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
                10 July 1992                        10 July 1992




                       R E P O R T   N  23/92

            on  the extrasensory  works on  extrasensory
            diagnostics of the aircraft state for cracks
            on the list of technological control charts
                        carried out in July
                   by Grigoriy Petrovich Grabovoy

     We, the  undersigned,  the  executor of the work the extrasense
G.P.Grabovoy and representatives of the  Customer:  a  head  of  the
engineering  and  information  centre  of the aviation and technical
base of the National Airline of  the  Republic  of  Uzbekistan  V.M.
Saulkin  and  the  senior  project  engineer  of the engineering and
information centre  of  the  aviation  and  technical  base  of  the
National Airline of the Republic of Uzbekistan S.V.Nemtzov,  drew up
the present report that G.P.Grabovoy carried out the  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 July 1992 G.P.Grabovoy carried out the work on the agreement
N 14/92 of 04.07.1992 on subitem 1.3 ("Diagnostics of aircrafts  and
load-carring  elements  of  air-frame structire to detect cracks and
failures, thereatening the flights safety") of the work schedule.
     The aim  of  the  carried out work is to show the efficiency of
extrasensory  diagnostics  of  load-carring  elements  of   airframe
structure  at  the  expense  of  reduction  of  the labour input (in
comparison with some traditional types of works) and at the  expense
that  the extrasense G.P.Grabovoy is able to detect cracks where the
inspection by technological charts has not been carried out.
     Diagnostics of the aircraft TU-154 state for cracks was carried
out by G.P.Grabovoy  by  extrasensory  method,  using  the  List  of
technological control charts NN 35,  36,  39,  40, 41, 42, 44 before
the works conduction on the techical service on periodical  standing
order types.
     The following aircrafts were diagnosed:
     TU-154 side number 85578  05.07.92
     TU-154 side number 85398  05.07.92
     For both  the  information  by G.P.Grabovoy was:  there were no
cracks.  The  information  was  fully  confirmed  at  the  technical
inspection  on  abovmentioned  control  charts  the  cracks were not
determined.
     Thus all  extrasensory  information  by G.P.Grabovoy,  got as a
result of his work according to  the  subitem  1.3  "Diagnostics  of
aircrafts  and load-carring elements of airframe structure to detect
cracks and failures,  thereatening the flight safety"  of  the  work
schedule in July 1992 were fully confirmed.


                     Sheet N  2  Report N 23/92



      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