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SERVICE BULLETIN SB 28-3967

Beechcraft G36 Bonanza · Service Bulletins

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Overview

This Service Bulletin (SB 28-3967) issued by Hawker Beechcraft Corporation in June 2009 addresses a mandatory inspection related to the Beechcraft G36 Bonanza. It specifically targets certain serial numbers of the G36 Bonanza, detailing the need to inspect the P60/J60 electrical connector, associated wiring, and fuel line for potential chafing that could lead to fuel leaks. The bulletin emphasizes the importance of compliance within a specified timeframe to ensure safety and airworthiness. It provides instructions for inspection and corrective actions, as well as information on warranty coverage for the work performed. This document is crucial for owners and operators of the affected aircraft to maintain safety standards and comply with regulatory requirements.

  • Mandatory inspection for Beechcraft G36 Bonanza within 10 flight hours or 6 months.
  • Inspect P60/J60 electrical connector and fuel line for chafing.
  • Replace damaged components if chafing is found during inspection.
  • Estimated man-hours: 1 hour for inspection, 2 hours for chafe protection installation, 3 hours for fuel line replacement.
  • Warranty credit available for compliance, expiring 6 months after issuance.

Document

Source

Originally published by download.aopa.org. Sprinkle hosts a reference copy with an added summary, specifications and searchable full text.

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Document details

Type
Service Bulletins
Year
2009
Pages
8
File size
725 KB
Publisher
download.aopa.org
How rare is it?
1Beechcraft G36 Bonanza registered worldwide · 0 active

Common. Rarer than 24% of the aircraft models we track.

Documentation completeness
4/7

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In this document

Effectivity

The Service Bulletin applies to Beechcraft G36 Bonanza aircraft with serial numbers E-3630, E-3636 through E-3817, E-3819 through E-3834, E-3836 through E-3887, E-3889 through E-3896, E-3898, and E-3899.

Reason

The bulletin warns that pilots should not take off if there is a fuel odor in the cockpit or fluid present on the floor. It instructs operators to investigate any fluid presence and land as soon as practical if erratic instrument readings occur.

Description

An inspection is required for the P60/J60 electrical connector and associated wiring, as well as the fuel line, to ensure proper clearance and installation of protective insulating tubes. If chafing is found, damaged components must be replaced.

Compliance

Compliance with this Service Bulletin is mandatory and must be completed within 10 flight hours or six calendar months from receipt, whichever comes first.

Manpower

Estimated man-hours for the inspection are 1 hour, with an additional 2 hours for installing chafe protection and 3 hours if a new fuel line is needed. It is suggested that one person perform the inspection.

Warranty Credit

Warranty coverage for labor and parts is available for compliance with this Service Bulletin, expiring six months from the issuance date.

Safety notes

  • Do not take off if fuel odor is present in the cockpit.
  • Investigate any fluid presence in the cockpit immediately.

