Service difficulty report · Skin Panel · Airbus A320232

Difficulty date
July 30, 2022
Submitted
August 2, 2022
Operation
Air carrier
Aircraft
N535JB
Make and model
Airbus A320232
Aircraft serial
01739
Aircraft time
76,093 hours, 27,546 cycles
System (JASC)
5711 · Wing Spar
Part
Skin Panel
Condition
Corroded
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

DURING HEAVY MAINTENANCE: CORROSION REAR SPAR LOC. TOP SKIN, LOWER SURFACE, OVERHANG BTW RIB10 T O RIB11 ON LH WING. REFER TO THE MPD TASK 572178-01; PERFORMED REPAIR ON TOP SKIN LOWER SURFACE OVERHANG BTW RIB 10 TO RIB 11 ON LH WING I.A.W. EC NO. A22-605-01 AND EA NO. 57-0204-22, PART 1,2,7,8,10,11,12 ,EA# 57-0358-22 COVER REV. 0 THIS REPAIR IS CATEGORY B AND MUST BE INSPECTED FOR TOP SKIN PANEL2 UPPER SURFACE AT THE REAR SPAR AT THRESHOLD (OR INSPECTION START POINT) 10000FC/20000FH INTERVAL 10000FC/20000FH METHOD SDI,DET EXTERNAL , FOR REAR SPAR TOP FLANGE AT THRESHOLD (OR INSPECTION START POINT) 33100FC/66200FH. INTERVAL: TBD METHOD: TBD I.A.W. RDAF NO. 81076198/141/2022#A TOOL USED CALIPER P/N: 500-464, S/N: B17030932, DUE DATE: NOV-29-2022; TOOL USED EDDY CURRENT EQUIPMENT P/N: NORTEC 600D, S/N: 200048001, DUE DATE: MAR-30-2023; TOOL USED ULTRASONIC EQUIPMENT P/N: 35DL, S/N: 091419910, DUE DATE: JAN-26-2023; TOOL USED MICROMETER P/N: 293-340-30, S/N: A18229497, DUE DATE: SEP-21-2022; TOOL USED TORQUE P/N: QD1R200A, S/N: 0821901619, DUE DATE: AUG-13-2022 COMPLETED MX-220 FROM BY CPCP PROGRAM ACCOMPLISHED ON AEROMAN: W/O:2022 76/1 NRC: 2022 - 327724 TECH: R. BRITO 8603909 INSP: INSP. S. ASCENCIO PERFORMED REPAIR ON TOP SKIN LOWER SURFACE OVERHANG BTW RIB 10 TO RIB 11 ON LH WING I.A.W. EC NO. A22-605-01 AND EA NO. 57-0204-22, PART 1,2,7,8,10,11,12 ,EA# 57-0358-22 COVER REV. 0 THIS REPAIR IS CATEGORY B AND MUST BE INSPECTED FOR TOP SKIN PANEL2 UPPER SURFACE AT THE REAR SPAR AT THRESHOLD (OR INSPECTION START POINT) 10000FC/20000FH INTERVAL 10000FC/20000FH METHOD SDI,DET EXTERNAL , FOR REAR SPAR TOP FLANGE AT THRESHOLD (OR INSPECTION START POINT) 33100FC/66200FH. INTERVAL: TBD METHOD: TBD I.A.W. RDAF NO. 81076198/141/2022#A TOOL USED CALIPER P/N: 500-464, S/N: B17030932, DUE DATE: NOV-29-2022; TOOL USED EDDY CURRENT EQUIPMENT P/N: NORTEC 600D, S/N: 200048001, DUE DATE: MAR-30-2023; TOOL USED ULTRASONIC EQUIPMENT P/N: 35DL, S/N: 091419910, DUE DATE: JAN-26-2023; TOOL USED MICROMETER P/N: 293-340-30, S/N: A18229497, DUE DATE: SEP-21-2022; TOOL USED TORQUE P/N: QD1R200A, S/N: 0821901619, DUE DATE: AUG-13-2022 COMPLETED MX-220 FROM BY CPCP PROGRAM ACCOMPLISHED ON AEROMAN: W/O:2022 76/1 NRC: 2022 - 327724 TECH: R. BRITO 8603909 INSP: INSP. S. ASCENCIO (CONSIDERED AS A MAJOR REPAIR)

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