Service difficulty report · Control Rod · Boeing 767259

Difficulty date
October 31, 2008
Submitted
December 4, 2008
Operation
Air carrier
Aircraft
N986AN
Make and model
Boeing 767259
Aircraft serial
24835
Part
Control Rod
Part number
114T01151
Condition
Defective
Location
Le Slat
Stage of operation
NR
How discovered
O
Nature of condition
J
Precautionary procedure
A

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

What was found

AIR TURN BACK REPORT LEADING EDGE SLAT ASYM EICAS MSG, DISPLAYED AT 400 FT WITH LEADING EDGE LIGHT ON WITH FLAPS TO 5 DEGREE WHILE TURNING LT WITH 180KTS, 25 DEGREE BANK, WITHOUT FLAPS MOVEMENT STICK SHACKER WAS ACTIVATED WITH NO REASON AND STOPPED FEW SECONDS AFTER. IAW AMM 27-81-01 PAG 401 TO 429 THE INBD LEADING EDGE SLAT NR 7 WAS REMOVED. SLAT CONTROL ROD WAS REPLACED AND IAW 27-81-01 PAG 430 OPS TEST IS SATISFACTORY AND IAW AMM 27-88-01 PAG 214 TO 224 THE LEADING EDGE SLAT SENSORS W SWITCH TEST IS SATISFACTORY. IT WAS FOUND CRACKED SKIN FIXED LEADING EDGE RT STA WS 197.4 AND INBD SLAT 7 WAS REMOVED. IAW SRM 57-41-01 AND SRM 51-70-17 ITEM 4A PAG 16 THE LEADING EDGE SKIN STA 197, 4 WAS REPAIRED PHASE I OPTION A INSPECTION WAS PERFORMED IAW AMM 05-51-35 / 201 BY OVERWEIGHT LANDING REPORTED, DURING INSPECTION NO FAULT FOUND. SLAT CONTROL ROD PART NR 114T0115-1.