Full document text

1 of 8 SERVICE BULLETIN MANDATORY SB 28-3967 Issued: June, 2009 The export of these commodities, technology or software are subject to the U.S. Export Administration Regulations. Diversion contrary to U.S. law is prohibited. For guidance on export control requirements, contact the Commerce Department's Bureau of Export Administration at http://www.bis.doc.gov. Hawker Beechcraft Corporation (HBC) issues Service Information for the benefit of owners and fixed base operators in the form of two classes of Service Bulletins. The first class, Mandatory Service Bulletins (red border) includes changes, inspection and modifications that could affect safety or crashworthiness. HBC also issues Service Bulletins with no red border which are designated as either recommended or optional in the compliance section within the bulletin. In the case of recommended Service Bulletins, HBC feels the changes, modifications, improvements or inspections will benefit the owner/operator and although highly recommended, Recommended Service Bulletins are not considered mandatory at the time of issuance. In the case of Optional Service Bulletins, compliance with the changes, modifications, improvements or inspections is at the owner/operator's discretion. Both classes are available on the web at http://pubs.hawkerbeechcraft.com and mailed to: (a) Owners of record on the FAA Aircraft Registration Branch List and the HBC Safety of Flight Information (SOFI) List. (b) Those having a publications subscription. Information on Safety of Flight Information (SOFI) or subscription can be obtained through the Hawker Beechcraft Corporation Technical Manual Distribution Center (TMDC). As Mandatory Service Bulletins and Service Bulletins are issued, the Service Bulletin Master Index will be updated and available online at http://pubs.hawkerbeechcraft.com. Warranty will be allowed only when specifically defined in the Service Bulletin and in accordance with HBC Warranty Policy. Unless otherwise designated, HBC Mandatory Service Bulletins, Service Bulletins and HBC Kits are approved for installation on HBC airplanes in original or HBC modified configurations only. HBC Mandatory Service Bulletins, Service Bulletins and Kits may not be compatible with airplanes modified by STC installations or modifications other than HBC approved kits. Beechcraft 1. Planning Information A. Effectivity (1) Airplanes Model G36 Bonanza, Serials E-3630, E-3636 through E-3817, E-3819 through E-3834, E-3836 through E-3887, E-3889 through E-3896, E-3898 and E-3899. If you are no longer in possession of the airplane, please forward this information to the present owner. (2) Spares None. B. Reason Owners / operators shall not take off if fuel odor is present in the cockpit or evidence of fluid is present on the floor forward of the pilot’s seat. Investigate fluids in the inspection area to ensure no fuel has leaked into the cockpit. If either condition is noted during flight, land as soon as practical at a suitable airport. If erratic instrument readings are encountered, follow procedures listed in the Model G36 Bonanza Pilot’s Operating Handbook/ Airplane Flight Manual, Section 3 Emergency Procedures and Section 3A Abnormal Procedures. This Service Bulletin is being issued to inspect for and, if found, correct an improper installation of the P60 / J60 electrical connector, associated wiring, and fuel line. Contact between the fuel line and electrical components may cause damage to the fuel line, up to and including leakage. Safety Communiqué 303 was issued on this subject in April of 2009. TITLE: FUEL - INSPECTION FOR CHAFING OF ELECTRICAL CONNECTOR AND ASSOCIATED WIRING ON FUEL LINE SERVICE BULLETIN Issued: June, 2009 SB 28-3967 2 of 8 MANDATORY C. Description An inspection is performed on the P60 / J60 electrical connector [part numbers (P/N) 207019-1 / 207020-1, respectively], associated wiring, and fuel line (P/N 36-920001-13) to verify that proper clearance exists between the components and that the protective insulating tube is installed on the proper section of the fuel line. If chafing is found, damaged components are replaced and positive clearance is established. D. Compliance An Airworthiness Directive will be requested on the matter covered by this Service Bulletin. Hawker Beechcraft Corporation (HBC) considers this to be a Mandatory Service Bulletin. It must be accomplished within the next 10 flight hours or six (6) calendar months from receipt of this Service Bulletin, whichever occurs first. E. Approval The engineering data contained in this Service Bulletin is FAA approved. Prior to accomplishment, owners / operators of airplanes registered in countries other than the United States shall consult with their local Aviation Regulatory Authority. Incorporation of this Service Bulletin restores the airplane to original type design. F. Manpower The following information is for planning purposes only: Estimated man-hours to perform inspection: 1 hour. Estimated man-hours to install chafe protection: 2 hours. Estimated additional man-hours to install new fuel line, if required: 3 hours. Suggested number of men to perform inspection / maintenance: 1 man. The above is an estimate based on experienced, properly equipped personnel complying with this Service Bulletin. Occasionally, after work has started, conditions may be found that could result in additional man- hours. G. Weight and Balance None. H. Electrical Load Data Not changed. SERVICE BULLETIN Issued: June, 2009 3 of 8 SB 28-3967 MANDATORY I. Software Accomplishment Summary Not applicable. J. References Safety Communiqué 303 dated April, 2009; Bonanza Series Maintenance Manual (MM) P/N 36-590001-9B2 or subsequent revision, Chapter 20-06-00; Advisory Circular (AC) 43.13-1B, Paragraph 8-31. K. Publications Affected None. L. Interchangeability of Parts Not applicable. M. Warranty Credit

