Tesla Power Supply TI2000GPU-24 User manual

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TI2000 GPU-24
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www.TESLAind.com
WARNING
*******SHOCK HAZARD POTENTIAL*******
IMPROPER USE/FAILURE TO FOLLOW INSTRUCTIONS IN OPERATORS MANUAL CAN
RESULT IN UNIT FAILURE AND/OR POSSIBLE INJURY, OR DEATH, BY ELECTRICAL SHOCK.
THE TI2000GPU-24 IS A MAINTENANCE FREE, SEALED UNIT
NO REPAIRS ARE AUTHORIZED.
WARRANTY WILL BE VOID IF
UNIT IS TAMPERED WITH.
FOR TECHNICAL SUPPORT CONTACT:
TESLA INDUSTRIES INC.
109 CENTERPOINT BLVD.
CENTERPOINT INDUSTRIAL PARK
NEW CASTLE,DELAWARE 19720
PH.(302)324-8910
FAX (302)324-8912
WARNING
*******SHOCK HAZARD POTENTIAL*******
ATTEMPTS TO OPEN OR ENTER THE INSIDE OF THIS UNIT (BY USING ANY TOOL
OR DEVICE; i.e. PROBE, BORESCOPE, etc.) CAN RESULT IN UNIT FAILURE
AND/OR POSSIBLE INJURY BY ELECTRICAL SHOCK.
THIS UNIT IS MAINTENANCE
FREE AND SHALL NOT BE OPENED OR DISASSEMBLED FOR ANY REASON.
***SHIPPING HAZARDS***
“NONE”
“DRY” Non-spillable, POWER CELL (battery),
No Free liquids,
to leak or toxic gases.
Always protect unit from short circuit.
Return Power cells to Tesla for Recycling.
i
TABLE OF CONTENTS
TITLE
Page
CHAPTER 1
INTRODUCTION
1-1
CHAPTER 2
UNIT DESCRIPTION AND OPERATION
2-1
Section I
Unit
2-1
Section II
Description
2-2
CHAPTER 3
OPERATING LIMITS AND RESTRICTIONS
3-1
Section I
General
3-1
Section II
Operational Restrictions and Safety Limits
3-1
CHAPTER 4
OPERATING PROCEDURES
4-1
Section I
Unit Operation
4-1
Section II
Operating Procedures
4-2
Section III
Functional Check Procedures
4-5
CHAPTER 5
PERFORMANCE DATA
5-1
Section I
Introduction
5-1
Section II
Data Criteria
5-2
CHAPTER 6
CARE AND MAINTENANCE
6-1
Section I
Unit Care
6-1
Section II
Maintenance
6-2
INDEX
Index 1
LIST OF ILLUSTRATIONS
Figure
Title
Page
2-1
Dimensions
2-3
2-2
General Details
2-2
2-3
Fuse Setting Procedures
2-4
5-1
Temperature Conversion Chart
5-3
5-2
Discharge Load Curve
5-4
5-3
Maximum Output Current
5-5
ii
CHAPTER 1
INTRODUCTION
1-1.
GENERAL
These instructions are for use by the owner/operator.
They apply to
handling and operation of the TI2000GPU-24 (Turbo Start 2000) ground
power unit.
1-2.
WARNING, CAUTION, AND NOTE DEFINED
A warning, caution, or note is used to emphasize important and critical instructions as defined for the following conditions:
WARNING
An operating procedure, practice, etc., which,
if not correctly followed, could result in
personal injury or loss of life.
CAUTION
An operating procedure, practice, etc., which,
if not strictly observed, could result in
damage to or destruction of equipment.
NOTE
An operating procedure, condition, etc., which
is essential to highlight.
1-3.
DESCRIPTION
This manual contains the complete operating instructions and procedures for the TI2000GPU-24 (Turbo Start 2000) ground power unit.
The
Turbo Start 2000 is intended to provide DC electrical ground power
for aircraft flight line and maintenance ground support operations.
The unit is designed to provide 24 volt DC electrical power output
for aircraft engine starting and 24 or 28.5 volts DC electrical support for ground maintenance, avionics/electrical trouble shooting and
testing.
The observance of procedures, limitations and performance
criteria is essential to ensure peak operating efficiency and to
maximize operational capabilities and life of the Turbo Start 2000
ground power unit.
1-1
1-4.
INDEX
The index lists, in alphabetical order, every titled paragraph and
figure contained in this manual.
1-5.
ABBREVIATIONS AND SYMBOLS
Abbreviations and symbols are used within text, headings and titles.
Unless otherwise indicated, the following list of abbreviations and
symbols are used in this manual:
LIST OF ABBREVIATIONS AND SYMBOLS
Abbreviation
Definition
amp
Ampere
AC
Alternating Current
C
Celsius
cont
Continuous
DC
Direct Current
F
Fahrenheit
Ft
Feet
FWD
Forward
GPU
Ground Power Unit
Hr
Hour
Hz
Hertz
Kg
Kilograms
Kw
Kilowatts
°
Degree
LED
Light Emitting Diode
MAX
Maximum
MIN
Minimum
VAC
Volts, Alternating Current
VDC
Volts, Direct Current
Explosion Hazard Potential
Shock Hazard Potential
Guard from moisture
䩢 䩰䩜䩭 䩟䨻 䩡 䩭䩪 䩨 䨻 䩤 䩩 䩞䩪䩭䩭䩠 䩞䩯
䩫 䩪䩲䩠 䩭䨻 䩮 䩪䩰 䩭䩞䩠
Guard from incorrect power source
Guard from incorrect power source
1-2
1-6.
FORMS AND RECORDS
NONE REQUIRED.
1-7.
USE OF WORDS SHALL, SHOULD, AND MAY.
Within this technical manual the word “shall” is used to indicate a
mandatory requirement for proper operation and warranty purposes.
The word “should” is used to indicate a non-mandatory but preferred
method of accomplishment. The word “may” is used to indicate an acceptable method of accomplishment.
1-3
CHAPTER 2
UNIT DESCRIPTION AND OPERATION
SECTION I. UNIT
2-1.
GENERAL
The TI2000GPU-24 (Turbo Start 2000) (Figure 2-1 and 2-2) is a compact, portable
and highly versatile 24/28.5 VDC electrical ground power unit. The unit incorporates a 120-240 VAC to 28.5 VDC converter, a 24 volt unique (dry) power cell
and an internal intelligent 120 to 240 volt AC charger to recharge the power
cells. These built-in features give the Turbo Start 2000 self-sufficiency and
mobility for short-term operations without AC electrical power or long term
operations with AC electrical power. Short term operations rely solely on
power cell output and the fast recharge rates that the unit’s internal charger
provides from any standard 120 or 240 VAC electrical outlet. Longer term operations incorporate the continuous 20 amp output of the 120-240 VAC to 28.5
VDC converter, or a combination of converter and power cell output to provide
24 VDC output. The following are the unit’s four (4) main operational support
capabilities:
a. 24 VDC 3000 amp peak power output for engine starting or constant (one
hour) rated power output (without a 120-240 VAC power source) for short term
trouble shooting and flexible flight line support ground power.
b. 24 VDC constant (one hour) rated power output or variable high load demand output (less than one hour) with a 120-240 VAC power source for extended
maintenance (hangar) and routine flight line maintenance, ground support
power.
c. 28.5 VDC continuous rated (AC to DC converter) power output with a 120240 VAC power source for hangar and routine flight line maintenance support,
and avionics bench testing.
d. Rapid recharge of the unit’s power cells from any 120-240 VAC common
power source. This feature eliminates the need for special recharge equipment and dedicated maintenance support man-hours.
