Sun Apr 17, 2011 10:55 pm
Tue Apr 19, 2011 9:30 am
Tue Apr 19, 2011 4:04 pm
Tue Apr 19, 2011 4:11 pm
Tue Apr 19, 2011 4:24 pm
Tue Apr 19, 2011 10:02 pm
Yes, but not the color coat. I believe he had some tapes come off that were bonded on using butyrate dope over Stits fabric. As I understand it, the sizing used on the Stits fabric is not compatible with butyrate dope.airnutz wrote:Mixing unmatched materials...isn't that what led to Steve Wittman's fatal crash?
Thu Apr 21, 2011 4:03 pm
bdk wrote:Yes, but not the color coat. I believe he had some tapes come off that were bonded on using butyrate dope over Stits fabric. As I understand it, the sizing used on the Stits fabric is not compatible with butyrate dope.airnutz wrote:Mixing unmatched materials...isn't that what led to Steve Wittman's fatal crash?
Thu Apr 21, 2011 5:16 pm
Date: 27-APR-1995
Time: 1210
Type: Wittman O&O
Operator: private
Registration: N41SW
C/n / msn: 13
Fatalities: Fatalities: 2 / Occupants: 2
Other fatalities: 0
Airplane damage: Written off (damaged beyond repair)
Location: Stevenson, AL - United States of America
Phase: En route
Nature: Private
Departure airport: Ocala, FL (FDO4)
Destination airport: Oshkosh, WI (OSH)
Narrative:
REPORTS FROM GROUND WITNESSES, NONE OF WHOM ACTUALLY SAW THE AIRPLANE, VARIED FROM HEARING A HIGH REVVING ENGINE TO AN EXPLOSION. EXAMINATION OF THE WRECKAGE REVEALED THAT THE AIRPLANE EXPERIENCED AN IN-FLIGHT BREAKUP. DAMAGE AND STRUCTURAL DEFORMATION WAS INDICATIVE OF AILERON-WING FLUTTER. WING FABRIC DOPE WAS DISTRESSED OR MISSING ON THE AFT INBOARD PORTION OF THE LEFT WING UPPER SURFACE AND ALONG THE ENTIRE LENGTH OF THE TOP OF THE MAIN SPAR. LARGE AREAS OF DOPE WERE ALSO MISSING FROM THE LEFT WING UNDERSURFACE. THE ENTIRE FABRIC COVERING ON THE UPPER AND LOWER SURFACES OF THE RIGHT WING HAD DELAMINATED FROM THE WING PLYWOOD SKIN. THE DOPED FINISH WAS SEVERELY DISTRESSED AND MOTTLED. THE FABRIC COVERING HAD NOT BEEN INSTALLED IN ACCORDANCE WITH THE POLY-FIBER COVERING AND PAINT MANUAL; THE PLYWOOD WAS NOT TREATED WITH THE POLY-BRUSH COMPOUND. CAUSE: AILERON-WING FLUTTER INDUCED BY SEPARATION AT THE TRAILING EDGE OF AN UNBONDED PORTION OF WING FABRIC AT AN AILERON WING STATION. THE DEBONDING OF THE WING FABRIC WAS A RESULT OF IMPROPER INSTALLATION.
Thu Apr 28, 2011 10:39 pm