CL−605 AIRCRAFT MAINTENANCE MANUAL − PART II
PARKING - MAINTENANCE PRACTICES
1.
TASK 10−10−01−000−801
Removal of the Nose Landing Gear (NLG) Lockpin
A.
Reference Information
REFERENCE
B.
DESIGNATION
TASK 32−22−00−010−801
Open the Nose Landing Gear (NLG) Forward Doors
TASK 32−22−00−410−801
Close the Nose Landing Gear (NLG) Forward Doors
Tools and Equipment
REFERENCE
DESIGNATION
GSE 24−00−24
NOTE:
C.
Tag, Circuit Breaker
Refer to the Illustrated Tool and Equipment Manual to make sure that you use
the correct equipment configuration.
Job Set−Up
(1) Open the NLG forward doors (TASK 32−22−00−010−801).
(2) Open and tag the circuit breaker that follows:
LOCATION
CBP−1
D.
CB NUMBER
F2
CB NAME
WOW/GEAR/SPLR NO. 1
ZONE
221
Procedure
Refer to Figure 201.
WARNING:
KEEP THE LOCKPIN IN POSITION IF IT IS NOT EASY TO REMOVE. IF
YOU REMOVE THE LOCKPIN, THE LANDING GEAR IS NOT SAFE,
AND CAN ACCIDENTALLY RETRACT. THIS CAN CAUSE INJURIES
TO PERSONS AND DAMAGE TO THE AIRCRAFT.
(1) Remove the lockpin (1) by hand, from the hole (2) in the upper link of the NLG drag
brace.
NOTE:
If the lockpin is not easy to remove, there may be a problem with the
landing gear and you must correct the problem.
EFFECTIVITY: ALL
10−10−01
Page 201
Nov 28/2008
CL−605 AIRCRAFT MAINTENANCE MANUAL − PART II
E.
Close Out
(1) Remove the tag and close the circuit breaker that follows:
LOCATION
CBP−1
CB NUMBER
F2
CB NAME
WOW/GEAR/SPLR NO. 1
ZONE
221
(2) Close the NLG forward doors (TASK 32−22−00−410−801).
(3) Remove all tools, equipment, and unwanted materials from the work area.
EFFECTIVITY: ALL
10−10−01
Page 202
Nov 28/2008
CL−605 AIRCRAFT MAINTENANCE MANUAL − PART II
2
LMM1010012_001
1
Nose Landing Gear (NLG) Lockpin − Removal/Installation
Figure 201
EFFECTIVITY: ALL
10−10−01
Page 203
Nov 28/2008
CL−605 AIRCRAFT MAINTENANCE MANUAL − PART II
2.
TASK 10−10−01−400−801
Installation of the Nose Landing Gear (NLG) Lockpin
A.
Reference Information
REFERENCE
B.
DESIGNATION
TASK 32−22−00−010−801
Open the Nose Landing Gear (NLG) Forward Doors
TASK 32−22−00−410−801
Close the Nose Landing Gear (NLG) Forward Doors
Tools and Equipment
REFERENCE
GSE 10−10−11
Lockpin, NLG
GSE 24−00−24
Tag, Circuit Breaker
NOTE:
C.
DESIGNATION
Refer to the Illustrated Tool and Equipment Manual to make sure that you use
the correct equipment configuration.
Job Set−Up
(1) Open the NLG forward doors (TASK 32−22−00−010−801)
(2) Open and tag the circuit breaker that follows:
LOCATION
CBP−1
D.
CB NUMBER
F2
CB NAME
WOW/GEAR/SPLR NO. 1
ZONE
221
Procedure
Refer to Figure 201.
(1) Put the lockpin (1) fully into the hole (2) in the upper link of the NLG drag brace.
NOTE:
If the lockpin is not easy to install, there may be a problem with the
landing gear and you must correct the problem.
EFFECTIVITY: ALL
10−10−01
Page 204
Nov 28/2008
CL−605 AIRCRAFT MAINTENANCE MANUAL − PART II
E.
Close Out
(1) Remove the tag and close the circuit breaker that follows:
LOCATION
CBP−1
CB NUMBER
F2
CB NAME
WOW/GEAR/SPLR NO. 1
ZONE
221
(2) Close the NLG forward doors (TASK 32−22−00−410−801).
