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Cracks found in Partenavia wing skin

----- Forwarded by Jim Bredy/RO/R2/FWS/DOI on 02/18/03 12:10 PM -----
To: con-aero@und.edu
02/18/03 10:57 AM
Subject: N737 Wing Skin Cracks

To all Partenavia Drivers,

The following is an e-mail I received, including digital photos, regarding some structural stress cracks on the aft portion of the leading edge ribs and the engine firewalls, that were found on our Partenavia Observer II aircraft during a routine inspection.

Jim Bredy
(505) 248-6630
Jim_Bredy@fws.gov

 

----- Forwarded by Guy Exon/OAS/OS/DOI on 02/18/2003 10:54 AM -----

To: Jim_Bredy@fws.gov
02/18/2003 10:51 AM
Subject: N737 Wing Skin Cracks

I inspected the P68TC OBS, S/N 400-04-OBS down in Albuquerque last week. Two inch cracks had been discovered on the bottom skin of the inboard leading edge. They were located outboard near the engine nacelle. Closer inspection and removal of the skin revealed the outboard rib cracked and broken where it attaches to the main spar. The middle rib also had cracks starting between the two rivet holes that fasten it to the spar. Cracks were also observed in the upper firewall near the engine mounts and edges. This damage was identical on both left and right wings.

The outboard portion of the inner leading edge helps support the engine cowling. On the left engine the outer rib supports the induction filter and alt air box assy. The right engine airbox assembly is mounted on the inboard rib of the outboard leading edge. No cracks were found on the outboard leading edge assy.

I do not suspect these cracks are related to an overstress situation. I also do not feel the weight of the filter assy. is the source since they appear on the right side without the filter assembly as well. Long term fatigue (5200 hrs A/C TT) operating in low level environment or engine vibrations could be contributors. The firewall is not structural and although I would not consider them directly related, probably developed for the same reasons.

The damage was discovered at a point of being minor although the repair requires the leading edge being replace as an assembly.  See the attached photo's showing the cracks.
 

Photo above is the firewall left hand crack

 

Mid Rib

 

Rib and skin

 

Leading edge skin