# SDR HALA2019071500360

- Type: Service difficulty report (as reported; unverified)
- Difficulty date: July 11, 2019
- Submitted: July 16, 2019
- Operation: Air carrier
- Aircraft: [N392HA](https://openairdocs.org/aircraft/N392HA), registered now
- Make and model: Airbus A330-243
- Registry model: [Airbus A330-243](https://openairdocs.org/model/airbus-a330-243) (OpenAirDocs)
- Aircraft serial: 1404
- Aircraft time: 27,493 hours, 4,390 cycles
- System (JASC): [7830 · Engine Thrust Reverser](https://openairdocs.org/jasc/7830)
- Part: Heat Shield
- Condition: Damaged
- Location: Thrust Reverser
- Stage of operation: IN
- How discovered: V
- Nature of condition: O
- Precautionary procedure: K
- FAA source: FAA Service Difficulty Reporting System (https://sdrs.faa.gov/)
- Page: https://openairdocs.org/sdr/HALA2019071500360

## Discrepancy

ETOPS SIGNIFICANT SYSTEM - #2 ENG VIEW FROM AFT AT 4:00 CLOCK POSITION TR HEAT SHIELD BLANKET HAS A HOLE 4" LONG. WELDED TEXTURE PATCH PER SAFRAN CMM 78-30-20 FRSX066 REPAIR 1. REMOVED #2 ENG O/B CENTER HEAT SHIELD BLANKET REF MM 78-30-20. INSTALLED #2 ENG CENTER HEAT SHIELD BLANKET REF CMM 78-30-20 UP TO SHEET METAL BLIND FASTENER INSTALL AND SEALANT INSTALL. INSTALLED BLIND FASTENERS ON AFT END OF HEAT SHIELD BLANKET PER CMM 78-30-20. PEND FASTENERS INSTALL                       ON CENTER POSITION OF BLANKET. INSTALLED FASTENERS IN CENTER SECTION OF HEAT SHIELD BLANKET.

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