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ARTEX ELT-200 ARM
EBC Model 502 - ARM
EBC Model 102A - OFF
ARTEX ME 406 ARM
24.
Fire Extinguisher check
25.
Rescue Hammer check
26.
Baggage stowed, baggage net attached
27.
Canopy clean, undamaged
B. Walk Around Check and Visual Inspection
CAUTION
VISUALLY INSPECT FOR THE FOLLOWING CONDITIONS: DEFECTS, CONTAMINATION, CRACKS, DELAMINATIONS, EXCESSIVE PLAY, INSECURE OR IMPROPER MOUNTING AND GENERAL CONDITION.
ADDITIONALLY, CHECK THE CONTROL SURFACES FOR FREEDOM OF MOVEMENT.
CAUTION
SET PARKING BRAKE PRIOR TO REMOVING WHEEL CHOCKS.
1.
Left Main Landing Gear a) Landing Gear Strut visual inspection b) Wheel Fairing visual inspection c) Tire Pressure (33 psi / 2.3 bar) check d) Tire, Wheel, Brake visual inspection e) Wheel Chocks remove
2.
Left Wing a) Entire Wing visual inspection b) Stall Warning check (suck on opening) c) Pitot-Static Probe clean, holes open d) Tie down remove e) Taxi and Landing Lights visual inspection f) Wing Tip, Position Lights and Strobe visual inspection g) Aileron Balancing Weight visual inspection h) Aileron including Inspection Panel visual inspection i) Wing Flap including Inspection Panel visual inspection
3.
Fuselage a) Skin visual inspection b) Fuel Tank Vent check c) Fuel Drains drain water d) Structural Temperature Indicator check that structural
(for aircraft with other than white temperature does Undersides) not exceed) 55o C
(131o F) e) Maintenance Fuel Drains no leaks f) Fuel Quantity visual inspection (use fuel
pipette) g) Antennas visual inspection
4.
Empennage a) Stabilizers and Control Surfaces visual inspection b) Tie down remove c) Fixed Tab on Rudder visual inspection
5.
Right Wing a) Entire Wing visual inspection b) Wing Flap including Inspection Panel visual inspection c) Aileron including Inspection Panel visual inspection d) Aileron Balancing Weight visual inspection e) Wing Tip, Position Lights and Strobe visual inspection f) Tie down remove
6.
Right Main Landing Gear a) Landing Gear Strut visual inspection b) Wheel Fairing visual inspection c) Tire Pressure (33 psi / 2.3 bar) check d) Tire, Wheel, Brake visual inspection e) Wheel Chocks remove
7.
Nose
a) Oil check level by using dip-stick. Max level is 6 US quarts Min level is 4 US quarts
b) Cowling visual inspection c) Air Intakes clear d) Propeller visual inspection, Ground
Clearance; minimum: approx.
25 cm (10 in). e) Propeller Blades check for damage f) Spinner visual inspection g) Nose Gear visual inspection, towbar
removed h) Wheel Fairing visual inspection i) Tire Pressure (26 psi / 1.8 bar) check j) Tire and Wheel visual inspection k) Wheel Chocks remove
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本文链接地址:钻石20系列飞机维护手册 DA 20 SERIES AIRPLANE MAINTENANCE MANUAL(30)
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