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STAR MARIANAS AIR, INC. Approved Training Manual’s Lesson Plans And Courseware. Recurrent – Flight Crew Part III – Aircraft Ground Training Section 2 – Aircraft Systems. Before We Start. Complete Class Roster Cell Phones OFF. Aircraft Ground Training:.
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STAR MARIANAS AIR, INC. Approved Training Manual’s Lesson Plans And Courseware Recurrent – Flight Crew Part III – Aircraft Ground Training Section 2 – Aircraft Systems
Before We Start Complete Class Roster Cell Phones OFF
Aircraft Ground Training: Section 2 - Aircraft Systems
Training Materials Current copy of the General Operations Manual Aircraft flight Manual
A. Aircraft general B. Power plant C. Electrical D. Hydraulic E. Fuel F. Air Conditioning G. Flight controls H. Landing gear I. Equipment and furnishings J. Navigation Equipment K. Flight instruments L. Communications equipment M. Warning systems N. Lighting O. Emergency equipment (aircraft specific) Aircraft Ground Training: Section 2 - Aircraft Systems
Aircraft Ground Training: Section 2 - Aircraft Systems G. Flight controls
G. Flight controls • Primary controls (yaw, pitch and roll devices) • Secondary controls (Leading/trailing edge devices, flaps, trim and dampening mechanisms) • Means of actuation (direct/indirect) Aircraft Ground Training: Section 2 - Aircraft Systems
Flight controls – Primary • The Cherokee Six is controlled in flight by the use of three standard primary control surfaces, consisting of: • Ailerons, • Stabilator and • Rudder. • Operation of these controls is through the movement of the control column-tee bar assembly and rudder pedals. • On the forward end of each control column is a sprocket assembly. A chain is wrapped around the sprockets to connect the right and left controls and then back to idler sprockets on the column’s tee bar, which in turn connect to the aileron primary control cables. Aircraft Ground Training: Section 2 - Aircraft Systems
Flight controls – Primary • The cables operate the aileron bellcrank and push-pull rods. • The stabilator is controlled by a cable connected to the bottom of the tee bar assembly and at the balance arm of the stabilator. • Cables also connect the rudder pedals with the rudder horn. Aircraft Ground Training: Section 2 - Aircraft Systems
Flight controls – Trim • Provisions for directional and longitudinal trim control is provided by an adjustable trim mechanism for the stabilator and rudder. • The stabilator trim is controlled by a wheel and drum mounted on the floor tunnel between the front seats. Cables routed aft from the drum to the tail cone operate a screw assembly which in turn moves the stabilator trim tab. • The rudder trim is controlled by a knob and screw assembly attached to the rudder pedal assembly. Aircraft Ground Training: Section 2 - Aircraft Systems
Flight controls – Flaps • The wing flap system consists of an operating handle, a cable routed from the handle to a torque tube and push-pull rods. • Through the push-pull rods and torque tube, the flaps are interconnecting and can be positioned in three locations of 10, 25 and 40 degrees. Aircraft Ground Training: Section 2 - Aircraft Systems
Aircraft Ground Training: Section 2 - Aircraft Systems H. Landing gear
H. Landing gear • Brake system • Nose wheel steering • Landing gear system schematic Aircraft Ground Training: Section 2 - Aircraft Systems
Landing Gear - General • The landing gear incorporated on the PA-32 is a fixed, tricycle type, fitted with three 600 x 6 wheels. • The landing gear struts are of the air-oil type. Normal extension for nose gear = 3-1/4 inches. Normal extension for main gear = 4-1/2 inches. Aircraft Ground Training: Section 2 - Aircraft Systems
Landing Gear – Brake System • The two main wheels are equipped with a single disc hydraulic brake assembly which is actuated by a hand lever connected to a cylinder located below and behind the center of the instrument panel, or by individual cylinders attached to each rudder pedal. • The hand lever also doubles as a parking brake and may be operated by pulling back on the handle and pushing in on the button at the side of the handle. • To disengage the parking brake, pull back on the handle. • A brake fluid reservoir is installed on the left forward face of the engine firewall. Aircraft Ground Training: Section 2 - Aircraft Systems
Landing Gear – Nose Wheel Steering • The nose gear, steerable through a 60 degree arc, enables a 30 degree turn in each direction. • To aid in nose wheel and rudder centering and to provide rudder trim is a spring device attached to the rudder pedal torque tube assembly. • A shimmy dampener is also incorporated in the nose wheel steering mechanism . Aircraft Ground Training: Section 2 - Aircraft Systems
Aircraft Ground Training: Section 2 - Aircraft Systems I. Equipment and furnishings
I. Equipment and furnishings • Exits, both normal and emergency • Cargo areas • Crewmember and passenger seats • Bulkheads • Seating and or cargo configurations • Non emergency equipment and furnishings Aircraft Ground Training: Section 2 - Aircraft Systems
Equipment & Furnishings - Exits Aircraft Ground Training: Section 2 - Aircraft Systems
Equipment & Furnishings – Cargo Areas Aircraft Ground Training: Section 2 - Aircraft Systems
Equipment & Furnishings – Crew and Passenger Seats • Front Seats Adjustable Forward and Aft • Center and Rear Seats Easily Removed for Additional Cargo Space Aircraft Ground Training: Section 2 - Aircraft Systems
Bulkheads • 2 main bulkheads forward and aft. Seating and or cargo configurations • N4599X does not have optional 7th seat installed • Rear and middle seats can be removed for larger cargo operations. Non emergency equipment and furnishings • Class Discussion Aircraft Ground Training: Section 2 - Aircraft Systems
Examination Written examination required
Completion of Paperwork Student Fill-out Student Feedback Form Sign Training Record (if applicable) Instructor Sign Class Roster Fill-out Instructor Feedback Form Sign Training Record (if applicable)
