PARKING - MAINTENANCE PRACTICES

Similar documents
PARKING - MAINTENANCE PRACTICES

ELECTRICAL POWER, EXTERNAL - SERVICING

TOWING - MAINTENANCE PRACTICES

TOWING - MAINTENANCE PRACTICES. Lockpins. Installation of the Air Driven Generator (ADG) Lockpin

TOWING MAINTENANCE PRACTICES. A. Towing Aircraft (Figure 201 and Figure 202) Cord, headset extension GSE Ref. No

CHAPTER 09 TOWING AND TAXIING LIST OF EFFECTIVE PAGES

BD 700 AIRCRAFT MAINTENANCE MANUAL PART II GRAVITY REFUELING - SERVICING

Falcon 50 AIRCRAFT MAINTENANCE MANUAL

PRESSURE REFUELING - SERVICING

E4610 (2 8160) Wing Landing Gear Retract Actuator Assy E4620 (2 8189) Wing Landing Gear Unlock Actuator Assy

CHAPTER HYDRAULIC POWER LIST OF ILLUSTRATIONS

Bombardier Global Express - Hydraulics

- (Ref , P. Block 001) - (Ref , P. Block 301) - (Ref , P. Block 301)

Fokker 50 - Landing Gear

EMERGENCY GEAR DOWN HANDLE CHECK VALVE GEAR DROP TO EXTEND POSITION DOOR SELECTOR DOOR SELECTOR VALVE UPLOCK RELEASE CYLINDER DOOR CYLINDER

/200/300/400/500 SERIES FLAMMABLE MATERIAL LOCATIONS

A AMM - KRUEGER FLAP ACTUATOR - REMOVAL/INSTALLATION

SERVICE BULLETIN REVISION

Bombardier Challenger Hydraulic System

Seal Dynamics McCormick Drive Tampa, Florida Installation Instructions

canadair chsfflencjibr

Landing Gear & Brakes

MODEL 510 MAINTENANCE MANUAL

SECTION II AIRPLANE AND SYSTEMS MODEL 750 HYDRAULIC

Aircraft Handling Ground Connections

Hawker 800XP Ground Handling Checklist. Procedures

AVANTI P180. Ground Handling

LEAR Description

General. Gear Retraction and Extension

GRAVITY REFUELING - SERVICING

LANDING GEAR. Table of Contents. Sep 13/2004 Flight Crew Operating Manual Volume 2 REV 1 CSP REV 1

RAYTHEON PREMIER I. TOWING Information This section of this sub-chapter provides information on towing procedures for the Model 390 airplane.

DESIGNATION. (1) Access Platform, 3.0 m (10 ft.) (2) 98A Guard - Safety, Flap/Slat Ctl Lever. (6) Circuit Breaker Safety Clips and Tags

FALCON SERVICE ADVISORY

SD3-60 AIRCRAFT MAINTENANCE MANUAL. These procedures will be required by personnel engaged in manoeuvring the aircraft on the ground.

Service Bulletin No: Ref No: 105 Modification No: INSPECTION ATA Chapter: 32

LAD Inc. Beechcraft King Air 200 Series Technical Ground School Syllabus Material Covered

Surface and Brakes Anti-Ice Systems

CHAPTER ICE AND RAIN PROTECTION SYSTEM

CHAPTER 10 PARKING AND MOORING

BEECHJET 400A TOWING AND TAXIING

THS ACTUATOR VALVE BLOCKS - ADJUSMENT/TEST

Canadair Regional Jet 100/200 - Auxiliary Power Unit

B757 AMM - DC GENERATION - ADJUSTMENT/TEST

SECTION III HYDRAULICS & LANDING GEAR

BALLAST UNIT Ea 5 New REPAIRABLE INDICATOR FLAP POSITION Ea 1 Overhauled ROTABLE

CHAPTER FUEL SYSTEM

SD3-60 AIRCRAFT MAINTENANCE MANUAL. This chapter includes information on dimensions, areas, zoning, etc. and is presented as follows:

Rotary Speed Brake Actuation System ICA Supplement

DOORS Table of Contents REV 3, May 03/05 CHAPTER DOORS. INTRODUCTION Introduction System Circuit Breakers