WARNING
Check fuse holder window to ensure the fuse setting reads either 120 or
240 prior to connecting recharge cord to AC power source. Fuse setting (120/
240) must match AC power source (hangar wall, flight line AC power) prior to
connecting TURBO START for recharging.
(SEE PAGE 2-4 FOR
FUSE SETTING PROCEDURES)
120 VAC Setting
2-1
SECTION II
2.2.
240 VAC Setting
DESCRIPTION
GENERAL SPECIFICATIONS
WEIGHT
UNIT:
111 lbs (50.39 Kg)
DC POWER CABLE:
8.5 lbs (3.86 Kg)
AC POWER CORD:
0.4 lbs (0.18 Kg)
INPUT POWER AC
TI2000GPU-24:
105-125 VAC 60 Hz
6.50 amps max.
TI2000GPU-24-UNV:
210-250 VAC 50/60 Hz
3.25 amps max.
TI25000-U01 NORTH AMERICAN LINE CORD
105-125 VAC 60 Hz
6.50 amps max.
TI25000-U04 OLD BRITISH LINE CORD
210-250 VAC 50/60 Hz
TI25000-U03 EUROPEAN
3.25 amps max.
10A/250V
210-250 VAC 50/60 Hz
3.25 amps max.
TI25000-U05 ENGLAND 10A/250V
210-250 VAC 50/60 Hz
3.25 amps max.
OUTPUT POWER DC
CONVERTER:
28.5 VDC TO 20 AMPS, 24 VDC 21 AMPS AND ABOVE.
POWER CELLS:
24 VDC
PEAK OUTPUT:
3000 AMPS
POWER CELL
DRY, HIGH RATE DISCHARGE, RECHARGEABLE, MAINTENANCE-FREE
DC POWER CABLE
LENGTH: 8 FT
AIRCRAFT CONNECTOR: 3 PIN RECEPTACLE (MS25488)
2-3
Fuse Setting Procedures
for Switching Voltages or Changing Blown Fuses
1) Grab both tabs
on left and right side
of the fuse clip. Press
tabs inward and pull
fuse clip out of housing
GENTLY.
2) Completely pull
fuse clip from housing,
being careful not to
drop the fuses from
the fuse clip.
3) Note: The fuses
are not fastened into
the fuse clip, they are
lose. Take care to ensure
fuses are not dropped or
lost.
4) GENTLY pull the
white clip from the
fuse clip, taking care
not to bend any of
the tabs. (See
enlargement 1)
TABS
ENLARGEMENT 2 120 VAC SETTING
ENLARGEMENT 1
7) Replace the
white clip back into
the fuse clip. Take
care not to damage
the tabs.
ENLARGEMENT 3 240 VAC SETTING
5) Completely remove
the white clip from the
fuse clip.
6) Ensure that the
proper voltage is selected
on the white clip. (See
Enlargement 2 & 3)
8) Completely insert
white clip in to fuse
clip (GENTLY) until
it snaps into place.
9) Insert fuse clip
back into fuse housing
EVENLY on both sides.
DO NOT FORCE, if fuse
clip does not go in easy,
it means fuses are misaligned, realign fuses and
insert again.
2-4
10) Snap fuse clip
back into the housing
(GENTLY). DOUBLE
CHECK VOLTAGE
WINDOW PRIOR
TO PLUGGING UNIT
INTO AC POWER
2-2
CHAPTER 3
OPERATING LIMITS AND RESTRICTIONS
SECTION I. GENERAL
3-1.
PURPOSE
Chapter 3 includes all important operating limits and restrictions
that must be observed for proper and safe operation of the TI2000GPU24 (Turbo Start 2000) ground power unit.
3-2.
GENERAL
The operating limitations set forth in this chapter are the direct
result of design analysis, testing, and operating experience.
Compliance with these limitations and restrictions will ensure that owners/operators obtain maximum continued capability from the Turbo
Start 2000 ground power unit.
SECTION II. OPERATIONAL RESTRICTIONS AND SAFETY LIMITS
3-3.
POWER CELL RECHARGE LIMITS
Any time the unit’s power cells are fully discharged the unit shall
be recharged within 24 hours to prevent performance degradation and
ensure maximum life.
CAUTION
Unit’s power cells may be damaged if recharged by NiCad or Lead Acidtype battery chargers.
Power cells should only be charged by either
the TURBO START internal charger and the AC power cord furnished with
the equipment, or when connected aircraft external DC power receptacle.
3-1
3-4.
120-240 VAC CHARGER AND AC TO DC CONVERTER LIMITS
The unit is designed with a single point AC receptacle for external
power to operate both the internal charger and converter.
The units
AC voltage range can be factory set from 105 to 250 VAC at 50 to 60
Hz depending upon customer requirements.
The AC power cord provided
with the unit is the mechanism that ensures the specified AC power
source is properly supplied to the unit (see paragraph 3-5).Use no
others
INTERNAL CHARGER: NO LIMIT AC power cord can remain connected
when power cells are fully charged. When the power cells are fully
charged the unit’s intelligent charger will go to a stand-by mode,
monitor the power cells state of charge, and only charge the power
cells to ensure they stay at maximum capacity.
* 8 $ 5 ’ ) 5 2 0 ,1 & 2 5 5 ( & 7
32: (5 628 5&(
INTERNAL AC TO DC CONVERTER: LIMITED (see paragraph 3-6,
3-10). AC power cord does not have to be disconnected when
verter power output is no longer
required. Once DC power
is terminated the unit’s intelligent charger will remain on
ensure power cells are charged to maximum capacity.
3-8 and
condemand
line to
CAUTION
Unit will be damaged if unapproved AC power is applied.
3-5
AC POWER CORD LIMITS
The AC power cord governs which AC power source the unit is set to
operate from. The Turbo Start 2000 is supplied with a single customer specified AC power cord.
Some customers may specify a universal AC option (for worldwide mobility), which comes with two (2)
power cords, one for 120 VAC 60 Hz and the other for 240 VAC 50 Hz
(SEE APPENDIX A). Each power cord is marked accordingly. Below are
the following three (3) types of AC power cords available and their
limits.
120 VAC 60 Hz power cord (USA): LIMITED TO 105-125 VAC 60 Hz power
source only.
120 VAC 60 Hz power cord (Universal): LIMITED TO 105 VAC to 250 VAC
50/60 Hz power source using proper cord set.
240 VAC 50 Hz power cord (European):
power source only.
LIMITED TO 210-250 VAC 50-60 Hz
FOR MORE INFORMATION ON POWER CORDS SEE APPENDIX A
3-2
AC Line Cords
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乓 乒乚么 乕丣 乖 乒乘 乕乆么
Cont. Europe
U.K.
Old British
North American
CAUTION
Unit will be damaged if unapproved AC power is applied by fitting
120 or 240 VAC power cord with any kind of unapproved modification or
adapter that changes the specified input power characteristics.
WARNING
********SHOCK HAZARD POTENTIAL*********
Failure to use proper grounding can cause a potential shock hazard!
In different countries, the 240 VAC 50 Hz power cord may require
the use of a plug adapter to achieve plug style compatibility for
240 VAC 50 Hz operation. Use only adapters with proper grounding
mechanism.
3-6.
ONE (1) HOUR RATE, 24 VDC CONSTANT OUTPUT
46 amp hour (without AC power connected), power cell output.
