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TABLE OF CONTENTS
TITLE
Page
1-1
2-1
2-1
2-2
3-1
3-1
3-1
4-1
4-1
4-2
4-5
5-1
5-1
5-2
6-1
6-1
6-2
Index 1
CHAPTER 1
CHAPTER 2
Section I
Section II
CHAPTER 3
Section I
Section II
CHAPTER 4
Section I
Section II
INTRODUCTION
UNIT DESCRIPTION AND OPERATION
Unit
Description
OPERATING LIMITS AND RESTRICTIONS
General
Operational Restrictions and Safety Limits
OPERATING PROCEDURES
Unit Operation
Operating Procedures
Section III Functional Check Procedures
CHAPTER 5
Section I
Section II
CHAPTER 6
Section I
Section II
INDEX
PERFORMANCE DATA
Introduction
Data Criteria
CARE AND MAINTENANCE
Unit Care
Maintenance
LIST OF ILLUSTRATIONS
Figure
2-1
Title
Page
2-3
2-2
2-4
5-3
5-4
5-5
Dimensions
2-2
General Details
2-3
Fuse Setting Procedures
Temperature Conversion Chart
Discharge Load Curve
Maximum Output Current
5-1
5-2
5-3
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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 criti-
cal 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 proce-
dures 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 sup-
port 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.
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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
Ampere
amp
AC
Alternating Current
Celsius
C
cont
DC
Continuous
Direct Current
Fahrenheit
Feet
F
Ft
FWD
GPU
Hr
Forward
Ground Power Unit
Hour
Hz
Hertz
Kg
Kilograms
Kw
Kilowatts
°
Degree
LED
MAX
MIN
VAC
VDC
Light Emitting Diode
Maximum
Minimum
Volts, Alternating Current
Volts, Direct Current
Explosion Hazard Potential
Shock Hazard Potential
Guard from moisture
Guard from incorrect power source
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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 ac-
ceptable method of accomplishment.
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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 incor-
porates 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 op-
erations 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 de-
mand 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 120-
240 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 equip-
ment 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)
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120 VAC Setting
2-1
240 VAC Setting
SECTION II DESCRIPTION
2.2. GENERAL SPECIFICATIONS
WEIGHT
UNIT:
111 lbs (50.39 Kg)
8.5 lbs (3.86 Kg)
0.4 lbs (0.18 Kg)
DC POWER CABLE:
AC POWER CORD:
INPUT POWER AC
TI2000GPU-24:
105-125 VAC 60 Hz
6.50 amps max.
3.25 amps max.
TI2000GPU-24-UNV: 210-250 VAC 50/60 Hz
TI25000-U01 NORTH AMERICAN LINE CORD
105-125 VAC 60 Hz
6.50 amps max.
3.25 amps max.
3.25 amps max.
3.25 amps max.
TI25000-U04 OLD BRITISH LINE CORD
210-250 VAC 50/60 Hz
TI25000-U03 EUROPEAN 10A/250V
210-250 VAC 50/60 Hz
TI25000-U05 ENGLAND 10A/250V
210-250 VAC 50/60 Hz
OUTPUT POWER DC
CONVERTER:
28.5 VDC TO 20 AMPS, 24 VDC 21 AMPS AND ABOVE.
POWER CELLS:
PEAK OUTPUT:
24 VDC
3000 AMPS
POWER CELL
DRY, HIGH RATE DISCHARGE, RECHARGEABLE, MAINTENANCE-FREE
DC POWER CABLE
LENGTH: 8 FT
AIRCRAFT CONNECTOR: 3 PIN RECEPTACLE (MS25488)
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2-3
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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)
ENLARGEMENT 2 120 VAC SETTING
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)
10) Snap fuse clip
back into the housing
(GENTLY). DO UBLE
CHECK VO LTAGE
WINDO W PRIO R
TO PLUGGING UNIT
INTO AC PO WER
7) Replace the
8) Completely insert
white clip in to fuse
clip (GENTLY) until
it snaps into place.
