Service difficulty report · Clamp · Cndair CL600*

Difficulty date
October 10, 2014
Submitted
March 12, 2015
Operation
General aviation
Make and model
Cndair CL600*
Aircraft time
29,684 hours
Engine
Ge CF348C5
Part
Clamp
Part number
BBDREF001927143
Condition
Torn
Location
Rt Pylon Saddle
Stage of operation
CL
How discovered
O
Nature of condition
K
Precautionary procedure
A

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

What was found

(CAN) AFTER DEPARTURE AND GEAR UP THE NO 2A HYD PUMP CAUTION LIGHT CAME ON AND SYSTEM QTY WENT TO 0% MAINTENANCE FOUND LEAK AT FLEXIBLE LINE (REF IPC 29-17-06, FIG. 1C, ITEM 128) FROM IB AFT NR 2 PYLON DOWN TO THE HYDRAULIC DAMPENER. THE SADDLE CLAMP P/N BBDREF001927143 SECURING THE FLEX LINE P/N AE717812-1 HAD CHAFFED THROUGH THE HYDRAULIC FLEX LINE DUE TO THE CLAMPS RUBBER SLEEVE TORN EXPOSING THE METAL PART OF THE CLAMP WHICH CHAFFED A HOLE THROUGH THE HYDRAULIC LINE. DAMAGED HOSE FROM HYDRAULIC DAMPER ASSY REPLACED AND SECURED WITH NEW CLAMP. INSPECTION COMPLETED ON NR 2 ENGINE DRIVEN HYDRAULIC SYSTEM IAW AMM TASK 05-51-33-210-801. NR 2 HYDRAULIC PRESSURE MANIFOLD FILTER AND EDP CASE DRAIN FILTER REMOVED AND INSPECTED FOR CONTAMINATION. NONE FOUND. NEW FILTERS INSTALLED AND HYDRAULIC SYSTEM SERVICED, LEAK CHECKED AND FUNCTION TESTED. NO FAULTS FOUND.