Piper Comanche PA-24 User Manual

PIPER COMANCHE SERVICE MANUAL
TABLE V·U. TKOUBLESHOOTING OIART (SURFACE CONTROLS) (conL)
Trouble
Rudder pedals not
neuaal when rudder
is sueamlined.
Incorrect rudder
lnvd.
SURFACE CONTROLS
ISSUED: 8/18n2
eaa.
RUDDER CONTROL SYSTEM (cont.)
Rudder
cabin ineOr-
rectly rigcd.
Rudder bcUcrank stop
incorrectly adjusted.
Nose whccl
comacu
stop' before rudder.
IH12
Rcmody
.
Rig in accordance with
Parqraph 5-27.
Rig in accordance with
Parqraph 5-27.
Rig in accordance with
Par&IRph
S·27 .
.

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)