LANDING GEAR - REPLACEMENT OF NOSE LANDING GEAR RETRACT PLUNGER ASSEMBLY

Transcription

1 Beechcraft TITLE: SERVICE BULLETIN LANDING GEAR - REPLACEMENT OF NOSE LANDING GEAR RETRACT PLUNGER ASSEMBLY 1. Planning Information A. Effectivity (1) Airplanes (a) Civil (i) (ii) (b) Military (i) The following serials shall proceed to incorporate this Service Bulletin: Model G36 Bonanza, Serials E-3750 through E-3887; E-3889 through E-3907; Model G58 Baron, Serials TH-2206 through TH-2262 and TH The following models shall review applicable airplane maintenance records before complying with this Service Bulletin: Model 33 Series, Model 35 Series, Model 36 Series, Model 55 Series, Model 56TC, Model 58 Series, Model 95 Series (Travel Air). This Service Bulletin applies to airplanes that have installed Nose Landing Gear (NLG) plunger assembly, P/N , or NLG retract rod assembly, P/Ns or , purchased from Hawker Beechcraft Corporation (HBC) RAPID between December 20, 2006 and July 15, The following military models shall review applicable airplane maintenance records before complying with this Service Bulletin: Model 34C, Model T-34C and T-34C-1. This Service Bulletin applies to airplanes that have installed NLG plunger assembly, P/N , or NLG retract rod assembly, P/N purchased from HBC RAPID between December 20, 2006 and July 15, If you are no longer in possession of the airplane, please forward this information to the present owner. 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 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 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 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. Issued: October, 2009 SB of 12

2 (2) Spares B. Reason SERVICE BULLETIN NLG plunger assembly P/N , or NLG retract rod assembly P/Ns , or purchased from HBC RAPID between December 20, 2006 and July 15, This Service Bulletin is being issued to inform owners/operators of the required replacement of the NLG plunger assembly, P/N Due to an improper braze to the plunger joint during the manufacturing process, the plunger could separate from the push-pull tube during landing gear operation. The NLG could subsequently collapse during landing. HBC issued Safety Communiqué 306 on this subject in August, C. Description NOTE The NLG plunger assembly is common to all airplanes in Paragraph 1.A. Effectivity. However, it is a component of the larger retract rod assembly, which varies by airplane model. Therefore, this Service Bulletin is accomplished by replacing ONLY the NLG plunger assembly P/N within the modelspecific NLG retract rod assembly, P/Ns , or For G36 Bonanza and G58 Baron models, instructions are provided to remove and replace the NLG plunger assembly P/N , which is a component of the NLG retract rod assembly, P/Ns or , located in the NLG wheel well. Removed plunger assemblies, as well as spares inventory, shall be returned to HBC. All other models shall review applicable airplane maintenance records to determine applicability of this Service Bulletin. Replacement of the NLG plunger assembly P/N , which is a component of the NLG retract rod assembly P/Ns , or is performed per appropriate shop or maintenance manual. Removed plunger assemblies, as well as spares inventory, shall be returned to HBC. D. Compliance An Airworthiness Directive will be requested on the matter covered by this Service Bulletin. (1) Civil Airplanes HBC considers this to be a mandatory modification. It must be accomplished as soon as possible after receipt of this Service Bulletin, but no later than the next 50 flight hours or nine (9) calender months, whichever occurs first. (2) Military Airplanes For compliance information on military airplanes affected by this Service Bulletin, contact the appropriate headquarters. Issued: October, 2009 SB of 12

3 E. Approval The engineering data contained in this Service Bulletin is FAA approved. 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 for NLG plunger assembly replacement: 4 hours. Suggested number of men: 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 manhours. G. Weight and Balance Negligible. H. Electrical Load Data Not changed. I. Software Accomplishment Summary Not applicable. J. References HBC Safety Communiqué 306, August 2009, or subsequent revision. Part A Bonanza Series Maintenance Manual (MM), P/N C or subsequent revision, Chapters and ; Bonanza (Model G36) Maintenance Manual Supplement (MMS), P/N B or subsequent revision, Chapter ; Bonanza (G36) Illustrated Parts Catalog (IPC), P/N N or subsequent revision, Chapter 32; Baron Maintenance Manual, P/N G or subsequent revision, Chapters and ; Baron (Model G58) Maintenance Manual Supplement, P/N C or subsequent revision, Chapter ; Baron (G58) Illustrated Parts Catalog (IPC), P/N L or subsequent revision, Chapter 3. Issued: October, 2009 SB of 12

