Service difficulty report · Tire · Airbus A330243

Difficulty date
March 10, 2020
Submitted
April 1, 2020
Operation
Air carrier
Aircraft
N370HA
Make and model
Airbus A330243
Aircraft serial
1511
Aircraft time
27,240 hours, 4,156 cycles
System (JASC)
3244 · Tire
Part
Tire
Condition
Separated
Location
Rt Mlg
Stage of operation
TO
How discovered
O
Nature of condition
S
Precautionary procedure
K

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

What was found

SUP - #3 TIRE TREAD SEPARATED. // ON DESCENT HOLE 6" IN WING ROOT RIGHT SIDE #3 TIRE CAP DETACHED POST INSPECTION, ACCOMPLISHED "AFT TIRE BURST OR TREAD THROW FAILURE INSPECTION" PER A330 AMM 05-51-15-200-801. CONTACTED ATL MCC & ENGINEERING. 1)PERFORMED A DVI OF ALL THE DAMAGED AREA & SURROUNDING STRUCTURES. NO ADDITIONAL DAMAGE FOUND. 2)CONDUCTED A COIN TAP TEST & DVI AROUND THE ENTIRETY OF THE UPPER AND LOWER SURFACE OF PANEL & THE UNDER WING STIFFENING BEAMS. NO DE-LAMINATION FOUND. 3)PERFORMED A330 AMM 05-51-15-200-001-A."INSPECTION AFTER A TIRE BURST OR TREAD THROW OR WHEEL FAILURE - INSPECTION/CHECK". NO ADDITIONAL DAMAGE FOUND ON WHOLE OF AIRCRAFT. CONTACTED ENGINEERING. 4)PERFORMED VI AS PER A330 AMM 20-23-11-200-802A. NO LEAK & DAMAGE OF HYD HOSE FOUND. CONTACTED ENGINEERING. 5) PERFORMED THE FUNCTIONAL CHECK TO MONITOR "EXTERNAL" LEAKAGE OF HYD COMPARTMENTS AS PER A330 AMM 29-00-00-790-801A. NO LEAKAGE FROM HYD COMPONENTS FOUND AS PER ER/A 586148-14 REV ORIG PRI. ENGINEERING CREATED PRI ER/A 586148-14 REV 0RIG. PERFORMED STEP 1-7. ISSUED PRI ER/A586148-14 REV 1. PERFORMED STEP 7(RE-FABRICATED UPPER AND LOWER DOUBLERS). ACCOMPLISHED PRI ER/A 586148-14 REV 2. . FINALLY ISSUED ER/A 586148-14 REV ORIGINAL. VERIFIED PERFORM SEC 1. TIME LIMITED REPAIR MADE. A/C OK FOR SERVICE UNDER MAINTENANCE FERRY FLIGHT. ITEM DEF TO MON. PERMANENT REPAIR REQUIRED WITH IN 2 FLIGHT CYCLES. ASSOCIATED ER/A 14-586148 ADDED FOR AC 0370. CYCLES.

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