航空 发表于 2011-4-15 19:19:38

CFM Fuel and Oil Filter Delta Pressure Switch

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航空 发表于 2011-4-15 19:19:54

February 2002 WTT face to face CFMI / Boeing Proprietary Information - Unauthorized Disclosure, Use, or Export are Prohibited 1<BR>Fuel and Oil Filter Delta Pressure<BR>Switch<BR>February 2002 WTT face to face CFMI / Boeing Proprietary Information - Unauthorized Disclosure, Use, or Export are Prohibited 2<BR>Fuel and Oil Filter Delta Pressure Switch<BR>Background / Status<BR>Numerous QA07985 field removals  MTBUR = 42,000 Hrs<BR>36 VIN QA07995 units received @ vendor  MTBUR = 54,000 Hrs<BR> Calculation uses total time accumulated by Switches introduced on<BR>production engines only  Very pessimistic<BR> Using time accumulated by all switches delivered to customers<BR> MTBUR &gt; 80,000 Hrs<BR>Reliability Increasing<BR>February 2002 WTT face to face CFMI / Boeing Proprietary Information - Unauthorized Disclosure, Use, or Export are Prohibited 3<BR>Investigations<BR>Old Design : QA07985<BR> 85% removals failure modes corrected in VIN QAO7995<BR>– SB 73-042 issued Jan 2000<BR>– Introduced on aircraft delivered since Mar 2000<BR> 15% with no fault duplicated and assumed to be due to micro-switch<BR>erratic indications due to temperature, and vibrations<BR>New Design : QA07995 - 36 units received @ vendor<BR> 5 units (14%) found with contact resistance value out of ATP limit<BR>– Only one high enough to cause switch disagree fault<BR> 21 units (58%) tested and No Fault Found<BR> No mechanical failure identified<BR> 10 units pending testing<BR>Root Cause Suspected to Be Intermittent Indication<BR>Inherent to Micro-switch Technology<BR>Fuel and Oil Filter Delta Pressure Switch<BR>February 2002 WTT face to face CFMI / Boeing Proprietary Information - Unauthorized Disclosure, Use, or Export are Prohibited 4<BR>Corrective Action<BR>• Aircraft DDG revised to allow for one (1) flight dispatch allowance prior fuel filter<BR>replacement, provided:<BR> Fault verified to be in warning system<BR> No contamination found at filter drain plug<BR>• QA07995 field implementation on-going<BR>• QA07995 failures root cause status<BR> System tests (accelerated life testing ) with harness and EEC card<BR>– Tests completed with 6 field switches but no failure duplicated<BR>• One hermetic and 3 reed switch prototypes passed engineering qualification<BR>tests<BR> Go-ahead decision when current design failure root cause will be<BR>demonstrated<BR>• Switch disagree fault logic change under evaluation<BR> Switch fault to illuminate light at the end of the flight<BR>– No change in the clogging logic<BR> If launched will be implemented in 7BO software expected by end of 2002<BR>Fuel and Oil Filter Delta Pressure Switch<BR>February 2002 WTT face to face CFMI / Boeing Proprietary Information - Unauthorized Disclosure, Use, or Export are Prohibited 5<BR>Background / Status<BR>VIN QA07656 - Same technology as the Fuel Filter DP Switch<BR>• 35 reported oil filter bypass light illumination over last 12 month<BR> 12 cases Switch fault reported, and switch replaced<BR> 13 cases NO switch fault reported, but switch replaced<BR> 8 cases NO switch fault reported, and no switch replacement reported<BR>• 34 occurred on ground / 1 in-flight and ground<BR>• 94 units received @ vendor last 24 month  MTBUR = 90,000 Hrs<BR> 72 with contact resistance values above ATP limit<BR>– 34 high enough to set switch disagree fault<BR>• Additional finding<BR> Crack initiation at red wire solder joint (not separated) on 3 returned units<BR>due to heat shrinkable sleeve being too close to solder<BR>Fuel and Oil Filter Delta Pressure Switch<BR>February 2002 WTT face to face CFMI / Boeing Proprietary Information - Unauthorized Disclosure, Use, or Export are Prohibited 6<BR>Corrective Action<BR>• Switch assembly procedure to be revised to move red wire heat shrinkable<BR>sleeve away from solder<BR> Reduce stress applied to the red wire<BR>• Fuel switch disagree fault logic change may be applied to the oil filter system<BR> Switch Fault to illuminate light at the end of the flight<BR>– No change in the clogging logic<BR> If launched, will be implemented in 7BO software expected by end of<BR>2002<BR>Fuel and Oil Filter Delta Pressure Switch<BR>February 2002 WTT face to face CFMI / Boeing Proprietary Information - Unauthorized Disclosure, Use, or Export are Prohibited 7<BR>Summary<BR>• Fuel filter DP switch new design, and oil filter DP switch reliability<BR>increasing towards expectations<BR>• No short term solutions for remaining FFDPS, and OFDPS erratic<BR>indications/ high contact resistance<BR> Issue inherent to micro-switch technology<BR>• Hermetic and reed switch prototypes could be evaluated if current<BR>design failure root cause demonstrated<BR>• Switch disagree fault logic implementation being evaluated<BR> In 7BO software (if launched) expected by end of 2002<BR>Fuel Filter DP Switch Reliability Increasing<BR>Oil Filter DP Switch Reliability Meeting Expectations<BR>Fuel and Oil Filter Delta Pressure Switch

979199501 发表于 2011-4-16 00:00:47

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Arm
Proposed Switch Configuration
Current Double Throw
Proposed Single Throw
Run contact eliminated
Introduction Logistics
• CFMI/Boeing/Honeywell laun

kinran 发表于 2011-6-4 23:18:46

:victory: :victory:

bocome 发表于 2011-7-31 04:52:11

CFM Fuel and Oil Filter Delta Pressure Switch
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