Garmin CARAVAN 675 User Manual
Optional Equipment
Selection Guide
Effective for G1000 Equipped Aircraft to be Delivered in 2009 & 2010
Printed June 2009
Revision A
OPTIONAL EQUIPMENT SELECTION GUIDE
EFFECTIVE FOR G1000 EQUIPPED AIRCRAFT TO BE DELIVERED IN 2009 & 2010
REVISION A
PRINTED JUNE 2009
Caravan Marketing
Cessna Aircraft Company
P.O. Box 7704
Wichita, Kansas 67277-7704
Telephone (316) 517-5667
Fax (316) 517-7250
2
For G1000 Equipped Aircraft Delivered in 2009 & 2010
NOTE: OPTIONAL EQUIPMENT AND VENDORS ARE SUBJECT TO CHANGE WITHOUT NOTICE.
AIRCRAFT PROFILE
STANDARD EQUIPMENT
AIRCRAFT CERTIFICATION AND OPERATIONAL APPROVAL
Aircraft Certification: If the Purchaser elects to meet the certification criteria other than those required for U.S. F AAFAR
23–Normal category (day, night, VFR, IFR), compliance may necessitate airframe modifications and additional systems. Certification Kits are, or will be, available to meet the type design requirements set forth by the relevant civil
authority, at an additional charge.
Aircraft Operating Approval: The Purchaser is responsible for obtaining Aircraft operating approval from the relevant civil
aviation authority. Additional equipment or airframe modifications, dependent upon the location and planned operations,
may be identified by that authority (various regions within one country may have differing requirements).
International Certification: The Purchaser must furnish to Cessna the country of Aircraft registration, a properly
assigned or designated aircraft registration with the applicable Artex ELT and Mode S code identification, and any additional equipment or systems (if different from those mandated by the FAA for a similar operational category) required
for the category of registration intended (e.g., private, commercial).
The Purchaser is responsible for added Aircraft modifications and associated expense to comply with operational
requirements. International Certification Kit information is available upon request.
AIRCRAFT EQUIPMENT REGISTRATION
The Purchaser must furnish to Cessna from the relevant civil aviation authority, the binary code and country protocol
for operation of the Artex ELT and the binary Mode S Transponder.
AVIONICS:
Standard Avionics Kit (includes Two
Headsets)
Garmin G1000 System includes:
GDU 1040A Pilot & Co-Pilot Primary Flight
Display (PFD)
GDU 1040A Multi Function Display (MFD)
GIA 63W Dual Com/Nav/GPS (WAAS)
GDC 74A Dual Air Data Computer (ADC)
GEA 71 Engine/Airframe Unit
GRS 77 Dual Attitude and Heading
Reference System (AHRS)
GFC 700 with GMC 710 Mode Controller,
Three Axis Automatic Flight Control
System (AFCS) with Integrated Pitch Trim
GMA 1347 Single Audio System with
Integrated Marker Beacon Receiver
GTX 33 Mode S Transponder, Non-
Diversity
Garmin Relative Terrain/Obstacles, Garmin
Flight Charts (No Geographic Aircraft
Overlay), Garmin SafeTaxi (Domestic
Only)
KN-63 DME
Switch, Avionics Power (Two) (On-Off)
Artex ME-406 2-Frequency (Non-Nav
Interfaced) ELT with Remote Switch and
Monitor Light (Dorsal Fin Installation)
Avionics Cooling, (2) cowl deck fans and
(3) display fans
PASystem with Aft Cabin Speakers
ENGINE INDICATION SYSTEM (EIS)
Displayed on MFD During Normal
Operations:
Engine and System Displays - Show
numeric readouts of critical engine, fuel
and electrical indications and calcula-
tions for the following:
Torque
Interstage Turbine Temperature
Gas Generator Speed
Propeller Speed
Oil Pressure
Oil Temperature
Fuel Quantity
Fuel Flow
Ammeter/Voltmeter
Standby Engine Instrument:
Engine Torque Gauge, Wet Type
Altair Digital ADAS Engine Trend
Monitoring System
FLIGHT INSTRUMENTS:
Indications Displayed on each PFD:
Airspeed
Attitude with Slip/Skid Indication
Altitude
Vertical Deviation, Glideslope and Glidepath
Vertical Speed
Horizontal Situation Indication
Outside Air T emperature
System Time
Generic Timer
Wind Data
Standby Flight Instruments:
Airspeed Indicator
Attitude Gyro
Altimeter
Magnetic Compass
Heated Pitot System, Pilot & Co-Pilot
Alternate Static Source
Static Source Drains
Instrument Static System
Second Independent Pitot-Static System
FLIGHT CONTROLS:
Brake, Parking
Brakes, Hydraulic, Toe-Operated
Control Cables — Corrosion Resistant Steel
Printed June 2009
3
NOTE: OPTIONAL EQUIPMENT AND VENDORS ARE SUBJECT TO CHANGE WITHOUT NOTICE.
