Service difficulty report · Skin · Emb ERJ190100IGW

Difficulty date
July 24, 2024
Submitted
July 25, 2024
Operation
Air carrier
Aircraft
N318JB
Make and model
Emb ERJ190100IGW
Aircraft serial
364
Aircraft time
36,027 hours, 24,211 cycles
Part
Skin
Condition
Corroded
Location
Zone 100
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: FUSELAGE / CENTER FUSELAGE II & III / FR 73-74 / STGR 28 RH TO 29 LH / LOWER SKIN / CORROSION – PERMANENT REPAIR; REFERENCES: /1/ TOMX ETI-190-24-211 REV 01 /2/ EMBRAER ETD2024-190-018554. DESCRIPTION: AT CURRENT (7/2024) BASIC 6 CHECK FOR N318JB MSN 364 AT QRO, TOMX REPORTED CORROSION AFFECTING THE CENTER FUSELAGE II LOWER REAR SKIN P/N: 190-25004-001 AND CENTER FUSELAGE III LOWER SKIN P/N: 170-91883-005 BETWEEN FR 73 TO FR 74 BETWEEN STGR 28R TO 29L. THE DAMAGES ARE SHOWN IN FIGURE 1 AND 2 OF THE REF /1/ ETI. AS PER THE REF /1/ ETI, TOMX BLENDED OUT THE AREAS IAW SRM 51-10-03 AND FOUND OUT OF THE LIMITS AS PER SRM 52-23-01 AD 51 DUE TO REMAINING THICKNESS LESS THAN 10%. TOMX CONTACTED EMBRAER FOR REPAIR DISPOSITION, EMBRAER PROVIDED THE REF /2/ ETD WHICH CONSISTS OF A DOUBLER AND TRIPLER REINFORCEMENT AS THE PERMANENT REPAIR WITH POST REPAIR INSPECTION REQUIREMENTS. THIS EC ACCOMPLISHES THE PERMANENT REPAIR PER THE REF /1/ ETI AND COMPLIES WITH REF /2/ ETD WITHOUT DEVIATION. EC E24-895-01 IS ISSUED TO ACCOMPLISH THE PERMANENT REPAIR PER THE REF /2/ RDAF. EC E24-895-02 IS ISSUED TO ACCOMPLISH THE POST REPAIR INSPECTION REQUIREMENTS (LFEC THRESHOLD= INTERVAL = 7500FC) PER THE REF /2/ ETD AND ANAC FORM. SUBSTANTIATION: THIS PERMANENT REPAIR HAS BEEN APPROVED VIA REF /2/ETD AND IS CLASSIFIED AS MAJOR. (E/C: E24-895-01)

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