Service difficulty report · Longeron · Dhav DHC8103

Difficulty date
June 19, 2013
Submitted
September 14, 2015
Operation
General aviation
Make and model
Dhav DHC8103
Part
Longeron
Part number
85360421109
Condition
Out Of Position
Stage of operation
NR
How discovered
9
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

(CAN) DUE TO LAMINATED SHIM NOT BEING INSTALLED IAW ENGINEERING REQUIREMENTS THE TEMPERING GAP OF .005 TO .016 EXISTS BETWEEN LONGERON AND MACHINE FITTING AND FRAME STN 373-380 AT STR 7S & 7P. MID FUSELAGE BUILD SINCE NOV 2006 TO MAR 2013 ARE AFFECTED. POTENTIALLY 239 MID FUSELAGES AFFECTED. STRESS ENGINEERING IS CONCERNED THAT THE LACK OF SHIMS COULD LEAD TO STRESS CORROSION CRACKING OF THE JOINT FITTING. IT IS RECOMMENDED TO RELEASE A SB TO ENSURE SHIMS ARE FITTED AND TO FIX ANY ACFT IN-HOUSE. AFFECTED RANGE OF ACFT 4156-4442.