Part catalog
39-18698
2016-22-09 09/12/2016 to detect and correct fatigue cracking at certain skin lap splice locations of the fuselage, which c 757-53-0090 37500 13400 AD is OPEN, under review of COLT Engineering. First action should be done when aircraft reaches 37,5 Supersedes AD 2006-20-11
Catalog record
- Part number
- 39-18698
- Source observations
- 6
- Last observed
- 2017-02-17
Catalog data is source-backed reference information. It does not establish availability, repair capability, certification, traceability, ownership, or airworthiness.