(3) Remove all tools, equipment, and unwanted materials from the work area.
EFFECTIVITY: ALL
10−10−01
Page 205
Nov 28/2008
CL−605 AIRCRAFT MAINTENANCE MANUAL − PART II
3.
TASK 10−10−01−000−802
Removal of the Main Landing Gear (MLG) Lockpins
A.
Procedure
Refer to Figure 202.
WARNING:
KEEP THE LOCKPIN IN POSITION IF IT IS NOT EASY TO REMOVE. IF
YOU REMOVE THE LOCKPIN, THE LANDING GEAR IS NOT SAFE,
AND CAN ACCIDENTALLY RETRACT. THIS CAN CAUSE INJURIES
TO PERSONS AND DAMAGE TO THE AIRCRAFT.
(1) Remove the lockpin (3) by hand, from the hole (2) in the retraction actuator.
NOTE:
If the lockpin is not easy to remove, there may be a problem with the
landing gear and you must correct the problem.
(2) Move the spring clip (1) to the holes on the retraction actuator.
B.
Close Out
(1) Remove all tools, equipment, and unwanted materials from the work area.
EFFECTIVITY: ALL
10−10−01
Page 206
Nov 28/2008
CL−605 AIRCRAFT MAINTENANCE MANUAL − PART II
SHOCK STRUT
ACTUATOR
1
A
2
LMM1010012_011
3
A
Main Landing Gear (MLG) Lockpin − Removal/Installation
Figure 202
EFFECTIVITY: ALL
10−10−01
Page 207
Nov 28/2008
CL−605 AIRCRAFT MAINTENANCE MANUAL − PART II
4.
TASK 10−10−01−400−802
Installation of the Main Landing Gear (MLG) Lockpins
A.
Tools and Equipment
REFERENCE
GSE 10−10−51
NOTE:
B.
DESIGNATION
Lockpin, MLG
Refer to the Illustrated Tool and Equipment Manual to make sure that you use
the correct equipment configuration.
Procedure
Refer to Figure 202.
WARNING:
DO NOT STAY BELOW THE AIRCRAFT IF YOU CANNOT EASILY
INSTALL THE LOCKPIN. IF YOU CANNOT EASILY INSTALL THE
LOCKPIN, THE LANDING GEAR IS NOT SAFE, AND CAN
ACCIDENTALLY RETRACT. THIS CAN CAUSE INJURIES TO
PERSONS AND DAMAGE TO THE AIRCRAFT.
(1) Move the spring clip (1) at the outboard end of the retraction actuator to one side to
open the lockpin holes (2).
(2) Put the lockpin (3) by hand, fully into one of the holes (2) in the retraction actuator.
NOTE:
C.
If the lockpin is not easy to install there may be a problem with the landing
gear and you must correct the problem.
Close Out
(1) Remove all tools, equipment, and unwanted materials from the work area.
EFFECTIVITY: ALL
10−10−01
Page 208
Nov 28/2008
CL−605 AIRCRAFT MAINTENANCE MANUAL − PART II
5.
TASK 10−10−01−000−803
Removal of the Air Driven Generator (ADG) Lockpin
A.
Reference Information
REFERENCE
B.
DESIGNATION
TASK 32−22−00−010−801
Open the Nose Landing Gear (NLG) Forward Doors
TASK 32−22−00−410−801
Close the Nose Landing Gear (NLG) Forward Doors
Tools and Equipment
REFERENCE
DESIGNATION
GSE 24−00−24
NOTE:
C.
Tag, Circuit Breaker
Refer to the Illustrated Tool and Equipment Manual to make sure that you use
the correct equipment configuration.
Job Set−Up
(1) Open the nose landing gear (NLG) forward doors (TASK 32−22−00−010−801)
(2) Open and tag the circuit breaker that follows:
LOCATION
CBP−1
D.
CB NUMBER
F2
CB NAME
WOW/GEAR/SPLR NO. 1
ZONE
221
Procedure
Refer to Figure 203.
