Service difficulty report · Journal · Dhav DHC8102

Difficulty date
November 2, 2006
Submitted
December 4, 2006
Operation
General aviation
Make and model
Dhav DHC8102
Aircraft time
37,760 hours
Engine
Pwa PW120A
Propeller
Hamstd 14SF7
Part
Journal
Part number
104071
Condition
Worn
Location
Mlg Stab
Part time
41,530 hours
Component
Stabilizer · Messier
Component part number
10400105
Stage of operation
IN
How discovered
9
Nature of condition
O
Precautionary procedure
K

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

What was found

(CAN) AIRCRAFT WAS POSITIONED ON GATE FOR NEXT FLIGHT. IT WAS THEN FOUND THAT RT MAIN LANDING GEAR PIN COULD NOT BE REMOVED. TROUBLESHOOTING BY MAINTENANCE FOUND ON THE FOLLOWING ON THE RT MAIN LANDING GEAR STABILIZER STAY ASSEMBLY. THE AFT LINED JOURNAL BUSHING (ITEM 305) FOUND TO HAVE EXCESSIVE WEAR (1/16TH 3/32ND) CAUSING THE DOWN LOCK PIVOT POINT LOCK LINK ASSEMBLY (ITEM 280) TO OVERCENTER TOO FAR. THE STAY ASSEMBLY WAS REPLACED PER DHC 8 AMM 32-10-26, OPERATION AND LEAK CHECKS CARRIED OUT WITH NO FAULTS, AND THE AIRCRAFT RETURNED TO SERVICE. REFERENCE MESSIER-DOWTY COMPONENT MAINTENANCE MANUAL 32-10-04 FIG 1, PAGES 1010-1016.