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HT-F-30

Product catalog summary

Overview: The HYCOM HT engine-driven mobile hydraulic test stand is designed for aircraft maintenance, specifically for tasks related to AMM/ATA Chapter 29. It is ideal for filling, draining, and flushing aircraft hydraulic systems to meet NAS1638 Class 6 standards or better.

Model Specifications: The test stand is available in two models: HTM and HTC, with a flow range of 0-30 USGPM. It can be configured as a single system (S) or a dual system (S2), with the latter featuring two pressure and two return lines.

Key Features:

Axial piston pump with variable stroke and proportional control.
Stainless steel reservoir with a 240-liter capacity.
Large fuel tank for up to 8 hours of operation.
Oil-air cooler suitable for tropical conditions.
Operator panel with digital display for maintenance and failure notifications.
PLC system control with safety devices and switches.
Weatherproof operator panel cover and steel canopy.
Maximum towing speed of 16 km/h with parking brake on front wheels.

Technical Data:

Hydraulic hoses: 9 meters for single system, 12 meters for dual system.
Noise level: Less than 85 dBA at 2 meters.
Fluid compatibility: Mineral-based and phosphate ester-based fluids.
Pressure range: 300-3000 psi at 30 USGPM, 4000 psi at reduced flow.
High and low-pressure filters with electric clogging indicators.
Engine: Deutz 4-stroke Tier II, 52 kW at 2200 rpm.

Dimensions & Weight:

Length: 2870 mm
Width: 1650 mm
Height: 1650 mm
Weight: Approximately 2100 kg

Optional Features: Options include quick disconnect couplings, high accuracy flowmeter, integrated purifier, particle counter, water sensor, and emission standard diesel engine Stage V / Tier IV Final.

Contact Information: HYCOM B.V., P.O. Box 1079, 7301 BH Apeldoorn, Antillen 43, 7333 PE Apeldoorn. Phone: +31 88 0597 200, Email: [email protected], Website: www.hycom.nl

Catalog excerpts

HYCOM DATASHEET MOBILE HYDRAULIC TEST STAND FOR AIRCRAFT MAINTENANCE MODEL HT engine driven MAINTENANCE AND OVERHAUL CHECKS OF AMM / ATA CHAPTER 29 FILLING AND DRAINING OF AIRCRAFT RESERVOIR FLUSHING OF AIRCRAFT HYDRAULIC SYSTEM TO CLASS 6 NAS1638 OR BETTER HYDRAULIC SUPPLY FOR RAT TESTS WITH HYCOM GROUND CHECK MOTOR FLOW RANGE OUTPUT = S : SINGLE SYSTEM = S2 :

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FEATURES • Single system (S): one pressure and one return line or • Dual system (S2): single system with two pressure and two return lines with shutoff valves • • • • • Axial piston pump variable stroke with proportional control of flow and pressure Boost pump for closed loop circuit Stainless steel reservoir of 240 liter with drain valve and filling cap Large fuel tank for 8 hours operation Fluid contamination level NAS 1638 class 6 or better Oil-air cooler with low noise level suitable for tropical conditions Open loop configuration for filling and draining of A/C reservoir Temperature and...

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OPERATOR PANEL A Digital display with failure and maintenance notifications B Digital readout of acutal flow C High and return pressure gauges

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TECHNICAL DATA GENERAL Hydraulic hoses – single system Hydraulic hoses – dual system Noise level 9 meter 12 meter less than 85 dbA at 2 meters distance HYDRAULIC Fluid HTM Fluid HTC Mineral based e.g. MIL-H-5606, MIL-H-83282 or MIL-H-87257 Phosphate ester based e.g. Skydrol or Hyjet 300-3000 psi at 30 USGPM, 4000psi at reduced flow High (3 micron) and low pressure (10 micron) filters with electric clogging indicators MEASUREMENT High pressure gauge 0-5000 psi Accuracy 1% of full scale Return pressure gauge 0-200 psi Accuracy 1% of full scale Digital readout of actual flow Accuracy of < 2% of...

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DIMENSIONS & WEIGHT Quick disconnect couplings to connect hoses to the aircraft High accuracy flowmeter, 0,3% of actual value PUR = Integrated purifier for filtering, degassing and dewatering PC = Particle counter and water sensor Emission standard diesel engine Stage V / Tier IV Final Other options and accessories are available upon request.

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