35iS/U-07 The brake lines were secured to the gear legs by using the plastic tubing and tie-wraps provided.
38iS/U-11 The gear seal assemblies were reinstalled onto the fuselage.
38iS/U-17 The turnbuckles for the stabilator cables were calibrated by placing the control sticks at a position of 10in away from the control panel and using a tensionmeter to achieve a tension between 35-45 (since the tension should be calibrated at a temperature of 70F and the temperature was actually of 75F-80F, the tension was set at the lower setting of the treshold). The travel of the stabilator was confirmed to be stopped by its stops instead of the control stick stops.
38iS/U-18 Since the tension was already confirmed at that setting, the lock clips were installed. NOTE: The tension will be once again checked before flight testing.
38iS/U-19 The crotch straps and lap belts were installed onto the fuselage, the access covers were also installed.
