CFM56 Inlet Gearbox Hardware No 3 Bearing Reliability CFM56-7B Aft Air/Oil Seal
**** Hidden Message ***** CFMI Proprietary information<BR>CFM56 Inlet Gearbox Hardware<BR>No 3 Bearing Reliability<BR>CFM56-7B Aft Air/Oil Seal<BR>October, 2004<BR>2<BR>CFMI Proprietary information<BR>CFM56-7B Inlet Gearbox Assembly<BR>No 3 Ball Bearing<BR>Spring Housing No 3 Roller Bearing<BR>Horizontal Bevel Gear<BR>No 3 Forward Air/Oil Seal No 3 Aft Air/Oil Seal<BR>No 3 Bearing Lock Nut<BR>Inlet Gearbox Housing<BR>24 Nuts that hold 3B/3R/Spring<BR>Housing to IGB Housing<BR>This gearbox is used in the CFM56-5A, CFM56-5B,<BR>CFM56-5C, and CFM56-7B engine applications<BR>3<BR>CFMI Proprietary information<BR>CFM56 No. 3 Ball Bearing Reliability<BR>October 2003 thru September 2004<BR>UER's IFSD Hours UER Rate IFSD Rate<BR>CFM56-3 1 1 9.898 0.101 0.101<BR>CFM56-7 2 0 9.250 0.216 0.000<BR>Total 3 1 19.148 0.157 0.052<BR>Note: Rates are<BR>per Million<BR>Engine Flight<BR>Hours<BR>• CFM56-3/-7B Models- Hard Particle Contamination<BR>– CFM56-3 S/B 72-923 recommends 50-75 Hour inspection interval on engines delivered<BR>between April, 1997 and ESN 860-226 until they reach 10,000 Hours<BR>– Extensive IGB Cleanliness Improvements incorporated across all CFM56 Production<BR>• CFM56-7B Programs - Ball Skidding<BR>– Engineering investigation – Bearing offset has impact on skidding<BR>– Engine Testing Complete – Able to reproduce skidding with minimum offset housing<BR>– Design change in place to increase min offset<BR>– Field action to inspect Spring Housing at exposure, re-identify or modify to achieve offset<BR>• CFM56-3/-7B Models - Winsted Non-Tumbled Ball Population (Fleet Highlites Aug 2002)<BR>– Root Cause Identified – No Field Actions recommended<BR>– Corrective Actions implemented at all bearing suppliers<BR>• Residual Stress Specification Implemented 12/00<BR>• Heat Treat and Improved Tumbling Process are now VSE controlled at all vendors<BR>• CFM56-3/-7B Models - MRC Ball Cracking<BR>– Root Cause Identified – Corrective Actions Implemented – No Field Actions recommended<BR>4<BR>CFMI Proprietary information<BR>CFM56-7B No 3 Bearing Reliability<BR>How does the No 3 bearing reliability compare with total fleet?<BR>CFM56-Total Fleet vs. CFM56-7B No 3 Ball Bearing Reliability<BR>12 Month Rolling Average<BR>0.000<BR>0.200<BR>0.400<BR>0.600<BR>0.800<BR>1.000<BR>1.200<BR>Jan-99<BR>Mar-99<BR>May-99<BR>Jul-99<BR>Sep-99<BR>Nov-99<BR>Jan-00<BR>Mar-00<BR>May-00<BR>Jul-00<BR>Sep-00<BR>Nov-00<BR>Jan-01<BR>Mar-01<BR>May-01<BR>Jul-01<BR>Sep-01<BR>Nov-01<BR>Jan-02<BR>Mar-02<BR>May-02<BR>Jul-02<BR>Sep-02<BR>Nov-02<BR>Jan-03<BR>Mar-03<BR>May-03<BR>Jul-03<BR>Sep-03<BR>Nov-03<BR>Jan-04<BR>Mar-04<BR>May-04<BR>Jul-04<BR>Sep-04<BR>Date<BR>Quantity of Events Per Million EFH<BR>CFM56-7B UER Rate<BR>CFM56-7B IFSD Rate<BR>CFM56-Total IFSD Rate<BR>CFM56-Total UER Rate<BR>CFM56-7B Reliability is similar to total CFM56 fleet<BR>Cleanliness and ball process improvements having<BR>impact on total reliability<BR>5<BR>CFMI Proprietary information<BR>CFM56-7 No 3 Bearing Reliability<BR>No 3 Bearing Events since Entry into Service<BR>• 15 Total UER’s / 5 IFSD’s in 32.44 Million Engine Flight Hours<BR>– Cumulative UER/IFSD Rates – 0.462/0.154 events per MEFH<BR>• Investigation Findings<BR>– Hard Particle Contamination – 6 events<BR>– Ball Skidding – 2 Events<BR>– Winsted Ball Residual Stress – 1 Event<BR>– MRC Ball Cracking – 1 Event<BR>– No Root Cause Established – 3 Events<BR>– Under Investigation – 2 Event<BR>Event Date<BR>Eng<BR>Mod<BR>Prod<BR>or O/H ESN<BR>IFSD<BR>UER<BR>Brg TSN Brg CSN Bearing P/N Brg S/N<BR>Engine<BR>Delivery<BR>Date Last MCDI Oil Type<BR>Winsted<BR>Population<BR>MRC<BR>Population<BR>Investigation Findings<BR>9-May-00 7B Prod 874-618 X 3913 1729 1460M52P03 FCAB2990 Mar-99 Normal MCD Insp Mobil Jet 2 Yes No Hard Particle Contamination<BR>27-Aug-01 7B Prod 875-386 X X 7044 3136 