10-11-02 Pageblock 201

PROLONGED PARKING - MAINTENANCE PRACTICES

Effective on: AAL ALL

1. General

A. The procedures necessary for the protection of a parked airplane are given in this section. These procedures are

the task named "Airplane Storage Procedures".

B. The procedures necessary to put the airplane back to a serviceable condition are also found in this section. These

procedures are the task named "Put the Airplane Back to a Serviceable Condition After Storage".

List of Maintenance Tasks:

10-11-02-622-001 Airplane Storage Procedures

10-11-02-632-002 Put the Airplane Back to a Serviceable Condition After Storage

American Airlines

Printed: 8/31/2015; 1:28pm.

Rel. 59.0 - 08/20/15

LAA_B767

AIRCRAFT MAINTENANCE MANUAL

PGBLK EFFECTIVITY: AAL ALL 10-11-02-201

04/22/2012

BOEING PROPRIETARY - Copyright © Unpublished Work Page 1 of 35   

For Reference Only 
Task 10-11-02-622-001 "USE MCM CARD 05-92-09, 05-92-10, 05-92-12, 05-92-13, 05-92-14, 05-92-16, 05-92-20, 05-

92-62, 05-92-71, 05-92-72, 05-92-73, 05-92-74, 05-92-75, 05-92-76, as required by GPM 03-07"

Airplane Storage Procedures

Effective on: AAL ALL

A. General

(1) When an airplane is not in active service or is not being actively maintained for a period of 7 days or more, the

airplane must be protected. The procedures that follow will help prevent deterioration of the airplane structure,

finish, or system components. There are different procedures to prepare some systems for storage. These

procedures are calculated by the length of time the airplane is in storage. Follow the instructions and use the

equipment list in PAGEBLOCK 10-11-01/201 prior to starting this procedure.

The storage times are as follows:

(a) Short Term Storage - Applies to times that are 0-60 days unless specified differently.

(b) Long Term Storage - Applies to times that are more than 60 days unless specified differently.

(c) If the storage duration is unknown at the time of induction, or there is a chance that the storage

duration may change during the storage period, both the Short Term tasks and the Long Term

tasks should be completed.

(2) The procedure for attaching static port covers to the airplane and the locations of the static ports and pitot

probes are given in Airplane Normal Parking, TASK 10-11-01-582-001 .

B. References

Reference Title

10-11-01 P/B 201 NORMAL PARKING - MAINTENANCE PRACTICES

10-11-01-582-001 Airplane Normal Parking (P/B 201)

10-11-03-582-001 Airplane Parking In High Winds (P/B 201)

10-11-05-552-001 Chock Installation in Winds of less than 35 Knots (P/B 201)

10-11-05-552-003 Chock Installation in Winds of more than 35 Knots (P/B 201)

12-11-01 P/B 301 FUEL TANK PRESSURE FUELING - SERVICING

12-11-02 P/B 301 FUEL TANK OVERWING FUELING-SERVICING

12-12-01 P/B 301 HYDRAULIC SYSTEMS - SERVICING

12-13-05 P/B 301 AIR DRIVEN PUMP (ADP) - SERVICING

12-15-01 P/B 301 MAIN GEAR SHOCK STRUT - SERVICING

12-15-02 P/B 301 NOSE GEAR SHOCK STRUT - SERVICING

12-15-03 P/B 301 LANDING GEAR TIRES - SERVICING

12-15-04 P/B 301 PARKING BRAKE ACCUMULATOR - SERVICING

12-15-08 P/B 301 OXYGEN - SERVICING

12-15-09 P/B 301 BRAKE HYDRAULIC SYSTEM SURGE ACCUMULATOR - SERVICING

12-17-01 P/B 301 WASTE TANK - SERVICING

American Airlines

Printed: 8/31/2015; 1:28pm.

Rel. 59.0 - 08/20/15

LAA_B767

AIRCRAFT MAINTENANCE MANUAL

PGBLK EFFECTIVITY: AAL ALL 10-11-02-201

04/22/2012

BOEING PROPRIETARY - Copyright © Unpublished Work Page 2 of 35   

For Reference Only 
Reference Title

12-21-04 P/B 301 ELEVATOR CONTROL SYSTEM - SERVICING

12-21-10 P/B 301 SPOILER/SPEEDBRAKE CONTROL - SERVICING (LUBRICATION)

12-21-12 P/B 301 NOSE GEAR AND ACTUATING MECHANISMS - LUBRICATION

12-21-14 P/B 301 MAIN GEAR AND ACTUATING MECHANISMS - SERVICING

12-21-15 P/B 301 MAIN GEAR DOORS AND ACTUATING MECHANISMS - SERVICING

12-21-31 P/B 301 CONTROL CABLES - SERVICING (LUBRICATION)

12-25-01 P/B 301 CLEANING AND POLISHING-SERVICING

20-41-00 P/B 201 STATIC GROUNDING - MAINTENANCE PRACTICES

20-41-01 P/B 201 ELECTROSTATIC DISCHARGE SENSITIVE DEVICES - MAINTENANCE PRACTICES

21-31-00 P/B 001 CABIN PRESSURE CONTROL SYSTEM - DESCRIPTION OPERATION

21-31-02 P/B 401 AUTOMATIC CABIN PRESSURE CONTROLLER - REMOVAL/INSTALLATION

21-51-00 P/B 501 COOLING PACK SYSTEM - ADJUSTMENT/TEST

21-51-14 P/B 401 PACK TEMPERATURE CONTROLLER AND PACK STANDBY CONTROLLER - REMOVAL/INSTALLATION

21-53-02 P/B 501 RAM AIR EXHAUST DOOR - ADJUSTMENT/TEST

21-58-00 P/B 001 Config 4 EQUIPMENT COOLING SYSTEM - DESCRIPTION AND OPERATION

21-58-00 P/B 001 Config 6 EQUIPMENT COOLING SYSTEM - DESCRIPTION AND OPERATION

21-58-00 P/B 001 Config 7 EQUIPMENT COOLING SYSTEM - DESCRIPTION AND OPERATION

21-61-03 P/B 401 ZONE TEMPERATURE CONTROLLER - REMOVAL/INSTALLATION

21-61-12 P/B 401 AUXILIARY ZONE TEMPERATURE CONTROLLER - REMOVAL/INSTALLATION

24-31-01 P/B 401 MAIN BATTERY - REMOVAL/INSTALLATION

24-31-04 P/B 401 APU BATTERY - REMOVAL/INSTALLATION

27-11-00 P/B 501 AILERON AND AILERON TRIM CONTROL SYSTEM - ADJUSTMENT/TEST

27-21-00 P/B 501 Config 1 RUDDER AND RUDDER TRIM CONTROL SYSTEM - ADJUSTMENT/TEST

27-21-00 P/B 501 Config 2 RUDDER AND RUDDER TRIM CONTROL SYSTEM - ADJUSTMENT/TEST

27-31-00 P/B 501 ELEVATOR CONTROL SYSTEM - ADJUSTMENT/TEST

27-41-00 P/B 501 HORIZONTAL STABILIZER TRIM CONTROL SYSTEM - ADJUSTMENT/TEST

27-51-00 P/B 201 TRAILING EDGE FLAP SYSTEM - MAINTENANCE PRACTICES

27-61-00 P/B 201 SPOILER/SPEEDBRAKE CONTROL SYSTEM - MAINTENANCE PRACTICES

27-81-00 P/B 201 LEADING EDGE SLAT SYSTEM - MAINTENANCE PRACTICES

28-10-00 P/B 201 MICROBIAL GROWTH - MAINTENANCE PRACTICES

American Airlines

Printed: 8/31/2015; 1:28pm.

Rel. 59.0 - 08/20/15

LAA_B767

AIRCRAFT MAINTENANCE MANUAL

PGBLK EFFECTIVITY: AAL ALL 10-11-02-201

04/22/2012

BOEING PROPRIETARY - Copyright © Unpublished Work Page 3 of 35   

For Reference Only 
Reference Title

29-11-00 P/B 201 MAIN (LEFT, RIGHT, AND CENTER) HYDRAULIC SYSTEMS - MAINTENANCE PRACTICES

30-43-00 P/B 201 Config 1 WINDSHIELD RAIN REPELLENT SYSTEM - MAINTENANCE PRACTICES

30-43-00 P/B 201 Config 2 WINDSHIELD RAIN REPELLENT SYSTEM - MAINTENANCE PRACTICES

32-00-15 P/B 201 LANDING GEAR DOOR LOCKS - MAINTENANCE PRACTICES

32-00-15-002-001 Remove the Door Locks (P/B 201)

32-00-20-402-006 Install the Downlocks on the Landing Gear (P/B 201)

32-32-09 P/B 401 MAIN GEAR GEAR-OPERATED SEQUENCE VALVE CAM BOX - REMOVAL/INSTALLATION

33-51-07 P/B 201 POWER SUPPLY - MAINTENANCE PRACTICES

33-51-07 P/B 201 Config 2 POWER SUPPLY - MAINTENANCE PRACTICES

49-11-00 P/B 201 AUXILIARY POWER UNIT - MAINTENANCE PRACTICES

GA: 71-00-03 P/B 201 POWER PLANT - MAINTENANCE PRACTICES (PRESERVATION AND DEPRESERVATION)

GE: 71-00-03 P/B 201 POWER PLANT - MAINTENANCE PRACTICES (PRESERVATION AND DEPRESERVATION)

C. Tools/Equipment

Reference Description

STD-1106 Bag - Polyethylene, Capacity 1 Pint Polyethylene Bottle with Cap

STD-1130 Cap - Protective, Flareless Tube, 1/2-20 Thread

D. Consumable Materials

Reference Description Specification

B01000 Solvent - General Cleaning Of Metal (AMM 20-30-80)

C00924 Coating - Alkaline Removable, Temporary Protective BMS15-12, Type I

D00013 Grease - Aircraft And Instrument Grease MIL-PRF-23827 (NATO G-354)

(Supersedes MIL-G-23827)

D00016 Grease - Aircraft, General Purpose, Wide Temperature Range MIL-PRF-81322

D00054 Fluid - Hydraulic Assembly Lubricant - MCS 352B (Formerly Monsanto

MCS 352B)

D00070 Fluid - Hydraulic, Petroleum Base MIL-PRF-5606 (Replaces MIL-H-5606)

D00106 Fluid - Hydraulic, Petroleum Base, For Preservation And Operation MIL-PRF-6083 (NATO C-635)

D00153 Fluid - Hydraulic Fluid, Fire Resistant (Interchangable And Intermixable

With BMS 3-11 Type V)

BMS3-11 Type IV

D00467 Fluid - Landing Gear Shock Strut BMS3-32, Type II

American Airlines

Printed: 8/31/2015; 1:28pm.

Rel. 59.0 - 08/20/15

LAA_B767

AIRCRAFT MAINTENANCE MANUAL

PGBLK EFFECTIVITY: AAL ALL 10-11-02-201

04/22/2012

BOEING PROPRIETARY - Copyright © Unpublished Work Page 4 of 35   

For Reference Only 
Reference Description Specification

D00510 Lubricant - Landing Gear Shock Strut Additive - Lubrizol 1395

D00633 Grease - Aircraft General Purpose BMS3-33

D50022 Fluid - Landing Gear Shock Strut (Specifically For Preservation) BMS3-32, Type I

G00009 Compound - Organic Corrosion Inhibiting BMS3-23

G00087 Fabric, Insulation Covering (Self-Extinguishing) BMS8-142

G00452 Additive, Fuel - Biobor JF

G02145 Tape - Aluminum Foil BMS8-289

G02219 Tape - Yellow Vinyl Adhesive, Scotch Brand No.471, 1.5 Inches (38.1

mm) Wide

G02347 Biocide - Fuel - Kathon FP1.5

G02444 Tag - Red Paper, "STATIC PORTS COVERED" - 3 inches (76.2 mm) Wide,

6 inches (152.4 mm) Long

G02447 Tag - Red Paper, "PITOT PROBES COVERED" - 3 inches (76.2 mm) Wide,

6 inches (152.4 mm) Long

G50309 Coating - Protective, Ardrox 306-N BMS 15-12

E. Procedure

Effective on: AAL ALL

SUBTASK 862-058

(1) Use this table to put the airplane in storage:

Item

Procedures Repeat Intervals

(Days)

Initial 7 14 30 60 90 180 As

Rqd

ALL AREAS

1. Make sure all protective coverings are installed correctly. Reinstall the

protective coverings where required.

