CFM Turbine Rear Frame
**** Hidden Message ***** February 2002 WTT face to face CFMI / Boeing Proprietary Information - Unauthorized Disclosure, Use, or Export are Prohibited 1<BR>Turbine Rear Frame<BR>February 2002 WTT face to face CFMI / Boeing Proprietary Information - Unauthorized Disclosure, Use, or Export are Prohibited 2<BR>Turbine Rear Frame<BR>Structural Life Limit Part Status<BR>Two Turbine Rear Frame references life limits have been increased, and<BR>certified by the Authorities<BR>• 340-027-110-0 (SAC Engine) is now 17,400 cycles 19 Dec 2001<BR>• 340-027-116-0 (DAC Engine) is now 14,000 cycles 17 Dec 2001<BR>TRF Par t Number Current life<BR>(Cycles)<BR>New Certified<BR>life (Cycles)<BR>Projected limit<BR>(Cycles)<BR>Scheduled<BR>Extension Date<BR>340-027-110-0<BR>(SAC)<BR>11,600 17,400 N/A N/A<BR>340-027-113-0<BR>(SAC)<BR>25,000 N/A No limit 2005<BR>340-027-115-0<BR>(SAC)<BR>20,400 N/A 30,000 2003<BR>340-166-205/206-0<BR>(SAC)<BR>20,400 N/A 30,000 2003<BR>340-027-116-0<BR>(DAC)<BR>7,300 14,000 N/A<BR>18,000<BR>N/A<BR>2001<BR>340-117-502/503-0<BR>(DAC)<BR>16,300 N/A No limit 2005回复 1# 航空 的帖子
ArmProposed Switch Configuration
Current Double Throw
Proposed Single Throw
Run contact eliminated
Introduction Logistics
• CFMI/Boeing/Honeywell laun :victory: :victory: CFM Turbine Rear Frame
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