F-18 (Aviation Ground Support Equipment)

    F-18 GSE

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F-18 (Aviation Ground Support Equipment)

MHLUS

 F-18 (Aviation Ground Support Equipment)

P/N 971480-70 (NSN 1730-01-446-2422) replaces MJ-4 Jammer

Electric Driven Model: MHU-83/E

P/N: 99511-100  replaced by P/N: 121233-100 (NSN: 1730-01-446-2422)

APPLICATION

Standard equipment for loading/unloading & transporting of aerial stores including munitions, fuel tanks, pylons, special weapons, & SAR packs weighing up to  7,000 lbs  onto/into tactical aircraft.

 F-18 (Aviation Ground Support Equipment)

MUNITIONS HANDLING AND LOADING UNIT (MHU-83D/E Bomb Loader)

OPERATIONAL STATUS: Qualification tested per USAF specification MIL-T-38646 REV. C Certified for handling nuclear weapons in accordance with requirements of USAF Weapons Laboratory, Kirtland AFB, NM, and USAF/LG – Airforce Manual 91-118 Safety design and Evaluation Criteria for Nuclear Weapons Systems.

F-18 (Aviation Ground Support Equipment)

ASLT

MJ-1C (2)

P/N 8141050-70 (NSN 1730-01-491-1557)

 F-18 (Aviation Ground Support Equipment)

APPLICATION

Standard equipment for loading/unloading & transporting of aerial stores including munitions, fuel tanks, pylons, special weapons, & SAR pack weighing up to 3,000 pounds onto/into tactical aircraft.

 F-18 (Aviation Ground Support Equipment)

AERIAL STORES LIFT TRUCK (MJ-1C BOMB LOADERS)

OPERATIONAL STATUS: Environmental tested per MIL-E-4970 (-65oF to 160oF). Qualification tested to insure compliance with the MJ-1A test requirements. Certified for handling nuclear weapons in accordance with requirements of USAF Weapons Laboratory, Kirtland AFB, NM. EMI tested and qualified for Radiated Emissions (RE102), and Radiated Susceptibility (RS103) per MIL-STD-461D and MIL-STD-462D. CE certified per European Machinery Directives and Standards of EN60204-1:1997. Engine exhaust emission is certified to TIER 2 of European Emission Standards. Noise emission is limited to less than 80dBA at one meter distance of the unit or operator station per latest issue of ISO 3744.

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LALS

AE32K

 F-18 (Aviation Ground Support Equipment)

LINKLESS AMMUNIION LOADING SYSTEMS (LALS)

 A/E32K-7 (P/N 3141AS799-1) consisting of :

1) Ammunition Loader GFK-21/E32K-7 (P/N 3141AS798-1)

and

2) Ammunition Replenisher: GFK-20/E32K-7 (P/N 3141AS500-1)

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SUMMARY OF HII RECENT MILITARY GSE DESIGN AND DEVELOPMENTS

LALS is the next generation and latest development in ground support equipment for storing,

transporting and loading 20mm rounds into the Navy aircraft gun system while downloading and

restoring empty cases and unfired rounds. The ammunition loader interfaces with the F- 14A, B and

D, F/A 18A, C, and D aircraft M61A1 gun system.

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                                                                                             GFU-24AE

SUMMARY OF HII RECENT MILITARY GSE DESIGN AND DEVELOPMENTS

GFU-24A/E32K-7 (P/N: 3305AS1400-1) is a cross-platform,

service, mobile ammunition transfer system for loading and

unloading 20mm ammunition from the ALS, UALS, LALS II,

or LALS 3 Linkless Ammunition Loading Systems. Capable of

being crank or pneumatically with an air ratchet, the 7 can load

new 20mm ammunition into the LALS while simultaneously

downloading unexpected ammunition into the spent casings.

The unexpended ammunition is unloaded into a tray for returning to bulk ammunition storage containers while spent casings are dropped out of the system into bulk cans below the Unit. The removable frame assembly can be removed for deployments where the entire structure is not required and can be mounted on the aft of the USN/USMC LALS II with included arm sections. The GFU-24A/E32K-7 incorporates an auto-detection system that automatically stops the system is an empty space occurs during loading. The system can also be operated in forward and reverse direction when cycling the system and not loading.

F-18 (Aviation Ground Support Equipment)

CLTS

                         AFM32

 

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

3

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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UHTS (3)
F-18 (Aviation Ground Support Equipment)
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          F18 including T-50, F-4, F-5, F-16, 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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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.
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UHTS (F16)
UNIVERSAL HYDRAULIC TEST STAND (UHTS)
Electric Motor Driven,
Dual Independent System
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101198-100 (2)
4920
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P/N: 101198-100,
NSN: 4920-01-591-9361RN
Model: A/M27T-16
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Model: A/M27T-16 replace MK-3A & 040499-100
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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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F-18 (Aviation Ground Support Equipment)
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                                                             UHTS F16 Diesel
UNIVERSAL HYDRAULIC TEST STAND (UHTS)
Diesel Engine Driven,
Dual Independent Systems
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101197-100 (2)
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
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Model: A/M27T-17 replacing MJ-2A and 040489-100
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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

F-18 (Aviation Ground Support Equipment)

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.

