Scorecard/Fleet Experience
**** Hidden Message ***** CFMI PROPRIETARY INFORMATION<BR>Data through December 2001<BR>Scorecard/Fleet Experience<BR>CFMI PROPRIETARY INFORMATION<BR>Data through December 2001<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: 10,741,308<BR>Cycles: 5,582,418<BR>Engines: 2,137<BR>Aircraft 1,004<BR>Issue Status<BR>• HPSOV Switch<BR>• Oil/Fuel Delta P Switch<BR>• Fan Disk<BR>• Platform Aft Pin<BR>• LPT Blade (DAC)<BR>• N1 Vibration - Flight Line<BR>• EEC<BR>• HPT Blades<BR>• HMU - FMV<BR>• AGB - N2 hand cranking pad gear<BR>• MSV position faults<BR>• N2 Tone - Flight Line<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 0.028<BR>Total SV Rate<BR>Goal 0.100<BR>Current 0.024<BR>Total UER rate<BR>Goal 0.040<BR>Current 0.015<BR>Issue Leading Indicators<BR>Booster Spool FWD Flange Wear<BR>VBV Guide Pad Delamination<BR>Booster Abradable Corrosion<BR>Fan Platform Life<BR>LPT2 Nozzle Cracking<BR>R<BR>G<BR>G<BR>Y<BR>Y<BR>R<BR>G<BR>G<BR>G<BR>Y<BR>Y<BR>R<BR>CFMI PROPRIETARY INFORMATION<BR>Data through December 2001<BR>• Air Algerie (7)<BR>• Air Berlin (24)<BR>• Air China (7)<BR>• Air Europa (12)<BR>• Air Pacific (3)<BR>• Alaska (21)<BR>• Aloha (5)<BR>• Amiri Flight (4)<BR>• American (76)<BR>• American Transair (14)<BR>• ARAMCO (5)<BR>• Axon (2)<BR>• Azzura (2)<BR>• Braathens (11)<BR>• Britannia (5)<BR>• BWIA (6)<BR>• City Bird (3)<BR>• Continental (116)<BR>• COPA (8)<BR>• China Airlines (9)<BR>• China Southwest (7)<BR>• China Wuhan (2)<BR>• China Yunnan (3)<BR>• Delta (61)<BR>• Easyjet (9)<BR>• El Al (5)<BR>• Euralair (6)<BR>• Futura (7)<BR>• Germania (10)<BR>• GOL Transportes (7)<BR>• Hainan (7)<BR>• Hamburg Intl (3)<BR>• Hapag-Lloyd (27)<BR>• Helios Airways (2)<BR>• Jet Airways (19)<BR>• Kibris (3)<BR>• KLM (17)<BR>• Korean (15)<BR>• Lauda (6)<BR>• LAPA (8)<BR>• Maersk (7)<BR>• Mandarin (3)<BR>• Midway (10)<BR>• North American (2)<BR>• Novair (3)<BR>• Pegasus (11)<BR>• RAM (9)<BR>• Ryanair (17)<BR>• Sahara (3)<BR>• SAS (53)<BR>• Shanghai (6)<BR>• Shenzen (6)<BR>• South African (14)<BR>• Southwest (115)<BR>• Sterling (6)<BR>• Suncountry (6)<BR>• Sunexpress (6)<BR>• TAROM (3)<BR>• Transaero (2)<BR>• Transavia (14)<BR>• THY (25)<BR>• Tunis (8)<BR>• US Navy (4)<BR>• Varig (7)<BR>• Virgin Blue (6)<BR>• Westjet (4)<BR>• Xiamen (6)<BR>• Xinjiang (5)<BR>• BBJ (62)<BR>• Others (23)<BR>737-6/-7/-8/-900 Customers and Fleet Size<BR>CFMI PROPRIETARY INFORMATION<BR>Data through December 2001<BR>Age Distribution - Hours<BR>0<BR>50<BR>100<BR>150<BR>200<BR>250<BR>0<BR>50<BR>100<BR>150<BR>200<BR>250<BR>Number of Engines<BR>ETSN Distribution<BR>CFMI PROPRIETARY INFORMATION<BR>Data through December 2001<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 December 2001<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>Data through December 2001<BR>IFSD Causes - Total Last 12 Months<BR>Cause Quantity Corrective Action<BR>Oil Temperature Sensor 4 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 (3 failures in 10 million Flt hours)<BR>Ps3 Line 1 Safety wire introduced to production engines -<BR>June 01, and SB 72-333 introduces lock wire at<BR>shop visit. Safety wire provisions introduced into<BR>EEC SB 73-062R1<BR>No 4 brg Suspect 1 New outer race material 1st Qtr 02<BR>Radial Drive Shaft 1 Under Investigation<BR>Separation<BR>Starter Failure (P08) 1 Under Investigation - Turbine bearing failure<BR>Engine Controls 1 EEC PSS flex failure CH B (CFMSB 73-0065) along with a VSV<BR>out of range fault on CH B of the HMU<BR>Engine controls 1 HMU under investigation - Eng. Stuck at 85% N1<BR>Data for total rate:<BR>Lightening strike 1 Under investigation - DFDR and EEC received<BR>Maintenance error 1 IDG not properly secured after IDG replacement<BR>Oil filter bypass 1 Chips in oil filter … previous starter failure - AMM improvements<BR>FOD - Bird Strike 1 No Active Program<BR>CFMI PROPRIETARY INFORMATION<BR>Data through December 2001<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 Aborted Takeoff Causes - Last 12 monththsrough December 2001<BR>Cause Quantity Corrective Action<BR>Data for basic rate:<BR>MSV position fault 8 Cell 58 testing continues. Solenoid driver output not enough<BR>to activate solenoid under certain conditions. Containment<BR>and improvement options being defined<BR>Eng Control light 4 Fleet highlights published, maintenance hand book<BR>(No faults recorded) developed to aid mtc im FMC-CDU interrogation<BR>TBV Position fault 3 Under Investigation<BR>Oil/fuel Filter DP 2 New FFDP design P/N QA7995 field penetration<BR>progressing .. further mechanical switch