2018 PRODUCT CATALOG - TEXTRON AVIATION SPECIAL MISSIONS
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2 0 1 8 P R O D U C T C A T A L O G
K I N G A I R C 9 0 G Tx KING AIR 250 KING AIR 350ER
2 0 1 8 P R O D U C T C A T A L O G PURPOSE This catalog describes available configuration options and modifications for aircraft customization offered by the Special Mission Aircraft Systems organization of Textron Aviation and its suppliers. The Textron Aviation Special Mission Aircraft Systems organization can provide OEM expertise to assist with design, certification and installation of modifications specifically tailored to meet individual requirements. STANDARD GENERAL TERMS Textron Aviation standard terms and conditions are applicable to all items offered in this catalog. Textron Aviation will, where possible, accommodate specific contractual requests.
TABLE OF CONTENTS
General Modifications and Services Wet and Contaminated Supplement
Aircraft: B300 (350), B300C (350C) 14
Aircraft-Specific Electrical Load Analysis
Aircraft: All Models 1 Special Mission Rudder Installation
Aircraft: B300 (350), B300C (350C) 15
TCN-500 TACAN Installation Kit
Aircraft: B300 (350), B300C (350C) 2 Special Mission Dual Aft Strakes
Aircraft: B300 (350), B300C (350C) 16
PT6A-67A Engine Installation
Aircraft: B300 (350), B300C (350C) 3 Installation of Baggage Door
Aircraft: C90, B200, B300 17
Engine Wash Rings
Aircraft: B300 (350), B300C (350C) 4 Digital Audio Control System (DACS)
Aircraft: B300 (350), B300C (350C) 18
Engine Wash Rings
Aircraft: B200 5 Nose Ballast Installation
Aircraft: B300 (350), B300C (350C) 19
PT6A-60A or -67A Engine Compressor
Wash Drain (CWD) Installation 400-Amp Generator Installation
Aircraft: B300 (350), B300C (350C) 6 Aircraft: B300 (350), B300C (350C) 20
PT6A-42 Engine Compressor Wash Extended Pedestal Installation
Drain (CWD) Installation Aircraft: B300 (350), B300C (350C) 21
Aircraft: B200, B200C 7
Pulselite Control System
High Flotation Gear Doors Aircraft: B300 (350), B300C (350C), B200, B200C,
Aircraft: B300, B300C (350/350ER), B200, B200C, B200GT, B200CGT 22
B200GT (250) 8
Aircraft Survivability Equipment
Crown Wing Locker System (ASE) Structural Provisions
Aircraft: B200, B200GT (250), C90 9 Aircraft: B300 (350), B300C (350C) 23
Wing Locker Lighting (WLL) Installation Weather Research Application —
Aircraft: B300 (350), B300C (350C), B200C, B200GT 10 CAPS and Hawkeye
Aircraft: C90GTi 24
Gravel Runway Kit
Aircraft: B300 (350), B300C (350C) 11 Cloud Research and Seeding System
Aircraft: B200 25
Grass Runway Supplement
Aircraft: B300 (350), B300C (350C) 12 Weather Research and LIDAR Application
Aircraft: C90GTi 26
Dirt Runway Supplement
Aircraft: B300 (350), B300C (350C) 13 SKYTRAC
Aircraft: B300 (350), B300C (350C), B200, B200C 27
Attendant Divan Seat Installation Spectrum Aeromed Air Ambulance Conversion
Aircraft: B300 (350), B300C (350C), B200GT, Aircraft: B300 (350), B300C (350C), B200, B200C, C90GTi,
B200CGT, C90GTi 28 B200GT, B200CGT, C90GT 39
Four-Place Stretcher/Divan Installation AvFab Stretcher Installation
Aircraft: B300 (350), B300C (350C), B200GT, Aircraft: B300 (350), B300C (350C), B200GT, B200CGT 40
B200CGT, C90GTi 29
Flight Inspection Modifications and Services
Two-Place Lateral Tracking
Attendant Divan Installation
Flight Inspection Installation
Aircraft: B300 (350), B300C (350C), B200GT,
Aircraft: B300 (350) 41
B200CGT, C90GTi 30
Flight Inspection System — UNIFIS 3000
Aerial Survey Modifications and Services
Aircraft: B300 (350) 42
King Air 200 Series Aft Toilet Installation
Surveillance Modifications and Services
Aircraft: B200, B200C, B200GT, B200CGT, B300, B300C 31
Radome and EO/IR Fairing
Provisions for Installation of Tandem Cameras
Aircraft: B300 (350), B300C (350C) 43
Aircraft: B300 (350), B300C (350C), B200, B200C,
B200GT, B200CGT 32
Radar Pressure Box
Aircraft: B300 (350), B300C (350C) 44
Installation of Camera Window With
Sliding Door and Drift Sight
Aircraft: C90, C90GT, C90GTi 33 EO/IR Lift
Aircraft: B300 (350), B300C (350C) 45
Provisions for Installation of Baggage Scanner
Aircraft: B300, B200GT, B200CGT 34 Bubble Window
Aircraft: B300 (350) 46
Installation Provisions for Magnetometer
Aircraft: B300 (350), B200 35 Drop Hatch
Aircraft: B300 (350) 47
Utility/Transport Modifications and Services
Maritime Surveillance Aircraft
Aircraft: B200GT 48
High-Density Seating
Aircraft: B300 (350), B300C (350C), B200, B200C, B200GT 36
Acronyms and Abbreviations 49
Aft Jump Seat
Aircraft: B300 (350), B300C (350C), B200, B200C, B200GT 37
Air Ambulance Modifications and Services
LifePort Stretcher, Patient Loading
and Support System
Aircraft: B300 (350), B300C (350C), B200, B200GT,
B200CGT, C90GT 38
Aircraft-Specific
Electrical Load
Analysis
AIRCRAFT All Models Description
An aircraft-specific electrical load
analysis (ELA) report can be developed
to assist non-OEM third parties with
post-delivery aircraft modification and
certification. An ELA lists the electrical
equipment and the associated electrical
loads on the sources of electrical
power as installed on the airplane prior
to delivery unless otherwise noted.
