Technically

Technically

Service Bulletin 34-4170: Navigation – Fusion Equipped King Air 200/300 Electronic Standby Instrument System (ESIS) – Magnetometer Relocation Kit

Issued: March 2017

Effectivity: Super King Air Model B200GT, Serial Numbers BY-207, BY-239, BY-250 thru BY-291; Super King Air Model B200CGT, Serial Number BZ-1; Super King Air Model B300, Serial Numbers FL-954, FL-1010, FL-1031 thru FL-1093; Super King Air Model B300C, Serial Numbers FM-66 thru FM-71.

NOTE: No further action is necessary for the following airplanes on which Kit 434-3013 has been accomplished: B200GT, Serial Numbers BY-268 thru BY-276, BY-278 thru BY-286, BY-288 thru BY-291; B300, Serial Numbers FL-1050, FL-1052, FL-1062, FL-1072 thru FL-1074, FL-1076 thru FL-1079, FL-1082 thru FL-1093; B300C, Serial Numbers FM-67, FM-69 and FM-70.

Compliance – Recommended: This service bulletin should be accomplished within the next 200 flight hours, but no later than 24 months, whichever occurs first.

A service bulletin published by Textron Aviation may be recorded as completed in an aircraft log only when the following requirements are satisfied:

  1. The mechanic must complete all of the instructions in the service bulletin, including the intent therein.
  2. The mechanic must correctly use and install all applicable parts supplied with the service bulletin kit. Only with written authorization from Textron Aviation can substitute parts or rebuilt parts be used to replace new parts.
  3. The mechanic or airplane owner must use the technical data in the service bulletin only as approved and published.
  4. The mechanic or airplane owner must apply the information in the service bulletin only to aircraft serial numbers identified in the Effectivity section of the bulletin.
  5. The mechanic or airplane owner must use maintenance practices that are identified as acceptable standard practices in the aviation industry and governmental regulations.

No individual or corporate organization other than Textron Aviation is authorized to make or apply any changes to a Textron Aviation-issued service bulletin, service letter, or flight manual supplement without prior written consent from Textron Aviation.

Textron Aviation is not responsible for the quality of maintenance performed to comply with this document, unless the maintenance is accomplished at a Textron Aviation Authorized Service Center.

Reason: Fusion equipped King Airs experiencing heading errors on their ESIS displays can relocate the ESIS magnetometer from the canted bulkhead to the aft end of the tailcone, per field service kit 434-3013-0001.

This new location will provide enhanced accuracy for the ESIS system.

Description: This service bulletin provides parts and instructions to install field service kit 434-3013-0001. This kit should be installed if magnetometer is located under the panel as defined in step one of the Accomplishment Instructions.

Service Bulletin 30-4166: Ice and Rain Protection – Air Intake – Ram Air Recovery System

Issued: March 2017

Effectivity: Super King Air B200GT, Serial Numbers BY-122, BY-128 thru BY-278 with Raisbeck Engineering Ram Air Recovery System (STC SA3366NM) installed.

The equivalent of this service bulletin has been incorporated on production airplanes BY-279 and On for the brush issue and BY-222 and On for the remainder of issues.

Compliance – Recommended: This service bulletin should be accomplished within the next 200 flight hours or 12 months, whichever occurs first.

A service bulletin published by Textron Aviation may be recorded as “completed” in an aircraft log only when the following requirements are satisfied:

  1. The mechanic must complete all of the instructions in the service bulletin, including the intent therein.
  2. The mechanic or airplane owner must use the technical data in the service bulletin only as approved and published.
  3. The mechanic or airplane owner must apply the information in the service bulletin only to aircraft serial numbers identified in the Effectivity section of the bulletin.
  4. The mechanic or airplane owner must use maintenance practices that are identified as acceptable standard practices in the aviation industry and governmental regulations.

No individual or corporate organization other than Textron Aviation is authorized to make or apply any changes to a Textron Aviation-issued service bulletin, service letter, or flight manual supplement without prior written consent from Textron Aviation.

Textron Aviation is not responsible for the quality of maintenance performed to comply with this document, unless the maintenance is accomplished at a Textron Aviation-owned and Textron Aviation-authorized Service Center.

Reason: This service bulletin is being issued to do a one-time inspection for Textron Aviation-approved factory installed Raisbeck Ram Air Recovery System (RARS) and to verify rigging as required per Raisbeck STC SA3366NM and Raisbeck Engineering Document 93-1021.

Description: This service bulletin provides parts and instructions to inspect the Raisbeck STC SA3366NM installation to verify that parts were installed and rigged properly per STC Installation Document 93-1021 (Installed at Revision F dated December 19, 2007, Revision G dated January 11, 2011, and Revision H dated December 4, 2015). Refer to current Raisbeck installation documentation at www.raisbeck.com.

The above information is abbreviated for space purposes. For the entire communication, go to www.txtavsupport.com.

PWI, Inc. KAR 200 Dimming Issue Service Bulletin

Issued: January 2017

Effectivity: King Air 90, 100, and 200 series

Compliance – Optional: This change is not required as it is a purely aesthetic change.

Reason: This Service Bulletin is being issued to address the concerns of some customers that the KAR 200 dimmer switch does not produce a noticeable change.

Description: This Service Bulletin provides instructions and diagrams that show how to make the KAR 200 dimmer switch create a more noticeable dimming effect. The problem is that, for some customers, the dimmer switch is set at too low of a setting and this can be solved by using a soldering iron to move the wire attached to the middle of the resistor to the far right connector.

Warranty: There is no warranty associated with this Service Bulletin as it is a non-mandated change.

Link: The full service bulletin with exact instructions and pictures for the process can be found at: http://pwi-e.com/wp-content/uploads/2017/02/PWI-Service-Bulletin-02.pdf

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