航空 发表于 2011-4-12 11:09:21

CFM56-7 Scorecard Data through April 2002

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航空 发表于 2011-4-12 11:10:00

CFMI PROPRIETARY INFORMATION<BR>Data through April 2002<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 99.96<BR>Fleet Statistics<BR>• 12 month rolling<BR>average<BR>In-Service and Flight Line Issues<BR>Current month<BR>Previous month<BR>Fleet Experience<BR>Hours: 12,662,532<BR>Cycles: 6,589,450<BR>Engines: 2,333<BR>Aircraft 1,096<BR>Issue Status<BR>• Oil/Fuel Delta P Switch<BR>• Fan Disk<BR>• Platform Aft Pin<BR>• N1 Vibration - Flight Line<BR>• EEC<BR>• HPT Blades<BR>• HMU - FMV<BR>• MSV position faults<BR>• EEC Ram Corruption<BR>• VBV Guide Pad Delamination<BR>CFM56-7 Scorecard<BR>Total IFSD Rate<BR>Goal 0.003<BR>Current 0.003<BR>Total ATO Rate<BR>Goal 0.020<BR>Current 0.029<BR>Total SV Rate<BR>Goal 0.100<BR>Current 0.026<BR>Total UER rate<BR>Goal 0.040<BR>Current 0.014<BR>Leading Indicators<BR>Booster Abradable<BR>Vane Corrosion<BR>LPT2 Nozzle Cracking<BR>AGB axial link (spherical bearing)<BR>Y<BR>Y<BR>Y<BR>Y<BR>R<BR>G<BR>G<BR>Y<BR>Y<BR>Y<BR>CFMI PROPRIETARY INFORMATION<BR>Data through April 2002<BR>• Air Algerie (7)<BR>• Air Berlin (25)<BR>• Air China (7)<BR>• Air Europa (13)<BR>• Air Pacific (3)<BR>• Alaska (21)<BR>• Aloha (5)<BR>• Amiri Flight (4)<BR>• American (76)<BR>• American Transair (18)<BR>• ARAMCO (3)<BR>• Braathens (11)<BR>• Britannia (5)<BR>• BWIA (6)<BR>• City Bird (3)<BR>• Continental (122)<BR>• COPA (8)<BR>• China Airlines (9)<BR>• China Southwest (7)<BR>• China Wuhan (2)<BR>• China Yunnan (3)<BR>• Delta (68)<BR>• Easyjet (10)<BR>• Excel (7)<BR>• El Al (5)<BR>• Euralair (6)<BR>• Futura (7)<BR>• Germania (10)<BR>• GOL Transportes (14)<BR>• Hainan (7)<BR>• Hamburg Intl (3)<BR>• Hapag-Lloyd (27)<BR>• Helios Airways (2)<BR>• Jet Airways (20)<BR>• Kibris (3)<BR>• KLM (17)<BR>• Korean (17)<BR>• Lauda (6)<BR>• LAPA (8)<BR>• Maersk (9)<BR>• Mandarin (3)<BR>• Midway (7)<BR>• Novair (3)<BR>• Pegasus (12)<BR>• Qantas (5)<BR>• RAM (9)<BR>• Ryanair (19)<BR>• Sahara (4)<BR>• SAS (53)<BR>• Shanghai (9)<BR>• Shenzen (8)<BR>• South African (16)<BR>• Southwest (118)<BR>• Sterling (6)<BR>• Suncountry (6)<BR>• Sunexpress (6)<BR>• TAROM (2)<BR>• Transaero (2)<BR>• Transavia (11)<BR>• THY (25)<BR>• Tunis (7)<BR>• US Navy (4)<BR>• Varig (7)<BR>• Virgin Blue (10)<BR>• Westjet (5)<BR>• Xiamen (7)<BR>• Xinjiang (4)<BR>• BBJ (67)<BR>• Others (33)<BR>737-6/-7/-8/-900 Customers and Fleet Size<BR>CFMI PROPRIETARY INFORMATION<BR>Data through April 2002<BR>Age Distribution - Hours<BR>0<BR>50<BR>100<BR>150<BR>200<BR>250<BR>300<BR>0<BR>50<BR>100<BR>150<BR>200<BR>250<BR>300<BR>Number of Engines<BR>ETSN Distribution<BR>CFMI PROPRIETARY INFORMATION<BR>Data through April 2002<BR>Age Distribution - Cycles<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>Number of Engines<BR>ECSN Distribution<BR>CFMI PROPRIETARY INFORMATION<BR>Data through April 2002<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>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 MonDtahtasthrough April 2002<BR>Cause Quantity Corrective Action<BR>Oil Temperature Sensor 3 Redesign insert incorp’d in production (88T-481)<BR>June 01, Field containment issued SB 72-A336<BR>TEO system logic revised in - SB 72-064 (S/W<BR>7.B.M1) to preclude invalid oil pressure indication<BR>Fleet plan defined: Rework or replace at shop visit<BR>No 3 brg 2 No active program<BR>No 4 brg 2 New outer race material 3 rd Qtr 02<BR>Radial Drive Shaft 1 Root cause not found; Closed<BR>Separation<BR>Starter Failure (P08) 1 Turbine thrust bearing - one case since EIS<BR>Engine Controls 1 EEC PSS flex failure CH B (CFMSB 73-0065) along with a VSV<BR>out of range fault on CH A of the HMU<BR>Engine controls 1 Eng. remained at at 85% N1 when commanded to idle - EEC RA<BR>Corruption - S/W version 7.B.O to introduce accommodation<BR>Control Alternator 1 Control alternator cover crack - oil loss (Could not be duplicated in<BR>lab testing - 1 occurrence in 13,000 alternators.