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12 Cards in this Set
- Front
- Back
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F/A 18 Composite Material |
Graphite and carbon/epoxy |
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When is composite material hazardous? |
When broken and fiber is exposed |
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To minimize aircraft damage during tow what must be done? |
-structural access doors installed -radome closed/secure -hydraulic brake pressure 2900 psi (min.) -68 L/R closed -all support equipment removed -all obstacles clear |
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Static Charge Removal Kit |
Used to discharge static build up in canopy and windshield stored during flight |
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How many tie down points are on an aircraft? |
12 (2 added when aircraft is jacked) |
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Purpose of composite material |
-limit weight -increase strength -decrease effect of corrosion |
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Name & describe the 3 types of aircraft repair. |
One Time - restores limited load carrying requirements; allow aircraft to be flown to repair station for permanent repairs Temporary Repair - restores full load carrying capabilities; allow aircraft to be flown to repair station for permanent repairs Permanent Repair - meets or exceeds strength of original structure |
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Purpose of LEX (Leading Edge Extension) |
Provides added lift at high angles of attack |
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Purpose of Launch Bar |
For steering aircraft |
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Purpose of Arresting Hook |
A means of stopping the aircraft |
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Similarities & differences of HS1 & HS2 |
HS1 - provides hydraulic fluid pressure to primary flight controls HS2 - provides hydraulic fluid pressure to primary flight controls and all other non-fiction control systems |
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What is Switching Valve |
Allow backup hyd. pressure to replace primary hyd. pressure when primary fails |