STANDARD EQUIPMENT
Control Lock, Ailerons and Elevator
Flight Control System, Pilot & Co-Pilot
(Includes All-Purpose Control Wheel, Pedals
and Toe Brakes)
Friction Lock, Engine Controls
Powerplant, Quadrant Type Controls:
Condition Lever
Primary Engine Power
Back-up Engine Power ( Emergency Power
Lever)
Propeller, Speed and Feather
Rudder, Extended Chord
Rudder Gust Lock
Trim System, Aileron/ Rudder (Manual),
Elevator (Manual & Electric Pilot & Co-Pilot)
Wing Flaps, Electric Pre-Select with Standby
Motor
ENVIRONMENTAL:
Defroster, Windshield (Pilot and Copilot)
Heating System, Cabin (Bleed Air Type)
Soundproofing
Ventilation System, Cockpit (Ram Air)
Ventilator , Adjustable, Cabin Air
Ventilation System, Fan Driven
ELECTRICAL POWER:
Battery, 24 Volt, 38 Amp/Hr, Sealed Lead-
Acid
Battery Switch (On-Off)
Circuit Breakers, Electrical
Generator Switch (Trip-On-Reset)
Ground Service Plug Receptacle
Starter/Generator, 200 Amp
Generator Control Unit
Generator Control Unit Mounting
(Provisions for Mounting Standby Unit)
Power Outlet, 12V Cockpit
Standby Electrical System, 75 amp
EXTERIOR LIGHTS:
Beacon – Omni Flash (Red)
Courtesy, Under Wing
Wing Ice Detection, LH
Landing, L.H. & R.H. (Wing Leading Edge-
Outboard)
Navigation (3)
Strobe (2) Wing Tip Mounted
Taxi, L.H. & R.H. (Wing Leading Edge-
Inboard)
INTERIOR LIGHTS:
LED Backlit Instrument Panel Lighting
Map Light, Control Wheel Mounted, Pilot & Co-
Pilot (Variable Intensity)
Overhead Courtesy (3) (Aisle, Aft Cargo
Area and Passenger Door)
Overhead Flood (Pilot and Copilot) (3)
Passenger Reading Lights (10)
Dimming Controls, Switch Panel, Avionics
Circuit Breaker Panel, Left Hand Panel &
Environmental Panel
POWERPLANT:
Chip Detector Installation
Cowling, Rigid-Mounted (Quick
Removable) Lower and Easily Openable
Upper Sides
Cowl Locks, Medco
Engine Inlet Cover (2) and Propeller Tie-
Down Sleeve
Engine, Turboprop PT6A-114A, 675 SHP,
3600 TBO
Engine Wash Ring (Integral)
Engine Support, Vibration Isolation
Filter, Integral, Full Flow Oil
Fire Detection System, Engine
Compartment
Ignition System Excitor Unit Mounting
(Provisions for Mounting Standby Unit)
Ignition System (Dual Ignitors)
Intake Inertial Separator (Manual)
Oil Cooler, High Capacity
Overspeed Governor
Propeller, Anti-Ice, Electric, 3 Blade
Aluminum, Constant Speed, Full
Feathering, Reversible – McCauley
Propeller Governor
Propeller Spinner (Polished)
Shielding, Engine Ignition
Shutdown Fuel Collector, Engine
Valve, Oil Quick Drain
FUEL SYSTEM:
Fuel Boost Switch, Auxiliary
Fuel Caps with Anti-Siphon Doors
Fuel Control Heater, Engine
Fuel Filling Ports, (4)
Fuel Filter with Quick Drain
Fuel Low Level Warning System
Fuel Pump, Auxiliary (Electric)
Fuel Pump, Engine
Fuel Reservoir with Quick Drain
Fuel Selector Valves
Fuel Shutoff Valve
Fuel Tanks, 332 Gallons Usable
Fuel Valves, Quick Drain (8)
Fuel Vents, Non-Icing
Fuel Sampler Cup
INTERIOR:
Aircraft Keys
Approach Plate Holder, L.H. & R.H.
