
5050
104108114
5674
105108114
6448
107109114
7419
--------
--------
13,000 LBS
v1 (KiAS)vr (KiAS)v2 (KiAS)toFl (Ft)
98104111
3351
98104111
3815
98104110
4053
98104111
4397
100104110
4921
101105110
5572
103106110
6381
--------
--------
12,000 LBS
v1 (KiAS)vr (KiAS)v2 (KiAS)toFl (Ft)
97104111
3095
97104111
3521
97104111
3749
97104110
4049
98104110
4499
99104110
5029
100104109
5667
--------
--------
11,000 LBS
v1 (KiAS)vr (KiAS)v2 (KiAS)toFl (Ft)
96104111
2844
95104111
3235
95104111
3440
95104111
3713
96104110
4144
98104110
4642
99104109
5235
--------
--------
10,500 LBS AnD UnDER
v1 (KiAS)vr (KiAS)v2 (KiAS)toFl (Ft)
95104112
2722
94104111
3094
94104111
3290
94104111
3548
96104110
3955
97104110
4449
98104109
5023
--------
--------
Takeoff Speeds & Field Length Reference (6000 ft)
> Flaps in UP position > A/C and Bleed Air ON
11-5MilViz 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)
105110117
4956
106111117
5689
106111117
6127
107111117
6850
109112117
7761
111112117
8926
--------
--------
--------
14,000 lbS
v1 (KiAS)vr (KiAS)v2 (KiAS)toFl (Ft)
102107114
4317
102107114
4955
102107114
5341
103108114
5956
105108114
6723
107109114
7673
109109114
8913
--------
--------
13,000 LBS
v1 (KiAS)vr (KiAS)v2 (KiAS)toFl (Ft)
98104111
3778
98104110
4314
98104110
4641
99105110
5166
101105110
5811
102106110
6616
104106110
7634
--------
--------
12,000 LBS
v1 (KiAS)vr (KiAS)v2 (KiAS)toFl (Ft)
97104111
3487
97104111
3987
97104110
4286
97104110
4721
98104110
5250
100104109
5893
101104108
6683
--------
--------
11,000 LBS
v1 (KiAS)vr (KiAS)v2 (KiAS)toFl (Ft)
95104111
3204
95104111
3658
95104111
3926
96104110
4350
97104110
4842
98104109
5442
100104109
6167
--------
--------
10,500 LBS AnD UnDER
v1 (KiAS)vr (KiAS)v2 (KiAS)toFl (Ft)
94104111
3065
94104111
3497
94104111
3751
95104110
4153
96104110
4652
98104110
5231
99104109
5916
--------
--------
Takeoff Speeds & Field Length Reference (8000 ft)
> Flaps in UP position > A/C and Bleed Air ON
11-6MilViz 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)
106111117
5693
106111117
6599
107111117
7329
109112117
8242
110112117
9437
--------
--------
--------
--------
14,000 lbS
v1 (KiAS)vr (KiAS)v2 (KiAS)toFl (Ft)
102107114
4962
102108114
5756
103108114
6360
104108114
7134
106109114
8117
108109114
9379
--------
--------
--------
13,000 LBS
v1 (KiAS)vr (KiAS)v2 (KiAS)toFl (Ft)
98104110
4320
98104110
5007
99105110
5523
100105110
6168
102106110
6996
104106110
8030
--------
--------
--------
12,000 LBS
v1 (KiAS)vr (KiAS)v2 (KiAS)toFl (Ft)
96104111
3993
97104110
4613
97104110
5041
98104110
5575
99104109
6224
101104109
7032
--------
--------
--------
11,000 LBS
v1 (KiAS)vr (KiAS)v2 (KiAS)toFl (Ft)
95104111
3664
95104111
4226
96104110
4646
97104110
5140
98104109
5751
99104109
6487
--------
--------
--------
10,500 LBS AnD UnDER
v1 (KiAS)vr (KiAS)v2 (KiAS)toFl (Ft)
94104111
3502
94104111
4036
95104110
4436
96104110
4936
97104110
5521
99104109
6234
--------
--------
--------
Takeoff Speeds & Field Length Reference (10,000 ft)
> Flaps in UP position > A/C and Bleed Air ON
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
Preflight Inspection [continued]
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
10. Wheel Chocks REMOVE
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
Preflight Inspection [continued]
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
30. Wheel Chocks REMOVE
31. Flush Fuel Vent & Heated Fuel Vent CLEAR
12-6MilViz KA350i
Preflight Inspection [continued]
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
Preflight Inspection [continued]
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
22. Fuel Quantity CHECK
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)
1. GEN TIES MAN CLOSE
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
�waite]� After N1 reaches 12% (minimum):
12. Left Condition Lever LOW IDLE
13. Left ITT & N1 MONITOR
14. Left Oil Pressure CHECK
�waite]� After N1 reaches 50%:
15. Left Ignition & Engine Start OFF
16. Right Condition Lever LOW IDLE
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
�observee] � [L GEN TIE OPEN] EXTINGUISHED