New
 F-18 (Aviation 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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PHTS R

F-18 (Aviation Ground Support Equipment)

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Portable Hydraulic Power Supply

F-18 (Aviation Ground Support Equipment)

PORTABLE HYDRAULIC POWER SUPPLY

Diesel Engine Driven

040489

Qualified to High Impact Shock Test (MIL-STD-901D)

P/N: 040489-100 

Test Medium:  Hydraulic fluid, MIL-H-83282, MIL-H-5606, or as specified by customer when ordering.

Flow Rate Capacity: 32 GPM at 3000 PSI, 22 GPM at 5000 PSI

Electric Motor Driven

040499

Qualified to High Impact Shock Test (MIL-STD-901D)

P/N: 040499-100 

Test Medium: Hydraulic fluid, MIL-H-83282, MIL-H-5606, or as specified by customer when ordering.

Flow rate Capacity: 40 GPM at 3000 PSI, 25 GPM at 5000 PSI

 F-18 (Aviation Ground Support Equipment)

 F-18 (Aviation Ground Support Equipment)

Hydraulic Testing on F-18 being carried out by 040489-100

Hydraulics International, Inc. (HII) is under Contract in the United States to build these new Units (P/N: 040489-100 & 040499-100) with more modern, reliable, maintainable and supportability for replacing all their existing old Units of different models. These new Units can be used to support military or civil helicopters based ashore or afloat including supporting intermediate activities at the flight line or in hangars, at air stations and air capable ships. These new Units are designed to troubleshoot and functionally check helicopter or any aircraft hydraulic systems. Besides having incorporated the latest state of the art innovations, these Units also come with a much higher capacity (flow rate & pressure).  These Units come with NATO or National Stock Numbers and are fully provisioned for spare and replacement parts for more than 20 years. Although specifically designed and built for supporting all military helicopter including those built by other Countries, these Units can also support fixed wing military aircraft including narrow body aircraft such as Boeing B737, B757, AIRBUS A318, A319, A300, A310, A320, A321,  C919,   ARJ21, M700, ERJ145, SAAB340, ATR72, Superjet 100, BAE146, F28, Falcon Jets,  KAI T-50 Golden Eagle etc or as long as the capacity of the hydraulic system is within the range of test stand flow and pressure.

These Units are designed and built for connecting to US Navy Standard Hydraulic Fluid Purifiers (P/N: 040505-100) to provide removal of hydraulic fluid particulates, water, chlorinated solvents, absorbed air & gases, which is common problem with aircraft.

F-18 (Aviation Ground Support Equipment)

PHTS R

       F-18  including F-4, F-5, F-16, C-130, MiG29, Su-30, F-2A, F-2B, F-CK-1, Rafael, Gripen, Hawk, Eurofighter, Transport Aircraft & Helicopter etc
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F-18 (Aviation Ground Support Equipment)
PORATBLE HYDRAULIC TEST STAND
Electric Motor Driven,
Dual Independent System
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MK-3A
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NSN: 4920-00-528-8780
and
4920-00-045-7543 (MK-3A)
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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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MK3A is 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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MJ2A
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PORATBLE HYDRAULIC TEST STAND
Diesel Engine Driven,
Dual Independent Systems
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2000 units sold
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MJ-2A
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P/N 070515-100 (MJ2A)
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Test Medium: Hydraulic fluid:
L-H-5606,
MIL-H-83282
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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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F-18 (Aviation Ground Support Equipment)

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.

2

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.

4

Test Medium

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

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

5

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

6

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

7

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.

9

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.

10

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.

11

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.

13

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.

14

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.

15

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.

17

Wet Weight

6,3000 Lbs

7,800 Lbs

All stated Specifications are subject to change

F-18 (Aviation Ground Support Equipment)
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US Navy HPS

040505

P/N: 040505-100 * NSN: 4920-01-523-0592 

A/M37M-11 (US Navy Standard Hydraulic Fluid Purifiers)

connected to either MK-3A or MJ-2A or 040499-100 or 040489-100

Navy Purifier 040505-100

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P/N: 040505-100, NSN: 4920-01-0592

removes:

1) 100% free water .

2) Dissolved water to less than 100 ppm .

3) 100% entrained gases .

4) 98% of dissolved gases

5) Particulate contamination to produce a cleanliness level of NAS1638, Class 2.

Dual Power Driven:

Diesel Engine Driven

or

Power Supply (3 Phase 115 VAC) can be provided by 040489-100 or 040499-100 .

Towable at 20 mph max. over improved roads.

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