KA350 i
user 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 except 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 info@milviz.com.
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.
MilViz KA350i
i
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
MilViz KA350i
1-1
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 acquainted with the MilViz KA350i. Divided into
sections, you’ll find information related to installation, configuring the aircraft within the simulator, 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 flying, taking hold and hand flying it will also bring a
wide grin to your face.
Regardless of how you approach it, it’s a wonderful aircraft to learn. We sincerely hope you enjoy every minute of your many exciting flights to
come!
MilViz KA350i
1-2
MilViz KA350i
Product Features
>> Designed primarily for procedural flight training, the MilViz KA350i represents 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
2-1
MilViz KA350i
3-1
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.
Lockheed Martin Prepar3D, version 4.5 (Hotfix 1 required)
Supported Platforms:
(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.
Joystick, yoke, or other gaming controller (a means of controlling the aircraft rudder, either with twist
joystick function or dedicated pedals, is additionally recommended).
Gaming Controller:
(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.
MilViz KA350i
4-1
Product Installation
Pre-Installation Tasks
KA350i Setup Wizard
As with other flight simulator add-ons, pre-installation precautions should involve closing any open
applications, as well as temporarily disabling any
active antivirus software.
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 legitimately purchased copies of the KA350i are in use.
Failure to temporarily disable antivirus software
when installing may result in a non-functioning
product and/or simulator!!!
Beginning Installation
The setup wizard will then determine the correct location for installation. If incorrect, this can
changed. Please note that the MilViz KA350i only
supports Prepar3D version 4.
After purchase, this product may be supplied as
a compressed (.zip) file. This compressed file contains an executable (.exe) file, which is the installer
for the MilViz KA350i.
Clicking ‘Install’ at the Ready to Install screen will
proceed with the installation of the KA350i.
Using the Windows File Explorer or file compression utility of your choice, unzip this file to a location of your choosing.
Once the aircraft files are finished being installed,
the installer will automatically run the MilViz Addon Management System (MVAMS) Setup Wizard.
Once unzipped, you may begin installation by right
clicking on the executable (.exe) file, then selecting “Run as administrator”. The installer will run,
showing an initial welcome screen. Left click on
the “Next” button to continue.
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.
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 ensure that these components are installed and correctly configured for use.
MVAMS Setup Wizard
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 liveries 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 notification 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 available, 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 forums for our individual products are restricted to
owners of that product. To register, please contact oisin@milviz.com for details. Please note that
proof of purchase will be required.
MilViz KA350i
5-1
Simulator Configuration
Options - Realism
MilViz aircraft are developed with an overall goal of
replicating a realistic level of accuracy in regards to
operation and flight response. To this end, development 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 necessary 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 Model
For correct operation, all sliders in the flight model
section should be set fully to the right.
Instruments and Lights
The MilViz KA350i has a sophisticated lighting system 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 Damage
The choices in this section may left to user preference.
Engines
All three checkboxes in this section must remain
unchecked for correct operation.
Special Effects
This may be left to user preference.
Flight Controls
For the most realistic flight experience, “Autorudder” should not be selected.
Attachments
correct tip will display to the user that the fuel is
low.
Options - Information
To prevent this from showing, please deselect this
option, located in General/Information/Miscellaneous Text.
These should remain unchecked.
The only option of concern in this section is concerning ‘User Tips’. There exists an issue in Prepar3D where if the aircraft uses custom code to
handle fuel flow (as the KA350i does), then an in-
MilViz KA350i
6-1
MVAMS Overview
MVAMS stands for MilViz Addon Management System. It is a standalone application used by many
of our product releases which represents our user-friendly solution to the growing complexity of
options and choices available within our aircraft.
It provides a central location to manage your aircraft, as well as providing incremental update capabilities.
If not already present, the MilViz KA350i installs,
and fully integrates with, the MVAMS application.
This allows the user access to a range of configuration 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 otherwise 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 MVAMScompatible 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 available 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 aircraft 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 configuration options available, the options are organized
into a series of tabs to group similar or related options together. Tabs may be moved between without loss of selections or changes made.
MilViz KA350i
6-2
‘Load’ Tab
‘Show/Hide Items’ Tab
The KA350i has a configurable loadout for passengers, fuel, and cargo/baggage, 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.
This tab contains initial display settings for the wheel chocks, the engine covers, and the pitot covers. Selecting these allows for these items to be visible
when the aircraft is loaded.
‘Options’ Tab
Saving and Closing MVAMS
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.
To save any changes or selections made, click the ‘Save Defaults’ button located 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.)
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 engine, or external engine sounds.
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.
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.
MilViz KA350i
Engine State: Explained
As previously mentioned, the KA350i tracks and saves the health of the engine. 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 during normal operation. From perfect condition, a full bar depleting to an empty
bar represents approximately 100 hours of operation. After that point, the aircraft 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 instrumentation!
6-3
MilViz 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).
7-1
MilViz KA350i
8-1
KA350i Specifications & Limitations
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 Type
Constant-speed, Full-feathering, Reversing, Counterweighted, Hydraulically Actuated
Usable Fuel
Main Fuel System
2546 lbs (380 gal)
Auxiliary Fuel System
1065 lbs (159 gal)
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
Maximum Weights
Wing Loading
48.4 pounds per square foot
Power Loading
7.14 pounds per shaft horsepower
MilViz KA350i
Aircraft & Cabin Dimensions
Turning Radius
Airspeed Limitations
8-2
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
Inside Gear
4 feet
Nose Wheel
20 feet, 6 inches
Outside Gear
21 feet, 2 inches
Wing Tip
41 feet, 7 inches
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)
MilViz KA350i
Airspeed Limitations (continued)
8-3
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)
Flight Load Factor Limits
Steep Approach Limitations
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 approach 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
Flaps Up
3.1 G + to 1.24 G -
Flaps Down
2.0 G + to 0.0 G -
Maximum Approved Approach Angle
5.5°
One-Engine-Inoperative Steep Approaches
Not Approved
Flaps Up Steep Approaches
Not Approved
MilViz KA350i
8-4
Engine Operating Limits
Operating Condition
Torque
%
Maximum ITT
°C
GAS GENERATOR RPM
% N1
Prop RPM
N2
Oil Press
PSI
Oil temp
°C
0 - 200
-40
Starting
1000
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
1870
200
0 to 110
Transient
156
850
104
>> 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
MilViz KA350i
9-1
Systems & Controls Overview
General Overview
Annunciator System
The KA350i is a twin-engine, all-metal, low-wing monoplane, with fully cantilevered wings and a T-tail empennage.
The annunciator system consists of a warning annunciator panel located in
the center of the glareshield, and a caution/status annunciator panel located 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).
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 conventional 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 operating due to the control switch being in the OFF position or the trim disconnect
switch being pressed.
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 additional warning annunciator illuminates.
When a triggering fault requires pilot attention and possible future action, an
appropriate amber caution annunciator will illuminate and both amber MASTER CAUTION flashers will begin flashing. The flashers may be extinguished
by pressing the face of either flasher. They will then stop flashing until an additional 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 annunciators do not have a corresponding master flasher.
Flaps
The flaps are operated through the use of a sliding handle on the center pedestal 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.
MilViz KA350i
9-2
Landing Gear
Propulsion System
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.
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.
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 GEAR
DOWN 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 GEAR
CONTROL 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 parking brake handle, and may be released by pushing the parking brake handle in.
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 operating 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 HIGH
IDLE.
Propeller Ground Fine Operation
Propeller ground fine operation provides optimum deceleration wile the airplane is on the ground during landing by utilizing the maximum available propeller drag. Operation is achieved through a gate position for the power levers,
retarded past IDLE into the GROUND FINE gate.
Propeller Reversing
The 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.
MilViz KA350i
9-3
Engine Instrumentation
Electronic Flight Instrument System (EFIS)
Engine instruments are displayed in the upper area of the MFD. Along with incorporated 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
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.
