Service difficulty report · Stop Fitting · Airbus A319131

Difficulty date
December 10, 2020
Submitted
December 11, 2020
Operation
Air carrier
Aircraft
N812UA
Make and model
Airbus A319131
Aircraft serial
0850
Aircraft time
68,808 hours, 29,036 cycles
Part
Stop Fitting
Condition
Cracked
Location
R1 Door
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

R1 DOOR STOP NR 7 FRAME 16 AT DOUBLE JOGGLE AREA HOLE NR 6 IS CRACKED IN THE CORNER DOUBLER AND FRAME AT 2:00. CONTACT ENGINEERING F OR REPAIR-A3NB-53-4-0024 NR 9294237 GENERATED BY V061633 AT HA ECO LCQ, DUE TO CRACK AT RI DOOR STOP NR 7 FRAME 16 AT DOUBLE JOGGLE AREA HOLE NR 6, ECRA5311-02481 REQUIRES DIP FOR INITAL AND REPETITIVE INSPECTIONS. ACCOMPLISH THE INITAL INSP REQUIREMENTS REPAIR AT RT FR 16 DOUBLE JOGGLE DOOR STOP FITTING NR 7 HOLES NR 5 & NR 6, PER PART 2 OF LATEST REVISION OF ECRA5311-02481 ON OR BEFORE THE ACFT REACHES 35,835 FC. ACCOMPLISH REPEAT INSPECTIONS AT INTERVALS NOT TO NSIDERED PERMANENT IF INSPECTIONS, PER PART 2 ARE COMPLIED WITH. EXCEED 3,200 FC THEREAFTER. ACCOMPLISHED REPAIR PER PART 1 IS CO DIP FOR INITAL AND REPETITIVE INSPECTIONS. ACCOMPLISH THE INITAL INSPECTION REQUIREMENTS REPAIR AT RT FR 16 DOUBLE JOGGLE DOOR STOP FITTING NR 7 HOLES NR 5 & NR 6, PER PART 2 OF LATEST REVISION OF ECRA5311-02481 ON OR BEFORE THE ACFT REACHES 35,835 FC. ACCOMPLISH REPEAT INSPECTIONS AT INTERVALS NOT TO EXCEED 3,200 FC THEREAFTER. ACCOMPLISHED REPAIR PER PART 1 IS CONSIDERED PERMANENT IF INSPECTIONS, PER PART 2 ARE C TOMC-APPROVAL FROM SC1ELBYC COMMENT QC RECORDS UPDATE-AP QC REVIEWED. INIT: 35,835 TAFC INIT WILL ITO TO RIR (-2131) RIR: 3200 FC AP/U366012.

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