Service difficulty report · Plenum · Airbus A330243

Difficulty date
May 7, 2020
Submitted
May 8, 2020
Operation
Air carrier
Aircraft
N381HA
Make and model
Airbus A330243
Aircraft serial
1114
Aircraft time
43,634 hours, 7,028 cycles
Part
Plenum
Condition
Delaminated
Location
Ac Bay
Stage of operation
IN
How discovered
V
Nature of condition
O
Precautionary procedure
K

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

What was found

ETOPS SIGNIFICANT SYSTEM - DIRECT Z190 NT: LH PACK PLENUM FOUND BADLY DE-LAMINATED AT MOUNTING BOLT AREAS AND CRACK LINES AT AFT EDGE. // ELECTRICAL CONNECTORS 521HH5 AND 521HH7 DISCONNECTED. 1)LH PACK PLENUM CHAMBER, PRIMARY HEAT EX-CHANGER, MAIN HEAT EX-CHANGER AND DUCT ARE REMOVED AS A SINGLE UNIT AS PER AMM21-51-41-000-803-A. 2)LH PACK PLENUM CHAMBER REMOVED AS PER AMM21-52-22-000-801-A. 3)LH PACK PLENUM CHAMBER INSTALLED AS PER AMM21-52-22-420-801-A REV 75.02 SN: 2230A00LI000571, PN:2230A000-01, FOUND SATISFACTORY. 4)LH PACK PLENUM CHAMBER, PRI AND MAIN HEAT EX-CHANGER AND DUCT ARE INSTALLED AS A SINGLE UNIT AS PER AMM21-51-41-400-803-A, REL 75.02 FOUND SATISFACTORY. 5)ELECTRICAL CONNECTORS 521HH5 AND 521HH7 ELECTRICALLY CONNECTED IAW AMM21-52-41-400-801, FOUND NIL DEFECT. LEAK CHECK PERFORMED AT DUCT JOINTS AND PLENUM CHAMBER CONNECTIONS AS PER AMM12-33-21-018-801-A-02, REL 75.02, FOUND NIL LEAK AND DEFECTS. OP TEST OF PACK CONTROL AND INDICATING SYSTEM PERFORMED AS PER AMM21-53-00-710-801-A REL 75.02, FOUND NIL LEAK AND DEFECTS. OP TEST OF THE CONDITIONED SERVICE - AIR SYSTEM WITH BLEED AIR PERFORMED AS PER AMM21-58-00-710-803-A. REL 75.02, FOUND NIL LEAK AND DEFECTS. RESET OF THE HEAT EX-CHANGER TREND MONITORING VIA MCDU PERFORMED AS PER AMM21-53-00-740-801-A REV 75.02, FOUND NIL DEFECT. PN OFF: 2230A0000-01 PN ON: 2230A0000-01

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