Cj1 Procedures

Front 1

Before Start Check

Back 1

1. Preflight Inspection
2. Wheel Chocks REMOVED
3. Cabin Door CLOSE AND LOCK 5 green indicators
4. Passenger Briefing COMPLETE
5. Seats, Seat Belts, Shoulder Harnesses, and Rudder Pedals
6. Fuel Quantity CHECKED
7. Flashing Beacon ON
8. Air Conditioner OFF

Front 2

Engine Start Check

Back 2

1. Flood and Center Panel Lights.FULL BRIGHT (FOR NIGHT OPERATIONS)
2. Start ButtonPRESS BUTTON LIGHTS
3. Throttles IDLE AT 8-12% (N2) AND FAN (N1) RPM
4. ITT RISE in 10 sec.(975<7.5 sec)
5. Engine Instruments NORMAL
6. Fuel, Oil, Generator, and Hydraulic Annunciators EXTINGUISHED
7. Other Engine START; REPEAT STEPS 2 THRU 6
During generator cross starts, both start buttons illuminate indicating that both start relays are closed.
8. External Power CHECK CLEAR (IF APPLICABLE)
9. Generators GEN (IF EXTERNAL POWER WAS USED FOR START)
10. DC Amperes and Volts CHECK
a. LH Gen OFF Check LH AMP drop, RH AMP INCR, voltage 29 ± 0.25
b. RH Gen OFF Check RH AMP drop, Check voltage drop to battery voltage (24 volts minimum).
c. LH Generator GEN Check on line (AMPS INCR, voltage 29 ± 0.25)
d. RH Generator GEN Check generators parallel and voltage 29 ± 0.25.
e. Battery Switch OFF Check LH AMP and RH AMP drop and voltmeter reads zero.
f. Battery Switch BATT Check voltage 29 ± 0.25 volts

Front 3

Before Taxi Check

Back 3

1. A/C, Fans, Temp cntrl AS REQUIRED - Test l/r airsource select
2. Lights AS REQUIRED
3. Avionics Power Switch ON
4. AC Inverter Switch (SNs 0001 through 0099) CHECK INV 1 AND INV 2 AND SELECT INV 1 OR INV 2
5. Passenger Advisory Lights PASS SAFETY
6. Pressurization AUTO/SET DESTINATION PRESSURE ALTITUDE +200 FEET
7. Electric Elevator Trim CHECK AND SET
8. Flaps CHECK AND SET
Set the flaps to ground flaps and verify that both speedbrakes deploy. Advance the throttles to above 85% N2 and verify that the speedbrakes retract and that the flaps >35° annunciator light illuminates. Retard the throttles to idle and verify that the annunciator lights extinguish and that the speedbrakes redeploy. Set the flaps to TAKEOFF AND APPROACH and verify that the speedbrakes retract.
9. Flight Controls FREE AND CORRECT
10. Thrust Attenuators ............................................................. CHECK/AUTO
Place the thrust attenuator switch in stow; a white ATT STOW SELECTED advisory light will illuminate. Advance either throttle beyond 85% N2 with the thrust attenuator switch in stow; the MASTER CAUTION light will illuminate. Bring the throttles to idle and place the thrust attenuators switch to TEST; The MASTER CAUTION light will illuminate. Place the thrust attenuator switch in AUTO with the throttles at idle; the thrust attenuators will deploy. Advance either throttle above idle; the thrust attenuators will stow then redeploy when the throttle is returned to idle.
SNs 0100 through 0359:
10 A. Inverter Switch CHECK INVERTERS
Valid gyro information to pilot and copilot ADIs.
a. Select INV 1 and verify illumination of the INVERTER FAIL 2 light and valid P and CP ADIs.
b. Select INV 2 and verify illumination of the INVERTER FAIL 1 light and valid P and CP ADIs.
c. Select NORM and verify annunciator lights extinguish.
11. ATIS, Clearance, Flight Management System, Charts CHECK
12. Takeoff Data CONFIRM/SET
SNs 0001 through 0099:
13. RH Attitude PULL-TO-CAGE Knob. PULL AND RELEASE
Check for no comparator monitor indication.
SNs 0100 through 0359:
13 A. RH Attitude Indicator TEST
Press the ATT button and observe 30° right bank, 15° pitch, and fail flag. Release the button and observe straight and level indications and no flag.
14. Avionics CHECK AND SET
EFIS Test Button PUSH Pilot
a. Radio altimeter test value on the pilot’s display is 50 feet (if installed).
b. “Minimums”auralortonewarningsound(ifradaraltimeterinstalled).
c. All digit readouts replaced with dashes (except radio altimeter).
d. Allflagsinview.
e. Command cue (if selected) bias from view.
f. Comparator monitor annunciates ATT and HDG.
g. TEST annunciated.
h. After five seconds, the text page appears showing each test function status. As each function is tested, the FAIL annunciation will change to PASS.

