Kratos - 115.115,-1,3,4
Kratos - 115.115,-1,3,4
Pasadena, California
POTABLE WATER
QUANTITY INDICATOR
WITH
THE CONTENT OF THIS PUBLICATION IS THE PROPERTY OF, AND CONTAINS INFORMATION PROPRIETARY TO ROGERSON
AIRCRAFT CORPORATION. IN ORDER TO MINIMIZE THE POSSIBILITY OF OBSOLETE DATA BEING USED FOR MAINTENANCE.
OVERHAUL, AND REPAIR OF OUR EQUIPMENT, IT IS MADE AVAILABLE FOR THE EXCLUSIVE USE OF OWNERIOPERATORS OF
APPLICABLE AIRCRAFT. THIS MANUAL MAY NOT BE REPRODUCED IN WHOLE OR PART, NOR DISTRIBUTED TO OTHERS,
WITHOUT EXPLICIT WRITTEN PERMISSION FROM ROGERSON AIRCRAFT CORPORATION.
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COMPONENT MAINTENANCE MANUAL
PART NO. 115.115
RECORD OF REVISIONS
Rev 1 12-30-83
Rev 2 4-15-85
Rev 3 8-15-00
date issued
Retain this record in front ofthe manual. On receipt of revision, insert revised pages in the manual and enter revision number,
date filed and initials.
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PART NO. 115.115
TEMPORARY
REVISION PAGE DATE INSERTED DATE REMOVED
NUMBER NUMBER ISSUED BY REMOVED BY
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PART NO. 115.115
SERVICE DATE
BULLETIN DATE INCORPORATED/ INSERTED
NUMBER ISSUED SUPERCEDES BY
115.115-38-02 4-15-85
Retain this record in front of the manual. On receipt of a service bulletin, insert service bulletin number, date issued and initials.
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PART NO. 115.115
LIST OF EFFECTIVE PAGES
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PART NO. 115.115
TABLE OF CONTENTS
TITLE PAGE
Introduction......................................................... INTRO-I
Disassemblyv....................................................................................................................... 301
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PART NO. 115.115
INTRODUCTION
A. General
This manual can be used to perform maintenance and repairs on Potable Water Quantity
Indicator, part number 115.115 after the unit has been removed from the aircraft. The
Testing and Fault Isolation, Disassembly, Repair and Assembly sections are written so
that malfunctions can be determined and the affected component removed, repaired and
replaced.
B. Manufacturin2
C. Manual Layout
This technical manual consists of ten (10) topic sections which include the following:
Introduction
Description
Testing and Fault Isolation
Disassembly
Cleaning
Check
Repair
Assembly
Fits and Clearances (Only as they pertain)
Special Tools, Fixtures and Equipment
Illustrated Parts List
Refer to the Table of Contents for the page location of applicable procedure sections.
An explanation of the use of the Illustrated Parts List is provided in the beginning of
that topic section.
All weights and measurements are in English units and S.I. metric equivalent values
in parentheses
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PART NO. 115.115
D. Revision Service
E. Shot Verification
This manual has been shop validated to the 115.115 configuration, as noted in the
following:
SECTION DATE
Testing 6/2/81
Disassembly 6/2/81
Assembly 6/2/81
F. List of Abbreviations
AR As Required
ASSY Assembly
co Celsius Degree
CU Cubic
DIA Diameter
DVM Digital Voltmeter
EFF Effectivity
F0 Fahrenheit Degree
FIG (Fig.) Figure
IN. (in.) Inch
LB. (lb.) Pound
MAX Maximum
MIN Minimum
MM (nun) Millimeter
NM (Nm) Newton-Meter
NHA Next Higher Assembly
NO Number
Oz Ounce
PN Part Number
RF Reference
V Volts
W Watt(s)
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B. Operation
The indicator receives 0 to +I OVdc signal input power at pins 4 (+) and 3 (-) of connector
lights
(Figure 6). Pad resistors RI and R2 facilitate indicator calibration. Indicator dial
at pins I (+) and 2 (-) at
DS 1, DS2, and DS3 are activated by 5Vac aircraft input power
the connector.
115.115 115.115-1
115.115-3 115-4
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C. Leading Particulars
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PART NO. 115.115
A. Test Equipment
B. Functional Testin2
(a) Connect DC power supply topi 1 (+) and 2 (-) of the indicator being
tested.
