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AD/PA-44/7 - Nose Cone Spar - Inspection and Modification
1AD/PA-44/7 - Nose Cone Spar - Inspection and Modification
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COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 105 CIVIL AVIATION SAFETY AUTHORITY
SCHEDULE OF AIRWORTHINESS DIRECTIVES
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Piper PA-44 (Seminole) Series Aeroplanes
| AD/PA-44/7 | Nose Cone Spar - Inspection and Modification | 11/80 |
|---|---|---|
| Applicability: | All model PA-44-180 with S/Nos. 44-7995001 to 44-8095021. | |
| Document: | Piper SB No. 695. |
Compliance: 1. Inspect within 50 hours time in service after 15 October 1980 and thereafter at intervals not exceeding 50 hours time in service until modified.
- Modify within 300 hours time in service after 15 October 1980.
Background: The manufacturer has received reports of cracking in the nose cone spar in the area of the nose landing gear upper drag brace attach point.