It shows that generator capacity is
sufficient to supply the electrical load
during day or night operations under hot
or cold day conditions while maintaining
a full charge on the aircraft batteries.
This report also calculates the length
of time each battery is able to supply
power to essential equipment during
battery-only emergency conditions.
1 General Modifications and Services
TCN-500
TACAN
Installation Kit
AIRCRAFT B300 (350), Description transmit-receive mode, air-to-air
B300C (350C) This kit installs the TCN-500 tactical air receive mode and air-to-air transmit-
navigation (TACAN) system. The TCN- receive mode.
FAA CERTIFIED Yes
500 TACAN provides distance, ground The TACAN transceiver, located in
EASA CERTIFIED No speed, time-to-station, station identifier the forward avionics compartment, is
and TACAN bearing information. interfaced with the flight displays, top
Navigation information appears on and bottom-mounted antennas, and the
both the pilot’s and copilot’s primary audio control panels. The TACAN
flight display (PFD) and multi-function system receives power through a
display (MFD) via nav source selection. 5-ampere circuit breaker.
TACAN audio selection is available on
both pilot and copilot audio panels. A
The sale and export of this equipment,
dedicated TACAN control is mounted
associated maintenance support and/or
in the cockpit pedestal. unique technical data generally require USG
The AN/ARN-153(V) supports four export license approval under the ITAR (Title
modes of operation: receive mode, 22 CFR Parts 120-130) or the EAR (Title 15 CFR
Parts 730-774).
2 General Modifications and Services
PT6A-67A
Engine
Installation
AIRCRAFT B300 (350), Description
B300C (350C) This kit installs PT6A-67A P&WC engines
in place of PT6A-60A engines. At higher
FAA CERTIFIED Yes
field elevations and hotter temperatures,
EASA CERTIFIED Yes the PT6A-67A engine provides
increased thrust over the PT6A-60A
CANADA TRANSPORT engine. This allows the aircraft increased
AGENCY Yes takeoff and climb performance from
airports with high field elevations or
airports with very high temperatures,
or a combination of both.
3 General Modifications and Services
Engine
Wash Rings
AIRCRAFT B300 (350), Description
B300C (350C) This kit provides information and parts
required to add engine wash rings to
FAA CERTIFIED Yes
Pratt & Whitney PT6A-60 and -67A
EASA CERTIFIED Yes engines. The wash rings provide an
easy method to clean the engine and
help prevent corrosion due to a salty or
other adverse environment.
4 General Modifications and Services
Engine
Wash Rings
AIRCRAFT B200 Description
This kit provides information and
FAA CERTIFIED Yes
parts required to add engine wash rings
EASA CERTIFIED No to Pratt & Whitney PT6A-41, -42 and -52
engines. The wash rings provide an easy
method to clean the engine and help
prevent corrosion due to a salty or other
adverse environment. Compressor wash
drain included for PT6A-52 engine.
5 General Modifications and Services
PT6A-60A or
-67A Engine
Compressor
Wash Drain
(CWD) Installation
AIRCRAFT B300 (350), Description
B300C (350C) The engine compressor wash drain
system provides an efficient method
FAA CERTIFIED Yes
for draining fluids from the engine
EASA CERTIFIED No casing without requiring removal of the
forward cowls. This modification reduces
the maintenance time and manpower
required to perform engine compressor/
turbine washing and rinsing.