(b) Apply 2.7 Vdc and verify that the indicator illumination shows uniform
dial and pointer brightness per BAC specification D6T 10783-1 or
equivalent parameters.
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(a) Connect indicator UUT to DC Calibrator from pins 4 (+) and 3 (-) of
UUT connector P 1. Allow for sufficient UUT and test equipment
warmup time.
(b) Verify that the calibrator is set to zero. Raise the calibrator voltage until
the meter reads 120 gallons. Apply calibrator voltages as shown in Table
102 and very that meter indication agrees (within tolerances) with those
listed.
(a) Connect indicator UUT to DC Calibrator from pins 4 (+) and 3 (-) of
UUT connector PI. Allow for sufficient UUT and test equipment
warmup time.
(b) Verify that the calibrator is set to zero. Raise the calibrator voltage until
the meter reads 160 gallons. Apply calibrator voltages as shown in Table
103 and very that meter indication agrees (within tolerances) with those
listed.
(c) Shut off power and disconnect DC Calibrator from indicator UUT.
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C. Fault Isolation Analysis
(1) Procedure
(a) If the indicator fails to pass accuracy testing described in the TESTING
portion of this section, perform calibration procedures stated in the
FAULT ISOLATION ANALYSIS guide prior to performing fault
isolation analysis of the indicator itself.
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SIGNAL R2
RNN
1/2WWW PAD
PAD 1%
0-10 voc R3 ml
20K
1%
SIGNAL(
INPUT
5VACI
LIGHTING 053
3S2
SSI
5V RTN 2
CASE GNO
Schematic Diagram
Figure 101
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PART NO. 115.115
DISASSEMBLY
NOTE: Refer to TESTING AND FAULT ISOLATION section to determine most probable
cause of any malfunction. Disassemble only to the extent required to correct the
problem. Inspect visually and perform testing and Fault Isolation prior to disassembly.
A. All items referenced throughout this section refer to IPL Figure 1001, unless otherwise
noted.
B. To disassemble the Potable Water Ouantity Indicator, proceed as follows:
NOTE: It is recommended that the Potable Water Quantity Indicator be returned to
Rogerson Aircraft Corp. for the appropriate maintenance to be performed in the
event extensive maintenance or repair of that assembly is required.
NOTE: Do not remove terminal board assembly unless determined defective (refer to
TESTING section.)
(5) Remove terminal board assembly (45) by removing two screws (50), two lock-
washers (55) and two flat washers (60). Unsolder and remove brown and red
wires from terminal board assembly (45). Note position of meter assembly to
facilitate reassembly.
(6) Using a low wattage (25 to 40W) soldering device, tag and unsolder red and black
wires from meter to CBA (70).
(7) Remove meter assembly (25) by removing two screws (30), lockwashers (35), and
washers (40). Remove four spacers (65).
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(2) Note position, mounting, routing and clipping of wires for facilitating reassembly.
(3) Using the soldering device, tag and unsolder orange and yellow wires from PCBA
(70) to connector (105).
(4) Remove PCBA (70) by removing two screws (75) and lockwashers (80).
(5) Remove solder lug (90) by removing screw (85) and lockwasher (90).
NOTE: Connector mounting screws are secured with hydraulic sealant. Some force may
be required to loosen the screws. If screws cannot be loosened easily, heat screws
with the soldering device sufficiently to ease in removal of the screws.
(6) Remove connector (105) from frame (120) by removing four screws (110).
Remove and discard gasket (115).
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CLEANING
A. Cleaning Requirements
MATERIAL SPECIFICATION
Solvent, Stoddard Federal Standard P-D-680
Alcohol, Isopropyl (or glass cleaner) Commercially Available
Brush, Soft Bristle Commercially available
Brush, Static Commercially available
Cloth, Line-Free Commercially available
Cleaning Materials
Table 401
B. Cleaning Procedures
WARNING: USE SOL VENTS INA WELL VENTILA TED AREA. KEEP WAY
FROM OPEN FLAME. A VOID INHALA TION OF FUMES OR
PROLONGEDCONTACT OF SOLVENT WITH SKIN
(a) Clean outside of case (10, IPL Fig. 1001) with a soft bristled brush
moistened with Stoddard solvent. Wipe dry with a clean, lint-free cloth
(b) Clean case lens with glass cleaner or isopropyl alcohol and a clean, lint-
free cloth. Dry thoroughly with a clean, dry, lint-free cloth.
