AD 48-39-01

Active

Control Stick Rework

Key Information
48-39-01
Active
Not specified
Not specified
Unknown
N/A
Applicability
["Aircraft"]
["Small Airplane"]
American Champion Aircraft Corp.
7AC 7ACA 7BCM (Army L-16A) 7CCM (Army L-16B) 7DC 7EC 7ECA 7FC 7GC 7GCA 7GCAA 7GCB 7GCBA 7GCBC 7HC 7JC 7KC 7KCAB S7AC S7CCM S7DC S7EC
Regulatory Text

48-39-01 AERONCA: Applies to All Model 7 Series Aircraft.

To be accomplished as soon as possible but not later than November 1, 1948.

Inspect front and rear control stick socket castings, P/N 2-705, for cracks at the ears to which the push-pull tube attaches. If found cracked, the castings should be replaced. To prevent future failures the bolt, nut and washer now installed are to be replaced with a clevis bolt, AN 24- 16 (11/16 grip) and an AN 320-4 shear nut so that excessive loads cannot be placed on the socket ears.

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References
This information is not available.
--- - Part 39
FAA Documents