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WARRANTY Laversab Inc., warrants its products to conform to or exceed the specifications as set forth in its catalogs in use at the time of sale and reserves the right, at its own discretion, without notice and without making similar changes in articles previously manufactured, to make changes in materials, designs, finish, or specifications.
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COPYRIGHT NOTICE Copyright (c) 2008 onward by Laversab Inc. All rights reserved. The content of this manual may not be reproduced in any form by any means, in part or in whole, without the prior written permission of Laversab Inc.
REVISION HISTORY Document No. Release Date Description 9052 10/10/2008 Model 6150 User’s Manual 9052 03/11/2011 Model 6150 Rev B1 User’s Manual...
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WARNING THE 6150 USES LINE VOLTAGES FOR ITS OPERATION WHICH ARE POTENTIALLY DANGEROUS. IMPROPER OPERATION OF THIS EQUIPMENT MAY RESULT IN PERSONAL INJURY OR LOSS OF LIFE. HENCE THE EQUIPMENT DESCRIBED IN THIS MANUAL SHOULD BE OPERATED ONLY BY PERSONNEL TRAINED IN PROCEDURES THAT WILL ASSURE SAFETY TO THEMSELVES, TO OTHERS AND TO THE EQUIPMENT.
SECTION 1 INTRODUCTION The 6150 Digital Air Data and Leak Tester is a high accuracy Pitot Static Tester which can be used for performing leak checks on the Pitot and Static systems of all aircraft. It can also be used to perform accuracy checks on altimeters, airspeed indicators, air data computers and other air data related equipment on-board aircraft.
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6. VENT metering valve This valve is used to vent-to-ambient, pressure or vacuum from the Pitot output. With the Cross-bleed valve open, the Vent valve can also vent-to-ambient, pressure or vacuum from the Static system. CAUTION : This metering valve seals before it reaches its STOP. Do Not tighten at all past this STOP.
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Leak-test mode, both of these solenoid-valves are automatically closed to isolate the aircraft from the metering valves of the 6150. The 6150 can still monitor the altitude and airspeed on the Static and Pitot ports. However, once the solenoid-valves are closed, none of the metering valves will have any effect on the pressure (or vacuum) on the Static or Pitot outputs.
This section explains all the different screens and functions of the 6150. 2.1 Power On. When power is turned ON to the 6150, the display shows the sign-on screen for 3 seconds. The pumps remain OFF. After the sign-on screen, the display shows the Limits and Leak-times screen.
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1000 feet higher than the maximum altitude that will normally be generated with the 6150 for the user’s typical aircraft. For example, if the user will normally perform tests up to 30,000 ft. then the limit should be set at 31,000 ft..
decrement in steps of 1 minute. The minimum value for leak-time 1 is 1 minute and the maximum is 18 minutes. When GO is pressed, the displayed value is accepted and the screen changes as shown below: Leak-time 1= 3 min.
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In this screen, (the values displayed on your screen will likely be different), 425 feet is the altitude being measured at the Static output of the 6150 and 6.5 knots is the airspeed being measured at the Pitot output. There is no change of altitude so the VSI is indicated as 0 ft/min.
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constantly make changes to the Vacuum valve. Slowly close the Vacuum valve as you approach the desired altitude. Decrease altitude: Close the Vacuum valve completely, then slowly open the Vent valve while watching the VSI. This will allow you to achieve altitudes all the way down to Ground.
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-30 knots. This relief-valve is active even when the 6150 is powered-off. There are two conditions during the operation of the 6150 when the internal relief-valve will NOT protect against negative airspeed.
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b. During Calibration Mode, the Leak Test Shutoff solenoids are closed. This prevents the relief-valve from providing the negative airspeed protection. However, this protection is normally not required during Calibration Mode. 2.3.7 Warnings While in the Main Screen, several warning messages are displayed to alert the user to existing or potential error conditions.
Pitot and Static outputs from the pumps and the metering valves. In Leak Check mode the aircraft is not protected against negative airspeed. If a negative airspeed condition exists, the 6150 will automatically trip out of Leak Check mode to prevent excessive negative airspeed. See section 2.3.6 above.
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The start of the second, third and fourth lines show “1m:”, “2m:” and “3m:” which indicates that the leak times have been programmed for 1, 2 and 3 minutes. For changing leak-time values please see Section 2.2. At the end of 1 minute of elapsed time, the display appears as below: 4995 feet 0 ft/min.