<BR>AGB Hand Cranking Brg 1 Under investigation, awaiting findings<BR>Data for total rate:<BR>Lightening strike 1 Engine stalled due to lightening induced airflow disruption<BR>Pilot cut fuel to engine.<BR>FOD - Bird Strike 1 No Active Program<BR>DMS Detector 1 DMS detector not completely engaged: Spool valve o-ring<BR>damaged<BR>Maintenance 1 Hand cranking pad not installed - Oil loss<BR>CFMI PROPRIETARY INFORMATION<BR>Data through April 2002<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>ATOper 1000 departures.<BR>Basic 12 mo Rolling<BR>Total 12 mo Rolling<BR>CFMI PROPRIETARY INFORMATION<BR>Data through April 2002<BR>Aborted Takeoff Causes - Last 12 months<BR>Cause Quantity Corrective Action<BR>Data for basic rate:<BR>MSV position fault 8 Dual current software approach S/W 7.B.N July 02<BR>Eng Control light (-2) 3 Fleet highlights published, maintenance hand book<BR>(No faults recorded) developed to aid mtc with FMC-CDU interrogation<BR>TBV Position fault 3 EHSV design improvements incorp’d 4th Qtr 02; S/W<BR>Accommodation being considered<BR>Fuel Filter DP 1 New FFDP design P/N QA7995 field penetration<BR>progressing .. further mechanical switch improvements being<BR>evaluated. Software accommodation under consideration<BR>HMU - FMV 1 Corrective action for 11 out of 12 failure modes defined<BR>Rotor winding improvements 4th Qtr 02<BR>Eng Control light 1 HPTACC TC fault - 7.B.M1 SB 73-064 Issued<BR>Oil Pressure Sensor 1 Under Investigation<BR>HMU - No response to 1 Manufacturing defect in HMU’s shutoff shuttle valve<BR>thrust lever input Population capped; approved plan to inspect at HMU shop visit<BR>N2 Overspeed indication 1 N2 Speed Sensor replaced<BR>Fan Blade Platform 1 Fan blade platform pin torque check SB to issue July 2002;<BR>Repetitive re-torque under-consideration<BR>Data for total rate:<BR>Bird strike (1) 4 N/A<BR>Operation 6 N/A<BR>Fumes in cabin - Mtnc 2 N/A<BR>HPC Blade Lock liberation 1 Assembly error: preventive actions in place<BR>A/C system APU Fumes 1 N/A<BR>CTAI Valve (1) 4 Ref regulator improvements in work - 2nd qtr 2002<BR>Misc A/C Indications 3 Thrust Reverser, Speed Brake, Cargo Door<BR>Yaw During Take Off Roll 1 Left MLG Brake did not release<BR>CFMI PROPRIETARY INFORMATION<BR>Data through April 2002<BR>Shop Visit Rate<BR>CFM56-7 Total Shop Visit Rate<BR>0<BR>0.01<BR>0.02<BR>0.03<BR>0.04<BR>0.05<BR>0.06<BR>0.07<BR>0.08<BR>199712<BR>199803<BR>199806<BR>199809<BR>199812<BR>199903<BR>199906<BR>199909<BR>199912<BR>200003<BR>200006<BR>200009<BR>200012<BR>200103<BR>200106<BR>200109<BR>200112<BR>200203<BR>Shop Visit per 1K hours<BR>12 Month Rolling Average<BR>CFMI PROPRIETARY INFORMATION<BR>Data through April 2002<BR>Shop Visit Top Causes - Total engine Last 12 months<BR>Cause Quantity Corrective Action<BR>LPT Blade 46 DAC unique. Control actions in place. New blade 3rd 02<BR>Proactive No 4 brg removal 8 Bearings from suspect lot of 47<BR>Maintenance 6 N/A<BR>FOD/Other 7 N/A<BR>HPT Blade<BR>Blade Evaluation 5 Sampling program to evaluate HPT blade shank cracks<BR>Trailing edge cracks (2) 7 SB 72-115 R1 issued to retire P05 blades at first shop visit. SB 72-326<BR>recommends a 1000 cycle BSI interval<BR>HPT blade TE (1) 3 Manufacturing process change (new core dies) - Identification of<BR>airfoil material loss population in process.