X

EXTERNAL SURFACE PROTECTION

Short Term

1. Apply a temporary layer of Protective Coating to all metal that is not

painted. Do not include the engine tail cones, brakes or other components

that operate with high temperatures (the paint would burn off). Apply a

layer ofC00924 coating orG50309 coating :

X

A. Procedure

(1) Apply with a spray gun (air or airless) to get a uniform dry film

thickness of 1.5 ±0.5 mils. The applied layer must be smooth, transparent,

and continuous.

B. Cure

(1) Before you touch - let the Protective Coating cure at room temperature

American Airlines

Printed: 8/31/2015; 1:28pm.

Rel. 59.0 - 08/20/15

LAA_B767

AIRCRAFT MAINTENANCE MANUAL

PGBLK EFFECTIVITY: AAL ALL 10-11-02-201

04/22/2012

BOEING PROPRIETARY - Copyright © Unpublished Work Page 5 of 35   

For Reference Only 
Item

Procedures Repeat Intervals

(Days)

Initial 7 14 30 60 90 180 As

Rqd

for 20 minutes (minimum).

(2) Before you stack - let the Protective Coating cure at room temperature

for 4 hours (minimum).

Long Term

1. Apply the Protective Coating to all metal that is not painted. Follow the

instructions in the Short Term procedures of the External Surface Protection

paragraphs.

X

2. Make an inspection of all external surfaces each 14-day cycle. Make sure

the Protective Coating has not worn off.

X

3. Examine all painted surfaces each 14-day cycle. Look for stains. To

remove the stains, wash the airplane ( PAGEBLOCK 12-15-01/301 ).

X X

NOTE: Stains are the discoloration of the finish because of the collection of oil or other liquids. When the oil

and other liquids are mixed together with dust or other particles, the airplane finish can be

permanently deteriorated. The collection of rain-streaked dust will not cause damage unless the

dust contains corrosive industrial or chemical pollutants.

4. PutG02145 tape or other reflective material (such as aluminized mylar)

over the outside of the control cabin windows and windshields. Do not put

material that will permit heat to build up on the windshield.

X

5. Examine the structural drain holes each 60-day cycle. Make sure they are

open.

X

EQUIPMENT/FURNISHINGS

Short Term

To give protection for a maximum of 30 days, do the procedures that follow.

1. Put dust covers on the seats. X

2. Carpets and seats can stay in the airplane for 30 days after the storage

starts. Humidity control is not necessary for this time.

X

3. If the toilet waste systems are serviced and activated, do the steps that

follow:

A. Flush each toilet. X

B. Drain the waste tanks ( PAGEBLOCK 12-17-01/301 ). X

C. Put the water supply override shutoff valve to the closed position and

flush the toilet twice.

X

4. Clean as necessary all tray carriers, storage compartments waste

containers, and dispenser compartments in the lavatories and galleys.

X

5. Examine the lavatories and galley(s). Look for unusual conditions and

correct as necessary.

X

6. Close the window shades and put a cover on the main entry and service

door windows. Use an opaque material to prevent the fading of the seats

and carpet materials because of the sun's ultraviolet rays. When the seats

and carpets are removed, the window shades can be put up.

X

7. Make sure that all main entry doors are in the manual (disarmed) mode. X

8. Open the closet, galley, and lavatory doors. This will permit the air to X

American Airlines

Printed: 8/31/2015; 1:28pm.

Rel. 59.0 - 08/20/15

LAA_B767

AIRCRAFT MAINTENANCE MANUAL

PGBLK EFFECTIVITY: AAL ALL 10-11-02-201

04/22/2012

BOEING PROPRIETARY - Copyright © Unpublished Work Page 6 of 35   

For Reference Only 
Item

Procedures Repeat Intervals

(Days)

Initial 7 14 30 60 90 180 As

Rqd

flow.

Long Term

To give protection for a maximum of two years, do the procedures that

follow:

1. Examine the upholstery and carpets for moisture and mildew. Do this

after the storage and correct as necessary.

X

2. When the seats and carpets stay in the airplane longer than 30 days, the

humidity in the airplane must be controlled to a maximum of 70%. If the

necessary humidity cannot be controlled, remove the seats and carpets and

put them in a storage area that can control the humidity.

X

3. Disconnect and disassemble the attendant's flashlights and put them in

storage.

X

4. Remove the seats and floor panels in the area of the center wing section

canted bulkhead. This will permit access to the airplane structure. Examine

the area when airplane is first stored and again when airplane is removed

from storage. Remove any moisture accumulation.

X X

INCLEMENT WEATHER CONDITIONS

1. When the snow on the airplane gets to a depth of 8 to 10 inches, remove

the snow.

X

2. To make sure the airplane stays in its position when the wind is up to 60

knots, do the steps that follow ( Airplane Parking In High Winds, TASK 10-

11-03-582-001 ):

X

A. Make sure the engines or an equivalent weight are installed on the

airplane.

B. Put the flaps to the full up position and set the control surfaces to the

neutral position.

C. Install the wheel chocks on all landing gear wheels ( Chock Installation

in Winds of less than 35 Knots, TASK 10-11-05-552-001 or Chock

Installation in Winds of more than 35 Knots, TASK 10-11-05-552-003 ).

CAUTION: MAKE SURE THAT YOU INSTALL THE STRAPS CORRECTLY. THE ATTACH LUGS CAN CAUSE

DAMAGE TO THE HYDRAULIC LINES AND THE ELECTRICAL WIRES.

D. Put two tie-down straps around the attach lugs of the lower drag strut on

the nose landing gear. Put the straps outboard and in opposite directions,

and angled forward to clear the doors. Attach the straps to the ground

anchors on each side of the airplane. To prevent the airplane from weathercocking, the side loads applied to the drag brace must be 15,000 pounds.

NOTE: Make sure you do not damage the hydraulic lines and the electrical wires that are found in the area

of the attach lugs.

INSPECTION CRITERIA

1. Remove the dirt and contamination you can see on the surfaces that are

not painted. The maximum time recommended between the contamination

and the cleaning is 24 hours ( PAGEBLOCK 12-25-01/301 ).

X

NOTE: When the airplane skin becomes discolored, or stained, or if the blending of adjacent surfaces for

appearance is necessary, refer to the operators standard procedures.

American Airlines

Printed: 8/31/2015; 1:28pm.

Rel. 59.0 - 08/20/15

LAA_B767

AIRCRAFT MAINTENANCE MANUAL

PGBLK EFFECTIVITY: AAL ALL 10-11-02-201

04/22/2012

BOEING PROPRIETARY - Copyright © Unpublished Work Page 7 of 35   

For Reference Only 
Item

Procedures Repeat Intervals

(Days)

Initial 7 14 30 60 90 180 As

Rqd

LANDING GEAR

Short Term

1. Install the wheel chocks on all landing gear tires ( Chock Installation in

Winds of less than 35 Knots, TASK 10-11-05-552-001 or Chock Installation

in Winds of more than 35 Knots, TASK 10-11-05-552-003 )

X

2. Release the parking brake. X

3. Make sure the downlocks are installed on the nose and main landing gear

( Install the Downlocks on the Landing Gear, TASK 32-00-20-402-006 ).

X

WARNING: USE THE PROCEDURE IN PAGEBLOCK 32-00-15/201 TO REMOVE THE DOOR LOCKS. THE

DOORS OPEN AND CLOSE QUICKLY AND CAN CAUSE INJURY TO PERSONS OR DAMAGE TO

EQUIPMENT.

4. Remove the door locks from the landing gear doors and close the doors (

Remove the Door Locks, TASK 32-00-15-002-001 ).

X

5. Do not deflate the shock struts of the landing gear.

6. Lubricate the areas that follow withD00633 grease (optionalD00013

grease ).

A. The surfaces of the uplock hooks on the main landing gear doors (

PAGEBLOCK 12-21-15/301 ).

X

B. The bare surface of the spherical trunnion bearing of the main landing

gear ( PAGEBLOCK 12-21-14/301 ).

X

C. Lubricate all of the bearings on all of the hydraulic components and

linkages that have lubrication fittings.

X

7. Do a check of the tire pressure each two week cycle. Make sure to keep

the tire pressure at the specified level ( PAGEBLOCK 12-15-03/301 ).

X X

8. When you think the weather will freeze for a long time, put coarse sand

or a coarse fiber mat between the tires and the ground surface.

X

NOTE: This is not necessary if the airplane will not be moved during this time, and if the tires will be

discarded.

Long Term

Do the procedures that follow at the start of the storage cycle and at the

specified intervals. Also, do the short term storage procedures.

CAUTION: DO NOT LET THE GREASE TOUCH THE ADJACENT AREAS. THE GREASE CAN CAUSE

CONTAMINATION TO OTHER COMPONENTS.

1. Inflate the shock struts of the main landing gear until they are extended

6 inches. Butter lubricate the bare inner cylinder area that is chrome,

withD00633 grease and put the shock struts back to their specified

condition ( PAGEBLOCK 12-15-01/301 ). Remove any remaining grease.

X

2. Inflate the shock strut of the nose landing gear until it is extended 6

inches. Butter lubricate the bare inner cylinder area that is chrome,D00633

grease and put the shock strut back to its specified condition (

PAGEBLOCK 12-15-02/301 ). Remove any remaining grease.

X

3. Apply a layer ofD00013 grease orD00633 grease to all landing gear parts

that are not painted (This does not include the steering actuators or piston

X X X

American Airlines

Printed: 8/31/2015; 1:28pm.

Rel. 59.0 - 08/20/15

LAA_B767

AIRCRAFT MAINTENANCE MANUAL

PGBLK EFFECTIVITY: AAL ALL 10-11-02-201

04/22/2012

BOEING PROPRIETARY - Copyright © Unpublished Work Page 8 of 35   

For Reference Only 
Item

Procedures Repeat Intervals

(Days)

Initial 7 14 30 60 90 180 As

Rqd

rods because their bare finished surfaces must be lubricated with Skydrol).

Do this lubrication each 180 day cycle. Examine the specified areas each 90

day cycle and lubricate again as necessary.

4. Examine the shock struts of the landing gear for hydraulic leaks. X

5. Lubricate all of the joints on the nose landing gear that have lubrication

fittings. UseD00633 grease ( PAGEBLOCK 12-21-12/301 ).

X X

6. Lubricate all of the joints on the main landing gear that have lubrication

fittings. UseD00633 grease ( PAGEBLOCK 12-21-14/301 ).

X X

7. Lubricate the areas that follow withD00633 grease . (Optional grease

isD00013 grease ).

A. The surface of the uplock hooks of the main landing gear doors (

PAGEBLOCK 12-21-15/301 ).

X

B. The bare surfaces of the spherical trunnion bearings of the main landing

gear ( PAGEBLOCK 12-21-12/301 ).

X

8. Do a check of the tires for flat spots. X

A. If there are flat spots on the tires:

(1) Rotate the tires, or

(2) Tow the airplane a short distance.

9. Lubricate the wheel bearings withD00016 grease X

10. Put a cover on the tires. Use an opaque material which will keep the

weather wear to a minimum.

X

11. Do a check of the pressures of the landing gear shock struts each 90-

day cycle. If you find a decrease in pressure, look for leaks and repair the

shock strut as necessary.

X

Short and Long Term

1. Use the ground release levers and operate the landing gear doors one

time each 30-day cycle.

X

2. On the nose landing gear, disconnect the torsion link and operate the

steering actuators each 30-day cycle. Lubricate the bare surfaces of the

torsion link withD00633 grease and keep the link disconnected.

X

3. After the initial lubrication (when the storage started), and at each 90

day cycle, do the servicing of all the lubrication joints.

X X

4. After the initial lubrication at the start of the storage and at each 90- day

cycle, lubricate all control cables (this does not include the cables in the

body of the airplane).

X X

5. Lubricate the cables in the body of the airplane one time each year after

the initial lubrication.

