F-16 (Aviation Ground Support Equipment)

Hydraulics International (Asia) - (http://hiigroupasia.com/) Aircraft Ground Support Equipment (AGSE), Gas Boosters, Liquid Pumps & Flowmetrics Products (http://hiigroupasia.com/) F-16 (Aviation Ground Support Equipment)   * F-16 (Aviation Ground Support Equipment) . Noise emission is limited to less than 85dBA at one meter distance of the unit or operator station per latest issue of ISO 3744. pylons. CE certified per European Machinery Directives and Standards of EN60204-1:1997. Engine exhaust emission is certified to TIER 2 of European Emission Standards. NM. & SAR packs weighing up to  7. fuel tanks.000 lbs  onto/into tactical aircraft.                                                                                    *    P/N 971480-30 (NSN 1730-01-446-2422) APPLICATION Standard equipment for loading/unloading & transporting of aerial stores including munitions. MUNITIONS HANDLING AND LOADING UNIT (MHU-83D/E Bomb Loader) OPERATIONAL STATUS: Qualification tested per USAF specification MIL-T-38646 REV.com/aircraft-bomb-loaders-aerial-munitions-lift-trucks/)               P/N 8141050-70 (NSN 1730-01-491-1557) APPLICATION (Model: MJ-1C) . Kirtland AFB. EMI tested and qualified for Radiated Emissions (RE102). C Certified for handling nuclear weapons in accordance with requirements of USAF Weapons Laboratory. special weapons. (http://hiigroupasia. and Radiated Susceptibility (RS103) per MIL-STD-461D and MIL- STD-462D. and USAF/LG – Airforce Manual 91-118 Safety design and Evaluation Criteria for Nuclear Weapons Systems.  special weapons. Standard equipment for loading/unloading & transporting of aerial stores including munitions. transporting    and loading 20mm rounds into the Air Force aircraft gun     system while downloading and restoring empty cases and unfired rounds. AERIAL STORES LIFT TRUCK (MJ-1C BOMB LOADERS) OPERATIONAL STATUS: Environmental tested per MIL-E-4970 (-65oF to 160oF). NM. . Qualification tested to insure compliance with the MJ-1A test requirements. * LINKLESS AMMUNTIONS LOADING SYSTEMS (LALS) P/N: 029999-3 (NSN: 1730‐01‐504‐6347) LALS is the next generation and latest development  in ground support equipment for storing. EMI tested and qualified for Radiated Emissions (RE102). LALS II. & SAR pack weighing up to 3. and Radiated Susceptibility (RS103) per MIL-STD-461D and MIL-STD-462D. fuel tanks.000 pounds onto/into tactical aircraft. pylons. Noise emission is limited to less than 80dBA at one meter distance of the unit or operator station per latest issue of ISO 3744. CE certified per European Machinery Directives and Standards of EN60204-1:1997. service. Kirtland AFB. mobile ammunition transfer system for loading and unloading 20mm ammunition from the ALS. Engine exhaust emission is certified to TIER 2 of European Emission Standards. UALS. Certified for handling nuclear weapons in accordance with requirements of USAF Weapons Laboratory. F-16 or F-22 aircraft M61A 1 gun system. *                                                                                       GFU-24A/E32K-7 (P/N: 3305AS1400-1) is a cross-platform. The ammunition loader interfaces with the F-15. C-5. NSN: 4920-01-381-4950 (http://hiigroupasia. or LALS 3 Linkless Ammunition Loading Systems. 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. C-17. Capable of being crank or pneumatically with an air ratchet. Eurofighter. F-18. Su-30. USMC. F-CK-1. USN. The system can also be operated in forward and reverse direction when cycling the system and not loading.com/aircraft-cabin-pressurization-leakage-tester/) (http://hiigroupasia. P/N: 96384-100. 