C-130 Aviation Ground Support Equipment

Hydraulics International, Inc. (HII) has over 40 years history of cutting edge aircraft ground support equipment (GSE) ingenuity and new product technology innovation. HII is one of the world’s leading manufacturers of both military and commercial aircraft ground support equipment (GSE), especially in the supply of our new generation Hydraulic Test Equipment, which will keep hydraulic system in aircraft, helicopter, aircraft hydraulic flight components, hoses, pipes, tubing, valves, valve actuation etc. operating safely and effectively. Our Hydraulic Test Equipment are also robustly designed to provide diagnostic instrumentation for innovative testing, self-calibration, maintaining, servicing and troubleshooting of hydraulic equipment, components & system under testing.  HII is the preferred Provider of our new generation Portable Hydraulic Test Stands, Stationary Hydraulic Test Benches etc. to the military & commercial aerospace industry.

C-130 Aviation Ground Support Equipment

C-130 Aviation Ground Support Equipment

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Cabin Leakage Tester (CLT)

Military Aircraft Ground Support Equipment

AF/M32T-1

CLT

CABIN PRESSURIZATION AND LEAKAGE TESTER

Qualified and in-service with the USAF, USN, USMC. Services all rotary and fixed wing military and commercial aircraft.

AF/M32T-1 Military Aircraft Ground Support Equipment

Flow  400 SCFM

Diesel Engine Drive (AF/M32T-1, P/N: 93038-100, NSN: 4920-01-381-4950

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4

   Flow  400 SCFM

     Electric Motor Driven (AF/M24T-3, P/N: 78011-100, NSN: 4920-01-063-0120)

  Electric Motor Driven (AF/M24T-3, P/N: 96384-100, NSN: 4920-01-435-8545)

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Aircraft Engine Corrosion Control Cart (CCC)

CCC

840 Units

LARGE CORROSION CONTROL CART, MODEL 051496-100

SMALL CORROSION CONTROL CART, MODEL 051497-100, Model: A/M32M-40, NSN: 4920-01-536-1924

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Microsoft Word - CCC, 051496-100

CCC, 051496-100 (2)

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C-130 (Aviation Ground Support Equipment)

SUMMARY OF HII RECENT MILITARY GSE DESIGN AND DEVELOPMENTS

CORROSION CONTROL CART, MODEL 051496-100 providing servicing support  to V-22 Osprey (US Marine Corps)

Also used by US Navy, US Air Force, Foreign Military Sales (FMS) for supporting their P-3 Program, KC-130R, KC-130J etc

See Solicitation Number: N68335-13-P-0361 (Department of US Navy):

https://www.fbo.gov/index?s=opportunity&mode=form&id=102c269c5338bd491e6b960a7d4e2f3a&tab=core&_cview=0

See Solicitation Number: N68335-05-R-0038 (Department of US Navy):

https://www.fbo.gov/index?s=opportunity&mode=form&id=bba3579ae869b7fce9620168da9574c0&tab=core&_cview=1

Leading Particulars

ENVELOPE SIZE: Length: 86 inches

Width:  60 inches

Height:  52 inches

Weight (Empty): 1665 LBS Weight (Gross): 3450 LBS

GENERATOR SET:

Diesel Engine: 10 HP at 3600 RPM, 418CC, Air Cooled

Fuel Tank: 4 Gallons

Generator: 240 VAC, 3 Phase, 60 Hz WATER SYSTEM:

Tank Capacity: 200 Gallons

Pressure: 0-110 PSI (60 Nominal)

Flow: 6 GPM SOLUTION  SYSTEM:

Tank Capacity: 25 Gallons

Pressure: 0-110 PSI

Flow: 6 GPM AIR SYSTEM:

Compressor: 8 SCFM at 60 PSI

WATER/SOLUTION PUMPS: Positive Displacement Gear Type Bronze Construction

PUMP MOTOR: 2 HP, 1750 RPM, Totally Enclosed, None Ventilated, 230/460 VAC, 3 Phase

BATTERY: 12 VDC, Dry Cell (Sealed). 220 CCA

TIRES: 4.48-8, 8 Ply, 60 P5 PSI

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UHTS Military Aircraft Ground Support Equipment

F-16 (Aviation Ground Support Equipment)

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     F-16 including T-50, F-4, F-5, F-18, C-130, C-17,C-5, MiG29, Su-30, A400M, F-2A, F-2B, F-CK-1, Rafael, Gripen, Hawk, Eurofighter, Transport Aircraft & Helicopter etc
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USAF Acquisition Program for UHTS: 

https://govtribe.com/contract/idv/fa853311d0001

HII ‘s new generation of Universal Hydraulic Test Stand (UHTS) with the latest state-of-the-art features and components. UHTS utilizes a high resolution LCD Display HMI (Human Machine Interface)  with resistive touch screen for operation and monitoring of UHTS System and functions. HII is currently on Contract with USAF to build UHTS.  Accepted in-service by USAF for supporting their F-16 and can be used to support any transport or fighter aircraft or helicopter in their inventory.