Front 4

Taxi Check

Back 4

1. Brakes CHECK
antiskid selftesting must be completed while the airplane is stationary.
2. Flight Instruments CHECK
3. Crew Briefing COMPLETE

Front 5

Before Takeoff Check

Back 5

1.Anti-Ice/Deice Systems CHECK
2. Passenger Seats CHECK FULL UPRIGHT AND OUTBOARD
3. Cockpit Air Distribution Knob (AT Config) ..................... AS REQUIRED
4. Air Source Selector BOTH
5. Flaps SET FOR TAKEOFF
6. Trim SET FOR TAKEOFF
7. Thrust Attenuator Switch AUTO
8. Ignition ON
9. Pitot & Static Heat ON
10. Anti-ice/Deice Systems ON IF REQUIRED
11. Anti-Collision Lights ON
12. Landing or Recognition Lights AS DESIRED
13. Transponder ALT
14. Radar ................................................................................ AS REQUIRED
15. Annunciator CHECK

Front 6

Takeoff Check

Back 6

1. Throttles SET TAKEOFF THRUST
2. Engine Instruments CHECK
3. Brakes RELEASE

Front 7

After Takeoff Check

Back 7

1. Landing Gear UP
2. Flaps UP
3. Ignition NORM
4. Climb Power SET
5. Engine Synchronizer (optional) AS REQUIRED
6. Yaw Damper AS REQUIRED
7. Passenger Advisory Lights AS REQUIRED
8. Anti-Ice/Deice Systems AS REQUIRED
9. Landing or Recognition Lights OFF
10. Pressurization CHECK
11. Oxygen Control Valve NORMAL
12. Altimeters SET TO 29.92 AT TRANSITION ALTITUDE AND CROSS-CHECK

Front 8

Cruise Check

Back 8

1. Cruise Power SET
2. Anti-ice/Deice Systems AS REQUIRED
3. Cockpit Air Distribution Knob (AT Config) AS REQUIRED
.

Front 9

Descent Check

Back 9

1. Defog Systems AS REQUIRED
: a. Defog fan—HI b.Cockpit air distribution knob MAXc. Windshield bleed-air manual valves—MAX and windshield bleed- air switch—LOW below 18,000 feet if landing temperature/dew point spread is less than 10°F (5°C).
AS Configured:
a. b.
Defog Fan—HI prior to descent
Windshield bleed-air manual valves—MAX and windshield bleed-air switch—LOW prior to descent if landing temperature/dew point spread is less than 10°F (5°C). Warming the windshield with W/S BLEED air will assist in defrosting.
2. Pressurization SET DESTINATION PRESSURE ALTITUDE +200
3. Anti-ice/Deice Systems AS REQUIRED
4. Throttles AS REQUIRED
5. Altimeters SET
6. Landing Data CONFIRM
7. Approach BRIEF
8. Landing or Recognition Lights AS REQUIRED

Front 10

Before Landing Check

Back 10

1. Ignition ON
2. Landing Gear DOWN AND LOCKED
3. Flaps LAND
4. Pressurization CHECK ZERO DIFFERENTIAL
5. Autopilot and Yaw Damper OFF
6. Airspeed VREF
Power management 65-68 percent range will normally provide the desired indicated airspeed

