barfield DPS1000 Operator's manual

Copyright © 2017 Barfield Inc. All Rights Reserved.
DPS1000
RVSM Pitot-Static Test Set
USER INSTRUCTION MANUAL
M/N DPS1000, P/N: 101-01175
Doc. P/N: 56-101-01175
Revision I
October 10, 2017
____________________________________

56-101-01175 Revision I Page | ii
Corporate Headquarters
4101 Northwest 29thStreet
Miami, Florida 33142
www.barfieldinc.com
Barfield Inc. Confidential and Proprietary Information.
This document and all the information contained herein is the sole property of Barfield Inc.
No intellectual property rights are granted by the delivery of this document or the disclosure of its content.
This entire document is proprietary information and shall not be reproduced or disclosed to a third party without
the express written consent of Barfield Inc.
This document and its content shall not be used for any purpose other than that for which it is supplied.

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SAFETY
Before using this instrument the operator should read and understand all of the related data. This
includes the applicable local safety procedures, this publication and the instructions for the
accessories/options/equipment you are using it with and the system or components under test.
This equipment was designed to be safe when used as per the procedures of this Instruction
Manual.
Before you start an operation or procedure in this publication, make sure you have the required
skills (if necessary, with qualifications from an approved training establishment).
Follow good engineering practice at all times.
WARNING: A WARNING notice indicates a hazard with a potential for property damage,
personal injury or death if the instructions are not followed. The operator should not
proceed beyond the WARNING notice until required conditions are understood and
fully complied with.
CAUTION: A CAUTION notice indicates a hazard with a potential for damage to the equipment
and or loss of data if the instructions are not followed. The operator should not
proceed beyond the CAUTION notice until required conditions are understood and
fully complied with.
WARNINGS
WARNING: Do not use this equipment when it is not in its normal condition.
WARNING: When testing with this equipment follow the appropriate procedures as per the AMM
or CMM observing all safety instructions.
WARNING: Do not use this equipment for purposes other than as specified in this manual.
WARNING: Do not use this equipment in a wet environment.
WARNING: Do not use this equipment in an atmosphere of explosive gas.
WARNING: This test equipment shall only be serviced by authorized personnel.
CAUTIONS
CAUTION: Inspect the aircraft Static Vents for dirt or debris before making any connections.
CAUTION: Inspect the aircraft Pitot Probes for dirt or debris before making any connections.
CAUTION: Do not connect this equipment to a contaminated aircraft pitot-static system.
CAUTION: To prevent damage to this equipment, do not allow water or other contaminants to
be introduced into the ports.
CAUTION: When equipment is connected to the hoses, exercise care not to stand on, or in
anywise kink the hoses.

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CAUTION: Always monitor aircraft instruments to Ensure the maximum rates of change are not
exceeded.
CAUTION: Failure to follow procedures as written could produce a negative airspeed condition
capable of damaging the aircraft instruments.
SYMBOLS ON THE INSTRUMENT
Warning –Read and
understand operator’s manual
before using this machine

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ATTENTION
Although every effort has been made to provide the end user of this equipment with the most
current and accurate information, it may be necessary to revise this manual in the future. Please
be sure to complete and return the enclosed OWNER WARRANTY REGISTRATION CARD to
Barfield in order to validate the warranty and to ensure that you will receive updated information
when published. You MUST have your name and address on file at Barfield as a registered user
of this equipment to be able to obtain the service covered by the warranty.
Visit the company website, http://barfieldinc.com/, for publication updates.
Please send the Registration Card to:
Barfield, Inc.
P.O. Box 025367
Miami, FL 33102-5367
USA
CONTACT INFORMATION
Users are requested to notify the manufacturer of any discrepancy, omission, or error found in this
manual. Inquiries should include specific questions and reference the publication title, number,
chapter, page, figure, paragraph, and effective date.
Please send comments to:
TECHNICAL CUSTOMER SUPPORT - GSTE
BARFIELD, INC.
P.O. BOX 025367
MIAMI, FL 33102-5367
USA
Telephone (305) 894-5400
(800) 321-1039
Fax (305) 894-5401
Email gsesales@barfieldinc.com