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. Transport Aircraft & Helicopter etc * . C-130.com/aircraft-cabin-pressurization-leakage-tester/) Flow  400 SCFM Diesel Engine Drive (AF/M32T-1. Rafael. P/N: 78011-100. NSN: 4920-01-435-8545) * *      F-16 including T-50.com/aircraft-cabin-pressurization-leakage-tester/)    Flow  400 SCFM      Electric Motor Driven (AF/M24T-3. The GFU-24A/E32K-7 incorporates an auto-detection system that automatically stops the system is an empty space occurs during loading. P/N: 93038-100. the 7 can load new 20mm ammunition into the LALS while simultaneously downloading unexpected ammunition into the spent casings. * (http://hiigroupasia.com/aircraft-cabin-pressurization-leakage-tester/) CABIN PRESSURIZATION AND LEAKAGE TESTER Qualified and in-service with the USAF. Hawk. F-5. F-2A. Gripen. (http://hiigroupasia. NSN: 4920-01-063-0120)   Electric Motor Driven (AF/M24T-3. MiG29. Services all rotary and fixed wing military and commercial aircraft. A400M. F-2B. F-4. NSN: 4920-01-591-9361RN * Model: A/M27T-16 replacing MK3A * Test Medium: Hydraulic fluid: MIL-PRF-83282. 64   GPM at 5000 PSI Or   combined * UHTS comes with an integral   built Hydraulic Purification System (HPS) that provides continuous cooling.   chlorinated solvents. 32   GPM at 5000 PSI per system Two System: 106   GPM at 3000 PSI.             UNIVERSAL HYDRAULIC TEST STAND (UHTS) Electric Motor Driven. Puri cation   Performance 1)  Contaminant  removal: 55 gallon of hydraulic fluid in 5 hours. HII ‘s new generation of Universal Hydraulic Test Stand (UHTS) with the latest state-of-the-art features and components. 3)  Chlorinated  solvents:  From 400 to less than 100 PPM. water.   Keeping hydraulic fluid clean and eliminates the need of changing     hydraulic fluid for a long period of time. Dual Independent System * Model: A/M27T-16 * * P/N: 101198-100. 40   GPM at 4000 PSI. *                                                                          UNIVERSAL HYDRAULIC TEST STAND (UHTS) Diesel Engine Driven. reduce deployment foot print and sharply   reduce   hydraulic maintenance and associated costs. 80   GPM at 4000 PSI. Dual Independent Systems * Model: A/M27T-17 * * P/N: 101197-100. HII is currently on Contract with USAF to build UHTS. 2)  Water:  From   1000 to less than 200 PPM. 98% (by   volume) removal. MIL-PRF-5606 and MIL-PRF-87257 * * Flow Rate Capacity: One System: 53   GPM at 3000 PSI.  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. absorbed air & gases removal from hydraulic fluid. 5)  Particulate:   Cleanliness level equal to or better than   NAS 1638 class 3. UHTS utilizes a high resolution LCD Display HMI (Human Machine Interface)  with resistive touch screen for operation and monitoring of UHTS System and functions.   filtering moisture and to remove hydraulic fluid particulates. minimize hazardous   waste disposal needs. HPS work in a very   cost-effective way to minimize hydraulic fluid usage. NSN: 4920-01-592-0750RN * Model: A/M27T-17 replacing MJ-2A * Test Medium: Hydraulic fluid: . 4)  Air & Gas: 100% dissolved air removal. Puri cation Performance 1)   Contaminant   removal: 55 gallon of hydraulic fluid in 5 hours.  IVS is certified and traceable to NIST. 64   GPM at 5000 PSI Or   combined * UHTS comes with an integral   built Hydraulic Purification System (HPS) that provides continuous cooling. 3)  Chlorinated   solvents:  From 400 to less than 100 PPM. 80   GPM at 4000 PSI. HPS work in a very   cost-effective way to minimize hydraulic fluid usage.   filtering moisture and to remove hydraulic fluid particulates.   chlorinated solvents. 4)  Air   & Gas: 100% dissolved air removal.  IVS can be connected directly  to UHTS to verify that Transducers & Flowmeters are within acceptable accuracy. * * .com/instrument-verification-set-ivs/) 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.   Keeping hydraulic fluid clean and eliminates the need of changing     hydraulic fluid for a long period of time. MIL-PRF-5606. 2) Water: From   1000 to less than 200 PPM. 32   GPM at 5000 PSI per system Two System: 106   GPM at 3000 PSI. 5)  Particulate:  Cleanliness level equal to or better than   NAS 1638 class 3. All readings on UHTS are shown on high resolution LCD Display & Engine Performance Module. * (http://hiigroupasia. MIL-PRF-83282.  NO GAUGES including Transducers or Flowmeters are required to be removed for calibration. 40   GPM at 4000 PSI. MIL-PRF-87257 * * Flow Rate Capacity: One System: 53   GPM at 3000 PSI. 98% (by   volume) removal. reduce deployment foot print and sharply   reduce   hydraulic maintenance and associated costs. absorbed air & gases removal from hydraulic fluid. water. minimize hazardous   waste disposal needs. 