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ABS Spar Web Investigation

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ABS Spar Web Investigation. Report to Wichita ACO/ FAA Small Airplane Directorate Wichita, Kansas July 23, 2009. 1. Mandatory Service Bulletins. MSB 2269 issued August 1989 Barons (except 58P and 58TC) Travel Airs MSB 2360 issued November 1990 Bonanzas H35 and later - PowerPoint PPT Presentation
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1 ABS Spar Web ABS Spar Web Investigation Investigation Report to Wichita ACO/ FAA Small Airplane Directorate Wichita, Kansas July 23, 2009 1 ABS-ASF Proprietary Data 7/23/2009
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1

ABS Spar Web ABS Spar Web InvestigationInvestigation

Report to Wichita ACO/

FAA Small Airplane Directorate

Wichita, Kansas

July 23, 2009

1ABS-ASF Proprietary Data 7/23/2009

Mandatory Service BulletinsMandatory Service Bulletins

• MSB 2269 issued August 1989– Barons (except 58P and 58TC)– Travel Airs

• MSB 2360 issued November 1990– Bonanzas H35 and later– All Model 33 Debonairs/Bonanzas – All Model 36 Bonanzas

• Required inspection and repairs

2ABS-ASF Proprietary Data 7/23/2009

Airworthiness Directives

• AD 90-08-14– Incorporates MSB 2269 (multiengine)

• AD 92-08-07– Incorporates MSB 2360 (singe engine)– One time inspection– Required reporting to Beech

• No record of any data

• AD 95-04-03 – Repetitive inspections– No reporting

3ABS-ASF Proprietary Data 7/23/2009

44ABS-ASF Proprietary Data 7/23/2009

Current AD InspCurrent AD Inspectionection

• Initial inspection @1500TT

• No cracks: every 500 hours thereafter

• Small cracks: every 200 hours thereafter

5ABS-ASF Proprietary Data 7/23/2009

66ABS-ASF Proprietary Data 7/23/2009

  Survey Reported %          

Model Responses Cracks Cracked Notes        35 (O/IO-

470) 328 1 0.3% Short body, <3300 MGW    

35 (IO-520) 538 19 3.5% Short body, 3300 MGW or greater  

33 (IO-470) 163 4 2.5% Short body, <3300 MGW    

33 (IO-520) 182 8 4.4% Short body, 3300 MGW or greater  

36 25 4 16.0% Long body, MGW 3600 lbs    

A36 232 30 12.9% Long body, MGW 3600 lbs (3650 lbs 1984 and later)

A36TC 21 0 0.0% Long body, MGW 3600 lbs    

B36TC 21 2 9.5% Long body, MGW 3850 lbs    

Baron 55/56 218 34 15.6% Short body, twin-engine    

Baron 58 41 14 34.1% Long body, twin engine    

95 9 1 11.1% Short body, twin-engine    

ABS Member Survey ABS Member Survey

7ABS-ASF Proprietary Data 7/23/2009

Location of CracksLocation of Cracks

8ABS-ASF Proprietary Data 7/23/2009

9ABS-ASF Proprietary Data 7/23/2009

FAA No-Crack Policy

• The Old Policy– For cracks found in structural components some ADs

have allowed continued operational flight if the cracks are smaller than a certain size.

– Inspection requirements will be more stringent for known cracks.

• The New Policy– Continued operational flight with known cracks in

primary structural components should not be allowed.

– Small Airplane Directorate will adhere to this basic policy.

10ABS-ASF Proprietary Data 7/23/2009

ABS PositionABS Position

• Known issue for two decades

• Current inspection process has ensured ongoing safety

• No history of in-flight failure

• ABS asked FAA for time to investigate

11ABS-ASF Proprietary Data 7/23/2009


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