PILATUS AIRCRAFT LTD. CH-6371 STANS, SWITZERLAND SERVICE BULLETIN SERVICE BULLETIN NO: REF NO: 184 MODIFICATION NO: ATA CHAPTER: 32

LANDING GEAR TABLE OF CONTENTS CHAPTER 15

SECTION II EMERGENCY INFORMATION

Dornier 328Jet - Pneumatic

Canadair Regional Jet 100/200 - Fuel System

DCS L-39 ALBATROS REAL PILOT START-UP, TAXI AND TAKEOFF CHECKLISTS V 1.0 PREPARED BY LINO_GERMANY

B737 NG APU REMOVAL / INSTALLATION

CFM56-7B POWER PLANT REMOVAL & INSTALLATION

Приложение 1 ТЕХНИЧЕСКО ЗАДАНИЕ

Embraer Systems Summary [Landing Gear & Brakes]

INTRODUCTION TO THE COMPANY

Preflight Inspection. Table of Contents. Left Main Landing Gear... 2A-15 Left Fuselage... 2A-16. Left Wing Trailing Edge... 2A-13

A310 MEMORY ITEMS Last Updated: 20th th October 2011

FUEL SYSTEM REPLENISHING. NOTE: For calculation of fuel weights refer to Chapter 28. British Canadian American Specific Gravity

Airworthiness Directive Schedule

OPERATIONS MANUAL SECTION 6-2

AIRPLANE GENERAL Exterior REV 3, May 03/05

CHAPTER 14 LANDING GEAR

DUCHESS BE-76 AND COMMERCIAL MULTI ADD-ON ORAL REVIEW FOR CHECKRIDE

AW 169 Commercial in Confidence AW 169 VIP CONFIGURATION Airframe Transmission Drive System and Hydraulic System Electrical Systems

A AMM - MAIN GEAR SPHERICAL BEARING - REMOVAL/INSTALLATION

PNEUMATICS CONTENTS HST-TAMPER

SR22 Airplane Flight Manual (AFM) Temporary Change

CAL Ramp Operations Safety Notes

DASSAULT FALCON 7X SYSTEMS SUMMARY

ColumbusJACK/Regent. The Strength of Experience. Bead Breakers

ARIANA AFGHAN AIRLINES MPD Tally Sheet - Routine Jobs

SD3-60 AIRCRAFT MAINTENANCE MANUAL PROTECTION DESCRIPTION & OPERATION

SR22T Airplane Flight Manual (AFM) Temporary Change

FLIGHT CONTROLS SYSTEM

Preservation. A.1. Preservation for a Period of up to 30 Days. Pág. 2. Memoria ** ON A/C , , TASK

Main Landing Gear Torque Links - Remove procedures

SD3-60 AIRCRAFT MAINTENANCE MANUAL - DESCRIPTION & OPERATION

AIRCRAFT EXPOSURE TO VOLCANIC ASH PROPRIETARY NOTICE

HYDRAULICS & LANDING GEAR

Bombardier Q300 nose landing gear incidents

CIRRUS AIRPLANE MAINTENANCE MANUAL

Installation Work for Alpha Systems Angle of Attack System DSTR-AOA-9600K 05/28/2015

AIRCRAFT INFORMATION MSN: 4066

Chapter Four CASTER POWER-BACK AND INDICATION SYSTEM

World Leaders in Engineered Performance. Regional and Business Aircraft

DASSAULT AVIATION Proprietary Data

Offers for Sale Q Series: Q400 Aircraft MSN 4064

Models Affected: Certain 2013 Model Year Propane Vision Buses Equipped with Ford 6.8L Engines CORRECTIVE ACTION ---- PROCEDURE

TRANSPORT WINGS 1:72 Mixed-media kit of the DC Second generation jet airliner History, Notes and Instructions

Lucinda Handwriting & Arial Black 11, 16, 18 34

CHAPTER 6 ELECTRICAL SYSTEMS

Prevent corrosion that can decrease the aircraft structure life. Do a thorough inspection for corrosion and other types of damage.

