Paravion Heliporter H250 Series User manual

Heliporter®
By
Paravion Technology, Inc.
®
Owner’s Manual
H250 Series
Copyright© 2020
Paravion Technology, Inc.
®

Introduction
Congratulations! You have purchased one of the finest helicopter ground handling vehicles on the
market today. We at Paravion to be as
® ®
Technology, Inc. have strived to engineer the Heliporter
maintenance free and simple to operate as possible. This vehicle will be a useful addition to your
helicopter flight operation.
As with any new equipment, a necessary period of orientation should be observed. To maximize the
use and safety of the , we recommend that the operator practice the operations withoutHeliporter®
the aircraft abroad; then when proficiency is achieved, begin using with your aircraft in unconfined
areas.
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1
2001 Airway Avenue
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USA
©Copywright 2020, Paravion Technology, Inc. Paravion and Heliporter
®®
are registered trademarks of Paravion Technology, Inc.
Product specifications, prices, warranty and availability are subject to change without notice.

Table of Contents
Description Page
H250E Assembly Instructions....................................................................................3
H250TP Assembly Instructions .................................................................................4
H250E Operation .......................................................................................................5-6
H250TP Operation .....................................................................................................7-8
Socket Schedule .........................................................................................................9
H250 Battery Charger Operation ...............................................................................10
Service Instructions....................................................................................................11-12
APU Operation ..........................................................................................................13
Basic Replacement Parts ............................................................................................14
Warranty .....................................................................................................................15
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2

HP250E Assembly Instructions
Steering Handle Assembly
1. Remove tape from steering yoke.
2. Insert set screw into yoke.
3. Remove tape from the handle end.
4. Ensure key is still in handle end while inserting handle end into yoke.
5. Tighten set screw. Set screw should be recessed inside the yoke when tight.
Batteries
1. Connect leads labeled “Pump Power” to Positive (+) terminal.
2. Connect “Jumper” between the two batteries as shown below.
3. Connect “Frame Ground” to Negative (-) terminal on second battery. Ensure all connections
are tight.
4. If the APU option was included, this will also be operational by following the above steps.
Batteries
+_
Pump
Power Jumper Frame
Ground
+_
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HP250TP Assembly Instructions
Steering Handle Assembly
1. Locate tongue to line up holes.
2. Insert bolt as provided.
3. Tighten as necessary to engage locking nut.
Batteries
1. Connect leads labeled “Pump Power” to Positive (+) terminal.
2. Connect leads labeled “Frame Ground” to Negative (-) terminal.
Battery
Pump Power Frame Ground
+_
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4

Heliporter®
H250E Operation
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1. While the hydraulic power/pump is in the off position, rotate the twist grip (see Fig. 1) to aft
stop. With additional pressure, force the grip past stop to the “Coast” detent position. This
position allows the to freewheel and be maneuvered manually.Heliporter®
Note: Never attempt to position the under the aircraft by using the hydrostaticHeliporter®
drive system.
2. Observe that the lifting platform is in a full “Down” position before maneuvering the
Heliporter®under the aircraft.
3. Guide the between the skid gear by rotating the control handle assembly counterHeliporter®
clockwise to turn left and clockwise to turn right (see Fig. 1). Maneuver the Heliporter®
under the aircraft from front to rear.
Caution: Observe the aircraft belly area to avoid contacting antennas, lights, etc. with the
Heliporter®while maneuvering under the helicopter.
4. Engage the hydraulic pump switch by pushing the toggle switch forward and holding it in the
forward position.
Note: The toggle switch is preloaded toward the “Off” position, therefore the willHeliporter®
stop automatically when pressure is released. Never operate the pump switch unless the
Twist Grip and Raise & Lower Lever are in the neutral position.

Heliporter®
H250E Operation
4. Engage the hydraulic pump switch by pushing the toggle switch forward and holding it in
the forward position.
Note: The toggle switch is preloaded toward the “Off” position, therefore the Heliporter®
will stop automatically when pressure is released. Never operate the pump switch unless the
Twist Grip and Raise & Lower Lever are in the neutral position.
5. Raise the lifting platform slowly by pulling aft on the platform control until the Heliporter®
lift pads make contact with the aircraft pickup points. Release the platform control stick and
pump switch.
6. With proper alignment achieved and with the pump switch off, rotate the twist grip forward
to the spring loaded “Neutral” position. This will engage the hydrostatic brakes and prevent
the from moving as the helicopter's skids leave the ground. Re-engage the pumpHeliporter®
and continue to raise the platform.
7. When the desired height is achieved, release the platform control and hydraulic pump
switch. With controls released, the aircraft will remain in the desired position.
Caution: The helicopter can be lowered by pushing forward on the platform control without
the hydraulic pump operating. An abrupt forward movement of the platform control will
cause rapid lowering of the helicopter, possibly causing damage to the aircraft or personnel.
With the weight of the helicopter on the ground, it may be necessary to use the hydraulic
pump to fully lower the platform.
8. The twist grip (see Fig. 1) controls forward and aft movement of the , it also controlsHeliporter®
the throttle speed. The speed is determined by the degree of rotation to the twist grip. A small
rotation will move the slowly and full rotation will move the at fullHeliporter Heliporter
® ®
speed of 2.5 mph .
Caution: When engaging the hydrostatic drive, rotate the twist grip .slowly
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6