<BR>HPT Blade separation 1 Telemetry testing on-going<BR>Fan Disk replacement 5 CESM 005 and S/B 72-253 issued. Testing planned for expand limits<BR>further<BR>TEO sensor 3 Redesign insert incorp’d in production (88T-481) June 01, Field<BR>containment issued SB 72-A336 TEO system logic revised in - SB 72-<BR>064 (S/W 7.B.M1) to preclude invalid oil pressure indication Fleet plan<BR>defined: Rework or replace at shop visit<BR>VBV Pad disbondment 4 EEC software improvements 3 Qtr 02 (7.B.N). Exploring mechanical<BR>fastening since failure in non-suspect population occurred<BR>AGB hand cranking pad (1) 4 Population defined. Imbalance in grinding tool root cause. Bearing<BR>replacement at shop visit - SB brg issued<BR>No. 3 Bearing 3 No active program<BR>No. 4 Bearing 3 New outer race material 3rd Qtr 02<BR>Fan Blade Platform (1) 4 Fan blade platform pin torque check SB to issue July 2002; Repetitive<BR>re-torque under-consideration<BR>CFMI PROPRIETARY INFORMATION<BR>Data through April 2002<BR>Total Unscheduled Engine Removals<BR>CFM56-7B Unscheduled Engine Removals<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>199803<BR>199806<BR>199809<BR>199812<BR>199903<BR>199906<BR>199909<BR>199912<BR>200003<BR>200006<BR>200009<BR>200012<BR>200103<BR>200106<BR>200109<BR>200112<BR>200203<BR>UERs per 1k hours<BR>CFMI PROPRIETARY INFORMATION<BR>Data through April 2002<BR>CFM56-7 Dispatch Reliability<BR>99.700<BR>99.750<BR>99.800<BR>99.850<BR>99.900<BR>99.950<BR>100.000<BR>199712<BR>199803<BR>199806<BR>199809<BR>199812<BR>199903<BR>199906<BR>199909<BR>199912<BR>200003<BR>200006<BR>200009<BR>200012<BR>200103<BR>200106<BR>200109<BR>200112<BR>200203<BR>Successful Departures<BR>12 Month Rolling Average<BR>CFMI PROPRIETARY INFORMATION<BR>Delay and Cancellation Top CauseDasta through April 2002<BR>(basic engine last 12 months)<BR>Cause Quantity Corrective Action<BR>HMU: 1st QTR MTBUR up to 14,000 hours<BR>- HPSOV 67 Field program underway - No switch faults<BR>- FMV 42 Corrective action for 11 out of 12 failure modes defined<BR>Rotor winding improvements 4th Qtr 02<BR>- TBV 27 EHSV design improvements incorp’d 4th Qtr 02; S/W<BR>Accommodation being considered<BR>- MSV 12 Dual current software approach (3Q’02)<BR>Ignition System 43 Ignition lead/exciter ... no anomalies<BR>Power switching relay available for Aircraft incorp.<BR>Soft time recommendation not universally incorp’d<BR>Utilize improved EEC S/W troubleshooting capability - Fleet<BR>Highlights published Feb 02<BR>Starter 37 P09 introduction July 02 - Carbon Seal (in-service leakage<BR>allowance in work); P10 - turbine stack improvements Sept 02<BR>EEC 29 PSS modification SB 73-065. Improved ATP in place.<BR>Program improvements being monitored<BR>Fuel delta pressure switch 27 Potted switch improvement S/B 73-042<BR>1 flight allowance added to DDPG MMEL<BR>PALL offering discount on switch upgrade<BR>Software accommodation under consideration<BR>Oil delta P switch 22 Under Investigation<BR>N1 Vibration 16 Vibration Maint. Action published - CESM 007<BR>issued<BR>Engine Control light 14 Fleet highlights published, maintenance hand book developed<BR>(No fault code) to aid mtc with FMC-CDU interrogation<BR>HPTACC Valve 11 Improved LVDT S/B 75-002. TCC thermocouple<BR>input eliminated in EEC S/W 7.B.M1 - SB 73-064<BR>CFMI PROPRIETARY INFORMATION<BR>Data through April 2002<BR>CFM56-7B Revenue Service Status<BR>Entry into service December 1997<BR>Operators/aircraft in service 115/1096<BR>Cumulative engine hours/cycles 12,662,532/<BR>6,589,450<BR>Daily utilization hours/cycles 9.5/4.9<BR>Average flight leg 1.88<BR>High time and cycle engines: hours/cycles 17,687 / 11,020<BR>Total SVR (per 1,000 EFH) .026<BR>Total IFSD rate (per 1,000 EFH) .003<BR>Dispatch reliability 99.96<BR>Meeting or Exceeding Reliability Goals

doxingpu 发表于 2011-4-12 11:31:19

CFM56-7 Scorecard Data through April 2002

979199501 发表于 2011-4-12 14:20:21

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kinran 发表于 2011-6-4 23:36:55

:victory: :victory:

bocome 发表于 2011-7-31 04:22:41

CFM56-7 Scorecard Data through April 2002
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