Front 11

Before Start Check

Back 11

1. Preflight Inspection
2. Wheel Chocks REMOVED
3. Cabin Door CLOSE AND LOCK 5 green indicators
4. Passenger Briefing COMPLETE
5. Seats, Seat Belts, Shoulder Harnesses, and Rudder Pedals
6. Fuel Quantity CHECKED
7. Flashing Beacon ON
8. Air Conditioner OFF

Front 12

Engine Start Check

Back 12

1. Flood and Center Panel Lights.FULL BRIGHT (FOR NIGHT OPERATIONS)
2. Start ButtonPRESS BUTTON LIGHTS
3. Throttles IDLE AT 8-12% (N2) AND FAN (N1) RPM
4. ITT RISE in 10 sec.(975<7.5 sec)
5. Engine Instruments NORMAL
6. Fuel, Oil, Generator, and Hydraulic Annunciators EXTINGUISHED
7. Other Engine START; REPEAT STEPS 2 THRU 6
During generator cross starts, both start buttons illuminate indicating that both start relays are closed.
8. External Power CHECK CLEAR (IF APPLICABLE)
9. Generators GEN (IF EXTERNAL POWER WAS USED FOR START)
10. DC Amperes and Volts CHECK
a. LH Gen OFF Check LH AMP drop, RH AMP INCR, voltage 29 ± 0.25
b. RH Gen OFF Check RH AMP drop, Check voltage drop to battery voltage (24 volts minimum).
c. LH Generator GEN Check on line (AMPS INCR, voltage 29 ± 0.25)
d. RH Generator GEN Check generators parallel and voltage 29 ± 0.25.
e. Battery Switch OFF Check LH AMP and RH AMP drop and voltmeter reads zero.
f. Battery Switch BATT Check voltage 29 ± 0.25 volts

Front 13

Before Taxi Check

Back 13

1. A/C, Fans, Temp cntrl AS REQUIRED - Test l/r airsource select
2. Lights AS REQUIRED
3. Avionics Power Switch ON
4. AC Inverter Switch (SNs 0001 through 0099) CHECK INV 1 AND INV 2 AND SELECT INV 1 OR INV 2
5. Passenger Advisory Lights PASS SAFETY
6. Pressurization AUTO/SET DESTINATION PRESSURE ALTITUDE +200 FEET
7. Electric Elevator Trim CHECK AND SET
8. Flaps CHECK AND SET
Set the flaps to ground flaps and verify that both speedbrakes deploy. Advance the throttles to above 85% N2 and verify that the speedbrakes retract and that the flaps >35° annunciator light illuminates. Retard the throttles to idle and verify that the annunciator lights extinguish and that the speedbrakes redeploy. Set the flaps to TAKEOFF AND APPROACH and verify that the speedbrakes retract.
9. Flight Controls FREE AND CORRECT
10. Thrust Attenuators ............................................................. CHECK/AUTO
Place the thrust attenuator switch in stow; a white ATT STOW SELECTED advisory light will illuminate. Advance either throttle beyond 85% N2 with the thrust attenuator switch in stow; the MASTER CAUTION light will illuminate. Bring the throttles to idle and place the thrust attenuators switch to TEST; The MASTER CAUTION light will illuminate. Place the thrust attenuator switch in AUTO with the throttles at idle; the thrust attenuators will deploy. Advance either throttle above idle; the thrust attenuators will stow then redeploy when the throttle is returned to idle.
SNs 0100 through 0359:
10 A. Inverter Switch CHECK INVERTERS
Valid gyro information to pilot and copilot ADIs.
a. Select INV 1 and verify illumination of the INVERTER FAIL 2 light and valid P and CP ADIs.
b. Select INV 2 and verify illumination of the INVERTER FAIL 1 light and valid P and CP ADIs.
c. Select NORM and verify annunciator lights extinguish.
11. ATIS, Clearance, Flight Management System, Charts CHECK
12. Takeoff Data CONFIRM/SET
SNs 0001 through 0099:
13. RH Attitude PULL-TO-CAGE Knob. PULL AND RELEASE
Check for no comparator monitor indication.
SNs 0100 through 0359:
13 A. RH Attitude Indicator TEST
Press the ATT button and observe 30° right bank, 15° pitch, and fail flag. Release the button and observe straight and level indications and no flag.
14. Avionics CHECK AND SET
EFIS Test Button PUSH Pilot
a. Radio altimeter test value on the pilot’s display is 50 feet (if installed).
b. “Minimums”auralortonewarningsound(ifradaraltimeterinstalled).
c. All digit readouts replaced with dashes (except radio altimeter).
d. Allflagsinview.
e. Command cue (if selected) bias from view.
f. Comparator monitor annunciates ATT and HDG.
g. TEST annunciated.
h. After five seconds, the text page appears showing each test function status. As each function is tested, the FAIL annunciation will change to PASS.