1460M52P03 FCAB3906 Nov-98 DMS System- Did not register chip2s3a8t f0ailure. Yes No No Root Cause Established<BR>17-Dec-01 7B Prod 877-205 X X 3262 4984 1665M98P02 MDAHH822 Jan-00 424H/377C 2380 No No Ball Skidding<BR>1-May-02 7B Prod 889-331 X 3136 3098 1460M50P03 FBGE5245 May-01 Normal MCD Insp Aeroshell 560 No No Ball Skidding<BR>28-May-02 7B Prod 877-419 X 5527 3895 1665M98P02 MDAHN045 Jun-00 Normal MCD Insp Mobil Jet 254 No Yes Ball Cracking - MRC<BR>15-Sep-02 7B Prod 876-663 X X 5249 2262 1460M52P03 FCAC1025 Nov-00 280 Hrs/137 Cyc 2380 No No No Root Cause Established<BR>20-Dec-02 7B Prod 888-278 X 4571 2099 1665M98P02 MDAJC188 Apr-01 Normal MCD Insp No No Hard Particle Contamination<BR>12-Mar-03 7B Prod 888-972 X 2688 1927 1665M98P02 MDAKG935 May-02 Normal MCD Insp MJ254 No Yes Under Investigation - BSD<BR>11-Apr-03 7B Prod 888-639 X 3353 1030 1460M52P03 FCAC9834 Oct-01 Normal MCD Insp MJ2 No No Hard Particle Contamination<BR>28-May-03 7B Prod 874-440 X 17154 7200 1460M52P03 FCAB3897 Nov-98 Normal MCD Insp Yes No Residual Stress<BR>4-Jun-03 7B Prod 889-274 X X 7760 2083 1665M98P02 MDAHY887 Mar-01 Chips generated prior to IFSD MJ2 No No Hard Particle Contamination<BR>29-Jul-03 7B Prod 888-301 X 8549 4824 1665M98P02 MDAJC203 Apr-01 500 hours No No Hard Particle Contamination<BR>10-Sep-03 7B Prod 888-321 X X 8621 2476 1665M98P02 MDAJC232 Apr-01 Not reported No No No Root Cause Established<BR>17-Jun-04 7B Prod 876-635 X 10480 3690 1665M98P02 MDAHN623 Oct-00 500 Hours No No Hard Particle Contamination<BR>22-Aug-04 7B Prod 890-691 X 1354 736 1460M52P03 FCAF6023 Jan-04 294 Hours MJ2 No No Under Investigation<BR>6<BR>CFMI Proprietary information<BR>CFM56-7B No 3 Aft Air/Oil Seal Teflon<BR>Problem/Background:<BR>• Epoxy adhesive used to bond the Teflon<BR>seal onto the Air-Oil seal has suffered<BR>cohesive failures on two high time<BR>CFM56-7B engines<BR>• Review of parts at shop visit does not<BR>indicate this is a wide spread issue<BR>• Analysis indicates that this epoxy<BR>adhesive may not have adequate long<BR>term temperature capability<BR>• CFM has a program to qualify a new<BR>higher temperature adhesive for Teflon<BR>– Expect new adhesive availability 4Q04<BR>• Recommendation – replace Teflon at<BR>next shop visit using current adhesive<BR>until new adhesive is available<BR>– CFM requests customers to report any<BR>findings of loose teflon<BR>7<BR>CFMI Proprietary information<BR>Actions / Plan<BR>• Two new adhesives currently in evaluation<BR>– Back-back comparison to current adhesive<BR>• Room temp and elevated temperatures<BR>• Humidity conditioning<BR>• Fluid resistance<BR>– Test completion in Nov-04<BR>• Go Forward Plan<BR>– Document experience at overhaul shops for all CFM models<BR>– Complete testing of new adhesives<BR>– Complete root cause assessment<BR>– Go fwd decision - target 4Q04<BR>8<BR>CFMI Proprietary information<BR>Actions / Plan<BR>• New Adhesive<BR>– Two new 400 F adhesives currently being tested<BR>• EA9673 (Loctite) and FM2550 (Cytec) being compared to baseline<BR>adhesive<BR>• Adhesives have been assessed at room temperature and 350 F in pristine<BR>condition with equal or better performance versus baseline epoxy<BR>• Humidity conditioning (60 days) of other shear test samples in-process.<BR>Will be ready for testing in late October, 04<BR>• Fluid resistance of new adhesives to be assessed based on supplier data<BR>– All testing will be complete in mid November, 04<BR>– GE EMPIS spec drafted to define new adhesive<BR>• Go Forward Plan<BR>– Document experience at overhaul shops for all CFM models<BR>– Complete testing of new adhesive – 4Q04<BR>– Obtain CFMI Tech Review approval<BR>• Target intro by CID – 4Q04<BR>– Intro new adhesive to ESM repairs – 4Q04回复 1# 航空 的帖子
考试题扫描 :victory: :victory: CFM56 Inlet Gearbox Hardware No 3 Bearing Reliability CFM56-7B Aft Air/Oil Seal
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