737 rudder issues resurface despite
redesign
Boeing's long-running
problems with the 737 rudder, thought to have been
finally settled six years ago with the redesign of the
power control units (PCU), have resurfaced with the
discovery of fractures in the input control rods to
the units, and a subsequent call for wide-ranging
corrective action by the US Federal Aviation
Administration.
The original rudder
control system redesign was prompted by a number of
rudder incidents, and two fatal accidents judged to
have been caused by large, uncommanded rudder
deflections. The new system had a different rudder PCU
design, with two independent valves and actuator arms
or rods.
The latest FAA
airworthiness directive (AD) follows reports of
fractures in the ends of rods connected to both the
main and standby PCU. The FAA says the action will
"prevent failure of one of the two input control rods
of the main rudder PCU, which, under certain
conditions, could result in reduced controllability of
the airplane and to prevent failure of any combination
of two input control rods of the main rudder PCU
and/or standby rudder PCU, which could cause an
uncommanded rudder hardover event and result in loss
of control of the airplane".
Boeing says the
fractures in the rods have been caused by a quality
control issue that resulted in the units becoming
"over-baked and brittle". Although Boeing identified
the problem in 2006 and initiated a retrofit program,
the FAA AD and acceleration of the replacement effort
was made inevitable by "the subsequent discovery of a
second broken rod in December".
Boeing says 880
aircraft have been fitted with the "enhanced" rudder
system, of which 681 were discovered to have been
delivered with "suspect rods".
Feb 13