What was found
PREVIOUS BLEND OUT ON EXTERNAL FUSELAGE SKIN STA Y=200 AND Y= 201 LONG 3 RT AT UPPER FUSELAGE. AREA OUT LIMITS ON FUSELAGE SKIN ON STA Y= 200 AND 201 LONG 3 RT WAS REPAIRED PER SRM 53-04-3 FIG 8.
- Difficulty date
- July 21, 2017
- Submitted
- July 24, 2017
- Operation
- Air carrier
- Aircraft
- N911DL
- Make and model
- Doug MD88
- Aircraft serial
- 49542
- Aircraft time
- 76,124 hours, 58,812 cycles
- System (JASC)
- 5330 · Fuselage Main, Plate/Skin
- Part
- Skin
- Condition
- Damaged
- Location
- Fuselage
- 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.