Report RL 2004:21e. Accident involving aircraft LN-ALK at Malmö Sturup Airport, M county, Sweden, on 14 April 2004

The 747 s body gear Project Report

Transcription:

PARKING - MAINTENANCE PRACTICES TASK 000 801 1. Removal of the Nose Landing Gear (NLG) Lockpin A. Reference Information TASK 32 22 00 010 801 TASK 32 22 00 410 801 Open the Nose Landing Gear (NLG) Forward Doors Close the Nose Landing Gear (NLG) Forward Doors B. Tools and Equipment GSE 24 00 24 Tag, Circuit Breaker NOTE: Refer to the Illustrated Tool and Equipment Manual to make sure that you use the correct equipment configuration. C. 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 CB NUMBER CB NAME ZONE CBP 1 F2 WOW/GEAR/SPLR NO. 1 221 D. 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. Page 201

E. Close Out (1) Remove the tag and close the circuit breaker that follows: LOCATION CB NUMBER CB NAME ZONE CBP 1 F2 WOW/GEAR/SPLR NO. 1 221 (2) Close the NLG forward doors (TASK 32 22 00 410 801). (3) Remove all tools, equipment, and unwanted materials from the work area. Page 202

2 1 LMM1010012_001 Nose Landing Gear (NLG) Lockpin Removal/Installation Figure 201 Page 203

TASK 400 801 2. Installation of the Nose Landing Gear (NLG) Lockpin A. Reference Information CL 605 AIRCRAFT MAINTENANCE MANUAL PART II TASK 32 22 00 010 801 TASK 32 22 00 410 801 Open the Nose Landing Gear (NLG) Forward Doors Close the Nose Landing Gear (NLG) Forward Doors B. Tools and Equipment GSE 10 10 11 GSE 24 00 24 Lockpin, NLG Tag, Circuit Breaker NOTE: Refer to the Illustrated Tool and Equipment Manual to make sure that you use the correct equipment configuration. C. 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 CB NUMBER CB NAME ZONE CBP 1 F2 WOW/GEAR/SPLR NO. 1 221 D. 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. Page 204

E. Close Out (1) Remove the tag and close the circuit breaker that follows: LOCATION CB NUMBER CB NAME ZONE CBP 1 F2 WOW/GEAR/SPLR NO. 1 221 (2) Close the NLG forward doors (TASK 32 22 00 410 801). (3) Remove all tools, equipment, and unwanted materials from the work area. Page 205

TASK 000 802 3. Removal of the Main Landing Gear (MLG) Lockpins A. Procedure Refer to Figure 202. CL 605 AIRCRAFT MAINTENANCE MANUAL PART II 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. Page 206

SHOCK STRUT ACTUATOR 1 A 2 3 A LMM1010012_011 Main Landing Gear (MLG) Lockpin Removal/Installation Figure 202 Page 207

TASK 400 802 4. Installation of the Main Landing Gear (MLG) Lockpins A. Tools and Equipment CL 605 AIRCRAFT MAINTENANCE MANUAL PART II GSE 10 10 51 Lockpin, MLG NOTE: Refer to the Illustrated Tool and Equipment Manual to make sure that you use the correct equipment configuration. B. 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: If the lockpin is not easy to install there may be a problem with the landing gear and you must correct the problem. C. Close Out (1) Remove all tools, equipment, and unwanted materials from the work area. Page 208

TASK 000 803 5. Removal of the Air Driven Generator (ADG) Lockpin A. Reference Information CL 605 AIRCRAFT MAINTENANCE MANUAL PART II TASK 32 22 00 010 801 TASK 32 22 00 410 801 Open the Nose Landing Gear (NLG) Forward Doors Close the Nose Landing Gear (NLG) Forward Doors B. Tools and Equipment GSE 24 00 24 Tag, Circuit Breaker NOTE: Refer to the Illustrated Tool and Equipment Manual to make sure that you use the correct equipment configuration. C. 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 CB NUMBER CB NAME ZONE CBP 1 F2 WOW/GEAR/SPLR NO. 1 221 D. 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. Page 209

E. Close Out (1) Remove the tag and close the circuit breaker that follows: LOCATION CB NUMBER CB NAME ZONE CBP 1 F2 WOW/GEAR/SPLR NO. 1 221 (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). Page 210

