Service difficulty report · Drive Gear · Cessna 421C

Difficulty date
September 29, 2001
Submitted
October 4, 2001
Operation
General aviation
Aircraft
N112MJ
Make and model
Cessna 421C
Aircraft serial
421C0907
Engine
Cont GTSIO520L
Engine time
535 hours
Part
Drive Gear
Part number
646655A1
Condition
Damaged
Location
Alternator
Component
Alternator · Teledynecrit
Component part number
649304
Stage of operation
CR
How discovered
C
Nature of condition
E, H
Precautionary procedure
A

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

What was found

L. ALTERNATOR FAILED DURING FLIGHT AND A VIBRATION WAS NOTED ABOUT 20 MINUTES LATER. THE ENGINE OIL PRESSURE DROPPED ABOUT 25 PSI AND A PRECAUTIONARY LANDING WAS MADE. UPON REMOVAL OF THE ALTERNATOR IT WAS DISCOVERED THE DRIVE HUB WAS NEARLY DESTROYED AND THE DRIVE GEAR BOLTS WERE MISSING AND THE GEAR WAS LOOSE ON THE BULLGEAR SHAFT. THE REMNANTS OF THE DRIVE GEAR WERE LOCATED IN THE OIL PAN ALONG WITH THE CASTLE NUT AND COTTER PIN. (SEE PHOTO)THIS IS THE SECOND OCCURRENCE OF THIS TYPE FAILURE IN THE PAST 2 WEEKS, THE OTHER WAS ON THE I. ENGINE OF A 421C WITH ABOUT 1400 HOURS ON THE ENGINE AND LESS THAN 100 HOURS ON THE ALTERNATOR SMOH. NEITHER ALTERNATOR EXHIBITED ANY BEARING PROBLEMS. WE HAVE BEEN UNABL

More about the Cessna 421C