(c) Clean connector assembly (105) with a soft bristled brush moistened with
solvent.
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(a) Clean inside of case (10) with a soft bristled brush moistened with
Stoddard solvent Dry thoroughly with a clean, lint-free cloth
(b) Clean inside of case lens with glass cleaner or isopropyl alcohol and a
clean, lint-free cloth. Dry thoroughly with a clean, dry, lint-free cloth
Brush dried lens with a static brush to remove any excess static buildup.
(c) Clean Mounting Board Assembly (70) and inside of connector (105) with
a soft bristled brush moistened with isopropyl alcohol. Air dry or dry
with clean, soft shop cloth.
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PART NO. 115.115
CHECK
A. General
Refer to IPL, Figure 1001 and check all parts for obvious defects in accordance with
industry standards.
(1) Visually check all parts for burrs, nicks, scratches, abrasions, gouges
and/or corrosion.
NOTE: Burrs, nicks and scratches are defined as material raised above normal
surface, which, if not removed would prevent complete and proper mating
of parts and sealing surfaces.
(2) Visually check any threaded parts for crossed or otherwise damaged threads.
(3) Visually check seating and mating surfaces for corrosion or damage.
(1) Check indicator case for any sign of broken pins, scraping or deformation of
mating surfaces. Replace case if necessary, referring to Disassembly and
Assembly sections of this CMM.
(2) Check indicator connector assembly (105) for loose, bent, broken or missing pins.
Replace connector assembly if defective (refer to Disassembly and Assembly
sections of this CMM).
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PART NO. 115.115
(1) Check Printed Circuit Board Assembly (PCBA) for any sign of damage,
overheating, component dislocation, disconnection or deformation. Note location
and type of component (part) and identify per the appropriate IPL illustration.
(2) Inspect PCBA for breaks, shorts, or peeling of circuit traces. Repair or replace
any defective PCBA as is necessary.
(3) Check wiring for any sign of wear, wicking of solder at wire ends, breakage,
burns, broken solder joints of other common wire damage. Inspect electrical
connector and banana plug for frayed or burned insulation. Replace any defective
wires in accordance with the REPAIR Section in this CMM.
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PART NO. 115.115
REPAIR MATERIALS
NOTE: In Table 601, Repair Materials, uivalent substitutes may be used for listed items.
TOOLS/MATERIALS TYPE / SPECIFICATION
Emery paper No. 400 Grade; Commercially Available
Paint, Flat Brown Epoxy, BAC 8328 Finch (per Boeing specification)
Soldering Station 25-40 Watt capacity
Solder, 60/40 Tin-lead resin flux-core Federal Standard QQ-S-571
Desoldering Implement (Part of Solder Station) Suction, Commercially Available
Repair Materials
Table 601
2. REPAIR PROCEDURES
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PART NO. 115.115
F. Return extensively damaged or defective PCBAs to Rogerson Kratos for repair. Repair on-
site if the specific repair is a routine component change which can be accomplished wit
out extensive removal of protective coating, ICs or small components.
The following general instructions apply to the repair of PCBAs (Refer to Figure 601
Wiring Diagram):
(1) Support the PCBA so it will not move or cause the soldering device to strike other
components, i.e. generally recognized shop practice.
(3) Install components in the same location, angle, and attitude with relation to the
PCBA as original installation.
(5) Repair breaks in circuit traces by bridging with a piece of copper wire soldered to
the trace. Do not attempt to solder across the break otherwise. If the break is
non-repairable, replace the PCBA.
(6) Use desoldering equipment, such as a solder sucker, when unsoldering PCBA
components.
(7) Use heat sinks on transistor or diode leads when soldering or unsoldering parts or
wires on a PCBA.
(8) Clean area of excess scrap, excess solder, solder spatter, and/or resin overflow
after repairs.
H. Refer to the wiring diagram, Figure 601 for color and proper connection of wiring. Note
routing and clipping of wires prior to any wire removal. Remove damaged wires and
install new wires with 60/40 solder, using a 25 to 40 Watt soldering station.
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PART NO. 115.115
1 BROWN -
2 RED-
- LAMPS
3 ORANGE METER
* BLUE BLACK
4YELLOW(i
4
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PART NO. 115.115
1. ASSEMBLY
NOTE: The tools and materials listed in Table 701 are required in addition to
standard shop tools. The tools and materials listed are called out in
their appropriate procedures and are also called listed again in the
SPECIAL TOOLS. FIXTURES AND EQUIPMENT section along with
their sources.
