T-52 LONG RANGE AUXILIARY FUEL SYSTEM All new Engineering for MD369 and 500/500N/600/600N/Explorer Helicopters Aux. Fuel Systems Specifications Capacity: 52 U.S. Gallons Weight: 93Lbs (42kg.) Shipping Weight: 213 Lbs. (97kg.) Fuel Pump: Twin Electrical V NE Reduction: None Approved On: All MD 500 and 500N, 369, series helicopters FAA STC SH667NW DO YOU HAVE A SPECIFIC APPLICATION HELICOPTER OR SIZE OR VOLUME? We Can Design and Build to Prototype CONTACT US Benefits One to Two Hour Extended Range Upgraded Composite Materials Dual Pumps for Backup Modern Control Panel Custom Seat Cushions- Molded Seat T-52 LONG RANGE AUXILIARY FUEL SYSTEM has been in service for thirty years. It has a protective, strong, stress resistant casing and F.A.A. quality approved components. These units are literally crafted to completion and rigidly inspected for long life and complete safety. A quality product from Tower Aerospace Inc., Nelson, British Columbia, Canada. Tank 52 U.S. Gallons Double Shell Composite Construction Doubles as Rear Passenger Seat External Fill Located Above Existing Filler Well Internally Baffled to Prevent Sloshing and Increase Strength Twin Fuel Pumps Provide 25 GPH Individually – 50 GPH Combined External Pre-Flight Drain Pumps Twin pumps are provided which individually pump at approximately 30 GPH – together 60 GPH enabling any combination of transfer required. Installation Initial Installation 8 Hours Subsequent Installations 1 Hour Installation Kit Contains All Required Hardware, Including a State of the Art Digital Control Panel and Fuel Indication Permanent Hardware Kit Available to Enable One Tank Unit to Service Several Helicopters Pre-Flight Drain Independent pre-flight drain to assure no contaminants enter primary tank, to be checked prior to each flight. Plumbing Outlet is plumbed directly to the filler of the main tank. Accessibility System is designed to allow any normal maintenance -100 hr. and 300hr. inspections without removal of tank. Ease of fuel pump system maintenance and inspection is accomplished by an access panel in the side of the tank. Fuel system does not need to be drained to change the pumps. Electrical Console located switch box is provided complete with push to start/stop switches, circuit breaker, fuel quantity gauge, and power lights. Vent All vent and drain lines double-jacketed. Any overfill spills go outside of fuselage. Testing FAA Drop Tower Tested In Four Positions Expansion Space, Sump Space, Flow Rates and Vent System Tested From 20,000 Ft in Maximum Auto-rotation Pressure Tested Immersion Tested Fluid Volume Tested Electrical Operating and Measuring Systems Tested Optional Equipment Custom seat cushions to match interiors or custom made interiors Documentation Each System Ships With A Comprehensive Owners Manual Containing the Following Documents: Installation Drawings Installation Instructions Operating Instructions Maintenance Instructions FAA STC Approved Flight Manual Supplement Weight And Balance Data Parts List 12 Month Warranty All Field Consultation, Inspections Requested “On Site”, and Engineering Advice, is Ongoing Support, Free of Charge SYSTEM BENEFITS EXTENDED POLICE, SEARCH AND RESCUE EXTENDED ENVIRONMENTAL MISSIONS EXTENDED FIRE PATROL EXTENDED HYDRO, GAS AND OIL MISSIONS HIGHER REVENUE BEARING HOURS DO YOU HAVE A SPECIFIC APPLICATION, HELICOPTER OR SIZE OR VOLUME? We Can Design and Build to Prototype CONTACT US
