What was found
MANIFOLD IS CRACKED IN THE PASSAGE BETWEEN THE FILTER PORT AND EXTEND CHECK VALVE TEST PORT. ALSO, THE APEX BETWEEN THE EXTEND PORT PASSAGE AND RETRACT PORT PASSAGE IS CRACKED ALONG THE UPPER EDGE. POSSIBLE CAUSE: STRESS CRACKS.
- Difficulty date
- April 14, 1999
- Submitted
- March 26, 2000
- Operation
- General aviation
- Filed by
- IU6R626N
Aero Controls, LLC - Make and model
- Boeing 737*
- System (JASC)
- 2760 · Drag Control System
- Part
- Manifold
- Part number
- 65445656
- Condition
- Cracked
- Location
- Spoiler
- Part time
- 11,998 hours
- Component
- 654456114
- 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.