APPROVED APPROVED Director General Deputy Director General of the joint venture of the National Airline of "ASKON" the Republic of Uzbekistan I.V. Khamrakulov S.M. Sumbaev 3 July 1992 4 July 1992 R E P O R T N 18/92 on extrasensory works on extrasensory predication of failures, faults and deviations from operation specificatitons on the aircraft IL-62M side number 86492 during the test flight, carried out by Grigoriy Petrovich Grabovoy on 16 June 1992 We, the undersigned, the executor of works the extrasense G.P. Grabodoy and the representatives of the Customer: the head of the flight-test station of the plant N 243 of the Civil Aviation V.N.Kubrak, senior project engineer of the flight-test station of the plant 243 of the Civil Aviation G.N.Saldin and the 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, drew up the present report that G.P.Grabovoy in June 1992 carried out the undermentioned mentioned extrasensory works on the agreement N 9 of 02.12.1991 between the joint Soviet-American enterprise "ASKON" and the Uzbek Department on Civil Aviation on the subject "Non-traditional methods of aviation technique diagnostics". The senior project engineer G.N.Saldin set a task to the extrasense G.P.Grabovoy to diagnose failures, faults and devia- tions from specifications on the aircraft IL-62M side number 86486 during the test flight on the following points: 1. To make the prediction on engines. 2. To make the prediction on the work of automated control of SAU 1T-2. 3. To make the prediction on the work of measuring part of SPUT-8V with the predictions of the following devices, determining the working capacity of the fuel gauge: DK11-2T, DTC20-1, DT40-3, DT40-2, DT40-1, DT40, DTC20, VI26-1, VI27-2, UT32-3T 826-1, UT32-3T 0828-1, 2PPT26-3T, BU10V-1, DK11-3T, DTC20-3, DT40-5, DT40-4, DTC20-2, DT40-7, DTC20-4, DT40-6, VI26-2, UT32-1T, PPT26-1T, UT32-2T, 2PPT26-1T 0845-01, UT32-1T, PPT26-1T, DTC20-5, DTC20-6, DK11-1T, DTC20-6, VI26-2, DT40-6, DTC20-4, DT40-7, VI03-2, PGA3K-1T, DK11-3T, DTC20-3, DT40-5, DT40-4, DTC20-2, 2PPT25-2TT, UT32-3T, UT32-2T, DTC20-1, DT40-3, DT40-2, DT40-1, DT40, DTC20. 4. To make prediction on work of the following fuel pumps of fuel transfer of auxiliary tanks: 7-4121, 7-4501, 6-4125, 6-4126, 6-4508, 7-4122, 7-4592. 5. To make the predication on the work of the following pumps of fuel transfer to consumption section: 7-4141, 6-4143, 6-4147, 6-4144, 6-4148, 7-4142, 7-4146, 7-4145. Sheet N 2 Report N 18/92 6. To make the prediction on the work of the following pumps of fuel pumping: 7-4169, 7-4165, 6-4171, 6-4167, 6-4172, 7-4166, 7-4170. 7. To make the prediction on fault of the following lamps: 15-4539, 4541/16, 15-4092, 4540/15, 15-4536, 15-4359, 15-4361, 15-4365, 15-4352, 15-4366, 15-4360, 15-4364, 15-4363, 15-4437, 15-4279, 15-4439, 15-4281, 15-4222, 15-4440, 15-4280, 15-4438. 8. To make the prediction on the following points: - fuel system; - fuel system units; - oil system and it's units; - fuselage; - wing; - vertical tail; - system of elevations and it's units; - rudder, flap, power plant etc and their units control; - hydraulic and hydronitrogen system and it's units; - radiocommunication equipment; - navigation enquipment; - radar equipment; - instrumental equipment; - electrical equipment; - undercarriage, including wheels; - flight recorders; - aviation incident. 9. To make the prediction on fuel pump signalization failure. The work was carried out by G.P.Grabovoy on 16.06.1992 on devices schemes with the data, got with the help of clairvoyance. The purpose of the work by G.P.Grabodvoy was to diagnose the aircraft in a flight in contrast to the analogous work for the aircraft on the ground before the test flight, carried out by G.P.Grabovoy in March, 14, 1992 to confirm the result, got 13.11.1991. The results of the work by G.P.Grabovoy on the prediction of the technical state of the aircraft IL-62M side number 86492 are set down in accordance with abovementioned items of the task. Confirmations of the predictions were based on information, set down in the log on the test flight of the aircraft IL-62M side number 86492 of 16.06.1992. The predictions were transfered on 16.06.1992 during the test flight of the aircraft side number 86492 25 a minute before the aircraft landing. 