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Evaluation of aged B737 & B747 single element dual load path (SE-DLP) flight control components.

Conference ·
OSTI ID:900845
 [1]; ; ; ;  [2]
  1. FAA William J. Hughes Technical Center, Atlantic City, NJ
  2. FAA William J. Hughes Technical Center, Atlantic City, NJ
+ Show Author Affiliations

No abstract prepared.

Research Organization:
Sandia National Laboratories
Sponsoring Organization:
USDOE
DOE Contract Number:
AC04-94AL85000
OSTI ID:
900845
Report Number(s):
SAND2006-0836C
Country of Publication:
United States
Language:
English

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Related Subjects

42 ENGINEERING
AGING
AIRCRAFT
Aircraft accidents.
Aircraft industry
EVALUATION
Flight control.
Structural dynamics.
Structural failure-Testing.
Structural stability.
TESTING
United States.