CFM56-7 Scorecard
**** Hidden Message ***** CFMI PROPRIETARY INFORMATION<BR>ATO Rate<BR>Goal 0.010<BR>Current rate 0.012<BR>ATO Rate<BR>Goal 0.010<BR>Current rate 0.012<BR>Dispatch Reliability<BR>Goal 99.95<BR>Current 99.94<BR>Fleet Statistics<BR>• 12 month rolling average<BR>thru Jan 31<BR>• Air Algerie (4)<BR>• Air Berlin (14)<BR>• Air China (8)<BR>• Air Europa (8)<BR>• Air Pacific (3)<BR>• Alaska (13)<BR>• American (50)<BR>• ARAMCO (3)<BR>• Axon (2)<BR>• Azzura (2)<BR>• Braathens (9)<BR>• Britannia (5)<BR>• BWIA (4)<BR>• Continental (93)<BR>• COPA (6)<BR>• China Airlines (11)<BR>• China Southwest (3)<BR>• China Yunnan (4)<BR>• Delta (38)<BR>• El Al (5)<BR>• Euralair (4)<BR>• Futura (5)<BR>• Germania (14)<BR>• Hainan (7)<BR>• Hapag-Lloyd (20)<BR>• Jet Airways (14)<BR>• KLM (13)<BR>• Korean (8)<BR>• Lauda (4)<BR>• LAPA (8)<BR>• Maersk (8)<BR>• Midway (5)<BR>• Novair (3)<BR>• Pegasus (3)<BR>• RAM (9)<BR>• Ryanair (12)<BR>• Sabre (4)<BR>• Sahara (3)<BR>• SAS (49)<BR>• Shanghai (5)<BR>• Shenzen (3)<BR>• South African (6)<BR>• Southwest (91)<BR>• Sterling (5)<BR>• Sunexpress (4)<BR>• Transavia (10)<BR>• THY (23)<BR>• Tunis (7)<BR>• Varig (5)<BR>• Xiamen (6)<BR>• BBJ (48)<BR>• Others (19)<BR>In-Service and Flight Line Issues<BR>Current month<BR>Previous month<BR>Fleet Experience<BR>Hours: 6,089,214<BR>Cycles: 3,145,614<BR>Engines: 1,555<BR>Aircraft 726<BR>Issue Status<BR>T<BR>• Starter<BR>• HPSOV Switch<BR>• No. 4 bearing<BR>• DAC durability<BR>• Oil/Fuel Delta P Switch<BR>• Fan Blade/Booster Flange/Platform<BR>• LPT Blade (DAC)<BR>• N1 Vibration<BR>• EEC<BR>• Acoustic Panel<BR>• Ignition System<BR>• Ps3 Line “B” Nut Connections<BR>Y<BR>CFM56-7 Scorecard<BR>G<BR>G<BR>Y<BR>G<BR>R<BR>G<BR>Y<BR>Total IFSD Rate<BR>Goal 0.003<BR>Current 0.003<BR>Total ATO Rate<BR>Goal 0.015<BR>Current 0.014<BR>Total SV Rate<BR>Goal 0.100<BR>Current 0.028<BR>Total UER rate<BR>Goal 0.040<BR>Current 0.015<BR>G<BR>Y<BR>Leading Indicators<BR>Issue<BR>HPT Blades<BR>G<BR>Y<BR>CFMI PROPRIETARY INFORMATION<BR>Age Distribution - Hours<BR>0<BR>50<BR>100<BR>150<BR>200<BR>250<BR>300<BR>350<BR>0<BR>50<BR>100<BR>150<BR>200<BR>250<BR>300<BR>350<BR>1000 2000 3000 4000 5000 6000 7000 8000 9000 10000 11000 12000 13000<BR>Number of Engines<BR>ETSN Distribution<BR>CFMI PROPRIETARY INFORMATION<BR>Age Distribution - Cycles<BR>0<BR>50<BR>100<BR>150<BR>200<BR>250<BR>300<BR>350<BR>400<BR>450<BR>500<BR>0<BR>50<BR>100<BR>150<BR>200<BR>250<BR>300<BR>350<BR>400<BR>450<BR>500<BR>1000 2000 3000 4000 5000 6000 7000 8000 9000<BR>Number of Engines<BR>ECSN Distribution<BR>CFMI PROPRIETARY INFORMATION<BR>IFSD Rate<BR>CFM56-7 IFSD Rate<BR>0.000<BR>0.010<BR>0.020<BR>0.030<BR>0.040<BR>0.050<BR>0.060<BR>0.070<BR>0.080<BR>0.090<BR>199712<BR>199802<BR>199804<BR>199806<BR>199808<BR>199810<BR>199812<BR>199902<BR>199904<BR>199906<BR>199908<BR>199910<BR>199912<BR>200002<BR>200004<BR>200006<BR>200008<BR>200010<BR>200012<BR>IFSD