Show full text

Warranty credit for labor and parts to the extent noted under MANPOWER and MATERIAL will be allowed on all affected airplanes. Warranty coverage offered in this Service Bulletin will expire six (6) months from the last day of the month this Service Bulletin is issued. After that date, the owner / operator assumes the responsibility for compliance cost. Hawker Beechcraft Corporation (HBC) reserves the right to void warranty coverage in the area affected by this Service Bulletin until the date the Service Bulletin is accomplished by an HBC Authorized Service Center (ASC). All warranty work must be accomplished by an HBC ASC rated to perform maintenance on the specific model of Hawker Beechcraft airplane. The HBC ASC will submit the appropriate paperwork directly to HBC Warranty for parts and labor to the extent noted under Section 1.M. Warranty Credit for warranty consideration. The owner / operator should contact an HBC ASC to schedule the work to be accomplished. In the event that work will not be accomplished at an HBC ASC, parts may be purchased directly from RAPID and a warranty claim for parts only should be submitted directly to HBC Warranty. After the Service Bulletin has been accomplished, a warranty claim must be submitted to HBC within 60 days of the Service Bulletin completion date. 2. Material Information A. Materials - Price and Availability Contact a Hawker Beechcraft Authorized Service Center for information. SERVICE BULLETIN Issued: June, 2009 SB 28-3967 4 of 8 MANDATORY B. Industry Support Not applicable. C. Airplane The following parts required for this modification may be ordered through a Hawker Beechcraft Authorized Service Center or RAPID: D. Spares Not applicable. E. Reidentified Parts None. F. Tooling - Price and Availability Not applicable. 3. Accomplishment Instructions This Service Bulletin shall be accomplished as follows: NOTE Should any difficulty be encountered in accomplishing this Service Bulletin, contact Hawker Beechcraft Corporation at 1-800-429-5372 or 316-676-3140. Observe all Warnings and Cautions contained in the airplane manuals referenced in this Service Bulletin. Whenever any part of this system is dismantled, adjusted, repaired or renewed, detailed investigation must be made on completion to make sure that distortion, tools, rags or any other loose articles or foreign matter that could impede the free movement and safe operation of the system are not present, and that the systems and installations in the work area are clean. Part Number Description Quantity Per Airplane HT1/2T Spiral Wrap As Required 207019-1 P60 Electrical Connector As Required 207020-1 J60 Electrical Connector As Required 36-920001-13 Fuel Line As Required SERVICE BULLETIN Issued: June, 2009 5 of 8 SB 28-3967 MANDATORY (1) Remove all power from the airplane and disconnect the battery. Display warning notices prohibiting reconnection of airplane electrical power. (2) Gain access to inspection area, which is aft of the firewall and forward of the pilot’s instrument panel on the left side. Refer to Figure 1. (3) Just aft of the firewall and forward of the instrument panel on the pilot’s side, inspect fuel line P/N 36-920001-13, P60 / J60 electrical connector and associated wiring for damage as a result of chafing. (4) Make the following determinations: (5) Install items removed in Step (2) to gain access to inspection area. (6) Reconnect the airplane battery, remove warning notices and restore power. (7) Ensure all work areas are clean and clear of tools and miscellaneous items of equipment. (8) Return airplane to service. IF: THEN: The fuel line, connector or associated wiring is damaged. Replace fuel line if damaged. Replace or repair damaged wiring (Refer to AC 43-13-1B, Chapter 11). Replace connector if damaged. Ensure fuel line, electrical connectors and associated wiring are secure and have a minimum of 0.50-inch separation. The fuel line has factory protective insulating tube properly installed (starting at the firewall and continuing for a minimum of 10.50 inches past the first bend in the fuel line). Refer to Figure 2. No damage to the fuel line, electrical connector or associated wiring. Ensure fuel line, electrical connectors, and associated wiring are secure and have a minimum of 0.50-inch separation. The fuel line does not have factory protective insulating tube properly installed and there is no damage to the fuel line, electrical connector, or associated wiring. Install spiral wrap P/N HT1/2T on the fuel line in the location depicted in Figure 2. Ensure fuel line, electrical connectors, and associated wiring are secure and have a minimum of 0.5-inch separation. NOTE If fuel line is already protected with approved chafe protection, it is not necessary to add spiral wrap. SERVICE BULLETIN Issued: June, 2009 SB 28-3967 6 of 8 MANDATORY A. Spares Not applicable. B. Record of Compliance Upon completion of this Service Bulletin, make an appropriate maintenance record entry. SERVICE BULLETIN Issued: June, 2009 7 of 8 SB 28-3967 MANDATORY View Looking Up and Outboard from Above Pilot’s Rudder Pedals Figure 1 SERVICE BULLETIN Issued: June, 2009 SB 28-3967 8 of 8 MANDATORY B396703.AI A DETAIL A WL 0.0 10.50 INCHES FIREWALL 106242-6 INSULATING TUBE FORWARD Fuel Line with Insulation Tube Installed During the Manufacturing Process Figure 2