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REVISION RECORD
REV.
ECO #
REV. DATE
DESCRIPTION OF CHANGE
A
May 28, 2014
Initial Release
B
260-01041
October 15, 2014
Update Barfield logo and warranty
C
260-01092
March 18, 2015
Completely Revised
D
260-01118
August 11, 2015
TOC Page vii, Chapter #s Pages 54 & 55
E
260-01135
October 29, 2015
Update navigation screens and introduce OPT-A
F
260-01175
October 17, 2016
Updated Format & Logo, Updated Approved
Repair Facility Information, Added new software
upload procedure from latest released app.
Added Cabin Pressure Mode. Added IBF Mode.
G
260-01184
November 7, 2016
Updated with software six month note reminder
H
260-01200
May 12, 2017
Updated page numbers, format and “custom limit”
deletion note.
I
260-01213
October 10, 2017
TOC reformatted. Operating limits modified.
Software Update procedure modified.

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MAINTENANCE AND REPAIR INFORMATION
The manufacturer of this equipment does not recommend the user to attempt any maintenance or
repair. In case of malfunction, contact the manufacturer to obtain the list of approved repair
facilities worldwide, ensuring that this equipment will be serviced using proper procedures and
certified instruments.
BARFIELD PRODUCT SUPPORT
DIVISION
Shipping Address:
Telephone (305) 894-5400
(800) 321-1039
Fax (305) 894-5401 (305) 894-5401
Barfield, Inc.
4101 NW 29th Street
Miami, Florida 33142
USA
Mailing Address:
Barfield, Inc.
P.O. Box 025367
Miami, FL 33102-5367
USA
Vector Aerospace
Shipping Address:
Telephone 33 (0)1 30 18 53 48
Fax 33 (0)1 30 18 53 45
Vector Aerospace
1 Boulevard du 19 Mars 1962 –BP50064
F95503 GONESSE Cedex,
France

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TABLE OF CONTENTS
Safety
Cautions
Attn / Cont
Rev / Maint
Table of Contents
List of Figures and Tables
PAGE
INTRODUCTION......................................................................................................................... 13
1. PUBLICATION BREAKDOWN.....................................................................................13
2. INFORMATION PROVIDED WITH THE TEST SET .....................................................13
3. RECERTIFICATION.....................................................................................................14
4. SOFTWARE UPDATE ....................................................................................................14
CHAPTER 1: GENERAL............................................................................................................. 16
1. INTENDED USE...........................................................................................................16
2. SPECIFICATIONS........................................................................................................16
3. INSTRUCTIONS FOR USE ..........................................................................................19
4. TECHNICAL ASSISTANCE .........................................................................................19
CHAPTER 2: RATINGS............................................................................................................. 20
1. SUPPLY VOLTAGES...................................................................................................20
2. CONNECTION DESCRIPTION.....................................................................................20
3. ENVIRONMENTAL.......................................................................................................20
CHAPTER 3: INSTALLATION................................................................................................... 21
1. ASSEMBLY..................................................................................................................21
2. GROUNDING (EARTHING)..........................................................................................22
3. ELECTRICAL CONNECTIONS....................................................................................23
4. VENTILATION / DRAINAGE........................................................................................23
5. PNEUMATIC PRESSURE CONNECTIONS.................................................................24
CHAPTER 4: OPERATION........................................................................................................ 25
1. OPERATING CONTROLS............................................................................................25
2. POSITIONING..............................................................................................................26
3. ACCESSORIES............................................................................................................26
4. PREPARATION............................................................................................................29
5. POWER ON INITIALIZATION ......................................................................................29
6. OPERATING MODES ..................................................................................................30
7. TEST SET CONFIGURATION STATUS DISPLAY ......................................................31

