CSP−900RMM−2 MD Helicopters, Inc.
Rotorcraft Maintenance Manual
Page 208
Revision 34
04-00-00
FAA Approved
Table 1.
TENSION−TORSION STRAP EXPIRATION DATE
Manufacturers Cure Date Expiration Date
Before March 1999 September 2008
March 1999 thru February 2001 March 2009
March 2001 thru February 2005 March 2010
March 2005 thru February 2008 Cure Date Plus 5 Years
(22) Accelerated Life Limit: For all rotorcraft SNs 900−000008 thru 000124 that have incorporated Service
Bulletin SB900−105 and all rotorcraft SNs 900−000125 thru subsequent, time−in−service is accumulated at
an accelerated rate. To calculate the accelerated time−in−service, take the actual flight hours of the
rotating swashplate and multiply by 1.07 to determine hours toward 7,285 life limit.
Example: 6,808 actual flight hours x 1.07 accelerated life factor equals 7,285 hours.
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