WARNING:
KEEP THE LOCKPIN IN POSITION IF IT IS NOT EASY TO REMOVE. IF
YOU MUST USE FORCE TO REMOVE THE LOCKPIN, THE ADG
UPLOCK IS NOT SAFE, AND THE ADG CAN ACCIDENTALLY
EXTEND. THIS CAN CAUSE INJURIES TO PERSONS AND DAMAGE
TO THE AIRCRAFT. IF THE LOCKPIN IS NOT EASY REMOVE. YOU
MUST CORRECT THE PROBLEM.
(1) Remove the lockpin by hand from the hole on the right side of the nose gear well.
EFFECTIVITY: ALL
10−10−01
Page 209
Nov 28/2008
CL−605 AIRCRAFT MAINTENANCE MANUAL − PART II
E.
Close Out
(1) Remove the tag and close the circuit breaker that follows:
LOCATION
CBP−1
CB NUMBER
F2
CB NAME
WOW/GEAR/SPLR NO. 1
ZONE
221
(2) Remove all tools, equipment, and unwanted materials from the work area.
(3) Close the nose landing gear NLG forward doors (TASK 32−22−00−410−801).
EFFECTIVITY: ALL
10−10−01
Page 210
Nov 28/2008
CL−605 AIRCRAFT MAINTENANCE MANUAL − PART II
A
GROUND SAFETY PIN
B
ADG UPLOCK
A
GROUND SAFETY PIN
LMM1010012_021
B
Air Driven Generator (ADG) Lockpin − Removal/Installation
Figure 203
EFFECTIVITY: ALL
10−10−01
Page 211
Nov 28/2008
CL−605 AIRCRAFT MAINTENANCE MANUAL − PART II
6.
TASK 10−10−01−400−803
Installation of the Air Driven Generator (ADG) Lockpin
A.
Reference Information
REFERENCE
B.
DESIGNATION
TASK 32−22−00−010−801
Open the Nose Landing Gear (NLG) Forward Doors
TASK 32−22−00−410−801
Close the Nose Landing Gear (NLG) Forward Doors
Tools and Equipment
REFERENCE
GSE 10−10−14
Lockpin, ADG
GSE 24−00−24
Tag, Circuit Breaker
NOTE:
C.
DESIGNATION
Refer to the Illustrated Tool and Equipment Manual to make sure that you use
the correct equipment configuration.
Job Set−Up
(1) Open the nose landing gear (NLG) forward doors (TASK 32−22−00−010−801).
(2) Open and tag the circuit breaker that follows:
LOCATION
CBP−1
D.
CB NUMBER
F2
CB NAME
WOW/GEAR/SPLR NO. 1
ZONE
221
Procedure
Refer to Figure 203.
(1) Put the lockpin by hand, fully into the hole on the right side of the nose gear well.
E.
Close Out
(1) Remove the tag and close the circuit breaker that follows:
LOCATION
CBP−1
CB NUMBER
F2
CB NAME
WOW/GEAR/SPLR NO. 1
ZONE
221
EFFECTIVITY: ALL
10−10−01
Page 212
Nov 28/2008
CL−605 AIRCRAFT MAINTENANCE MANUAL − PART II
(2) Remove all tools, equipment, and unwanted materials from the work area.
(3) Close the nose landing gear NLG forward doors (TASK 32−22−00−410−801).
EFFECTIVITY: ALL
10−10−01
Page 213
Nov 28/2008
CL−605 AIRCRAFT MAINTENANCE MANUAL − PART II
7.
TASK 10−10−01−587−801
Short Term Parking
A.
Reference Information
REFERENCE
B.
DESIGNATION
TASK 09−10−00−584−801
Towing of the Aircraft
TASK 10−10−01−400−801
Installation of the Nose Landing Gear (NLG) Lockpin
TASK 10−10−01−400−802
Installation of the Main Landing Gear (MLG)
Lockpins
TASK 10−10−01−400−803
Installation of the Air Driven Generator (ADG)
Lockpin
TASK 10−10−01−867−801
Grounding of the Aircraft
TASK 10−10−01−910−801
Set the Parking Brake
TASK 10−10−01−910−802
Release the Parking Brake
TASK 10−10−04−400−801
Installation of the Covers and Plugs
TASK 10−20−00−587−801
Aircraft Mooring
Tools and Equipment
REFERENCE
DESIGNATION
GSE 10−10−09
NOTE:
C.
Chocks, Rubber
Refer to the Illustrated Tool and Equipment Manual to make sure that you use
the correct equipment configuration.