per 1K hours<BR>120 Minute ETOPS Criteria<BR>Basic 12 Month Rolling Average<BR>Total 12 Month Rolling Average<BR>180 Minute ETOPS Criteria<BR>CFMI PROPRIETARY INFORMATION<BR>IFSD Causes - Total Last 12 Months<BR>Cause Quantity Corrective Action<BR>#4 Bearing 3 MCD Inspection - SB 72-180<BR>New outer race material - 4th Qtr 01<BR>Maintenance error 3 N/A<BR>Ps3 Line 2 Short term plan to triple torque in Prod<BR>Long term plan is to introduce lock wire in Prod<BR>Starter 1 Improved Gear Design - October 99<BR>S/Bs 80-004, 80-005 issued<BR>HPT blade 1 No Root Cause Established<BR>Oil Temperature Sensor 1 Over-torque root cause: redesign insert<BR>for improved durability<BR>Oil Temperature Indication 1 No Root Cause Established<BR>Fuel Filter Rotation 1 Boeing issued fleet inspection recommendation<BR>Incorrect o-ring installed prior to delivery. CFMI<BR>has standardized Viton as o-ring for all CFM56<BR>CFMI PROPRIETARY INFORMATION<BR>Aborted Takeoff Rate<BR>CFM56-7 ATO Rate<BR>0.000<BR>0.005<BR>0.010<BR>0.015<BR>0.020<BR>0.025<BR>0.030<BR>0.035<BR>0.040<BR>199712<BR>199802<BR>199804<BR>199806<BR>199808<BR>199810<BR>199812<BR>199902<BR>199904<BR>199906<BR>199908<BR>199910<BR>199912<BR>200002<BR>200004<BR>200006<BR>200008<BR>200010<BR>200012<BR>ATOper dep.<BR>Basic 12 mo Rolling<BR>Total 12 mo Rolling<BR>CFMI PROPRIETARY INFORMATION<BR>Aborted Takeoff Causes - Last 12 months<BR>Cause Quantity Corrective Action<BR>Data for basic rate:<BR>MSV position fault 2 EEC/HMU replaced - Root caused not<BR>established<BR>HPC IGV Lever Arm 1 Field inspected engines vertically side<BR>cased at Shop. Assy aids incorporated<BR>in production.<BR>Fuel Filter DP 1 Introduced FFDP with potting in<BR>connector housing , SB 73-042<BR>issued<BR>HPT Blade 1 HPT blade failure - Under investigation<BR>Fuel Pump 1 Failure to attain T/O power - under<BR>investigation<BR>Data for total rate:<BR>Bird strike 3 N/A<BR>Eng Cont Light 2 No Fault Codes reported<BR>Maintenance 1 N/A<BR>Operation 1 Runway excursion<BR>CFMI PROPRIETARY INFORMATION<BR>Shop Visit Rate<BR>CFM56-7 Total Shop Visit Rate<BR>0.000<BR>0.010<BR>0.020<BR>0.030<BR>0.040<BR>0.050<BR>0.060<BR>0.070<BR>0.080<BR>199712<BR>199802<BR>199804<BR>199806<BR>199808<BR>199810<BR>199812<BR>199902<BR>199904<BR>199906<BR>199908<BR>199910<BR>199912<BR>200002<BR>200004<BR>200006<BR>200008<BR>200010<BR>200012<BR>Shop Visits per 1K hours<BR>12 Month Rolling Average<BR>CFMI PROPRIETARY INFORMATION<BR>Shop Visit Causes - Total engine Last 12 months<BR>Cause Quantity Corrective Action<BR>LPT Blade 60 DAC unique. Control actions in place.<BR>Maintenance 11 N/A<BR>HPC Blade 8 Clearances adjusted, top case and blending repairs in place<BR>FOD/Other 6 N/A<BR>#4 Bearing 5 MCD Inspection - SB 72-180, New outer race material 4th Qtr 01<BR>Core vibration 2 Top case core balance procedure developed.. Rotor stack improvements<BR>incorp’d into production.