The P92-JS is a two-seater side by side, single strut braced, high wing aircraft. The aircraft is suitable for flying schools and training activities and for many other missions such as touring, territory surveillance, patrol, etc. The wing is an all-aluminium conventional structure with a single strut. The top and bottom engine cowls are removable making any maintenance easier to accomplish. A wide rear window together with large side windows complete the visibility allowing 360 of vision in the cockpit. The all moving Stabilator is fitted with a trim tab controlled by buttons on the control column. The aircraft has neutral handling which makes it more stable for people of any weight/height. The flaps are deployed electrically and allow a stall speed lower than 41 KTS (76 km/h). The low stall speed and the general slow flying characteristics of the aircraft allows it to operate with ease on short runways.
Aircraft does not have a valid Certificate of Airworthiness.
Aircraft is not in an airworthy condition.

Airplane time state:
Airplane time state: 1.818 hours.
Engine type: one Bombardier-Rotax 912S3 engine.
The aircraft is not enrolled on the Tecnam Factory Airframe and Engine programme. The engine has been overhauled 85 hours previously. Propellers need overhaul.
Aircraft does not have a valid Certificate of Airworthiness.
Aircraft is not in an airworthy condition.

The avionics comprise: VHF NEV REC.AND VHF/COMM TRANSCEIVER KING KX 125; VOR/LOC INDICATOR GARMIN GI106A; VHF/COMM TRANSCEIVER GARMIN SL 40; TRANSPONDER GARMIN GTX 330; GPS/NAV R/T COM GARMIN GNS 430; AUDIO PANEL GARMIN GMA 340; ALTITUDE ENCODER; INTERCOM FLYGHTCOM 403MC; GPS RECIVER KING SKXMAP III C; ADF RECEIVER KING KR 87; ADF INDICATOR KING KI 227