A GROUND SAFETY PIN B ADG UPLOCK A GROUND SAFETY PIN B LMM1010012_021 Air Driven Generator (ADG) Lockpin Removal/Installation Figure 203 Page 211

TASK 400 803 6. Installation of the Air Driven Generator (ADG) Lockpin A. Reference Information CL 605 AIRCRAFT MAINTENANCE MANUAL PART II TASK 32 22 00 010 801 TASK 32 22 00 410 801 Open the Nose Landing Gear (NLG) Forward Doors Close the Nose Landing Gear (NLG) Forward Doors B. Tools and Equipment GSE 10 10 14 GSE 24 00 24 Lockpin, ADG Tag, Circuit Breaker NOTE: Refer to the Illustrated Tool and Equipment Manual to make sure that you use the correct equipment configuration. C. 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 CB NUMBER CB NAME ZONE CBP 1 F2 WOW/GEAR/SPLR NO. 1 221 D. 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 CB NUMBER CB NAME ZONE CBP 1 F2 WOW/GEAR/SPLR NO. 1 221 Page 212

(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). Page 213

TASK 587 801 7. Short Term Parking A. Reference Information CL 605 AIRCRAFT MAINTENANCE MANUAL PART II TASK 09 10 00 584 801 TASK 400 801 TASK 400 802 TASK 400 803 TASK 867 801 TASK 910 801 TASK 910 802 TASK 10 10 04 400 801 TASK 10 20 00 587 801 Towing of the Aircraft Installation of the Nose Landing Gear (NLG) Lockpin Installation of the Main Landing Gear (MLG) Lockpins Installation of the Air Driven Generator (ADG) Lockpin Grounding of the Aircraft Set the Parking Brake Release the Parking Brake Installation of the Covers and Plugs Aircraft Mooring B. Tools and Equipment GSE 10 10 09 Chocks, Rubber NOTE: Refer to the Illustrated Tool and Equipment Manual to make sure that you use the correct equipment configuration. C. 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 CB NUMBER CB NAME ZONE CBP 6 B3 CLOCK STANDBY 212 Page 214

(2) If the aircraft is parked in a closed hanger, do the steps that follow: (a) (b) (c) (d) (e) (f) (g) Set the parking brake (TASK 910 801). Install the wheel chocks at the nose landing gear (NLG) and main landing gear (MLG). Release the parking brake (TASK 910 802). Install the NLG lockpin (TASK 400 801). Install the MLG lockpins (TASK 400 802). Install the air driven generator (ADG) lockpin (TASK 400 803). Install the grounding wire (TASK 867 801). (3) If the aircraft is parked in an open area, do the steps that follow: (a) (b) (c) (d) (e) (f) (g) (h) (i) (j) Park the aircraft in the correct position to point in the direction of the wind. Set the parking brake (TASK 910 801). Install the wheel chocks at the nose landing gear (NLG) and main landing gear (MLG). Release the parking brake (TASK 910 802). Install the NLG lockpin (TASK 400 801). Install the MLG lockpins (TASK 400 802). Install the (ADG) lockpin (TASK 400 803). Install the grounding wire (TASK 867 801). Install all applicable covers and plugs (TASK 10 10 04 400 801). 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). Page 215 May 29/2009

CAUTION: 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. D. Close Out 3 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). (1) Remove all tools, equipment, and unwanted materials from the work area. Page 216

TASK 587 802 8. Long Term Parking A. Reference Information CL 605 AIRCRAFT MAINTENANCE MANUAL PART II TASK 09 10 00 584 801 TASK 400 801 TASK 400 802 TASK 400 803 TASK 867 801 TASK 910 801 TASK 910 802 TASK 10 10 04 400 801 TASK 10 10 07 550 801 TASK 10 20 00 587 801 TASK 24 32 00 040 801 TASK 24 32 00 040 802 Towing of the Aircraft Installation of the Nose Landing Gear (NLG) Lockpin Installation of the Main Landing Gear (MLG) Lockpins Installation of the Air Driven Generator (ADG) Lockpin Grounding of the Aircraft Set the Parking Brake Release the Parking Brake Installation of the Covers and Plugs Aircraft Storage Aircraft Mooring Disconnect the Main Battery Disconnect the Auxiliary Power Unit (APU) Battery B. Tools and Equipment GSE 10 10 09 Chocks, Rubber NOTE: Refer to the Illustrated Tool and Equipment Manual to make sure that you use the correct equipment configuration. Page 217