X

6. Lubricate the cam and the cam follower for the gear-operated sequence

valve ( PAGEBLOCK 32-32-09/401 ).

X

7. If the shock struts are serviced with pureD00070 fluid or pureD00106

fluid , then service the shock struts withD00510 Lubrizol 1395 lubricant (

PAGEBLOCK 12-15-02/301 ).

X

American Airlines

Printed: 8/31/2015; 1:28pm.

Rel. 59.0 - 08/20/15

LAA_B767

AIRCRAFT MAINTENANCE MANUAL

PGBLK EFFECTIVITY: AAL ALL 10-11-02-201

04/22/2012

BOEING PROPRIETARY - Copyright © Unpublished Work Page 9 of 35   

For Reference Only 
Item

Procedures Repeat Intervals

(Days)

Initial 7 14 30 60 90 180 As

Rqd

NOTE: It is not necessary to drain and service the shock struts that are filled withD50022 fluid orD00467

fluid .

FUEL SYSTEM

Short and Long Term

NOTE: The procedures that follow are for protection of the fuel system.

1. Fill all fuel tanks to a minimum of 10 percent or more of capacity and

keep the fuel at that capacity ( PAGEBLOCK 12-11-02/301 ) (

PAGEBLOCK 12-11-01/301 ).

X

NOTE: 10 percent fuel is required to prevent fuel seals from drying and leaking.

2. Each year, inspect one main fuel tank for corrosion. If corrosion is found,

inspect all fuel tanks for corrosion. Examine the engine dry bay, and the

center wing dry cavities (if it is applicable) for corrosion Remove moisture

that has collected. ApplyG00009 corrosion inhibiting compound Type II,

corrosion inhibiting compound to the applicable area that does not have

fuel.

YR

NOTE: If the fuel tanks are being examined for corrosion on a second and subsequent inspection, examine

a tank other than the one you examined before.

WARNING: DO NOT BREATHE OR TOUCH THE BIOCIDE FUEL ADDITIVE. IF YOU BREATHE THE FUMES OR

TOUCH THE BIOCIDE FUEL ADDITIVE, IT COULD KILL YOU.

CAUTION: DO NOT ADD A LARGE CONCENTRATION OF THE BIOCIDE FUEL ADDITIVE TO THE FUEL TANKS.

A LARGE CONCENTRATION OF THE FUEL ADDITIVE CAN MAKE SALT DEPOSITS IN THE FUEL

TANKS.

IF METERED INJECTION EQUIPMENT IS NOT AVAILABLE, REFER TO (

PAGEBLOCK 28-10-00/201 ) FOR OTHER APPROVED PROCEDURES TO ADD

BIOCIDE TO THE FUEL TANKS.

3. Put the fuel additive in the fuel tanks. The fuel should containG00452

Biobor JF additive , 270 parts per million maximum by weight orG02347

Kathon FP1.5 biocide , 100 parts per million by volume to prevent microorganism in fuel tanks ( PAGEBLOCK 28-10-00/201 ).

X

NOTE: The fuel additive will prevent sealant deterioration in the fuel tanks.

4. Put a screen, mesh cloth, or an equivalent material over each vent

opening and cavity vent opening. UseG02219 Scotch Brand No.471 tape or

an equivalent to prevent the entry of insects into the lines. Attach red flags

to the material on each opening.

X

5. For long term storage, examine the material on each opening, each 6 to

8 weeks.

X

FLIGHT DECK

Short Term

1. To give protection for a maximum of 30 days, do these procedures: A.

Install the pitot-static probe covers (4 locations).

X

B. Put the static port covers on all of the static ports. The procedure to

attach the static port covers to the airplane is in Normal Parking (

PAGEBLOCK 10-11-01/201 ).

X

American Airlines

Printed: 8/31/2015; 1:28pm.

Rel. 59.0 - 08/20/15

LAA_B767

AIRCRAFT MAINTENANCE MANUAL

PGBLK EFFECTIVITY: AAL ALL 10-11-02-201

04/22/2012

BOEING PROPRIETARY - Copyright © Unpublished Work Page 10 of 35   

For Reference Only 
Item

Procedures Repeat Intervals

(Days)

Initial 7 14 30 60 90 180 As

Rqd

C. Put covers on the temperature probes, angle-of-attack sensors, and ice

detector (if installed) ( PAGEBLOCK 10-11-01/201 .)

X

D. Install dust covers on the seats. X

Long Term

Do the procedures that follow at the start of the storage cycle and at the

specified intervals. Also, do the short term storage procedures.

1. It is not necessary to remove the mode control panels and the panel

modules when the relative humidity is controlled. The humidity in the

airplane must be controlled to a maximum of 70%. When the necessary

humidity cannot be controlled, remove the specified components and put

them in a storage area that can control the humidity. This area must be for

storage of electronic equipment to prevent the deterioration of the

components. Follow the electrostatic discharge to sensitive devices

procedure, ( PAGEBLOCK 20-41-01/201 ).

X

NOTE: Put plugs in the cooling air orifices and the input vents for the components that were removed. This

is to make sure that an adequate cooling air flow will get to the components that stay in the

airplane.

A. Remove the module that follows from the Overhead Panel: X

(1) M-59 S242T101-203, IRS Mode Selector

B. Remove the modules that follow from the Electronics Panel. X

(1) M-76 S242T102-131, FMC CDV

(2) M-77 S242T102-131, FMC CDV

(3) M-93 S242T404-344, EFIS CONT

(4) M-94 S242T404-344, EFIS CONT

C. Remove the modules that follow from the Pilot's Main Panel.

(1) N-4 S242T404-577, EADI Display (2)

(2) N-44 S242T404-577, EADI Display

(3) N-5 S242T404-611, EASI/EICAS Display

(4) N-45 S242T404-611, EASI/EICAS Display

(5) N-10013 S242T404-611, EASI/EICAS Display

(6) N-10014c S242T404-611, EASI/EICAS Display

(7) N-3 S242T403-109, IND-RDMI

(8) N-43 S242T403-109, IND-RDMI

(9) N-70 S241T120-3, Autopilot Status Annunciator

(10) N-71 S241T120-3, Autopilot Status Annunciator

(11) P3-1 S241T200-154, Thrust Mode Select Panel

X

D. Remove the module that follows from the Right Side Panel.

(1) N-10029 S242T404-601, EICAS Display

X

E. Remove these modules from the glareshield panel:

(1) M-90 S241T100-211, Mode Control Panel

(2) M-90 S241T100-501, Autothrottle Switch Lens Cap

(3) M-90 S241T100-404, Switch Guard

X

American Airlines

Printed: 8/31/2015; 1:28pm.

Rel. 59.0 - 08/20/15

LAA_B767

AIRCRAFT MAINTENANCE MANUAL

PGBLK EFFECTIVITY: AAL ALL 10-11-02-201

04/22/2012

BOEING PROPRIETARY - Copyright © Unpublished Work Page 11 of 35   

For Reference Only 
Item

Procedures Repeat Intervals

(Days)

Initial 7 14 30 60 90 180 As

Rqd

2. When the seats and carpets stay in the airplane longer than 30 days, the

humidity in the airplane must be controlled to a maximum of 70%. If the

necessary humidity cannot be controlled, remove the seats and carpets and

put them in a storage area that can control the humidity.

X

Effective on: AAL 301-307, 316, 319-325, 327-329, 332, 335, 336, 338, 339, 351-391 PRE SB 767-30-0028

3. Remove the rain repellent can ( PAGEBLOCK 30-43-00/201 Config 1 or

PAGEBLOCK 30-43-00/201 Config 2 ).

X

Effective on: AAL 301-307, 316, 319-325, 327-329, 332, 335, 336, 338, 339, 351-391 PRE SB 767-30-0028

4. Use dry, filtered air to remove the rain repellent fluid from the two lines. X

X

ELECTRICAL/ELECTRONIC SYSTEMS

Short Term (5 to 30 days)

To give protection for a maximum of 30 days, do the procedures that follow.

1. Static the airplane ( PAGEBLOCK 20-41-00/201 ). X

2. Put all switches to the OFF position. This does not include the switches

used to deactivate the systems.

X

3. Open the circuit breakers for all electrical/electronic components that

have been removed from the airplane.

X

4. Open the circuit breakers that follow on the panel, P6, and attach the

DO-NOT-CLOSE tags. This will prevent the discharge of the battery.

X

A. 6G3, CLOCK TIME BASE L

B. 6G4, CLOCK TIME BASE R

C. 6D6, EQUIP COOL GND WARN

D. 6C4, BUS TIE ENABLE

E. 6E1, L SPAR FUEL VALVE

F. 6E2, R SPAR FUEL VALVE

G. 6E3, APU FUEL VALVE

H. 6G5, ACARS DC PWR

I. 6D3, L IRS

J. 6D5, R IRS

K. 6D4, C IRS

Long Term (30 days to unlimited time period)

The procedures that follow are for protection of the airplane for as long as it

is in storage. Do the procedures that follow at the start of the storage cycle

and at the specified intervals. Also, do the short term storage procedures. If

relative humidity is controlled below 70% in area of the electronic

equipment, it is not necessary to remove the electronic equipment from the

airplane.

1. Static the airplane ( PAGEBLOCK 20-41-00/201 ). X

2. Remove the main battery from the airplane. Examine, clean, and put the

battery in a storage area. The battery must be in a discharged condition.

The storage area humidity must be less than 90% and the temperatures

must not be more than 120°F (49°C) ( PAGEBLOCK 24-31-01/401 ).

X

American Airlines

Printed: 8/31/2015; 1:28pm.

Rel. 59.0 - 08/20/15

LAA_B767

AIRCRAFT MAINTENANCE MANUAL

PGBLK EFFECTIVITY: AAL ALL 10-11-02-201

04/22/2012

BOEING PROPRIETARY - Copyright © Unpublished Work Page 12 of 35   

For Reference Only 
Item

Procedures Repeat Intervals

(Days)

Initial 7 14 30 60 90 180 As

Rqd

NOTE: If some electrical components will stay on the airplane, as shown in subsequent steps, do not

remove the battery.

3. Remove the APU battery from the airplane. Examine, clean, and put the

battery in a storage area. The battery must be in a discharged condition.

The storage area humidity must be less than 90% and the temperatures

must not be more than 120°F (49°C) ( PAGEBLOCK 24-31-04/401 ).

X

NOTE: If some electrical components will stay on the airplane, as shown in the subsequent steps, do not

remove the battery.

4. Remove all of the batteries (wet and dry) that follow from the airplane: X

NOTE: When applicable, the batteries that are in the emergency radio beacons, and are found in the

slide/raft covers and the slide raft do not have to be removed. These batteries operate only when

they touch water.

A. Power Megaphone Batteries

B. The Emergency Light Batteries ( PAGEBLOCK 33-51-07/201 or

PAGEBLOCK 33-51-07/201 Config 2 )

C. The Emergency Power Supply Batteries ( PAGEBLOCK 33-51-07/201 or

PAGEBLOCK 33-51-07/201 Config 2 )

D. The batteries which you think are on the airplane in the customer

variable equipment.

CAUTION: REMOVAL OF THE RACK-MOUNTED ELECTRONIC PACKAGES WILL CAUSE A DECREASE OF THE

COOLING AIR TO THE EQUIPMENT THAT IS USUALLY COOLED BY THE ELECTRONICS COOLING

SYSTEM. THE EQUIPMENT NOT REMOVED FROM THE AIRPLANE WILL BECOME TOO HOT IF THE

SPECIFIED PRECAUTIONS ARE NOT FOLLOWED.

5. Remove all rack-mounted electronic packages and make an inspection of

their condition, cleanliness, and signs of corrosion. After the inspection,

pack the components in moisture-resistant containers or plastic bags, and

store them in a bonded area. These electronic packages are found in the

Main Equipment Center, E1, E2, and E3 racks. They area also found in the

E5 Mid Equipment Center, the E6 Aft Equipment Center, and the E7 Voice

and Flight Recorder Shelf. Remove also the Warning Electronic Unit Modules

from the chassis which is found in the P51 rack.

X

6. Remove the video equipment (when installed) from the passenger cabin.

This equipment includes the projectors mounted in the ceilings. It also

includes the VTR, the tuner and control units installed in the out- board

storage bins or other areas such as in the galley.

