Service difficulty report · Control Unit · Cndair CL6002B19

Difficulty date
April 1, 2007
Submitted
May 1, 2007
Operation
General aviation
Make and model
Cndair CL6002B19
Engine
Ge CF343B1
Part
Control Unit
Part number
706010
Part serial
623
Condition
Malfunctioned
Location
Horizontal Stab
Stage of operation
CL
How discovered
O
Nature of condition
F
Precautionary procedure
B, A

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

What was found

(CAN) SHORTLY AFTER TAKEOFF, FLIGHT EXPERIENCED A HSTA RUNAWAY. ACFT HAD JUST DEPARTED RUNWAY AND FLAPS WERE RETRACTED TO 0 DEGREES. AUTOPILOT DISENGAGED. TRIM SELECTION INPUT MADE. STABILIZER TRIM CONTINUED TO RUN & ASSOCIATED AURAL ALERT SOUNDED. IMMEDIATE ACTION CHECKLIST WAS COMPLETED, AS WAS QRH PROCEDURE. MODERATE CONTROL PULL FORCES WERE REQUIRED TO FLY ACFT AT 10,000 & 250 KNOTS. CREW USED ACARS SYSTEM TO CALCULATE A WEIGHT & BALANCE, & REDISTRIBUTED CABIN LOAD TO ALLEVIATE CONTROL FORCES. ICE ENCOUNTERED AT 10,000 FT & REQUIRED DESCENT TO 8,000 FT. EMERGENCY DECLARED. ACFT RETURNED. FLAPS SELECTED TO 20 DEGREES WHILE BETWEEN 8000 & 6000 FT. CONTROL FORCES WERE SIGNIFICANTLY LIGHTER ONCE FL