Front 14

Taxi Check

Back 14

1. Brakes CHECK
antiskid selftesting must be completed while the airplane is stationary.
2. Flight Instruments CHECK
3. Crew Briefing COMPLETE

Front 15

Before Takeoff Check

Back 15

1.Anti-Ice/Deice Systems CHECK
2. Passenger Seats CHECK FULL UPRIGHT AND OUTBOARD
3. Cockpit Air Distribution Knob (AT Config) ..................... AS REQUIRED
4. Air Source Selector BOTH
5. Flaps SET FOR TAKEOFF
6. Trim SET FOR TAKEOFF
7. Thrust Attenuator Switch AUTO
8. Ignition ON
9. Pitot & Static Heat ON
10. Anti-ice/Deice Systems ON IF REQUIRED
11. Anti-Collision Lights ON
12. Landing or Recognition Lights AS DESIRED
13. Transponder ALT
14. Radar ................................................................................ AS REQUIRED
15. Annunciator CHECK

Front 16

Takeoff Check

Back 16

1. Throttles SET TAKEOFF THRUST
2. Engine Instruments CHECK
3. Brakes RELEASE

Front 17

After Takeoff Check

Back 17

1. Landing Gear UP
2. Flaps UP
3. Ignition NORM
4. Climb Power SET
5. Engine Synchronizer (optional) AS REQUIRED
6. Yaw Damper AS REQUIRED
7. Passenger Advisory Lights AS REQUIRED
8. Anti-Ice/Deice Systems AS REQUIRED
9. Landing or Recognition Lights OFF
10. Pressurization CHECK
11. Oxygen Control Valve NORMAL
12. Altimeters SET TO 29.92 AT TRANSITION ALTITUDE AND CROSS-CHECK

Front 18

Cruise Check

Back 18

1. Cruise Power SET
2. Anti-ice/Deice Systems AS REQUIRED
3. Cockpit Air Distribution Knob (AT Config) AS REQUIRED
.

Front 19

Descent Check

Back 19

1. Defog Systems AS REQUIRED
: a. Defog fan—HI b.Cockpit air distribution knob MAXc. Windshield bleed-air manual valves—MAX and windshield bleed- air switch—LOW below 18,000 feet if landing temperature/dew point spread is less than 10°F (5°C).
AS Configured:
a. b.
Defog Fan—HI prior to descent
Windshield bleed-air manual valves—MAX and windshield bleed-air switch—LOW prior to descent if landing temperature/dew point spread is less than 10°F (5°C). Warming the windshield with W/S BLEED air will assist in defrosting.
2. Pressurization SET DESTINATION PRESSURE ALTITUDE +200
3. Anti-ice/Deice Systems AS REQUIRED
4. Throttles AS REQUIRED
5. Altimeters SET
6. Landing Data CONFIRM
7. Approach BRIEF
8. Landing or Recognition Lights AS REQUIRED

Front 20

Before Landing Check

Back 20

1. Ignition ON
2. Landing Gear DOWN AND LOCKED
3. Flaps LAND
4. Pressurization CHECK ZERO DIFFERENTIAL
5. Autopilot and Yaw Damper OFF
6. Airspeed VREF
Power management 65-68 percent range will normally provide the desired indicated airspeed

