Piper Comanche PA-24 User Manual

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PIPER COMANCHE SERVICE MANUAL
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FIGURE 6-22. LANDING GEAR WARNING SWITCH INSTALLATION
6-60. Landing Gear Warning Switch. (Refer to Figure 6-22.)
6-61. Removal
Of Landing Gear Warning Switch.
a. On airplanes with Serial Nos. 24-1 to 24-4782 inclusive. 24-4784 to 24-4803 inclusive and
PA-24-400. remove the landing gear warning micro switch. located on the throttle shaft forward of the
instrument panel.
by removing attaching nuts. washers and screws.
b. Disconnect the electrical leads at the micro switch.
c. On airplanes with Serial Nos. 24-4783. 24-4804 and up. remove the landing gear warning micro
switch. located in the throttle quadrant. by the following procedure:
I. Remove the left trim cover from the throttle quadrant by removing attaching screws.
2. Remove switch mounting nuts. washers and screws.
3. Disconnect the electrical leads at the micro switch.
6-62. Installation
Of Landing Gear Warning Switch.
a. On airplanes with Serial Nos. 24-1 to 24-4782 inclusive. 24-4784 to 24-4803 inclusive and
PA-24-400. install micro switch by the following procedure:
I. Connect electrical leads to micro switch.
2. Install actuator and micro switch on mounting bracket and secure with screws. lockwashers
and nuts.
3. Adjust switch per Paragraph 6-63.
b. On airplanes with Serial Nos. 24-4783. 24-4804 and up. install micro switch by the following
procedure:
I. Connect electrical leads to micro switch.
ISSUED: 8/18/72
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LANDING GEAR AND BRAKE SYSTEM

Piper Comanche PA-24 Specifications

General

Manufacturer	Piper Aircraft
Model	Comanche PA-24
Type	Light aircraft
First Flight	May 24, 1956
Number Built	4, 857
Seating Capacity	4
Engine	Lycoming O-360
Wingspan	36 ft (11 m)
Length	24 ft 8 in (7.5 m)
Stall Speed	62 mph (100 km/h, 54 kn)
Height	7 ft 6 in (2.3 m)