Service difficulty report · Structure · Boeing 727223

Difficulty date
May 15, 2006
Submitted
June 27, 2006
Operation
Air carrier
Aircraft
N754DH
Make and model
Boeing 727223
Aircraft serial
22008
Aircraft time
61,652 hours, 30,725 cycles
Part
Structure
Condition
Chafed
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.

What was found

LOWER FUSELAGE COWL FLANGE ANTI-CHAFE AREA IS WORN, AFT OF BULKHEAD (MARKED STA 1343). REMOVED FASTENERS LWR FUSELAGE AFT BULKHEAD STA 1343 IAW B727 SRM 51-30-2. CUT OUT DAMAGE AREA IAW B727 SRM 54-10-3 FIG 1 DIM 6.25 X .5 INCHES. FABRICATED ANGLE REPAIR FROM 7075-0 .063" PO 9002827 DIM 18 X 2.25 INCHES IAW B727 SRM 53-10-2 FIG 6 AND 51-40-4 FIG 1 FILLER FROM 7075T6 .050 PO 6149108 DIM 6.5 X .75 INCHES. HEAT TREATED PART TO T6 CONDITION IAW FLIGHTTSTAR AIRCRAFT SERVICES ENGINEERING REPORT 2-37153-801-1 REV IR. TREATED & PRIMED ANGLE & FILLER IAW B727 SRM 51-10-2. INSTALLED ANGLE & FILLER LWR FUSELAGE COWL AFT OF BULKHEAD STA 1343 IAW B727 SRM 54-10-3.