P/N: 101198-100

NSN: 4920-01-591-9361RN

UHTS
           New
UNIVERSAL HYDRAULIC TEST STAND (UHTS)
Electric Motor Driven,
Dual Independent System
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Model: A/M27T-16
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101198-100
4920-01-591-9361RN
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P/N: 101198-100, NSN: 4920-01-591-9361RN
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Model: A/M27T-16 replacing MK3A
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Test Medium: Hydraulic fluid:
MIL-PRF-83282,
MIL-PRF-5606 and MIL-PRF-87257
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Flow Rate Capacity:

One System: 53   GPM at 3000 PSI, 40   GPM at 4000 PSI, 32   GPM at 5000 PSI per system

Two System: 106   GPM at 3000 PSI, 80   GPM at 4000 PSI, 64   GPM at 5000 PSI Or   combined

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UHTS comes with an integral   built Hydraulic Purification System (HPS) that provides continuous cooling,   filtering moisture and to remove hydraulic fluid particulates, water,   chlorinated solvents, absorbed air & gases removal from hydraulic fluid.   Keeping hydraulic fluid clean and eliminates the need of changing     hydraulic fluid for a long period of time. HPS work in a very   cost-effective way to minimize hydraulic fluid usage, minimize hazardous   waste disposal needs, reduce deployment foot print and sharply   reduce   hydraulic maintenance and associated costs.

USAF Hydraulic Purification Articles: 

http://www.wpafb.af.mil/News/Article-Display/Article/399918/hydraulic-fluid-purification-could-soon-be-a-dod-wide-program/

Purification   Performance

1)  Contaminant  removal: 55 gallon of hydraulic fluid in 5 hours.

2)  Water:  From   1000 to less than 200 PPM.

3)  Chlorinated  solvents:  From 400 to less than 100 PPM.

4)  Air & Gas: 100% dissolved air removal, 98% (by   volume) removal.

5)  Particulate:   Cleanliness level equal to or better than   NAS 1638 class 3.

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F-16 (Aviation Ground Support Equipment)

P/N: 101197-100

NSN: 4920-01-592-0750RN

                                                             UHTS F16 Diesel
          New
UNIVERSAL HYDRAULIC TEST STAND (UHTS)
Diesel Engine Driven, Dual Independent Systems
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Model: A/M27T-17
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101197-100
4920-01-592-0750RN
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P/N: 101197-100, NSN: 4920-01-592-0750RN
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Model: A/M27T-17 replacing MJ-2A
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Test Medium: Hydraulic fluid:
MIL-PRF-83282, MIL-PRF-5606, MIL-PRF-87257
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Flow Rate Capacity:

One System: 53   GPM at 3000 PSI, 40   GPM at 4000 PSI, 32   GPM at 5000 PSI per system

Two System: 106   GPM at 3000 PSI, 80   GPM at 4000 PSI, 64   GPM at 5000 PSI Or   combined

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UHTS comes with an integral   built Hydraulic Purification System (HPS) that provides continuous cooling,   filtering moisture and to remove hydraulic fluid particulates, water,   chlorinated solvents, absorbed air & gases removal from hydraulic fluid.   Keeping hydraulic fluid clean and eliminates the need of changing     hydraulic fluid for a long period of time. HPS work in a very   cost-effective way to minimize hydraulic fluid usage, minimize hazardous   waste disposal needs, reduce deployment foot print and sharply   reduce   hydraulic maintenance and associated costs.

Purification Performance

1)   Contaminant   removal: 55 gallon of hydraulic fluid in 5 hours.

2) Water: From   1000 to less than 200 PPM.

3)  Chlorinated   solvents:  From 400 to less than 100 PPM.

4)  Air   & Gas: 100% dissolved air removal, 98% (by   volume) removal.

5)  Particulate:  Cleanliness level equal to or better than   NAS 1638 class 3.

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New
Military Aircraft Ground Support Equipment

UHTS is set-up with Instruments capability to be verified by an inexpensive Instrument Verification Set (IVS) within 15 minutes minimizing UHTS downtime and cost. All readings on UHTS are shown on high resolution LCD Display & Engine Performance Module.  NO GAUGES including Transducers or Flowmeters are required to be removed for calibration.  IVS can be connected directly  to UHTS to verify that Transducers & Flowmeters are within acceptable accuracy.  IVS is certified and traceable to NIST.

