What was found
INSPECTION TYPE: C1, CRACKED APPROX .5 INCH ON LONG 15 UPPER FLANGE 2ND CANTED FRAME FROM STA 1766 INSIDE MAIN CABIN RH SIDEWALL. REMOVED DAMAGE SECTION OF LONGERON, FABRICATED, AND INSTALLED REPAIR I AW DC-8 SRM 53-2-2 FIG 10.
- Difficulty date
- June 28, 2005
- Submitted
- July 20, 2005
- Operation
- Air carrier
- Aircraft
- N851UP
- Make and model
- Doug DC873F
- Aircraft serial
- 46051
- Aircraft time
- 75,626 hours, 25,638 cycles
- System (JASC)
- 5313 · Fuselage Main, Longeron/Stringer
- Part
- Longeron
- Condition
- Cracked
- Location
- Fuselage
- 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.