Baggage Area Partition Net
Baggage Tie-Down Straps (4)
Beverage Cup Holders (Pilot and Copilot)
Cargo Tie-Down Fittings Provisions
Cargo Tie-Down Fittings (Baggage Area)
Checklist, Pilot’s (Laminated)
Corrosion Proofing, Internal
Crew Door Storage Area LH, RH
Fire Extinguisher Cabin– Hand Type
Floor Covering, Lightweight Vinyl
Glareshield, Padded
Handbook, Customer Care, Includes
Engine/Flight Logs, Warranty, Etc.
Handbook, Pilot's Operating
Headliner – Vinyl
Hooks, Clothes Hanger
Instrument Panel – Metal
Map/Glove Compartment
Oxygen System, Partial Installation
(Consists of Difficult to Install Plumbing)
Passenger Door Cables, 2 Sets
Pilot and Copilot Restraint – Integral 5 Point
Lap and Shoulder Harness with Inertial
Reel
Plotter, Weight & Balance (Cargo &
Passengers)
Pilot’s LH Pre-Flight Assist Handle
Recorder, Flight Hour
Relocated Microphone Installation
Seats, Pilot & Copilot, Adjustable Fore, Aft
and Vertical with Articulating Recline and
Arm Rest
Sign, Fasten Seat Belts & No Smoking
Steps, Cabin Entrance, Retractable (LH &
RH Crew Entry Door)
Sunvisors, Rosen
Window, Foul Weather, Pilot Door
Windows Tinted All-Around
EXTERIOR:
Anti-Precipitation Static Kit
Bonding Straps, Control Surface (Aileron,
Elevator and Rudder)
Cargo Pod Provisions with Straight Stack
Corrosion Proofing, External
Door, Cargo, Two-Piece (Left Side of
Aircraft, with Upper Door Unlocked
Annunciator Light)
Door, Copilot (Full Opening)
Door, Pilot (Full Opening)
Door, Passenger with Airstair Feature
(Right Side of Aircraft with Upper Door
Unlocked Annunciator Light)
Hoisting Rings
Jack Points (Fuselage and Main Landing
Gear)
Landing Gear, Fixed, Nose, Steerable
Landing Gear, Fixed, Main
Lock, Key-Operated (One Key Fits All
Doors)
Paint, All Over (Modified Polyurethane)
Stabilizer Abrasion Boots
Stall Warning System, Heated
Tires, 8.50 x 10, 8 Ply Main, 22 x 8.00, 6 ply
Nose With Extended Nose Gear Fork
Tie-Down Rings, Aircraft
Tow Bar
4
For G1000 Equipped Aircraft Delivered in 2009 & 2010
NOTE: OPTIONAL EQUIPMENT AND VENDORS ARE SUBJECT TO CHANGE WITHOUT NOTICE.
FLIGHT DECK
Estimated
Weight (lbs)
Warranty
(Years)
Price
(USD)
655B
690K
624H
629U
GARMIN G1000 OPTIONS
Jeppesen Chart View (Exchange for Garmin Flight Charts)
ChartView resembles the paper version of Jeppesen terminal procedures
charts. The charts are displayed in full color with high-resolution. The MFD
depiction shows the aircraft position on the moving map in the plan view
of the approach charts and on airport diagrams. Available data includes
Arrivals (STAR), Departure Procedures (DP), Approaches, Airport
Diagrams and NOTAMS. Requires Jeppesen Database Subscription
Service.
NOTE:
The availability of the optional Jeppesen ChartView or standard Garmin FlightCharts and SafeTaxi in electronic form does not
preclude the requirement to carry paper charts aboard the aircraft.
See AC 120-76A for more information.
Synthetic Visual Technologies (SVT)
Position sensors on the aircraft integrate with a high resolution terrain
database to present synthetic terrain imagery on the Primary Flight
Display. Flight information is overlaid to provide greater safety and situational awareness.
GTX-33 Mode S Transponder, 2nd Unit
Adds a second GTX-33 Mode S Transponder, non-diversity, additional single
antenna
WEATHER, TRAFFIC AND TERRAIN AVOIDANCE SYSTEMS
Garmin GWX 68 - 4 Color Digital Weather Radar
The Garmin GWX 68 Airborne Color Weather Radar is a four-color digital
pulsed radar that combines excellent range and adjustable scanning profiles with a high-definition target display. The Caravan uses a 12-inch
phased array antenna that is fully stabilized to accommodate 30 degrees
of pitch and roll. Sector Scanning offers pilot-adjustable horizontal scan
angles and a vertical scanning function helps to analyze storm tops, gradients, and cell build-up at various altitudes.