CWD
6 General Modifications and ServicesPT6A-42 Engine
Compressor Wash
Drain (CWD)
Installation
AIRCRAFT B200, B200C Description
The engine compressor wash drain
FAA CERTIFIED Yes
system provides an efficient method
EASA CERTIFIED No for draining fluids from the engine
casing without requiring removal of the
CASA (AUSTRALIA) Yes forward cowls. This modification reduces
the maintenance time and manpower
required to perform engine compressor/
turbine washing and rinsing.
CWD
7 General Modifications and ServicesHigh Flotation
Gear Doors
AIRCRAFT B300, B300C Description Technology
(350/350ER), B200, B200C, This STC installs fully enclosed main • Fully encloses the protruding high-
B200GT (250) landing gear doors, aerodynamically flotation gear, wheels and tires.
encasing the OEM high-float gear option.
FAA CERTIFIED Yes • Aerodynamically area-ruled to
maximize drag reduction.
EASA CERTIFIED Yes • Constructed of lightweight
Benefits
composites for maximum strength
Wheel wells, tires and brakes are
and minimum weight.
kept clean and dry.
8 General Modifications and ServicesCrown Wing
Locker System
AIRCRAFT B200, Description Technology
B200GT (250), C90 This STC installs overwing storage • Lightweight composite construction
lockers and lower flap fairings, adding allows for infinite-life structural
FAA CERTIFIED Yes
storage with no performance penalty. certification.
EASA CERTIFIED Yes • Aerodynamically area-ruled to
minimize drag.
Benefits
• Fully self-contained for a clean and
• FAA certified to carry 600 pounds total dry locker interior.
cargo in 16 cubic feet of luggage space.
• Removable in minutes for any aircraft
• Accommodates skis, snowboards, maintenance or inspections.
camping gear and hunting equipment
as well as golf bags and luggage.
• Factory-installed on all new
King Air 350s.
9 General Modifications and ServicesWing Locker
Lighting (WLL)
Installation
AIRCRAFT B300 (350), Description
B300C (350C), B200C, The wing locker lighting (WLL) system
B200GT illuminates the interior of the nacelle wing
lockers to improve visibility while loading
FAA CERTIFIED No and securing items in low-light conditions.
The system is activated when the locker
EASA CERTIFIED No
is opened. Inside each locker, an on/off
CASA (AUSTRALIA) Yes switch allows the light to be turned off
when the locker is open for extended
periods, such as during maintenance or
in daylight, preventing unnecessary drain
on the aircraft’s battery.
WLL
10 General Modifications and ServicesGravel
Runway Kit
AIRCRAFT B300 (350), Description
B300C (350C) This kit provides parts and information
to install gravel guards on the inboard
FAA CERTIFIED Yes
flap, a belly anti-collision light and
EASA CERTIFIED Yes belly antennas.
The performance supplement for
gravel runways is for 15,000-pound
350/350C aircraft and 16,500-pound
350ER/350CER aircraft with no other
performance-impacting changes.
11 General Modifications and ServicesGrass Runway
Supplement
AIRCRAFT B300 (350), Description
B300C (350C) This supplement provides performance
information for takeoff and landing from
FAA CERTIFIED Yes
grass runways.
EASA CERTIFIED Yes
Note
The grass runway supplement is only for
15,000-pound 350 and 350C aircraft with
no other performance-impacting changes.
12 General Modifications and ServicesDirt Runway
Supplement
AIRCRAFT B300 (350), Description
B300C (350C) This supplement provides performance
information for takeoff and landing from
FAA CERTIFIED Yes
dirt runways.
EASA CERTIFIED Yes
Note
The dirt runway supplement is only for
15,000-pound 350 and 350C aircraft with
no other performance-impacting changes.
13 General Modifications and ServicesWet and
Contaminated
Supplement
AIRCRAFT B300 (350), Description
B300C (350C) This supplement provides performance
information for takeoff and landing from
FAA CERTIFIED Yes
wet and contaminated runways.
EASA CERTIFIED Yes
Note
The wet and contaminated runway
supplement is only for 15,000-pound
and 16,500-pound 350 and 350C
aircraft with no other performance-
impacting changes.
14 General Modifications and ServicesSpecial Mission
Rudder
Installation
AIRCRAFT B300 (350), Description
B300C (350C) This kit removes the standard rudder
and replaces it with a special mission
FAA CERTIFIED Yes
rudder. The special mission rudder has
EASA CERTIFIED No different trim-tab gearing and a larger
trailing-edge bulge for more positive
control surface self-centering. The
special mission rudder is standard
on the 350ER/350CER/300HW.
15 General Modifications and ServicesSpecial
Mission Dual
Aft Strakes
AIRCRAFT B300 (350), Description
B300C (350C) This kit installs stand-alone dual aft
special mission ventral strakes by
FAA CERTIFIED Yes
removing the Raisbeck dual aft ventral
EASA CERTIFIED Yes strakes installed by STC SA5151NM.
