Mahindra GIPPSAERO GA8-TC 320 - Amplified Procedures

CASA Approved
C01-01-08 5 Feb 2009 Page 4-9
Section 4
Model GA8-TC 320 Normal Procedures
4.3.11 Baulked Landing
Power .....................................................APPLY TAKE-OFF POWER - Monitor MAP and limit
power to 40 in Hg MAP / 2500 RPM below 5000 ft pressure
altitude and 38 in Hg MAP/ 2500 RPM above 5000 ft pressure
altitude
Wing Flaps .............................................RETRACT SLOWLY Approximately 3 sec per setting
Airspeed .................................................ESTABLISH NORMAL CLIMB SPEED
initially 71 KIAS
4.3.12 After Landing/Securing
Wing Flaps .............................................UP
Fuel Pump ..............................................OFF
Cowl Flap ...............................................OPEN
Parking Brake .........................................ON/AS REQUIRED
Radios and Electrical Equipment ...........OFF
Idle until there is a decided decrease in CHT, then:
Mixture ...................................................IDLE CUT OFF
Ignition ....................................................OFF
Master Switches Bus 1 and Bus 2 .........OFF
Controls ..................................................SECURE
4.4 AMPLIFIED PROCEDURES
This section is provided to supply the pilot with additional information concerning normal
procedures in general. Elaboration of the procedures specied in the NORMAL PROCEDURES
CHECK LISTS as well as the inclusion of some more generalised procedures that can be better
covered by a general descriptive procedure rather than a formal check list are included in this
section. This will give the pilot a more complete understanding of these procedures.
4.4.1 Preight Inspection
The Preight inspection as covered by the PREFLIGHT INSPECTION CHECKLIST is
recommended prior to the rst ight of the day. Inspection procedures for subsequent ights
can be abbreviated provided essential items such as fuel and oil quantities, security of fuel and
oil ller caps are satisfactory. After refuelling fuel samples must be taken from all drain points,
ve in total, one in each of the two wing fuel tanks and three under the fuselage below the right
side cockpit door.
Aircraft operated from rough strips, especially at high altitudes, are subject to abnormal landing
gear abuse. Frequent checks of all landing gear components, tyres and brakes is warranted in
these situations.
01 Aug 2011