Service difficulty report · Cotter Pin · Hawker BAE125700B

Difficulty date
October 5, 2017
Submitted
October 9, 2017
Operation
General aviation
Filed by
6EMY460C
Execujet MRO Services Middle East LLC DWC-Branch
Aircraft
N180EG
Make and model
Hawker BAE125700B
Aircraft serial
258188
Aircraft time
10,140 hours, 5,923 cycles
Part
Cotter Pin
Condition
Missing
Location
Rudder Tab
Component
Tab Assy
Component part number
25TR221AG
Stage of operation
IN
How discovered
V
Nature of condition
W
Precautionary procedure
K

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

What was found

DURING INSPECTION, NOTED THAT THE RUDDER TRIM TAB APPEARED TO HAVE EXCESSIVE PLAY. THE RUDDER TRIM TAB ROD ACTUATOR COVER PANEL WAS REMOVED AND IT WAS NOTED THAT A NUT WAS LYING LOOSE INSIDE THE PANEL. FURTHER INSPECTION REVEALED THAT THIS NUT ORIGINATED FROM THE RUDDER TRIM TAB ACTUATOR ROD LOWER MOUNTING BRACKET. THE BOLT WAS STILL IN PLACE AND THERE WAS NO EVIDENCE OF THE REQUIRED LOCKING COTTER PIN. IT WAS FURTHER NOTED THAT THE NUT ON THE BOLT OF THE UPPER MOUNTING BRACKET WAS STILL IN PLACE BUT LOOSE TO THE TOUCH. NO LOCKING COTTER PIN WAS PRESENT. INITIAL INDICATIONS SUGGEST THAT DURING A PREVIOUS MAINTENANCE INPUT THE RUDDER TRIM TAB ACTUATOR RODS WERE DISCONNECTED AND THEN ONLY PARTIALLY REINSTALLED LEAVING THE SAID NUTS NOT AT THE PRESCRIBED TORQUE VALUES AND THE REQUIRED COTTER PINS NOT INSTALLED. IT IS ASSUMED THAT WITH TIME AND VIBRATION ONE NUT VIBRATED LOOSE AND BECAME DETACHED FROM THE BOLT WHILE THE SECOND NUT ALSO VIBRATED LOOSE BUT REMAINED ATTACHED TO THE BOLT.