Propeller Synchrophaser
The propeller synchrophaser system serves to match the RPM of both propellers 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.
The upper area of the PFD displays the Attitude Director Indicator (ADI), altitude 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.
Starting & Ignition System
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.
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 annunciator 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.
Basic display formats are controlled through the line select keys that are provided 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.
Auto Ignition
Display Control Panel (DCP)
The auto ignition system is used to prevent engine loss in the case of combustion failure. This ensures constant ignition during turbulence or flight in
icing or precipitation conditions.
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.
MilViz KA350i
Control Display Unit (CDU)
A color LCD-based Control Display Unit (CDU) is located on the center pedestal. 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 communications and navigation, including the Flight Management System (FMS).
Flight Management System (FMS)
The Flight Management System (FMS) serves to provide flight plan management, 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.
9-4
MilViz KA350i
10-1
Panel Overview - Front
1.
2.
3.
4.
5.
6.
7.
PFD
MFD
FLIGHT GUIDANCE PANEL
RADIO TUNING UNIT
COMM/RADIO SWITCH PANEL
CAUTION/STATUS ANNUNCIATOR PANEL
WARNING ANNUNCIATOR PANEL
8. MASTER CAUTION/WARNING LIGHTS
9. BACKUP ATTITUDE INDICATOR
10. PARKING BRAKE CONTROL
11. PILOT’S LEFT LOWER PANEL
12. PILOT’S RIGHT LOWER PANEL
13. CO-PILOT’S LEFT LOWER PANEL
14. CO-PILOT’S RIGHT LOWER PANEL
[7]
[ 21 ]
[8]
15. FLAP INDICATOR
16. CABIN VERTICAL SPEED INDICATOR
17. CABIN PRESSURE INDICATOR
18. CENTER SWITCH PANEL
19. DISPLAY CONTROL PANEL
20. TAWS INHIBIT LAMPS
21. FIRE / EMERGENCY LAMPS
[ 21 ]
[8]
[3]
[ 20 ]
[9]
[1]
[2]
[1]
[ 19 ]
[ 19 ]
[4]
[5]
[5]
[ 18 ]
[6]
[ 10 ]
[ 11 ]
[ 12 ]
[ 13 ]
[ 15 ] [ 16 ]
[ 17 ]
[ 14 ]
MilViz KA350i
10-2
Panel Overview - Pilot’s Left Lower Panel
AVIONICS
MASTER
POWER
EXT
PWR
ARM
EGN
AUTO
IGN
LEFT
BAT BUS
GEN
RESET
NORM
OFF
RIGHT
ENGINE ANTI-ICE
LEFT
RIGHT
ON
ON
EMER
OFF
BAT
L GEN
ESIS
ON
BUS SENSE
RESET
OFF
TEST
TEST
ENGINE AND
IGNITION START
LEFT
N
O
R
M
GEN TIES
MAN CLOSE
ACTUATORS
MAIN
OPEN
STANDBY
AUTOFEATHER
RIGHT
ARM
ON
OFF
STARTER ONLY
PARKING BRAKE
OFF
OFF
R GEN
PROP TEST
GOV
GND IDLE
STOP
OFF
TEST
OFF
MilViz KA350i
10-3
Panel Overview - Pilot’s Right Lower Panel
LANDING
LEFT
TAXI
RIGHT
NAV
RECOG
SURFACE
DEICE
SINGLE
AUTO
MANUAL
DOWN
FUEL VENT
DOWN
LOCK
REL
LEFT
STALL
WARN
PITOT
OFF
LEFT
STROBE
UP
ICE PROTECTION
PROP
O
F
F
MANUAL
L
I BEACON
G
H
T
S
L
I
G
H
T
S
OFF
WSHLD ANTI-ICE
NORMAL
O
F
F
HIGH
PILOT
CO-PILOT
BRAKE
DEICE
ICE
RIGHT
RIGHT
GEAR
DOWN
TAIL
FLOOD
NOSE
HD LT
TEST
L
R
OFF
LANDING
GEAR
HYD FLUID
SENSOR
RELAY
TEST
MilViz KA350i
10-4
Panel Overview - Co-pilot’s Left Lower Panel
OVERSPEED
WARN TEST
STALL
WARN TEST
O
F
F
OFF
LFG GEAR
WARN TEST
ENVIRONMENTAL
TEMP
BLOWER
MAN COOL
AUTO
MAN
HEAT
MAN TEMP
INCR
WINDOW
DEFOG
OFF
AUTO
INCR
INCR
MODE
COCKPIT
BLOWER
TEMP
A
U
T
O
ENVIR
BLEED AIR
NORMAL
INCR
INCR
CABIN
BLEED AIR VALVES
LEFT OPEN RIGHT
ALT
WARN
SILENCE
O
F
F
DECR
ENVIR
OFF
LOW
AUTO
ELEC
HEAT
CABIN
TEST
OFF
ENG
CABIN DIFF
WARN TEST
FIRE
DET
TEST
OFF
PNEU & ENVIR OFF
EXT
LEFT
RIGHT
OFF
MilViz KA350i
10-5
Panel Overview - Overhead Control Panel
PILOT
OVHD
FLOOD
OFF
WINDSHIELD WIPER
OFF
PARK
SLOW
ANNUN
PUSH BRT
FAST
DIM
BRT
MASTER
PANEL
LIGHTS
ON
OFF
BRT
BRT
PILOT
INSTR
PNL
OFF
PILOT
DISPLAYS
OVHD PED
& SUBPANEL
OFF
SIDE
PANEL
OFF
COPILOT
DISPLAYS
COPILOT
INSTR
PNL
OFF
BRT
BRT
BRT
BRT
BRT
BRT
CABIN
LIGHT
PAX
D
I
M
OFF
INTERIOR
NO SMK MASTER
FSB
ON
O
F
F
FSB
OFF
ENTRY
LIGHTS
ON
MAXIMUM
IAS KNOTS
DC
DC%LOAD
L GEN
BAT
DC%LOAD
VOLT
AMP
CTR
R GEN
TPL FED
EXT
PWR
BAT
VOLT METER
BUS SELECT
PROP AMPS
GR EXTENSION
GR RETRACT
GR EXTENDED
APPROACH FLAP
FULL ON FLAP
MANEUVERING
INSTRUMENT
EMERG LIGHTS
ON
184
166
184
202
158
184
OFF
MilViz KA350i
10-6
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
--
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
MilViz KA350i
10-7
Panel Overview - Caution / Advisory / Status Annunciator Panel
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
Nomenclature
Color
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
Cause For Illumination
MilViz KA350i
10-8
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
MilViz KA350i
10-9
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
MilViz KA350i
10-10
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
MilViz KA350i
11-1
Takeoff Speeds & Field Length Reference (Sea Level)
Outside air temperature °C
Takeoff Weight
Item
-35
-15
-5
5
15
25
35
45
52
15,000 lbs
v1 (KIAS)
VR (KIAS)
V2 (KIAS)
TOFL (FT)
106
109
117
3085
106
110
117
3505
106
110
117
3716
106
110
117
3949
106
110
117
4192
106
110
117
4541
108
111
117
5181
110
111
117
5919
111
112
117
6493
14,000 lbs
v1 (KIAS)
VR (KIAS)
V2 (KIAS)
TOFL (FT)
103
106
114
2682
102
106
114
3057
102
106
114
3255
102
107
114
3459
102
107
114
3654
102
107
114
3955
104
107
114
4504
106
108
114
5129
107
108
114
5607
13,000 lbs
v1 (KIAS)
VR (KIAS)
V2 (KIAS)
TOFL (FT)
101
104
112
2373
99
104
111
2692
99
104
111
2857
99
104
111
3026
99
104
111
3203
99
104
111
3458
100
104
111
3910
102
105
110
4430
103
105
110
4843
12,000 lbs
v1 (KIAS)
VR (KIAS)
V2 (KIAS)
TOFL (FT)
