What was found
(CAN) DURING ACFT STRUCTURE FULL-SCALE FATIGUE TESTS, CRACKS HAVE BEEN DETECTED IN THE REAR FUSELAGE UPPER SKIN NEAR FRAME 94 AND FRAME 97 IN STR 3LT/RT. REPAIRS DONE IAW AVAILABLE SBS.
- Difficulty date
- September 6, 2011
- Submitted
- September 14, 2015
- Operation
- General aviation
- Make and model
- Emb ERJ190100IGW
- Aircraft time
- 9,419 hours
- Engine
- Ge CF3410E5A1
- System (JASC)
- 5330 · Fuselage Main, Plate/Skin
- Part
- Skin
- Condition
- Cracked
- Location
- Frames 94-97
- Stage of operation
- IN
- How discovered
- 9
- Nature of condition
- O
- Precautionary procedure
- K
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.