(see Figure 5-2)
66 amp hours (with AC power connected), both power cell and AC to
DC converter output.
NOTE
If power output is greater than rated amp hour rate, power cell
discharge rate will increase correspondingly.
3-7.
RATED PEAK OUTPUT (ENGINE STARTING)
3000 peak amps at 25oC (77oF) (See Figure 5-3).
3-3
3-8.
CONTINUOUS OUTPUT RATE, 28.5 VDC CONSTANT OUTPUT
20 amp hours
(with AC power connected)
NOTE
If current demand exceeds 20 amps, converter output voltage will drop
below 28.5 VDC and two or more LED status indicator bars will illuminate. If all LED status indicator bars illuminate, both the converter and power cells are supplying 24 VDC power output (see paragraph 3-4 and 4-7.4.).
3-9.
ENGINE STARTING POWER
Operators should always ensure the unit is charged above 80% prior to
ground support engine starting.
However, circumstances may exist
during use where unit recharge is not readily available and immediate
external engine starting power is required.
The following provides
minimum states of charge necessary to provide ample power for an efficient engine start under specific current load demands.
ENGINE START CURRENT LOAD DEMAND
650-850
peak starting amps
MINIMUM CHARGE
40% charged
850-1000
peak starting amps
50% charged
1000-1500 peak starting amps
60% charged
1500-1800 peak starting amps
70% charged
1800-2500 peak starting amps
80% charged
2500-3000 peak starting amps
90% charged
3-10.
TEMPERATURE
Temperatures refer to the unit’s cold/heat soaked temperature.
A
unit’s cold/heat soaked temperature shall be established by the ambient temperature that a unit is exposed to for one (1) hour or more.
If unit’s cold/heat soaked temperature exceeds operating temperature
range, unit shall be stabilized prior to operation as follows: COLD
SOAKED, warmed for a minimum of 3 hours above +10Co (+41oF) or 2
hours above +20Co (+68oF); WARMED SOAKED, cooled for 1 hour below
+38Co (+100oF).
Operating range:
without AC power -40Co (-40oF) TO +60Co (+140oF)
with AC Power -30Co (-22oF) TO +50Co (+124oF)
Storage range:
-60Co (-76oF) TO +60Co (+140oF)
(C0NTINUED ON NEXT PAGE)
3-4
CAUTION
Unit may be damaged if operated when unit’s cold or heat soaked temperature exceed the specified limit. If unit is operated when cold or heat
soaked temperature limit is exceeded, a full functional check should be
accomplished prior to continued use.
NOTE
If unit should overheat, an over-temperature sensor will shut down 120240 VAC functions (charger and converter) until unit cools to normal
operating temperatures.
3-11.
ENVIRONMENTAL
Operating any electrical equipment in the presence of moisture creates possible safety hazards and/or potential for equipment damage.
Every effort has been made, within the scope of existing technology
to prevent foreseeable safety hazards and make the Turbo Start 2000
moisture resistant to prevent damage or failure.
If the Turbo Start
3000 is exposed to moisture, preventive measures and precautions
shall be taken to:
a.
prevent accumulation of moisture on AC and DC connectors/receptacles
b.
minimize moisture entering FWD inlet and AFT outlet cooling fan vent ports
The limits and operational constraints listed below shall apply for
the following environmental (weather) conditions:
Heavy or steady rain:
OPERATION NOT RECOMMENDED
Light rain, drizzle:
NO CONVERTER OR CHARGER 120-240 VAC
fog, snow or sleet:
POWER SHALL BE APPLIED.
Unit inlet and outlet vent ports shall be covered from exposure.
Unit shall be kept horizontal.
3-5
WARNING
********SHOCK HAZARD POTENTIAL*********
Severe injury, or Death, from electrical shock is possible when personnel and/or Turbo Start 2000 are wet during use and when 120-240
VAC power is being supplied to unit.
CAUTION
Damage may occur if unit is operated after exposure to moisture
(rain, drizzle, fog, sleet or snow) or moisture contamination is suspected.
DO NOT USE until unit’s exterior and receptacles are dried.
Operation shall be restricted to use without 120 or 240 power cord.
DO NOT CONNECT 120 or 240 VAC power cord until unit has been dried
for a MINIMUM of one (1) hour, prior to use.
Blowing sand or dust:
Minimize exposure to sand and dust
when 120-240 AC power is used. Unit shall be kept horizontal during use.
3-12.
OPERATING POSITION
Without 120-240 VAC power cord:
Horizontal or vertical.
Horizontal only, for propper unit ventilation, when 120-240
cord is plugged in and exhaust fan is running.
VAC line
CAUTION
Unit may be damaged if blown over by propeller, rotor or jet wash, or
accidentally knocked over.
Unit should be kept horizontal during
use.
3-6
CAUTION
Unit damage may occur if inlet and outlet vent ports are obstructed
and/or cooling air flow is restricted.
3-13.
UNIT OPERATION DURING AIRCRAFT FUELING/DEFUELING
Power output is restricted to 24 VDC power cell output only. DO
NOT CONNECT 120 or 240 VAC POWER SUPPLY. 120-240 VAC power
(charger or AC-DC converter) functions of unit shall not be operated during any aircraft fuel handling operation.
WARNING
*******FIRE/EXPLOSION HAZARD POTENTIAL********
Severe injury, or Death, may occur from fire or explosion, as a
result of electrical sparks produced near fuel vapors.
3-7
CHAPTER 4
OPERATING
PROCEDURES
SECTION I. UNIT OPERATION
4-1.
GENERAL
Correct operation of the TI2000GPU-24 (Turbo Start 2000) includes
both pre-use and operational checks of the unit.
Knowledge of the
operating limits, restrictions, performance, unit capabilities and
functions is fundamental to correct and safe operation.
The operator
shall ensure compliance with the instructions in this manual that
affect operational safety and the warranty of the unit.
4-2.
OPERATING LIMITS AND RESTRICTIONS
The minimum, maximum and normal operating ranges result from careful
engineering and evaluation of test data.
These limitations must be
adhered to during all phases of operation. Refer to Chapter 3, Section II, OPERATING LIMITS AND RESTRICTIONS, for detailed information.
4-3.
PERFORMANCE
Refer to Chapter 5, PERFORMANCE DATA to determine the capability of
the Turbo Start.
Consideration must be given to changes in performance resulting from variations in ambient temperature, mode of operation, state of charge (with or without 120 or 240 VAC power), and
aircraft DC bus system inefficiency (voltage drops).
4-1
SECTION II. OPERATING PROCEDURES
4-4. OPERATING PROCEDURES
This section deals with normal procedures, and includes all steps
necessary to ensure safe and efficient operation of the TI2000GPU-24
(Turbo Start 3000). As experience is gained with the Turbo Start
3000, the user will be able to maximize the unit’s unique capabilities to enhance the flexibility of aircraft maintenance and support
operations.
NOTE
When the TURBO START 2000 is not in use, it should always remain
plugged into a suitable AC power source to insure operational readiness at all times. REMEMBER,when the AC line cord is plugged in, the
unit must be placed in the horizontal position to allow the cooling
fan to operate properly!
4-5. BEFORE OPERATION CHECK
CHECK FUSE WINDOW FOR PROPER SETTING (120/240) BEFORE PLUGGING
INTO THE AC POWER SOURCE TO BE USED. REMEMBER,when the AC line
is plugged in, the unit must be placed in the horizontal posito allow the cooling fan to STATUS
operate properly!