Heliporter®
H250TP Operation
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7
1. While the hydraulic power/pump is in the off position, rotate the twist grip (see Fig. 1) to aft
stop. With additional pressure, force the grip past stop to the “Coast” detent position. This
position allows the to freewheel and be maneuvered manually.Heliporter®
Note: Never attempt to position the under the aircraft by using the hydrostaticHeliporter®
drive system.
2. Observe that the lifting platform is in a full “Down” position before maneuvering the
Heliporter®under the aircraft.
3. Guide the between the skid gear by rotating the control handle assembly counterHeliporter®
clockwise to turn left and clockwise to turn right (see Fig. 1). Maneuver the Heliporter®
under the aircraft from front to rear.
Caution: Observe the aircraft belly area to avoid contacting antennas, lights, etc. with the
Heliporter®while maneuvering under the helicopter.
4. Engage the hydraulic pump switch by pushing the toggle switch forward and holding it in the
forward position.
Note: The toggle switch is preloaded toward the “Off” position, therefore the Heliporter®
will stop automatically when pressure is released. Never operate the pump switch unless the
Twist Grip and Raise & Lower Lever are in the neutral position.

Heliporter®
H250TP Operation
5. Raise the lifting platform slowly by pulling aft on the platform control until the Heliporter®
lift pads make contact with the aircraft pickup points. Release the platform control stick and
pump switch.
6. With proper alignment achieved and with the pump switch off, rotate the twist grip forward
to the spring loaded “Neutral” position. This will engage the hydrostatic brakes and prevent
the from moving as the helicopter's skids leave the ground. Re-engage the pumpHeliporter®
and continue to raise the platform.
7. When the desired height is achieved, release the platform control and hydraulic pump
switch. With controls released, the aircraft will remain in the desired position.
Caution: The helicopter can inadvertently be lowered by pushing forward on the platform
control without the hydraulic pump operating. An abrupt forward movement of the platform
control will cause rapid lowering of the helicopter, possibly causing damage to the aircraft or
personnel. With the weight of the helicopter on the ground, it may be necessary to use the
hydraulic pump to fully lower the platform.
8. The twist grip (see Fig. 1) controls forward and aft movement of the , it also controlsHeliporter®
the throttle speed. The speed is determined by the degree of rotation to the twist grip. A small
rotation will move the slowly and full rotation will move the at fullHeliporter Heliporter
® ®
speed of 2.5 mph .
Caution: When engaging the hydrostatic drive, rotate the twist grip .slowly
9. To move a helicopter while being supported on the lifting platform, engage the hydraulic pump
switch and rotate the left hand grip forward to move rearward. To move forward, rotateslowly
the left handgrip aft (See Fig. 1).slowly
10. When the aircraft is raised and proper speed and direction are achieved, the operator can move
the entire control handle assembly to the right or left of the aircraft to facilitate viewing the area
toward which the aircraft is moving.
CAUTION: Never take off or land over the .Heliporter®
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8

Heliporter®
HP250 Socket Schedule
C
B
A
C
B
A
E
D
G
F
H
JJ
N
LK
P
N
L
F
G
H
I
E
D
I
K
P
RR
QQ
SOCKETSCHEDULE
B
C
D
F
G
I
J
K
L
N
H
222, EC120
212,412,UH-1H
206B,206L,407,427
BK117,EC145,LUH-72
204
350,355
206B
206L,407,427,EC145,LUH-72,MD900
222,BK117,350,355,
212,412,UH-1H,BO105
204,430,MD900
BO105
EEC135/MD900
A430,EC130
EC120,EC130,EC135
P
OH-58
Q
OH-58
R
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9

Heliporter®
H150E-7200-3
Battery Charger Assembly
H150E-7200-3: This charger is fully automatic. It can be plugged in anytime the isHeliporter®
not in use and will maintain the batteries as needed.
LED Indicator information:
Red Flashing: Battery Bad Cell
Amber: Battery Weak < 12.5 V
Green: Full Charge/Power Connected
Green Flashing: Battery ECO Mode
Blue: Analysis stage
Blue Flashing: Desulfating pulses are in process
CAUTION: Do not operate while charger is plugged in.Heliporter®
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W - Service batteries with water
G - Grease all zerk locations
C - Charge batteries using provided charger
H - Service hydraulic system with 10W30
motor oil
Fig. 4
Heliporter®
Servicing Instructions
H
P
Fig. 3
H
Fig. 2
WC WC
G
G
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11