C. Consumable Materials CL 605 AIRCRAFT MAINTENANCE MANUAL PART II MANUFACTURERS AND/OR SPECIFICATION 05 065 Desiccant, Silica Gel MIL D 3464 D. Procedure (1) If the aircraft is parked in a closed hangar, do the steps that follow: (a) (b) (c) (d) (e) (f) (g) (h) (i) Set the parking brake (TASK 910 801). Install the wheel chocks at the nose landing gear (NLG) and main landing gear (MLG). Release the parking brake (TASK 910 802). Install the NLG lockpin (TASK 400 801). Install the MLG lockpin (TASK 400 802). Install the air driven generator (ADG) lockpin (TASK 400 803). Install the grounding wire (TASK 867 801). Disconnect the main battery (TASK 24 32 00 040 801) 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) (b) (c) (d) (e) (f) (g) (h) (i) Park the aircraft in the correct position to point in the direction of the wind. Set the parking brake (TASK 910 801). Install the wheel chocks at the nose landing gear (NLG) and main landing gear (MLG). Release the parking brake (TASK 910 802). Install the NLG lockpin (TASK 400 801). Install the MLG lockpins (TASK 400 802). Install the ADG lockpin (TASK 400 803). Install the grounding wire (TASK 867 801) Disconnect the main battery (TASK 24 32 00 040 801). Page 218 May 29/2009

(j) (k) (l) Disconnect auxiliary power unit (APU) battery (TASK 24 32 00 040 802). Install all applicable covers and plugs and install desiccant where necessary to prevent contamination (TASK 10 10 04 400 801). 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: 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. 3 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. Page 219 May 29/2009

TASK 867 801 9. Grounding of the Aircraft A. Reference Information CL 605 AIRCRAFT MAINTENANCE MANUAL PART II TASK 24 00 00 910 801 TASK 32 22 00 010 801 TASK 32 22 00 410 801 Electrical/Electronic Safety Precautions Open the Nose Landing Gear (NLG) Forward Doors Close the Nose Landing Gear (NLG) Forward Doors B. Tools and Equipment GSE 24 00 24 Tag, Circuit Breaker NOTE: Refer to the Illustrated Tool and Equipment Manual to make sure that you use the correct equipment configuration. C. 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 CB NUMBER CB NAME ZONE CBP 1 F2 WOW/GEAR/SPLR NO. 1 221 D. 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. Page 220

E. Close Out (1) Remove the tag and close the circuit breaker that follows: LOCATION CB NUMBER CB NAME ZONE CBP 1 F2 WOW/GEAR/SPLR NO. 1 221 (2) Remove all tools, equipment, and unwanted materials from the work area. (3) Close the NLG forward doors (TASK 32 22 00 410 801). Page 221

B 1 2 B A LMM1010012_031 Grounding of the Aircraft Maintenance Practices Figure 204 Page 222

TASK 910 801 10. Set the Parking Brake A. Reference Information CL 605 AIRCRAFT MAINTENANCE MANUAL PART II TASK 12 00 04 862 803 Pressurize Hydraulic System No. 3 TASK 12 00 04 862 804 Release Hydraulic Pressure System No. 3 B. Job Set Up (1) In the flight compartment, make sure that the brake systems have sufficient hydraulic pressure as follows: (a) (b) (c) (d) Push the HYD pushbutton on the engine indication and crew alerting system (EICAS) control panel to get the hydraulic page. Examine the hydraulic pressure for system No. 3. Make sure that the pressure indication shows 0 psi. On the HYDRAULIC control panel, set the 3A switch to ON. Examine the HYDRAULIC synoptic page on EICAS. Make sure that the conditions that follow: C. Procedure 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). (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. Page 223

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. Page 224

TASK 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. CL 605 AIRCRAFT MAINTENANCE MANUAL PART II Page 225