Abstract: Aircraft systems having thrust reversers with locking assemblies are disclosed herein. In one embodiment, an aircraft system includes a fan casing and a thrust reverser attached to the fan casing. The fan casing includes a first member. The thrust reverser includes a nozzle inner wall, a second member proximate to the nozzle inner wall for engaging with the first member, and a locking member positioned proximate to the first member. The locking member is movable between (a) a first position in which the first member is positioned between the locking member and the second member such that the locking member inhibits disengagement of the first and second members, and (b) a second position in which the locking member does not inhibit disengagement of the first and second members. The first member can be a V-groove, and the second member can be a V-blade.

Abstract: A computer-implemented method for providing on-line ultrasonically scanned images of composite parts for immediate feedback in a manufacturing environment is discussed. The scanned images are edited to indicate each deficiency that has been repaired on a previously assembled composite part. Quality assurance personnel enter data associated with each composite part and verify the data content. Repair personnel enter data associated with correcting an identified deficiency of the composite part. Historical data suitable for developing statistics and trends are stored for each type of composite part. When queries are launched, the statistical and trend data is filtered to produce reports that are displayed. That is, reports are generated that identify particular statistics and trends. The scan image and data associated with a composite part are linked together for cross-referencing and stored in a database that is accessible by client and server computers on a network.