$4,350
$20,500
$6,525
$26,525
0.0 2
0.0 2
5.71 2
15.85 2
EST. STD. EMPTY WEIGHT:
4239 LBS.
MAX. RAMP WEIGHT: 8035 LBS.
2009 LIST PRICE $1,778,200.00
2010 LIST PRICE $1,831,600.00
List Price F.A.F. (Fly Away Factory)
Wichita, Kansas, U.S.A.
Printed June 2009
5
NOTE: OPTIONAL EQUIPMENT AND VENDORS ARE SUBJECT TO CHANGE WITHOUT NOTICE.
FLIGHT DECK
Standard Garmin G1000 Avionics Package (Options also pictured.)
6
NOTE: OPTIONAL EQUIPMENT AND VENDORS ARE SUBJECT TO CHANGE WITHOUT NOTICE.
Estimated
Weight (lbs)
Warranty
(Years)
Price
(USD)
For G1000 Equipped Aircraft Delivered in 2009 & 2010
FLIGHT DECK
650C
632K
629R
635Q
673A
632B
668N
675W
Garmin TAWS-B
The Garmin TAWS (Terrain Awareness and Warning System) is an optional feature to increase situational awareness and aid in reducing controlled
flight into terrain (CFIT). TAWS satisfies TSO-C151b Class B requirements
for certification. T A WS provides visual and aural annunciations when terrain
and obstacles are within the given altitude threshold from the aircraft. Class
B TAWS is required for all Part 91 aircraft operations with six or more
passenger seats and for Part 135 turbine aircraft operations with six
to nine passenger seats (FAR Parts 91.223, 135.154.)
XM Satellite Weather/Entertainment
XM Satellite Weather data provides information for avoiding hazardous
weather. Graphical weather information and associated text is received on
the GDL 69Aremote-mounted data link satellite receiver and is displayed on
the MFD and the PFD Inset map. The GDL 69A can also receive XM
Satellite Radio entertainment services. Includes FK 675W, 4-place intercom
in cabin. Domestic Customers Only. Requires Subscription Service.
L-3 Communications Stormscope Model WX-500
WX-500 detects electrical discharges associated with thunderstorms within a 200 nm radius of the aircraft. In “Normal” mode displays on the MFD.
Can be configured to display on PFD inset map.
KTA 870 Traffic Advisory System (Bendix King)
The KTA 870 TAS actively interrogates other transponder-equipped traffic
and will display and warn of aircraft that pose a potential conflict. Meets
FAATSO C147 for traffic advisory systems.
GENERAL AVIONICS
KRA 405B Radar Altimeter
Gives an absolute altitude indication from 2000 to 0 feet AGL. Provides selection of warning altitude, and annunciation via both a decision height light and an
aural warning.
KHF-1050 High Frequency Transceiver
The KHF-1050 High Frequency Transceiver includes a compact digital controller that provides advanced squelch features, enhanced channel storage,
and quicker tuning.
KR 87 ADF (Bendix King) Displayed on PFD w/Stand Alone Control
Displayed as a pointer on the HSI on the pilot’s and co-pilot’s PFD.
Cabin Intercom - Four (4) Position
Cabin intercom jacks located two (2) on Left-Hand and two (2) on RightHand lower sidewalls. (Includes four (4) headsets).
0.0 2
4.03 2
4.89 2
17.0 2
5.21 2
44.74 2
6.32 2
.60 2
$8,550
$7,550
$10,150
$29,200
$20,850
$63,750
$8,625
$2,000
Printed June 2009
7
NOTE: OPTIONAL EQUIPMENT AND VENDORS ARE SUBJECT TO CHANGE WITHOUT NOTICE.
Estimated
Weight (lbs)
Warranty
(Years)
Price
(USD)
GENERAL
175H
161A
16D
02B
60N
60P
EMERGENCY LOCATOR TRANSMITTER
C 406-N 3 Frequency ELT (Exchange)
Replaces the standard Artex ME-406 2-Frequency (Non-Nav Interfaced) ELT.