9) Insert fuse clip
white clip back into
the fuse clip. Take
care not to damage
the tabs.
back into fuse housing
EVENLY on both sides.
DO NOT FO RCE, if fuse
clip does not go in easy,
it means fuses are mis-
aligned, realign fuses and
insert again.
2-4
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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 TI2000GPU-
24 (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. Com-
pliance with these limitations and restrictions will ensure that own-
ers/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 Acid-
type 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 recep-
tacle.
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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’ )520 ,1&255(&7
32: (5 6285&(
INTERNAL AC TO DC CONVERTER: LIMITED (see paragraph 3-6, 3-8 and
3-10). AC power cord does not have to be disconnected when con-
verter power output is no longer required. Once DC power demand
is terminated the unit’s intelligent charger will remain on line to
ensure power cells are charged to maximum capacity.
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 cus-
tomer specified AC power cord. Some customers may specify a univer-
sal 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): LIMITED TO 210-250 VAC 50-60 Hz
power source only.
FOR MORE INFORMATION ON POWER CORDS SEE APPENDIX A
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3-2
AC Line Cords
Cont. Europe
U.K.
Old British
CAUTION
North American
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)
o
o
3000 peak amps at 25 C (77 F) (See Figure 5-3).
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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 illumi-
nate. If all LED status indicator bars illuminate, both the con-
verter and power cells are supplying 24 VDC power output (see para-
graph 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 ef-
ficient 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
1000-1500 peak starting amps
1500-1800 peak starting amps
1800-2500 peak starting amps
2500-3000 peak starting amps
50% charged
60% charged
70% charged
80% charged
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 ambi-
ent 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
o
o
SOAKED, warmed for a minimum of 3 hours above +10C (+41 F) or 2
o
o
hours above +20C (+68 F); WARMED SOAKED, cooled for 1 hour below
o
o
+38C (+100 F).
Operating range:
o
o
o
o
without AC power -40C (-40 F) TO +60C (+140 F)
o
o
o
o
with AC Power -30C (-22 F) TO +50C (+124 F)
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Storage range:
o
o
o
o
-60C (-76 F) TO +60C (+140 F)
(C0NTINUED ON NEXT PAGE)
3-4
CAUTION
Unit may be damaged if operated when unit’s cold or heat soaked tempera-
ture exceed the specified limit. If unit is operated when cold or heat
soaked temperature limit is exceeded, a full functional check should be
accolished prior to continued use.
NOTE
If unit should overheat, an over-temperature sensor will shut down 120-
240 VAC functions (charger and converter) until unit cools to normal
operating temperatures.
3-11. ENVIRONMENTAL
Operating any electrical equipment in the presence of moisture cre-
ates 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 con-
nectors/receptacles
b. minimize moisture entering FWD inlet and AFT out-
let 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.
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3-5
WARNING
********SHOCK HAZARD POTENTIAL*********
Severe injury, or Death, from electrical shock is possible when per-
sonnel 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 sus-
pected. 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 dur-
ing use.
3-12. OPERATING POSITION
Without 120-240 VAC power cord: Horizontal or vertical.
Horizontal only, for propper unit ventilation, when 120-240 VAC line
cord is plugged in and exhaust fan is running.
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.
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3-6
CAUTION
Unit dainlet and outlet d
and/or s restricted.
3-13. UNIT OPERATION DURING AIRCRAFT FUELING/DEFUELING
Power ouput is restricted to 24 VDC power cell output oly. DO
NOT CONNECT 120 or 240 VAC POWER SUPPLY. 120-240 VAC power
(charger or AC-DC converter) functions of unit shall not be oper-
ated 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.
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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, Sec-
tion 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 perfor-
mance resulting from variations in ambient temperature, mode of op-
eration, state of charge (with or without 120 or 240 VAC power), and
aircraft DC bus system inefficiency (voltage drops).
