Service difficulty report · Bolt · Beech 1900D

Difficulty date
April 29, 2005
Submitted
June 2, 2005
Operation
General aviation
Make and model
Beech 1900D
Aircraft time
12,936 hours
Engine
Pwa PT6A67D
Propeller
Hartzl HCE4A3I
Part
Bolt
Part number
NAS336CA17
Condition
Sheared
Location
Nlg
Stage of operation
CL
How discovered
O
Nature of condition
O
Precautionary procedure
E, A

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

What was found

AFTER T/O & GEAR UP SELECTED, CREW HEARD A LOUD THUD IN NOSE AREA. GEAR IND SHOWED AN UNSAFE CONDITION, GEAR SELECTED DOWN & 3 GREENS WERE OBTAINED FOR DOWN & LOCKED. DURING FLYBY, OBSERVED NLG TO BE PERPENDICULAR TO STRAIGHT. DECIDED TO FLY TO MAIN BASE. IT APPEARS THAT THE N/G CENTERING BOLT BROKE AT THE HEAD AND CAUSED THE CENTERING ROLLER TO BECOME JAMMED IN THE CENTERING CAM, NOT ALLOWING THE SPRING STRUT TO CENTER THE NOSE GEAR. ALL OF THE DAMAGED PARTS WERE REPLACED, INCLUDING THE CENTERING SPRING STRUT AND GEAR SWINGS ACCOMP TO ENSURE SERVICEABILITY. THE REMAINING 2 A/C IN THE FLEET WERE ALSO CHECKED AND FOUND WITH NO FAULTS. RAYTHEON A/C HAS BEEN CONSULTED ON THE BOLT BREAKAGE ISSUE.

More about the Beech 1900D