The purpose of this installation is to
provide additional aircraft directional
stability should this be required for
special mission applications on the
King Air B300 (350) and B300C (350C).
Performance supplement is included.
16 General Modifications and ServicesInstallation of
Baggage Door
AIRCRAFT C90, B200, Description
B300 In lieu of the standard factory OEM
cargo door option, this STC installs a
FAA CERTIFIED Yes
baggage door in the aft fuselage. The
EASA CERTIFIED Yes baggage door is 13 inches wide by 38
inches tall and retains the standard
airstair door.
17 General Modifications and ServicesDigital Audio
Control System
(DACS)
AIRCRAFT B300 (350), Description
B300C (350C) This STC provides a four-place expandable
intercommunications system (ICS) that has
FAA CERTIFIED Yes
the capacity to transmit and receive on
EASA CERTIFIED No eight radios. It is connected to the pilot
and copilot audio panels as well as up to
four audio panels in the cabin. The DACS
also has an isolate function to separate
crew from passengers. Also included is a
crew call button.
18 General Modifications and ServicesNose Ballast
Installation
AIRCRAFT B300 (350), Description
B300C (350C) This kit provides the parts and information
required to add up to 190 pounds of
FAA CERTIFIED Yes
ballast in the nose of the aircraft,
EASA CERTIFIED Yes allowing adjustment of the aircraft’s
center of gravity (CG).
BALLAST BOX
19 General Modifications and Services400-Amp
Generator
Installation
AIRCRAFT B300 (350), Description
B300C (350C) This kit provides parts and information
to upgrade the standard aircraft
FAA CERTIFIED Yes
300-amp-rated starter-generator
EASA CERTIFIED Yes system on a PT6A-60A/67A-equipped
King Air 350 with 400 amps. The 400-
amp starter generators and generator
control units (GCUs) are fully integrated
into the existing three-bus electrical
power distribution system. The kit
includes a 200-amp mission bus from
each generator. The mission buses are
controlled by a mission power switch
located in the cockpit pedestal. The
mission bus is automatically load-shed
in the event of a generator failure.
20 General Modifications and ServicesExtended
Pedestal
Installation
AIRCRAFT B300 (350), Description
B300C (350C) This installation provides a 4-inch-longer
pedestal than the standard pedestal in
FAA CERTIFIED Yes
the Beechcraft model B300 and B300C.
EASA CERTIFIED Yes
Note
This installation restricts opening of
solid forward partition stowages.
21 General Modifications and ServicesPulselite
Control System
AIRCRAFT B300 (350), Description
B300C (350C), B200, This STC installs a lighting controller
B200C, B200GT, B200CGT that pulses landing, taxi and recognition
lights. Includes a traffic collision
FAA CERTIFIED Yes avoidance system (TCAS) interface to
assist in resolution advisory (RA) and
EASA CERTIFIED No
traffic advisory (TA).
22 General Modifications and ServicesAircraft
Survivability
Equipment
(ASE) Structural
Provisions
AIRCRAFT B300 (350), Description The sale and export of this equipment,
B300C (350C) associated maintenance support and/or
These kits install structural provisions unique technical data generally require USG
for AN/AAR-47 missile warning export license approval under the ITAR (Title
FAA CERTIFIED Yes
sensors and flush-mounted AN/ALE-47 22 CFR Parts 120-130) or the EAR (Title 15 CFR
countermeasures dispensers. No line- Parts 730-774).
EASA CERTIFIED No
replaceable units (LRUs), wire harnesses,
switches, power supplies or sensors
are included with these kits. These kits
provide structure and aerodynamic
fairings for two forward sensors and two
aft sensors as well as structure for two
aft fuselage flush-mounted dispensers.
23 General Modifications and ServicesWeather
Research
Application —
CAPS and
Hawkeye
AIRCRAFT C90GTi Description A cloud aerosol and precipitation
This STC modifies a King Air C90GTi spectrometer (CAPS) probe developed
FAA CERTIFIED No by Droplet Measurement Technologies
for weather research missions. The
aircraft’s wingtips are equipped with (Boulder, CO) is mounted on the left-
EASA CERTIFIED Yes hand wingtip. One passenger seat is
hardpoints to carry various sensor
probes. The weather research probe, superseded by an operator console to
named Hawkeye, is from SPEC Inc. control CAPS measuring equipment.
(Boulder, CO) and is installed on the An Ethernet socket is integrated into
right wingtip. A 19-inch rack is installed the cupholder to provide a remote
in the baggage compartment with control via laptop for all systems. This
standard quick-change fittings into seat configuration is approved for flights into
tracks to carry the Hawkeye measuring known icing conditions.
and control systems.