�observee] � [R GEN TIE OPEN] EXTINGUISHED
21. Right Generator ON
(Engine Starting (Battery) checklist complete)
12-12MilViz KA350i
Engine Starting (External Power)
1. Battery VERIFY ON
2. GEN TIES MAN CLOSE
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 IGNITION ON] ILLUMINATED
�observee] � [R FUEL PRES LO] EXTINGUISHED
�waite]� After N1 reaches 12% (minimum):
16. Right Condition Lever LOW IDLE
17. Right ITT & N1 MONITOR
18. Right Oil Pressure CHECK
�waite]� After N1 reaches 50%:
19. Right Ignition & Engine Start OFF
20. Left Ignition & Engine Start ON
�observee] � [L IGNITION ON] ILLUMINATED
�observee] � [L FUEL PRES LO] EXTINGUISHED
�waite]� After N1 reaches 12% (minimum):
21. Left Condition Lever LOW IDLE
22. Left ITT & N1 MONITOR
12-13MilViz KA350i
Engine Starting (External Power) [continued]
23. Left Oil Pressure CHECK
�waite]� After N1 reaches 50%:
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
�observee] � [L GEN TIE OPEN] EXTINGUISHED
�observee] � [R GEN TIE OPEN] 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
�observee] � [L GEN TIE OPEN] EXTINGUISHED
�observee] � [R GEN TIE OPEN] EXTINGUISHED
31. Prop Levers FULL FORWARD
32. Left & Right Prop RPM 1050 MINIMUM
�observee] � [L PROP PITCH] ILLUMINATED
�observee] � [R PROP PITCH] ILLUMINATED
(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
�observee] � [L GEN TIE OPEN] EXTINGUISHED
�observee] � [R GEN TIE OPEN] EXTINGUISHED
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] � [L GEN TIE OPEN] EXTINGUISHED
�observee] � [R GEN TIE OPEN] EXTINGUISHED
�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
2) Cockpit/Cabin Temp AS REQUIRED
3) Cockpit/Cabin Blower AS REQUIRED
4) Environmental Bleed Air AS REQUIRED
5) Bleed Air Valves OPEN
c. Manual Control Heating AS REQUIRED
1) ECS Mode MAN HEAT
2) Cockpit/Cabin Blower AS REQUIRED
3) Cockpit/Cabin Temp AS REQUIRED
4) Environmental Bleed Air AS REQUIRED
5) Bleed Air Valves OPEN
6) Man Temp Incr/Decr AS REQUIRED
d. Recirculation Blowers AS REQUIRED
1) ECS Mode OFF
2) Cockpit/Cabin Blower AS REQUIRED
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
Before Taxi [continued]
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
Before Taxi [continued]
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
Before Takeoff - Runup [continued]
�observee] � [L PROP PITCH] ILLUMINATED
�observee] � [R PROP PITCH] ILLUMINATED
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
�observee] � Pneumatic pressure and vacuum gages
ZERO PRESSURE
12-21MilViz KA350i
Before Takeoff - Runup [continued]
�observee] � [L BLEED FAIL] ILLUMINATED
�observee] � [R BLEED FAIL] ILLUMINATED
c. Left Bleed Air Switch OPEN OR ENVIR OFF
�observee] � Pneumatic pressure and vacuum gages
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
�observee] � [L IGNITION ON] ILLUMINATED
�observee] � [R IGNITION ON] ILLUMINATED
3) Power Levers ADVANCE TO ABOVE 17% TORQUE
�observee] � [L IGNITION ON] EXTINGUISHED
�observee] � [R IGNITION ON] EXTINGUISHED
4) Power Levers IDLE
�observee] � [L IGNITION ON] ILLUMINATED
�observee] � [R IGNITION ON] ILLUMINATED
5) Engine Auto-Ignition Switches OFF
�observee] � [L IGNITION ON] EXTINGUISHED
12-22MilViz KA350i
Before Takeoff - Runup [continued]
�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
17. Fuel Quantity CHECK
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
6. Prop Levers FULL FORWARD
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
�observee] � [L AFX] ILLUMINATED
�observee] � [R AFX] ILLUMINATED
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
�observee] � [L AFX] ILLUMINATED
�observee] � [R AFX] ILLUMINATED
�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
�waite]� At 125 knots, minimum:
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
5. Prop Levers FULL FORWARD
�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
6. Prop Levers FULL FORWARD
�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
�waite]� At 125 knots, minimum:
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)
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