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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 capabili-
ties 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 readi-
ness 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
1. CHECK FUSE WINDOW FOR PROPER SETTING (120/240) BEFORE PLUGGING
UNIT INTO THE AC POWER SOURCE TO BE USED. REMEMBER,when the AC line
cord is plugged in, the unit must be placed in the horizontal posi-
tion to allow the cooling fan to operate properly!
STATUS
NOTE:
A full charge is indicated by her a sdy lighted green bar or a
blinking green bar at the bottof the graph column.The fan will
also exhibit ratcheting but winot comon when the unit is fully
rged.
2. CHECK UNIT FOR EVIDENCE OF DAMAGE - Check for dents, punctures,
case distortion or misalignment, cracked or loose connectors, and
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that cooling fan is functioning.
4-2
REMEMBER,when the AC line in, the unit must be placed
in the horizontal position cooling fan to operate prop-
Unit may overheat if coolDo not operate if cooling
fan fails.(More than 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 recep-
tacle. 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
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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 DE-
MAND (21 amps and above) OR ENGINE STARTING.
1. TRANSPORT UNIT - The Turbo Start 2000 is easily transported us-
ing 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 SET-
TING).- - 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 cur-
rent demand is above 20 amps, converter output voltage will drop be-
low 28.5 VDC and two or more LED status indicator bars will illumi-
nate. 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
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(if necessary).
4-4
4-8 28.5 VDC GROUND POWER (WITH 120/240 VAC POWER) SYSTEM LOW POWER
DEMAND (20 amps or less).
1. TRANSPORT UNIT - The Turbo Start 2000 is easily transported us-
ing 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 SET-
TING).- 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 air-
craft power demand is less than 20 amps converter output will remain
at 28.5 VDC (only one GREEN LED status indicator bar will illumi-
nate). 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 neces-
sary).
4-9 POWER CELL RECHARGE
1. CONNECT AC POWER CORD TO UNIT - Unit shall be in horizontal po-
sition 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 approxi-
mately 5-8 seconds, ensure unit’s LED status indicator illuminates
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indicating power cell state of charge and cooling fan is operating.
Unit may overhefan 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 con-
nected 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 dis-
play ratcheting but not come on whe the unit is fully charged.
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4-6
SECTION III.
FUNCTIONAL CHECK PROCEDURES
4-10. FUNCTIONAL CHECK PROCEDURES
This section deals with normal functional check procedures, and in-
cludes all steps necessary to ensure the Turbo Start 2000 is func-
tioning 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 SET-
TING).-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
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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. Ensure
power cells are fully charged (see step 6.)
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.
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4−8
CHAPTER 5
PERFORMANCE DATA
SECTION 1. INTRODUCTION
5-1. PURPOSE
This chapter provides performance data for the TI2000GPU-24 (Turbo
Start 2000). 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 rea-
sons:
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 malfunc-
tion exists by comparing actual performance with expected perfor-
mance.
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 perfor-
mance that can reasonably be expected. In each area of performance,
the effects of temperature and DC electrical load demand relating to
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the ground power support requirements are presented. Wherever practi-
cal, data is presented conservatively. However, NO GENERAL CONSERVATISM
HAS BEEN APPLIED. All performance data presented is within the appli-
cable 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. Controlled test data
obtained on a similar unit type.
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 phys-
ics, mathematics, and electrical engineering principles and con-
cepts, 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 perfor-
mance will be given.