improvements being<BR>evaluated<BR>HMU - FMV 2 Product improvements for 12 of 13 known issues<BR>Evaluating revising EEC SW fault logic from 2 to 4<BR>degrees to alleviate position & signal disagree faults<BR>HPT Blade 1 HPT blade Airfoil separation - Telemetry Test completed -<BR>Evaluating the results<BR>Eng Control light 1 HPTACC TC fault - 7.B.M1 SB 73-064 Issued<BR>Fuel Pump 1 Failure to attain T/O power - Fuel pump fault confirmed<BR>HMU - No response to 1 Manufacturing defect in HMU’s shutoff shuttle valve<BR>thrust lever input<BR>Data for total rate:<BR>Bird strike 4 N/A<BR>Operation 2 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 Ref regulator improvements in work - 2nd qtr 2002<BR>CFMI PROPRIETARY INFORMATION<BR>Data through December 2001<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>Shop Visit per 1K hours<BR>12 Month Rolling Average<BR>CFMI PROPRIETARY INFORMATION<BR>Data Shop Visit Causes - Total engine Last 12 montthhrsough December 2001<BR>Cause Quantity Corrective Action<BR>LPT Blade 42 DAC unique. Control actions in place. New blade 2Qtr 02<BR>Proactive No 4 brg removal 14 Bearings from suspect lot of 47<BR>Maintenance 9 N/A<BR>FOD/Other 6 N/A<BR>HPT Blade Evaluation 6 Sampling program to evaluate HPT blade shank cracks<BR>Fan Disk replacement 5 CESM 005 and S/B 72-253 issued, New AMM limits issued<BR>TEO sensor 4 Redesign inserts for additional robustness. TEO system logic revised in S/W 7.B.M1 - SB 72-064 to<BR>preclude invalid oil pressure indication. Field containment for housing issued 72-A336<BR>VBV Pad disbondment 3 Bonding process improvement incorp’d into production. EEC software improvements 2 Qtr 02<BR>No. 3 Bearing 2 No active program<BR>No. 4 Bearing 2 MCD Inspection - SB 72-180, New outer race material 1st Qtr 02<BR>Combustor distress 2 Secondary swirler material loss - Under investigation<BR>AGB hand cranking pad 2 In investigation<BR>brg<BR>HPT Blade separation 1 In-investigation, telemetry test scheduled Oct 2001<BR>Core vibration 1 Top case core balance procedure developed.. Rotor stack improvements<BR>incorp’d into production.<BR>Oil Leak 1 Oil leak into fan disk and booster - Assy error<BR>Metal in HPT 1 HPT air manifold spalsh plate --- CFM56-7 S/B 72-167<BR>Air manifold<BR>HPC stg 4 blade lock 1 Assembly error. Assembly planning to require set screw drop measurement.<BR>separation<BR>Fan abradable shroud 1 Attributed to quality issue - audit & corrective actions complete<BR>dsibondment<BR>Fan Blade Platform 1 Fan blade platform pin undertorqued<BR>No 1 brg 1 Under Investigation<BR>CFMI PROPRIETARY INFORMATION<BR>Data through December 2001<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>UERs per 1k hours<BR>CFMI PROPRIETARY INFORMATION<BR>Data through December 2001<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>Successful Departures<BR>12 Month Rolling Average<BR>CFMI PROPRIETARY INFORMATION<BR>Data Delay and Cancellation Top Causesthrough December 2001<BR>(basic engine last 12 months)<BR>Cause Quantity Corrective Action<BR>HMU:<BR>- FMV 42 Under investigation<BR>- HPSOV 45 SB 73-067 to issue Feb 02 - Introduces SPST switch<BR>Ignition System 40 Ignition lead/exciter ... no anomalies<BR>Power switching relay available for Aircraft incorp.<BR>Soft time recommendation not acknowledged<BR>Utilize improved EEC S/W troubleshooting capability<BR>Fuel delta pressure switch 30 Potted switch improvement S/B 73-042<BR>1 flight allowance added to DDPG MMEL<BR>PALL offering discount on switch upgrade<BR>Starter 30 50 % oil leaks and 50 % mechanical failures<BR>EEC 21 PSS modification SB 73-065. Improved ATP in place.<BR>Program improvements being monitored<BR>Oil delta P switch 20 Under Investigation<BR>N1 Vibration 19 Vibration Maint. Action published - CESM 007<BR>issued<BR>Engine Control light 13 Under Investigation - Need airline FDR data<BR>(No Fault Codes)<BR>HPTACC Valve 10 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 December 2001<BR>CFM56-7B Revenue Service Status<BR>Entry into service December 1997<BR>Operators/aircraft in service 115/1004<BR>Cumulative engine hours/cycles 10,741,308/<BR>5,582,418<BR>Daily utilization hours/cycles 9.5/4.9<BR>Average flight leg 1.92<BR>High time and cycle engines: hours/cycles 16,326 / 10,324<BR>Total SVR (per 1,000 EFH) .024<BR>Total IFSD rate (per 1,000 EFH) .003<BR>Dispatch reliability 99.96<BR>Meeting or Exceeding Reliability Goals回复 1# 航空 的帖子
CFM56-7B TRAINING MANUAL ENGINE FAN TRIM BALANCE :victory: :victory: Scorecard/Fleet Experience
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