What was found
FUSELAGE MAIN ENTRY DOOR CUTOUT, ANGLE CRACKED BETWEEN STOP FITTING NR 6 AND NR 7, DEFECT SIZE, LENGTH .375. ANGLE REPLACED AT MAIN ENTRY DOOR, FORWARD SECTION PER SRM 51-10-1, PAGE 5, AND SRM 51-30-2. (M)
- Difficulty date
- January 6, 1999
- Submitted
- March 26, 2000
- Operation
- Air carrier
- Aircraft
- N209US
- Make and model
- Boeing 737222
- Aircraft serial
- 19548
- System (JASC)
- 5330 · Fuselage Main, Plate/Skin
- Part
- Skin
- Condition
- Cracked
- Location
- Fuselage
- Stage of operation
- IN
- Nature of condition
- O
- Precautionary procedure
- K
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.