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 * * * * PORATBLE HYDRAULIC TEST STAND * Diesel Engine Driven. or as specified by customer when ordering. MiG29. F-18. Su-30. Rafael. C-17. Dual Independent Systems * * P/N 070515-100 (MJ2A) * (https://i0. UHTS (Model: A/M27T-17. F-2B. Skydrol 500 A and B. F-CK-1.wp. F-5. Dual Independent System * * NSN: 4920-00-528-8780 & 4920-00-045-7543 (MK-3A) * MK-3A being replaced by UHTS * Test Medium: Hydraulic fluid: MIL-H-5606. Eurofighter. F-2A. Hawk.com/hiigroupasia.gif) * . Gripen. * * * *         F-16 including F-4. NSN: 4920-01-592-0750RN) undergoing vigorous testing (June 2012) at HII facility. C-5. * * Flow Rate Capacity: One System: 35   GPM at 3000 PSI. Transport Aircraft & Helicopter etc * * PORATBLE HYDRAULIC TEST STAND * Electric Motor Driven. C-130. MIL-H-83282.com/wp- content/uploads/2013/11/2000-units-sold. absorbed air & gases from aircraft hydraulic fluid as   well as test stand. (See attached article from USAF. UHTS has also been qualified to the 1 Design of major   component are most rigorous military   requirement testings such as environmental. Electro Magnetic Interference.   Mobility. obsolete.   chlorinated solvents. This purification process eliminates the need of changing   hydraulic fluid for a long period of time. number art features   and components. etc. System (HPS) 1)       Contaminant removal: 55 gallons of hydraulic fluid in 5   hrs. UHTS comes with an AF qualified integral   built Hydraulic Purification System (HPS) that provides continuous cooling. which is self-explanatory. MIL-H-83282Skydrol 500 A and B. reduce deployment foot print and   sharply reduce aircraft hydraulic components maintenance and associated   costs. Test Medium: Hydraulic fluid: MIL-H-5606.) Hydraulic Purification Puri cation   Performance 3 Using normal Filter Elements. 98% (by   volume) removal 5)       Particulate: Cleanliness level equal to or better than   NAS 1638 class 3. water. 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. HPS works   in a very cost effective way to minimize aircraft hydraulic fluid usage. Reliability.   filtering to remove hydraulic fluid particulates. 30 GPM (15 GPM/system at 5000 PSI) Or  combined * * COMPARISON (MJ-2A vs UHTS)   ITEM SPECIFICATIONS MJ-2A UHTS   New   generation of Hydraulic Test stands with the latest state-of-the- 30 years old Technology. or as specified by customer when ordering. aircraft.   . Accepted in-service by USAF for Accepted in-service by USAF for supporting   their F-16 and can be 2 Aircraft Application their F-16   and some designated used to support any transport or fighter aircraft in   their inventory.        * MJ2A is OBSOLETE and replaced by UHTS        * Flow Rate Capacity: One System: 35   GPM at 3000 PSI. Maintainability.   minimize hazardous waste disposal needs. 15 GPM at 5000 PSI Two System: 70 GPM (35 GPM/system at 3000 PSI). Diesel Engine. naturally Diesel Engine. Hydraulic   fluid. Multi Fuel. MIL-H-5606. MIL-PRF-83282. turbo-turbo charged.7 is an electronic fuel and Governor Engine Diagnostic 10 No controlled via Electronic   Control Module (ECM) and full diagnostic System control feature facilitating safety   and troubleshooting features. 11 Fuel tank capacity 42 US gallons 60 US   gallon . 9 Drive Unit aspirated. MIL-PRF-5606. moisture and air to enter hydraulic   fluid. 210 HP. maintaining vented to atmosphere and fluid is purity of hydraulic fluid all the time. Gallon capacity Is completely sealed to atmosphere. Hydraulic   fluid. subject   to ambient   Combination of manual and automated   controls.S.   EPA certified to TIER III. Gallon capacity 60 U.S. Troubleshooting and ease of Calibration.   non-EPA certified. Built-in Test   System and Human Control Panel Instrumentation Machine Interface Touch Screen Operator Panel enabling ease   of Operator Operation. 