5-5. GENERAL CONDITIONS
In addition to the specific conditions, the following general condi-
tions are applicable to the performance data.
a. Variation in Aircraft. Power demand differences between indi-
vidual aircraft of the same make and model are known to exist due
to variations in DC electrical system efficiency. These differ-
ences, however, are considered insignificant and are not individu-
ally accounted for.
b. Ground Support and Aircraft Instrument Variations. The data
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shown in the performance charts do not account for instrument toler-
5
U
b
FIGURE 5-1
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TI2000GPU-24 OUTPUT VOLTAGE
24
20
16
12
8
4
0
0
30
50
10
20
40
60
MINUTES
46 AMP CONSTANT CURRENT LOAD
FIGURE 5-2
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MAXIMUM O UTPUT CURRENT
3000
2700
2400
2100
1800
1500
1200
900
*
*
*
*
*
*
*
*
*
*
*
*
*
0
*
(+ 25 C Temp)
*
*
*
*
*
*
*
*
*
*
*
*
*
*
*
*
*
*
*
*
*
*
*
*
*
*
*
*
*
*
*
*
*
*
*
*
*
*
*
*
*
(-290 C Temp)
*
*
*
**
600
300
0
5
20
0
10
15
25
30
SECO NDS
Calculations based on actual test data at Pratt-Whitney Canada on 30 March 1992.
FIGURE 5-3
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5-5
CHAPTER 6
CARE AND MAINTENANCE
SECTION I. UNIT CARE
6-1. 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 recep-
tacles.
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.
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6
SECT
MAINT
6-3. MAINTENANCE OF UNIT - The Tus a maintenance-
free unit, no repairs are authorizell be void if unit
is tampered with. If unit fails tt Manufactures War-
ranty Claim (see unit warranty).
WARRENTY VOID STICKERS
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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 MODIFICA-
TION 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 PER-
FORM 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
R
0
Y
G
1/2
OK
7-1
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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 De-
mand (20 Amps or less), 4-8
Abbreviations, 1-5
AC Power Cord Limits, 3-5
After Use, 6-2
Appendix A Line Cord Table
Before Operation Check, 4-5
Continuous Output Rate, 28.5 VDC Constant Output, 3-8
Data Basis, 5-3
DC Functional Check, 4-12
Definitions of Abbreviations, 5-6
Dimensions, Figure 2-1
Discharge Load Curve, Figure 5-2
Description 1-3
Engine Starting Power, 3-9
Environmental, 3-11
Functional Check Procedures, 4-10
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
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PARAGRAPH INDEX
Index, 1-4
Maintenance of Unit, 6-3
Maximum Output Current, Figure 5-3
One (1) Hour Rate, 24 VDC Constant Output, 3-6
Operating Limits and Restrictions, 4-2
Operating Procedures, 4-4
Operating Position, 3-12
Performance, 4-3
Power Cell Recharge, 4-9
Power Cell Recharge Limits, 3-3
Purpose, Chapter 3, 3-1
Purpose, Chapter 5, 5-1
Rated Peak Output (Engine Starting), 3-7
Required Equipment for Functional Check, 4-11
Specific Conditions, 5-4
Temperature, 3-10
Temperature Conversion Chart, Figure 5-1
Unit Operation During Aircraft Fueling/Defueling, 3-13
Use of Word Shall, Should and May, 1-7
Warning, Caution and Notes Defined, 1-2
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APPENDIX A
OPTIONAL LINE CORDS FOR WORLDWIDE OPERATIONS
COUNTRY
Afganistan
Algeria
American Samoa
Angola
Anguilla (U.K.)