4 Part B Appropriate chapter of the applicable Maintenance Manual, Shop Manual, Technical Order, Job Guide or Illustrated Parts Catalog, Chapter 32. K. Publications Affected None. L. Interchangeability of Parts Not applicable. M. Warranty Credit (1) Civil Warranty credit for labor and parts to the extent noted under MANPOWER and MATERIAL will be allowed on all affected airplanes and spares as specified in Paragraph 2.D. Claims for compliance with this Service Bulletin are to be filed as a W4-type claim against SB Warranty coverage offered in this Service Bulletin will expire nine (9) 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. HBC reserves the right to void continued 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 Department. After the Service Bulletin has been accomplished, a warranty claim must be submitted to HBC within 60 days of the Service Bulletin completion date. NLG plunger assembly P/N , removed from the airplane or from spares inventory, MUST be returned to RAPID at the following address in order to receive warranty credit: Rapid Aircraft Parts Inventory and Distribution Company (RAPID) Attention: Warranty Hold Area 370 N. Webb Road, West Dock, Bldg. 65 Wichita, Kansas Phone: RAPID-44 ( ) or ; FAX: (2) Military For warranty information on military airplanes affected by this Service Bulletin, contact the appropriate headquarters. Issued: October, 2009 SB of 12

5 2. Material Information A. Materials - Price and Availability Contact a Hawker Beechcraft Authorized Service Center for information. B. Industry Support Not applicable. C. Airplanes NOTE The NLG plunger assembly is common to all airplanes in Paragraph 1.A. Effectivity. However, it is a component of the larger retract rod assembly, which varies by airplane model. Therefore, this Service Bulletin is accomplished by replacing ONLY the NLG plunger assembly, P/N within the modelspecific NLG retract rod assembly, P/Ns , or (1) The following parts required for this modification may be ordered through a Hawker Beechcraft Authorized Service Center or RAPID: Part Number Description Quantity Per Airplane NLG Plunger Assembly 1 (2) The following materials may be obtained locally: Part Number Description Quantity Per Airplane MS Pin, Cotter 3 D. Spares Inspect stock for NLG plunger assembly P/N , or NLG retract rod assembly P/Ns , or purchased from HBC RAPID between December 20, 2006 and July 15, ONLY the NLG plunger assembly, P/N , shall be returned to RAPID for replacement. Refer to Section 1. M. Warranty Credit for return information. E. Reidentified Parts None. F. Tooling - Price and Availability Not applicable. Issued: October, 2009 SB of 12

6 3. Accomplishment Instructions SERVICE BULLETIN NOTE The Accomplishment Instructions are presented in two (2) parts. Refer to the section corresponding to the specific model of airplane being modified. This Service Bulletin shall be accomplished as follows: NOTE Should any difficulty be encountered in accomplishing this Service Bulletin, contact Hawker Beechcraft Corporation at or A. Airplane Military airplanes should contact appropriate headquarters for assistance. 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 A - Model 36 and G36 Bonanza, Model 58 and G58 Baron: NOTE Refer to the applicable Illustrated Parts Catalog (IPC) to determine the correct retract rod assembly part number for the specific airplane undergoing maintenance. (1) Model G36 Bonanza and G58 Baron serials shall proceed to incorporate this Service Bulletin. Refer to Paragraph 1.A. to confirm effectivity and proceed to Step (3) below. (2) Models 36 Bonanza and 58 Baron: Review applicable airplane maintenance records to determine if the NLG plunger assembly P/N , or NLG retract rod assembly P/Ns or were purchased from HBC RAPID between December 20, 2006 and July 15, 2009, and installed on the airplane. (a) If it is confirmed that no component replacement was performed during the noted time frame, proceed to Paragraph 3.C. Record of Compliance. (b) If component replacement was performed during the noted time frame, proceed to Step (3) below. (3) Place airplane on jacks. Refer to MM Chapter (Bonanza) or Chapter (Baron). Issued: October, 2009 SB of 12