99
104
112
2199
98
104
112
2489
98
104
112
2646
98
104
111
2799
97
104
111
2960
97
104
111
3193
99
104
110
3602
100
104
110
4037
101
104
110
4361
11,000 lbs
v1 (KIAS)
VR (KIAS)
V2 (KIAS)
TOFL (FT)
98
104
112
2028
97
104
112
2290
97
104
112
2431
96
104
112
2577
96
104
112
2722
96
104
111
2931
97
104
111
3301
99
104
110
3733
99
104
110
4021
10,500 lbs and under
v1 (KIAS)
VR (KIAS)
V2 (KIAS)
TOFL (FT)
97
104
112
1943
97
104
112
2192
96
104
112
2326
96
104
112
2465
95
104
112
2606
95
104
111
2803
96
104
111
3155
98
104
110
3562
99
104
110
3681
>> Flaps in UP position
>> A/C and Bleed Air ON
MilViz KA350i
11-2
Takeoff Speeds & Field Length Reference (2000 ft)
Outside air temperature °C
Takeoff Weight
Item
-35
-15
-5
5
15
25
35
45
52
15,000 lbs
v1 (KIAS)
VR (KIAS)
V2 (KIAS)
TOFL (FT)
106
110
117
3458
106
110
117
3931
106
110
117
4191
106
110
117
4443
106
110
117
4713
107
111
117
5324
109
111
117
6109
111
112
117
7017
-----
14,000 lbs
v1 (KIAS)
VR (KIAS)
V2 (KIAS)
TOFL (FT)
103
106
114
3014
102
107
114
3443
102
107
114
3654
102
107
114
3878
102
107
114
4108
103
107
114
4637
105
108
114
5295
107
108
114
6068
-----
13,000 lbs
v1 (KIAS)
VR (KIAS)
V2 (KIAS)
TOFL (FT)
100
104
111
2655
99
104
111
3014
99
104
111
3204
98
104
111
3397
98
104
111
3586
99
104
111
4028
101
105
110
4585
103
105
110
5233
-----
12,000 lbs
v1 (KIAS)
VR (KIAS)
V2 (KIAS)
TOFL (FT)
98
104
112
2455
98
104
111
2788
97
104
111
2960
97
104
111
3139
97
104
111
3313
98
104
110
3709
99
104
110
4169
100
104
109
4693
-----
11,000 lbs
v1 (KIAS)
VR (KIAS)
V2 (KIAS)
TOFL (FT)
97
104
112
2259
96
104
112
2566
96
104
112
2722
96
104
111
2883
95
104
111
3044
96
104
111
3400
98
104
110
3855
99
104
110
4348
-----
10,500 lbs and under
v1 (KIAS)
VR (KIAS)
V2 (KIAS)
TOFL (FT)
97
104
112
2163
96
104
112
2455
95
104
112
2606
95
104
112
2759
95
104
111
2910
96
104
111
3250
97
104
110
3679
98
104
110
4161
-----
>> Flaps in UP position
>> A/C and Bleed Air ON
MilViz KA350i
11-3
Takeoff Speeds & Field Length Reference (4000 ft)
Outside air temperature °C
Takeoff Weight
Item
-35
-15
-5
5
15
25
35
45
52
15,000 lbs
v1 (KIAS)
VR (KIAS)
V2 (KIAS)
TOFL (FT)
106
110
117
3879
106
110
117
4429
106
110
117
4719
106
110
117
5016
107
111
117
5531
108
111
117
6300
110
112
117
7219
-----
-----
14,000 lbs
v1 (KIAS)
VR (KIAS)
V2 (KIAS)
TOFL (FT)
102
107
114
3399
102
107
114
3866
102
107
114
4114
102
107
114
4370
103
107
114
4819
104
108
114
5454
106
108
114
6244
-----
-----
13,000 lbs
v1 (KIAS)
VR (KIAS)
V2 (KIAS)
TOFL (FT)
99
104
111
2977
98
104
111
3387
98
104
111
3600
98
104
111
3821
99
104
111
4191
100
105
110
4728
102
105
110
5388
-----
-----
12,000 lbs
v1 (KIAS)
VR (KIAS)
V2 (KIAS)
TOFL (FT)
98
104
111
2755
97
104
111
3130
97
104
111
3325
97
104
111
3526
97
104
110
3860
98
104
110
4316
100
104
110
4853
-----
-----
11,000 lbs
v1 (KIAS)
VR (KIAS)
V2 (KIAS)
TOFL (FT)
96
104
112
2535
96
104
111
2875
95
104
111
3056
95
104
111
3239
96
104
111
3538
97
104
110
3978
98
104
110
4477
-----
-----
10,500 lbs and under
v1 (KIAS)
VR (KIAS)
V2 (KIAS)
TOFL (FT)
96
104
112
2424
95
104
112
2751
95
104
111
2922
94
104
111
3099
95
104
111
3381
96
104
110
3797
98
104
110
4297
-----
-----
>> Flaps in UP position
>> A/C and Bleed Air ON
MilViz KA350i
11-4
Takeoff Speeds & Field Length Reference (6000 ft)
Outside air temperature °C
Takeoff Weight
Item
-35
-15
-5
5
15
25
35
45
52
15,000 lbs
v1 (KIAS)
VR (KIAS)
V2 (KIAS)
TOFL (FT)
106
110
117
4378
106
110
117
5007
106
110
117
5332
106
111
117
5795
108
111
117
6535
110
112
117
7448
111
112
117
8599
-----
-----
14,000 lbs
v1 (KIAS)
VR (KIAS)
V2 (KIAS)
TOFL (FT)
102
107
114
3823
102
107
114
4363
102
107
114
4664
102
107
114
5050
104
108
114
5674
105
108
114
6448
107
109
114
7419
-----
-----
13,000 lbs
v1 (KIAS)
VR (KIAS)
V2 (KIAS)
TOFL (FT)
98
104
111
3351
98
104
111
3815
98
104
110
4053
98
104
111
4397
100
104
110
4921
101
105
110
5572
103
106
110
6381
-----
-----
12,000 lbs
v1 (KIAS)
VR (KIAS)
V2 (KIAS)
TOFL (FT)
97
104
111
3095
97
104
111
3521
97
104
111
3749
97
104
110
4049
98
104
110
4499
99
104
110
5029
100
104
109
5667
-----
-----
11,000 lbs
v1 (KIAS)
VR (KIAS)
V2 (KIAS)
TOFL (FT)
96
104
111
2844
95
104
111
3235
95
104
111
3440
95
104
111
3713
96
104
110
4144
98
104
110
4642
99
104
109
5235
-----
-----
10,500 lbs and under
v1 (KIAS)
VR (KIAS)
V2 (KIAS)
TOFL (FT)
95
104
112
2722
94
104
111
3094
94
104
111
3290
94
104
111
3548
96
104
110
3955
97
104
110
4449
98
104
109
5023
-----
-----
>> Flaps in UP position
>> A/C and Bleed Air ON
MilViz KA350i
11-5
Takeoff Speeds & Field Length Reference (8000 ft)
Outside air temperature °C
Takeoff Weight
Item
-35
-15
-5
5
15
25
35
45
52
15,000 lbs
v1 (KIAS)
VR (KIAS)
V2 (KIAS)
TOFL (FT)
105
110
117
4956
106
111
117
5689
106
111
117
6127
107
111
117
6850
109
112
117
7761
111
112
117
8926
-----
-----
-----
14,000 lbs
v1 (KIAS)
VR (KIAS)
V2 (KIAS)
TOFL (FT)
102
107
114
4317
102
107
114
4955
102
107
114
5341
103
108
114
5956
105
108
114
6723
107
109
114
7673
109
109
114
8913
-----
-----
13,000 lbs
v1 (KIAS)
VR (KIAS)
V2 (KIAS)
TOFL (FT)
98
104
111
3778
98
104
110
4314
98
104
110
4641
99
105
110
5166
101
105
110
5811
102
106
110
6616
104
106
110
7634
-----
-----
12,000 lbs
v1 (KIAS)
VR (KIAS)
V2 (KIAS)
TOFL (FT)
97
104
111
3487
97
104
111
3987
97
104
110
4286
97
104
110
4721
98
104
110
5250
100
104
109
5893
101
104
108
6683
-----
-----
11,000 lbs
v1 (KIAS)
VR (KIAS)
V2 (KIAS)
TOFL (FT)
95
104
111
3204
95
104
111
3658
95
104
111
3926
96
104
110
4350
97
104