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UHTS Testing at HII Facility (1)
UHTS (Model: A/M27T-17, NSN: 4920-01-592-0750RN) undergoing vigorous testing (June 2012) at HII facility.
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Military Aircraft Ground Support Equipment
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        F-16 including F-4, F-5, F-18, C-130, C-17, C-5, MiG29, Su-30, F-2A, F-2B, F-CK-1, Rafael, Gripen, Hawk, Eurofighter, Transport Aircraft & Helicopter etc
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MK-3A
PORATBLE HYDRAULIC TEST STAND
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Electric Motor Driven,
Dual Independent System
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MK-3A
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NSN: 4920-00-528-8780
&
4920-00-045-7543 (MK-3A)
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MK-3A being replaced by UHTS
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Test Medium: Hydraulic fluid:
MIL-H-5606, MIL-H-83282, Skydrol 500 A and B, or as specified by customer when ordering.
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Flow Rate Capacity:

One System: 35   GPM at 3000 PSI, 15 GPM at 5000 PSI

Two System: 70 GPM (35 GPM/system at 3000 PSI), 30 GPM (15 GPM/system at 5000 PSI) Or combined

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MJ2A
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PORATBLE HYDRAULIC TEST STAND
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Diesel Engine Driven,
Dual Independent Systems
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MJ-2A
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P/N 070515-100 (MJ2A)
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2000 units sold
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Test Medium: Hydraulic fluid:

MIL-H-5606, MIL-H-83282Skydrol 500 A and B, or as specified by customer when ordering.

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MJ2A is OBSOLETE and replaced by UHTS
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Flow Rate Capacity:

One System: 35   GPM at 3000 PSI, 15 GPM at 5000 PSI

Two System: 70 GPM (35 GPM/system at 3000 PSI), 30 GPM (15 GPM/system at 5000 PSI) Or  combined

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COMPARISON

(MJ-2A vs UHTS)

ITEM

SPECIFICATIONS

MJ-2A

 

UHTS

 

1

Design

30 years old Technology, number of major   component are obsolete.

New   generation of Hydraulic Test stands with the latest state-of-the-art features   and components. UHTS has also been qualified to the most rigorous military   requirement testings such as environmental, Electro Magnetic Interference,   Mobility, Reliability, Maintainability, etc.

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Aircraft Application

Accepted in-service by USAF for their F-16   and some designated aircraft.

Accepted in-service by USAF for supporting   their F-16 and can be used to support any transport or fighter aircraft in   their inventory.

3

Hydraulic Purification

System (HPS)

Using normal Filter Elements.

UHTS comes with an AF qualified integral   built Hydraulic Purification System (HPS) that provides continuous cooling,   filtering to remove hydraulic fluid particulates, water,   chlorinated solvents, absorbed air & gases from aircraft hydraulic fluid as   well as test stand. This purification process eliminates the need of changing   hydraulic fluid for a long period of time. HPS works   in a very cost effective way to minimize aircraft hydraulic fluid usage,   minimize hazardous waste disposal needs, reduce deployment foot print and   sharply reduce aircraft hydraulic components maintenance and associated   costs. (See attached article from USAF, which is self-explanatory.)

Purification   Performance

1)       Contaminant removal: 55 gallons of hydraulic fluid in 5   hrs.

2)       Water:  From   1000 to less than 100 PPM

3)       Chlorinated solvents:    From 400 to less than 100 PPM

4)       Air & Gas: 100% dissolved air removal, 98% (by   volume) removal

5)       Particulate: Cleanliness level equal to or better than   NAS 1638 class 3.

 

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Test Medium

Hydraulic   fluid, MIL-H-5606, MIL-H-83282

Hydraulic   fluid, MIL-PRF-5606, MIL-PRF-83282, and MIL-PRF-87257.

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Flow Rate Capacity

One system

35   GPM at 3000 PSI

15 GPM at 5000 PSI

Two system

70 GPM (35 GPM/system   at 3000 PSI)

30   GPM (15 GPM/system at 5000 PSI)

or   combined

One system

53   GPM at 3000 PSI

40   GPM at 4000 PSI

32   GPM at 5000 PSI per system

Two system

106   GPM at 3000 PSI

80   GPM at 4000 PSI

64   GPM at 5000 PSI

Or   combined

 

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Operating Conditions

Ambient Temperature Range

-40ºF to +125ºF

Altitude:     Sea level to 6000 feet

Relative Humidity:   0% to 100%

Test Stand Position:   Up to 8 1/2° from horizontal

Ambient Temperature Range

-40ºF to +125ºF

Altitude:     Sea level to 7000 feet

Relative Humidity:   0% to 100%

Test Stand Position:    Up to 8 1/2° from horizontal

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Hydraulic Reservoir

60 U.S. Gallon capacity

vented to atmosphere and fluid is subject   to ambient

90 U.S. Gallon capacity

Is completely sealed to atmosphere. This   feature prevents airborne particulate, moisture and air to enter hydraulic   fluid, maintaining purity of hydraulic fluid all the time.