Front 21

Before Start Check

Back 21

1. Preflight Inspection
2. Wheel Chocks REMOVED
3. Cabin Door CLOSE AND LOCK 5 green indicators
4. Passenger Briefing COMPLETE
5. Seats, Seat Belts, Shoulder Harnesses, and Rudder Pedals
6. Fuel Quantity CHECKED
7. Flashing Beacon ON
8. Air Conditioner OFF

Front 22

Engine Start Check

Back 22

1. Flood and Center Panel Lights.FULL BRIGHT (FOR NIGHT OPERATIONS)
2. Start ButtonPRESS BUTTON LIGHTS
3. Throttles IDLE AT 8-12% (N2) AND FAN (N1) RPM
4. ITT RISE in 10 sec.(975<7.5 sec)
5. Engine Instruments NORMAL
6. Fuel, Oil, Generator, and Hydraulic Annunciators EXTINGUISHED
7. Other Engine START; REPEAT STEPS 2 THRU 6
During generator cross starts, both start buttons illuminate indicating that both start relays are closed.
8. External Power CHECK CLEAR (IF APPLICABLE)
9. Generators GEN (IF EXTERNAL POWER WAS USED FOR START)
10. DC Amperes and Volts CHECK
a. LH Gen OFF Check LH AMP drop, RH AMP INCR, voltage 29 ± 0.25
b. RH Gen OFF Check RH AMP drop, Check voltage drop to battery voltage (24 volts minimum).
c. LH Generator GEN Check on line (AMPS INCR, voltage 29 ± 0.25)
d. RH Generator GEN Check generators parallel and voltage 29 ± 0.25.
e. Battery Switch OFF Check LH AMP and RH AMP drop and voltmeter reads zero.
f. Battery Switch BATT Check voltage 29 ± 0.25 volts

Front 23

Before Taxi Check

Back 23

1. A/C, Fans, Temp cntrl AS REQUIRED - Test l/r airsource select
2. Lights AS REQUIRED
3. Avionics Power Switch ON
4. AC Inverter Switch (SNs 0001 through 0099) CHECK INV 1 AND INV 2 AND SELECT INV 1 OR INV 2
5. Passenger Advisory Lights PASS SAFETY
6. Pressurization AUTO/SET DESTINATION PRESSURE ALTITUDE +200 FEET
7. Electric Elevator Trim CHECK AND SET
8. Flaps CHECK AND SET
Set the flaps to ground flaps and verify that both speedbrakes deploy. Advance the throttles to above 85% N2 and verify that the speedbrakes retract and that the flaps >35° annunciator light illuminates. Retard the throttles to idle and verify that the annunciator lights extinguish and that the speedbrakes redeploy. Set the flaps to TAKEOFF AND APPROACH and verify that the speedbrakes retract.
9. Flight Controls FREE AND CORRECT
10. Thrust Attenuators ............................................................. CHECK/AUTO
Place the thrust attenuator switch in stow; a white ATT STOW SELECTED advisory light will illuminate. Advance either throttle beyond 85% N2 with the thrust attenuator switch in stow; the MASTER CAUTION light will illuminate. Bring the throttles to idle and place the thrust attenuators switch to TEST; The MASTER CAUTION light will illuminate. Place the thrust attenuator switch in AUTO with the throttles at idle; the thrust attenuators will deploy. Advance either throttle above idle; the thrust attenuators will stow then redeploy when the throttle is returned to idle.
SNs 0100 through 0359:
10 A. Inverter Switch CHECK INVERTERS
Valid gyro information to pilot and copilot ADIs.
a. Select INV 1 and verify illumination of the INVERTER FAIL 2 light and valid P and CP ADIs.
b. Select INV 2 and verify illumination of the INVERTER FAIL 1 light and valid P and CP ADIs.
c. Select NORM and verify annunciator lights extinguish.
11. ATIS, Clearance, Flight Management System, Charts CHECK
12. Takeoff Data CONFIRM/SET
SNs 0001 through 0099:
13. RH Attitude PULL-TO-CAGE Knob. PULL AND RELEASE
Check for no comparator monitor indication.
SNs 0100 through 0359:
13 A. RH Attitude Indicator TEST
Press the ATT button and observe 30° right bank, 15° pitch, and fail flag. Release the button and observe straight and level indications and no flag.
14. Avionics CHECK AND SET
EFIS Test Button PUSH Pilot
a. Radio altimeter test value on the pilot’s display is 50 feet (if installed).
b. “Minimums”auralortonewarningsound(ifradaraltimeterinstalled).
c. All digit readouts replaced with dashes (except radio altimeter).
d. Allflagsinview.
e. Command cue (if selected) bias from view.
f. Comparator monitor annunciates ATT and HDG.
g. TEST annunciated.
h. After five seconds, the text page appears showing each test function status. As each function is tested, the FAIL annunciation will change to PASS.

