Piper Aircraft Corporation PA-24-260 Flight Manual

TO 116 BAGIC ALRPLANE FLIGHT June 30, 1965
MANUAL AND KRUT IN TII: AIRPLANE ~ Piper Model PA-24-260
WIEN THE ITEM OF BQULDMENT Equipped with Piper
DESIGNATED BELOW IS INGTALLED. AutoControl II
Normal Category Only
INSTALLATION OF PIPER AUTOCONTROL II (MODEL AKO65-E)
Placards:
WITH ZERO HEADING DIRECTIONAL GYRO INSTALLED
On instrument panel in full view of pllot:
1. For instrument identification on face of D.G.:
"Modified for PiperAutoContrcl"
2. On the control console:
Piper AutoControl II
INSTRUCTIONS
TO ENGAGE: Push Heading Lock button to"OUT"position
Center TURN-TRIM knob. Engage roll,
TO TURN: Move TURN-TRIM knob in desired direction.
FOR HEADING LOCK: Set D.G. at 0°, Uncage. Push
"Heading Lock" Button to "IN" position.
Use TURN-TRIM knob to obtain exact 0°
heading".
DISENGAGE: During take-off and landing.
WITH COURSE SELECTOR DIRECTIONAL GYRO INSTALLED
*¥1., TFor instrument identification on face of D.G.:
*Not applicable when Piper 3" face gyros are installed.
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