 

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Control Panel

Conventional Control and Analog Instrumentation

Combination of manual and automated   controls. Fully military qualified with System Diagnostic, Built-in Test   System and Human Machine Interface Touch Screen Operator Panel enabling ease   of Operator Operation, Troubleshooting and ease of Calibration.

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Drive Unit

Diesel Engine, 210 HP, naturally aspirated,   non-EPA certified, obsolete

Diesel Engine, 300 HP, turbo-turbo charged,   EPA certified to TIER III, Multi Fuel.

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Engine Diagnostic System

No

Cummins   engine QSB6.7 is an electronic fuel and Governor controlled via Electronic   Control Module (ECM) and full diagnostic control feature facilitating safety   and troubleshooting features.

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Fuel tank capacity

42 US gallons

60 US   gallon

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External Fill and Purification Ports

No

External Reservoir Fill and Discharge Ports enables the Operator   to fill the Hydraulic Reservoir from an outside source, or to remove clean   filtered hydraulic fluid from the Reservoir also External Purification Ports   allow purification of external fluid source.

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Back Pressure Regulator

No

Back Pressure Regulator allows operation in both aircraft   (Closed Loop) or test Stand Reservoir (Open Loop) operation with pressurized   or non-pressurized aircraft reservoir systems.

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Instrument Calibration/Verification

All Instruments require removal and   verified calibration by third party, these results in equipment downtime and   excessive cost.

UHTS is set-up with Instruments capability to be verified by an   inexpensive Instrument Verification Set (IVS) within 15 minutes minimizing Equipment   downtime and cost.

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Fault Diagnostic System

No

If a fault exists before system operation or a fault occurs   during system operation, fault conditions will immediately report to HMI   message field and warning horn is activated. Any fault condition will be   permanently stored to retentive memory of HMI computer. Up to 200 fault   conditions can be stored in retentive memory

If a critical fault occurs during system operation, engine will   be automatically shut down in 10 seconds. Each fault condition has a   corresponding fault diagnostics page at HMI. Fault diagnostics page provides   detail fault information and recommend corrective actions.

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115 VAC Utility Power

No

UHTS incorporates Invertor to provide 115 VAC, Single Phase   Electrical Power for Utilities.

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Wet Weight

6,3000 Lbs

7,800 Lbs

All stated Specifications are subject to change.

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USAF HPS
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100033-100
P/N: 100033-100 * NSN: 4330-01-587-5425
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100033-100, Air Force Purifier 115 VAC_Page_1 (US Air Force Standard Hydraulic Fluid Purifier)
connected to either MK-3A or MJ-2A
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Removes:
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1) 100% free water .
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2) Dissolved water to less than 100  ppm .
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3) 100% entrained gases .
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4) 98% of dissolved gases
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5) Particulate contamination to produce a cleanliness level of NAS Class 3.
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Dual Power Driven: Diesel Engine Driven or operates on household power supply.
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  Towable at 20 mph max. over improved roads.
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Aircraft Fuel Tank Test Trolley

C-130 (Aviation Ground Support Equipment)
P/N: 99556-100
C-130 (Aviation Ground Support Equipment)
C-130 (Aviation Ground Support Equipment)
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Hydraulic Jack Pumping Unit

https://hiigroupasia.com/aircraft-fuel-tank-test-trolley/

Hydraulic Jack Pumping Unit, Diesel / Electric Power Driven

P/N: 071699-100

NSN: 4320-01-562-6243

Standard Unit used by US Air Force  for all their tankers, bombers and transport aircraft such as:

C-130, KC-130, KC-135, B-2, B-52 & C-5.

C-130 (Aviation Ground Support Equipment)

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F-16 (Aviation Ground Support Equipment)
 Portable Hydraulic Fluid Servicing Unit, PMU-71/E
pmu-71e
P/N: 061481-100, NSN: 3040-01-546-5962
pmu-71e
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 Portable Engine Oil Servicing Unit, PMU-72/E
pmu-72e
P/N: 061475-100, NSN: 3040-01-546-4129
pmu-72e
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Portable Transmission Fluid Servicing Unit, PMU-73/E
pmu73e1
P/N: 061477-100, NSN: 3040-01-546-4146
 pmu-73e
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Portable Rotor Fluid Servicing Unit, PMU-74/E
pmu74e1
P/N: 061479-100, NSN: 3040-01-546-4126
9-pmu-74e1
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Hydraulic Fluid Servicing Unit, Filler and Pressurization,
0-3000 PSI Output Pressure, HSU-1-3K
fsu-1-5-3k
P/N: 080026-100, NSN: 4910-01-602-5069
10-fsu-1-5-3k-4

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