NOTE:
A full charge is indicated by Either a steady lighted green bar or a
blinking green bar at the bottom of the bar graph column.The fan will
also exhibit ratcheting but will not come on when the unit is fully
charged.
1.
UNIT
cord
tion
2. CHECK UNIT FOR EVIDENCE OF DAMAGE - Check for dents, punctures,
case distortion or misalignment, cracked or loose connectors, and
that cooling fan is functioning.
4-2
CAUTION
REMEMBER,when the AC line cord is plugged in, the unit must be placed
in the horizontal position to allow the cooling fan to operate properly!
Unit may overheat if cooling fan fails. Do not operate if cooling
fan fails.(More than one green bar present on bar graph)
3. CHECK DC POWER CABLE/CONNECTORS FOR DAMAGE - Check cable for
cuts, chafing or evidence of being crushed.
Check connectors for
cracks, cuts, distortions, excessive wear, broken/loose fasteners or
loose cable attachment.
4-6. 24 VDC GROUND POWER (NO 120 OR 240 VAC POWER SUPPLY) ENGINE
STARTING OR DC SYSTEM POWER
1. TRANSPORT UNIT - The Turbo Start 2000 is easily transported using
the wheels that are incorparated into the unit. The AXEL EXTENTION
kit (included with the unit) ensures that the Turbo Start 2000 is
stable. The unit is engineered to be pushed rather than pulled.
2. CONNECT DC POWER CABLE TO UNIT - Ensure power cable connector is
fully seated into unit’s connector.
Set the unit down horizontally
ensuring vent ports are un-blocked.
3.
CONNECT DC POWER CABLE TO AIRCRAFT - Ensure ground power
cable connector is fully seated into aircraft ground power receptacle. DC bus power should come on and aircraft volt meter should
indicate 24 VDC to 23.5 VDC (23 VDC minimum).
4. ENGINE STARTING - Check power cable for security and correct
installation prior to engine start.
Follow ground power engine
starting procedure as specified in aircraft operators manual.
5.
REMOVING DC POWER SUPPLY FROM AIRCRAFT
a. Remove DC power cable GPU connector from aircraft.
b. Remove DC power cable connector from Turbo Start
(if necessary).
4-3
4-7. 24 VDC GROUND POWER (WITH 120/240 VAC POWER) SYSTEM HIGH POWER DEMAND (21 amps and above) OR ENGINE STARTING.
1. TRANSPORT UNIT - The Turbo Start 2000 is easily transported using the wheels that are incorparated into the unit. The AXEL
EXTENTION kit (included with the unit) ensures that the Turbo Start
2000 is stable. The unit is engineered to be pushed rather than
pulled.
2. CONNECT AC POWER CORD TO UNIT (CHECK FUSE WINDOW FOR PROPER SETTING).- - Ensure 120 or 240 VAC power cord is properly connected to
an approved AC power supply. Unit shall be in horizontal position to
ensure unit’s vent ports are free from blockage.
After approximately
5-8 seconds, unit’s LED status indicator will illuminate indicating
power cell state of charge. Cooling fan will operate. Ensure LED
status indicator and cooling fan are operational prior to continuing
to step 3.
3. CONNECT DC POWER CABLE TO UNIT - Ensure power cable connector is
fully seated into unit’s receptacle.
4. CONNECT DC POWER CABLE TO AIRCRAFT - Connect to aircraft ground
power receptacle. DC bus power should come on and aircraft volt
meter should indicate 27.5 VDC to 23.5 VDC (23 VDC minimum). If current demand is above 20 amps, converter output voltage will drop below 28.5 VDC and two or more LED status indicator bars will illuminate.
At approximately 21 amps of current demand, converter output
voltage will be regulated at 24 VDC output and the last (RED) LED
status indicator bar will illuminate.
NOTE
When all LED status indicator bars illuminate, both the converter and
power cells are supplying 24 VDC power output for current demands
above 21 amps (see paragraph 3-4).
5.
ENGINE STARTING - UNPLUG AC POWER CORD BEFORE STARTING
ENGINE WITH TURBO START. (see paragraph 4-6.).
Prior to engine
start, ensure power cell charge is sufficient to provide an efficient
engine start (see paragraph 3-7).
6.
REMOVING DC POWER SUPPLY FROM AIRCRAFT
a. Remove DC power cable GPU connector from aircraft.
b. Remove DC power cable connector from Turbo Start
(if
necessary).
4-4
4-8 28.5 VDC GROUND POWER (WITH 120/240 VAC POWER) SYSTEM LOW
DEMAND (20 amps or less).
POWER
1. TRANSPORT UNIT - The Turbo Start 2000 is easily transported using the wheels that are incorparated into the unit. The AXEL
EXTENTION kit (included with the unit) ensures that the Turbo Start
2000 is stable. The unit is engineered to be pushed rather than
pulled.
2. CONNECT AC POWER CORD TO UNIT (CHECK FUSE WINDOW FOR PROPER SETTING).- Ensure 120 or 240 VAC power cord is properly connected to an
approved AC power supply.
Unit shall be in horizontal position to
ensure unit’s vent ports are free from blockage.
After approximately
5-8 seconds, unit’s LED status indicator will illuminate indicating
power cell state of charge. Cooling fan will operate. Ensure LED
status indicator and cooling fan are operational prior to continuing
to step 3.
3. CONNECT DC POWER CABLE TO UNIT - Ensure power cable connector is
fully seated into unit’s receptacle.
4. CONNECT DC POWER CABLE TO AIRCRAFT - Connect to aircraft ground
power receptacle. DC bus power should come on and aircraft volt
meter should indicate 28.5 VDC to 27 VDC (26.5 VDC minimum). If aircraft power demand is less than 20 amps converter output will remain
at 28.5 VDC (only one GREEN LED status indicator bar will illuminate).
If aircraft power demand exceeds 20 amps converter voltage
output will decrease and two or more LED status indicator bars will
illuminate (see paragraph 3-4, and 7-4.4.).
5.
REMOVING POWER SUPPLY FROM AIRCRAFT
a. Remove DC power cable GPU connector from aircraft.
b. Remove DC power cable connector from Turbo Start (if
sary).
4-9
neces-
POWER CELL RECHARGE
1. CONNECT AC POWER CORD TO UNIT - Unit shall be in horizontal position to ensure unit’s vent ports are free from blockage. (CHECK
FUSE WINDOW FOR PROPER SETTING).- Ensure 120 or 240 VAC power cord is
properly connected to an approved AC power supply.
After approximately 5-8 seconds, ensure unit’s LED status indicator illuminates
indicating power cell state of charge and cooling fan is operating.
4-5
CAUTION
Unit may overheat if cooling fan fails.
Do not operate if cooling fan fails.
2. CHECK FOR FULL CHARGE INDICATION - After 2 HR 30 minutes, LED
charge indicator should show a single steady or flashing green LED
bar when fully charged, the last LED bar. AC power may be left connected to unit when power cells are fully charged.
NOTE
Under a full charge, two things will be observable with the unit. A
non-blinking lighted green bar or a blinking green bar at the bottom
of the bar graph, both indicate a full charge.Also the fan will display ratcheting but not come on whe the unit is fully charged.
4-6
SECTION III.
FUNCTIONAL CHECK PROCEDURES
4-10.
FUNCTIONAL CHECK PROCEDURES
This section deals with normal functional check procedures, and includes all steps necessary to ensure the Turbo Start 2000 is functioning within specific operational parameters prior to operational
use. As users gain experience with the Turbo Start 2000, they will
incorporate these functional checks as a routine practice.