110
4842
98
104
109
5442
100
104
109
6167
-----
-----
10,500 lbs and under
v1 (KIAS)
VR (KIAS)
V2 (KIAS)
TOFL (FT)
94
104
111
3065
94
104
111
3497
94
104
111
3751
95
104
110
4153
96
104
110
4652
98
104
110
5231
99
104
109
5916
-----
-----
>> Flaps in UP position
>> A/C and Bleed Air ON
MilViz KA350i
11-6
Takeoff Speeds & Field Length Reference (10,000 ft)
Outside air temperature °C
Takeoff Weight
Item
-35
-15
-5
5
15
25
35
45
52
15,000 lbs
v1 (KIAS)
VR (KIAS)
V2 (KIAS)
TOFL (FT)
106
111
117
5693
106
111
117
6599
107
111
117
7329
109
112
117
8242
110
112
117
9437
-----
-----
-----
-----
14,000 lbs
v1 (KIAS)
VR (KIAS)
V2 (KIAS)
TOFL (FT)
102
107
114
4962
102
108
114
5756
103
108
114
6360
104
108
114
7134
106
109
114
8117
108
109
114
9379
-----
-----
-----
13,000 lbs
v1 (KIAS)
VR (KIAS)
V2 (KIAS)
TOFL (FT)
98
104
110
4320
98
104
110
5007
99
105
110
5523
100
105
110
6168
102
106
110
6996
104
106
110
8030
-----
-----
-----
12,000 lbs
v1 (KIAS)
VR (KIAS)
V2 (KIAS)
TOFL (FT)
96
104
111
3993
97
104
110
4613
97
104
110
5041
98
104
110
5575
99
104
109
6224
101
104
109
7032
-----
-----
-----
11,000 lbs
v1 (KIAS)
VR (KIAS)
V2 (KIAS)
TOFL (FT)
95
104
111
3664
95
104
111
4226
96
104
110
4646
97
104
110
5140
98
104
109
5751
99
104
109
6487
-----
-----
-----
10,500 lbs and under
v1 (KIAS)
VR (KIAS)
V2 (KIAS)
TOFL (FT)
94
104
111
3502
94
104
111
4036
95
104
110
4436
96
104
110
4936
97
104
110
5521
99
104
109
6234
-----
-----
-----
>> Flaps in UP position
>> A/C and Bleed Air ON
MilViz KA350i
12-1
Normal Procedures
Emergency and Abnormal procedures are not
listed.
References to details obviously unavailable
within a simulation environment have been included for those interested, but should not be
taken literally.
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
MilViz KA350i
12-2
Preflight Inspection
Cabin
1.
Baggage
15. Landing Gear Indicators
secure
2. Aft Exit Sign
ON-TEST
check illumination
off-reset
3. Forward Exit Sign
Stow ON-TEST
check illumination
off-reset
4. Emergency Exits
secure & unlocked
5. Control Locks
remove
6. Parking Brake
set
7.
Landing Gear
8. Condition Levers
9.
down
fuel cutoff
Elevator Trim
2 units nose up
10. Rudder Trim
0 units
11. Aileron Trim
0 units
12. Battery Bus
norm
13. Voltmeter - BAT Position
14. Battery
23 volts min
on
16. Fuel Quantity
17. Voltmeter - TPL FED
18. Voltmeter - L GEN & R GEN
19. Voltmeter - CTR
20. Voltmeter - EXT PWR
21. GEN TIES
22. Flaps
23. Battery
(Preflight (Cabin) Inspection complete)
illuminated
Check
22 volts min
0 volts
23 Volts Min
0 volts
MAN CLOSE
check
off
MilViz KA350i
12-3
Preflight Inspection [continued]
LEFT WING & Engine NACELLE
16. Inverter Cooling Louvers
Clear
Check
17. Flush Fuel Vent & Heated Fuel Vent
Clear
2. Handrails
Check
18. Landing Gear
Check
3. Left Side Windows
Check
19. Engine Oil Vent
Clear
4. Flaps
check
20. Brake Line
Check
5. Aileron & Trim Tab
check
21. Brakes
Check
6. Static Wicks
Check
22. Wheel Chocks
7.
Check
23. Fuel Strainer & Fuel Filter Drains
Drain
8. Lights
check
24. Ice Vane & Oil Radiator Exhaust
Clear
9.
Main Fuel Tank Cap
Secure
25. Ice Light
Check
10. Stall Warning Vane
Check
26. Engine Oil
Check, secure Cap
1.
Cabin Door Seal
Siphon Break Vent
11. Tie-Down
Remove
Remove
27. Cowling Air Exhaust
Clear
12. Outboard Fuel Drain
Drain
28. Left Side Engine Cowling, Doors, & Panels
Secure
13. Outboard Deice Boot & Stall Strip
check
29. Left Side Exhaust Stack
Check
14. Wing Panels
Secure
30. Left Side Top Cowling Camlocks
Secure
15. Leading-Edge Fuel Tank & Gravity-Line Drains
Drain
31. Propeller
Check , rotate
MilViz KA350i
12-4
Preflight Inspection [continued]
LEFT WING & Engine NACELLE (continued)
Nose
32. Top Cowling Air Intakes
Clear
1.
33. Engine & Oil Radiator Air Intakes
Clear
2. Brake Reservoir Vent
Clear
34. Right Side Top Cowling Camlocks
Secure
3. Left Avionics Access Panel
Secure
35. Right Side Exhaust Stack
Check
4. Air Conditioner Condenser Exhaust Duct
Clear
36. Swing Check Valve Exhaust
Clear
5. Windshield & Windshield Wipers
Check
37. Generator Air Intake
Clear
6. Radome
Check
38. Right Side Engine Cowling, Doors, & Panels
Secure
7.
Clear
39. Auxiliary Fuel Tank Cap
Secure
8. Landing & Taxi Lights
Check
40. Hydraulic Gear Service Door
Secure
9.
Nose Gear
Check
41. Inboard Deice Boot
Check
10. Wheel Chocks
Remove
42. Heat Exchanger Air Intake & Exhaust
Clear
11. Nose Gear Doors & Wheel Well
Check
43. Hydraulic Gear Overfill & Vent Lines
Clear
12. Air Conditioner Condenser Intake Duct
Clear
44. Auxiliary Fuel Tank Drain
Drain
13. Right Avionics Access Panel
Secure
45. Lower Antennas & Panels
Secure
(Preflight (Left Wing & Engine Nacelle) Inspection complete)
OAT Probe & Relief Tube Vent
Pitot Masts
(Preflight (Nose) Inspection complete)
Check
MilViz KA350i
12-5
Preflight Inspection [continued]
Right WING & Engine NACELLE
16. Top Cowling Air Intakes
Clear
Clear
17. Engine & Oil Radiator Air Intakes
Check
2. Auxiliary Fuel Tank Drain
Drain
18. Right Side Top Cowling Camlocks
Secure
3. Battery Box Drain
Clear
19. Right Side Exhaust Stack
Check
4. Lower Panels
Secure
20. Swing Check Valve Exhaust
Clear
5. Heat Exchanger Air Intake & Exhaust
Clear
21. Generator Air Intake
Clear
6. Inboard Deice Boot
Check
22. Right Side Engine Cowling, Doors, & Panels
Secure
7.
Battery Access Panel
Secure
23. Ice Light
Check
8. Auxiliary Fuel Tank Cap
Secure
24. Oil Radiator & Ice Vane Exhaust
Clear
Check, secure Cap
25. Fuel Filter & Fuel Strainer Drains
Drain
1.
