// FAA AD DETAIL

FAA AD Detail

FAA 98-10-14

Back to AD List

FAA 98-10-14

Current

Final Rule

Subject
Rear Spar Fatigue Cracking
Model
L-1011-385-1 | L-1011-385-1-14 | L-1011-385-1-15 | L-1011-385-3
Docket Number
96-NM-257-AD
Amendment Number
39-10526
Publish Date
1998-05-15
Effective Date
1998-06-19
Superseded AD
FAA 96-07-13
Superseded By
Download AD Back to List