Piper Comanche PA-24 User Manual

PIPER COMANCHE SERVICE MANUAL
TABLE V·II. TROUBLESHOOTING CHART (SURFACE CONTROLS) (CODL)
Trouble
Trim indicator fails
to indicate COrT'ect
aim position.
Trim indicator fails
to indicate ilny
movement.
Cause
Remedy
STABILATOR TRIM CONTROL SYSTEM (CDftL)
Trim indicator nOt
properly adjuRed.
Trim indicator wire
broken.
Trim indicator wire
broken.
Broken indicator tension
spri",.
Forward trim puUey
slippinl when
crank
is tIImod.
IH15
-
Adjust in accordance
with Puqraph 5·39
Replace wire.
Replace wire.
Replace spri"l.
Cleek for oil or
grease or loose
cables and tighten
in accordance with
Table V·I.
-.
SURFACE CONTROLS
ISSUED: 8118n2

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)