4 Test Medium MIL-H-83282 One system One system 53   GPM at 3000 PSI 35   GPM at 3000 PSI 40   GPM at 4000 PSI 15 GPM at 5000 PSI 32   GPM at 5000 PSI per system Two system Two system Flow Rate Capacity 5 70 GPM (35 GPM/system   at 106   GPM at 3000 PSI 3000 PSI) 80   GPM at 4000 PSI 30   GPM (15 GPM/system at 5000 PSI) 64   GPM at 5000 PSI or   combined Or   combined   Ambient Temperature Range Ambient Temperature Range -40ºF to +125ºF -40ºF to +125ºF Operating Conditions Altitude:     Sea level to 6000 feet Altitude:     Sea level to 7000 feet 6 Relative Humidity:   0% to 100% Relative Humidity:   0% to 100% Test Stand Position:   Up to 8 1/2° Test Stand Position:    Up to 8 1/2° from horizontal from horizontal 90 U. 300 HP. obsolete Cummins   engine QSB6. Fully military 8 Conventional Control and Analog qualified with System Diagnostic. and MIL-PRF-87257. This   feature prevents airborne Hydraulic Reservoir 7 particulate. Any fault condition will be   permanently stored to retentive memory of HMI computer. * 3) 100% entrained gases . * 2) Dissolved water to less than 100  ppm . All Instruments require removal UHTS is set-up with Instruments capability to be verified by an   Instrument and   verified calibration by third inexpensive Instrument Verification Set (IVS) within 15 minutes 14 Calibration/Verification party. Back Pressure Regulator allows operation in both aircraft   (Closed Back Pressure 13 No Loop) or test Stand Reservoir (Open Loop) operation with pressurized   Regulator or non-pressurized aircraft reservoir systems. these results in equipment minimizing Equipment   downtime and cost. * 4) 98% of dissolved gases * 5) Particulate contamination to produce a cleanliness level of NAS Class 3. or to remove clean   No Purification Ports filtered hydraulic fluid from the Reservoir also External Purification Ports   allow purification of external fluid source.3000 Lbs 7. Fault diagnostics page provides   detail fault information and recommend corrective actions. fault conditions will immediately report to HMI   message field and warning horn is activated. 17 Wet Weight 6. Up to 200 fault   conditions can be stored in retentive memory 15 Fault Diagnostic System No If a critical fault occurs during system operation. If a fault exists before system operation or a fault occurs   during system operation. *   Towable at 20 mph max. downtime and   excessive cost. * Dual Power Driven: Diesel Engine Driven or operates on household power supply. engine will   be automatically shut down in 10 seconds. UHTS incorporates Invertor to provide 115 VAC. Single Phase   16 115 VAC Utility Power No Electrical Power for Utilities. * . Each fault condition has a   corresponding fault diagnostics page at HMI.800 Lbs All stated Specifications are subject to change. * * * * P/N: 100033-100 * NSN: 4330-01-587-5425 *  (US Air Force Standard Hydraulic Fluid Puri er) connected to either MK-3A or MJ-2A * Removes: * 1) 100% free water . External Reservoir Fill and Discharge Ports enables the Operator   to fill 12 External Fill and the Hydraulic Reservoir from an outside source. over improved roads. com/aircraft-fluid- dispensers-or-portable-fluid-servicing-units/)  Portable Hydraulic Fluid Servicing Unit. NSN: 3040-01-546-4126 .com/aircraft-fluid-dispensers-or-portable-fluid-servicing-units/) P/N: 061477-100. NSN: 3040-01-546-5962 (http://hiigroupasia. NSN: 3040-01-546-4129 (http://hiigroupasia.com/aircraft-fluid-dispensers-or-portable-fluid-servicing-units/) P/N: 061475-100.com/aircraft-fluid-dispensers-or-portable-fluid-servicing-units/) *  Portable Engine Oil Servicing Unit. PMU-74/E P/N: 061479-100.com/aircraft-fluid-dispensers-or-portable-fluid-servicing-units/) P/N: 061481-100.com/aircraft-fluid-dispensers-or-portable-fluid-servicing-units/) * Portable Rotor Fluid Servicing Unit. PMU-73/E (http://hiigroupasia. (http://hiigroupasia. PMU-71/E (http://hiigroupasia. PMU-72/E (http://hiigroupasia.com/aircraft-fluid-dispensers-or-portable-fluid-servicing-units/) * Portable Transmission Fluid Servicing Unit. NSN: 3040-01-546-4146   (http://hiigroupasia. All Rights Reserved HII GROUP ASIA Search for: Search HII GROUP ASIA CONTACTS (http://hiigroupasia. 0-3000 PSI Output Pressure. 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