X

NOTE: Remove the equipment only if the necessary humidity cannot be controlled as specified in the

EQUIPMENT/FURNISHING long term storage procedures.

7. Remove the cards from the P50, P51, P54 and P29 panels and remove

the weather radar transceiver.

NOTE: After the removal of an equipment item, put plugs in the cooling air orifices and the input vents for

components that were removed. This is to make sure an adequate cooling air flow will get to the

components that stay in the airplane.

8. The electrical equipment that follows can stay installed during the time of

storage. This is to supply electrical power for regular system tests, engine

operations, or other installed system tests.

X

Generator Control Units Bus Power Control Units Main Battery Charger APU

American Airlines

Printed: 8/31/2015; 1:28pm.

Rel. 59.0 - 08/20/15

LAA_B767

AIRCRAFT MAINTENANCE MANUAL

PGBLK EFFECTIVITY: AAL ALL 10-11-02-201

04/22/2012

BOEING PROPRIETARY - Copyright © Unpublished Work Page 13 of 35   

For Reference Only 
Item

Procedures Repeat Intervals

(Days)

Initial 7 14 30 60 90 180 As

Rqd

Battery Charger Static Inverter Transformer-Rectifier Units EICAS

Computers Spoiler Control Modules Caution Advisory Computer CSEU Power

Supply Modules

NOTE: When this equipment stays installed, the electrical power must be supplied, and the equipment

operated, each 14- day cycle, Do this for a minimum of 2 hours. External electrical power is

satisfactory. Make sure that the batteries stay in a fully charged condition. Open all switches and

circuit breakers, and disconnect the batteries after the electrical power is removed.

9. The instructions in the FLIGHT CONTROLS storage procedures make it

necessary to operate the flight controls each 90 day cycle. To do this, the

Spoiler Control Modules and the CSEU Power Supply Modules must be

installed in the airplane. Remove or install these modules as specified in the

ELECTRICAL/ELECTRONIC Long Term procedures.

X

10. The POWER PLANT AND APU storage procedures make it necessary to

operate the engines where specified. To do this, the engine N2 speed cards

(2) must be installed in the airplane. Remove or install these N2 speed

cards as specified in the ELECTRICAL/ELECTRONIC Long Term procedures.

X

AIR CONDITIONING SYSTEM

Short Term

To give protection for a maximum of 30 days, do the procedures that follow.

1. Close the ram air inlet ( PAGEBLOCK 21-51-00/501 ) and ram air exhaust

( PAGEBLOCK 21-53-02/501 ) doors.

X

2. Close the E/E cooling inboard supply and outboard exhaust valves (

PAGEBLOCK 21-58-00/001 Config 4 or PAGEBLOCK 21-58-00/001

 Config 6 or PAGEBLOCK 21-58-00/001 Config 7 ).

X

3. Close the outflow valves of the Cabin Pressure Control System (

PAGEBLOCK 21-31-00/001 ).

X

4. Put covers on the static sense port. Use theG00087 fabric Type 1, Class

3. Hold it in place withG02219 Scotch Brand No.471 tape or an equivalent.

X

5. Operate the air conditioning system during each engine or APU operation. X

Long Term

The procedures that follow are for protection of the airplane for a time up to

180 days. Do the procedures that follow at the start of the storage cycle and

at the specified intervals. Also, do the short term storage procedures.

X

1. Put covers on the components that follow. UseG00087 fabric , Type 1,

Class 3. Hold it in position withG02219 Scotch Brand No.471 tape or

equivalent.

X

A. The outflow overpressure relief valves

B. The ram air inlet and exit valves

C. The ground air connect flange

D. The pneumatic ground connect fittings

E. The static sense port

2. When the storage time will be more than 30 days, remove the control

units from the air conditioning system. Put the control units that follow in

X

American Airlines

Printed: 8/31/2015; 1:28pm.

Rel. 59.0 - 08/20/15

LAA_B767

AIRCRAFT MAINTENANCE MANUAL

PGBLK EFFECTIVITY: AAL ALL 10-11-02-201

04/22/2012

BOEING PROPRIETARY - Copyright © Unpublished Work Page 14 of 35   

For Reference Only 
Item

Procedures Repeat Intervals

(Days)

Initial 7 14 30 60 90 180 As

Rqd

storage.

NOTE: This must be done when there is no schedule to operate the air conditioning system.

The Zone Temperature Controller ( PAGEBLOCK 21-61-03/401 )

The Pack Temperature Controller ( PAGEBLOCK 21-51-14/401 )

Effective on: AAL 342-344, 366-399

The Auxiliary Zone Temperature Controller ( PAGEBLOCK 21-61-12/401 )

Effective on: AAL ALL

The Automatic Cabin Pressure Controller ( PAGEBLOCK 21-31-02/401 )

Make sure the E/E cooling system can operate in the standby mode. This is

necessary for the operations specified in the Electrical/Electronics system

storage for ambient temperatures below 90°F (32°C) procedures. For

ambient temperatures above 90°F (32°C) use the Automode for periodic

power operation.

3. When the air conditioning system will stay in the airplane, operate the air

conditioning system during each engine or APU run.

X

HYDRAULIC SYSTEM

Short Term

1. Make a check of the total hydraulic system for hydraulic fluid leakage.

Repair the leakage as necessary. Do this check each 14-day cycle.

X X

2. Make sure the hydraulic system is filled withD00153 hydraulic fluid to the

specified level ( PAGEBLOCK 12-12-01/301 ).

X

3. Clean and apply a layer ofD00153 hydraulic fluid to the bare finished

surfaces on all actuator piston rods, valve slides, and other hydraulic

components.

X

NOTE: Do not use BMS 3–11 or MCS 352B on components that contain MIL-PRF-5606 or MIL-PRF-6083

(i.e., landing gear shock struts).D00054 MCS 352B fluid contains SKYDROL and will cause damage

to the seals that are used in MIL oil systems.

4. Do the servicing of the pneumatic drive for the hydraulic pump gearbox (

PAGEBLOCK 12-13-05/301 ).

X

5. Release the pressure in the hydraulic reservoirs and pressurize them with

dry nitrogen ( PAGEBLOCK 29-11-00/201 ).

X

6. Release the pressure in the hydraulic accumulators that follow and

pressurize them with dry nitrogen.

X

The Parking Brake Accumulator ( PAGEBLOCK 12-15-04/301 ).

The Brake Hydraulic System Surge Accumulator ( PAGEBLOCK 12-15-

09/301 ).

7. Put a screen, mesh cloth, or an equivalent material over the opening of

the pneumatic drive for the air- driven pump exhaust. Attach a red flag to

the material on the opening.

X

Long Term

1. When the storage is more than 30 days the procedures that follow are for

American Airlines

Printed: 8/31/2015; 1:28pm.

Rel. 59.0 - 08/20/15

LAA_B767

AIRCRAFT MAINTENANCE MANUAL

PGBLK EFFECTIVITY: AAL ALL 10-11-02-201

04/22/2012

BOEING PROPRIETARY - Copyright © Unpublished Work Page 15 of 35   

For Reference Only 
Item

Procedures Repeat Intervals

(Days)

Initial 7 14 30 60 90 180 As

Rqd

protection of the airplane for as long as it is in storage. Do the procedures

that follow at the start of the storage cycle and at the specified intervals.

Also, do the short term storage procedures.

A. Each 60-day cycle, make a check of the hydraulic system components

that were cleaned and lubricated withD00153 hydraulic fluid . Make sure

the specified components have a full layer of lubricant and do not have

corrosion.

X X

NOTE: When the lubrication is not complete and some components are corroded, clear the area fully and do

the preservation procedure. Refer to the Boeing Corrosion Manual, document D6-82560, for the

necessary procedures.*[1]

B. Each 180-day cycle, release the pressure in the hydraulic reservoirs and

pressurize them with dry nitrogen ( PAGEBLOCK 29-11-00/201 ).

X X

C. Each 180-day cycle, release the pressure in the hydraulic accumulators

that follow and pressurize them with dry nitrogen.

X X

The Parking Brake Accumulator ( PAGEBLOCK 12-15-04/301 ).

The Brake Hydraulic System Surge Accumulator ( PAGEBLOCK 12-15-

09/301 .)

FLIGHT CONTROLS

Short and Long Term

The procedures that follow are for protection of the airplane for as long as it

is in storage. Do the procedures that follow at the start of the storage cycle

and at the specified intervals.

1. Initially and at each 90-day cycle, operate the flight controls that follow.

Do this for the complete cycles specified below:

A. The leading edge slats (1 cycle) ( PAGEBLOCK 27-81-00/201 ) X X

B. The trailing edge flaps (1 cycle) ( PAGEBLOCK 27-51-00/201 ) X X

C. The spoilers (3 cycles) ( PAGEBLOCK 27-61-00/201 ) X X

D. The ailerons (3 cycles) ( PAGEBLOCK 27-11-00/501 ) X X

E. The elevators (3 cycles) ( PAGEBLOCK 27-31-00/501 ) X X

F. The rudder (3 cycles) ( PAGEBLOCK 27-21-00/501 Config 1 or

PAGEBLOCK 27-21-00/501 Config 2 )

X X

G. The horizontal stabilizer (3 cycles). Put the stabilizer to a different

stabilizer trim position for each cycle ( PAGEBLOCK 27-41-00/501 ).

X X

2. After the flight controls have been cycled, put the flaps and slats to the

retracted position. Also put the control surfaces to the neutral position (

PAGEBLOCK 27-51-00/201 and PAGEBLOCK 27-81-00/201 ).

X X

3. Initially and at each 90-day cycle, operate the rudder trim (

PAGEBLOCK 27-21-00/501 Config 1 or PAGEBLOCK 27-21-00/501

 Config 2 ) and the aileron trim ( PAGEBLOCK 27-11-00/501 ) for one

complete cycle. Put the stabilizer trim, the rudder trim, and aileron trim to a

different position than it was set during the last cycle.

X X

NOTE: You can use external electrical and hydraulic power when the airplane power is not available.

American Airlines

Printed: 8/31/2015; 1:28pm.

Rel. 59.0 - 08/20/15

LAA_B767

AIRCRAFT MAINTENANCE MANUAL

PGBLK EFFECTIVITY: AAL ALL 10-11-02-201

04/22/2012

BOEING PROPRIETARY - Copyright © Unpublished Work Page 16 of 35   

For Reference Only 
Item

Procedures Repeat Intervals

(Days)

Initial 7 14 30 60 90 180 As

Rqd

4. Initially and at each 90-day cycle, lubricate all joints and gearbox service

points withD00633 grease ( PAGEBLOCK 12-21-04/301 through

PAGEBLOCK 12-21-10/301 ).

X X

5. Initially and at each 90-day cycle, lubricate all specified control cables (

PAGEBLOCK 12-21-31/301 ).

X X

NOTE: This does not include the cables that are in the body of the airplane.

6. Initially and at each 1-year cycle, lubricate the control cables that are in

the body of the airplane ( PAGEBLOCK 12-21-31/301 ).

X YR

7. Lubricate all of the bearings on all of the hydraulic components and

linkages that have lubrication fittings.

X

OXYGEN SYSTEM

Short Term

When an airplane is put in storage for time that is not more than 60 days,

no special precautions are necessary. But, you must make sure that the

high pressure valves on the oxygen supply cylinders are closed. These

oxygen cylinders are for the crew and the passenger systems.

Long Term

The procedures that follow are for protection of the airplane for as long as it

is in storage. Do the procedures that follow at the start of the storage cycle

and at the specified intervals.

WARNING: OBEY THE PRECAUTIONS FOR THE REMOVAL AND INSTALLATION OF THE OXYGEN CYLINDERS.

IF YOU DO NOT OBEY THE PRECAUTIONS, INJURIES TO PERSONNEL, AND DAMAGE TO

EQUIPMENT CAN OCCUR.

1. Remove the portable oxygen cylinders, the crew oxygen cylinders, and

the regulator ( PAGEBLOCK 12-15-08/301 ). Obey your airline's procedures

to put them in a spares storage.

X

NOTE: Attach a tag that identifies each cylinder as a serviceable part when the pressure is above 50 psi.