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8. USER INTERFACE MENU AND DISPLAY..................................................................33
10. TEST SET LEAK TEST................................................................................................52
11. AIRCRAFT TESTING...................................................................................................57
12. ENGINE PRESSURE RATIO (EPR) TEST...................................................................71
13. SHUTDOWN PROCEDURE.........................................................................................73
CHAPTER 5: RECEIVING, SHIPPING, AND STORAGE........................................................... 75
1. RECEIVING..................................................................................................................75
2. SHIPPING ....................................................................................................................75
3. STORAGE....................................................................................................................75
CHAPTER 6: MAINTENANCE................................................................................................... 76
1. GENERAL....................................................................................................................76
2. PREVENTATIVE ..........................................................................................................76
3. TROUBLESHOOTING .................................................................................................76
4. CALIBRATION.............................................................................................................76
Appendix A: Abbreviations & Glossary................................................................................... 77
Appendix B: Operating Limits .................................................................................................. 79
Appendix C: DPS1000 Internal Pneumatic Diagram................................................................ 82
Appendix D: Menu Navigation.................................................................................................. 83
Appendix E: Cabin Pressure Mode .......................................................................................... 84
Appendix F: IBF System Mode ................................................................................................. 92
Appendix G: Field Firmware Update Procedure via USB and Barfield ADTS App................ 98

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LIST OF FIGURES
FIGURE 1 IDENTIFICATION LABEL.......................................................................................... 13
FIGURE 2 OWNER WARRANTY REGISTRATION CARD......................................................... 14
FIGURE 3LIMITED 2 YEAR WARRANTY................................................................................. 15
FIGURE 4 POWER ENTRY MODULE ........................................................................................ 20
FIGURE 5 CASE DIMENSIONS................................................................................................. 21
FIGURE 6 OPTIONAL TRAVEL / SHIPPING CASE.................................................................... 22
FIGURE 7 POWER SUPPLY CABLE......................................................................................... 23
FIGURE 8 DO NOT OBSTRUCT VENTS................................................................................... 23
FIGURE 9 HUMID AIR EXHAUST.............................................................................................. 23
FIGURE 10 DPS1000 PRESSURE CONNECTIONS ................................................................. 24
FIGURE 11 DPS1000 FRONT PANEL........................................................................................ 25
FIGURE 12 INSTRUCTION MANUAL, P/N 56-101-01175......................................................... 27
FIGURE 13 ELECTRICAL CABLE, P/N AE9887-ND.................................................................. 27
FIGURE 14 HOSE KIT ............................................................................................................... 27
FIGURE 15 ANTENNA, P/N 126-00001...................................................................................... 28
FIGURE 16 CARRYING BAG, P/N 195-00021............................................................................ 28
FIGURE 17 AN4 CAPS WITH LANYARD, P/N 176-00001 (OPT-A)........................................... 28
FIGURE 18 POWER ON INITIALIZATION DISPLAY .................................................................. 29
FIGURE 19 DEFAULT 2-CHANNEL (DUAL PS, PT) MODE ...................................................... 31
FIGURE 20 OPTIONAL 1-CHANNEL (PT ONLY) MODE............................................................ 31
FIGURE 21 TEST SET CONFIGURATION INFORMATION DISPLAYED................................. 32
FIGURE 22 DISPLAY SETUP AERONAUTICAL MENU ........................................................... 33
FIGURE 23 TARGET VALUE KEYPAD SCREEN...................................................................... 34
FIGURE 24 DISPLAY SETUP: 4-PARAMETER FORMAT ......................................................... 34
FIGURE 25 DISPLAY SETUP:2-PARAMETER FORMAT......................................................... 35
FIGURE 26 DISPLAY UNITS –FOR AERONAUTICAL MODE.................................................. 35
FIGURE 27 DISPLAY UNITS –FOR PRESSURE UNITS MODE .............................................. 36
FIGURE 28 LEAK TESTING MENU........................................................................................... 36
FIGURE 29 LEAK RATE TIMER RESULTS............................................................................... 37
FIGURE 30 SELECT ATP LEAK TEST PROFILE...................................................................... 38
FIGURE 31 ATP LEAK TEST - PARAMETER PROFILE SCREEN............................................ 39
FIGURE 32 ATP LEAK TEST RESULTS SCREEN.................................................................... 39
FIGURE 33 GO TO GROUND CONFIRM SCREEN................................................................... 40
FIGURE 34 CONCLUSION OF GO TO GROUND ..................................................................... 40
FIGURE 35 CONCLUSION OF GO TO GROUND ..................................................................... 41
FIGURE 36 SETUP 1................................................................................................................. 41
FIGURE 37 ALTITUDE CORRECTION SCREEN ...................................................................... 42
FIGURE 38 ALTITUDE CORRECTION ON-AIRCRAFT............................................................. 43
FIGURE 39 ALTITUDE CORRECTION KEYPAD........................................................................ 43
FIGURE 40 TEST SET CONFIGURATION, UPDATED ALTITUDE CORRECTION................... 44
FIGURE 41 SETUP 1 CONTROL MODE(S)............................................................................... 44
FIGURE 42 SETUP 2 - SELECTING LIMIT FILE TO EDIT......................................................... 45
FIGURE 43 SETUP 2 –EDIT CUSTOM LIMITS......................................................................... 46
FIGURE 44 DELETE CUSTOM LIMITS ..................................................................................... 47
FIGURE 45 BACKLIGHT ADJUSTMENT................................................................................... 48
FIGURE 46 DPS1000 FRONT PANEL........................................................................................ 49
FIGURE 47 INITIALIZATION DISPLAY...................................................................................... 50
FIGURE 48 LEAK TESTING MENU(S) ...................................................................................... 52
FIGURE 49 SELECTING ATP LEAK TEST PROFILE............................................................... 53
FIGURE 50 LEAK TEST PROFILE - PARAMETERS SCREEN ................................................ 53
FIGURE 51 MEASURE TIME VS LEAK TIME............................................................................ 54