9.
Ejector Exhaust
Engine Oil
10. Cowling Air Exhaust
Clear
26. Landing Gear
Check
11. Left Side Engine Cowling, Doors, & Panels
Secure
27. Engine Oil Vent
Clear
12. Collector Drain
Clear
28. Brake Line
Check
13. Left Side Exhaust Stack
Check
29. Brakes
Check
14. Left Side Top Cowling Camlocks
Secure
30. Wheel Chocks
15. Propeller
Check , rotate
31. Flush Fuel Vent & Heated Fuel Vent
Remove
Clear
MilViz KA350i
12-6
Preflight Inspection [continued]
Right WING & Engine NACELLE (continued)
Right Aft Fuselage
32. Inverter Cooling Louvers
Clear
1.
Lower Antennas & Beacon
Check
33. Leading-Edge Fuel Tank & Gravity-Line Drains
Drain
2. Oxygen Service Access Door
Secure
34. External Power Door
Secure
3. Static Ports
Clear
35. Wing Panels
Secure
4. ELT Antenna
Check
36. Outboard Deice Boot & Stall Strip
Check
5. Aft Compartment Lower Access Door
Secure
37. Outboard Fuel Drain
Drain
6. Tie-down
Remove
38. Tie-Down
Remove
7.
39. Main Fuel Tank Cap
Secure
8. Cabin Air Exhaust
Clear
40. Lights
Check
9.
Secure
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)
Ventral Fin Drain Holes
Access Panel
(Preflight (Right Aft Fuselage) Inspection complete)
Clear
MilViz KA350i
12-7
Preflight Inspection [continued]
Tail
1.
Ventral Fin & Static Wick
Left Aft Fuselage
Check
1.
2. VOR Antennas
Check
2. Static Ports
Clear
3. Rudder & Trim Tab
Check
3. Oxygen Discharge & Aft Drain Tubes
Clear
4. Horizontal Stabilizer
Check
4. Relief Tube
Clear
5. Elevator & Trim Tab
Check
(Preflight (Left Aft Fuselage) Inspection complete)
6. Trim Tabs in Neutral Position
Verify
(Preflight Inspection checklist complete)
7.
Check
Lights
(Preflight (Tail) Inspection complete)
Access Panels
Secure
MilViz KA350i
12-8
Before Engine Starting
1.
Weight, CG, Performance, & V-Speeds
2. Doors
3. Load & Baggage
Checked
Locked
Confirm Secured
b. Battery Bus
c.
Engine Anti-ice
d. Landing Gear Relay Circuit Breaker
Confirm NORM
ON & MAIN
IN
4. Passenger Briefing
Complete
e. Landing Gear Control
Down
5. Cabin Equipment
Positioned
12. Power Console & Pedestal
Check
6. Parking Brake
Confirm Set
7.
Control Locks
8. Oxygen System Preflight
9.
b. Prop Levers
Confirm Complete
c.
Arm
10. Fuel Panel
Check
Standby Pumps
b. Crossfeed
c.
Aux Transfer Switches
d. Circuit Breakers
11. Pilot’s Instrument Panel & Subpanel
a.
ESIS Power
Power Levers
Confirm Removed
ELT Switch
a.
a.
Off
Off
Auto
In
Check
ON
Idle
Full Forward
Condition Levers
Fuel Cutoff
d. Oxygen Controls
Set
e. Landing Gear Alternate Extension Handle
13. Reversionary Switch Panel
a.
DG FREE/NORM
b. SLEW +/c.
Stowed
Check
Norm
Center
ATC Select
STBY
d. PILOT DISPLAY
NORM
e. AHRS
NORM
MilViz KA350i
12-9
Before Engine Starting [continued]
f.
ADC
NORM
a.
g. TUNE
NORM
b. Standby Pumps
Off
h. RMT TUNE
Norm
c.
Crossfeed
Off
d. Fuel Quantity
Test
i.
GND COM
14. Copilot’s Subpanel & Instrument Panel
a.
Window Defog
b. ECS Mode
c.
Extinguished
Check
Off
Off
Cabin Blower
Auto
d. Env. Bleed Air
As Required
15. Electric Heat
16. Right Panel Circuit Breakers
As Required
In
Firewall Fuel Valves
Open
22. Fuel Quantity
Check
23. Pilot’s Subpanel
Check
a.
Landing Gear Control Lights
b. Hydraulic Fluid Sensor
c.
Beacon
24. Copilot’s Subpanel
a.
Test
Test
On
Check
Cabin Altitude Warning
Test
b. Cabin Differential Warning
Test
17. Pilot’s Static Air Source
Normal
18. Interior Master Switch
Off
c.
Stall & Landing Gear Warning
Test
19. Battery
On
d. Fire Detector & Extinguisher
Test
20. Annunciators
Test
21. Fuel System
Check
(Before Engine Starting checklist complete)
MilViz KA350i
12-10
Engine Starting (Battery)
1.
GEN TIES
2. Propeller Area
3. Right Ignition & Engine Start
MAN Close
Clear
ON
[observe]
[R GEN TIE OPEN]
10. Battery
11. Left Ignition & Engine Start
Extinguished
Charge
On
[observe]
[R IGNITION ON]
Illuminated
[observe]
[L IGNITION ON]
Illuminated
[observe]
[R FUEL PRES LO]
Extinguished
[observe]
[L FUEL PRES LO]
Extinguished
[wait]
After N1 reaches 12% (minimum):
[wait]
After N1 reaches 12% (minimum):
4. Right Condition Lever
Low Idle
12. Left Condition Lever
Low Idle
5. Right ITT & N1
Monitor
13. Left ITT & N1
Monitor
6. Right Oil Pressure
Check
[wait]
After N1 reaches 50%:
7.
Right Ignition & Engine Start
8. Right Condition Lever
9.
Right Generator
14. Left Oil Pressure
Check
[wait]
After N1 reaches 50%:
Off
High Idle
Reset, Then On
15. Left Ignition & Engine Start
16. Right Condition Lever
17. Left and Right Prop RPM
Off
Low Idle
1050 minimum
[observe]
[R DC GEN]
Extinguished
[observe]
[L PROP PITCH]
Illuminated
[observe]
[L GEN TIE OPEN]
Extinguished
[observe]
[R PROP PITCH]
Illuminated
MilViz KA350i
12-11
Engine Starting (Battery) [continued]
18. Voltmeter - L GEN
27.5 - 29.0 volts
19. Left Generator
Reset, Then On
[observe]
[L DC GEN]
20. Right Generator
Extinguished
Reset
[observe]
[L GEN TIE OPEN]
EXTINGUISHED
[observe]
[R GEN TIE OPEN]
EXTINGUISHED
21. Right Generator
(Engine Starting (Battery) checklist complete)
ON
MilViz KA350i
12-12
Engine Starting (External Power)
1.
Battery
Verify ON
14. Propeller Area
2. GEN TIES
MAN CLOSE
15. Right Ignition & Engine Start
CLEAR
On
[observe]
[R IGNITION ON]
ILLUMINATED
[observe]
[R FUEL PRES LO]
EXTINGUISHED
3. Voltmeter - BAT
20.0 Volts Minimum
4. External Power
VERIFY OFF
5. Avionics Master
VERIFY OFF
[wait]
After N1 reaches 12% (minimum):
6. Left and Right Generators
Verify Off
16. Right Condition Lever
Low Idle
7.
Verify Off
17. Right ITT & N1
Monitor
Interior Master Switch
8. Battery Bus
9.