24 General Modifications and ServicesCloud Research
and Seeding
System
AIRCRAFT B200 Description
This STC modifies a King Air B200 into
FAA CERTIFIED No
a cloud research aircraft with a seeding
EASA CERTIFIED Yes system. The wingtips are equipped
with hardpoints to carry special cloud
research probes manufactured by
Droplet Measurement Technologies
(Boulder, CO). Each wing has a flare rack
support to release condensation nuclei
into the clouds. Operator and equipment
racks are installed inside the cabin.
25 General Modifications and ServicesWeather
Research
and LIDAR
Application
AIRCRAFT C90GTi Description on the left-hand wingtip is shown in the
This STC modifies a King Air C90GTi photo. This multipurpose pod consists of
FAA CERTIFIED No a laser scanner, camera, data recorder,
into an airborne laboratory for
atmospheric environmental research. inertial measurement unit (IMU) and
EASA CERTIFIED Yes computer-controlled navigation system
The modification includes a weather
research sensor probe and a light (CCNS4). The entire system combines
detection and ranging (LIDAR) system aircraft guidance, mission planning and
for 3-D geo-referencing. The aircraft direct geo-referencing. A quick-change
is equipped on both wingtips with interconnection panel is provided inside
hardpoints to carry various systems so the pylon feet on the wingtip for an easy
that different configurations are possible. system change.
The LIDAR from RIEGL (Horn, Austria)
26 General Modifications and ServicesSKYTRAC
AIRCRAFT B300 (350), Description
B300C (350C), B200, B200C This STC installs the ISAT-100, ISAT-
200R or ISAT-200A flight following/
FAA CERTIFIED Yes
satcom system, which comprises the
EASA CERTIFIED Yes CDP-300, DVI-300, antenna and all
associated wiring.
27 General Modifications and ServicesAttendant Divan
Seat Installation
AIRCRAFT B300 (350), Description
B300C (350C), B200GT, This STC installs an attendant divan
B200CGT, C90GTi seat on the existing seat rails opposite
a stretcher. The seat can be one-place,
FAA CERTIFIED Yes two-place or three-place. Optional
under-seat stowage drawers are
EASA CERTIFIED Yes
available. Removal of the sidewall
armrest and tables is required to
facilitate installation. On the B300,
installation also requires removal of
the two center pyramid cabinets.
28 General Modifications and ServicesFour-Place
Stretcher/Divan
Installation
AIRCRAFT B300 (350), Description
B300C (350C), B200GT, This installs a four-place stretcher/
B200CGT, C90GTi divan on the existing seat rails. The
stretcher/divan quickly and easily
FAA CERTIFIED Yes converts between passenger and patient
configurations. You can carry passengers
EASA CERTIFIED No
on one leg of a flight and then convert
it for an ambulatory person on the next
leg. Occupancy in either configuration
is FAA-approved during all phases
of operation. Removal of the sidewall
armrest and tables is required to facilitate
installation. On the B300, installation
also requires removal of the two center
pyramid cabinets.
29 General Modifications and ServicesTwo-Place
Lateral Tracking
Attendant Divan
Installation
AIRCRAFT B300 (350), Description
B300C (350C), B200GT, This installs a two-place lateral tracking
B200CGT, C90GTi attendant divan on the existing seat
rails. The divan allows seated passenger
FAA CERTIFIED Yes attendants 3 inches of lateral mobility
for improved patient access, without
EASA CERTIFIED Yes
having to unbuckle the restraint system.
Optional under-seat stowage drawers
are available. Removal of the sidewall
armrest and tables is required to
facilitate installation.
30 General Modifications and ServicesKing Air 200
Series Aft Toilet
Installation
AIRCRAFT B200, B200C, Description
B200GT, B200CGT, B300, The STC installs an aft toilet in King Air
B300C 200/300 series aircraft. It is also eligible
as a passenger seat for occupancy
FAA CERTIFIED Yes during all phases of aircraft operation.
The STC includes oxygen, air and light
EASA CERTIFIED Yes
for the toilet seat.
31 Aerial Survey Modifications and ServicesProvisions for
Installation of
Tandem Cameras
AIRCRAFT B300 (350), Description requires the relocation of selected
B300C (350C), B200, This STC installs structural provisions for aircraft environmental control system
B200C, B200GT, B200CGT single or dual cameras in the fuselage components that are installed in a
cabin area of the aircraft. The provisions cabinet either just aft of the copilot chair
FAA CERTIFIED Yes support a multitude of sensors including or in the aft right-hand baggage area.
digital mapping cameras (medium and The STC also supports the install of
EASA CERTIFIED Yes
large format), as well as LIDAR and a retractable electro-optical infrared
hyperspectral systems. Installation (EO/IR) turret in either camera well
includes doors to mitigate FOD damage with an associated pressure dome
to the installed sensor during takeoff, in the cabin.
landing and taxi operations. Installing
the forward camera well provisions
32 Aerial Survey Modifications and ServicesInstallation of
Camera Window
With Sliding Door
and Drift Sight
AIRCRAFT C90, Description
C90GT, C90GTi This STC installs structural provisions for
a single camera window in the mid-cabin
FAA CERTIFIED Yes
area of the C90. The camera window
EASA CERTIFIED Yes supports medium- and large-format film
or digital mapping cameras, scanners
and LIDAR sensors. Provisions include a
sliding door to mitigate FOD damage to
the sensor lens during takeoff, landing
and taxi operations. An optional drift
(navigation) sight is also available. A
retractable EO/IR turret with pressure
dome can also be installed.
