Issue Date: 29 Jan 2009 Rev 1
Page 25
INSPECTION AFTER HARD LANDING
It is necessary to do a detailed inspection following any unusual stressing of the hang glider
this full inspection should include all details listed for six-monthly maintenance.
The inspection should be noted in the logbook, and any replacements recorded.
DEFECT REPORTS
Details of any defect which develops in service and which, if kept uncorrected, would
compromise the continued safe operation of the hang glider should be reported to
Airborne
as soon as practicable.
Summary of Contents for Sting 3
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Page 34: ...Issue Date 29 Jan 2009 Rev 1 Page 34 STING X BAR LEADING EDGE JUNCTION A4 4716...
Page 37: ...Issue Date 29 Jan 2009 Rev 1 Page 37 REAR LEADING EDGE ASSEMBLY STING A4 6859...
Page 38: ...Issue Date 29 Jan 2009 Rev 1 Page 38 STING III 154 NOSE JUNCTION ASSEMBLY A4 4717...
Page 40: ...Issue Date 29 Jan 2009 Rev 1 Page 40 STING III 168 NOSE JUNCTION ASSEMBLY A4 7743...
Page 42: ...Issue Date 29 Jan 2009 Rev 1 Page 42 STING III KEEL ASSEMBLY A4 7608...
Page 45: ...Issue Date 29 Jan 2009 Rev 1 Page 45 CONTROL FRAME STING III 154 PREASM A4 7625...
Page 47: ...Issue Date 29 Jan 2009 Rev 1 Page 47 CONTROL FRAME STING III 168 PREASM A4 7747...
Page 49: ...Issue Date 29 Jan 2009 Rev 1 Page 49 STING HANG LOOP ASSEMBLY A4 4796...
Page 50: ...Issue Date 29 Jan 2009 Rev 1 Page 50 STING III SAIL TO AIRFRAME ASSEMBLY A4 7748...
Page 53: ...Issue Date 29 Jan 2009 Rev 1 Page 53 STING III INTERCHANGE TABLE A4 7749...
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