Antigua
Argentina
Aruba
Australia
Austria
VOLTS
HZ TESLA PART #
220
220
240
220
240
230
220
115
240
220
220
50
50
60
50
50
60
50
60
50
50
50
TI25000-004 Old British Line Cord Set
TI25000-004 Old British Line Cord Set
TI25000-011 Australian Line Cord Set
TI25000-100 Europlug Line Cord Set
TI25000-005 United Kingdom Line Cord Set
TI25000-005 United Kingdom Line Cord Set
TI25000-011 Australian Line Cord Set
TI25000-001 North American Line Cord Set
TI25000-011 Australian Line Cord Set
TI25000-003 Cont. European Line Cord Set
TI25000-004 Old British Line Cord Set
Azores (Portugal)
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 North American Line Cord Set
TI25000-005 United Kingdom Line Cord Set
TI25000-004 Old British Line Cord Set
TI25000-001 North American Line Cord Set
TI25000-003 Cont. European Line Cord Set
TI25000-001 North American Line Cord Set
TI25000-004 Old British Line Cord Set
TI25000-005 United Kingdom Line Cord Set
TI25000-003 Cont. European Line Cord Set
TI25000-005 United Kingdom Line Cord Set
TI25000-001 North American Line Cord Set
TI25000-003 Cont. European Line Cord Set
TI25000-100 Europlug Line Cord Set
TI25000-005 United Kingdom Line Cord Set
TI25000-003 Cont. European Line Cord Set
Cambodia
Cameroon
Canada
220
230
120
220
220
120
220
220
240
220
220
240
240
220
220
240
120
110
240
220
50
50
60
b
TI25000-100 Europlug Line Cord Set
TI25000-003 Cont. European Line Cord Set
TI25000-001 North American Line Cord Set
TI25000-003 Cont. European Line Cord Set
TI25000-003 Cont. European Line Cord Set
TI25000-001 North American Line Cord Set
TI25000-100 Europlug Line Cord Set
TI25000-003 Cont. European Line Cord Set
TI25000-005 United Kingdom Line Cord Set
TI25000-002 Italian Line Cord Set
TI25000-011 Australian Line Cord Set
TI25000-011 Australian Line Cord Set
TI25000-011 Australian Line Cord Set
TI25000-100 Europlug Line Cord Set
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
50
60
50
50
50
50
50
50
50
60
50
50
60
60
50
50
TI25000-100 Europlug Line Cord Set
TI25000-011 Australian Line Cord Set
TI25000-001 North American Line Cord Set
TI25000-001 North American Line Cord Set
TI25000-005 United Kingdom Line Cord Set
TI25000-003 Cont. European Line Cord Set
Czech, Republic of
Denmark
Djibouti, Republic of
Dominica
220
220
230
110
50
50
50
60
TI25000-300 Denmark Line Cord Set
TI25000-003 Cont. European Line Cord Set
TI25000-005 United Kingdom Line Cord Set
TI25000-001 North American Line Cord Set
Dominican Republic
A-1
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APPENDIX A (Cont.)
OPTIONAL LINE CORDS FOR WORLDWIDE OPERATIONS
COUNTRY
Ecuador
Egypt
El Salvador
England
Equatorial Guinea
Estonia
VOLTS
120
220
115
240
220
220
220
HZ TESLA PART #
60
50
60
50
50
50
50
TI25000-001 North American Line Cord Set
TI25000-100 Europlug Line Cord Set
TI25000-001 North American Line Cord Set
TI25000-005 United Kingdom Line Cord Set
TI25000-100 Europlug Line Cord Set
TI25000-003 Cont. European Line Cord Set
TI25000-003 Cont. European Line Cord Set
Ethiopia
Fiji
Finland
France
240
220
220
220
50
50
50
50
TI25000-011 Australian Line Cord Set
TI25000-003 Cont. European Line Cord Set
TI25000-003 Cont. European Line Cord Set
TI25000-003 Cont. European Line Cord Set
French Guiana
Gabon
Gambia
Georgia
Germany
Ghana
Gibraltar
Greece
Greenland (Denmark)
Grenada
Guadeloupe
Guam
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
TI25000-003 Cont. European Line Cord Set
TI25000-005 United Kingdom Line Cord Set
TI25000-003 Cont. European Line Cord Set
TI25000-003 Cont. European Line Cord Set
TI25000-005 United Kingdom Line Cord Set
TI25000-005 United Kingdom Line Cord Set