33 Aerial Survey Modifications and ServicesProvisions for
Installation
of Baggage
Scanner
AIRCRAFT B300, B200GT, Description
B200CGT This STC installs structural provisions
for selected medium-format cameras
FAA CERTIFIED Yes
or scanners on the right-hand side of
EASA CERTIFIED No the King Air baggage compartment.
Provisions can include a pressure
dome if required.
AFT SENSOR LOCATION
WITH PRESSURE BOX
34 Aerial Survey Modifications and ServicesInstallation
Provisions for
Magnetometer
AIRCRAFT B300 (350), Description
B200 This STC installs provisions for a
magnetometer boom on the aft
FAA CERTIFIED Yes
fuselage area.
EASA CERTIFIED No
BOOM
35 Aerial Survey Modifications and ServicesHigh-Density
Seating
AIRCRAFT B300 (350), Description
B300C (350C), B200, This STC installs up to nine high-density
B200C, B200GT seats in the B200 aircraft, and up to
13 in the 350 aircraft, not including an
FAA CERTIFIED Yes aft toilet or aft jump seat. A flight data
recorder is required to be installed with
EASA CERTIFIED Yes
this installation on B300 aircraft.
36 Utility/Transport Modifications and ServicesAft Jump Seat
AIRCRAFT B300 (350), Description
B300C (350C), B200, This STC installs an aft jump seat (left-
B200C, B200GT hand, right-hand or dual) and includes
the necessary seat(s), occupant restraint
FAA CERTIFIED Yes system, attachment feet, oxygen drop-
down system, overhead lights and
EASA CERTIFIED Yes
overhead vents.
37 Utility/Transport Modifications and ServicesLifePort
Stretcher, Patient
Loading and
Support System
AIRCRAFT B300 (350), Description • One vacuum system, 28 VDC,
B300C (350C), B200, This STC installs a complete air rated at 559 millimeters of mercury
B200GT, B200CGT, C90GT ambulance system including a stretcher, with gas outlet
patient loading system and life support • One compressed air system
FAA CERTIFIED Yes systems. AeroSled TS PLUS Patient
• One remote oxygen fill port
Handling Systems are installed with the
EASA CERTIFIED Yes • Other equipment is available as
following medical components in
each system: options under this STC
• One or two 3,500-liter oxygen bottle • King Air 350: one or two stretchers
systems with free-flowing gas outlet • King Air 250: one or two stretchers
(providing approximately 3.8 hours of
• King Air 90: one stretcher
oxygen at 15 LPM)
• One output delivering 1,000 watts,
115 VAC, 50 hertz, 8.2 amps (or 1,000
watts, 230 VAC)
38 Air Ambulance Modifications and ServicesSpectrum
Aeromed Air
Ambulance
Conversion
AIRCRAFT B300 (350), Description • Electrical supply: one 28-volt DC
B300C (350C), B200, This STC installs a Spectrum Aeromed outlet and two 115-volt AC outlets,
B200C, C90GTi, B200GT, air ambulance system, including or four 230-volt AC outlets (in ALS
B200CGT, C90GT stretchers and life support systems. systems only)
Optional MedWall can be provided with • Inverter: several 115-volt AC and 230-
FAA CERTIFIED Yes the following stretcher installations: volt AC options (in ALS systems only)
EASA CERTIFIED Yes • King Air 350: one or two stretchers • Oxygen supply: 3,500 liters
• King Air 250: one or two stretchers
• King Air 90: one stretcher
• Dual air pumps: 11 LPM at 50 psi (in ALS
systems only)
• Vacuum pump: 14 LPM at 14 inches of
mercury (in ALS systems only)
39 Air Ambulance Modifications and ServicesAvFab Stretcher
Installation
AIRCRAFT B300 (350), Description
B300C (350C), B200GT, This installation consists of a stretcher on
B200CGT the seat rails. Generally it requires that
the cabin sidewall armrests and tables be
FAA CERTIFIED Yes removed. A version is available that allows
retention of standard cabin sidewalls
EASA CERTIFIED No
and tables. The aft cabin partition with
sliding doors must be removed to facilitate
loading and unloading the stretcher with a
patient on board.