1. Information of the prediction on engines: deviations in the work of the signalization, related to the engine N 4. Confirmation, recording in the log - The indicator lighted up three times in half heat "Fault in the engine selection N 4". 2. Information of the prediction on SAU 1T-2: Deviation in the work of SAU 1T-2 at the go-around. Confirmation recording in the log - SAU 1T-2 periodically went on pitching at the go-around. 3. Information by G.P.Grabovoy on the work of fuel device and confirmation of his information are given in the table 1. Sheet N 3 Report N 18/92 Table 1 ________________________________________________________________ Information on the prediction : Confirmation by G.P.Grabovoy : ________________________________________________________________ DK11-2T no faults confirmed DTC20-1 no faults confirmed DT40-3 no faults confirmed DT40-2 no faults confirmed DT40-1 no faults confirmed DT40 no faults confirmed DTC20 no faults confirmed BI27-1 no faults confirmed BI27-2 no faults confirmed UT32-3T 826-1 no faults confirmed UT32-3T 0828-1 no faults confirmed 2PPT26-3T no faults confirmed BU10V-1 no faults confirmed DK11-3T no faults confirmed DTC20-3 no faults confirmed DT40-5 no faults confirmed DT40-4 no faults confirmed DTC20-2 no faults confirmed DT40-7 no faults confirmed DTC-20-4 no faults confirmed DT40-6 no faults confirmed BI26-2 no faults confirmed UT32-1T no faults confirmed PPT26-1T no faults confirmed UT32-2T no faults confirmed 2PPT26-1T 0845-01 no faults confirmed UT32-1T no faults confirmed PPT26-1T no faults confirmed DTC20-5 no faults confirmed DTC2-6 no faults confirmed DK11-1T no faults confirmed DTC20-6 no faults confirmed BI26-2 no faults confirmed DT40-6 no faults confirmed DTC20-4 no faults confirmed DT40-7 no faults confirmed BIO3-2 no faults confirmed PGA3K-1T no faults confirmed DK11-3T no faults confirmed DTC20-3 no faults confirmed DT40-5 no faults confirmed DT40-4 no faults confirmed DTC20-2 no faults confirmed 2PPT25-2TT no faults confirmed UT32-3T no faults confirmed UT32-2T no faults confirmed DTC20-1 no faults confirmed DT40-3 no faults confirmed DT40-2 no faults confirmed DT40-1 no faults confirmed DT40 no faults confirmed DTC20 no faults confirmed ________________________________________________________________ 4. Information on the prediction on the work of transfer pumps of auxiliary tanks and the confirmation is given in the Table 2. Sheet N 4 Report N 18/92 Table 2 ________________________________________________________________ Information on the prediction : Confirmation by G.P.Grabovoy : ________________________________________________________________ 7-4121 no faults confirmed 7-4501 no faults confirmed 6-4125 no faults confirmed 6-4126 no faults confirmed 6-4508 no faults confirmed 7-4122 no faults confirmed 7-4592 no faults confirmed ________________________________________________________________ 5. The prediction on the work of the following pumps of fuel transfer to the consumption sections and corresponding confirmation is given in the Table 3. Table 3 ________________________________________________________________ Information on the prediction : Confirmation by G.P.Grabovoy : ________________________________________________________________ 7-4141 no faults confirmed 6-4143 no faults confirmed 6-4147 no faults confirmed 6-4144 no faults confirmed 6-4148 no faults confirmed 7-4142 no faults confirmed 7-4146 no faults confirmed 7-4145 no faults confirmed ________________________________________________________________ 6. Information on the prediction on the work of fuel pumping and confirmation are given in the table 4. Table 4 ________________________________________________________________ Information on the prediction : Confirmation by G.P.Grabovoy : ________________________________________________________________ 7-4169 no faults confirmed 7-4165 no faults confirmed 6-4171 no faults confirmed 6-4167 no faults confirmed 6-4172 no faults confirmed 7-4160 no faults confirmed 7-4570 no faults confirmed ________________________________________________________________ 7. Information on the prediction on the works of lamps and confirmation is given in the Table 5. Table 5 ________________________________________________________________ Information on the prediction : Confirmation by G.P.Grabovoy : ________________________________________________________________ 15-4539 no faults confirmed 4541/16 no faults confirmed 15-4092 no faults confirmed 4540/15 no faults confirmed 15-4536 no faults confirmed 15-4359 no faults confirmed 15-4361 no faults confirmed 15-4365 no faults confirmed Sheet N 5 Report N 18/92 15-4352 no faults confirmed 15-4366 no faults confirmed 15-4360 no faults confirmed 15-4364 no faults confirmed 15-4363 no faults confirmed 15-4437 no faults confirmed 15-4279 no faults confirmed 15-4439 no faults confirmed 15-4281 no faults confirmed 15-4222 no faults confirmed 15-4440 no faults confirmed 15-4280 no faults confirmed ________________________________________________________________ 8. Prediction by G.P.Grabovoy on failures and faults or defects in aircraft system and design as well as confirmation is given below in the Table 6. Table 6 ________________________________________________________________ Information on the prediction : Confirmation and regis- by G.P.Grabovoy on the air- : tration in the log craft systems and design : ________________________________________________________________ In the fuel system and units: Confirmed "Pipe in the right side of the "Jets of transfer of the 5 wing has increased resistance to right tank shall be checked fuel transfer. The jet diameter (transfer is late)" is below the standard" No faults in the oil system and Confirmed units No defects in the fuselage Confirmed No defects in the wing Confirmed No defects in the tail Confirmed Elevation system and units - Confirmed no faults Aircraft control system: Confirmed Deviation in the aircraft "RM with witching APM-62 control system: shall be repaired (deviated to the left)" Hydraulic and hydronitrogen Confirmed system and units - no faults Radiocommunication equipment - Confirmed no faults Navigation equipment - Confirmed no faults Radar equipment - Confirmed Deviation in the work of "Pointing array incorrect, radar equipment declined to the right" Instrumentation Confirmed Deviation in the instrumen- "Fault in UUT (pitching tation work indicator)" Sheet N 6 Report N 18/92 Electrical equipment - Confirmed Deviation in the work of "Repair of an amplifier electrical equipment AP-309" Undercarriage (including Confirmed wheels) - no faults Flight recorders - Confirmed no faults Aviation incident - Confirmed no faults _________________________________________________________________ 9. The prediction on signalization failure of fuel pumps: deviation in transfer from 5 right tank. The confirmation is the registration in the log: To check the transfer jets from the right 5 tank (the transfer is late). Thus all extrasensory information by G.P.Grabovoy on the aircraft N 86492 was fully confirmed and the following conclusions can be made: there is no differences between the efficiency of the extrasensory diagnostics by G.P.Grabovoy of the aircraft both in a flight or ground, the information by G.P.Grabovoy is fully confirmed in any case. It makes sense to use the extrasensory diagnostics by G.P.Grabovoy in the future to increase the flights safety and timely detection of defects on ground. Executor of works Representatives of the Customer: G.P.Grabovoy Head of the flight-testing station of the plant N 243 of Civil Aviation V.N.Kubrak Senior project engineer of the flight testing station of the plant N 243 of Civil Aviation G.N.Saldin Head of engineering and information centre of aviation technical base of National Airlines of the Republic of Uzbekistan V.M.Saulkin