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pdf Gfa ad 438 issue 1 Popular

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gfa ad 438 issue 1.pdf

Gfa ad 438 issue 1

INSPECTION AND MODIFICATION OF THE TAILPLANE LOCKING MECHANISM

Due to a lack of maintenance or wear the locking hook on the tailplane may disengage allowing the tailplane to fall off. Applicable to Standard Cirrus / Standard Cirrus B  S/N 537, 586, 593, 595, 597 to 599 and 601 up; Nimbus-2 S/N 86, 93, 96 and up; Janus and Mini Nimbus HS7: all serial numbers. Schempp-Hirth combined Technical Note No.s: 278-36, 286-33, 295-26, 328-11, 798-3 refer.