Narrative:

Concerning a banner tow operation, a low approach was made 80-85 mph, 10 degree flap 16-17' of manifold pressure over the banner line after the pull up (I estimate 2G's) it was evident I had a problem with the cowling. I pulled the power and released the banner and landed with the remaining runway. Controling the aircraft was difficult due to the control yoke rubbing behind the panel. I then taxied off the active west/O any problem. It seems the top 2 motor mounts support channels broke free tearing the firewall with it. The engine dropped down about 25 degrees. It is evident these supporting channels have been cracked for some time leaving the firewall support stiffness to bear much of the load.

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Original NASA ASRS Text

Title: BANNER TOW SMA DROPS BANNER AFTER PICK WHEN PLT BECOMES AWARE OF ENGINE MOUNT PROBLEM. LANDS STRAIGHT AHEAD ON REMAINING RWY. CTLS PARTIALLY OBSTRUCTED BY WARPED FIRE WALL ENGINE MOUNT.

Narrative: CONCERNING A BANNER TOW OPERATION, A LOW APCH WAS MADE 80-85 MPH, 10 DEG FLAP 16-17' OF MANIFOLD PRESSURE OVER THE BANNER LINE AFTER THE PULL UP (I ESTIMATE 2G'S) IT WAS EVIDENT I HAD A PROB WITH THE COWLING. I PULLED THE PWR AND RELEASED THE BANNER AND LANDED WITH THE REMAINING RWY. CTLING THE ACFT WAS DIFFICULT DUE TO THE CTL YOKE RUBBING BEHIND THE PANEL. I THEN TAXIED OFF THE ACTIVE W/O ANY PROB. IT SEEMS THE TOP 2 MOTOR MOUNTS SUPPORT CHANNELS BROKE FREE TEARING THE FIREWALL WITH IT. THE ENG DROPPED DOWN ABOUT 25 DEGS. IT IS EVIDENT THESE SUPPORTING CHANNELS HAVE BEEN CRACKED FOR SOME TIME LEAVING THE FIREWALL SUPPORT STIFFNESS TO BEAR MUCH OF THE LOAD.

Data retrieved from NASA's ASRS site as of July 2007 and automatically converted to unabbreviated mixed upper/lowercase text. This report is for informational purposes with no guarantee of accuracy. See NASA's ASRS site for official report.