Also do this if the hydrostatic test date has not expired. When the hydrostatic test date has expired,

follow the operator's standard procedures.

2. Put aSTD-1130 tube cap on the cylinder end of the oxygen distribution

lines. Also, put a cap on the connector end of the hoses that are in the

oxygen mask stowage boxes. Put cleanSTD-1106 polyethylene bags (1 pint)

on the lines and hoses that have the caps. Attach red flags to the bags.

X

3. Remove the crew system oxygen masks. Put the masks in clean

polyethylene bags and send them back to spares. Cap the oxygen hose

connector part of stowage box assembly and put it away.

X

POTABLE WATER SYSTEM

Short and Long Term

1. Drain all of the water system. This includes the galley and the lavatory

tanks. Do a purge of the complete potable water system with dry air and

nitrogen. Close and seal all of the drains.

X

2. Remove all of the coffeemakers and water boilers from airplane. Store

them at temperatures that do not freeze.

X

POWER PLANT AND APU

American Airlines

Printed: 8/31/2015; 1:28pm.

Rel. 59.0 - 08/20/15

LAA_B767

AIRCRAFT MAINTENANCE MANUAL

PGBLK EFFECTIVITY: AAL ALL 10-11-02-201

04/22/2012

BOEING PROPRIETARY - Copyright © Unpublished Work Page 17 of 35   

For Reference Only 
Item

Procedures Repeat Intervals

(Days)

Initial 7 14 30 60 90 180 As

Rqd

1. Refer to ( GE: PAGEBLOCK 71-00-03/201 or GA: PAGEBLOCK 71-00-

03/201 ) for maintenance procedures that are applicable to engine storage.

X

2. Refer to ( PAGEBLOCK 49-11-00/201 1) for procedures that are

applicable to APU storage.

X

3. If the airplane is stored without engines do these steps: X

A. Cap and stow all fuel lines, hydraulic lines and wire bundles. X

B. Cover exposed metal surfaces on the pylon with a moisture barrier. X

C. Provide suitable drains in the moisture barrier to allow the escapement of

water.

X

D. Use a desiccant within the moisture barrier to maintain a low humidity

around the pylon.

X

*[1] Revision service for the Boeing Corrosion Manual, document D6-82560 will be discontinued. The related

corrosion prevention information is being incorporated into the Aircraft Maintenance Manual (AMM) or the

Structural Repair Manual (SRM).

(a) Make sure that you install streamers:

1 G02444 "STATIC PORTS COVERED" tag (P/N 2000S, or equivalent)

2 G02447 "PITOT PROBES COVERED" tag (P/N 1000P or equivalent)

(b) Additional consumable materials:

1 Turbo Oil 2197 CPN 4077968 (See Note)

NOTE: Turbo Oil 2197, CPN 4077968, is the preferred oil for APU's. If Turbo Oil

2197 is not available, Turbo Oil 2380, CPN 5736082, may be used. Notify

Maintenance Control when intermixing is necessary.

2 B01000 Series 80 solvent

American Airlines

Printed: 8/31/2015; 1:28pm.

Rel. 59.0 - 08/20/15

LAA_B767

AIRCRAFT MAINTENANCE MANUAL

PGBLK EFFECTIVITY: AAL ALL 10-11-02-201

04/22/2012

BOEING PROPRIETARY - Copyright © Unpublished Work Page 18 of 35   

For Reference Only 
Task 10-11-02-632-002 "USE MCM CARD 05-92-16, 05-92-63, 05-92-65, 05-92-79, as required by GPM 03-07"

Put the Airplane Back to a Serviceable Condition After Storage

Effective on: AAL ALL

F. General

(1) This procedure provides the instructions on how to put the airplane back to service after

storage.

G. References

Reference Title

07-11-01-582-015 Lift the Airplane with Jacks (P/B 201)

10-11-01-582-001 Airplane Normal Parking (P/B 201)

12-11-01 P/B 301 FUEL TANK PRESSURE FUELING - SERVICING

12-12-01-613-059 Hydraulic Reservoir Servicing - Manual Procedure (P/B 301)

12-12-01-613-060 Hydraulic Reservoir Servicing - Pressure Procedure (P/B 301)

12-14-01 P/B 301 POTABLE WATER SYSTEM - SERVICING

12-15-01-613-021 Main Gear Shock Strut Servicing (P/B 301)

12-15-02-613-031 Nose Gear Shock Strut Servicing (P/B 301)

12-15-03 P/B 301 LANDING GEAR TIRES - SERVICING

12-15-04-613-001 Parking Brake Accumulator Servicing (P/B 301)

12-15-08 P/B 301 OXYGEN - SERVICING

12-15-09-613-001 Surge Accumulator Servicing for the Brake Hydraulic System (P/B 301)

12-16-01-613-002 Service the Rain Repellent Bottle (P/B 301)

12-17-01 P/B 301 WASTE TANK - SERVICING

12-21-13-603-001 Nose Landing Gear Doors and the Operating Mechanisms Lubrication (P/B 301)

12-21-14 P/B 301 MAIN GEAR AND ACTUATING MECHANISMS - SERVICING

12-21-15 P/B 301 MAIN GEAR DOORS AND ACTUATING MECHANISMS - SERVICING

12-21-31 P/B 301 CONTROL CABLES - SERVICING (LUBRICATION)

12-25-01 P/B 301 CLEANING AND POLISHING-SERVICING

20-30-80-102-001 General Cleaning of Metal (Series 80) (P/B 201)

21-00-00 P/B 201 AIR CONDITIONING - GENERAL - MAINTENANCE/PRACTICES

24-11-00 P/B 501 INTEGRATED DRIVE GENERATOR (IDG) SYSTEM - ADJUSTMENT/TEST

24-21-00 P/B 501 APU GENERATOR - ADJUSTMENT/TEST

24-22-00-860-802 Supply and Remove Electrical Power (P/B 201)

American Airlines

Printed: 8/31/2015; 1:28pm.

Rel. 59.0 - 08/20/15

LAA_B767

AIRCRAFT MAINTENANCE MANUAL

PGBLK EFFECTIVITY: AAL ALL 10-11-02-201

04/22/2012

BOEING PROPRIETARY - Copyright © Unpublished Work Page 19 of 35   

For Reference Only 
Reference Title

24-25-00 P/B 501 HYDRAULIC MOTOR GENERATOR SYSTEM - ADJUSTMENT/TEST

24-30-00 P/B 501 DC GENERATION - ADJUSTMENT/TEST

24-31-01 P/B 401 MAIN BATTERY - REMOVAL/INSTALLATION

24-31-04 P/B 401 APU BATTERY - REMOVAL/INSTALLATION

24-33-00 P/B 601 STANDBY POWER - INSPECTION/CHECK

24-41-00 P/B 501 EXTERNAL POWER - ADJUSTMENT/TEST

25-31-03 P/B 401 GALLEY ELECTRICAL LOAD CONTROL UNITS - REMOVAL/INSTALLATION

27-00-01 P/B 201 FLIGHT CONTROL CABLES - MAINTENANCE PRACTICES

27-09-00 P/B 201 FLIGHT CONTROL SYSTEM ELECTRONICS UNIT (CSEU) - MAINTENANCE PRACTICES

27-11-00 P/B 501 AILERON AND AILERON TRIM CONTROL SYSTEM - ADJUSTMENT/TEST

27-13-00 P/B 601 LATERAL CONTROL SHUTOFF VALVES - INSPECTION/CHECK

27-18-00 P/B 501 AILERON POSITION INDICATING SYSTEM - ADJUSTMENT/TEST

27-21-00

P/B 501 Config 1

RUDDER AND RUDDER TRIM CONTROL SYSTEM - ADJUSTMENT/TEST

27-21-00

P/B 501 Config 2

RUDDER AND RUDDER TRIM CONTROL SYSTEM - ADJUSTMENT/TEST

27-23-00 P/B 501 RUDDER AND ELEVATOR SHUTOFF VALVES - ADJUSTMENT/TEST

27-28-00 P/B 501 RUDDER POSITION INDICATING SYSTEM - ADJUSTMENT/TEST

27-31-00 P/B 501 ELEVATOR CONTROL SYSTEM - ADJUSTMENT/TEST

27-32-00

P/B 501 Config 1

STALL WARNING SYSTEM - ADJUSTMENT/TEST

27-32-00

P/B 501 Config 3

STALL WARNING SYSTEM - ADJUSTMENT/TEST

27-38-00 P/B 501 ELEVATOR POSITION INDICATING SYSTEM - ADJUSTMENT/TEST

27-41-00 P/B 501 HORIZONTAL STABILIZER TRIM CONTROL SYSTEM - ADJUSTMENT/TEST

27-48-00 P/B 501 STABILIZER TRIM POSITION INDICATING SYSTEM - ADJUSTMENT/TEST

27-51-00 P/B 501 TRAILING EDGE FLAP SYSTEM - ADJUSTMENT/TEST

27-58-00 P/B 501 TRAILING EDGE FLAP POSITION INDICATING SYSTEM - ADJUSTMENT/TEST

27-61-00 P/B 501 SPOILER/SPEEDBRAKE CONTROL SYSTEM - ADJUSTMENT/TEST

27-62-00 P/B 501 AUTO-SPEEDBRAKE CONTROL SYSTEM - ADJUSTMENT/TEST

27-81-00 P/B 501 LEADING EDGE SLAT SYSTEM - ADJUSTMENT/TEST

27-88-00 P/B 501 LEADING EDGE SLAT POSITION INDICATING SYSTEM - ADJUSTMENT/TEST

American Airlines

Printed: 8/31/2015; 1:28pm.

Rel. 59.0 - 08/20/15

LAA_B767

AIRCRAFT MAINTENANCE MANUAL

PGBLK EFFECTIVITY: AAL ALL 10-11-02-201

04/22/2012

BOEING PROPRIETARY - Copyright © Unpublished Work Page 20 of 35   

For Reference Only 
Reference Title

28-10-00-202-001 Microbial Growth Detection Test (P/B 201)

28-11-00 P/B 201 FUEL TANKS - MAINTENANCE PRACTICES

28-22-07 P/B 601 FUEL LINES AND FITTINGS - INSPECTION/CHECK

28-26-00 P/B 201 DEFUELING - MAINTENANCE PRACTICES

29-11-00 P/B 501 MAIN (LEFT, RIGHT, AND CENTER) HYDRAULIC SYSTEMS - ADJUSTMENT/TEST

29-11-00 P/B 601 MAIN (LEFT, RIGHT, AND CENTER) HYDRAULIC SYSTEMS - INSPECTION/CHECK

29-11-00-860-801 Main (Left, Right, Center) Hydraulic System Pressurization (P/B 201)

29-11-15 P/B 401 LEFT AND RIGHT SYSTEM RETURN FILTER MODULE AND COMPONENTS - REMOVAL/INSTALLATION

29-11-16 P/B 401 CENTER SYSTEM RETURN FILTER MODULE AND COMPONENTS - REMOVAL/INSTALLATION

29-11-17 P/B 401 LEFT AND RIGHT SYSTEM ENGINE-DRIVEN PUMP (EDP) PRESSURE/CASE DRAIN FILTER MODULE AND

COMPONENTS - REMOVAL/INSTALLATION

29-11-18 P/B 401 ALTERNATING CURRENT MOTOR PUMP (ACMP) PRESSURE/CASE DRAIN FILTER MODULE AND COMPONENTS

- REMOVAL/INSTALLATION

29-11-19 P/B 401 CENTER SYSTEM AIR DRIVEN PUMP (ADP) PRESSURE/CASE DRAIN FILTER MODULE AND COMPONENTS -

REMOVAL/INSTALLATION

29-21-00 P/B 501 RAM AIR TURBINE (RAT) SYSTEM - ADJUSTMENT/TEST

29-31-00 P/B 501 HYDRAULIC PRESSURE INDICATING SYSTEM - ADJUSTMENT/TEST

29-32-00 P/B 501 HYDRAULIC FLUID TEMPERATURE INDICATING SYSTEM - ADJUSTMENT/TEST

29-33-00 P/B 501 HYDRAULIC FLUID QUANTITY INDICATING SYSTEM - ADJUSTMENT/TEST

30-31-00 P/B 501 PITOT STATIC PROBE ANTI-ICING - ADJUSTMENT/TEST

30-42-00 P/B 601 WINDSHIELD WIPER SYSTEM - INSPECTION/CHECK

32-00-20 P/B 201 LANDING GEAR DOWNLOCKS - MAINTENANCE PRACTICES

32-00-20-402-006 Install the Downlocks on the Landing Gear (P/B 201)

32-41-08

P/B 601 Config 2

MAIN GEAR WHEEL BRAKES - INSPECTION/CHECK

32-41-08

P/B 601 Config 3

MAIN GEAR WHEEL BRAKES - INSPECTION/CHECK

32-45-01-004-001 Main Gear Wheel and Tire Assembly Removal (P/B 401)

32-45-01-404-027 Main Gear Wheel and Tire Assembly Installation (P/B 401)

32-45-02-004-039 Nose Gear Wheel and Tire Assembly Removal (P/B 401)

32-45-02-404-020 Nose Gear Wheel and Tire Assembly Installation (P/B 401)

32-45-03 P/B 601 WHEELS - INSPECTION/CHECK

American Airlines

Printed: 8/31/2015; 1:28pm.

