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barfield 1811NG User Manual

barfield 1811NG
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Copyright © 2020 Barfield Inc. All Rights Reserved.
1811NG
Pitot-Static Test Set
USER INSTRUCTION MANUAL
M/N 1811NG, P/N: 101-01178
Doc. P/N: 56-101-01178
Revision K
September 2, 2020
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Table of Contents

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barfield 1811NG Specifications

General IconGeneral
DescriptionDigital Pressure Gauge
TypeDigital
Liquid FilledNo
Connection1/4" NPT
Dial SizeNot applicable
Temperature Range-10°C to 50°C

Summary

INTRODUCTION

PUBLICATION BREAKDOWN

Overview of the manual's purpose and content structure.

INFORMATION PROVIDED WITH THE TEST SET

Details the items included with the test set, such as manuals and labels.

RECERTIFICATION

Explains the required recertification process and its importance for accuracy.

MOBILE DEVICE’S APP INFORMATION

Information on downloading and using the mobile app for remote control.

SOFTWARE UPDATE

Guidance on checking for and applying software updates to the test set.

TEST SET EQUIVALENT

Lists aircraft applications for which the test set is a suitable substitute.

LIMITED TWO YEAR WARRANTY

CHAPTER 1: GENERAL

INTENDED USE

Specifies the primary purpose and applications of the 1811NG Pitot-Static Test Set.

SPECIFICATIONS

Outlines the physical, environmental, conformity, performance, and display unit specifications.

INSTRUCTIONS FOR USE

Provides guidance on connecting and operating the test set with aircraft systems.

TECHNICAL ASSISTANCE

Contact information and procedures for obtaining technical support for the 1811NG.

CHAPTER 2: RATINGS

SUPPLY VOLTAGES

Specifies the acceptable input power voltage and frequency ranges for the test set.

CONNECTION DESCRIPTION

Describes the power entry module and its components, including safety notes.

ENVIRONMENTAL

Details the operating and storage environmental conditions for the test set.

CHAPTER 3: INSTALLATION

ASSEMBLY

Instructions for unpacking, checking contents, and assembling the test set and its components.

GROUNDING (EARTHING)

Procedures for safely grounding the test set chassis to the aircraft or test instrument.

ELECTRICAL CONNECTIONS

Details the power supply cable and its specifications for connecting the test set.

VENTILATION / DRAINAGE

Information on keeping intake and exhaust vents clear and the humid air exhaust port.

PNEUMATIC PRESSURE CONNECTIONS

Specifies the Pitot (Pt) and Static (Ps) port connections using AN4 fittings.

CHAPTER 4: OPERATION

OPERATING CONTROLS

Identifies and describes the front panel switches, ports, and display components.

POSITIONING

Guidelines for positioning the test set safely for operation and quick disconnection.

ACCESSORIES

Lists included items and items not included with the test set package.

PREPARATION

Recommendations for familiarizing with the interface before connecting to aircraft systems.

POWER ON INITIALIZATION

Describes the sequence and information displayed during the test set's power-on process.

OPERATING MODES

Explains the 2-channel (Ps & Pt) and 1-channel (Pt-Only) operating modes.

TEST SET CONFIGURATION STATUS DISPLAY

Details how to interpret the status display for mode, limits, and altitude correction.

USER INTERFACE MENU AND DISPLAY

Explains the structure and navigation of the test set's graphical user interface.

DISPLAY SETUP

Instructions on configuring display format and selecting units of measure.

LEAK TESTING

Overview of the two leak testing methods: Leak Rate Timer and ATP Leak Test.

CONTROL MODE

Explains the Pneumatic Control Module (PCM) operation and its two-channel control.

TEST SET LEAK TEST

PRELIMINARY SETUP

Steps to prepare the test set and hoses for leak testing before use.

STATIC AND PITOT TEST SET LEAK TEST

Procedures for performing leak tests on the test set and hoses themselves.

APPLYING LEAK CORRECTION

How to record and subtract test set/hose leakage from aircraft test results.

AIRCRAFT TESTING

PRELIMINARY SETUP

Essential checks and connections before performing aircraft system tests.

LEAK TESTING - COMBINED ALT & CAS

Procedures for leak testing combined ALT & CAS using traditional or ATP methods.

TESTING THE AIRCRAFT STATIC SYSTEM

Detailed steps for testing the aircraft's static pressure system.

TESTING THE AIRCRAFT PITOT SYSTEM

Detailed steps for testing the aircraft's pitot pressure system.

COMBINE TESTING OF THE AIRCRAFT PITOT AND STATIC SYSTEM

Instructions for simultaneously testing both pitot and static systems.

MACH TEST AND CONSTANT MACH

How to perform tests with constant Calibrated Airspeed or constant Mach.

AIRSPEED SWITCH TEST

Procedure for testing airspeed switches using the Nudge feature.

ENGINE PRESSURE RATIO (EPR) TEST

PRELIMINARY

Steps to connect the test set and prepare for EPR transmitter testing.

TEST

Methods for performing EPR testing using aeronautical units or EPR mode.

SHUTDOWN PROCEDURE

TEST SET SHUTDOWN PROCEDURE

Steps to safely shut down the test set and return it to ambient pressure.

CHAPTER 5: RECEIVING, SHIPPING, AND STORAGE

RECEIVING

Recommendations for inspecting the test set upon receipt and retaining packaging.

SHIPPING

Guidelines for properly packing and preparing the test set for reshipment.

STORAGE

Instructions for storing the test set in a cool, dry place with desiccant.

CHAPTER 6: MAINTENANCE

GENERAL

Manufacturer's recommendation against user maintenance and for contacting approved facilities.

PREVENTATIVE

Routine visual inspections and checks for moisture or foreign matter.

TROUBLESHOOTING

Steps for recording error codes or noting issues during unit malfunction.

CALIBRATION

Information on the annual calibration interval and the importance of qualified service.

APPENDIX A: ABBREVIATIONS & GLOSSARY

APPENDIX B: OPERATING LIMITS

APPENDIX C: 1811NG INTERNAL PNEUMATIC DIAGRAM

APPENDIX D: MENU NAVIGATION

APPENDIX E: WI-FI CONNECTION PROCEDURE

ESTABLISHING WI-FI CONNECTION WITH ANDROID DEVICE

Step-by-step guide to connect the test set to an Android device via Wi-Fi.

ESTABLISHING WI-FI CONNECTION WITH APPLE DEVICE

Step-by-step guide to connect the test set to an Apple device via Wi-Fi.

APPENDIX F: CABIN PRESSURE MODE

ENABLING CABIN PRESSURE MODE

Instructions for activating the Cabin Pressure Mode feature on the test set.

USING “CABIN PRESSURE MODE” IN AIRCRAFT

Procedures for operating the test set in Cabin Pressure Mode during aircraft testing.

APPENDIX G: IBF SYSTEM MODE

ACCESSING IBF SYSTEM MODE

Steps to access and configure the Inlet Barrier Filter (IBF) system mode.

APPENDIX H: FIELD FIRMWARE UPDATE PROCEDURE VIA USB & BARFIELD ADTS APP

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