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Aircraft Tanker Aircraft Refueling Truck Aircraft Refueler TECHNICAL SCRUTINY REPORT (TSR) |
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NO |
PART NO |
INDENTED ITEM SPECS (BY USER) (T.O. REFERENCE) |
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AIRCRAFT REFUELLER (5,000 USG ) Air transportable internally by C-130 E Model Along with spare wheel, wheel brace, jack with handle and one set of complete tool kit and fire extinguisher:- |
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3 |
Engine |
No of Cylinders |
Diesel 6 cylinders water cooled & direct injection, OHV |
Mechanical drives between engine and pump. |
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4 |
Max Torque |
135 to 145 Kg at 1200 to 1400 RPM |
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5 |
Max Output |
340 to 360 PS at 2100 to 2200 RPM |
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6 |
Piston displacement |
11,000 cc to 11,300 cc |
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7 |
Transmission |
· 6 forward x I reverse speed · 6 x 4 Drive · Manual Transmission |
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8 |
Clutch |
Hydraulic control with air assisted dry single plate. |
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9 |
Dimensions |
Length |
10,000-11,000 mm |
Width |
2450-2550 mm |
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Height |
2550-2660 mm |
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Wheel Base |
5500-7000 mm |
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Grd Clearance |
270 to 300 mm |
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Weight empty |
12,800-14,000 Kg |
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Weight with load |
29,000-30,000 Kg |
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10 |
Colour |
Jungle Camouflage |
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11 |
Steering |
Right Hand Drive |
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Power Steering |
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12 |
Suspension |
Front |
Front semi elliptical steel leaf spring, hydraulic double acting telescopic shock absorbers. |
Rear |
Rear semi elliptical type steel leaf spring type. |
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13 |
Brakes |
Parking |
Hand operated hand brake for parking at rear 8 wheel |
Service |
Air pressure over hydraulic dual circuit on front and rear wheel. Automatic actuated braking system when the refueling is in operation |
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Auxiliary brakes |
Electro pneumatic control with better fly valve. |
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14 |
Electric System |
24 V system. |
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Batteries provided with housing and switch |
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Batteries cover made of fuel resistant material |
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Main battery shut off relay |
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Other standard electrical fitting to be provided (fire proof certificate for electrical wiring is to be provide by the firm). |
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15 |
Seating Capacity |
3 Persons in Front Cabin |
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16 |
Chassis |
Frame to be ladder type reinforced single channel equipped with hook on the front & rear frame |
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17 |
Axle |
Front |
· Reverse Elliot "T" / "I" beam type · Load capacity 6,500 to 8,000 Kg on road |
Rear |
· Two Axles · Single reduction banjo housing tandem type · Load capacity 22,500 to 24,000 Kg on road |
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18 |
Exhaust |
Horizontally mounted below front bumper with spark arrester. |
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19 |
Pump drive system |
T/M PTO Drive / Full power, Split Shaft PTO |
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Speed control gear box below chassis. |
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Control Provided at Control Panel as well as Cabin |
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20 |
Clamp Rings |
Suitable Qty of Clamp rings for shipment, located at appropriate locations |
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21 |
Cab |
All steel welded cab |
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Hydraulic tilt type |
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crew seats adjustable with shock absorber & coil spring |
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Windshield & windows with tinted glass3 |
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Center and Window side mirrors. |
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Good quality / durable up-holstry / cabin fittings |
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Fog light |
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22 |
Mudguards |
Built-in mudguards. |
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23 |
Spark Arrester |
Prevention from the spark. 1 unit to install in front of passenger side. |
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24 |
Control Board |
Control panel should be on the right side of vehicle |
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behind Driver cabin. |
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Provisioning of Roll up type shutter doors |
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Hand accelerator |
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Warning lights for fuel charging system |
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Pressure indicator for pump suction / delivery and refueling lines |
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Pump RPM digital indicator |
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Instruction plate (in English Language) |
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Control air pressure gauge. |
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Differential pressure gauges for filter / separator. |
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Reference pressure gauge for By pass valve. |
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Venturi pressure gauge (Fuelling pressure gauge). |
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Vacuum pressure gauge for defueling process |
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On-off switch for Dead Man System |
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Manual Deadman override switch |
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Main power switch |
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Emergency engine stop switch on control panel |
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Working Lamp switch |
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Deadman Lamp |
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Brake inter lock lamp |
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Pump speed control on control panel |
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Revolution counter on control panel |
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System flow diagram |
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25 |
Tank |
Capacity |
5000 US Gallons |
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Construction |
· Made of Aluminum Alloy as per International Aviation Standards (AW5454) · Material of the tank must be corrosion / oxidation free and resistant, and must comply with International Safety and Aviation Standards. · OEM to furnish complete details about tank material specs, its corrosion resistant properties, and International Aviation Standard to which material complies, in his technical quotes. Moreover, certificate to this effect be provided · Tank to be leak resistant and able to sustain jerks and jumps on rough track. · Tanks shape must be designed such that refueller is C-130 Aircraft transportable · Single compartment, provided on the inside with stress-resistant shell heads and anti-slashing baffles dividing tank into communicating compartments, such that all are accessible for cleaning / inspection. · Tank wall thickness is to be minimum 5 mm. · Baffle plates must be flushed with tank surface to ensure full drainage of fuel while defuelling operation |
Compartments |
All compartments assembled by welding of continuous bead type to the chassis |
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Man Holes |
· Qty Two (2) of 20" - 24" dia · Mounted to tank top side · Provided with covers, bolted to the man-hole collars · Fitted with fuel proof sealing · Provided with Vacuum pressure safety valve · Provided with one separate inlet for dip stick |
Tank Bottom |
· One stanch tape with hermetic seal cover fitted to the bottom of tank rear section and provided with automatic water drainage and one gate valve to drain the tank by hand. · The tank should be manufactured with a sloped channel forward to the water pump installed in the rear point of the tank bottom |
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Cat Walk |
· Non-skid type (Metallic Structure) · Running along the whole upper side of tank with safeguard |
Ladder |
One fixed ladder on rear of refueller for climbing up and down the catwalk way |
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Fuel System and Pump Compartment Doors |
· Large Size · Hinged type · Opening upwards / sideways · Provision of roll up type doors on both side of control panel |
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Hose Carriers |
· Qty Two for 3" hoses · Fitted on each side of the tank |
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Tank to |
· Inner piping with suction port |
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pumping station connection |
located in the lower part but above level of drainage sump. · One emergency valve on piping outlet to cut-off the tank from pumping stations. · Anti vibrating joints to damp possible vibration between the tank and the pump. |
Tank Vent Interlocking Device |
· Provided Air Vent valve at the top side of the tank. · Provided to prevent dispensing unless the vent is open. |
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Tank Level Gauge |
8" -10" Dia Aluminum Alloy, float type at the driver side of the tank |
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· Self-priming centrifugal pump with self-lubricating Anti-friction bearing |
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· With 6" and 4" delivery parts, capable to deliver the fuel by means of two reel hoses. |
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Type |
· Automatic Engine Speed Regulation for the pump |