<BR>Volcanic ash 2 N/A<BR>HPT Blade separation 2 In-investigation<BR>HPC IGV bridged 1 One time inspection of engines vertically top cased at shop. Assy aids connector mis-Assy<BR>incorporated in production. Affected field population inspected<BR>TEO sensor 1 Over-torque root cause: Redesign inserts for additional robustness. TEO<BR>system logic to be revised in next S/W revisionto preclude invalid oil pressure indication.<BR>Oil Leak 1 Aft sump oil supply leak - Assy error<BR>VBV Pad disbonndment 1 N/A<BR>Combustor distress 1 Under investigation<BR>Metal in HPT 1 HPT air manifold spalsh plate --- CFM56-7 S/B 72-167<BR>Air manifold<BR>FWD sump 1 Under Investigation<BR>Oil leak<BR>CFMI PROPRIETARY INFORMATION<BR>CFM56-7 Dispatch Reliability<BR>99.70<BR>99.75<BR>99.80<BR>99.85<BR>99.90<BR>99.95<BR>100.00<BR>199712<BR>199802<BR>199804<BR>199806<BR>199808<BR>199810<BR>199812<BR>199902<BR>199904<BR>199906<BR>199908<BR>199910<BR>199912<BR>200002<BR>200004<BR>200006<BR>200008<BR>200010<BR>200012<BR>Successful Departures<BR>12 Month Rolling Average<BR>CFMI PROPRIETARY INFORMATION<BR>Delay and Cancellation Top Causes<BR>(basic engine last 12 months)<BR>Cause Quantity Corrective Action<BR>DAC LPT Blade Program 101 Control action to BSI vibration shifts.<BR>Corrective actions being developed.<BR>HMU:<BR>- HPSOV 48 SB 73-037R2 issued, Allows A/L to R/R sw<BR>- FMV 22 Phase II resolver incorp’d in prod/rwk P07<BR>Fuel delta pressure switch 50 Potted switch improvement S/B 73-042<BR>Boeing proposing 1 flight allowance to DDPG MMEL<BR>PALL offering discount on switch upgrade<BR>Ignition System 29 Ignition hardware shows no anomolies<BR>(not confirmed) Power switching relay planned for Aircraft incorp.<BR>HPTACC Valve 25 Improved LVDT S/B 75-002. TCC thermocouple<BR>deletion 2nd Qtr 01<BR>Oil delta P switch 23 Manufacturing improvements incorporated<BR>EEC 21 PSS modification. Improved ATP in place.<BR>Program improvements being monitored.<BR>N1 Vibration 17 Vibration Maint. Action published - CESM 007<BR>issued<BR>Starter 12 Gear and oil catcher upgrade S/B s issued<BR>N2 Speed Sensor 7 SB 72-259 issued.<BR>CFMI PROPRIETARY INFORMATION<BR>CFM56-7B Revenue Service Status<BR>Entry into service December 1997<BR>Operators/aircraft in service 98/726<BR>Cumulative engine hours/cycles 6,089,214/<BR>3,145,614<BR>Daily utilization hours/cycles 9.5/4.9<BR>Average flight leg 1.93<BR>High time engines: hours/cycles 12,500 / 8,333<BR>Total SVR (per 1,000 EFH) .024<BR>Total IFSD rate (per 1,000 EFH) .003<BR>Dispatch reliability 99.94<BR>Data as of January 2001<BR>Meeting or Exceeding Reliability Goals回复 1# 航空 的帖子
CFM56-7 Starter Reliability 楼主很好!! :victory: :victory: CFM56-7 Scorecard 资料好珍贵啊
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