Service difficulty report · Static System · Cessna 560XL

Difficulty date
April 15, 2015
Submitted
April 15, 2015
Operation
General aviation
Filed by
IGXR989E
Heritage Aviation,Inc.
Make and model
Cessna 560XL
Part
Static System
Part number
68C48
Condition
Leaking
Location
Zone 100
Stage of operation
IN
How discovered
9
Nature of condition
O
Precautionary procedure
K

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

What was found

DURING RVSM RE-CERTIFICATION TESTS ON MULTIPLE MFG AIRFRAMES, EXCESSIVE INSTRUMENT STATIC SYSTEM LEAKAGE HAS BEEN TRACED TO LOOSE 90 DEGREE FITTINGS ATTACHED TO THE LOWER FUSELAGE STATIC SYSTEM MOISTURE DRAINS. TESTING HAS SHOWN THAT THE O-RING ON THE DRAIN BODY AT THE 90 DEGREE ELBOW FITTING WILL ONLY SEAL WITHIN 180 DEGREES OF THE FULL CLOCKWISE STOP AS THE ELBOW IS TIGHTENED ON THE DRAIN PORT. WE HAVE FOUND THAT INSTALLERS WILL RANDOMLY TIGHTEN THE DRAIN PORT TO THE SKIN AND THAT THE ELBOW WILL NOT CLOCK CORRECTLY TO PLACE THE ELBOW ROTATION IN LINE WITH THE ASSOCIATED FLARE FITTING LINE WITHIN THAT 180 DEGREE LIMIT, CAUSING THE O-RING TO NOT BE COMPRESSED SUFFICIENTLY TO SEAL. SUGGEST FIRMLY SNUGGING THE ELBOW ONTO THE DRAIN PORT, ALIGNING THE ELBOW TO PROPERLY ENGAGE THE TUBING FLARE FITTING; THEN SECURELY TIGHTEN THE DRAIN PORT MOUNTING NUT WITHOUT LOSING THE ALIGNMENT. THIS WILL RESULT IN THE BEST POSSIBLE SEAL AND MINIMIZE STATIC SYSTEM LEAKS AT THE DRAIN.

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