What was found
(CAN) T/O WAS REJECTED AT APPROX 60/70 KNOTS DUE TO T/O WARNING HORN ASSOCIATED WITH A GPW CAUTION LIGHT AND STICK SHAKER. LT AND RT SQUAT SWITCHES REPLACED. AIRCRAFT TEST FLOWN SATISFACTORY.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
(CAN) T/O WAS REJECTED AT APPROX 60/70 KNOTS DUE TO T/O WARNING HORN ASSOCIATED WITH A GPW CAUTION LIGHT AND STICK SHAKER. LT AND RT SQUAT SWITCHES REPLACED. AIRCRAFT TEST FLOWN SATISFACTORY.