APPROVED APPROVED Director of the State Deputy Director General Introduction scientific of the National Airline of and production enterprise the Republic of Uzbekistan "Progress" A.V.Zaitzev S.M. Sumbaev 30 September 1992 30 September 1992 R E P O R T N 32/92 on extrasensory works on extrasensory diagnostics of load-carring elements of aircrafts for cracks and failures threatening the flights safety, carried out by Grigoriy Petrovich Grabovoy in September 1992 We, the undersigned, the executor of works the extrasense G.P.Grabovoy and representatives of the Customer: a head of engineering and information centre of aviation and technical base of the National Airline of the Republic of Uzbekistan V.M.Saulkin, a head of the basic test-repair metrological laboratory of Aviation and technical base of the National Airline of the Republic of Uzbekistan A.V.Shatilov and a senior project engineer of engineering and information centre of aviation and technical base of National Airline of the Republic of Uzbekistan S.V.Nemtzov drew up the present report that G.P.Grabovoy in September carried out undermentioned extrasensory works on the agreement N 14/92 of 04. 07.92 on the subject "Non-traditional methods of diagnostics of aviation technique" between the State introduction scientific and production enterprise "PROGRESS" and the National Airline of the Republic of Uzbekistan "Uzbekistan Khavo Yullari". In September 1992 G.P.Grabovoy carried out the work on agreement N 14/92 of 04.07.1992 on subitem 1.3 "Diagnostics of aircrafts and load-carring airframe structure elements for cracks and failures, threatening flights safety" of the work schedule. Diagnostics of the state of aircrafts TU-154 for cracks was carried out by G.P.Grabovoy using extrasensory methods on the list of technological control charts NN 35, 36, 39, 40, 41, 42, 44, before the work conduction on technical servicing of the periodical types of regulations. The following aircrafts were diagnosed by G.P.Grabovoy: TU-154 side number 85438 before the form I-II stage 09.09.1992 TU-154 side number 85248 before the form I-Y stage 15.09.1992. For the first aircraft the information by G.P.Grabovoy was as follows: there are no cracks on the list of technological control charts NN 35, 36, 39, 40, 41, 42, 44. The information was fully confirmed. For the second aircraft the information was as follows: there are no defects threatening the flight safety. The information by G.P.Grabovoy was confirmed the defects threatening the flights safety were not detected. Thus all extrasensory information by G.P.Grabovoy, got during his work on the subitem 1.3 "Diagnostics of aircrafts and load-carring elements of the airframe structure for cracks and failures, threatening the flights safety" of the work schedule, carried out in September 1992 was fully confirmed. Sheet N 2 Report N 32/92 Executor of works Representatives of the Customer: G.P.Grabovoy Head of engineering and information centre of aviation technical base of National Airlines of the Republic of Uzbekistan V.M.Saulkin Senior project engineer of engineering and information centre of aviation technical base of the National Airline of the Republic of Uzbekistan S.V.Nemtzov Head of the base test-repair metrological laboratory of aviation technical base of the National Airline of the Republic of Uzbekistan A.V.Shatilov