7 (4) Position nose landing gear for ease of access to the retract rod and plunger assemblies. Refer to applicable MM Chapter , Figure 1, and Figure 2 (Bonanza) or Figure 3 (Baron). (5) Remove all power from the airplane and disconnect the battery per model-specific instructions below. Display warning notices prohibiting reconnection of airplane electrical power. G36 Bonanza: Perform ELECTRICAL POWER - DISCONNECT. Refer to MMS Chapter ; 36 Bonanza: Disconnect batteries. Refer to MM Chapter ; G58 Baron: Perform: ELECTRICAL POWER - DISCONNECT. Refer to MMS Chapter ; 58 Baron: Disconnect batteries. Refer to MM Chapter (6) Gain access to NLG plunger assembly through nose wheel well (Bonanza and Baron) and by removing floorboards under the copilot s rudder pedals (Baron only). Refer to Figures 2 and 3. (7) Remove NLG retract rod assembly. Discard cotter pins but retain other hardware. Refer to Figure 1. Maintenance personnel should be aware that the landing gear retract rod assembly compression spring is under load pressures and injury to personnel or damage to equipment may occur if proper handling is not exercised. (8) Remove plunger assembly from retract rod. Discard cotter pin but retain other hardware. (9) Red tag and return ONLY the removed P/N plunger assembly to HBC for warranty consideration. Refer to Paragraph 1.M. for return address. (10) Replace ONLY the P/N plunger assembly using hardware retained from Step (8) and new cotter pin, P/N MS Refer to applicable MM Chapter , Figure 1, and Figure 2 (Bonanza) or Figure 3 (Baron). (11) Install existing NLG retract rod assembly, including new plunger assembly, using hardware retained from Step (7) and new cotter pins, P/N MS (12) Connect external electrical power per model-specific instructions below: G36 Bonanza: Perform ELECTRICAL POWER - CONNECT. Refer to MMS, Chapter ; 36 Bonanza: Connect batteries. Refer to MM Chapter ; G58 Baron: Perform ELECTRICAL POWER - CONNECT. Refer to MMS, Chapter ; 58 Baron: Connect batteries. Refer to MM Chapter (13) Verify proper rigging of the landing gear system. Refer to the applicable MM, Chapter , Landing Gear - Rigging (Bonanza and Baron). Issued: October, 2009 SB of 12

8 (14) Remove airplane from jacks. Refer to applicable MM, Chapter (Bonanza) or Chapter (Baron). (15) Ensure all work areas are clean and clear of tools and miscellaneous items of equipment. (16) Return airplane to service. (17) Proceed to Paragraph 3.C. Record of Compliance. PART B - Model 33 Series, Model 35 Series, Model 55 Series, Model 56TC, and Model 95 Series (Travel Air); Military Airplanes: Model 34C, Model T-34C, and Model T-34C-1. NOTE Refer to the applicable Illustrated Parts Catalog (IPC) to determine the correct retract rod assembly part number for the specific airplane undergoing maintenance. (1) Review applicable airplane maintenance records to determine if the NLG plunger assembly P/N , or NLG retract rod assembly P/Ns , or were purchased from HBC RAPID between December 20, 2006 and July 15, 2009, and installed on the airplane. (a) If it is confirmed that no component replacement was performed during the noted time frame, proceed to Paragraph 3.C. Record of Compliance. (b) If component replacement was performed during the noted time frame, proceed to Step (2) below. Maintenance personnel should be aware that the landing gear retract rod assembly compression spring is under load pressures and injury to personnel or damage to equipment may occur if proper handling is not exercised. (2) Refer to Figures 1 through 3 and the applicable Maintenance Manual, Shop Manual, Technical Order, or Job Guide for airplane-specific instructions to remove and replace the NLG plunger assembly from the retract rod assembly. Discard cotter pins but retain other hardware. (3) Red tag and return ONLY the removed P/N NLG plunger assembly to HBC for warranty consideration. Refer to Paragraph 1.M. for return address. (4) Install existing NLG retract rod assembly including new plunger assembly using hardware retained from Step (2) above and new cotter pins, P/N MS (5) Verify proper rigging of the landing gear system. Refer to the applicable manual for instructions. (6) Ensure all work areas are clean and clear of tools and miscellaneous items of equipment. (7) Return airplane to service. Issued: October, 2009 SB of 12

9 B. Spares Research records to determine if NLG plunger assembly P/N , or NLG retract rod assembly P/Ns , or were purchased from RAPID between December 20, 2006 and July 15, ONLY the P/N plunger assembly purchased in this time frame shall be red tagged and returned to HBC RAPID for warranty consideration. Refer to Paragraph 1.M. for return address. C. Record of Compliance Upon completion of this Service Bulletin, make an appropriate maintenance record entry. Issued: October, 2009 SB of 12

10 Location of NLG Plunger Assembly Figure 1 Issued: October, 2009 SB of 12

11 Bonanza Access Points for Removal of Retract Rod Assembly in Nose Wheel Well Figure 2 Issued: October, 2009 SB of 12

12 Baron Access Points for Removal of Retract Rod Assembly in Nose Wheel Well Figure 3 Issued: October, 2009 SB of 12