Beacon
10. External Power Source
VERIFY NORM
12. External Power
[observe]
[EXT PWR]
13. Prop Levers
Check
VERIFY ON
[wait]
After N1 reaches 50%:
TURN OFF
19. Right Ignition & Engine Start
Off
CONNECT TO AIRPLANE
20. Left Ignition & Engine Start
On
TURN ON
11. Voltmeter - EXT PWR
18. Right Oil Pressure
28.0 - 28.4 VOLTS
On
ILLUMINATED
FEATHER
[observe]
[L IGNITION ON]
ILLUMINATED
[observe]
[L FUEL PRES LO]
EXTINGUISHED
[wait]
After N1 reaches 12% (minimum):
21. Left Condition Lever
Low Idle
22. Left ITT & N1
Monitor
MilViz KA350i
12-13
Engine Starting (External Power) [continued]
23. Left Oil Pressure
CHECK
[wait]
After N1 reaches 50%:
[observe]
[L GEN TIE OPEN]
EXTINGUISHED
[observe]
[R GEN TIE OPEN]
EXTINGUISHED
24. Left Ignition & Engine Start
Off
31. Prop Levers
FULL FORWARD
25. External Power
Off
32. Left & Right Prop RPM
1050 MINIMUM
26. External Power Source
TURN OFF
[observe]
[L PROP PITCH]
ILLUMINATED
DISCONNECT From Airplane
[observe]
[R PROP PITCH]
ILLUMINATED
SECURE DOOR
[observe]
[EXT PWR]
27. Right Generator
EXTINGUISHED
RESET, THEN ON
[observe]
[R DC GEN]
EXTINGUISHED
[observe]
[L GEN TIE OPEN]
EXTINGUISHED
[observe]
[R GEN TIE OPEN]
EXTINGUISHED
28. Voltmeter - L GEN
29. Left Generator
[observe]
[L DC GEN]
30. Right Generator
27.5 to 29.0 volts
RESET, THEN ON
EXTINGUISHED
.RESET, THEN ON
(Engine Starting (External Power) checklist complete)
MilViz KA350i
12-14
Before Taxi
1.
Electrical System
Check
e. Voltmeter - CTR
a.
OPEN
f.
GEN TIES
RESET
[observe]
[L GEN TIE OPEN]
ILLUMINATED
[observe]
[L GEN TIE OPEN]
EXTINGUISHED
[observe]
[R GEN TIE OPEN]
ILLUMINATED
[observe]
[R GEN TIE OPEN]
EXTINGUISHED
[observe]
[BAT TIE OPEN]
EXTINGUISHED
b. Voltmeter
1)
c.
Bus Sense
0 Volts
TPL FED
Check
26.5 TO 28.0 VOLTS
g. Voltmeter - CTR
27.5 TO 29.0 VOLTS
2) R GEN
27.5 TO 29.0 VOLTS
h. Generator Load
Check
3) L GEN
27.5 TO 29.0 VOLTS
4) CTR
23 VOLTS MINIMUM
GEN TIES
NORM
[observe]
Observe Parallel Loads - Within 10%
2. Avionics Master
On
3. Interior Master Switch
As Required
As Required
[observe]
[L GEN TIE OPEN]
EXTINGUISHED
4. Master Panel & Cockpit Lights
[observe]
[R GEN TIE OPEN]
EXTINGUISHED
5. Mic Switches
Normal
TEST
6. Cabin Lights
As Required
NO SMK/FSB
d. Bus Sense
[observe]
[L GEN TIE OPEN]
ILLUMINATED
7.
[observe]
[R GEN TIE OPEN]
ILLUMINATED
8. ESIS Display
[observe]
[BAT TIE OPEN]
ILLUMINATED
Cabin Sign
[observe]
INITIALIZATION COMPLETE
Check
MilViz KA350i
12-15
Before Taxi [continued]
9.
Exterior Lights
1)
As Required
ECS Mode
MAN HEAT
10. Overspeed Warning
Test
2) Cockpit/Cabin Blower
AS REQUIRED
11. Environmental System Controls
Set
3) Cockpit/Cabin Temp
AS REQUIRED
4) Environmental Bleed Air
AS REQUIRED
a.
Automatic Climate Control
1)
ECS Mode
2) Cockpit/Cabin Temp
5) Bleed Air Valves
AUTO
6) Man Temp Incr/Decr
As Required
3) Cockpit/Cabin Blower
AUTO
4) Environmental Bleed Air
AUTO
1)
5) Bleed Air Valves
OPEN
2) Cockpit/Cabin Blower
b. Manual Control Cooling
1)
ECS Mode
As Required
d. Recirculation Blowers
e. Electric Heat Control
1)
MAN COOL
ECS Mode
[observe]
[ELEC HEAT ON]
As Required
3) Cockpit/Cabin Blower
As Required
12. Brake Deice
4) Environmental Bleed Air
As Required
13. Prop Sync
Manual Control Heating
OPEN
As Required
Open
AS REQUIRED
AS REQUIRED
ECS Mode
2) Cockpit/Cabin Temp
5) Bleed Air Valves
c.
As Required
OFF
AS REQUIRED
AS REQUIRED
ELEC HEAT
ILLUMINATED
AS REQUIRED
14. TCAS II
a.
MFD - PRESS TFC KEY FOR > 1 SEC TO SELECT TCAS ONLY MAP
On
TEST
MilViz KA350i
12-16
Before Taxi [continued]
b. Ensure all TAWS+ inhibit switches (G/S INHIB, TERR INHIB, and FLAP
OVRD) are deselected
b. RTU - PRESS LSK R3 THREE TIMES TO ACTIVATE TEST
TCAS II test pattern will display on MFD
[observe]
c.
[observe]
TCAS TEST message will be displayed on PFDs and MFD
d. Select present position map and TERR for display on the MFD. Verify
no TERRAIN FAIL message is present
[observe]
The red TRAFFIC message will be displayed on PFDs
TCAS II vertical speed test pattern will be displayed on
[observe]
IVSIs
15. EMER FREQ
16. TAWS+
a.
Verify avionics on and the following is functioning:
Verify no TAWS+ inoperative mode messages (amber GPWS or TERR)
are displayed on the PFD
e. Conduct a self test of the system by depressing the G/S INHIB annunciator switch and releasing. The following annunciations and
alerts should be issued:
EXTINGUISHED
»» Amber GPWS and TERR annunciators on the PFD and TERRAIN FAIL
on the MFD
PREFLIGHT
»» A momentary illumination of the G/S INHIB and FLAP OVRD annunciator switches (ACTIVE)
»» Amber GND PROX message on the PFD
»» Radio Altimeter
»» A red PULL UP message on the PFD
»» ADC 1 and 2
»» Test pattern on the MFD terrain display
»» AHRS 1 and 2
»» Terrain display test pattern removed and all TAWS+ messages and
annunciator switches extinguished
»» GPS 1
17. Flight and Engine Instruments
CHECK
»» Gear and Flap Indicating System
a.
Altimeters
SET
»» Display System (PFD and MFD)
b. ESIS Altimeter
SET
»» FMS
18. Flaps
UP
MilViz KA350i
12-17
Before Taxi [continued]
19. Flight Controls
CHECK
»» FULL FREEDOM OF MOVEMENT
»» PROPER DIRECTION OF TRAVEL
20. Brakes
(Before Taxi checklist complete)
RELEASE, CHECK
MilViz KA350i
12-18
Before Takeoff - Runup
1.
Avionics & Radar
2. Pressurization
a.
Environmental Bleed Air
b. Bleed Air Valves
c.
Check
NORMAL
d. Electric Pitch Trim
Adjust cabin altitude knob to indicate 1,000 ft below pressure
altitude
e. Elevator
f.
HOLD AT TEST
position
e. Cabin Altimeter and VSI
CHECK FOR DESCENT
INDICATION
f.
Cabin Pressure Switch
a.
Pitch Trim
b. Elevator
Check
TAKEOFF POSITION
FORWARD POSITION
OPERATE both
directions
Centered
ENGAGE
Apply rearward pressure on the elevator; observe pitch trim
travel nose-down
g. AP/Trim Disconnect
Set
[observe]
Inner scale (ACFT ALT) should indicate planned cruise
altitude + 1,000 ft
ILLUMINATED (pfd)
2) Apply forward pressure on the elevator; observe pitch trim travel
nose-up
RELEASE
g. Pressurization Controller
3. Autopilot
Autopilot
1)
2) Set rate knob to 12-o’clock position.
d. Cabin Pressure Switch
ENGAGE
[observe]
Autopilot disengages with each operation; YD remains
engaged
OPEN
SET
Autopilot
[observe]
[AP]
CHECK, SET
Pressurization Controller
1)
c.