All items referenced throughout this section refer to IPL Figure 1001, unless otherwise
noted.
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PART NO. 115.115
NOTE: Apply Loctite sealant to all screw threads prior to insertion into place.
(a) Install new gasket (115, Figure 1001) on connector (105). Apply
hydraulic sealant to threads of screws (110) and secure connector (105) to
firame (120) with four screws (110).
(b) Lubricate new 0-ring (100) with Super O-Lube and install groove in
frame (120). Attach solder lug (90) to frame (120) and secure with screw
(85) and lockwasher (95).
(c) Using the low wattage soldering device, solder wires as tagged during
disassembly to solder lug (90) and PCBA (70).
(d) Install the PCBA (70) on mounting frame (120). Secure in place with two
lockwashers (80) and screws (75).
(a) Using a low-wattage (25 to 40W) soldering device, solder wires, as tagged
during disassembly, routed from the meter assembly (25) to PCBA (70).
(b) With meter assembly in position noted during disassembly, secure meter
assembly (25) and four spacers (65) to frame (120Z) using two screws
(30), lockwashers (35) and washers (40).
(c) Verify' that meter pointer is on first graduation. If not, use an Allen
wrench (or the straightened end of a metal paper clip). Insert into upper
hole in spring support as shown in Figure 701 and carefully adjust meter
movement until pointer is on first graduation.
(d) Install terminal board (45) and secure with two screws (50), two lock-
washers (55) and two flat washers (60). Solder brown and red wires as
tagged during disassembly.
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PART NO. 115.115
(h) Apply hydraulic sealant to threads of four screws (15) and install in case
(10).
(i) Install lamp housing assembly (5) in case (10) and secure with two
captive screws.
D. Calibration Procedure
(1) Verify that meter pointer is set at zero indication. Adjust mechanical zero if
necessary.
(2) Connect DC Calibrator to indicator pins 3 (-) and 4 (+) at connector (105).
(3) Connect resistance decade boxes in place of resistors RI and R2 (see IPL Figure
1002) and set initial values as shown in the following:
RI 500 Ohms
R2 15K Ohms
(4) Adjust decade R2 so that the indicator reads 120. From resistor kit 0349-202 1,
select appropriate RN55C resistor which will ensure nearest scale reading without
exceeding 120 reading.
(6) Reconnect calibrator and readjust RI so that indicator reads 120. From resistor
kit 0349-2009, select appropriate pad resistor which will ensure nearest scale
reading without exceeding 120 reading.
(7) Disconnect DC Calibrator and RI decade box. Install appropriate resistors and
confirm that calibration meets requirements of Performance Test.
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Material Type
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PART NO. 115.115
A. Special Tools
None required
B. Fixtures
None required
C. Equipment
Refer to Table 901 for equipment required for specific procedures in the manual. They are
considered to be standard shop items and are commercially available. Suitable equivalents may
be used in place of the items listed. These items are also referenced in the appropriate steps and
in each applicable section.
DC Calibrator John Fluke Mfg. Co., Inc. Mountlake Testing, Assembly, 0 - 2OVdc
Terrace, WA
Resistance Decade Box (2) Commercially Available Testing (0 to 1K ohms)
DC Power Supply Commercially Available 0 to 5OVdc
Soldering Iron Commercially Available Disassembly/Assembly 2540W
Desoldering Tool Commercially Available Suction or wicking
Special Tools, Fixtures and Equipment
Table 901
D. The following, Table 902, is a list of the consumable materials required for specific
procedures in the manual. They are considered to be standard shop items and are
commercially available. These items are also referenced in the appropriate steps and in
each applicable section.
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CONSUMABLE MATERIALS
Consumable Materials
Table 902
E. Special Conditions; All work performed on the indicator should be in a clean dust-free
area.
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PART NO. 115.115
(1) This section provides the illustration(s) and breakdown of parts for the
assembly(ies) which can be disassembled, repaired or replaced.
(2) This section contains a detailed list of six columns: Figure and Item, Part
Number, Airline Part Number, Nomenclature, Effectivity and Units per
Assembly.
