S/N: 172S10028
Registration: N19871

Airframe, Engine and Prop:
Airframe: 2005 Cessna 172 Skyhawk SP
No Damage History

Engine: Lycoming IO-360-L2A, 180HP
0 SMOH by Western Skyways

Prop: McCauley IA170E/JHA7660
1718 SNEW

Avionics and Options:
This aircraft has the NAV III package which includes the following components:

GDU 1040 – CONTROL DISPLAY UNITS (2)
The centerpiece of the G1000 system is the GDU 1040 Control Display Unit. The GDU’s provides a 10.4” size, high resolution (1024x768) LCD display, which is sunlight and wide viewing angle readable. Incorporated in the bezel of the GDU are the controls for all the remote avionics units that make up the G1000 system. Use of dedicate side controls which perform the same function on either the PFD or MFD, and soft key buttons along the bottom of each display make the GDU’s the avionics control center, positioned right in front of the pilot. The same GDU is used for either the PFD or the MFD; the displays role is determined when connected to the avionics harness. Each display can work in reversionary mode in the unlikely event of a failure of the either the PFD or MFD.

GMA 1347 – DIGITAL AUDIO PANEL
The GMA1347 Digital Audio Panel and Marker Beacon Receiver is designed to be placed vertically between the two displays. The GMA1347 provides four intercom modes: ALL, PILOT, COPILOT, and CREW. Capacity of the audio panel allows for the support of crew (Pilot, Co-Pilot) and up to eight additional passengers. Support for three communication radios, dual navigation radios, DME, ADF, and auxiliary audio input are built into the audio panel with more capacity available when using external switches and annunciations.

GDC 74 AIRDATA COMPUTER (ADC)
The GDC 74 Airdata computer provides all the dynamic and static pressure computations using internal absolute and differential pressure transducers, and an OAT probe. Pressure altitude, calibrated airspeed, true airspeed, vertical airspeed, and total outside air temperature are provided to the various other sub- systems that required this data for primary, reversionary and redundancy. Verification of the airdata computer performance has been shown from –1,400 feet to 55,000 feet, over temperature ranges of -55°C to +85°C.

GRS 77 – ATTITUDE HEADING & REFERENCE SYSTEM (AHRS)
The all solid-state GRS 77 AHRS provides the package for all the inertial sensors required for attitude output to the G1000 system. The use of solid-state technology inertial sensors, and leveraging additional attitude information from other G1000 components make this AHRS a superior product. Technical
advantages of this AHRS system are:

•Superior Performance over the entire flight envelope by using patented algorithmic approaches and taking in additional attitude information from the other integrated G1000 subsystems.
•On the move initialization of the AHRS to correctly determine attitude information. Other AHRS units require several minutes of stationary initialization before attitude information is available.
•In-Flight initialization of the AHRS at bank angles up to 20 degrees. Not possible with the competition, so any momentary loss of power and/or AHRS interruption the AHRS is gone for the rest of the flight.
•High integrity and reliability of the AHRS generated attitude outputs due to the cross checks of all the attitude information in the G1000 subsystems making it quicker for the AHRS to identify a sensor failure that could lead to potential HMI (Hazardous and Misleading Information).
•Lower cost AHRS since the system can use lower cost sensors; takes advantages of all the other integrated sub-systems that are required for other functions and leverages them to help compute superior attitude data.
•High availability of the AHRS since it does not require any one sub-system for continued operation. Reversionary modes can utilize data from GPS systems, airdata computer, and magnetometer.
•Solid state, so no mechanical parts to wear and small lightweight package design.

GMU 44 MAGNETOMETER
The magnetic field vector information for the AHRS is provided by the full three axis GMU 44 magnetometer. Unlike the flux-valve used in the HSI installations that provide only planar magnetic field information, the GMU 44 magnetometer can provide full three-axis magnetic field information in all flight attitudes.

GIA 63 – COMMUNICATION, NAVIGATION, & INTERFACE ADAPTER UNIT
The GIA 63 is the data hub for most all of the G1000 sub-systems, most installations use two GIA 63’s per aircraft installation.
Communication features of the GIA 63:
•Communication transceiver tuning from 118.00 to 136.990 MHz, 8.33 or 25 kHz user selected. - 16 watts transmitting power.
•FM immunity per ICAO Annex 10.
•Digital audio interface with the GMA 1347 audio panel.
•Emergency audio channel used to bypass the audio panel.
•Separate power supply from other internal components.

