1967 CHEVROLET CAMARO Chassis Workshop Manual

Page 49 of 659

CHEVROLET CAMARO 1967 1.G Chassis Workshop Manual 
HEATER AND AIR CONDITIONING 1A-26

clockwise for medium and high blower speed, as

desired. Low blower speed is automatic during

cooling operations.

4.
 "Def-Pull". This knob should be pushed fully

Page 50 of 659

CHEVROLET CAMARO 1967 1.G Chassis Workshop Manual 
HEATER AND AIR CONDITIONING 1A-27

POA SUCTION

THROTTLING 
RTJING
 ^EXTERNAL

EQUALIZER LINE

COMPRESSOR

(Operates

continually

while system

is in operation)

M
 H. P.
 VAPOR 
OIL BLEED LINE

SIG

Page 51 of 659

CHEVROLET CAMARO 1967 1.G Chassis Workshop Manual 
HEATER AND AIR CONDITIONING 1A-28

providing a protective film to reduce the possibility

of infection.

3.
 As soon as possible, call or consult an eye specialist

for immediate and future treatment

Page 52 of 659

CHEVROLET CAMARO 1967 1.G Chassis Workshop Manual 
HEATER AND AIR CONDITIONING 1A-29

time as possible will be required to perform the

operation. Dont leave the system open any longer

than is necessary.

• Finally, after the operation has been c

Page 53 of 659

CHEVROLET CAMARO 1967 1.G Chassis Workshop Manual 
HEATER AND AIR CONDITIONING 1A-30

Leak Detector

Tool J-6084 (fig. 43) is a propane gas-burning torch

which is used to locate a leak in any part of the system.

Refrigerant gas drawn into the sampl

Page 54 of 659

CHEVROLET CAMARO 1967 1.G Chassis Workshop Manual 
HEATER
 AND AIR
 CONDITIONING
 1A-31

FIVE
 AMP

TIME DELAY

FUSE

CORD
 TO

110
 AC
 SOURCE 
PUMP

INLET 
PUMP DISCHARGE

OUTLET

Fig.
 44—Vacuum Pump

the use of weighing equipment necessary with

Page 55 of 659

CHEVROLET CAMARO 1967 1.G Chassis Workshop Manual 
HEATER AND AIR CONDITIONING 1A-32

5.
 Check hose clamp connections. If clamp screw torque

is less than 10 lb. in., retighten to 20-25 lb. in. Do

not tighten to new hose specifications or hose leak

Page 56 of 659

CHEVROLET CAMARO 1967 1.G Chassis Workshop Manual 
HEATER AND AIR CONDITIONING 1A-33

within the system. The following fixed conditions must be

adhered to in order to make it possible to compare the

performance of the system being tested with the s