SDR 96ZZZX251

Service difficulty report · Bracket · Beech F33A

Difficulty date
December 21, 1995
Submitted
March 26, 2000
Operation
General aviation
Aircraft
N33BV
Make and model
Beech F33A
Aircraft serial
CE840
Part
Bracket
Condition
Elongated Hole
Location
Lt Mlg Uplock
Stage of operation
IN
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

WHEN THE GEAR WAS SWUNG ON JACKS DURING ANNUAL INSPECTION, THE LT MAIN WOULD NOT EXTEND. WHEN THE GEAR WOULD NOT EXTEND, THE LT LANDING GEAR ACTUATING ROD BUCKLED IN COMPRESSION IN THE TUBULAR SECTION, BENDING AT 2 PLACES ABOUT EQUIDISTANT FROM THE CENTER. THE RT MAIN AND NOSE GEAR EXTENDED NORMALLY. THE PROBLEM WAS THE LT UPLOCK BRACKET TIP HAD JAMMED INTO THE KNEE JOINT, PREVENTING GEAR FROM COMING DOWN. ON REMOVAL, UPLOCK BRACKET OBSERVED TO HAVE AN ELONGATED HINGE BOLT HOLE WHICH HAD ALLOWED TIP TO MOVE FORWARD (TOWARD THE FRONT OF AIRPLANE) INTO THE KNEE JOINT INSTEAD OF LINING UP WITH ITS ROLLER. TT, 3,500 HOURS.

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