AD/P68/20 Amdt 1 - Flap Bellcrank Attachment Mounting Brackets - Inspection and Modification
1AD/P68/20 Amdt 1 - Flap Bellcrank Attachment Mounting Brackets - Inspection and Modification
Start here
Get a plain-English read of 1
Turn the raw legal text into a practical explanation grounded in AD/P68/20 Amdt 1 - Flap Bellcrank Attachment Mounting Brackets - Inspection and Modification.
COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 105 CIVIL AVIATION SAFETY AUTHORITY
SCHEDULE OF AIRWORTHINESS DIRECTIVES
Image unavailable in extracted text
Partenavia P68 Series Aeroplanes
AD/P68/20
Amdt 1
Flap Bellcrank Attachment Mounting Brackets - Inspection and Modification
3/83
Applicability: All models P68, P68B, P68C, P68C-TC and P68 observer aircraft with S/Nos. to 277. Document: Partenavia SB 56. Note: R.A.I. AD No. 82-228/P68-27 Rev. 1 refers.
Compliance: 1. Unless already accomplished, inspect within 10 hours time in service after 22 September, 1982 for aircraft with more than 500 hours time in service.
- Repeat inspection at intervals not exceeding 100 hours time in service until modified.
Modify within 500 hours time in service after 31 March, 1983.
Background: Cracks in the area of the bellcrank attachment hole have been reported.
This AD has been amended to reference the service bulletin and modification requirements.