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FIGURE 52 LEAK RATE TIMER, UNIT SAFE AT GROUND...................................................... 55
FIGURE 53 ATP LEAK TEST.................................................................................................... 56
FIGURE 54 ATP LEAK TEST RESULTS................................................................................... 57
FIGURE 55 UNIT SAFE AT GROUND....................................................................................... 60
FIGURE 56 LEAK TEST RESULTS............................................................................................ 62
FIGURE 57 CONFIRM GO TO GROUND .................................................................................. 73
FIGURE 58 UNIT SAFE AT GROUND....................................................................................... 73
Figure E 1Main Menu Screen………….…………………………………..……………………...........85
Figure E 2Numbered Keypad Screen….….…………………………………………………...………85
Figure E 3Setup 2 Screen………….……………………………………………………………...…….86
Figure E 4Disabled Cabin Pressure Mode…………….………..……….…………………………...86
Figure E 5Enabled Cabin Pressure Mode….…………………………………………………………87
Figure E 6Initialization Screen…….…………………………………………………………………...87
Figure E 7Cabin Pressure Mode –Step 1…….…………………………………….……………....88
Figure E 8DPS1000 & 1811NG Connection Ports….………………………………………………...88
Figure E 9Warning Screen…….………………………………………………………………………...89
Figure E 10 Cabin Pressure Mode –Step 2……….………………………………………...………...89
Figure E 11 Cabin Pressure Mode –Step 3….………………………………………………...……...90
Figure E 12 Cabin Pressure Mode –Warning Screen….………………………………………...…..90
Figure E 13 Cabin Pressure Mode –Measuring Cabin Pressure and Rate………………………..91
Figure E 14 Cabin Pressure Mode –Step 2………….………...……………………………………...91
Figure E 15 Cabin Pressure Mode –Venting Process...…..………………………………………….92
Figure E 16 Cabin Pressure Mode –Step 2…………………………...……………………….……...92
Figure F 1 Low Pressure Hose…………………………………………………………………………..93
Figure F 2 Main Menu, Page 2…..………...…………………………………………………………….94
Figure F 3 Additional Functions Screen….……………………………………………………………..94
Figure F 4 IBF Step 1 Screen….…...……………………………………………………………………95
Figure F 5 Warning Screen…….…...……………………………………………………………………95
Figure F 6 IBF Step 2 Screen……………………………………………………………………………96
Figure F 7 IBF Control Mode Screen…………………………………………………………………...96
Figure F 8 Keypad Screen…….……………...………………………………………………………….97
Figure F 9 Vent to Ambient Screen…….…………………………………………………………….....97
Figure F 10 Unit Safe at Ground….……………………………………………………………………..98
LIST OF TABLES
TABLE 1 PHYSICAL CHARACTERISTICS................................................................................ 16
TABLE 2 ENVIRONMENTAL..................................................................................................... 16
TABLE 3 AERONAUTICAL SPECIFICATIONS.......................................................................... 17
TABLE 4 PRESSURE UNITS SPECIFICATIONS...................................................................... 17
TABLE 5 DISPLAY UNITS......................................................................................................... 18
TABLE 6 ENGINE PRESSURE RATIO TEST TABLE................................................................ 72
TABLE 7 AERONAUTICAL LIMITS PROFILE –(DEFAULT)..................................................... 79
TABLE 8 AERONAUTICAL LIMITS PROFILE –(MAX).............................................................. 79
TABLE 9 PRESSURE LIMITS PROFILE –(DEFAULT)............................................................. 80
TABLE 10 PRESSURE LIMITS PROFILE –(MAX).................................................................... 80
TABLE 11 EPR LIMITS PROFILE –(DEFAULT) ....................................................................... 81
TABLE 12 EPR LIMITS PROFILE –(MAX)................................................................................ 81

