General
Year: 1987
Manufacturer: CESSNA
Model: CARAVAN 208B GRAND
Serial Number: 208B0042
Condition: Used
Registration #: N70CL
Based at: KWDG Enid Oklahoma
Airframe
Total Time: 19,161.6
Airframe Notes: Phoenix I & II Program (Eddy-current inspection clock reset to “0”, see attached description) (STC
SA01850WI and SA01919W1).
Fresh annual
TKS deice system
Nose gear new (extended fork)
Main gear overhauled
New battery
New windshields
New side windows
Corrosion-X applied to all interior metal
2 Port oxygen system
Phoenix Caravan
FAA STC SA01850WI and SA01919WI
ASIC is unique in its ability to develop a procedure that drives out the cost of ownership caused by inspections that the manufacturer has dictated to maintain structural integrity of the aircraft through a Non-Destructive testing procedure known as Eddy Current. This is a process that in critical areas of the aircraft the attaching hardware is removed and sensors are placed in the structural fittings looking for fatigue cracks. This is a repetitive inspection and causes long periods of down time causing operators to look for alternate lift sources impacting profitability. For most of the inspections the first interval is at 12,500 operating hours followed by the same inspection only 2,500 hours later and then repeating every 2,500 hours. The cost of the inspection and the down time interval is increased on an hourly rate by five times. This makes a cost effective aircraft into something that no one wants to operate.
The ASIC FAA STC replaces the fittings originally installed by the manufacturer, starts the calculation for the next inspection at “zero” and not a short 2500 hours later. Dividing the cost of the inspection by 20% along with the down time disappearing for 12,500 hours bringing the operating cost back in line with a younger aircraft. The marketing name for the procedure is “Phoenix Caravan”.
The aft fuselage inspections start at 16,500 hours and repeats every 1,000 hours. All tail fittings as well as some structure and both spars in the horizontal stabilizer and both spars in the vertical fin are replaced with new. The cost of the inspection and the down time interval is increased on an hourly rate by sixteen times.
The Phoenix Caravan procedure to replace the fittings that eliminates the inspection requires special tooling along with training that is not available in any place other than ASIC, the FAA STC procedure is not available to any other facility nor can it be performed in any other location than ASIC.
Engine 1
Engine 1 Make/Model: PRATT & WHITNEY PT6A-114A
Engine 1 Time: 0 SNEW
Engine 1 TBO: 3600
Engine 1 Notes: Aircraft to be delivered with a factory New Pratt & Whitney PT6A-114A Engine with Pratt & Whitney Factory Warranty
Aircraft is equipped with the Pratt & Whitney FAST™ digital engine health management solution which captures, analyzes and wirelessly sends full-flight data intelligence to you within minutes of engine shutdown so you can maximize aircraft availability, optimize maintenance planning, and reduce operating costs. The FAST solution is tailored for your engine by the people who designed and know your engine best.
Props
Prop 1 Manufacturer: MCCAULEY
Prop 1 Time: 0 SMOH
Number of Blades: 3
Prop Notes: Prop equipped with TKS
Avionics
Flight Deck Manufacturer/Model: GARMIN
Avionics/Radios: Garmin GFC600 digital autopilot with roll, yaw, pitch, and pitch trim servos.
Garmin G600TXi 12 inch EFIS on pilot side with GAD43e and Synthetic Vision.
Garmin G600TXi 12 inch EFIS on copilot side with Synthetic Vision.
Garmin GCU485 PFD remote control.
Garmin GEA71B Engine Interface displayed on both pilot and copilot PFD’s.
Garmin GI275 Class III ADAHRS as backup flight instrument.
Garmin GTN750Xi as #1 GPS/Nav/Comm/MFD.
Garmin GTN750Xi as #2 GPS/Nav/Comm/MFD.
Garmin SmartGlide enabled.
Garmin GDL60 datalink with PlaneSync.
Garmin GMA35c remote Bluetooth audio panel with pilot and copilot positions.
Garmin GTX345R ADS-B Out/In remote transponder.
Two Garmin GSB15 USB hubs in cockpit. One wired to GI275 for updating.
Garmin GWX75 radar, displays on G600TXi’s and GTNXi’s.
Fresh FAR 91.411 static and FAR 91.413 transponder certifications.
406 ELT
Additional Equipment
Flight Into Known Icing (FIKI): Yes
Exterior
Year Painted: 2026
Exterior Notes: New strip and paint.
Paint scheme is made to order per customer choice.
Customer can pick their own paint scheme which is overall white and up to a three color stripe package.
Interior
Year Interior: 2026
Interior Notes: All new interior, new Kydex headliner, new vinyl carpet, new Kydex sidewalls, new window trims, new vinyl seating, etc. etc.
Interior seating configuration is made to order per customer choice.
10 place commuter
11 place commuter
14 place commuter
Executive interior (Oasis) available as well
Modifications/Conversions
Modifications/Conversions: Kydex crew door panels with pockets (ASIC STC)
Wing jack pad (ASIC STC)
New late model elevator and rudder hinges
Standby flap system limit switches (ASIC STC)
LED landing and taxi lights
Inspection Status
Inspection Status: Current on all maintenance, mandatory service bulletins and airworthiness directives at delivery
Airworthy: Yes
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