P96-GOLF STANDARD EQUIPMENT

FLIGHT INSTRUMENTS and INDICATORS
MAGNETIC COMPASS
AIRSPEED IND., Km
ALTIMETER 
VERTICAL SPEED
BANK INDICATOR
FLAPS INDICATOR
PITOT SYSTEM
STATIC SYSTEM
STABILATOR TRIM POSITION INDICATOR

ENGINE INSTRUMENTS
TACHOMETER
HOUR RECORDER
OIL PRESS
OIL TEMP.
HEAD TEMP.
FUEL PRESS.
VOLTMETER
LH + RH FUEL QTY

FLIGHT CONTROLS
HYDRAULIC BRAKES
PARKING BRAKE
ELECTRICAL FLAPS
DUAL FLIGHT CONTROLS
STEERABLE NOSE WHEEL
STABILATOR TRIM (Between the seats)
ENGINE CONTROLS
--THROTTLE, TWO
--CHOKE
FLIGHT TRIM CONTROLS
--STABILATOR with INDICATOR
FUEL CONTROL SELECTOR WITH ON/OFF
PANEL SWITCHES:
--STARTER
--FUEL PUMP
--ENGINE LH and RH IGNITION SWITCHES

ELECTRICAL SYSTEM
12 VOLT 18A AMP. BATTERY
12 VOLT ALTERNATORS-20 AMP.
SWITCHES
--Landing Light
--Strobe Light
CIRCUIT FUSES PANEL

FUEL SYSTEM
TWO INTEGRAL FUEL TANKS WITH 70 LITRES
TOTAL CAPACITY
ENGINE DRIVEN FUEL PUMP
AUXILIARY FUEL PUMPS, ELECTRIC
FUEL QUICK DRAIN

INTERIOR
PILOT and COPILOT SEATS
--Adjustable Fore and Aft
SEAT BELTS & Shoulder Harness, All Seats
WALL TO WALL CARPETING
LUGGAGE COMPARTMENTS

EXTERIOR
EPOXY CORROSION PROOFING, All structure
SLIDING CANOPY with lock and key
REAR WINDOW
TIE DOWN RINGS
MAIN WHEELS, 5,00 X 5
NOSE WHEEL, 4,00 X 6

EXTERIOR LIGHTS
VERTICAL TAIL STROBE
TAXI LIGHT

CABIN CONFORT SYSTEM
VENTILATOR ADJUSTABLE, 2 place

POWERPLANT AND PROPELLER
ENGINES - 1 ROTAX 912ULS2 100 HP, 4 Cylinders
liquid/air cooled, integrated reduction gear
DUAL IGNITION SYSTEM
THROTTLE CONTROL LH/RH
TUBULAR STEEL ENGINE MOUNT
PROPELLER - GT Propeller, 2 Blade fix
PROPELLER SPINNER
AIR FILTER
OIL FILTER
OIL AND WATER COOLERS

PRODUCT SUPPORT/DOCUMENTS
MANUFACTURERS FULL TWO YEAR LIMITED WARRANTY
PILOTS OPERATION HANDBOOK
MAINTENANCE MANUAL