![]() ![]() ![]() Lampa
Holdings Email:
|
DESCRIPTION of THE NANCHANG CJ-6 The engine is a 285HP normally aspirated Housai HS-6A nine cylinder 10 litre radial driving a J9-G1 two bladed all metal constant speed propeller. Engine life is 600 hours TBO. Under present rules extended operation is available “on condition”. Engine overhaul in Australia is not economical at present as zero time overhauled engines are available ex China at a lower cost that overhauling an engine. Engine starting, gear retraction, flap actuation and brakes are all driven by a high-pressure air system from an on-board main air reservoir. An engine driven air pump replenishes the main air tank and an emergency air tank provides back-up air for gear extension in case of a failure of the main air system. In case of loss of pressure during the starting sequence the main air reservoir can be replenished from an external air source. If such a supply of air is unavailable the engine is capable of being hand started by swinging the prop. Braking is via a combination of actuation of a handbrake in the control columns and rudder deflection. This arrangement deflects more or less air to the individual wheel brake that allows the castoring nose wheel to turn in the required direction. Both cockpits are normally fully instrumented for night and IFR flying although the aircraft’s Australian LIMITED category Certificate of Airworthiness limits operations to day VFR. Standard instrumentation includes electrically driven non-toppling AH, DG slaved from a gyro compass, ADF, engine instrumentation, gear retracted/down lights and manual indicators and very accurate fuel indicators in each tank driving a common gauge via a selector. |
|
|
Fuel capacity is 155 litres held in two wing tanks, one in each wing draining to a central sump before being pumped to the engine. There is no fuel selection valve; both tanks are selected ON when both of the firewall shutoff valves are open. Electrical system is 24 volt and the battery is charged via an engine driven generator. The front cockpit is fitted with a a combined ammeter and voltage indicator as well as charge indicator light. Where 12V avionics are fitted locally a 24 to 12 voltage reducer is installed as part of the avionics package. Avionics
are a combination of original equipment and locally installed. A VHF radio
with side tone intercom, transponder with mode C is installed here as
part of the “Westernisation” process. The throttles in each
cockpit are fitted with individual “press to talk” and “press
to transmit” switches. The Chinese valve powered ADF, operable from
either cockpit, is usually retained as it has proven to provide excellent
indication. |
||
Site
Designed and Maintained by Bizwiz
Australia 2009 |