Service difficulty report · Balance Weight · Piper PA44180T

Difficulty date
April 27, 2020
Submitted
April 27, 2020
Operation
General aviation
Aircraft
N8187H
Make and model
Piper PA44180T
Aircraft serial
448107002
Aircraft time
3,390 hours
Engine
Lyc TO360E1A6
Engine time
3,390 hours
Propeller
Hartzl HCC2YR2
Part
Balance Weight
Part number
3839805
Condition
Rusted
Location
Zone 300
Part time
3,390 hours
Component
Stab Trim Tab · Piper · PA44180T
Component part number
38399023839903
Stage of operation
IN
How discovered
O
Nature of condition
F
Precautionary procedure
K

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

What was found

DURING ANNUAL INSPECTION BY CRS # BIER466C, FOUND BALANCE WEIGHT ASSEMBLY P/N 38398-005 RUSTED THROUGH. RECEIVED NEW PIPER PART NUMBER 38398-005 AS REPLACEMENT. THE NEW ASSEMBLY COMES CONSIDERABLY OVER-SIZED. ADDRESS THE ISSUE WITH PIPER DSA TOM PENTECOST (DSA FLIGHTLINE GROUP) AND HE STATED NORMALLY AS THE FACTORY BALANCES THE STABILATOR, THE FACTORY WILL GROUND DOWN THE STAB TRIM TAB WEIGHT ASSEMBLY UNTIL THE STABILATOR FALLS WITHIN BALANCE SPECIFICATIONS. THE PROCEDURE FOR ACHIEVING PROPER STABILATOR STATIC BALANCE IS NOT IN THE PA44-180T M/M CHAPTER 55-23-00. AFTER THE FACTORY ACHIEVES A STATIC BALANCE, THE M/M STATES THE STAB NORMALLY SHOULD NOT REQUIRE RE-BALANCING. IT SEEMS TO ME A FIELD REQUIREMENT TO CHANGE A CORRODED BALANCE WEIGHT OR FOR RE-BALANCING A STABILATOR SHOULD BE PART OF THE MAINTENANCE MANUAL CHAPTER 55-23-00. THE DISTRIBUTION SERVICE ADMINISTRATOR (DSA) TOM PENTECOST LAST UPDATED, STATING THAT "ENGINEERING IS WORKING ON A PROCEDURE BUT THESE THINGS MOVE SLOWLY". PIPER SEMINOLES STANDARD AND TURBOCHARGED HAVE BEEN IN PRODUCTION SINCE 1979 AND ARE STILL AVAILABLE (NEW) THROUGH PIPER DEALERSHIPS. THE DATA SHOULD ALREADY EXIST AND SHOULD BE AVAILABLE FOR THE FIELD, CERTIFIED TECHNICIANS AND CERTIFIED REPAIR STATIONS.

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