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INTRODUCTION
1. PUBLICATION BREAKDOWN
This user instruction manual establishes the standards of operation for the DPS1000 Pitot-
Static Test Set.
Its purpose is to provide sufficient information for the personnel unfamiliar with this unit to
understand it, identify its parts, and operate it in accordance with proper procedures,
operating techniques, precautions and limitations.
Note: The manufacturer has designed this equipment to be safe when operated using the
procedures and instructions detailed in this manual. Do not use this equipment for any
other purpose than that stated, as the protection provided by the equipment may be
impaired.
2. INFORMATION PROVIDED WITH THE TEST SET
In addition to this User Instruction Manual, the Test Set is delivered with the four information
items described below.
A. The identification label, example (Figure 1), located on the front bulkhead of the Test
Set, provides the following information:
Manufacturer Name
Designation of Equipment
Equipment Part Number
Equipment Model Number Equipment Serial Number
Equipment Modification (if applicable) Equipment Options (if applicable)
Figure 1 Identification Label

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B. The Owner's Warranty Registration card (Figure 2), is to be completed by the owner and
returned to Barfield, Inc. within ten (10) days of purchase to ensure automatic update of
printed matter and validation of warranty.
Figure 2 Owner Warranty Registration Card
C. Each new or re-certified unit is delivered with a Certificate that shows the date when the
unit was tested by the manufacturer, its serial number and when the next certification is
due. This certificate confirms that the unit performed according to its design
specifications.
D. The DPS1000 Limited Two Year Warranty can be seen in Figure 3.
3. RECERTIFICATION
A. The Test Set has a one-year recertification requirement. Maintenance required by this
unit must be performed by qualified technicians in a shop equipped with the necessary
tooling and resources. Contact Barfield for Maintenance and Calibration requirements.
B. At the conclusion of the power up initialization the DPS1000 will display the date when it
was “Last Calibrated” in the format of Day–Month-Year and will provide the user with
the number of days remaining before its calibration due date with a statement of “Cal
due” in ### days format.
CAUTION: Recertification by a calibration/repair shop not possessing the necessary
technical knowledge, documentation, special test equipment, tooling and
standards will adversely affect the accuracy/capability of the DPS1000 for
testing the aircraft, including the demanding Reduced Vertical Separation
Minimum (RVSM) accuracy requirement.
4. SOFTWARE UPDATE
A pop up window will appear every six (6) months on the screen reminding the user to
update the software. Press “continue” to proceed with the update. Please, check
Barfield’s website regularly for the latest software updates and releases. Also, sign up
for automatic updates of Barfield ADTS app.

