SECTION 7
GROUND HANDLING & SERVICE
7 Introduction
This section contains factory-recommended procedures for proper ground handling and routine care and servicing. It also
identifies certain inspection and maintenance requirements, which must be followed if the aircraft is to retain its new-plane
performance and dependability. It is recommended to follow a planned schedule of lubrication and preventive maintenance
based on climatic and flying conditions encountered locally.
7.1 Aircraft Inspection Periods
Inspection intervals occur at 100 hours and in accordance with special inspection schedules, which are added to regularly,
scheduled inspections. Correct maintenance procedures are described in the aircraft’s Service Manual or in the engine’s
Line Maintenance Manual.
7.2 Aircraft Alterations or Repairs
For repairs, refer to aircraft’s Line Maintenance Manual.
7.3 Ground Handling
7.3.1 Towing
The use of a towbar is recommended. But, pulling on the propeller near the axle you can safely maneuver the aircraft.
Aircraft may be steered by turning rudder or, for steep turns, by pushing lightly on tailcone to lift nose wheel.
7.3.2 Parking and Tiedown
When parking airplane outdoors, head it into the wind and set the parking brake. It is preferable to use chocks if available.
Tie the airplane down in severe weather and high wind conditions. Tie-down ropes shall be fastened to the wing
attachments and anchoring shall be provided by ramp tie-downs. Nose gear fork can be used for front tie-down location or
the tail can be tied down with the optional Tiedown point.
Secure the flight controls to avoid possible weathervane damage to moving surfaces. Seatbelts may be used to latch control
stick to prevent its movement.
7.3.3 Jacking
Given the light empty weight of the aircraft, lifting one of the main wheels can easily be accomplished even without the use
of hydraulic jacks. For an acceptable procedure please refer to the Line Maintenance Manual.
7.3.4 Leveling
Aircraft leveling may become necessary to check wing incidence, dihedral or the exact location of CG. Longitudinal
leveling verification is obtained by placing a level longitudinally, over the aft part of the cabin floor (just in front of the
seat). See maintenance manual for instructions.
To Next Page
Loading...