TI25000-003 Cont. European Line Cord Set
TI25000-300 Denmark Line Cord Set
TI25000-005 United Kingdom Line Cord Set
TI25000-003 Cont. European Line Cord Set
TI25000-001 North American Line Cord Set
TI25000-001 North American Line Cord Set
TI25000-003 Cont. European Line Cord Set
TI25000-003 Cont. European Line Cord Set
Guatemala
Guinea
Guinea-Bissau
Guyana
50/60 TI25000-001 North American Line Cord Set
Haiti
110-120
110
220
50-60 TI25000-001 North American Line Cord Set
Honduras
Hong Kong
Hungary
60
50
50
TI25000-001 North American Line Cord Set
TI25000-005 United Kingdom Line Cord Set
TI25000-003 Cont. European Line Cord Set
220
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
50
50
50
50
50
50
50
50
50
50
TI25000-003 Cont. European Line Cord Set
TI25000-004 Old British Line Cord Set
TI25000-003 Cont. European Line Cord Set
TI25000-003 Cont. European Line Cord Set
TI25000-005 United Kingdom Line Cord Set
TI25000-005 United Kingdom Line Cord Set
TI25000-005 United Kingdom Line Cord Set
TI25000-200 Israel Line Cord Set
TI25000-002 Italy Line Cord Set
TI25000-100 Europlug Line Cord Set
220
Jamaica
Japan
Jordan
110
110
220
50
TI25000-001 North American Line Cord Set
50/60 TI25000-001 North American Line Cord Set
50
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
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APPENDIX A (Cont.)
OPTIONAL LINE CORDS FOR WORLDWIDE OPERATIONS
COUNTRY
Laos
Latvia
Lebanon
Lesotho
VOLTS
220
220
220
240
120
220
220
220
HZ TESLA PART #
50
50
50
50
60
50
50
50
50
TI25000-001 North American Line Cord Set
TI25000-003 Cont. European Line Cord Set
TI25000-100 Europlug Line Cord Set
TI25000-004 Old British Line Cord Set
TI25000-005 United Kingdom Line Cord Set
TI25000-006 Switzerland Line Cord Set
TI25000-003 Cont. European Line Cord Set
TI25000-003 Cont. European Line Cord Set
TI25000-002 Italy Line Cord Set
Liberia
Liechtenstein
Lithuania
Luxembourg
Libya
230
Macao
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 Old British Line Cord Set
TI25000-003 Cont. European Line Cord Set
TI25000-004 Old British Line Cord Set
TI25000-003 Cont. European Line Cord Set
TI25000-005 United Kingdom Line Cord Set
TI25000-005 United Kingdom Line Cord Set
TI25000-004 Old British Line Cord Set
TI25000-003 Cont. European Line Cord Set
TI25000-005 United Kingdom Line Cord Set
TI25000-003 Cont. European Line Cord Set
TI25000-100 Europlug Line Cord Set
TI25000-005 United Kingdom Line Cord Set
TI25000-001 North American Line Cord Set
TI25000-003 Cont. European Line Cord Set
TI25000-100 Europlug Line Cord Set
TI25000-005 United Kingdom Line Cord Set
TI25000-003 Cont. European Line Cord Set
TI25000-003 Cont. European Line Cord Set
Madagascar
Maderia (Portugal)
Majorca
Malawi
Malaysia
Maldives
Mali, Republic of
Malta
Martinique
Mauritania
Mauritius
Mexico
Monaco
Mongolia
Montseurrat
Morocco
Mozambique
Namibia (W.S. Africa)
Nepal
220-250
220
50
50
TI25000-004 Old British Line Cord Set
TI25000-004 Old British Line Cord Set
Neth. Antilles
Netherlands
New Caledonia
New Zealand
Nicaragua
Niger
220
220
220
230
120
220
230
240
50/60 TI25000-003 Cont. European Line Cord Set
50
50
50
60
50
50
50
50
60
50
TI25000-003 Cont. European Line Cord Set
TI25000-003 Cont. European Line Cord Set
TI25000-011 Australian Line Cord Set
TI25000-001 North American Line Cord Set
TI25000-100 Europlug Line Cord Set
TI25000-005 United Kingdom Line Cord Set
TI25000-011 Australian Line Cord Set
TI25000-005 United Kingdom Line Cord Set
TI25000-001 North American Line Cord Set
TI25000-003 Cont. European Line Cord Set
Nigeria
Norfolk Islands (Australia)
North Ireland
North Mariana Islands (U.S.)