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DPS1000/1811NG LIMITED TWO YEAR WARRANTY
BARFIELD INC. ("BARFIELD") warrants only to the original Purchaser of this DPS1000/1811NG product
from BARFIELD or an authorized distributor that this product will be free from defects in material and
workmanship under normal use and service for two years after date of purchase. BARFIELD reserves the
right, before having any obligation under this limited warranty, to inspect the damaged BARFIELD product,
and all costs of shipping the DPS1000/1811NG product to BARFIELD for inspection shall be borne solely
by the Purchaser. In order to recover under this limited warranty, Purchaser must make claim to BARFIELD
within 60 days of occurrence, and must present acceptable proof of original ownership (such as a purchase
order, invoice, warranty card registration, or other documentation BARFIELD deems acceptable) for the
DPS1000/1811NG product. BARFIELD, at its option, shall repair or replace the defective unit covered by
this warranty. Please retain the dated sales receipt as evidence of the original purchaser's date of
purchase. You will need it for any warranty service. In order to keep this limited warranty in effect, the
DPS1000/1811NG product must have been handled and used as prescribed in the instructions
accompanying this product. This limited warranty does not cover any damage due to accident, misuse,
abuse or negligence. This limited warranty is non‐transferable and does not apply to any purchaser who
bought the DPS1000/1811NG product from a reseller or distributor not authorized by BARFIELD, including
but not limited to purchases from internet sites. This warranty does not affect any other legal rights you may
have by operation of law. Contact BARFIELD at www.Barfieldinc.com or customer service at (305) 894‐
5506 for warranty service procedures.
DISCLAIMER OF WARRANTY
EXCEPT FOR THE LIMITED WARRANTY PROVIDED HEREIN, TO THE EXTENT PERMITTED BY LAW,
BARFIELD DISCLAIMS ALL WARRANTIES, EXPRESS OR IMPLIED, INCLUDING ALL WARRANTIES
OF MERCHANTABILITY AND/OR FITNESS FOR A PARTICULAR PURPOSE. TO THE EXTENT THAT
ANY IMPLIED WARRANTIES MAY NONETHELESS EXIST BY OPERATION OF LAW, ANY SUCH
WARRANTIES ARE LIMITED TO THE DURATION OF THIS WARRANTY. SOME STATES/PROVINCES
DO NOT ALLOW LIMITATIONS ON HOW LONG AN IMPLIED WARRANTY LASTS, SO THE ABOVE
LIMITATIONS MAY NOT APPLY TO YOU.
LIMITATION OF LIABILITY
REPAIR OR REPLACEMENT OF THIS PRODUCT, AS PROVIDED HEREIN, IS YOUR EXCLUSIVE
REMEDY. BARFIELD SHALL NOT BE LIABLE FOR ANY SPECIAL, INCIDENTAL OR CONSEQUENTIAL
DAMAGES, INCLUDING, BUT NOT LIMITED TO, LOST REVENUES, LOST PROFITS, LOSS OF USE OF
SOFTWARE, LOSS OR RECOVERY OF DATA, RENTAL OF REPLACEMENT EQUIPMENT,
DOWNTIME, DAMAGE TO PROPERTY, AND THIRD‐PARTY CLAIMS, ARISING OUT OF ANY THEORY
OF RECOVERY, INCLUDING WARRANTY, CONTRACT, STATUTORY OR TORT. NOTWITHSTANDING
THE TERM OF ANY LIMITED WARRANTY OR ANY WARRANTY IMPLIED BY LAW, OR IN THE EVENT
THAT ANY LIMITED WARRANTY FAILS OF ITS ESSENTIAL PURPOSE, IN NO EVENT WILL
BARFIELD'S ENTIRE LIABILITY EXCEED THE PURCHASE PRICE OF THIS PRODUCT. SOME
STATES/PROVINCES DO NOT ALLOW THE EXCLUSION OR LIMITATION OF INCIDENTAL OR
CONSEQUENTIAL DAMAGES, SO THE ABOVE LIMITATION OR EXCLUSION MAYNOT APPLY TO
YOU. THIS WARRANTY GIVES YOU SPECIFIC LEGAL RIGHTS AND YOU MAY ALSO HAVE OTHER
RIGHTS THAT VARY FROM STATE TO STATE AND PROVINCE TO PROVINCE.
BARFIELD INC.
4101 NW 29th Street
Miami, Florida 33142, USA
Form 7.5.3‐20
Dated 01/07/2015, Rev. 2
Figure 3Limited 2 Year Warranty