4-11.
REQUIRED EQUIPMENT FOR FUNCTIONAL CHECK.
FLUKE OR EQUIVALENT TYPE DIGITAL MULTIMETER.
4-12.
DC FUNCTIONAL CHECK.
1. CHECK UNIT FOR EVIDENCE OF DAMAGE - Check for dents, punctures,
case distortion or misalignment, cracked or loose connectors. If no
damage is evident proceed to step two.
IF DAMAGE IS EVIDENT contact distributor or manufacturer.
2. ENSURE UNIT IS NOT PLUGGED INTO 120 OR 240 VDC. Unplug AC power
if plugged in.
3. CHECK UNIT INTERNAL RESISTANCE (TEST FOR SHORTS) - Better than 10
Megohms. Ensure no short exists.
Negative (-) DC receptacle terminal and unit case.
Positive (+) DC receptacle terminal and unit case.
4.
CHECK DC VOLTAGE READING AT DC RECEPTACLE TERMINALS.
24 to 25.5 VDC depending on state of charge.
5. PLUG IN 120 OR 240 POWER CORD. (CHECK FUSE WINDOW FOR PROPER SETTING).-Ensure power unit is connected to a suitable AC power source
(120 USA or 240 European).
6. CHECK UNIT FOR STATE OF CHARGE - Unit shall be in horizontal
position to ensure unit’s vent ports are free from blockage. After
approximately 5-8 seconds, unit LED status indicator shall illuminate
indicating power cell state of charge.
Ensure LED status indicator
and cooling fan are operational. Prior to continuing to step 7, the
LED status indicator should show a single green bar (last LED bar) to
indicate the unit’s power cells are fully charged. Also under full
charge the fan will ratchet but not enable.
4−7
NOTE
Under a full charge, the last green LED bar may blink. This does not
indicate a malfunction. A nonblinking lighted green bar or a blinking
green bar at the bottom of the LED column, both indicate a full
charge.
7. CHECK DC VOLTAGE READING AT DC RECEPTACLE TERMINALS.
power cells are fully charged (see step 6.)
Ensure
28.5 (+-0.57 VDC) with power cells at full state of charge.
8. FUNCTIONAL CHECK COMPLETE - Unit should remain plugged in to AC
power until required for use.
4−8
CHAPTER 5
PERFORMANCE DATA
SECTION 1. INTRODUCTION
5-1.
PURPOSE
This chapter provides performance data for the TI2000GPU-24 (Turbo
Start 2 000).
Continual reference to this information will enable the
user to obtain maximum performance, utilization and service life from
the Turbo Start.
Although maximum performance is not always required,
regular referral to this chapter is recommended for the following reasons:
a.
To generate knowledge of unit’s performance margins to enable
the operator to make sound judgment when unexpected conditions or
alternate operational requirements are encountered.
b.
To enable the user to readily recognize situations requiring
maximum performance.
c.
To gain experience in accurately estimating the effects of
variables for which data is not presented.
d. To help the operator determine if an aircraft system malfunction exists by comparing actual performance with expected performance.
NOTE
The information provided in this chapter is primarily intended for
operational planning and is most useful when planning operations under
unfamiliar conditions or environmental extremes.
The data may also be
used to establish local operating procedures and to ensure
unit’s
operational life is maximized.
5-2.
GENERAL
The data presented covers the maximum range of conditions and performance that can reasonably be expected.
In each area of performance,
the effects of temperature and DC electrical load demand relating to
the ground power support requirements are presented. Wherever practical, data is presented conservatively. However, NO GENERAL CONSERVATISM
HAS BEEN APPLIED. All performance data presented is within the applicable limits of the Turbo Start.
5-1
SECTION II
DATA CRITERIA
5-3
DATA BASIS
The type of data used is indicated at the bottom of each performance
chart under DATA BASIS. The applicable report and date of the data
are also given. The data provided generally are based on one of
three categories:
a.
Derived From Actual Controlled Testing.
obtained on a similar unit type.
Controlled test data
b. Calculated Data. Data based on tests, but not on a similar
unit type placed under a controlled test.
c. Estimated Data. Data based on estimates using rules of physics, mathematics, and electrical engineering principles and concepts, but not verified by tests.
5-4.
SPECIFIC CONDITIONS
The data presented are accurate only for specific conditions listed
under the title of each chart or graph. Variables for which data are
not presented, but which may affect that phase of performance, are
discussed in associated text.
Where data are available or reasonable
estimates can be made, the amount that each variable affects performance will be given.
5-5.
GENERAL CONDITIONS
In addition to the specific conditions, the following general conditions are applicable to the performance data.
a.
Variation in Aircraft.
Power demand differences between individual aircraft of the same make and model are known to exist due
to variations in DC electrical system efficiency.
These differences, however, are considered insignificant and are not individually accounted for.
b.
Ground Support and Aircraft Instrument Variations.
The data
shown in the performance charts do not account for instrument tolerance differences or inaccuracies.
5-6.
DEFINITIONS OF ABBREVIATIONS
Unless otherwise indicated, the abbreviations defined in Chapter 1 will
be applicable to all charts and graphs in this chapter.
5-2
FIGURE 5-1
TI2000GPU-24 OUTPUT VOLTAGE
24
OUTPUT VOLTAGE
20
16
5-3
12
8
4
0
0
10
20
30
40
MINUTES
46 AMP CONSTANT CURRENT LOAD
FIGURE 5-2
50
60
MAXIMUM OUTPUT CURRENT
***
3000
2700
****
0
** **
(+25 C Temp)
2400
* ***
2100
*****
*****
AMPS
1800
1500
* * *****
1200
0
5-4
*********
(-29 C Temp)
900
*****
**********
****
600
300
0
0
5
10
15
20
SECONDS
Calculations based on actual test data at Pratt-Whitney Canada on 30 March 1992.
FIGURE 5-3
25
30
5-5
CHAPTER 6
CARE AND MAINTENANCE
SECTION I.
6-1.
UNIT CARE
GENERAL
Although the TI2000GPU-24 (Turbo Start 2000) has been ruggedized
and made weather resistant within the scope of unit’s intended use,
it is essential that good general care be taken to maintain unit in
good operating condition and to maximize unit’s operational life.
6-2. AFTER USE - Unit should be protected from the environmental
elements and man made hazards. Ideally unit should be secured in a
building or shed. Most importantly, unit shall be fully covered if
stored exposed to environmental elements.
1.
KEEP UNIT RECEPTACLES AND OUTER CASE CLEAN - wipe with dry cloth.
2.
KEEP FOREIGN OBJECTS OUT OF UNIT - Cover unit to prevent
foreign objects, water, and dirt from entering vent ports and receptacles.
3.
KEEP FROM PROLONGED EXPOSURE TO EXTREMELY DAMP ENVIRONMENTS
Cover unit to prevent migration of moisture. If unit is operated in
extremely damp environments unit should be kept in an environmentally
controlled building.
4. KEEP UNIT PLUGGED INTO AC POWER SUPPLY WHEN NOT IN USE. (CHECK
FUSE WINDOW FOR PROPER SETTING). To maximize life of power cells and
to ensure unit is always ready for use, unit should remained plugged
in to AC power when not in use. NEVER LET DISCHARGED UNIT SIT FOR
MORE THAN 24 HOURS WITHOUT FULLY RECHARGING POWER CELLS.