Front 24

Taxi Check

Back 24

1. Brakes CHECK
antiskid selftesting must be completed while the airplane is stationary.
2. Flight Instruments CHECK
3. Crew Briefing COMPLETE

Front 25

Before Takeoff Check

Back 25

1.Anti-Ice/Deice Systems CHECK
2. Passenger Seats CHECK FULL UPRIGHT AND OUTBOARD
3. Cockpit Air Distribution Knob (AT Config) ..................... AS REQUIRED
4. Air Source Selector BOTH
5. Flaps SET FOR TAKEOFF
6. Trim SET FOR TAKEOFF
7. Thrust Attenuator Switch AUTO
8. Ignition ON
9. Pitot & Static Heat ON
10. Anti-ice/Deice Systems ON IF REQUIRED
11. Anti-Collision Lights ON
12. Landing or Recognition Lights AS DESIRED
13. Transponder ALT
14. Radar ................................................................................ AS REQUIRED
15. Annunciator CHECK

Front 26

Takeoff Check

Back 26

1. Throttles SET TAKEOFF THRUST
2. Engine Instruments CHECK
3. Brakes RELEASE

Front 27

After Takeoff Check

Back 27

1. Landing Gear UP
2. Flaps UP
3. Ignition NORM
4. Climb Power SET
5. Engine Synchronizer (optional) AS REQUIRED
6. Yaw Damper AS REQUIRED
7. Passenger Advisory Lights AS REQUIRED
8. Anti-Ice/Deice Systems AS REQUIRED
9. Landing or Recognition Lights OFF
10. Pressurization CHECK
11. Oxygen Control Valve NORMAL
12. Altimeters SET TO 29.92 AT TRANSITION ALTITUDE AND CROSS-CHECK

Front 28

Cruise Check

Back 28

1. Cruise Power SET
2. Anti-ice/Deice Systems AS REQUIRED
3. Cockpit Air Distribution Knob (AT Config) AS REQUIRED
.

Front 29

Descent Check

Back 29

1. Defog Systems AS REQUIRED
: a. Defog fan—HI b.Cockpit air distribution knob MAXc. Windshield bleed-air manual valves—MAX and windshield bleed- air switch—LOW below 18,000 feet if landing temperature/dew point spread is less than 10°F (5°C).
AS Configured:
a. b.
Defog Fan—HI prior to descent
Windshield bleed-air manual valves—MAX and windshield bleed-air switch—LOW prior to descent if landing temperature/dew point spread is less than 10°F (5°C). Warming the windshield with W/S BLEED air will assist in defrosting.
2. Pressurization SET DESTINATION PRESSURE ALTITUDE +200
3. Anti-ice/Deice Systems AS REQUIRED
4. Throttles AS REQUIRED
5. Altimeters SET
6. Landing Data CONFIRM
7. Approach BRIEF
8. Landing or Recognition Lights AS REQUIRED

Front 30

Before Landing Check

Back 30

1. Ignition ON
2. Landing Gear DOWN AND LOCKED
3. Flaps LAND
4. Pressurization CHECK ZERO DIFFERENTIAL
5. Autopilot and Yaw Damper OFF
6. Airspeed VREF
Power management 65-68 percent range will normally provide the desired indicated airspeed