40 Air Ambulance Modifications and ServicesFlight Inspection
Installation
AIRCRAFT B300 (350) Description flight inspection system comes with
The modification consists of installing an integrated advanced autopilot
FAA CERTIFIED No interface, which increases flight and
Aerodata’s AeroFIS flight inspection
system into B300 aircraft equipped measurement accuracy, minimizes the
EASA CERTIFIED Yes cockpit workload and provides better
with a full set of flight inspection
antennas. The AD-AFIS system dynamic steering for perfectly following
provides established radio navigation the selected flight inspection track.
systems and the ability to inspect
advanced automatic dependent The sale and export of this equipment,
surveillance-broadcast (ADS-B) and associated maintenance support and/or
area navigation (RNAV) procedures. unique technical data generally require USG
export license approval under the ITAR (Title
A cockpit information display (CID) 22 CFR Parts 120-130) or the EAR (Title 15 CFR
shows pilots the flight inspection Parts 730-774).
profile and the way to intercept this
profile. The fully automatic AeroFIS
41 Flight Inspection Modifications and ServicesFlight Inspection
System —
UNIFIS 3000
AIRCRAFT B300 (350) Description The sale and export of this equipment,
associated maintenance support and/or
With the UNIFIS System from Norwegian unique technical data generally require USG
FAA CERTIFIED No
Special Mission, the King Air B300 is export license approval under the ITAR (Title
EASA CERTIFIED Yes modified for flight inspection purposes. 22 CFR Parts 120-130) or the EAR (Title 15 CFR
The installation consists of multiple Parts 730-774).
antennas, an optional flight inspection
operator console (FIOC), optional flight
inspection data analysis rack (FIDAR),
laser altimeter, camera, inertial reference
system (IRS) and course direction
indictor (CDI) to meet the defined tasks.
The modification provides a seat rail
adapter (SRA) and interconnection panel
for quick release and easy maintenance
of the system.
42 Flight Inspection Modifications and ServicesRadome and
EO/IR Fairing
AIRCRAFT B300 (350), Description In order to facilitate this installation,
B300C (350C) This modification provides an the following modifications are
aerodynamic belly radome that covers typically included:
FAA CERTIFIED Yes
the installed radar and its associated • Relocated antennas
EASA CERTIFIED Yes electronics, as well as an aerodynamic
• Relocated and additional anti-
fairing that encompasses the EO/IR
collision light
system to mitigate parasitic drag. The
two-piece belly-mounted radome is • Relocated radio altimeters
provided in X- or Ku-band. The EO/IR • Manual supplements
fairing is attached to the aft portion of
• Some configurations include special
the radome on the lower fuselage
mission rudder installation
of the aircraft.
• Special mission rudder and strakes
The sale and export of this equipment,
associated maintenance support and/or
unique technical data generally require USG
export license approval under the ITAR (Title
22 CFR Parts 120-130) or the EAR (Title 15 CFR
Parts 730-774).
43 Surveillance Modifications and ServicesRadar
Pressure Box
AIRCRAFT B300 (350), Description
B300C (350C) In conjunction with the radome and
EO/IR fairing installation, this installation
FAA CERTIFIED Yes
adds a pressure box vessel. The
EASA CERTIFIED Yes pressure box has unobstructed
dimensions of 12.7 inches forward to aft,
12.3 inches left to right and 7.7 inches
deep, giving a minimum usable volume
of 1,214 cubic inches.
The sale and export of this equipment,
associated maintenance support and/or
unique technical data generally require USG
export license approval under the ITAR (Title
22 CFR Parts 120-130) or the EAR (Title 15 CFR
Parts 730-774).
44 Surveillance Modifications and ServicesEO/IR Lift
AIRCRAFT B300 (350), Description operator’s console, if desired. This
B300C (350C) This installs a lift for an EO/IR camera system will accommodate a sensor up
system in the belly-mounted radome. to 18 inches in diameter and weighing
FAA CERTIFIED Yes up to 135 pounds.
The kit also modifies the center cockpit
EASA CERTIFIED Yes pedestal to install the EO/IR lift control
panel. This control panel allows the
Note
pilot to lift and lower the EO/IR lift/
turret (when installed) and also gives This lift must be used concurrently with
an indication of the lift’s position via radome and EO/IR fairing lift.
indicator lights. Logic is added to the
landing gear handle position system
The sale and export of this equipment,
so that when the contact is broken
associated maintenance support and/or
(moving the landing gear handle to the unique technical data generally require USG
DN position), the lift system, if down, will export license approval under the ITAR (Title
stow automatically. Wiring provisions 22 CFR Parts 120-130) or the EAR (Title 15 CFR
are located in the cabin for installation Parts 730-774).
of an EO/IR lift control panel in the
45 Surveillance Modifications and ServicesBubble Window
AIRCRAFT B300 (350) Description In order to facilitate this installation,
Two bubble windows, approximately the following modifications are
FAA CERTIFIED Yes typically included:
17 inches wide, 22 inches high and
EASA CERTIFIED Yes extending out from the fuselage, • Special mission strakes
are installed in the aft cabin
compartment, one on each side.