Procedure
(1) If the aircraft is going to be parked for more than 48 hours, gain access to CBP−6
by opening the right forward equipment bay door (212AR) and pull the circuit
breaker that follows:
LOCATION
CBP−6
CB NUMBER
B3
CB NAME
CLOCK STANDBY
ZONE
212
EFFECTIVITY: ALL
10−10−01
Page 214
Nov 28/2008
CL−605 AIRCRAFT MAINTENANCE MANUAL − PART II
(2) If the aircraft is parked in a closed hanger, do the steps that follow:
(a) Set the parking brake (TASK 10−10−01−910−801).
(b) Install the wheel chocks at the nose landing gear (NLG) and main landing gear
(MLG).
(c)
Release the parking brake (TASK 10−10−01−910−802).
(d) Install the NLG lockpin (TASK 10−10−01−400−801).
(e) Install the MLG lockpins (TASK 10−10−01−400−802).
(f)
Install the air driven generator (ADG) lockpin (TASK 10−10−01−400−803).
(g) Install the grounding wire (TASK 10−10−01−867−801).
(3) If the aircraft is parked in an open area, do the steps that follow:
(a) Park the aircraft in the correct position to point in the direction of the wind.
(b) Set the parking brake (TASK 10−10−01−910−801).
(c)
Install the wheel chocks at the nose landing gear (NLG) and main landing gear
(MLG).
(d) Release the parking brake (TASK 10−10−01−910−802).
(e) Install the NLG lockpin (TASK 10−10−01−400−801).
(f)
Install the MLG lockpins (TASK 10−10−01−400−802).
(g) Install the (ADG) lockpin (TASK 10−10−01−400−803).
(h) Install the grounding wire (TASK 10−10−01−867−801).
(i)
Install all applicable covers and plugs (TASK 10−10−04−400−801).
(j)
Do a regular inspection of the local weather conditions and do the steps that
follow:
1
If the direction of the wind changes, move the aircraft to point in the
direction of the wind, as necessary.
2
If high winds are possible, and a closed hangar is available, immediately
tow the aircraft into the hangar until the wind is not a problem
(TASK 09−10−00−584−801).
EFFECTIVITY: ALL
10−10−01
Page 215
May 29/2009
CL−605 AIRCRAFT MAINTENANCE MANUAL − PART II
CAUTION:
3
D.
DO NOT PARK OR MOOR THE AIRCRAFT IN AN OPEN
AREA WHEN WINDS OF 52 KNOTS (27 M/SEC) OR MORE
ARE POSSIBLE. DURING THESE CONDITIONS, YOU MUST
MOVE THE AIRCRAFT INTO A CLOSED HANGAR. IF YOU
DO NOT DO THIS, YOU CAN CAUSE DAMAGE TO THE
AIRCRAFT.
Moor the aircraft if high winds less than 52 kt (27 m/sec) are possible, and
the aircraft is kept in an open area (TASK 10−20−00−587−801).
Close Out
(1) Remove all tools, equipment, and unwanted materials from the work area.
EFFECTIVITY: ALL
10−10−01
Page 216
Nov 28/2008
CL−605 AIRCRAFT MAINTENANCE MANUAL − PART II
8.
TASK 10−10−01−587−802
Long Term Parking
A.
Reference Information
REFERENCE
B.
DESIGNATION
TASK 09−10−00−584−801
Towing of the Aircraft
TASK 10−10−01−400−801
Installation of the Nose Landing Gear (NLG) Lockpin
TASK 10−10−01−400−802
Installation of the Main Landing Gear (MLG)
Lockpins
TASK 10−10−01−400−803
Installation of the Air Driven Generator (ADG)
Lockpin
TASK 10−10−01−867−801
Grounding of the Aircraft
TASK 10−10−01−910−801
Set the Parking Brake
TASK 10−10−01−910−802
Release the Parking Brake
TASK 10−10−04−400−801
Installation of the Covers and Plugs
TASK 10−10−07−550−801
Aircraft Storage
TASK 10−20−00−587−801
Aircraft Mooring
TASK 24−32−00−040−801
Disconnect the Main Battery
TASK 24−32−00−040−802
Disconnect the Auxiliary Power Unit (APU) Battery
Tools and Equipment
REFERENCE
GSE 10−10−09
NOTE:
DESIGNATION
Chocks, Rubber
Refer to the Illustrated Tool and Equipment Manual to make sure that you use
the correct equipment configuration.
