Instrument Panel Mounted Clock Removal; Instrument Panel Mounted Clock Installation; Control Wheel Mounted Clock Removal And Installation; Electrical Switches And Circuit Breakers - Piper PA-44-180 SEMINOLE Maintenance Manual

REMOVAL OF INSTRUMENT PANEL MOUNTED CLOCK.
1. Remove power from electric clock circuit.
2. Remove two screws from face of clock that secure clock in panel.
3. Withdraw clock from panel and remove wires from back of clock.
INSTALLATION OF INSTRUMENT PANEL MOUNTED CLOCK.
1. Attach wires to back of clock.
2. Position clock in panel and secure with two screws previously removed.
3. Re-apply power to circuit.
REMOVAL OF CONTROL WHEEL MOUNTED CLOCK.
1. Remove power from electric clock circuit.
2. Disconnect wires at the point where they exit the control wheel tube assembly (behind instrument panel).
Attach a piece of cord of sufficient length to wire connectors to aid in re-routing wire during installation.
3. Remove four screws which secure clock in control wheel and withdraw clock. Disconnect cord from wire
connectors on.clock and allow cord to remain in control wheel tube assembly.
INSTALLATION OF CONTROL WHEEL MOUNTED CLOCK.
1. Attach cord to wire connectors of clock. Using cords to aid in re-routing electrical wiring, insert clock in
control wheel and secure with screws.
2. Remove cords from connectors. Connect wires to appropriate mating wire.
3. Re-apply power to circuit.
4. Refer to Pilot's Operating Handbook for instructions on setting clock.
MULTIPURPOSE ELECTRICAL PARTS.

ELECTRICAL SWITCHES AND CIRCUIT BREAKERS.

The switches are of the rocker type. The switches are mounted on the left side panel. The circuit breakers arc
single hole mounting, push button type with manual reset; they must be reset by the pilot whenever tripped.
They arc on a circuit breaker panel on the lower right hand corner of the instrument panel.
PA-44-180 S/N 44-7995001 thru 44-8195016 and PA-44-180T S/N 44-8107001 thru
44-8107044 refer to latest revision Piper Service Bulletin No. 696.
PIPER AIRCRAFT
PA - 4 4 - 1 8 0 / 1 8 0 T
AIRPLANE MAINTENANCE MANUAL
— Note —
2L4
3 9 - 4 1 - 0 0
Page 39-08
Revised: May 15, 1989