DEPRESS to 1st
level
[observe]
MOMENTARY RED [AP]
ILLUMINATED (pfd),
then extinguished
[observe]
AMBER [YD]
ILLUMINATED (pfd),
then extinguished
h. Repeat items a through g for copilot’s side
4. Yaw Damper
a.
Yaw Damper
[observe]
Green [YD]
Check
On
ILLUMINATED (pfd)
MilViz KA350i
12-19
Before Takeoff - Runup [continued]
»» AP/Trim Disconnect
[observe]
Yellow [YD]
5. Electric Pitch Trim
a.
Pilot’s and Copilot’s Trim Switches
b. AP/Trim Disconnect
[observe]
Red [TRIM]
c.
AP/Trim Disconnect
[observe]
Red [TRIM]
DEPRESS to 1st
level
Flashes
e. Power Levers (individually)
DEPRESS to 2nd
level
ILLUMINATED (pfd)
Extinguished
a.
Rudder Boost Switch
[observe]
[RUD BOOST OFF]
b. Rudder Boost Switch
HOLD TO GOV
»» INCREASE UNTIL PROP IS STABILIZED AT 1500 TO 1610 RPM
f.
AP/Trim Disconnect
[observe]
[RUD BOOST OFF]
Release
Set
Overspeed Governors & Rudder Boost
Full Forward
CHECK
7.
9.
Prop Levers
d. Prop Governor Test Switch
Set
8. Flaps
Extinguished
Check
6. Trim Tabs
Engine Controls Friction Locks
c.
[observe]
[RUD BOOST OFF]
g. AP/Trim Disconnect
[observe]
[RUD BOOST OFF]
h. Power Lever
DEPRESS to 1st
level
ILLUMINATED
Release
Extinguished
Idle
Check, Set
i.
Repeat steps e through h on the opposite engine
CHECK
j.
Prop Governor Test Switch
RELEASE
10. Low Pitch Stops & Primary Governors
CHECK
Off
ILLUMINATED
RUDDER BOOST
a.
Prop Levers
b. Low Pitch Stop Switch
FULL FORWARD
HOLD TO GND IDLE
STOP
MilViz KA350i
12-20
Before Takeoff - Runup [continued]
c.
[observe]
[L PROP PITCH]
ILLUMINATED
»» At approximately 10% torque:
BOTH ANNUNCIATORS - EXTINGUISHED
[observe]
[R PROP PITCH]
ILLUMINATED
d. Power Levers
Power Levers
SET 1500 RPM
[observe]
[L AFX]
EXTINGUISHED
CYCLE TO LOW AND
HIGH RPM
[observe]
[R AFX]
EXTINGUISHED
RELEASE
e. Autofeather Switch
RELEASE
d. Prop Levers
e. Low Pitch Stop Switch
f.
[observe]
[L PROP PITCH]
EXTINGUISHED
[observe]
[R PROP PITCH]
EXTINGUISHED
Prop RPM
11. Autofeather
a.
Autofeather Switch
CHECK
HOLD TO TEST
[observe]
[AUTOFTHER OFF]
Arm
EXTINGUISHED
13. Manual Propeller Feathering
CHECK
14. Vacuum & Deice Pressure
CHECK
Left Bleed Air Switch
PNEU & ENVIR OFF
APPROX. 22%
TORQUE
[observe]
Pneumatic pressure and vacuum
gages
NORMAL PRESSURE
[observe]
[L AFX]
ILLUMINATED
[observe]
[L BLEED FAIL]
EXTINGUISHED
[observe]
[R AFX]
ILLUMINATED
[observe]
[R BLEED FAIL]
EXTINGUISHED
Power Levers
Retard
Individually
b. Power Levers
c.
STABILIZED AT 1150
TO 1250 rpm
12. Autofeather
IDLE
»» At approximately 17% torque:
OPPOSITE ANNUNCIATOR - EXTINGUISHED
a.
b. Right Bleed Air Switch
[observe]
Pneumatic pressure and vacuum
gages
PNEU & ENVIR OFF
ZERO PRESSURE
MilViz KA350i
12-21
Before Takeoff - Runup [continued]
c.
[observe]
[L BLEED FAIL]
ILLUMINATED
[observe]
[R BLEED FAIL]
ILLUMINATED
Left Bleed Air Switch
OPEN OR ENVIR OFF
[observe]
Pneumatic pressure and vacuum
gages
NORMAL PRESSURE
a.
Engine Auto-Ignition
1)
Power Levers
CHECK
CHECK
IDLE
EXTINGUISHED
2) Engine Auto-Ignition Switches
[observe]
[R BLEED FAIL]
EXTINGUISHED
[observe]
[L IGNITION ON]
ILLUMINATED
OPEN OR ENVIR OFF
[observe]
[R IGNITION ON]
ILLUMINATED
15. Engine Anti-ice
Engine Anti-ice Actuators
b. Engine Anti-ice
c.
16. Ice Protection Equipment (If Required)
ILLUMINATED
[observe]
[L BLEED FAIL]
d. Right Bleed Air Switch
a.
[observe]
[R ENG ANTI-ICE]
CHECK
3) Power Levers
ARM
ADVANCE TO ABOVE
17% TORQUE
STANDBY
[observe]
[L IGNITION ON]
EXTINGUISHED
OFF
[observe]
[R IGNITION ON]
EXTINGUISHED
[observe]
[L ENG ANTI-ICE]
EXTINGUISHED
4) Power Levers
[observe]
[R ENG ANTI-ICE]
EXTINGUISHED
[observe]
[L IGNITION ON]
ILLUMINATED
MAIN
[observe]
[R IGNITION ON]
ILLUMINATED
Engine Anti-ice Actuators
d. Engine Anti-ice
[observe]
[L ENG ANTI-ICE]
ON
ILLUMINATED
5) Engine Auto-Ignition Switches
[observe]
[L IGNITION ON]
IDLE
Off
EXTINGUISHED
MilViz KA350i
12-22
Before Takeoff - Runup [continued]
[observe]
[R IGNITION ON]
b. Windshield Anti-ice
1)
Windshield Anti-ice
EXTINGUISHED
c.
Electrothermal Propeller Deice
1)
Automatic Prop Deice
[observe]
Deice Ammeter
2) Manual Prop Deice
[observe]
Deice Ammeter
3) Manual Prop Deice
[observe]
Deice Ammeter
4) Automatic Prop Deice
d. Surface Deice
High Idle
2) Pneumatic Pressure
Check
Hi
3) Surface Deice Switch
Single, Release
[observe]
Pneumatic Pressure
OFF, THEN NORMAL
[observe]
Increase on left & right loadmeters
3) Windshield Anti-ice
Condition Levers
Check
[observe]
Increase on left & right loadmeters
2) Windshield Anti-ice
1)
Off
CHECK
On
26 TO 32 AMPS
HOLD IN MANUAL
0 AMPS
RELEASE
26 TO 32 AMPS
Off
Check
MOMENTARY
DECREASE
[observe]
[WING DEICE]
ILLUMINATED,
THEN EXTINGUISHED
[observe]
[TAIL DEICE]
ILLUMINATED,
THEN EXTINGUISHED
4) Condition Levers
Low Idle
17. Fuel Quantity
Check
18. Flight & Engine Instruments
Check
19. Static Take-Off Power
20. V1, VR, V2
(Before Takeoff - Runup checklist complete)
Confirm
Set
MilViz KA350i
12-23
Before Takeoff - Final Items
1.
Engine Auto-Ignition
ARM (if required)
5. Transponder
SELECT 1 OR 2
[observe]
[L IGNITION ON]
ILLUMINATED
(If Armed)
6. Prop Levers
FULL FORWARD
[observe]
[R IGNITION ON]
ILLUMINATED
(If Armed)
7.