Norway
220
115
220
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
TI25000-004 Old British Line Cord Set
TI25000-001 North American Line Cord Set
TI25000-011 Australian Line Cord Set
TI25000-100 Europlug Line Cord Set
50/60 TI25000-001 North American Line Cord Set
60
50
50
50
60
TI25000-001 North American Line Cord Set]
TI25000-004 Old British Line Cord Set
TI25000-003 Cont. European Line Cord Set
TI25000-003 Cont. European Line Cord Set
TI25000-001 North American Line Cord Set
Qatar
240
50
TI25000-005 United Kingdom Line Cord Set
A-3
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APPENDIX A (Cont.)
OPTIONAL LINE CORDS FOR WORLDWIDE OPERATIONS
COUNTRY
Romania
Russia
VOLTS
220
220
HZ TESLA PART #
50
50
50
TI25000-003 Cont. European Line Cord Set
TI25000-003 Cont. European Line Cord Set
TI25000-100 Europlug Line Cord Set
Rwanda
220
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
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 TI25000-003 Cont. European Line Cord Set
50
50
50
50
50
50
50
50
50
50
60
60
50
50
50
60
50
50
50
50
50
TI25000-005 United Kingdom Line Cord Set
TI25000-003 Cont. European Line Cord Set
TI25000-005 United Kingdom Line Cord Set
TI25000-005 United Kingdom Line Cord Set
TI25000-005 United Kingdom Line Cord Set
TI25000-003 Cont. European Line Cord Set
TI25000-003 Cont. European Line Cord Set
TI25000-004 Old British Line Cord Set
TI25000-003 Cont. European Line Cord Set
TI25000-004 Old British Line Cord Set
TI25000-001 North American Line Cord Set
TI25000-005 United Kingdom Line Cord Set
TI25000-005 United Kingdom Line Cord Set
TI25000-005 United Kingdom Line Cord Set
TI25000-005 United Kingdom Line Cord Set
TI25000-003 Cont. European Line Cord Set
TI25000-003 Cont. European Line Cord Set
TI25000-004 Old British Line Cord Set
TI25000-003 Cont. European Line Cord Set
TI25000-006 Switzerland Line Cord Set
TI25000-100 Europlug Line Cord Set
Sweden
Switzerland
Syria
Tahiti
Taiwan
Tanzania
Thailand
Togo
220
110
230
220
220
115
230
220
220
50
60
50
50
50
60
60
50
50
TI25000-003 Cont. European Line Cord Set
TI25000-001 North American Line Cord Set
TI25000-005 United Kingdom Line Cord Set
TI25000-100 Europlug Line Cord Set
TI25000-003 Cont. European Line Cord Set
TI25000-004 Old British Line Cord Set
TI25000-005 United Kingdom Line Cord Set
TI25000-100 Europlug Line Cord Set
Tonga
Trinadad & Tobango
Tunisia
Turkey
TI25000-003 Cont. European Line Cord Set
Uganda
220
220
240
120
220
50
50
50
60
50
TI25000-004 Old British Line Cord Set
TI25000-005 United Kingdom Line Cord Set
TI25000-005 United Kingdom Line Cord Set
TI25000-001 North American Line Cord Set
TI25000-011 Australian Line Cord Set
United Arab Emir.
United Kingdom & Ireland
United States
Uraguay
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
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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, P/N: TI25000-U00, IS COMPRISED OF
THE FOLLOWING FOUR PART NUMBERS:
TI25000-U01
TI25000-U04
TI25000-U03
TI25000-U05
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 CUSTOM-
ERS OPERATIONAL REQUIREMENTS.)
A-5
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