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    You must be signed in to access this content.Various Aircraft/Engine 2-303-914-01 Packing Shelf Life

    Product Group: Engines (ME)

    Problem: Customer requires Shelf life for Packing 2-303-914-01
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    You must be signed in to access this content.BK117 Helicopter LTS 101-750-B1 Turbine P/N: 4-141-290-18 S/B LT101-72-50-00-0121.

    Product Group: Engines (ME)

    Problem: What Honeywell Service Bulletin Authorizes the Installation of Turbine Turbine Rotor Part Number: 2-141-290-18?
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    You must be signed in to access this content.Avro RJ85 LF507-1F Engine, Interchangeability of Igniter PN 2-300-732-05 and Element PN 2-303-431-01

    Product Group: Engines (ME)

    Problem: On a Avro RJ85 LF507-1F Engine (EIPC 507F.3, sub section 74-00-00), is Igniter PN 2-300-732-05 interchangeable with PN 2-300-732-04 as listed in IPC?  And, listed in EIPC 507F.3, sub section 79-00-00, is Element PN 2-303-431-01 interchangeable with PN 2-303-431-02?
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    You must be signed in to access this content.CL300 AS907-1-1A Spiral Wrap (Chafe Protection) P/N 2-300-519-01

    Product Group: Flight Controls (EL)

    Problem: Is there an alternate part number for (chafe protection) Spiral Wrap P/N 2-300-519-01?
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    You must be signed in to access this content.Boeing B737NG CMM 21-43-01 Revision Status for Thermal Switch Assembly PN 3000-46-2

    Product Group: Air & Thermal Management Systems (ME)

    Problem: What is the latest revision status of Honeywell CMM 21-43-01 for the Boeing B737NG Thermal Switch Assembly PN 3000-46-2?  It is not available on the Honeywell Tech Pubs portal.
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    You must be signed in to access this content.TPE331-5-252M-252D, Speed Switch, PN 3053954-2-X Configuration OHM 74-30-01

    Product Group: Engines (ME)

    Problem: I have a question on the correct technical data to use to overhaul a 305394-2. The manual being specified on your website is 74-30-01 rev 3 dated Dec 11, 1981. I have this manual but it only gives effective codes for the 305394-2-1, 305394-2-2 and the 305394-2-3. The speed switch I have does not have a second dash number. It is marked 305394-2 J. How can I determine the what the second dash number is?
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    You must be signed in to access this content.AD 88-14-01 Compliance

    Product Group: Engines (ME)

    Problem: How do I comply with AD 88-14-01 on LTS101-700D2 engine?
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    You must be signed in to access this content.Boeing 767 - Nose Wheel PN 2606735 - NDT inspection - Item 2.6 of temporary Revision 32-2 of CMM 32-43-01

    Product Group: Wheels & Brakes (WB)

    Problem: Clarification on item 2.6 in temporary Revision 32-2 of CMM 32-43-01 is required
    The item 2.6 in the page 5 of 6 was revised. 
    NDT needs to be performed at every tire change or only when required?
    The tubewell ID will call out a visual inspection at both tire change and overhaul and if any defects are found during this visual inspection, NDT inspection will be required to verify. 
    In other words, NDT inspection is required only when the verification is required. 
    Is our undersntanding correct? 
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    You must be signed in to access this content.Airbus A350 Air Management System Training Questions (BOMU PN 51090012-01 and ASCU PN 51090014-01)

    Product Group: Electric Power System (ME)

    Problem:

    ATA 21 and 36 Questions:
    1) Are BAS and BAM both able to provide data to CDS and who is the prime used by the CDS?
    2) What happen if BAS failed, which Data will be provided then by BAM? 
    3) What is the X-Talk CAN-Bus for in-between EBAS and BOMU? 
    4) If the HP Valve fails OPEN why does the MPV not take over to regulate the pressure until next landing of the AC automatically? 
    5) Will be the TM1 and 2 Data be supplied to both the BAS and BOMU to be used as a backup or will the units provide the data via the above mentioned X-Talk CAN-Bus 
    6) In single Pack operation with both engine bleed systems running and a reverse flow is detected, why does not the X-Bleed close automatic. It must be closed by the flight crew after receiving a caution failure message as far as I know?! 
    7) What is the SIS Connector used for on the front panel of the ASCU and CDM controller? 
    8) If both flow sensors fail in flight or on ground does the pack flow control valve behave always the same (go to full OPEN)? 
    9) Why is the Trim Air PRSOV not controlled from both ASCUs instead of only ASCU 1? 
    10) What is the detailed described reason for the Flow Divider Solenoid to be operated only on ground at specific percentage of APU speed? 

     
     
     
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    You must be signed in to access this content.Airbus A350 Flow Sensor P/N 51090032-00 vs -01 Interchangeable

    Product Group: Air & Thermal Management Systems (ME)

    Problem: We have a query concerning differences between the 2 dash numbers of Sensor P/N 51090032-00, i.e. -00 vs -01.

    The Airbus AIPC states that  -00 and -01 are not interchangeable. 
     
    Why are the two dash numbers cannot be used interchangeably.
     
     
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    You must be signed in to access this content.KI 825 difference between SW level 01 and 03

    Product Group: Flight Management Systems(BK)

    Problem: Customer wanted to know what features and or changes were made to SW level 03, and it he needed the update. 
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    You must be signed in to access this content.A330/A340 - GTCP331-350C APU - Repair of Upper Inlet Duct Assy PN 3810646-2

    Product Group: Auxilary Power Units (ME)

    Problem: During compliance of SB No. GTCP331-49-7723, the customer tried sourcing the Graphite Cloth No. G-171-50 that was mentioned in the SB but the supplier and also Honeywell do not recognize the part number. Customer asked for help in getting the correct part number.
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    You must be signed in to access this content.Boeing 737 - APU 131-9B - Wiring Harness CMM 49-11-01

    Product Group: Auxilary Power Units (ME)

    Problem:

    Often, operators of B737 APU 131-9B ask what is the part number of the backshell or connector on the wiring harness as it's not the Engine Illustrated Parts Catalogue?  

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    You must be signed in to access this content.Multiple Applications - Roller / Ball Bearing Inspections Per SPM 20-00-02/70-00-01

    Product Group: Engine Accessories (ME)

    Problem: We got two new part number of bearings from our customers: PN 3613703-1 and 3613704-1, can we inspect it according to Hwl SPM 20-00-02/70-00-01?
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    You must be signed in to access this content.Multiple Platforms - SATCOM MCS 6000/ 7000/ 7200 - Fault code CD 0 81/01

    Product Group: Communication, Navigation, Surveillance (EL)

    Problem:

    We see fault code CD 0 81/01 PP/CM SMPM SDU TOTC AUTO/MANUAL RESET in the logs, what does it mean ? Does it indicate a failure or fault?

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