AD/SWSA226/38 Amdt 1 - Elevator Return Spring Location - Modification
1AD/SWSA226/38 Amdt 1 - Elevator Return Spring Location - 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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Fairchild (Swearingen) SA226 and SA227 Series Aeroplanes
AD/SWSA226/38
Amdt 1
Elevator Return Spring Location - Modification
1/82
Applicability: 1. All model SA-226-AT with S/Nos. AT-001 to AT-999. All model SA-226-TC with S/Nos. TC-201 to TC-999.
- All model SA-227-AT with S/Nos. AT-423 to AT-469. All model SA-227-AC with S/Nos. AC-420 to AC-473.
Document: 1. Fairchild Swearingen SB No. 27-032.
- Fairchild Swearingen SB No. 27-002.
Note: FAA AD 81-ASW-39 Amdt. 39-4238 refers.
Compliance: Unless already accomplished, modify before 1 March 1982.
Background: Relocation of the elevator return spring is necessary to prevent jamming of the elevator control in the event of inflight failure of the spring. This amendment extends applicability by aircraft models and S/Nos.