EFFECTIVITY: ALL
10−10−01
Page 217
Nov 28/2008
CL−605 AIRCRAFT MAINTENANCE MANUAL − PART II
C.
Consumable Materials
REFERENCE
05−065
D.
DESIGNATION
Desiccant, Silica Gel
MANUFACTURERS’ REFERENCE
AND/OR SPECIFICATION
MIL−D−3464
Procedure
(1) If the aircraft is parked in a closed hangar, do the steps that follow:
(a) Set the parking brake (TASK 10−10−01−910−801).
(b) Install the wheel chocks at the nose landing gear (NLG) and main landing gear
(MLG).
(c)
Release the parking brake (TASK 10−10−01−910−802).
(d) Install the NLG lockpin (TASK 10−10−01−400−801).
(e) Install the MLG lockpin (TASK 10−10−01−400−802).
(f)
Install the air driven generator (ADG) lockpin (TASK 10−10−01−400−803).
(g) Install the grounding wire (TASK 10−10−01−867−801).
(h) Disconnect the main battery (TASK 24−32−00−040−801)
(i)
Disconnect auxiliary power unit (APU) battery (TASK 24−32−00−040−802)
(2) If the aircraft is parked in an open area, do the steps that follow:
(a) Park the aircraft in the correct position to point in the direction of the wind.
(b) Set the parking brake (TASK 10−10−01−910−801).
(c)
Install the wheel chocks at the nose landing gear (NLG) and main landing gear
(MLG).
(d) Release the parking brake (TASK 10−10−01−910−802).
(e) Install the NLG lockpin (TASK 10−10−01−400−801).
(f)
Install the MLG lockpins (TASK 10−10−01−400−802).
(g) Install the ADG lockpin (TASK 10−10−01−400−803).
(h) Install the grounding wire (TASK 10−10−01−867−801)
(i)
Disconnect the main battery (TASK 24−32−00−040−801).
EFFECTIVITY: ALL
10−10−01
Page 218
May 29/2009
CL−605 AIRCRAFT MAINTENANCE MANUAL − PART II
(j)
Disconnect auxiliary power unit (APU) battery (TASK 24−32−00−040−802).
(k)
Install all applicable covers and plugs and install desiccant where necessary to
prevent contamination (TASK 10−10−04−400−801).
(l)
Do a regular inspection of the local weather conditions and do the steps that
follow:
1
If the direction of the wind changes, move the aircraft to point in the
direction of the wind, as necessary.
2
If high winds are possible, and a closed hangar is available immediately
tow the aircraft into the hangar until the wind is not a problem
(TASK 09−10−00−584−801).
CAUTION:
3
DO NOT PARK OR MOOR THE AIRCRAFT IN AN OPEN
AREA WHEN WINDS OF 52 KNOTS (27 M/SEC) OR MORE
ARE POSSIBLE. DURING THESE CONDITIONS, YOU MUST
MOVE THE AIRCRAFT INTO A CLOSED HANGAR. IF YOU
DO NOT DO THIS, YOU CAN CAUSE DAMAGE TO THE
AIRCRAFT.
Moor the aircraft if high winds are less than 52 kt (27 m/sec) are possible,
and the aircraft is kept in an open area (TASK 10−20−00−587−801).
(3) If the aircraft storage is necessary, do the aircraft storage procedure
(TASK 10−10−07−550−801).
E.
Close Out
(1) Remove all tools, equipment, and unwanted materials from the work area.
EFFECTIVITY: ALL
10−10−01
Page 219
May 29/2009
CL−605 AIRCRAFT MAINTENANCE MANUAL − PART II
9.
TASK 10−10−01−867−801
Grounding of the Aircraft
A.
Reference Information
REFERENCE
B.
DESIGNATION
TASK 24−00−00−910−801
Electrical/Electronic Safety Precautions
TASK 32−22−00−010−801
Open the Nose Landing Gear (NLG) Forward Doors
TASK 32−22−00−410−801
Close the Nose Landing Gear (NLG) Forward Doors
Tools and Equipment
REFERENCE
DESIGNATION
GSE 24−00−24
NOTE:
C.