Navigational features of the GIA 63:
•VOR/ILS localizer receiver tuning from 108.00 to 117.95 MHz in 50 kHz increments.
•ILS Glide Slope receiver.
•VOR audio and identifier output

The GIA 63 uses multiple communication standards, including Ethernet data bus, to provide interface to a wide variety of avionics systems.

GTX 33 – MODE S TRANSPONDER with TIS
The GTX 33 Mode S Transponder provides the required ATC transponder and altitude reporting capabilities. Included with the GTX 33 is the Traffic Information Service (TIS) functionality. Some of the TIS capabilities and details are:
•TIS data link communication typically within 55 nm of a Mode S radar capable site. Most of these are in location where there is the highest traffic densities.
•TIS data when established provides estimated position, altitude, altitude trend and ground track information for up to 8 aircraft within 7 nm horizontal range and +3,500, -3, 000 feet of the aircraft.
•TIS data is derived from the same radar used by ATC and is updated approximately every 5 seconds.
•Altitude data for each intruder aircraft in 100 ft increments based off of the same Mode C altitude data provided ATC. So altitude separation data same as TAS level traffic.

GEA 71 – ENGINE / AIRFRAME UNIT
Providing the data acquisition and signal conditioning for all the engine sensors, airframe sensors and discrete signals the GEA 71 is the interface between the aircraft and the G1000 system. The GEA 71 can be configured to handle analog, digital & discrete I/O to meet the specific requirements of the aircraft. Digital output of measured voltages, currents and discrete input sources along with providing sensor excitation make the GEA 71 the only interface required. A data stream of all measured sensors and signals is provided to each of the CDU units for redundancy.

GDL 69A
XM Satelite Radio and XM Weather receiver.

KAP 140 Autopilot
The KAP 140 autopilot provides Dual-axis, Altitude Preselect Flight Control System with GPS Roll Steering functionality. Roll Steering enables the GPS navigational inputs to control the autopilot and automatically perform course changes and intercept the course to the next active waypoint.

BF Goodrich WX-500
WX-500 provides weather mapping of electrical discharges (lightning) up to 200 nautical miles away, and can map this activity for hazardous weather avoidance on the large MFD or PFD inset.

Front Seat Inflatable Restraints

Pilot Control Wheel - Pitch Trim Switch / Autopilot Disconnect
Control Wheel Push-To-Talk Switch - Pilot/Copilot
Mic & Phone Jacks - Pilot/Copilot/Passengers
Deck Skin Cooling Fan #1 - Instrument Panel
Avionics Cooling Fan #2 - PFD
Avionics Cooling Fan #3 - MFD
Aft Avionics Cooling Fan #4 - Avionics Equipment
Turn Coordinator for KAP-140 Roll Rate Data
Backup “Life-saver” Attitude Gyro, Altimeter and Airspeed Indicator
KN 63 DME ($10,000 upgrade)

Seller believes all specifications to be correct. However, all specifications are subject to verification by buyer and subject to prior sale. Purchaser is responsible to ensure that aircraft and its components are as described.

Investment Opportunity

This aircraft is currently placed in a lease back program in Utah. If so desired, the aircraft could be purchased as an investment. Call for more details.

Specs:
Specs:

Max ramp weight (lbs.): 2558
Gross weight (lbs.): 2558
Landing weight (lbs.): 2550
Empty weight (lbs.): 1757
Useful load (lbs.): 800.6
Payload, full fuel (lbs.): 577
Usable fuel (gals.): 53
Oil capacity (qts.): 8
Wingspan: 36 ft. 1 in.
Overall length: 27 ft. 2 in.
Height: 8 ft. 11 in.
Wing area (sq. ft.): 174
Wing loading (lbs./sq ft.): 14.7
Power loading (lbs./hp.): 14.2
Wheel size (in.): 6.00 x 6
Seating capacity: 4
Cabin doors: 2
Cabin width (in.): 39.5
Cabin height (in.): 48

Performance:

Cruise speed (kts.):
75% power @ 8,500 ft.: 124
65% power @ 8,500 ft.: 117
55% power @ 8,500 ft.: 108

Range @ 8,500 ft. (nm):
75% power: 518
65% power: 544
55% power: 580


Fuel consumption (gph):
75% power: 10.0
65% power: 8.6
55% power: 7.3


Vso (kts.): 48
Best rate of climb (SL fpm): 1225
Best rate of climb, 8,000 ft. (fpm): 350*
Service ceiling (ft.): 14,000
Takeoff ground roll (ft.): 960
Takeoff over 50-ft. obstacle (ft.): 1630
Landing ground roll (ft.): 575
Landing over 50-ft. obstacle (ft.): 1335

PRICE: $170,000