Service difficulty report · Switch · Dhav DHC8102

Difficulty date
January 2, 2008
Submitted
January 21, 2008
Operation
General aviation
Make and model
Dhav DHC8102
Aircraft time
48,229 hours
Engine
Pwa PW120A
Propeller
Hamstd 14SF7
Part
Switch
Part number
992236H18697
Condition
Broken
Location
Hyd System
Stage of operation
DE
How discovered
O
Nature of condition
J
Precautionary procedure
O

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

What was found

(CAN) SDR BEING SUBMITTED DUE TO (3) OCCURRENCES OF (RUD PRESS) AND (RUD FULL PRESS) CAUTION MESSAGES OVER A PERIOD OF (4) DAYS. (1ST) EVENT OCCURRED DECEMBER 30, 2007 JUST AFTER TAKEOFF AND CAUSED AN AIR TURN BACK TO THE DEPARTURE AIRPORT. MAINT PERFORMED GROUND CHECK, THEN AN OPS CHECK IAW AMM 27-30-38 WITH NO FAULTS FOUND. (2ND) EVENT OCCURRED ON DECEMBER 31, 2007 AGAIN JUST AFTER TAKEOFF. AC RETURNED TO AIRPORT OF DEPARTURE. MAINT TROUBLESHOOTING FOUND RUDDER PRESSURE DROPS APPROXIMATELY 800-1000 PSI ON NR 1 HYD SYS. RUDDER PRESSURE REGULATOR REPLACED BUT WITH NO FIX. NR 1 HYD SYS BLED AND ALSO NO FIX. NR 1 LWR ACTUATOR (PN 11200-1 SN UNK) WAS REPLACED AND OPERATION CHECKED IAW AMM 27-20-01 PG 215. (3RD) EVENT OCCURRED DURING DECENT TO ARRIVAL AIRPORT ON JANUARY 2, 2008. QTY AND HYD PRESS WAS OK, SO THE CREW CONTINUED IAW QRH. MAINT FOUND A BROKEN MICROSWITCH ON THE NR 1 RUD PUSH OFF ON THE GLARE SHIELD PANEL ABOVE THE FGC CONTROLLER. MICROSWITCH REPLACED AND RUDDER SYS TESTED SERVICEABLE IAW AMM 27-20-00. (TC NR 20080105002)