Boeing Components & Accessories #4 Bearing Program Status
**** Hidden Message ***** CFM56-7B WTT Meeting - September,25-26/2002 CFMI / Boeing Proprietary Information - Unauthorized Disclosure, Use, or Export are Prohibited 1<BR>#4 Bearing Program Status<BR>Components & Accessories<BR>CFM56-7B WTT Meeting - September,25-26/2002 CFMI / Boeing Proprietary Information - Unauthorized Disclosure, Use, or Export are Prohibited 2<BR>#4 bearing P/N installed on<BR>CFM56-7B<BR>305-355-717-0<BR>335-352-301-0<BR>335-352-302-0<BR>340-167-901-0<BR># 4 Bearing Status<BR>Background<BR>HP/LP Intershaft bearing<BR>• Constraints<BR> Bearing exposed at each shop<BR>visit<BR> Sensitive to agressors<BR>(handling, assembly ,<BR>contamination…)<BR>& manufacturing variability<BR>• Advantages :<BR>– Engine length reduction<BR>– Performance retention<BR>– Weight reduction<BR>CFM56-7B WTT Meeting - September,25-26/2002 CFMI / Boeing Proprietary Information - Unauthorized Disclosure, Use, or Export are Prohibited 3<BR>CFM56-All - UER & IFSD rates , #4 bearing fail cause<BR>IFSD<BR>0.00<BR>1.00<BR>2.00<BR>3.00<BR>4.00<BR>Fail per million EFH - 12 month rolling<BR>0<BR>100,000,000<BR>200,000,000<BR>Cumul effective flight<BR>hours<BR>UER + IFSD<BR>"UER" 1.32 as of July02<BR># 4 Bearing Status<BR>CFM56-7B WTT Meeting - September,25-26/2002 CFMI / Boeing Proprietary Information - Unauthorized Disclosure, Use, or Export are Prohibited 4<BR>CFM56--7B - UER & IFSD rates , #4 bearing fail cause<BR>"UER"<BR>IFSD<BR>UER + IFSD<BR>0.00<BR>2.00<BR>4.00<BR>6.00<BR>8.00<BR>Aug-98<BR>Feb-99<BR>Aug-99<BR>Feb-00<BR>Aug-00<BR>Feb-01<BR>Aug-01<BR>Feb-02<BR>Fail per million EFH - 12 month rolling<BR>0.88 as of July02<BR>CFM56-7B Average Better Than Global CFM Experience<BR># 4 Bearing Status<BR>CFM56-7B WTT Meeting - September,25-26/2002 CFMI / Boeing Proprietary Information - Unauthorized Disclosure, Use, or Export are Prohibited 5<BR>Ev# UER IFSD ESN DATE E.TSN E.CSN P/N<BR>1 1 874125 May/01/1998 520 220 335-352-301-0<BR>2 1 874254 Nov/01/1998 834 255 335-352-301-0<BR>3 1 875314 Dec/30/1998 1142 409 335-352-301-0<BR>4 1 874424 Sep/15/1999 1991 1271 305-355-717-0<BR>5 1 875529 Oct/19/1999 1225 791 305-355-717-0<BR>6 1 874596 Dec/14/1999 1997 650 340-167-901-0 Prod° stop 12-01 SB in progress<BR>7 1 874219 May/27/2000 5532 1814 305-355-717-0<BR>8 1 874669 Jul/18/2000 4844 1790 340-167-901-0 Prod° stop 12-01 SB in progress<BR>9 1 874103 Sep/29/2000 2975 1124 305-355-717-0<BR>10 1 874972 Nov/19/2000 3551 1687 340-167-901-0 Prod° stop 12-01 SB in progress<BR>11 1 876424 Dec/29/2000 943 670 305-355-717-0<BR>12 1 876403 Jan/27/2001 1422 875 305-355-717-0<BR>13 1 876686 Mar/23/2001 824 326 340-167-901-0<BR>14 1 874581 Aug/05/2001 6245 4662 340-167-901-0<BR>15 1 875652 Feb/28/2002 7908 5485 340-167-901-0<BR>16 1 876336 Mar/05/2002 6907 4068 305-355-717-0<BR>17 1 874816 May/31/2002 5465 2042 340-167-901-0<BR>18 1 876150 Jul/22/2002 7309 2504 340-167-901-0<BR>CFM56-7B #4bearing events summary<BR>Prod° stop 12-01<BR>Prod° stop 12-01<BR>Actions<BR>SB in progress<BR>SB in progress<BR>Batch of 47 suspect parts<BR>identified<BR>Production stopped in 1998 SB72-180 & 72-192<BR>SB72-328 & 72-329<BR>• reliability and quality monitored thru failure rates and failed bearing investigations<BR>• PN301 (retired > 1998) and PN 901 (thru2002) showed deviant failure rates<BR>• 2 ea.PN 717 from one defective batch<BR>• random other PN717 failures within large experience<BR># 4 Bearing Fleet Monitoring<BR>CFM56-7B WTT Meeting - September,25-26/2002 CFMI / Boeing Proprietary Information - Unauthorized Disclosure, Use, or Export are Prohibited 6<BR>#4 Bearing P/N340-167-901-0<BR>• Reliability and quality monitored thru failure rates and failed<BR>bearing investigations<BR> P/N340-167-901-0 showed deviant failure rates (See previous<BR>table)<BR> P/N 901 retirement program decided<BR>– From Production<BR>– From in-service engines when exposed at Shop visit<BR>regardless of age<BR>– SB72-0395 released September, 2002<BR># 4 Bearing Status<BR>CFM56-7B WTT Meeting - September,25-26/2002 CFMI / Boeing Proprietary Information - Unauthorized Disclosure, Use, or Export are Prohibited 7<BR>Material Improvement<BR>Outer race typical failure ----> improved outer race<BR>Introducing new Outer Race material : 32 CDV 13 + nitrogen hardening<BR> deep nitrite material<BR>– material structure gives high crack resistance<BR>– high compressive stress level --> high resistance to damage propagation<BR>(spalling) : aggression (dents, contamination) effects reduced<BR> successful tests<BR>– typically damaged samples<BR> better resistance than M50 to spalling propagation evidenced<BR>– large engine tests program satisfactorily achieved<BR> Implemented on production engines August, 2002<BR> Field implementation SB72-352 October, 2002<BR>32CDV13 Implemented to improve outer race reliability<BR># 4 Bearing Status<BR>CFM56-7B WTT Meeting - September,25-26/2002 CFMI / Boeing Proprietary Information - Unauthorized Disclosure, Use, or Export are Prohibited 8<BR>#4 brg vibration screening<BR>• Tool 856A2679 developed to measure roller passing frequency<BR> Based on development test bearing failure experience<BR>– Tested with intentionally pitted bearing -- refined signature<BR> To allow to early detect damaged bearing<BR>H (N2-N1)<BR>Tool 856A2679<BR>HP N2<BR>BP N1<BR>#4R detection<BR>message<BR>Accelerometer 1<BR>Accelerometer 2<BR>856A2679G0x<BR>Tool available for installation in<BR>CFM56 shop test facilities<BR>#4 brg Vibration Screening<BR># 4 Bearing Status<BR>CFM56-7B WTT Meeting - September,25-26/2002 CFMI / Boeing Proprietary Information - Unauthorized Disclosure, Use, or Export are Prohibited 9<BR>• Test cell and on-wing runs system - tool 856A2679-<BR>accumulating experience<BR>– CFM Production facilities and overhaul cells equipped<BR>– Less than 1% « delinquent » expected (experience)<BR>– Continuous working together efforts with shops to refine<BR>criteria<BR>• Screening procedure being implemented in the ESM for all<BR>CFM56 engine models<BR>• In February, 2003 ESM revision<BR>#4 bearing Vibrations Survey Initiative To Help Capture<BR>Damaged Bearing<BR>#4 brg vibration screening (cont’d)<BR>CFM56-7B WTT Meeting - September,25-26/2002 CFMI / Boeing Proprietary Information - Unauthorized Disclosure, Use, or Export are Prohibited 10<BR>Summary<BR>• CFM56-7B experience better than CFM experience<BR>• Material Improvement<BR>• 32 CDV13 material<BR>• higher outer race reliability<BR>• new bearing introduction expected 4 Qr 2002 for CFM56-7B<BR>• P/N -901 Shop Plan Defined, and issued<BR>• SB72-0395 issued in September, 2002<BR>• Damage Survey System<BR>• #4 bearing vibration survey initiative for outer Race damages<BR>• CFM tool available for test cell runs<BR>• Implementation started<BR>• Screening procedure to be implemented in Feb, 03 ESM revision<BR># 4 Bearing Status回复 1# 航空 的帖子
CFM56-7B TRAINING MANUAL ENGINE FAN TRIM BALANCE 看看去谢谢 Boeing Components & Accessories #4 Bearing Program Status
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