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1984 THORP T18

Details

General Specs

For Sale

1984

THORP T18

Chicago, IL USA


General Specs

694

694

298 SNEW

Used


Additional Classifications


Detailed Description

1984 Thorp T-18, 180hp, Constant Speed prop, 694TT A&E, 298 Since Teardown and NEW prop, very nice, always hangared, KX155, KLX135A GPS/com, KT76A, Intercom.

Avionics / Equipment

ENGINE: LYCOMING 0-360 AID, 180 
hp, S/N L-1791-36.

PROPELLER: Hartzell Constant 
Speed, Model HC-F2YR-IF, S/N 
CM12223B

The Thorp has always been and is 
now kept in a heated hanger at the 
Kenosha, Wisc. Regional Airport 
(ENW). The first flight took place at 
ENW on 12-9-1984. After the annual 
inspection in 1999 by the FBO at 
ENW the FBO did not tie down the 
tail before the FBO did their after 
inspection engine run-up. The tail 
lifted and the prop struck the 
ground. The engine was removed 
and was taken to G&N Aviation in 
Griffith, Indiana. The engine was 
disassembled and inspected. The 
engine was reassembled using 
new slick mags, new Lamar starter, 
rebuilt prop governor from 
Hartzell, new rod and main 
bearings, new oil pump gears, all 
new hardware and other 
miscellaneous parts. The engine 
was painted red and dynoed. The 
engine was installed on the Thorp 
with new Lord mounts and bolts. At 
this time a new Hartzell constant 
speed prop was installed. Total 
time on the Airframe was 398.0 hrs. 
at this time.

1. Total Time 694.4 hours airframe
2. Total Time SMOH O-360 180 HP 
694.4, 298.4 Since Tear Down due 
to prop strike
3. Total Time on prop since NEW 
298.4 hours
4. KT76A transponder, 24 month 
thru 6-17-2-18
5. KX155 navcom
6. KLX135A GPS/com
7. Navaid AP-1 wing leveler, tracks 
GPS
8. Intercom, Troll Avionics
9. Electronics International Engine 
Analyzer, Model SR-8A, CHT/EGT all 
cylinders
10. JPI-450 fuel scan: Gal/Hr., fuel 
used, fuel remaining.
11. ELT, Pointer Model 3000.
12. Wing Tip Strobes and 
Navigation Lights.
13. 29 Gal. Main Fuel Tank, 16 Gal. 
Aux tank.
14. Annual condition inspection 
current to 10-05-2016.
15. Aerobatics permitted by the 
FAA operating limitations. a) Stalls, 
Steep turns. b) Aileron Rolls (left & 
right). Hammer head stall. c) Loops.
16. Cruises at 195+ MPH IAS at 
25/2500 power setting. 17. 1034 lbs. 
empty weight; 1800 lbs. max gross 
weight.

Contact Info

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