5. PROTECT DC POWER CABLE AND AC POWER CORD FROM DAMAGE - Prevent
from being cut, gouged, crushed, dragged or otherwise abused.
6-1
SECTION II.
MAINTENANCE
6-3. MAINTENANCE OF UNIT - The Turbo Start 2000 is a maintenancefree unit, no repairs are authorized. Warranty will be void if unit
is tampered with.
If unit fails to operate contact Manufactures Warranty Claim (see unit warranty).
WARRENTY VOID STICKERS
Chapter 7
Push To Test Modification
General Information And Operation
7-1.
General
THIS MODIFICATION HAS BECOME STANDARD EQUIPMENT FOR EACH OF OUR
UNITS.
BOTH MILITARY AND CIVILIAN CLIENTS HAVE FOUND THIS MODIFICATION TO BE CRITICAL TO THEIR OPERATION. THE PUSH TO TEST BUTTON IS
USED TO INDICATE THE CAPACITY OF THE POWER CELLS WITHOUT APPLYING AC
INPUT POWER. IT ALLOWS THE END USER TO CHECK THE STATUS OF THE POWER
CELLS. THIS LETS THE OPERATOR KNOW IF THERE IS ENOUGH POWER TO PERFORM ANOTHER ENGINE START, OR IF THE UNIT HAS TO BE RETURNED TO AC
POWER TO ALLOW IT TO RECHARGE.
7-2.
OPERATION
1) MAKE SURE THAT YOU WAIT AT LEAST 2 MINUTES AFTER AC POWER IS APPLIED, OR
DC POWER IS EXTRACTED FROM THE UNIT, BEFORE YOU DEPRESS THE PUSH TO TEST
BUTTON. THIS WILL ENSURE A CORRECT READING.
2) WITHOUT AC POWER INPUT OR DC POWER OUTPUT, SIMPLY DEPRESS THE PUSH TO TEST
BUTTON ON THE FACE PLATE AND HOLD FOR APPROXIMATELY 15 SECONDS.
3) AT THIS TIME THE LED BAR GRAPH SHOULD LIGHT UP INDICATING THE STATUS OF
THE POWER CELLS.
4) THE FAN SHOULD ALSO OPERATE AT THIS TIME. IF YOU DO NOT HEAR THE FAN
RUNNING, STOP DEPRESSING THE BUTTON AND CHECK FOR ANY OBSTRUCTIONS TO THE
FAN.
5) NEVER DEPRESS THE PUSH TO TEST BUTTON WHILE THE UNIT IS PLUGGED INTO AC
POWER FOR RECHARGE, OR PLUGGED INTO AIRCRAFT FOR DC POWER OUTPUT.
6) NEVER DEPRESS THE PUSH TO TEST BUTTON FOR MORE THAN 30 SECONDS. THIS MAY
CAUSE A TEMPERATURE SENSOR TO TEMPORARILY DISRUPT PUSH TO TEST FUNCTION. (IF
THIS SENSOR IS TRIPPED, ALLOW TEN MINUTES FOR UNIT TO COOL BEFORE OPERATING
PUSH TO TEST BUTTON.)
STATUS
7-1
R
0
Y
1/2
G
OK
PARAGRAPH INDEX
120-240 VAC Charger and AC to DC Converter Limits,
3-4
24 VDC Ground Power (NO 120 or 240 VAC Power Supply) Engine Starting
or DC system Power, 4-6
24 VDC Ground Power (With 120/240 VAC Power) System High Power Demand
(21-1500 Amps) or Engine Starting,
4-7
28.5 VDC Ground Power (with 120/240 VAC Power) System Low Power Demand (20 Amps or less), 4-8
Abbreviations,
1-5
AC Power Cord Limits,
After Use,
3-5
6-2
Appendix A Line Cord Table
Before Operation Check,
4-5
Continuous Output Rate, 28.5 VDC Constant Output,
Data Basis,
5-3
DC Functional Check,
4-12
Definitions of Abbreviations,
Dimensions, Figure
2-1
Discharge Load Curve, Figure
Description
5-6
5-2
1-3
Engine Starting Power,
Environmental,
3-9
3-11
Functional Check Procedures,
Forms and Records,
1-6
General, Chapter 1,
1-1
General, Chapter 2,
2-1
General, Chapter 3,
3-2
General, Chapter 4,
4-1
General, Chapter 5,
5-2
General, Chapter 6,
6-1
General Conditions,
5-5
General Details, Figure
2-2
General Specifications,
2-2
4-10
3-8
PARAGRAPH INDEX
Index,
1-4
Maintenance of Unit,
6-3
Maximum Output Current, Figure
5-3
One (1) Hour Rate, 24 VDC Constant Output,
Operating Limits and Restrictions,
Operating Procedures,
Operating Position,
Performance,
4-2
4-4
3-12
4-3
Power Cell Recharge,
4-9
Power Cell Recharge Limits,
Purpose, Chapter 3,
3-1
Purpose, Chapter 5,
5-1
3-3
Rated Peak Output (Engine Starting),
3-7
Required Equipment for Functional Check,
Specific Conditions,
Temperature,
3-6
4-11
5-4
3-10
Temperature Conversion Chart, Figure
5-1
Unit Operation During Aircraft Fueling/Defueling,
Use of Word Shall, Should and May,
Warning, Caution and Notes Defined,
1-7
1-2
3-13
APPENDIX A
OPTIONAL LINE CORDS FOR WORLDWIDE OPERATIONS
COUNTRY
HZ
TESLA PART #
Afganistan
Algeria
American Samoa
Angola
Anguilla (U.K.)
Antigua
Argentina
Aruba
Australia
Austria
Azores (Portugal)
VOLTS
220
220
240
220
240
230
220
115
240
220
220
50
50
60
50
50
60
50
60
50
50
50
TI25000-004
TI25000-004
TI25000-011
TI25000-100
TI25000-005
TI25000-005
TI25000-011
TI25000-001
TI25000-011
TI25000-003
TI25000-004
Old British Line Cord Set
Old British Line Cord Set
Australian Line Cord Set
Europlug Line Cord Set
United Kingdom Line Cord Set
United Kingdom Line Cord Set
Australian Line Cord Set
North American Line Cord Set
Australian Line Cord Set
Cont. European Line Cord Set
Old British Line Cord Set
Bahamas
Bahrain
Bangladesh
Barbados
Belguim
Belize (Br. Hond.)