These windows facilitate low altitude Note
visual observation during search and NOT applicable to cargo aircraft.
rescue operations. The windows are
independently defogged with heated
air. The windows are comprised of
laminated stretched acrylic.
46 Surveillance Modifications and ServicesDrop Hatch
AIRCRAFT B300 (350) Description Note
This kit installs a drop hatch that NOT applicable to cargo aircraft.
FAA CERTIFIED Yes
allows an operator to drop surveillance
EASA CERTIFIED Yes or rescue equipment. The drop hatch
is located on the right side of the
aircraft between FS312 and FS339.
The diameter of the drop hatch is
approximately 20 inches and has a
separate integral hatch to drop dye
markers. There is a safety restraint
added for the person opening the
hatch. An annunciator alerts the flight
crew when the drop hatch is opened
or not latched securely.
47 Surveillance Modifications and ServicesMaritime
Surveillance
Aircraft
AIRCRAFT B200GT Description station. To enhance cabin/crew
The modification consists of the communication, cockpit links are
FAA CERTIFIED No provided to transfer mission flight plans,
installation of a belly-mounted radome
with integrated EO/IR elevator, a drop mission video streams and moving
EASA CERTIFIED Yes map data in the cockpit. The King Air
hatch and bubble windows, and the
integration of Aerodata’s AeroMission can be operated up to an extended
mission management system into King takeoff weight of 14,000 pounds in the
Air B200 aircraft. AeroMission provides restricted category.
situational awareness for maritime patrol
aircraft (MPA) missions by integrating a The sale and export of this equipment,
360-degree bell-mounted search radar, associated maintenance support and/or
an EO/IR camera system, direction- unique technical data generally require USG
finding and data/voice communication export license approval under the ITAR (Title
equipment into one operator work 22 CFR Parts 120-130) or the EAR (Title 15 CFR
Parts 730-774).
48 Surveillance Modifications and ServicesAcronyms and
Abbreviations
A Amperes ITAR International Traffic in
Arms Regulations
AFMS Airplane flight manual
supplement LB U.S. pounds (unit of weight)
CAPS Cloud aerosol and LIDAR Light detection and ranging
precipitation spectrometer
LPM Liters per minute
EASA European Aviation
Safety Agency MM Millimeters (unit of length)
FAA Federal Aviation MTOW Maximum takeoff weight
Administration
MPA Maritime patrol aircraft
FAR Federal Aviation Regulation
STC Supplemental type certificate
FDR Flight data recorder
TBD To be determined
FOD Foreign object debris
VAC Volts of alternating current
ISR Intelligence, surveillance
and reconnaissance VDC Volts of direct current
DISCLAIMER
This document is intended to provide information for evaluation of equipment offered by Textron Aviation Special Missions and
third-party suppliers. Whereas Textron Aviation makes every effort to ensure that the data contained in this catalog is accurate,
it is not intended to be a formal declaration of performance or equipment specification.
Textron Aviation makes no warranty or guarantee that any particular modification will meet the needs of the customer. The
customer shall rely on his or her own judgment and expertise in determining whether a modification is appropriate for the
aircraft and the mission.
Although each of the individual items offered in the catalog may have its own airworthiness approval, the installation of
multiple modifications could result in a requirement for additional evaluation to ensure airworthiness of the modified aircraft.
Textron Aviation reserves the right to modify, supersede, cancel or declare obsolete any item, configuration or specification
within this catalog without prior notice.
49U. S . + 1 . 8 0 0 . 4 5 6 . 3 5 8 0 | I N T E R N AT I O N A L + 1 . 3 1 6 . 5 1 7. 8 2 7 0 | S P E C I A LM I S S I O N S .T X TAV.C O M
Member of General Aviation Manufacturers Association. © 2018 Textron Aviation Inc. All rights reserved. The names of some aircraft manufactured by Textron
Aviation Inc. (“TAI”) or formerly Cessna Aircraft Company and Beechcraft Corporation, including Hawker aircraft, and the names of some TAI products or
services, whether or not appearing in large print with trademark symbols or otherwise denoting rights to or ownership of the same, are trademarks or service
marks of Textron Aviation Inc. or an affiliate and may be registered in the United States. Third-party product names, marks, etc., whether or not appearing in
large print with trademark symbols or otherwise denoting rights to or ownership of the same, are trademarks or service marks of others.
The sale and export of some configurations of Special Mission aircraft as well as the associated maintenance support and unique technical data generally
require USG export license approval under the ITAR (Title 22 CFR Parts 120-130) or the EAR (Title 15 CFR Parts 730-774).
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