A three frequency ELT that transmits on the International Emergency
Frequencies and the satellite frequency of 406 MHz. The EL Twill transmit the
aircraft information and position coordinates. Note: This system requires customer registration at time of delivery with NOAAfor recognition of the 406 MHz
transmission. May be required for country certification or operational requirements. Purchaser must furnish 24-bit code provided by registering
country’s aviation authority.
ELECTRICAL AND LIGHTING
12V DC Power Outlets (2), Cabin
Two automotive-style receptacles providing up to 138 watts. One receptacle
each side located at mid-ship.
300 Amp Starter/Generator (Exchange)
Replaces the standard 200 amp starter/generator. A 28 volt, 300 amp
engine-driven unit that functions as a motor for engine starting and, after
engine start, as a generator for the airplane electrical system.
ENVIRONMENTAL
Air Conditioning, Cabin System
This R-134A system is engine driven and includes two wing evaporators
and one tailcone evaporator. Meets FAA & CAA Requirements.
Oxygen System, Complete 13 Port System
The system includes a 115 cu. ft. composite bottle, 13 oxygen outlets and
13 partial rebreathing type oxygen masks. Two masks are equipped with a
microphone. (Fourteenth oxygen port available by SER at additional
charge).
Oxygen System, Complete 8 Port System
For Use With Oasis Interior Only
The system includes a 1 15 cu. ft. composite bottle, eight oxygen outlet s and
eight partial rebreathing type oxygen masks. Two masks are equipped with
a microphone for use by the crew. (
Requires CRQ to delete center and first
cabin row PSUs.)
$9,850
$1,300
$5,100
$21,150
$9,900
$9,700
2.33 2
2.0 2
17.0 2
118.0 2
39.5 2
37.0 2
8
For G1000 Equipped Aircraft Delivered in 2009 & 2010
NOTE: OPTIONAL EQUIPMENT AND VENDORS ARE SUBJECT TO CHANGE WITHOUT NOTICE.
Estimated
Weight (lbs)
Warranty
(Years)
Price
(USD)
GENERAL
22V/W
2S
91S
06W
ICING EQUIPMENT
TKS Anti-Ice System, Certified for Flight In Icing Conditions
The TKS anti-icing system incorporates porous panels attached to the exterior
leading edge of the wings, wing struts, and empennage. The system contains a
twenty gallon tank, two fluid pumps, windsheild pump, timer/controller, filters,
fluid level sensors, high pressure switch and low fluid level switch. A propeller
slinger system provides protection for the propeller, windshield and cargo pod.
Includes windshield ice detector light. The wing ice detection light and two (2)
heated pitot/static probes are installed as standard equipment.
(Weight does
not include fluid @ 184 lbs.) (Option available at serial number 20800518.)
MISCELLANEOUS
Cargo Door Removed Kit
The Cargo Door Removed Kit is designed for use during special purpose
operations such as skydiving, aerial photography , emergency air drops, etc.
The kit consists of a vented spoiler installed on the forward cargo door
hinges to minimize airflow buffeting within the cabin with the cargo doors
removed. Considered carry-on baggage.
Tires, 29” (Exchange)
Replaces standard main tires. Provides main tires 29.0 x 11-10, 10 ply
exchange for 8.50-10, 8 ply.
Cargo Equipment
Includes the following:
Cargo Barrier & Close-Out Nets (Sides and Center - 2900 lb. Rating)
The barrier and nets preclude loose cargo from moving forward into the
pilot and front passenger stations during an abrupt deceleration. Not
Available CAA. Installed.
Cargo Tie-Down Fittings
Includes structural reinforcements and anchor plates mounted on the cabin
sidewall and headliner at five stations. Used for securing cargo and baggage
area partition nets. 100 lb rating.
Cargo Area Partition Nets (2)
The cargo area partition nets are constructed of canvas with nylon webbing
reinforcement straps crisscrossing the partition for added strength. The
ends of the straps have quick-release fasteners that attach to the floor
tracks and to anchor plates located on the headliner and sidewalls. Four
straps have adjustable buckles for tightening the straps during installation
of the partition. Not for cargo tie-down.
Window Protection Plugs
Provides removable inserts that protect the inside of all windows (except
crew doors and windshield) during cargo hauling operations. Consists of
three spring-clips mounted on the inside edge of each window and ten
padded plugs with handles for easy removal.
TBD 2
2.28 2
29.3 2
63.17 1
$95,000
$1,450
$2,100
$14,950
CARGO
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