<!-- /* Style Definitions */ p.MsoNormal, li.MsoNormal, div.MsoNormal {mso-style-parent:""; margin:0cm; margin-bottom:.0001pt; mso-pagination:widow-orphan; font-size:12.0pt; font-family:"Times New Roman"; mso-fareast-font-family:"Times New Roman";} @page Section1 {size:612.0pt 792.0pt; margin:72.0pt 90.0pt 72.0pt 90.0pt; mso-header-margin:36.0pt; mso-footer-margin:36.0pt; mso-paper-source:0;} div.Section1 {page:Section1;} -->

== OUT OF PRODUCTION FROM 30/MAY/2008 ==

• airplane weights at 992lb,
• standard atmospheric condition level,
• hard surface,
• dry runways and no wind.

P96-GOLF STANDARD EQUIPMENT

FLIGHT INSTRUMENTS and INDICATORS
- MAGNETIC COMPASS
- AIRSPEED IND., Kts
- ALTIMETER (IN)
- 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 (Electric actuated from Stick)
- 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 92 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
- ALL WINDOWS TINTED
- TIE DOWN RINGS
- MAIN WHEELS, 5,00 X 5
- NOSE WHEEL, 4,00 X 6
- WHEEL PANTS

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