Service difficulty report · Casting · Boeing 737201

Difficulty date
June 24, 2004
Submitted
July 22, 2004
Operation
General aviation
Make and model
Boeing 737201
Aircraft time
60,289 hours, 55,926 cycles
Engine
Pwa JT8D9A
Part
Casting
Condition
Cracked
Location
Vertical Stab
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.

What was found

(CAN) DURING MAINTENANCE CHECK A CRACK WAS FOUND ON THE SPIDER CASTING AT RUDDER STATION 23.27 BELOW THE STANDBY RUDDER PCU IN THE VERTICAL STABILIZER. THE CRACK IS 3 INCHES IB OF OUTER EXTREMITIES, 7 INCHES FORWARD OF THE LOWER RUDDER HINGE POINT APPROX 1.5 INCHES LONG AND .6250 INCHES FROM THE BASE. CRACK REPAIRED WITH AN EXTRUSION ANGLE IAW INSTRUCTIONS FROM MFG MESSAGE 1-31239593. TIMES, 61592.12 CYCLES 59677.