Heliporter®
Service Instructions
Recommended Lubricants and Service Terms
Grease: Quality lithium based automotive-type grease
Battery Fluids: Distilled water
Hydraulic Fluid: 10W30 Motor Oil
Service Points: (See Figs. 2, 3, and 4)
1. Check the battery fluid levels monthly. Fill to proper levels if low. (Fig. 2).
2. Check the hydraulic fluid level monthly. Fill to 1/2 of reservoir capacity with the platform
in full “down” position. (Fig. 3)
3. If stored outdoors, cover the charging system with a waterproof cover when not in use.
(Fig. 3)
Caution: Never operate the charger while covered.
4. If using pneumatic tires, maintain tire pressure to the tire manufacture's recommendation.
5. Inspect tires, hoses, couplings, cables, and electrical wires for serviceable condition before
each use.
6. Plug the charging system into AC electric receptacle for system recharging as necessary.
(Fig. 3)
7. Check all hardware at attachment points for security before each use.
8. Grease all zerks, a minimum of twice yearly. The wheel bearings should be greased more
often, as usage and environmental conditions dictate. (Fig. 2 & 4).
9. Replace the protective pads at lift contact points as necessary.
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HP250E APU Operation
The optional APU is available in 24 VDC. Prior to its use, check for proper voltage. To
operate the APU, simply plug the connector into the aircraft receptacle.
Make sure APU is properly stowed when not in use and keep the cord from coming into
contact with any moving parts.
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Heliporter®
HP250E Basic Replacement Parts
HE89100-1
Wheel Assy.
(Roller)
HE89100-3
Wheel Assy
(Keyed)
HE63701-1
Motor
HE63600-1
Cylinder
HE50500-1
Light Assy.
HE39510-4
Collar
HE38500-1
Bearing
HE63000-1
Valve
5/8 X 3½ SB
Bolt, Shoulder
H150-3200-1
Bolt Assy.
HE39800-2
120” Control Cable
(Fore / Aft Motion)
HE39800-2
120” Control Cable
(Lift Motion)
HE50530-1
Switch, Pump
HE50530-2
Switch, Light
Steering Handle
Detail
HE89100-10
Tire
HE89100-12
Split Rim
HE89200-2
Hub, Keyed
HE89200-1
Hub, Roller
HE89100-1
Wheel Assy (Roller)
HE89100-3
Wheel Assy (Keyed)
HE89210-1
Bushing
H150E-7200-3
Battery Charger
Assembly
HE63500-5 - Power Unit for E Models
S/N ending in 1324 and subsequent.
or
H250E-8000-1
Conversion Kit
or
HE63500-4 - 12V Power Unit for TP Models
HE63500-6 - 24V Power Unit for TP Models
HE89500-1
Coupling &
H89500-2
Spider
or
H250E-6001-1
Chain Coupler
Conversion Kit
HP250E
Parts Breakdown
Technology
Inc.
Paravion
®
Paravion
®
©2017 Paravion Technology, Inc.
Group 31
Deep Cycle Marine Battery
CCA 650
AMP 225
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14

WARRANTY
Warranty Terms: Paravion Technology, Inc. warrants that the components contained in this
®
product shall be free from defects in materials and workmanship under normal use and service for 1
year from the date of purchase, if and only if the product is maintained and operated in accordance
with the specifications and instructions provided by Paravion Technology, Inc.
®
Limitations and Exclusions: This warranty shall not apply to any product repaired or altered by
parties other than Paravion Technology, Inc. unless express prior authorization is granted; nor
®
shall this warranty apply to any product subjected to misuse or accident unless proof is submitted to
the satisfaction of Paravion Technology, Inc. that such misuse or accident was not a cause for the
®
claimed defect.
The sole responsibility and liability of Paravion Technology, Inc. and your exclusive remedy
®
under any claim arising out of, connected with, or resulting from this sale or the performance or
breach of any condition of warranty thereunder, or from the manufacture, delivery, or use of the
product shall be the repair or replacement of the defective parts.
In no event, whether as a result of a breach of contract, warranty, tort (including negligence) or
otherwise, shall Paravion Technology, Inc. be liable for any special, consequential, incidental or
®
penal damages or expenses including but not limited to loss of profit, goodwill, or revenues, loss of
associated equipment, cost of capital, cost of substitute products, facilities or services, down time,
or costs or claims of third parties for such damages or expense.
The foregoing warranty is exclusive and in lieu of all other warranties or remedies whether
written, oral, implied or statutory. Any and all implied warranties or merchantability, fitness for a
particular purpose, course of dealing, or usage of trade are hereby disclaimed and excluded.
Acceptance of this product by you shall constitute your acknowledgement and acceptance of the
terms, provisions, limitations, and exclusions set forth herein. Such terms, provisions, limitations,
and exclusions shall not be modified, deleted, or supplemented except by the express written
acknowledgement of Paravion Technology, Inc. Warranty is non-transferable and subject to
®
change without notice
Warranty Performance: All claims under this warranty shall be made to Paravion®
Technology, Inc. All returned parts must be shipped prepaid for evaluation to Paravion®
Technology, Inc. Full details of the symptoms of the malfunction should be included to assist in
this evaluation. Warranty credit or replacement will be extended only after
Paravion Technology, Inc. has determined that all conditions of this warranty
®
have been met.
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15

2001 Airway Avenue
Fort Collins, CO 80524
USA
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Phone: [phone]
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