Cessna T182 Series User Manual

MODEL 182 & T182 SERIES SERVICE MANUAL
11-16. STATIC RUN-UP PROCEDURES. In a power loss.
case of suspected low engine power, a static RPM 3. Check magneto timing, spark plugs and
run-up should be conducted as
follows: ignition harness
for settings and condition.
a. Run up engine, using take-off power and
mix- 4. Check condition of induction
air filter. Clean
ture settings, with the aircraft facing 90
°
right and if required.
then
left to the wind direction.
5. Perform an engine compression
check. Refer
b. Record the
RPM obtained in each
run-up posi-
to engine manufacturer's
service manual.
tion.
NOTE
11-17.
REMOVAL.
If
an engine
is to be
placed in
storage or returned to the manufacturer for over-
Daily
changes
in atmospheric
pressure,
haul,
proper
preparatory
steps
should
be taken
for
temperature
and
humidity
will
have a
corrosion
prevention
prior
to beginning
the
removal
slight effect
on
static
run-up.
procedure.
Refer
to Section
2 for
storage
prepara-
tion.
The following engine
removal procedure
is
c. Average the
results of the RPM obtained, it based
upon the engine being removed from the
air-
should be within 50 RPM of 2380 RPM. craft with the engine mount attached to the firewall.
d.
If the average results
of the RPM obtained
are
lower
than stated above,
the following
recommended
NOTE
checks may be performed to determine a possible
deficiency.
Tag each item
when disconnected
to aid in
1. Check governor control
for proper rigging. identifying
wires, hoses, lines and control
It should be determined
that the governor
control
linkages when engine
is reinstalled. Like-
arm travels to the high
RPM stop on the governor and wise,
shop notes made during removal will
that the
high RPM stop screw
is adjusted properly.
often clarify
reinstallation. Protect
open-
(Refer to Section
13 for procedures.
)
ings, exposed
as a result of removing
or
disconnecting
units, against
entry of foreign
NOTE
material by installing
covers or
sealing with
tape.
If verification of governor operation is
necessary, the governor
may be removed a. Place
all cabin switches in the OFF position.
from the engine
and a flat plate installed b.
Place fuel selector valve in the OFF position.
over the engine
pad. Run up engine to
c. Remove
engine cowling
in accordance with para-
determine that
governor was adjusted
graph 11-3.
properly.
d. Disconnect battery
cables and insulate terminals
as a safety precaution.
2. Check carburetor heat control for proper e. Drain fuel strainer and lines with strainer drain
rigging.
If partially open it would cause
a slight control.
SHOP NOTES:
11-10

Cessna T182 Series Specifications

General

Engine Type	Lycoming IO-540-AB1A5
Horsepower	230 hp
Seating Capacity	4
Service Ceiling	18, 100 feet
Takeoff Distance	1, 600 feet
Landing Distance	1, 350 ft
Type	Single-engine
Max Takeoff Weight	3, 100 lb
Wingspan	36 ft
Length	29 ft
Height	9 feet 3 inches
Fuel Capacity	92 US gal (348 L)