Rel. 59.0 - 08/20/15

LAA_B767

AIRCRAFT MAINTENANCE MANUAL

PGBLK EFFECTIVITY: AAL ALL 10-11-02-201

04/22/2012

BOEING PROPRIETARY - Copyright © Unpublished Work Page 21 of 35   

For Reference Only 
Reference Title

32-45-03

P/B 601 Config 2

WHEELS - INSPECTION/CHECK

33-11-00 P/B 501 FLIGHT COMPARTMENT ILLUMINATION - ADJUSTMENT/TEST

33-13-00 P/B 501 INTEGRAL PANEL LIGHTS - ADJUSTMENT/TEST

33-16-00 P/B 501 MASTER DIM AND TEST - ADJUSTMENT/TEST

33-22-00 P/B 501 PASSENGER LOADING LIGHTS - ADJUSTMENT/TEST

33-42-00 P/B 501 LANDING, RUNWAY TURNOFF AND TAXI LIGHTS - ADJUSTMENT/TEST

33-43-00 P/B 501 POSITION LIGHTS - ADJUSTMENT/TEST

33-44-00 P/B 501 ANTI-COLLISION LIGHTS - ADJUSTMENT/TEST

33-51-00 P/B 501 EMERGENCY LIGHTS - ADJUSTMENT/TEST

34-11-00 P/B 301 PITOT-STATIC SYSTEM-SERVICING

34-23-00 P/B 201 STANDBY MAGNETIC COMPASS - MAINTENANCE PRACTICES

35-00-00 P/B 201 OXYGEN - MAINTENANCE PRACTICES

38-10-00 P/B 201 POTABLE WATER SYSTEM - MAINTENANCE PRACTICES

38-15-02 P/B 401 AIR FILTER - REMOVAL/INSTALLATION

38-32-00 P/B 501 VACUUM WASTE SYSTEM - ADJUSTMENT/TEST

49-11-00 P/B 201 AUXILIARY POWER UNIT - MAINTENANCE PRACTICES

GA: 71-00-00

P/B 201

POWER PLANT (OPERATING PROCEDURES) - MAINTENANCE PRACTICES

GE: 71-00-00

P/B 201

POWER PLANT (OPERATING PROCEDURES) - MAINTENANCE PRACTICES

H. Consumable Materials

Reference Description Specification

B00643 Remover - Alkaline Removable Coating BMS15-12, Type II

D00013 Grease - Aircraft And Instrument Grease MIL-PRF-23827 (NATO G-354)

(Supersedes MIL-G-23827)

D00233 Grease - Aircraft, General Purpose, Wide Temperature - Mobil 28 MIL-PRF-81322

D00378 Grease - Aircraft, General Purpose, Wide Temperature - Aeroshell 22 MIL-PRF-81322

D00633 Grease - Aircraft General Purpose BMS3-33

G00009 Compound - Organic Corrosion Inhibiting BMS3-23

G02444 Tag - Red Paper, "STATIC PORTS COVERED" - 3 inches (76.2 mm) Wide,

6 inches (152.4 mm) Long

American Airlines

Printed: 8/31/2015; 1:28pm.

Rel. 59.0 - 08/20/15

LAA_B767

AIRCRAFT MAINTENANCE MANUAL

PGBLK EFFECTIVITY: AAL ALL 10-11-02-201

04/22/2012

BOEING PROPRIETARY - Copyright © Unpublished Work Page 22 of 35   

For Reference Only 
Reference Description Specification

G02447 Tag - Red Paper, "PITOT PROBES COVERED" - 3 inches (76.2 mm) Wide,

6 inches (152.4 mm) Long

I. Clean the Airplane

Effective on: AAL ALL

SUBTASK 480-001

(1) If it is necessary, attach the static ports and pitot probe covers on the airplane ( TASK 10-11-01-582-001 ).

Effective on: AAL ALL

SUBTASK 612-003

(2) Remove the temporary layer of protective coating that was installed in the EXTERNAL SURFACE PROTECTION

procedure of the Long Term storage as follow:

CAUTION: DO NOT LET THE REMOVER BECOME DRY. DO NOT LET THE REMOVER TOUCH AN

ACRYLIC SURFACE FOR MORE THAN 60 MINUTES. DO NOT LET THE REMOVER TOUCH

HIGH-STRENGTH STEEL PARTS (180,000 PSI AND OVER) OR WHEELS, BRAKES AND

TIRES. IF YOU DO NOT OBEY THESE INSTRUCTIONS, DAMAGE TO THE COMPONENTS

CAN OCCUR.

(a) Apply the B00643 remover . Put the remover on approximately 20 mils thick and for a dwell time

of not less than 10 minutes.

1 Pressure rinse the area with water.

NOTE: Make sure that the water temperature is not more than 140°F (60°C).

(b) Remove the tape from the control cabin windows and windshields.

Effective on: AAL ALL

SUBTASK 612-004

(3) Clean the airplane ( PAGEBLOCK 12-25-01/301 ).

J. Landing Gear

Effective on: AAL ALL

SUBTASK 632-005

(1) Make sure you put the landing gear back to a serviceable condition. Do the steps that follow:

(a) Before you pressurize the landing gear, do these steps:

1 Make sure that all landing gear are locked in the down position ( PAGEBLOCK 32-00-

20/201 ).

2 Make sure that the downlocks are installed on the nose and main landing gear.

a If it is necessary, do this task: Install the Downlocks on the Landing

Gear, TASK 32-00-20-402-006

3 Make sure that the landing gear control handle, on the first officer's instrument

panel, is in the DOWN position.

4 Make sure that the main landing gear doors are closed.

5 Make sure that the ground door release handles for the main landing gear doors, are

in the DOOR CLOSE position. You can find the ground door release handles aft of the

American Airlines

Printed: 8/31/2015; 1:28pm.

Rel. 59.0 - 08/20/15

LAA_B767

AIRCRAFT MAINTENANCE MANUAL

PGBLK EFFECTIVITY: AAL ALL 10-11-02-201

04/22/2012

BOEING PROPRIETARY - Copyright © Unpublished Work Page 23 of 35   

For Reference Only 
main landing gear doors.

NOTE: When the doors are open, the door release handle cannot be put in the

DOORS CLOSED position. This cannot be done until the center hydraulic

system is pressurized.

6 Make sure that the forward doors of the nose landing gear are open.

7 Make sure that the torsion link of the nose landing gear is connected.

(b) Before you energize the airplane electrical system, do these steps:

1 Make sure that the alternate extension select switch is in the OFF position.

NOTE: The alternate extension select switch is found on the pilot's center

instrument panel, P3.

Effective on: AAL ALL

SUBTASK 642-006

(2) Lubricate the landing gear as follows:

(a) Lubricate the doors for nose landing gear with D00633 grease or optional D00013 grease (

TASK 12-21-13-603-001 ).

(b) Lubricate the doors for the main landing gear with D00633 grease or optional D00013 grease (

PAGEBLOCK 12-21-15/301 ).

NOTE: This includes the uplock hooks for the main landing gear.

(c) Lubricate the joints of the nose landing gear and actuator mechanisms that have fittings with

D00633 grease or optional D00013 grease ( TASK 12-21-13-603-001 ).

(d) Lubricate the joints of the main landing gear and actuator mechanisms that have fittings with

D00633 grease or optional D00013 grease ( PAGEBLOCK 12-21-14/301 ).

Effective on: AAL ALL

SUBTASK 212-007

(3) Examine the door areas of the nose and main landing gear.

(a) Make sure that there are no persons or equipment in the area.

Effective on: AAL ALL

SUBTASK 860-001

(4) Do this task to supply electrical power: Supply and Remove Electrical Power, TASK 24-22-00-860-802 .

Effective on: AAL ALL

SUBTASK 860-002

WARNING: KEEP PERSONNEL AND EQUIPMENT AWAY FROM THE FLIGHT CONTROL SURFACES, THE THRUST

REVERSERS, AND THE LANDING GEAR. THESE COMPONENTS CAN MOVE SUDDENLY WHEN YOU

SUPPLY HYDRAULIC POWER. THIS CAN CAUSE INJURIES TO PERSONNEL AND DAMAGE TO

EQUIPMENT.

(5) Do this task to supply the left, center, and right hydraulic power: Main (Left, Right, Center) Hydraulic System

Pressurization, TASK 29-11-00-860-801 .

Effective on: AAL ALL

SUBTASK 862-011

American Airlines

Printed: 8/31/2015; 1:28pm.

Rel. 59.0 - 08/20/15

LAA_B767

AIRCRAFT MAINTENANCE MANUAL

PGBLK EFFECTIVITY: AAL ALL 10-11-02-201

04/22/2012

BOEING PROPRIETARY - Copyright © Unpublished Work Page 24 of 35   

For Reference Only 
(6) Operate the doors of the main landing gear, 2 or 3 times.

NOTE: This is to find if they move freely when you use the ground release handles.

Effective on: AAL ALL

SUBTASK 612-012

(7) Do this task: Main Gear Shock Strut Servicing, TASK 12-15-01-613-021 ).

Effective on: AAL ALL

SUBTASK 612-013

(8) Do this task: Nose Gear Shock Strut Servicing, TASK 12-15-02-613-031 .

Effective on: AAL ALL

SUBTASK 612-014

(9) When there is too much grease on the inner cylinders of the shock struts, clean it off.

Effective on: AAL ALL

SUBTASK 092-015

(10) Remove the tie down straps and the wheel chocks.

Effective on: AAL ALL

SUBTASK 022-066

(11) Remove the wheel/brake covers.

Effective on: AAL ALL

SUBTASK 582-016

(12) Do this task: Lift the Airplane with Jacks, TASK 07-11-01-582-015 .

Effective on: AAL ALL

SUBTASK 030-001

(13) Do this task: ( Main Gear Wheel and Tire Assembly Removal, TASK 32-45-01-004-001 ).

Effective on: AAL ALL

SUBTASK 030-002

(14) Do this task: Nose Gear Wheel and Tire Assembly Removal, TASK 32-45-02-004-039 .

Effective on: AAL ALL

SUBTASK 022-017

(15) Apply lubricant on the nose and main gear wheels as follow::

(a) Do an inspection of the wheel bearings and the cups in the wheels ( PAGEBLOCK 32-45-03/601 or

PAGEBLOCK 32-45-03/601 Config 2 ).

(b) Fill the wheel bearings with D00378 Aeroshell 22 grease or D00233 Mobil 28 grease .

(c) Put the wheel bearings in the wheels.

Effective on: AAL ALL

SUBTASK 430-001

(16) Do this task: Main Gear Wheel and Tire Assembly Installation, TASK 32-45-01-404-027 .

American Airlines

Printed: 8/31/2015; 1:28pm.

Rel. 59.0 - 08/20/15

LAA_B767

AIRCRAFT MAINTENANCE MANUAL

PGBLK EFFECTIVITY: AAL ALL 10-11-02-201

04/22/2012

BOEING PROPRIETARY - Copyright © Unpublished Work Page 25 of 35   

For Reference Only 
Effective on: AAL ALL

SUBTASK 430-002

(17) Do this task: Nose Gear Wheel and Tire Assembly Installation, TASK 32-45-02-404-020 .