(1) The FIGURE and ITEM column lists the figure number and the item number
for each detail part. The figure number is listed once at the top of the column
and each part is called out by and item number. Any part which is not
illustrated will have an item number preceded by a dash (-)
(b) An alpha variant item number is not shown on the exploded view
when the appearance and location of the alpha variant item is the same
as the basic item number.
(2) The PART NUMBER column lists the part number for each detail part. Use
the part number exactly as listed when procuring parts unless the part is
proprietary, which is indicated by a letter "P" preceding the vendor code
number. (Refer to paragraph D in this section).
(3) The AIRLINE STOCK NUMBER column is provided for individual airline
use.
(4) The NOMENCLATURE column describes the detail part. A vendor code is
provided if the part is not manufactured by Rogerson Aircraft Corporation. If
vendor codes are used, the name and address for each vendor is listed at the
end of this introduction.
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The parts descriptions in the nomenclature column are indented to depict the
relationship of the part to the next higher assembly. For example:
1234567
Top Assembly
Attaching Parts
Deleted Parts
. Detail Parts for Top Assembly
. Subassembly
. . Detail Parts for Subassembly
Attaching Parts
. . . Sub-subassembly
.... Detail Parts for Sub-subassembly
(6) The UNITS PER ASSEMBLY column lists the total quantity of each part
required. The letters AR indicate that the quantity required will be determined
during assembly procedures. The letters RF indicate that the item is listed for
reference purposes only.
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PART NO. 115.115
D. Proprietary
An item listed in the nomenclature column of the illustrated parts list which is
proprietary to the component manufacturer (Rogerson Aircraft Corporation) is
identified by the letter "P" preceding the vendor code number. This item may be
listed with more than one model or part number but is identified by the component
manufacturer's source controlled part number which is to be used for any parts
procurement specification.
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PART NO. 115.115
E. Vendor Information
The following list contains the name and address of each vendor whose code number
is listed in the nomenclature column of the illustrated part list or is listed in other
sections of this manual in alphanumeric order.
V77820 Bendix
Electrical Components Division
Sidney, NY 13838
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I5
NOTE: 0
DIAL FACE ROTATED 135 DEGREES
65
5 70
80
15
85
40 /
45
0~u 1 15/00i
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PART NO. 115.115
20 0317-0106 * INSULATION 1
25 0356-0551 * METER ASSEMBLY, PRE SB115.115-38-02 A 1
-25A 0356-0795 * METER ASSEMBLY, PRE SB 115.115-38-02 B I
-25B 0356-0836 * METER ASSEMBLY, POST SBI15.115-38-02 B,D I
-25C 0356-0846 * METER ASSEMBLY, POST SB] 15.115-38-02 A,C I
ATTACHING PARTS
30 2840-9206 * SCREW, (V34830) 2
35 2833-0504 * WASHER, LOCK 2
40 2833-1004 * WASHER, FLAT (V34830) 2
65 0329-0058 * SPACER 4
70 0307-0523 * BOARD ASSY, PRINTED CIRCUIT (SEE FIG. 1002 FOR BDN) 1
ATTACHING PARTS
75 28404104 * SCREW (V34830) 2
80 2833-0503 * LOCKWASHER (V34830) 2
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Q R3 R2 RI
25
15 30 la 5 20
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2-1 0307-0523 BOARD ASSEMBLY, PRINTED CKT (REF IPL 1001, NHA) RF
5 4753-XXXX * RESISTOR, PAD, WW RI 1% 1/2W (SEE FOOTNOTE 1) I
-5A RNC55CXXXXFS * RESISTOR, PAD, FF, EST. RELI., 1% 1/10W (ALTERNAT.) I
10 4755-XXXX * RESISTOR, PAD, FF R2 1% 1/IOW (SEE FOOTNOTE 2) 1
-10A RNC55CXXXXFS . RESISTOR, PAD, FF EST. RELI. 1% 1/10W (ALTNERA.) 1
15 RN55C2002F . RESISTOR, FF R3 20K 1% 1/102 (V34830 PN 4755-2002) 1
15A RNC55C2002FS * RESISTOR, FF EST. RELI. 20K 1% 1/10KW (ALTERNAT.) 1
20 2148-0007 * TERMINAL 7
25 0329-0053 * SPACER 2
30 0306-0394 1 1 * BOARD, PRINTED CIRCUIT I
1= Resistor selected at time of calibration from resistor kit 0349-2009. Kit consists of 500 resistors
conforming to RK drawing 4753-XXXX as follows:
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