Main Screen. Please see Section 2.3.7 above. There is one exception. If airspeed goes more negative than -20 knots while in the Leak Check mode, the 6150 will automatically trip out of Leak Check mode and return to the Main Screen. The Leak Test Shutoff solenoids will be opened to allow the internal relief-valve to protect the aircraft against excessive negative airspeed.
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1m: 4995 / 99.8 / 0.2 2m: 4991 / 99.6 / 0.4 3m: 4988 / 99.5 / 0.5 This screen shows the starting values of the leak check on line 1 and the timed leak values on lines 2, 3 and 4. Please note that this function will only show the last-executed Leak Check, even if it is incomplete.
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Press CANCEL to return to the Main Screen. Press FUNCTIONS to scroll to the next function. 2.5.4 Select Units of Meters and kmph The fourth function allows you to select the Static units of Meters and the Pitot units of kmph.
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Units = Ps mb & Pt mb Press GO to select these units FUNCTIONS: next Fn. CANCEL: exit If GO is pressed, the effective units will be mbar (absolute) for both Static and Pitot. Press CANCEL to return to the Main Screen. Press FUNCTIONS to scroll to the next function.
SECTION 3 TYPICAL USE This section outlines the typical method of using the 6150. 3.1 Setup 1. Turn ON the 6150. 2. Check the limits and leak times to see if they are acceptable. Change them if required using the steps outlined in Section 2.2. Once these values are acceptable, press GO. You are now in the Main Screen.
7. Slowly open the Vent valve while watching the VSI. Altitude will reduce. Once altitude is close to Ground level, open the Vent valve completely to ensure that the system is completely vented. 8. Turn OFF the 6150. 9. Disconnect from the aircraft. 10. Close all valves.
+15 and -15 knots. 6. If an altimeter accuracy check needs to be performed, skip to Section 3.5 7. Turn OFF the 6150. 8. Disconnect from the aircraft. 9. Close all valves.
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8. Continue to open the Vent valve (while watching VSI) until the system is completely vented. 9. Turn OFF the 6150. 10. Disconnect from the aircraft 11. Close all valves.
CALIBRATION Equipment The calibration procedure for the 6150 requires the following equipment: 1. Pressure controller (Standard) with an accuracy of at least 0.004 inHg between 1 and 60 inHg absolute. The controller must be able to achieve pressures between 1.0 inHg (abs) and 60 inHg (abs).
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3. Using the Standard, generate exactly 1.000 inHg on both outputs. Allow the pressure to be stable for 1 minute to eliminate any temperature effects. 4. Note the actual readings on the 6150. These will be noted as the “As Found” Vacuum values in the calibration report. (Figure 4.1) 5.
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Allow the pressure to be stable for 1 minute to eliminate any temperature effects. 2. Note the actual Static value on the 6150. This will be noted as the “As Found” full- scale Static value in the calibration report (figure 4.1) 3.
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This error indicates that either the Standard did not actually generate 60.000 inHg when GO was pressed in step 4 above or there is large difference in accuracy between the Standard and the 6150. Unless this discrepancy can be resolved, calibration cannot proceed further.
1. Using the Standard, generate the following pressures on the Static output of the 6150 in units of inHg : 1.000, 3.200, 6.400, 9.600, 12.800, 16.000, 19.200, 22.400, 25.600, 28.800 and 32.000. Note the Static readings on the 6150 at each pressure.
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Model: 6150 Serial#: 74678 Full scale: Ps: 32 inHg Pt: 60 inHg Last Calibrated date: 10/10/08 _______________________________________________________________________ CALIBRATION RESULTS STATIC PRESSURE (Ps): TEST POINT AS FOUND AS LEFT DEVIATION inHg inHg inHg 1. Vacuum 1.003 1.000 0.003 2. Fullscale 32.005 32.000...
SECTION 5 MAINTENANCE Scheduled maintenance of the 6150 includes calibration once a year. The calibration procedure is described in Section 4. Apart from this there are no other scheduled maintenance requirements.
APPENDIX A SPECIFICATIONS Static Output Pressure units range: 1.0 to 32 inHg resolution: 0.001 inHg accuracy: 0.008 inHg Altitude units range: -2000 ft. to 60,000 ft. resolution: 1 foot accuracy: 8 ft. @ 0 ft. 24 ft. @ 35,000 ft. 48 ft.
Ship equipment to : LAVERSAB, INC. 505 Gillingham Ln.. Sugar Land, Texas 77478 U.S.A. Note: Please pack the 6150 in a carton prior to shipping. Do not ship without proper packing. Warranty will be void if the 6150 is shipped without proper packing.
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