Effective on: AAL ALL

SUBTASK 212-065

(18) Inspect the brakes for damage ( PAGEBLOCK 32-41-08/601 Config 2 or PAGEBLOCK 32-41-08/601 Config 3 ).

Effective on: AAL ALL

SUBTASK 612-018

(19) Make sure that the tires are inflated to the specified pressure with nitrogen ( PAGEBLOCK 12-15-03/301 ).

K. Fuel System

Effective on: AAL ALL

SUBTASK 632-019

(1) Remove the items that follow from each vent opening and each cavity opening:

(a) The screen

(b) The mesh cloth

(c) The red flags

(d) The 3M tape.

(e) All other equivalent material

Effective on: AAL ALL

SUBTASK 652-020

(2) Do the servicing of the fuel tanks as follows:

(a) Defuel the fuel tanks ( PAGEBLOCK 28-26-00/201 ).

(b) Do this task: Microbial Growth Detection Test, TASK 28-10-00-202-001

(c) When the airplane has been in storage for more than 12 months do these steps:

1 Go into the fuel tanks ( PAGEBLOCK 28-11-00/201 ).

2 Examine the fuel tanks for structural corrosion.

(d) Apply G00009 corrosion inhibiting compound , Type II to the engine dry bays, and center wing

dry cavity (if it is applicable).

NOTE: This will remove the moisture that collects.

(e) Refuel the airplane (fill all serviceable fuel tanks to full) ( PAGEBLOCK 12-11-01/301 ).

NOTE: When it is possible, do not operate the airplane for 24 hours. After 24 hours, examine

it for external fuel leaks.

Effective on: AAL ALL

SUBTASK 792-021

American Airlines

Printed: 8/31/2015; 1:28pm.

Rel. 59.0 - 08/20/15

LAA_B767

AIRCRAFT MAINTENANCE MANUAL

PGBLK EFFECTIVITY: AAL ALL 10-11-02-201

04/22/2012

BOEING PROPRIETARY - Copyright © Unpublished Work Page 26 of 35   

For Reference Only 
(3) Do the leakage test for the fuel system tubing ( PAGEBLOCK 28-22-07/601 ).

L. Electrical/Electronics Systems

Effective on: AAL ALL

SUBTASK 632-022

(1) Make sure that the Electrical/Electronic systems are serviceable as follows:

(a) Make sure that the electrical ground is installed on the airplane.

(b) Make sure that the Electrical/Electronic systems circuit breakers are open.

(c) Make sure that the Electrical/Electronic systems switches are in the OFF position.

(d) Make sure that the equipment racks are clean, dry, and have no corrosion.

(e) Remove the plugs that were installed in the cooling air orifices and the input vents. These plugs

were installed when the components were removed at the start of the storage.

were installed when the components were removed at the start of the storage.

(f) Install all of the electronic modules and cards that were removed in the FLIGHT DECK procedures

for Long Term storage when it is necessary.

Effective on: AAL ALL

SUBTASK 712-023

(2) Do an operational test of the electrical/electronic components that are installed.

(a) PAGEBLOCK 24-11-00/501 IDG System

(b) PAGEBLOCK 24-21-00/501 APU Generator

(c) PAGEBLOCK 24-25-00/501 HMG System

(d) PAGEBLOCK 24-30-00/501 DC Generation

(e) PAGEBLOCK 24-33-00/601 Standby Power

(f) PAGEBLOCK 24-41-00/501 External power

(g) PAGEBLOCK 25-31-03/401 Galley Power

(h) PAGEBLOCK 33-11-00/501 Flight Compartment Illumination

(i) PAGEBLOCK 33-13-00/501 Integral Panel Lights

(j) PAGEBLOCK 33-16-00/501 Master Dim and Test

(k) PAGEBLOCK 33-22-00/501 Passenger Loading Lights

(l) PAGEBLOCK 33-42-00/501 Landing, Runway Turnoff and Taxi lights

(m) PAGEBLOCK 33-43-00/501 Position Lights

(n) PAGEBLOCK 33-44-00/501 Anti-collision Lights

Effective on: AAL ALL

SUBTASK 422-024

(3) Install all of the batteries that were removed for storage.

American Airlines

Printed: 8/31/2015; 1:28pm.

Rel. 59.0 - 08/20/15

LAA_B767

AIRCRAFT MAINTENANCE MANUAL

PGBLK EFFECTIVITY: AAL ALL 10-11-02-201

04/22/2012

BOEING PROPRIETARY - Copyright © Unpublished Work Page 27 of 35   

For Reference Only 
Effective on: AAL ALL

SUBTASK 762-025

(4) Make sure that these batteries are fully charged:

(a) The Main battery ( PAGEBLOCK 24-31-01/401 )

(b) The APU battery ( PAGEBLOCK 24-31-04/401 ).

Effective on: AAL ALL

SUBTASK 722-059

(5) Do a functional test of these batteries:

(a) The main battery

(b) The APU battery

Effective on: AAL ALL

SUBTASK 862-077

(6) If the batteries were not removed at the start of the storage, close all circuit breakers.

NOTE: If the PARKING BRAKE VALVE circuit breaker and the AUTOBK/ANTISKID TEST IND circuit breakers

were opened, close these circuit breakers. Do this in the sequence that follows to prevent EICAS and

BITE messages that are errors.

(a) Close these circuit breakers:

Circuit Breaker Panel, P11

Row Col Number Name

U 12 C01176 AUTOBRKS ANTISKID TEST/IND 1

U 21 C01173 AUTOBRKS ANTISKID TEST/IND 2

Main Power Distribution Panel, P6

Row Col Number Name

Effective on: AAL 305-307, 316, 319-325, 327-329, 332, 335, 336, 338, 339, 342-399; AAL

301-304 POST SB 767-24-0007

F 4 C01179 PARKING BRAKE VALVE

Effective on: AAL ALL

SUBTASK 712-062

(7) Do the system test of the emergency light system ( EMERGENCY LIGHTS - ADJUSTMENT/TEST, PAGEBLOCK 33-

51-00/501 ).

(a) If the airplane was parked for less than 7 days, no procedures are necessary if the emergency

light system was completely charged before it was parked.

NOTE: This is if the emergency light system was not operated while the airplane was parked.

CAUTION: IF POWER HAS NOT BEEN APPLIED TO THE INSTALLED EMERGENCY LIGHT SYSTEM

WHILE THE AIRPLANE WAS PARKED FOR 6 DAYS OR MORE, DO NOT TURN ON ANY

ASSEMBLY FOR A MINIMUM OF 16 HOURS AFTER YOU APPLY POWER TO THE SYSTEM.

DO NOT DO A SYSTEM FUNCTIONAL TESTS FOR A MINIMUM OF 20 HOURS AFTER YOU

APPLY POWER TO THE SYSTEM.

American Airlines

Printed: 8/31/2015; 1:28pm.

Rel. 59.0 - 08/20/15

LAA_B767

AIRCRAFT MAINTENANCE MANUAL

PGBLK EFFECTIVITY: AAL ALL 10-11-02-201

04/22/2012

BOEING PROPRIETARY - Copyright © Unpublished Work Page 28 of 35   

For Reference Only 
(b) Do a charge of the emergency light system for 16 hours if:

1 The airplane was parked for 6 days or more.

2 The emergency light system was not fully charged before the airplane was parked.

3 The emergency light system was operated while the airplane was parked.

M. Flight Compartment Equipment

Effective on: AAL ALL

SUBTASK 632-028

(1) Do the steps to make the flight compartment equipment serviceable:

WARNING: MAKE SURE THAT YOU REMOVE ALL COVERS FROM PITOT PROBES. IF YOU DO NOT

REMOVE PITOT PROBE COVERS BEFORE FLIGHT, THE PITOT PROBE COVERS CAN

CAUSE INCORRECT AIR DATA. INCORRECT AIR DATA CAN MAKE FLIGHT DANGEROUS.

CAUTION: REMOVE THE PROTECTION COVERS FROM ALL OPENINGS. DAMAGE TO THE ENGINE

CAN OCCUR.

CAUTION: LOOK FOR DAMAGE OF THE PITOT-STATIC PROBE COVERS. MAKE SURE THAT THERE IS

NO FRAYING AROUND THE COVER OPENING OR OTHER DAMAGE. THE FIBERS GET

CONTAMINATION (DIRT, GREASE, AND FLUIDS) THAT CAN CAUSE BLOCKAGE OF THE

PROBE.

(a) Remove the covers [4] from the pitot-static probes.

(b) Remove the G02447 "PITOT PROBES COVERED" tag from the left control wheel in the flight

compartment.

(c) Remove the tape or covers from the these components:

1 The total air temperature probes

2 The angle-of-attack sensors

3 The ice detector (when installed)

WARNING: MAKE SURE THAT ALL BARRICADE TAPE, VINYL ADHESIVE TAPE, AND TAPE RESIDUE

IS REMOVED FROM THE STATIC PORTS. IF THE HOLES BECOME CLOGGED WITH TAPE

RESIDUE, INCORRECT AIRSPEED-SENSING AND ALTITUDE-SENSING SIGNALS CAN

OCCUR. THIS CAN CAUSE DANGEROUS FLIGHT CONDITIONS.

CAUTION: REMOVE ALL OF THE BARRICADE TAPE, AND VINYL ADHESIVE TAPE. DO NOT OPERATE

THE ENGINES WITH THE COVERS ON. THE COVERS CAN COME OFF AND CAUSE

DAMAGE TO THE ENGINES.

(d) Remove all barricade tape and vinyl adhesive tape from the static ports.

1 Inspect each static port and if necessary use naphtha or equivalent to remove all

tape residue, dirt and other contaminants around the port.

(e) Remove the G02444 "STATIC PORTS COVERED" tag from the left control wheel in the flight deck.

Effective on: (AAL 301-307, 316, 319-325, 327-329, 332, 335, 336, 338, 339, 351-391 PRE SB 767-

30-0028) 301-307, 316-316, 319-325, 327-329, 332-332, 335-336, 338-339, 351-391

(f) Install the pressurized rain repellent bottle ( TASK 12-16-01-613-002 ).

(g) Make a check of the windshield wiper system ( PAGEBLOCK 30-42-00/601 ).

American Airlines

Printed: 8/31/2015; 1:28pm.

Rel. 59.0 - 08/20/15

LAA_B767

AIRCRAFT MAINTENANCE MANUAL

PGBLK EFFECTIVITY: AAL ALL 10-11-02-201

04/22/2012

BOEING PROPRIETARY - Copyright © Unpublished Work Page 29 of 35   

For Reference Only 
Effective on: AAL ALL

SUBTASK 632-029

(2) Make the Pitot-Static System serviceable ( PAGEBLOCK 34-11-00/301 ).

(a) Drain the Pitot-Static System.

(b) Flush the Pitot-Static System.

(c) Do a leak check of the Pitot-Static System.

(d) Do a test of the Pitot-Static System Heaters ( PAGEBLOCK 30-31-00/501 ).

N. Air Conditioning System

Effective on: AAL ALL

SUBTASK 632-031

(1) Make the Air Conditioning System serviceable after a Short Term (0 - 30 days) Storage.

(a) Open the Air Conditioning System items that follow:

1 The ram air inlet doors

2 The ram air exit doors

3 The E/E cooling inlet valves

4 The E/E cooling outlet valves

5 The outflow valves of the Cabin Pressure Control System.

Effective on: AAL ALL

SUBTASK 712-032

(2) Operate the air conditioning system ( PAGEBLOCK 21-00-00/201 ).

Effective on: AAL ALL

SUBTASK 712-071

(3) Make sure there are no maintenance messages on the displays in the flight deck.

Effective on: AAL ALL

SUBTASK 632-033

(4) Make the Air Conditioning System serviceable after a Long Term (more than 30 days) Storage.

NOTE: Do these steps plus the servicing steps of the Short Term Storage procedures.

(a) Install the Air Conditioning System components that were removed during the AIR

CONDITIONING SYSTEM procedures for Long Term Storage when it is necessary.