Benon
Bermuda
Bolivia
Botswana
Brazil
Bulgaria
Burkina Faso
Burma (Now Myanmar)
Burundi
120
220
220
115
220
110
220
120
220
220
110
220
220
230
220
60
50
50
50
50
60
50
60
50
50
60
50
50
50
50
TI25000-001
TI25000-005
TI25000-004
TI25000-001
TI25000-003
TI25000-001
TI25000-004
TI25000-005
TI25000-003
TI25000-005
TI25000-001
TI25000-003
TI25000-100
TI25000-005
TI25000-003
North American Line Cord Set
United Kingdom Line Cord Set
Old British Line Cord Set
North American Line Cord Set
Cont. European Line Cord Set
North American Line Cord Set
Old British Line Cord Set
United Kingdom Line Cord Set
Cont. European Line Cord Set
United Kingdom Line Cord Set
North American Line Cord Set
Cont. European Line Cord Set
Europlug Line Cord Set
United Kingdom Line Cord Set
Cont. European Line Cord Set
Cambodia
Cameroon
Canada
Canary Islands (Spain)
Cape Verde, Rep. of
Cayman Islands
Central African Republic
Chad
Channel Islands
Chile
China, Peoples Republic of
Christmas Island (Australia)
Cocos Islands (Australia)
Columbia
Congo, Republic of
Cook Island (New Zealand)
Costa Rica
Curacao Islands
Cyprus
Czech, Republic of
220
230
120
220
220
120
220
220
240
220
220
240
240
220
220
240
120
110
240
220
50
50
60
b
50
60
50
50
50
50
50
50
50
60
50
50
60
60
50
50
TI25000-100
TI25000-003
TI25000-001
TI25000-003
TI25000-003
TI25000-001
TI25000-100
TI25000-003
TI25000-005
TI25000-002
TI25000-011
TI25000-011
TI25000-011
TI25000-100
TI25000-100
TI25000-011
TI25000-001
TI25000-001
TI25000-005
TI25000-003
Europlug Line Cord Set
Cont. European Line Cord
North American Line Cord
Cont. European Line Cord
Cont. European Line Cord
North American Line Cord
Europlug Line Cord Set
Cont. European Line Cord
United Kingdom Line Cord
Italian Line Cord Set
Australian Line Cord Set
Australian Line Cord Set
Australian Line Cord Set
Europlug Line Cord Set
Europlug Line Cord Set
Australian Line Cord Set
North American Line Cord
North American Line Cord
United Kingdom Line Cord
Cont. European Line Cord
Denmark
Djibouti, Republic of
Dominica
Dominican Republic
220
220
230
110
50
50
50
60
TI25000-300
TI25000-003
TI25000-005
TI25000-001
Denmark Line Cord Set
Cont. European Line Cord Set
United Kingdom Line Cord Set
North American Line Cord Set
A-1
Set
Set
Set
Set
Set
Set
Set
Set
Set
Set
Set
APPENDIX A (Cont.)
OPTIONAL LINE CORDS FOR WORLDWIDE OPERATIONS
COUNTRY
HZ
TESLA PART #
Ecuador
Egypt
El Salvador
England
Equatorial Guinea
Estonia
Ethiopia
VOLTS
120
220
115
240
220
220
220
60
50
60
50
50
50
50
TI25000-001
TI25000-100
TI25000-001
TI25000-005
TI25000-100
TI25000-003
TI25000-003
North American Line Cord
Europlug Line Cord Set
North American Line Cord
United Kingdom Line Cord
Europlug Line Cord Set
Cont. European Line Cord
Cont. European Line Cord
Fiji
Finland
France
French Guiana
240
220
220
220
50
50
50
50
TI25000-011
TI25000-003
TI25000-003
TI25000-003
Australian Line Cord Set
Cont. European Line Cord Set
Cont. European Line Cord Set
Cont. European Line Cord Set
Gabon
Gambia
Georgia
Germany
Ghana
Gibraltar
Greece
Greenland (Denmark)
Grenada
Guadeloupe
Guam
Guatemala
Guinea
Guinea-Bissau
Guyana
220
220
220
220
220
240
220
220
230
220
110-120
120
220
220
110
50
50
50
50
50
50
50
50
50
50
60
60
50
50
50/60
TI25000-003
TI25000-005
TI25000-003
TI25000-003
TI25000-005
TI25000-005
TI25000-003
TI25000-300
TI25000-005
TI25000-003
TI25000-001
TI25000-001
TI25000-003
TI25000-003
TI25000-001
Cont. European Line Cord
United Kingdom Line Cord
Cont. European Line Cord
Cont. European Line Cord
United Kingdom Line Cord
United Kingdom Line Cord
Cont. European Line Cord
Denmark Line Cord Set
United Kingdom Line Cord
Cont. European Line Cord
North American Line Cord
North American Line Cord
Cont. European Line Cord
Cont. European Line Cord
North American Line Cord
Set
Set
Set
Set
Set
Set
Set
Haiti
Honduras
Hong Kong
Hungary
110-120
110
220
220
50-60
60
50
50
TI25000-001
TI25000-001
TI25000-005
TI25000-003
North American
North American
United Kingdom
Cont. European
Set
Set
Set
Set
Iceland
India
Indonesia
Iran
Iraq
Ireland, Republic of
Isle of Man
Israel
Italy
Ivory Coast
220
220-250
220
220
220
220
240
230
220
220
50
50
50
50
50
50
50
50
50
50
TI25000-003
TI25000-004
TI25000-003
TI25000-003
TI25000-005
TI25000-005
TI25000-005
TI25000-200
TI25000-002
TI25000-100
Cont. European Line Cord Set
Old British Line Cord Set
Cont. European Line Cord Set
Cont. European Line Cord Set
United Kingdom Line Cord Set
United Kingdom Line Cord Set
United Kingdom Line Cord Set
Israel Line Cord Set
Italy Line Cord Set
Europlug Line Cord Set
Jamaica
Japan
Jordan
110
110
220
50
50/60
50
TI25000-001 North American Line Cord Set
TI25000-001 North American Line Cord Set
TI25000-005 United Kingdom Line Cord Set
Kenya
Korea, South
Kuwait
240
220
240
50
60
50
TI25000-005 United Kingdom Line Cord Set
TI25000-003 Cont. European Line Cord Set
TI25000-005 United Kingdom Line Cord Set
A-2
Line
Line
Line
Line
Cord
Cord
Cord
Cord
Set
Set
Set
Set
Set
Set
Set
Set
Set
Set
Set
Set
APPENDIX A (Cont.)
OPTIONAL LINE CORDS FOR WORLDWIDE OPERATIONS
COUNTRY
HZ
TESLA PART #
Laos
Latvia
Lebanon
Lesotho
Liberia
Liechtenstein
Lithuania
Luxembourg
Libya
VOLTS
220
220
220
240
120
220
220
220
230
50
50
50
50
60
50
50
50
50
TI25000-001
TI25000-003
TI25000-100
TI25000-004
TI25000-005
TI25000-006
TI25000-003
TI25000-003
TI25000-002
North American Line Cord Set
Cont. European Line Cord Set
Europlug Line Cord Set
Old British Line Cord Set
United Kingdom Line Cord Set
Switzerland Line Cord Set
Cont. European Line Cord Set
Cont. European Line Cord Set
Italy Line Cord Set
Macao
Madagascar
Maderia (Portugal)
Majorca
Malawi
Malaysia
Maldives
Mali, Republic of
Malta
Martinique
Mauritania
Mauritius
Mexico
Monaco
Mongolia
Montseurrat
Morocco
Mozambique
220
220
220
220
230
240
230
220
240
220
220
230
127
220
220
230
220
220
50
50
50
50
50
50
50
50
50
50
50
50
60
50
50
60
50
50
TI25000-004
TI25000-003
TI25000-004
TI25000-003
TI25000-005
TI25000-005
TI25000-004
TI25000-003
TI25000-005
TI25000-003
TI25000-100
TI25000-005
TI25000-001
TI25000-003
TI25000-100
TI25000-005
TI25000-003
TI25000-003
Old British Line Cord Set
Cont. European Line Cord Set
Old British Line Cord Set
Cont. European Line Cord Set
United Kingdom Line Cord Set
United Kingdom Line Cord Set
Old British Line Cord Set
Cont. European Line Cord Set
United Kingdom Line Cord Set
Cont. European Line Cord Set
Europlug Line Cord Set
United Kingdom Line Cord Set
North American Line Cord Set
Cont. European Line Cord Set
Europlug Line Cord Set
United Kingdom Line Cord Set
Cont. European Line Cord Set
Cont. European Line Cord Set
Namibia (W.S. Africa)
Nepal
Neth. Antilles
Netherlands
New Caledonia
New Zealand
Nicaragua
Niger
Nigeria
Norfolk Islands (Australia)
North Ireland
North Mariana Islands (U.S.)
