CFM Electrical Harnesses
**** Hidden Message ***** February 2002 WTT face to face CFMI / Boeing Proprietary Information - Unauthorized Disclosure, Use, or Export are Prohibited 1<BR>Electrical Harnesses<BR>February 2002 WTT face to face CFMI / Boeing Proprietary Information - Unauthorized Disclosure, Use, or Export are Prohibited 2<BR>Background<BR>• Harness outer metallic braid found damaged at clamp location<BR>Investigation<BR>• Chafing occurred at clamp locations.<BR>• Clamp cushion wear due to vibration and allow harness braid to contact /<BR>wear against clamp<BR>• Issue identified at 6 different clamp locations in core compartment<BR> Most of the time when two branches are in the same clamp<BR>Corrective Action<BR>• New clamps design validated (P/N 649-411-981/990-0)<BR> Includes an additional cushion in between the clamp and the harness<BR> S/B 72-0285 targeted for Mar 2002<BR>Electrical Harnesses<BR>CJ9 / CJ10 Chafing Issue<BR>February 2002 WTT face to face CFMI / Boeing Proprietary Information - Unauthorized Disclosure, Use, or Export are Prohibited 3<BR>Repairs<BR>• On-wing temporary repair<BR> Valid up to harness shop visit<BR> Communicated to airlines through Jan 2001 fleet highlight<BR>• 2 improved on-wing repairs to be introduced in AMM:<BR> 1) Wrapping of the wear external braid with fiberglass insulting tape +<BR>adjunction of a thermal protective metal wire wrapped around the<BR>repaired area<BR>– To be released in AMM Feb 2002 rev.<BR> 2) Adjunction of two half cylindrical shelves secured by the clamps<BR>themselves<BR>– To be released in AMM Jun 2002 rev.<BR>• Shop repair developed<BR> Metallic outer braid or complete branch replacement<BR>– CMM to be updated<BR>Electrical Harnesses<BR>CJ9 / CJ10 Chafing Issue<BR>February 2002 WTT face to face CFMI / Boeing Proprietary Information - Unauthorized Disclosure, Use, or Export are Prohibited 4<BR>Background<BR>• Numerous cases of TCC and T3 intermittent faults in-service<BR>• 60% sensors returned are not confirmed at vendor<BR>• Investigation showed oxidation/pollution on connectors pins side which<BR>could explain the intermittent faults<BR>Investigation<BR>• Deeper analysis shows<BR> Contaminant on pins identified as Si and Al oxides<BR> Pollution from high temperature sheath found on the connector<BR>sockets<BR> Flaking sheath found in backshells<BR> Sheath contain Si and Al oxides<BR>TCC (DAC) / T3 Connector Reliability<BR>Electrical Harnesses<BR>February 2002 WTT face to face CFMI / Boeing Proprietary Information - Unauthorized Disclosure, Use, or Export are Prohibited 5<BR>Pollution entries<BR>Deposit of flake of sheath<BR>High Temp. Sheath<BR>TCC (DAC) / T3 Connector Reliability<BR>Electrical Harnesses<BR>February 2002 WTT face to face CFMI / Boeing Proprietary Information - Unauthorized Disclosure, Use, or Export are Prohibited 6<BR>Corrective Action<BR>• Addition of Viton A heat<BR>shrinkable sleeve on the<BR>sheath<BR> Go-ahead decision<BR>1Q 2002<BR> Prod. intro 3Q 2002<BR>TCC (DAC) / T3 Connector Reliability<BR>Also<BR>• Hermetic connector design under evaluation<BR>Electrical Harnesses<BR>February 2002 WTT face to face CFMI / Boeing Proprietary Information - Unauthorized Disclosure, Use, or Export are Prohibited 7<BR>Background<BR>• Due to HPTACC thermocouple deletion on the SAC engines, the<BR>production harnesses will be modified and the TCC branch will be<BR>deleted from the CJ9 harness.<BR>• Engines with 7BM1 software can either be fitted with<BR> Old harness with TCC sensor OR<BR> Old harness with parking bracket OR<BR> New harness with plugged TCC orifice<BR>Action Plan<BR>• New harness design available.<BR>• New harness supporting Brackets design in process<BR>• Implementation in production targeted for 3Q 2002<BR>TCC Branch Deletion<BR>Electrical Harnesses<BR>February 2002 WTT face to face CFMI / Boeing Proprietary Information - Unauthorized Disclosure, Use, or Export are Prohibited 8<BR>Background<BR>• Wires chafing inside the 90° backshell of DP1102 connector<BR>(customer bleed)<BR>• SB 72-0262 issued 26 Jul 2000<BR> Introduces new improved harness design (P/N 325-029-905-0)<BR> Provides old configuration (P/N 325-029-901/902-0) rework<BR>instructions<BR>• One case of chafing recently reported on other terminal<BR>Actions Plan<BR>• SB to be revised to extend rework capability the others backshells if<BR>needed<BR> Design review in process to verify need/effectiveness vs<BR>connectors<BR>MW0311 Harness Chafing<BR>Electrical Harnesses<BR>February 2002 WTT face to face CFMI / Boeing Proprietary Information - Unauthorized Disclosure, Use, or Export are Prohibited 9<BR>Background<BR>• Component Maintenance Manuals concerning electrical harnesses<BR>have to be updated<BR>• Through WTT Telecon Customers put priority on:<BR> CMM 26-11-02 = Fire Detection Harnesses MW325, MW326<BR> CMM 73-24-03 = Engine Harnesses J5, J6, J7, and J8<BR>• Current plan<BR> CMM 26-11-02 Feb 2002<BR> CMM 73-24-03 Apr 2002<BR>• Overall activity plan targeted Feb 2002<BR>CMM For Harnesses<BR>Electrical Harnesses回复 1# 航空 的帖子
ArmProposed Switch Configuration
Current Double Throw
Proposed Single Throw
Run contact eliminated
Introduction Logistics
• CFMI/Boeing/Honeywell laun :victory: :victory: CFM Electrical Harnesses 好的资料!好的资料! 谢谢楼主 最近急需这些资料:) 好东西,谢谢楼主 看看。。。。。。。。。。。。。。。。。。。。。。。 回复才能看,实在不够意思
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