Trim
CONFIRM SET
AS REQUIRED
8. Flaps
CONFIRM SET
[observe]
[L ENG ANTI-ICE]
ILLUMINATED
(If On)
9.
[observe]
[R ENG ANTI-ICE]
ILLUMINATED
(If On)
2. Engine Anti-ice
3. Exterior Lights
AS REQUIRED
4. Ice Protection
AS REQUIRED
a.
Windshield Anti-ice
b. Prop Deice
c.
Left & Right Fuel Vent Heat
Environmental Bleed Air
a.
OAT above 10°C
b. OAT at or below 10°C
SET
AUTO or LOW
AUTO or NORMAL
10. Bleed Air Valves
AS REQUIRED
NORMAL/HI
(If Required)
11. ECS Mode
AS REQUIRED
Auto
(If Required)
12. Cockpit/Cabin Blower
AS REQUIRED
13. Cockpit/Cabin Temp
AS REQUIRED
14. Interior Lights
AS REQUIRED
On
d. Stall Warning Heat
On
e. Left & Right Pitot Heat
On
[observe]
[L PITOT HEAT]
EXTINGUISHED
[observe]
[R PITOT HEAT]
EXTINGUISHED
15. Generator Load
Check
16. Battery Ammeter
Check
17. Annunciators
(Before Takeoff - Final Items checklist complete)
Off / Considered
MilViz KA350i
12-24
Takeoff
Normal Takeoff
1.
Brakes
2. Power Levers
Rolling Takeoff
Hold
SET STATIC TAKE-OFF
POWER
1.
Brakes
2. Power Levers
SET STATIC TAKE-OFF
POWER
[observe]
[L AFX]
ILLUMINATED
[observe]
[L AFX]
ILLUMINATED
[observe]
[R AFX]
ILLUMINATED
[observe]
[R AFX]
ILLUMINATED
Release
[wait]
Upon reaching VR:
3. Brakes
[wait]
Upon reaching VR:
3. ROTATE TO APPROXIMATELY 10°
4. ROTATE TO APPROXIMATELY 10°
[wait] When positive climb established:
[wait] When positive climb established:
4. Landing Gear
5. Landing Gear
6. Airspeed
Up
MAINTAIN V35 UNTIL
CLEAR OF
OBSTACLES
[wait]
At 125 knots, minimum:
7.
Release
Flaps
(Normal Takeoff checklist complete)
5. Airspeed
MAINTAIN V35 UNTIL
CLEAR OF
OBSTACLES
[wait]
At 125 knots, minimum:
6. Flaps
Up
Up
(Rolling Takeoff checklist complete)
Up
MilViz KA350i
12-25
Climb & Cruise
Climb
1.
Bleed Air Valves
2. Environmental Bleed Air
Cruise
Open
AS REQUIRED
1.
Cruise Power
Set As Desired
2. Autofeather
Off
3. Yaw Damper
On
3. ECS Mode
4. Climb Power
Set
4. Engine Instruments
Monitor
5. Fuel Gauges
Monitor
5. Props
1600 rpm,
or as desired
6. Windshield Anti-Ice
Normal
7.
MONITOR
Engine Instruments
8. Cabin Sign
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.
AS REQUIRED
(Cruise checklist complete)
9.
Pressurization
10. Lights
(Climb checklist complete)
CHECK
AS REQUIRED
AS REQUIRED
MilViz KA350i
12-26
Descent & Before Landing
Descent
1.
Before Landing
Pressurization
Set
1.
a.
Set
2. Autofeather
Arm
3. Environmental Bleed Air
Low
Cabin Altitude
b. Rate Control
2. Altimeter
As Desired
Set
Approach Speeds
Confirm
4. Cabin Lights
AS REQUIRED
3. Cabin Sign
AS REQUIRED
5. Cabin Sign
NO SMK/FSB
4. Windshield Anti-ice
AS REQUIRED
6. Flaps
APPROACH
5. Brake Deice
AS REQUIRED
7.
[observe]
[L BK DEICE ON]
ILLUMINATED,
If On
8. Exterior and Interior Lights
AS REQUIRED
[observe]
[R BK DEICE ON]
ILLUMINATED,
If On
9.
AS REQUIRED
AS REQUIRED
10. Surface Deice
6. Window Defog
7.
Fuel Balance
8. Cabin Equipment
(Descent checklist complete)
Check
Positioned
Landing Gear
Radar
(Before Landing checklist complete)
DOWN
AS REQUIRED
MilViz KA350i
12-27
Landing & After Landing
Normal Landing
1.
MAXIMUM REVERSE THRUST LANDING
Flaps
Down
2. Airspeed
Flaps
Down
VREF
2. Airspeed
VREF
3. Yaw Damper
Off
3. Yaw Damper
Off
4. Power Levers
Idle
4. Condition Levers
5. Prop Levers
FULL FORWARD
[wait]
After Touchdown:
1.
5. Power Levers
6. Prop Levers
6. Power Levers
SELECT
GROUND FINE
[wait]
After Touchdown:
7.
AS REQUIRED
7.
Brakes
(Normal Landing checklist complete)
Power Levers
8. Brakes
9.
Condition Levers
(Maximum Reverse Thrust Landing checklist complete)
HIGH IDLE
IDLE
FULL FORWARD
Reverse
AS REQUIRED
Low Idle
MilViz KA350i
12-28
Landing & After Landing [continued]
Balked Landing
After Landing
Power
MAXIMUM
ALLOWABLE
2. Airspeed
MAINTAIN VREF
1.
1.
Engine Auto-Ignition
2. Engine Anti-ice
[wait]
Clear of obstacles:
3. Exterior and Interior Lights
3. Establish normal climb
4. Ice Protection
[wait]
VREF + 10 knots:
5. Transponder
4. Flaps
5. Landing Gear
Approach
Up
[wait]
At 125 knots, minimum:
6. Flaps
(Balked Landing checklist complete)
Up
6. Radar
7.
Off
On
AS REQUIRED
OFF
STANDBY
STANDBY OR OFF
Trim
Set
8. Flaps
Up
9.
Pressurization Differential
10. Bleed Air Valves
(After Landing checklist complete)
Verify 0
OPEN or ENVIR OFF
MilViz KA350i
12-29
SHUTDOWN & SECURING
1.
Parking Brake
Set
16. Cabin Entry Lights
2. Avionics Master
Off
[wait]
Below 15% N1:
3. ESIS Power
Off
17. Battery & Generator Switches
4. Autofeather
Off
18. Control Locks
5. Exterior Lights
Off
19. Instrument Emergency Lights
6. ECS Mode
Off
20. Tie-downs & Chocks
Install
AUTO
21. External Covers
Install
Off
22. Parking Brake
Off
23. Baggage Compartment Lights
Off
24. Cabin Entry Lights
Off
7.
Cockpit/Cabin Blower
8. Oxygen Controls
9.
Battery
10. Interior Master Switch
CHARGED
Off
11. ITT
STABILIZED
12. Instrument Emergency Lights
On,
If Desired
13. Condition Levers
14. Prop Levers
15. Overhead Panel Switches
FUEL CUTOFF
FEATHER
OFF
(Shutdown & Securing checklist complete)
AS REQUIRED
Off
INSTALL
Off
Credits
MV TeamCollin 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
Modeling & Textures
FSSI Engineering
Sound Environment
Mike Maarse - SimAcoustics
RealLight & TrueGlass
TFDi Design
Dmi Usatyi - 3DReach
Product Testers Steve McNitt
John M
Marlon Carter
Zach Alcantar
Mike Cameron
Ryan Butterworth
Tom Stovall
Sergio S
Jaroslaw Kowalczyk
Greg Morin
Daniel FaasAsid [D.O.W.]
Jerome Zimmermann
John White
Project Consultant
Ken (King Air 200/300 Instructor)