Effective on: AAL ALL

SUBTASK 712-034

(5) Do an operational test of the Air Conditioning System when it is necessary.

O. Hydraulic Systems

American Airlines

Printed: 8/31/2015; 1:28pm.

Rel. 59.0 - 08/20/15

LAA_B767

AIRCRAFT MAINTENANCE MANUAL

PGBLK EFFECTIVITY: AAL ALL 10-11-02-201

04/22/2012

BOEING PROPRIETARY - Copyright © Unpublished Work Page 30 of 35   

For Reference Only 
Effective on: AAL ALL

SUBTASK 632-035

(1) Make the hydraulic system serviceable after a Short Term (0 - 60 days) storage.

(a) If MCS-352B grease was applied during the HYDRAULIC SYSTEM procedures for Short Term

storage, it must be removed.

1 Remove the grease with solvent, Series 80 ( TASK 20-30-80-102-001 ).

(b) Remove the red flag and the cover from the opening to the pneumatic drive for the air-driven

pump exhaust.

Effective on: AAL ALL

SUBTASK 632-036

(2) Make the hydraulic system serviceable after a Long Term (more than 60 Days) storage.

NOTE: Do these steps plus the servicing steps of the Short Term storage procedures.

(a) Make sure that the hydraulic system components are serviceable ( PAGEBLOCK 29-11-00/601 ).

1 Examine all hydraulic systems for leakage.

(b) Remove the layer of grease that was applied to all bare finished surfaces during the Short Term

storage procedures.

1 Remove the grease with solvent, Series 80 ( TASK 20-30-80-102-001 ).

(c) Do this task to service the hydraulic reservoirs: Hydraulic Reservoir Servicing - Manual Procedure,

TASK 12-12-01-613-059 or Hydraulic Reservoir Servicing - Pressure Procedure, TASK 12-12-01-

613-060 .

(d) Do this task to service the parking brake accumulator: Parking Brake Accumulator Servicing,

TASK 12-15-04-613-001 .

(e) Do this task to service the surge accumulator of the brake hydraulic system: Surge Accumulator

Servicing for the Brake Hydraulic System, TASK 12-15-09-613-001 .

Effective on: AAL ALL

SUBTASK 712-037

(3) If the aircraft was in storage more than 60 days, do these tests:

(a) Main (Left, Right and Center) Hydraulic Systems ( PAGEBLOCK 29-11-00/501 )

(b) Ram Air Turbine (RAT) System ( PAGEBLOCK 29-21-00/501 )

(c) Hydraulic Fluid Quantity Indicating System ( PAGEBLOCK 29-33-00/501 )

(d) Hydraulic Pressure Indicating System ( PAGEBLOCK 29-31-00/501 )

(e) Hydraulic Fluid Temperature Indicating System ( PAGEBLOCK 29-32-00/501 )

Effective on: AAL ALL

SUBTASK 962-038

(4) If the aircraft was in storage more than 60 days, replace the hydraulic system filter elements that follow:

(a) System L and R Return Filter Elements ( PAGEBLOCK 29-11-15/401 )

(b) System C Return Filter Elements ( PAGEBLOCK 29-11-16/401 )

American Airlines

Printed: 8/31/2015; 1:28pm.

Rel. 59.0 - 08/20/15

LAA_B767

AIRCRAFT MAINTENANCE MANUAL

PGBLK EFFECTIVITY: AAL ALL 10-11-02-201

04/22/2012

BOEING PROPRIETARY - Copyright © Unpublished Work Page 31 of 35   

For Reference Only 
(c) System L and R EDP Pressure/Case Drain Filter Elements ( PAGEBLOCK 29-11-17/401 )

(d) ACMP Pressure/Case Drain Filter Elements ( PAGEBLOCK 29-11-18/401 )

(e) System C ADP Pressure/Case Drain Filter Elements ( PAGEBLOCK 29-11-19/401 )

P. Flight Controls

Effective on: AAL ALL

SUBTASK 632-040

(1) Make the flight control system serviceable after a long term (more than 30 days) storage.

(a) Make sure that the cable tension loads are correct in all primary and secondary control systems (

PAGEBLOCK 27-00-01/201 ).

NOTE: The cable tension charts can be found in the applicable AMM section for the cable

system.

(b) Examine all of the cables you can see visually and lubricate them ( PAGEBLOCK 12-21-31/301 ).

Effective on: AAL ALL

SUBTASK 712-041

(2) Do an operational test of the primary and secondary control systems:

(a) Control System Electronics Unit (CSEU) ( PAGEBLOCK 27-09-00/201 )

(b) Aileron and Aileron Trim Control System ( PAGEBLOCK 27-11-00/501 )

(c) Aileron and Spoiler Hydraulic Supply Shutoff ( PAGEBLOCK 27-13-00/601 )

(d) Aileron Position Indicating System ( PAGEBLOCK 27-18-00/501 )

(e) Rudder and Rudder Trim Control System ( PAGEBLOCK 27-21-00/501 Config 1 or

PAGEBLOCK 27-21-00/501 Config 2 )

(f) Rudder and Elevator Hydraulic Supply Shutoff ( PAGEBLOCK 27-23-00/501 ).

(g) Rudder Position Indicating System ( PAGEBLOCK 27-28-00/501 )

(h) Elevator Control System ( PAGEBLOCK 27-31-00/501

(i) Stall Warning System ( PAGEBLOCK 27-32-00/501 Config 1 or PAGEBLOCK 27-32-00/501

 Config 3 )

(j) Elevator Position Indicating System ( PAGEBLOCK 27-38-00/501 )

(k) Horizontal Stabilizer Trim Control System ( PAGEBLOCK 27-41-00/501 )

(l) Stabilizer Trim Indicating System ( PAGEBLOCK 27-48-00/501 )

(m) Trailing Edge Flap Slat Electronics Unit ( PAGEBLOCK 27-51-00/501 )

(n) Trailing Edge Flap and Slat Primary Drives and Position Indicating Systems ( PAGEBLOCK 27-51-

00/501 )

(o) Flap Alternate Power and Drive System ( PAGEBLOCK 27-51-00/501 )

(p) Trailing Edge Flap Position Indicating System ( PAGEBLOCK 27-58-00/501 )

American Airlines

Printed: 8/31/2015; 1:28pm.

Rel. 59.0 - 08/20/15

LAA_B767

AIRCRAFT MAINTENANCE MANUAL

PGBLK EFFECTIVITY: AAL ALL 10-11-02-201

04/22/2012

BOEING PROPRIETARY - Copyright © Unpublished Work Page 32 of 35   

For Reference Only 
(q) Spoiler/Speedbrake Control System ( PAGEBLOCK 27-61-00/501 )

(r) Auto Speedbrake Control System ( PAGEBLOCK 27-62-00/501 )

(s) Slat Alternate Power and Drive System ( PAGEBLOCK 27-81-00/501 )

(t) Leading Edge Slat Position Indicating System ( PAGEBLOCK 27-88-00/501 )

Q. Equipment/Furnishings

Effective on: AAL ALL

SUBTASK 612-042

(1) Do the servicing of the toilet tanks and flush systems ( PAGEBLOCK 12-17-01/301 ).

NOTE: The potable water system supplies water to flush the toilets. Pressurize the potable water system to

40 psi.

Effective on: AAL ALL

SUBTASK 712-043

(2) Do an operational test of the toilet system ( PAGEBLOCK 38-32-00/501 ).

Effective on: AAL ALL

SUBTASK 632-044

(3) Remove the covers from the main entry and service door windows.

Effective on: AAL ALL

SUBTASK 792-045

(4) Make a check of the galley and lavatory plumbing and drains for airlocks and leakage.

Effective on: AAL ALL

SUBTASK 632-046

(5) Remove the dust covers (when installed) from the seats.

Effective on: AAL ALL

SUBTASK 212-047

(6) Examine the upholstery, carpet, and tapestries for moisture and mildew.

(a) If you find moisture or mildew, remove it.

Effective on: AAL ALL

SUBTASK 422-049

(7) Install the attendant's flashlights.

Effective on: AAL ALL

SUBTASK 412-050

(8) Install the seats and floor panels that were removed in the EQUIPMENT/FURNISHING procedures for Long Term

storage.

R. Oxygen System

American Airlines

Printed: 8/31/2015; 1:28pm.

Rel. 59.0 - 08/20/15

LAA_B767

AIRCRAFT MAINTENANCE MANUAL

PGBLK EFFECTIVITY: AAL ALL 10-11-02-201

04/22/2012

BOEING PROPRIETARY - Copyright © Unpublished Work Page 33 of 35   

For Reference Only 
Effective on: AAL ALL

SUBTASK 612-056

WARNING: OBEY THE PRECAUTIONS WHEN YOU REMOVE AND INSTALL THE OXYGEN CYLINDERS. IF YOU DO NOT

OBEY THE PRECAUTIONS, INJURIES TO PERSONNEL AND DAMAGE TO EQUIPMENT CAN OCCUR.

(1) Obey the precautions for the oxygen cylinders ( PAGEBLOCK 12-15-08/301 ).

Effective on: AAL ALL

SUBTASK 612-076

(2) Make sure that the oxygen system is serviceable ( PAGEBLOCK 35-00-00/201 ):

(a) Make a visual check of the oxygen system and look for signs of corrosion. If you find corrosion,

correct it when it is necessary.

(b) Flush the crew oxygen system plumbing with dry nitrogen or clean air.

(c) Prepare to install the portable oxygen bottle and crew oxygen bottle as follows:

1 Remove the red flags from the polyethylene bags.

2 Remove the polyethylene bags from the lines and hoses that have the caps.

3 Remove the cap from the connector end of the hoses that are in the stowage boxes

for the oxygen masks.

4 Remove the cap from the cylinder end of the oxygen distribution lines.

(d) Install the oxygen bottles (this includes the regulator).

(e) Open the high pressure valves on the oxygen supply cylinders.

(f) Install the oxygen masks for the crew system.

NOTE: If the crew oxygen masks were in storage for more than 90 days, they must be

examined. Look for deterioration of the rubber and plastic parts.

1 Make sure the oxygen mask operate correctly.

(g) Make sure the passenger oxygen system operates correctly.

(h) Make sure the drop system for the passengers oxygen masks operates correctly.

S. Potable Water System

Effective on: AAL ALL

SUBTASK 612-052

(1) Make sure the potable water system is serviceable. Do the steps that follow ( PAGEBLOCK 38-10-

00/201 ):

(a) Remove the plugs and seals from all of the drains.

(b) Disinfect the water system and install new filters ( PAGEBLOCK 38-10-00/201 ).

(c) Install new filters in the potable water system ( PAGEBLOCK 38-15-02/401 ).

(d) Do the servicing of the water tanks ( PAGEBLOCK 12-14-01/301 ).

(e) Install the coffee makers.

American Airlines

Printed: 8/31/2015; 1:28pm.

Rel. 59.0 - 08/20/15

LAA_B767

AIRCRAFT MAINTENANCE MANUAL

PGBLK EFFECTIVITY: AAL ALL 10-11-02-201

04/22/2012

BOEING PROPRIETARY - Copyright © Unpublished Work Page 34 of 35   

For Reference Only 
(f) Install the water boilers.

T. Power Plant

Effective on: AAL ALL

SUBTASK 612-054

(1) Make sure that the power plants are serviceable ( GE: PAGEBLOCK 71-00-00/201 or GA: PAGEBLOCK 71-00-

00/201 ).

U. APU

Effective on: AAL ALL

SUBTASK 612-055

(1) Make sure that the APU is serviceable ( PAGEBLOCK 49-11-00/201 ).

V. Compass

Effective on: AAL ALL

SUBTASK 822-073

(1) If the airplane was parked for more than one year on the same heading, do the compass swing procedure (

PAGEBLOCK 34-23-00/201 ).

American Airlines

Printed: 8/31/2015; 1:28pm.

Rel. 59.0 - 08/20/15

LAA_B767

AIRCRAFT MAINTENANCE MANUAL

PGBLK EFFECTIVITY: AAL ALL 10-11-02-201

04/22/2012

BOEING PROPRIETARY - Copyright © Unpublished Work Page 35 of 35   

For Reference Only