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CHAPTER 1: GENERAL
1. INTENDED USE
A. The BARFIELD INC. DPS1000 Imperium Series (P/N: 101-01175) is a self-contained
flight line Pitot-Static Test Set. The DPS1000 provides complete measurement and
pneumatic control for performing leak testing, functional tests of air data instruments,
components and systems.
B. The DPS1000 Digital Pitot Static Test Set meets the demanding RVSM accuracy
requirement of ± 0.003 inHg and compliance requirements of 91.171.
2. SPECIFICATIONS
A. Physical Characteristics
Size (H, W, L)
9.0 in. (22.86 cm), 14.8 in. (37.6 cm), 22.2 in. (56.38 cm)
Weight
35 lbs. (15.9 kg)
Table 1 Physical Characteristics
B. Environmental
Operating Altitude
7,000 ft (2,134 m)
Operating Temp.
0°C to 50°C (32°F to 122°F)
Storage Temp.
-20°C to 60°C (-4°F to 140°F)
Operating Humidity
0 to 90% RH (non-condensing)
Power
100-120/200-240VAC, 50/60Hz, 400VA
Table 2 Environmental

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C. Performance
Aeronautical (DPS1000)
Ps Channel
Altitude
ALT
Rate of Climb
ROC
Pt Channel
Calibrated Airspeed
CAS
Rate of CAS
RtCAS
Mach
Units
Feet
ft/min
knots (kts)
kts/min
-
Operating
Range (*3)
-1,800 to 55,000
0 to 20,000
0 to 6,000 (*1)
0 to 650
50 to 600 (*2)
0 to 2.8
Accuracy
0.01% FS
± 3 ft @ 0 ft
± 6 ft @ 20,000 ft
± 8 ft @ 30,000 ft
± 14 ft @ 45,000 ft
± 22 ft @ 52,500 ft (*3)
± 29 ft @ 53,000 ft (*3)
± 22 ft @ 55,000 ft
± 2 % of value
± 1.0 kts @ 20 kts
± 0.5 kts @ 50 kts
± 0.2 kts @ 650 kts
± 2 % of value
Better than
± 0.005
MACH > 0.1
Repeatability
0.0025% FS
± 1 ft @ 0 ft
± 2 ft @ 20,000 ft
± 2 ft @ 30,000 ft
± 4 ft @ 45,000 ft
± 6 ft @ 52,500 ft
-
± 0.5 kts @ 20 kts
± 0.2 kts @ 50 kts
± 0.1 kts @ 650 kts
-
0.001 rising
to 0.005
Resolution
1
1
0.1
1
0.001
Stability (12
month) (*4)
0.01% FS
-
0.025% FS
-
-
Table 3 Aeronautical Specifications
Note (*1): ROC (with 125 cu.in volume)
Note (*2): RtCAS (with 75 cu.in volume) Default: 300 kts/min operating in Aeronautical mode.
Note (*3): If MOD “B” is designated, operating range is 55,000 ft, accuracy specification declared
up to 53,000 ft.
If MOD “B” is not designated, operating range and accuracy specification is ± 22 ft @
55,000 ft.
Note (*4): This tolerance represents the stability over a 12 month period. If tighter tolerances
are required, the calibration interval should be reduced or proof of stability should be
established.
Pressure Units (DPS1000)
Ps
Channel
Ps
Rate of Change
ROC
Qc
Channel
(Note: Pt = Qc + Ps)
RtQc
Rate of Qc
EPR
Units
inHg (abs)
inHg/min
inHg (diff)
inHg/min
Ratio: Pt7/Pt2
Operating Range
2.693 to 38.0
0.1 to 16
0.0 to 40 (*7)
0.5 to 10
0.1 to 10
Calibrated Range
3.040 to 38.0
0.1 to 16
0.0 to 40 (*7)
0.5 to 10
0.1 to 10
Accuracy
0.01% FS
± 0.003 inHg
± 2 % of value
± 0.020 inHg (*5)
± 2% of value
0.01
Repeatability
± 0.002 inHg
-
0.001 rising to 0.005
-
-
Resolution
0.0001
-
0.0001
-
1.000
Stability (12 mo.) (*6)
0.01% FS
-
0.025 % FS
-
-
Table 4 Pressure Units Specifications

