Service difficulty report · Clamp

Difficulty date
August 10, 2010
Submitted
January 4, 2011
Operation
General aviation
Part
Clamp
Condition
Cracked
Location
Elt
Stage of operation
NR
How discovered
V
Nature of condition
O
Precautionary procedure
O

As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.

What was found

H-CLAMP IS CRACKING/SEPARATING OTBD FROM THE BODY OF THE H-CLAMP. IT APPEARS TO BE CAUSED BY THE COMPRESSION OF THE O-RING SEAL THAT IS IN THE GROOVE OF THE H-CLAMP BETWEEN THE EDGE OF THE BATTERY CASE AND THE BODY OF THE H-CLAMP. THE DESIGN OF THE CASE SHOULD PREVENT OVERCRUSH OF THE O-RING BECAUSE THE BATTERY CASE HAS MOLDED IN BOSSES WHICH CONTACT THE STANDOFFS INTO WHICH THE BATTERY CASE SCREWS THREAD. IT WOULD APPEAR THAT FOR WHATEVER REASON THE DIMENSIONS OF THE CASE ARE INCORRECT ALLOWING EXCESSIVE FORCE TO BE APPLIED TO THE O-RING WHEN THE SCREWS ARE TIGHTENED, OR THE MATERIAL OF THE H-CLAMP IS SUBSTANDARD AND UNABLE TO WITHSTAND THE FORCES GENERATED WHEN THE BATTERY IS SECURED TO THE BODY OF THE ELT.