Norway
220-250
220
220
220
220
230
120
220
230
240
220
115
220
50
50
50/60
50
50
50
60
50
50
50
50
60
50
TI25000-004
TI25000-004
TI25000-003
TI25000-003
TI25000-003
TI25000-011
TI25000-001
TI25000-100
TI25000-005
TI25000-011
TI25000-005
TI25000-001
TI25000-003
Old British Line Cord Set
Old British Line Cord Set
Cont. European Line Cord Set
Cont. European Line Cord Set
Cont. European Line Cord Set
Australian Line Cord Set
North American Line Cord Set
Europlug Line Cord Set
United Kingdom Line Cord Set
Australian Line Cord Set
United Kingdom Line Cord Set
North American Line Cord Set
Cont. European Line Cord Set
Okinawa
Oman
100-120
240
60
50
TI25000-001 North American Line Cord Set
TI25000-005 United Kingdom Line Cord Set
Pakistan
Panama
Papua New Guinea
Paraguay
Peru
Philippines
Piccairn Islands (U.K.)
Poland
Portugal
Puerto Rico
230
110
240
220
110
115
240
220
220
120
50
60
50
50
50/60
60
50
50
50
60
TI25000-004
TI25000-001
TI25000-011
TI25000-100
TI25000-001
TI25000-001
TI25000-004
TI25000-003
TI25000-003
TI25000-001
Qatar
240
50
TI25000-005 United Kingdom Line Cord Set
A-3
Old British Line Cord Set
North American Line Cord Set
Australian Line Cord Set
Europlug Line Cord Set
North American Line Cord Set
North American Line Cord Set]
Old British Line Cord Set
Cont. European Line Cord Set
Cont. European Line Cord Set
North American Line Cord Set
APPENDIX A (Cont.)
OPTIONAL LINE CORDS FOR WORLDWIDE OPERATIONS
COUNTRY
HZ
TESLA PART #
Romania
Russia
Rwanda
VOLTS
220
220
220
50
50
50
TI25000-003 Cont. European Line Cord Set
TI25000-003 Cont. European Line Cord Set
TI25000-100 Europlug Line Cord Set
Saudia Arabia
Scotland
Senegal
Seychelles
Sierra Leone
Singapore
Slovakia
Somalia
South Africa
Spain
Sri Lanka
St. Pierre & Miquelon (France)
St. Kitts & Nevis
St. Lucia
St. Vincent
Sudan
Surinam
Svalbard (Norway)
Swaziland
Sweden
Switzerland
Syria
220
220
220
240
230
230
220
220
220-250
220
230
115
230
240
230
240
115
220
230
220
220
220
50/60
50
50
50
50
50
50
50
50
50
50
60
60
50
50
50
60
50
50
50
50
50
TI25000-003
TI25000-005
TI25000-003
TI25000-005
TI25000-005
TI25000-005
TI25000-003
TI25000-003
TI25000-004
TI25000-003
TI25000-004
TI25000-001
TI25000-005
TI25000-005
TI25000-005
TI25000-005
TI25000-003
TI25000-003
TI25000-004
TI25000-003
TI25000-006
TI25000-100
Cont. European Line Cord Set
United Kingdom Line Cord Set
Cont. European Line Cord Set
United Kingdom Line Cord Set
United Kingdom Line Cord Set
United Kingdom Line Cord Set
Cont. European Line Cord Set
Cont. European Line Cord Set
Old British Line Cord Set
Cont. European Line Cord Set
Old British Line Cord Set
North American Line Cord Set
United Kingdom Line Cord Set
United Kingdom Line Cord Set
United Kingdom Line Cord Set
United Kingdom Line Cord Set
Cont. European Line Cord Set
Cont. European Line Cord Set
Old British Line Cord Set
Cont. European Line Cord Set
Switzerland Line Cord Set
Europlug Line Cord Set
Tahiti
Taiwan
Tanzania
Thailand
Togo
Tonga
Trinadad & Tobango
Tunisia
Turkey
220
110
230
220
220
115
230
220
220
50
60
50
50
50
60
60
50
50
TI25000-003
TI25000-001
TI25000-005
TI25000-100
TI25000-003
TI25000-004
TI25000-005
TI25000-100
TI25000-003
Cont. European Line Cord Set
North American Line Cord Set
United Kingdom Line Cord Set
Europlug Line Cord Set
Cont. European Line Cord Set
Old British Line Cord Set
United Kingdom Line Cord Set
Europlug Line Cord Set
Cont. European Line Cord Set
Uganda
United Arab Emir.
United Kingdom & Ireland
United States
Uraguay
220
220
240
120
220
50
50
50
60
50
TI25000-004
TI25000-005
TI25000-005
TI25000-001
TI25000-011
Old British Line Cord Set
United Kingdom Line Cord Set
United Kingdom Line Cord Set
North American Line Cord Set
Australian Line Cord Set
Venezuela
Vietnam
Virgin Islands
120
220
120
60
50
60
TI25000-001 North American Line Cord Set
TI25000-003 Cont. European Line Cord Set
TI25000-001 North American Line Cord Set
Wales
Western Samoa
220
230
50
50
TI25000-005 United Kingdom Line Cord Set
TI25000-005 United Kingdom Line Cord Set
Yemen
Yugoslavia
220
220
50
50
TI25000-005 United Kingdom Line Cord Set
TI25000-003 Cont. European Line Cord Set
Zaire, Republic of
Zambia
Zimbabwe
220
220
220
50
50
50
TI25000-003 Cont. European Line Cord Set
TI25000-005 United Kingdom Line Cord Set
TI25000-005 United Kingdom Line Cord Set
A-4
APPENDIX A (Cont.)
UNIVERSAL LINE CORD KIT FOR WORLDWIDE OPERATIONS
NOTE: TESLA UNIVERSAL AC LINE CORD KIT, P/N: TI25000-U00, IS FOR
UNITS ORIGINALLY BUILT WITH THE UNIVERSAL AC LINE CORD OPTION ONLY.
THE AC ADAPTER OPTION IS TESLA P/N TI16000-19 AND MUST BE ORDERED
WITH THE ORIGINAL PROCUREMENT OF UNIT(S). UNIT(S) MAY BE RETURNED TO
TESLA INDUSTRIES, FOR A NOMINAL COST, AND MODIFIED TO ALLOW OPERATION
WITH THE UNIVERSAL AC LINE CORD KIT.
TESLA UNIVERSAL AC LINE CORD KIT,
THE FOLLOWING FOUR PART NUMBERS:
TI25000-U01
TI25000-U04
TI25000-U03
TI25000-U05
P/N: TI25000-U00, IS COMPRISED OF
NORTH AMERICAN LINE CORD
OLD BRITISH LINE CORD
EUROPEAN 10A/250V
ENGLAND 10A/250V
TESLA REPLACEMENT 8 FOOT DC POWER CORD, P/N: TI2006-501, IS AVAILABLE
UPON REQUEST. (CUSTOM LENGTHS ARE ALSO AVAILABLE TO SUIT THE CUSTOMERS OPERATIONAL REQUIREMENTS.)
A-5