What was found
CRACK ON CANTED FRAME STA 1178.225 BETWEEN LONGERON 16 LT AND 18 LT. INSTALLED ANGLE REPAIR 16 X 2 INCHES MAT USED 7075.0 0.80. HEAT TREATMENT TO 7075T6 GENERAL PROCESS SPECIFICATION 98 PMS 247.PS 01 AS PER SRM 51-70-11.
- Difficulty date
- May 13, 2007
- Submitted
- May 16, 2007
- Operation
- Air carrier
- Aircraft
- N937AT
- Make and model
- Boeing 717200
- Aircraft serial
- 55091
- System (JASC)
- 5311 · Fuselage Main, Frame
- Part
- Frame
- Condition
- Cracked
- Location
- Bs 1178 L16-18l
- 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.