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SYSTEM SCHEMATIC MANUAL

Air 2000, Ltd.
DOCUMENT NO. D280N016S

PUBLISHED BY BOEING COMMERCIAL AIRPLANES SEATTLE, WASHINGTON, USA A DIVISION OF THE BOEING COMPANY

JUL 29/1996

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SYSTEM SCHEMATIC MANUAL
REVISION TRANSMITTAL

TO: HOLDER OF Air 2000, Ltd. MODEL 757-225,-28A SYSTEM SCHEMATIC MANUAL, BOEING DOCUMENT NUMBER D280N016S REVISION: DATE: 11 JUL 29/2004

FILINGINSTRUCTIONS This revision of your manual is a complete issue of all pages in every Section. Please replace the existing contents of the manual, Section by Section.

MANUAL NO: D280N016S

REVISION TRANSMITTAL PAGE 1 JUL 29/2004

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SYSTEM SCHEMATIC MANUAL
BOEING REVISION RECORD

REV 0

EFFECTIVITY RANGE NA441-NA443 NA447-NA447 NA022-NA024

REVISION TYPE Basic

DATE JUL 29/1996

1 2 3 45 6 7 8 9 10 11

Follow-on

OCT 23/1997 MAR 27/1998 JUN 30/1998 MAR 20/2000 NOV 01/2000

NJ001-NJ003

Follow-on

JAN 03/2003 APR 03/2003 JUL 02/2003

NJ004-NJ004

Follow-on

FEB 02/2004 APR 30/2004 JUL 29/2004

MANUAL NO: D280N016S

BOEING REVISION RECORD PAGE 1 JUL 29/2004

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SYSTEM SCHEMATIC MANUAL
CUSTOMER REVISION RECORD REVISION DATE FILED BY REVISION DATE FILED BYMANUAL NO: D280N016S

CUSTOMER REVISION RECORD PAGE 1 FEB 02/2004

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SYSTEM SCHEMATIC MANUAL
CUSTOMER REVISION RECORD REVISION DATE FILED BY

CUSTOMER REVISION RECORD PAGE 2 MAR 20/2000

MANUAL NO: D280N016S

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SYSTEM SCHEMATIC MANUAL
TEMPORARY REVISION RECORD

TR

REVISION DATE

INCORP IN REVISION

TR

REVISION DATE

INCORP IN REVISION

MANUAL NO: D280N016STEMPORARY REVISION RECORD PAGE 1 JUL 29/1996

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SYSTEM SCHEMATIC MANUAL
MODIFICATION INCORPORATION INDEX

This list is provided so that the operator can determine which Service Bulletins and Customer Modifications have been incorporated in the manual to reflect the changes made to the airplane's configuration since delivery. The list consists of: 1. 2. 3. 4. 5. 6. The The The The The Theservice bulletin number with its revision level. customer change number, if supplied by the customer. aircraft affected by the referenced change. status of the change. title of the service bulletin or customer change. date of the manual revision which incorporated the change.

An 'S' is used in the status column to indicate Start (Dual) configuration and a 'C' to indicate Complete (Final)configuration.

SERVICE BULLETIN NUMBER 21-0035

CUSTOMER CHANGE NUMBER

CHANGE EFFECTIVITY 521-522

STATUS S OR C S

21-0041 R01

521-522

C

TITLE AIR CONDITIONING COOLING - EQUIPMENT COOLING SYSTEM CONTROL CARD MODIFICATION AIR CONDITIONING TEMPERATURE CONTROL - ZONE TEMPERATURE CONTROL SYSTEM WIRING REVISION

REVISION DATE OCT 23/1997

OCT 23/1997

MANUAL NO: D280N016SMODIFICATION INCORPORATION INDEX PAGE 1 OCT 23/1997

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SYSTEM SCHEMATIC MANUAL
MODIFICATION INCORPORATION INDEX SERVICE BULLETIN NUMBER 21-0047 CUSTOMER CHANGE NUMBER

CHANGE EFFECTIVITY 523-523

STATUS S OR C S

21-0050 R01

001-002

S

TITLE AIR CONDITIONING COOLING - AFT EQUIPMENT COOLING SUPPLY FAN CIRCUIT BREAKER AND WIRE REVISION AIR CONDITIONING EQUIPMENT COOLING SMOKE DETECTIONSMOKE DETECTOR RELOCATION AIR CONDITIONING COOLING - EQUIPMENT COOLING SYSTEM EXHAUST LOW FLOW DETECTOR - REMOVAL AIR CONDITIONING EQUIPMENT COOLING SYSTEM - EXHAUST LOW FLOW DETECTOR REMOVAL

REVISION DATE OCT 23/1997

MAR 20/2000

21-0061 R01

521-522 001-003

C

MAR 20/2000

21-0064

007-007 521-522

C

MAR 20/2000

MODIFICATION INCORPORATION INDEX PAGE 2 MAR 20/2000MANUAL NO: D280N016S

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SYSTEM SCHEMATIC MANUAL
MODIFICATION INCORPORATION INDEX SERVICE CUSTOMER BULLETIN CHANGE NUMBER NUMBER 22-0019 R01

CHANGE EFFECTIVITY 521-522

STATUS S OR C C

TITLE AUTOFLIGHT AUTOPILOT/FLIGHT CONTROL - FLIGHT CONTROL COMPUTER REPLACEMENT ELECTRICAL POWER AC GENERATION HYDRAULIC MOTOR DRIVEN GENERATOR SYSTEM INSTALLATION ELECTRICAL POWER INTEGRATED DRIVE...