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Note (*5): Regarding Qc Channel: Specification based on typical accuracy(0.05% FS). Maximum
error is 0.10% FS
Note (*6): This tolerance represents the stability over a 12 month period. If tighter tolerances
are required, the calibration interval should be reduced or proof of accuracy/stability
should be established.
Note (*7): Pt max = Ps max + Qc max = 38.0 + 40.0 = 78 inHg
Note: Accuracy specifications are based on performing the 12 month Recertification cycle
when connected to a leak tight system.
Specifications are subject to change without notice.
D. Display Units
CAS
kts, km/h, mph
ALT
ft , m
MACH
n/a (dimensionless ratio)
ROC
ft/min, m/min
Pt, Ps, Qc
inHg, mbar, psia, psid, kPa, mmHg, inH2O@4°C, inH2O@20°C,
inH2O@60°F
EPR
ratio (Pt/Ps), inHg, mbar, psia, psid, kPa, mmHg, inH2O@4°C,
inH2O@20°C, inH2O@60°F
Table 5 Display Units
E. Pressure Media
Two internal high reliability electric pumps generate the required pressure and vacuum.
The 4-head vacuum pump is configured to provide each channel (Ps & Pt) with its own
dedicated 2-headed vacuum source. The pressure pump is a single head unit and
supplies both channels (Ps & Pt) with a common pressure supply.
F. Transducers
The Ps channel uses an absolute pressure transducer while the Pt channel uses a
differential pressure transducer.
G. Input Power
Electronic switcher power supply module with auto input voltage detection circuitry for an
A/C input voltage of 100-120/200-240VAC @ 50-60Hz.
H. Fuse Protection
Fuse overload protection is provided by a Miniature Fuse, 5 x 20 mm, Time-Lag T, L, 250
VAC, 4A is installed on the fuse compartment of the power entry module.
Note: For 200-240 VAC Operation, 5x20 mm, Time-Lag T, L, 250 VAC @ 2A is
recommended.

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3. INSTRUCTIONS FOR USE
A. With the Barfield DPS1000 Pitot and Static ports connected via the hoses (included) and
mating aircraft adapters (not included) to their respective ports on the aircraft, the user is
able to enter pressures or equivalent aeronautical values using the Test Set’s touch
screen input display to drive the aircraft system to the required points of test.
B. Optionally the DPS1000 Test Set can be controlled using a Wi-Fi enabled tablet (not
supplied) as a wireless remote control device. The tester can be used with either an
Android or iOS tablet. Barfield provides a custom App which is available as a free
download from the Google Play Store and the Apple App Store. The tablet display will
exactly mirror that of the tester so that the transition to remote control is seamless. Please
refer to Appendix E for the Tablet App Wi-Fi Connect Procedure.
C. Please refer to Chapter 4 OPERATIONS for complete operating instructions.
D. Please refer to Appendix D for the Menu Navigation.
4. TECHNICAL ASSISTANCE
A. For technical assistance on the Barfield DPS1000, please contact Barfield Inc. at:
TECHNICAL CUSTOMER SUPPORT - GSTE
BARFIELD, INC.
P.O. BOX 025367
MIAMI, FL 33102-5367
USA
Telephone (305) 894-5400
(800) 321-1039
Fax (305) 894-5401
Email gsesales@barfieldinc.com

56-101-01175 Revision I Page | 20
CHAPTER 2: RATINGS
1. SUPPLY VOLTAGES
A. The Barfield DPS1000 Pitot Static Test Set may be powered from either 100 to 120 VAC
@ 50 or 60 Hz, 400 VA, or from 200 to 240 VAC @ 50 or 60 Hz, 400 VA.
2. CONNECTION DESCRIPTION
A. Power Entry - the power entry module pictured in Figure 4 is a connector Style IEC 320-
C14 module with an Illuminated ON/OFF Switch and equipped with an internal fuse
holder.
Figure 4 Power Entry Module
B. The tester must be connected to the correct electrical power supply as stated beneath
the power connector.
CAUTION: The supply must provide connection to a protective ground terminal. The
unit must always be connected to the supply ground.
3. ENVIRONMENTAL
A. Altitude: 7,000 ft (2,134 m)
B. Operating Temp: 0°C to 50°C (32°F to 122°F)
C. Storage Temp: -20°C to 60°C (-4°F to 140°F)
D. Operating Humidity: 0 to 90% RH (non-condensing)
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