Tag, Circuit Breaker
Refer to the Illustrated Tool and Equipment Manual to make sure that you use
the correct equipment configuration.
Job Set−Up
(1) Obey the electrical/electronic safety precautions (TASK 24−00−00−910−801).
(2) Open the NLG forward doors (TASK 32−22−00−010−801)
(3) Open and tag the circuit breaker that follows:
LOCATION
CBP−1
D.
CB NUMBER
F2
CB NAME
WOW/GEAR/SPLR NO. 1
ZONE
221
Procedure
Refer to Figure 204.
(1) If the grounding wire has an alligator clip, attach the clamp to the grounding lug (1)
on the right side wall of the nose gear compartment.
(2) If the grounding wire has a ground stud, put the stud in the nearest ground stud
receptacle (2) on the wing leading edge.
EFFECTIVITY: ALL
10−10−01
Page 220
Nov 28/2008
CL−605 AIRCRAFT MAINTENANCE MANUAL − PART II
E.
Close Out
(1) Remove the tag and close the circuit breaker that follows:
LOCATION
CBP−1
CB NUMBER
F2
CB NAME
WOW/GEAR/SPLR NO. 1
ZONE
221
(2) Remove all tools, equipment, and unwanted materials from the work area.
(3) Close the NLG forward doors (TASK 32−22−00−410−801).
EFFECTIVITY: ALL
10−10−01
Page 221
Nov 28/2008
CL−605 AIRCRAFT MAINTENANCE MANUAL − PART II
B
1
2
LMM1010012_031
B
A
Grounding of the Aircraft − Maintenance Practices
Figure 204
EFFECTIVITY: ALL
10−10−01
Page 222
Nov 28/2008
CL−605 AIRCRAFT MAINTENANCE MANUAL − PART II
TASK 10−10−01−910−801
10. Set the Parking Brake
A.
Reference Information
REFERENCE
B.
DESIGNATION
TASK 12−00−04−862−803
Pressurize Hydraulic System No. 3
TASK 12−00−04−862−804
Release Hydraulic Pressure − System No. 3
Job Set−Up
(1) In the flight compartment, make sure that the brake systems have sufficient
hydraulic pressure as follows:
(a) Push the HYD pushbutton on the engine indication and crew alerting system
(EICAS) control panel to get the hydraulic page.
(b) Examine the hydraulic pressure for system No. 3. Make sure that the pressure
indication shows 0 psi.
(c)
On the HYDRAULIC control panel, set the 3A switch to ON.
(d) Examine the HYDRAULIC synoptic page on EICAS. Make sure that the
conditions that follow:
C.
1
The input/output flow indication for system No. 3A changes to green
2
The system No. 3A shows a minimum pressure of 1500 psi (10342 kPa).
If the pressure is less than the necessary minimum, then pressurize
system No. 3A to a minimum of 1500 psi (10342 kPa)
(TASK 12−00−04−862−803).
Procedure
(1) With your foot. push down and hold the brake pedals.
(2) Fully release the parking brake handle.
(3) Turn the parking brake handle 90 degrees clockwise. Make sure that the parking
brake handle is locked in position.
(4) Release the parking brake handle.
(5) Release the brake pedals.
EFFECTIVITY: ALL
10−10−01
Page 223
Nov 28/2008
CL−605 AIRCRAFT MAINTENANCE MANUAL − PART II
D.
Close Out
(1) If necessary, release hydraulic pressure from system No. 3A
(TASK 12−00−04−862−804)
(2) Remove all tools, equipment, and unwanted materials from the work area.
EFFECTIVITY: ALL
10−10−01
Page 224
Nov 28/2008
CL−605 AIRCRAFT MAINTENANCE MANUAL − PART II
TASK 10−10−01−910−802
11. Release the Parking Brake
A.
Procedure
(1) With your foot, push down and hold the brake pedals.
(2) Fully release the parking brake handle.
(3) Turn the parking brake handle 90 degrees counterclockwise.
(4) Fully push in the parking brake handle and release it.
(5) Release the brake pedals.
EFFECTIVITY: ALL
10−10−01
Page 225
Nov 28/2008