Service difficulty report · Pin · Cessna 550

Difficulty date
February 13, 2015
Submitted
March 12, 2015
Operation
General aviation
Make and model
Cessna 550
Part
Pin
Part number
C4466CL08
Condition
Broken
Location
Flap Drive
Stage of operation
NR
How discovered
9
Nature of condition
O
Precautionary procedure
O

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

What was found

(CAN) DURING THE FLAP GEARBOX REPLACEMENT, BOTH DUE FOR OVERHAUL AT 3000 HRS INTERVAL. IT WAS NOTED THAT ONE OF THE CONNECTING LINKS BETWEEN THE UPPER PORTION OF THE CHAIN & THE CABLE OF THE LT FLAP CONTROL SYS SECONDARY RUN HAD AN UNUSUAL GAP. AFTER REMOVING THE LINK LOCK & THE SIDE PLATE IT WAS OBSERVED THAT ONE PIN OF THE CONNECTING LINK COULD BE PULLED OUT, INDICATING THAT THE PIN WAS BROKEN. THE BREAKAGE WAS IN THE MIDDLE OF THE PIN, CONNECTED TO THE CHAIN SIDE OF THE LINK. THE CONNECTING LINK WAS REPLACED & THE FLAP SYS WAS OPERATED. NO FAULTS FOUND. TENSION OF THE FLAP CABLES WAS CHECKED & WITHIN LIMITS. THE OTHER CONNECTING LINKS, 7 OTHERS, WERE INSPECTED BY REMOVING THE LOCK & THE SIDE PLATES & BY PULLING THE ENDS OF EACH INDIVIDUAL PINS TO SEE IF THEY WERE BROKEN. NO OTHER DAMAGE FOUND.

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