Bombardier Aerospace - 2005 - Crj200 - Composite Htab Tip - Srm - Damage Allowable Justification.pdf

TEMPLATE PREPARED AND MODIFIED AS OF 2000-07-31

BT0107-01 MW97 2000-07

WARNING: DO NOT DELETE THIS PAGE
When all known basic identification data is
entered, select “Print Preview” to update the
information in the document.

Title of Document: CRJ200 H-STAB TIP SRM DAMAGE
ALLOWABLE JUSTIFICATION
Doc. Number: RAS-601R-808
Revision Letter: NC
Date (yyyy-mm-dd): 2005-01-20
Program: CRJ200
Department: Stress
Status of Document:
(Draft / Preliminary) (Enter nothing if Report has no Status or enter your Status)
Classification:
(Restricted / Private / Confidential) (Enter nothing if Report has no Classification or
enter your Classification)
ATA Reference NOs: 55-12-51

Total of pages : 55
MAJOR SUPPLIER DOCUMENT NO.:
MAJOR SUPPLIER DOCUMENT REV.:
MAJOR SUPPLIER CAGE CODE:
ENGINEERING DOCUMENT
DISTRIBUTION LIST

PAGE: 1 of 1
DATE: 2005-01-20
DOCUMENT NUMBER: RAS-601R-808 REVISION: NC
TITLE: CRJ200 H-STAB TIP SRM DAMAGE ALLOWABLE JUSTIFICATION
SUMMARY
NAME DEPARTMENT BUILDING SITE REMARKS
K. Teague DCE Eng Belfast
W. McCrea Cust Support Belfast
G. Sarrazin Project Control CA Montreal





COMPLETE DOCUMENT

NAME DEPARTMENT BUILDING SITE REMARKS
D. Cottney Stress and Fatigue Eng Belfast
B. Mahoney 782 Montreal
A. Charbonneau 771 CA Montreal
J. Huddart 771 CA Montreal







BT0111-01 MW97 2000-07 © 2000 Bombardier Inc.
ENGINEERING DOCUMENT
SUMMARY

Bombardier Inc. PAGE: 1 of 1
CAGE CODE 3AB48
DATE: 2005-01-20
DOCUMENT NUMBER: RAS-601R-808 REVISION: NC
TITLE: CRJ200 H-STAB TIP SRM DAMAGE ALLOWABLE JUSTIFICATION
Author(s): MICHAEL PENDLEBURY
CONCLUSION

The structural analysis results show that generally the Horizontal Stabiliser Tip exhibits little
stress under normal operational conditions and can therefore tolerate relatively large damages.
High NS values are however found on the leading edge fasteners, an