日期： 2011-04-24 11:21:01
CHAPTER 27 Flight Controls 27-CONTENTS Page 17 D633W101-BEJ Jan 05/2002 FLIGHT CONTROLS -INTRODUCTION General The flight controls keep the airplane at the desired attitude during flight. They consist of movable surfaces on the wing and the...
日期： 2011-04-24 11:20:03
CHAPTER 26 Fire Protection CHAPTER 26 Fire Protection 26-CONTENTS Page 7 D633W101-BEJ Jan 05/2002 FIRE PROTECTION -INTRODUCTION Purpose The fire protection systems monitor the airplane for these conditions: * Fire * Smoke * Engine overheat...
日期： 2011-04-24 11:18:21
CHAPTER 25 Equipment and Furnishings CHAPTER 25 Equipment and Furnishings 25-CONTENTS Page 7 D633W101-BEJ Jan 05/2002 777 AIRCRAFT MAINTENANCE MANUAL CHAPTER 25 Equipment and Furnishings CH-SC-SU 25-66-00 25-66-00 25-66-00 Subject DOOR-MOU...
日期： 2011-04-24 11:16:35
CHAPTER 24 Electrical Power CHAPTER 24 Electrical Power 24-CONTENTS Page 6 D633W101-BEJ Jan 05/2002 ELECTRICAL POWER -INTRODUCTION General * EEC -electronic engine control * EEU -ELMS electronic unit The electrical power system makes, supp...
日期： 2011-04-24 11:15:03
The front panel has these items: * Touch-sensitive flat panel screen to select all functions BEJ 001-005 * LED to show too cold condition BEJ 006-999 * LED to show failure of panel lamp BEJ ALL * Connector J1 for 115v ac power input and co...
日期： 2011-04-24 11:10:16
CHAPTER 23 Communications CHAPTER 23 Communications 777 AIRCRAFT MAINTENANCE MANUAL THIS PAGE IS INTENTIONALLY LEFT BLANK 23-11-00 Page 1 D633W101-BEJ Jan 05/2002 HIGH FREQUENCY COMMUNICATION SYSTEM -INTRODUCTION General The high frequency...
日期： 2011-04-23 10:20:59
CHAPTER 22 Autoflight CHAPTER 22 Autoflight Subject/Page Date COC Subject/Page Date COC EFFECTIVE PAGES 22-11-00 (cont.) 1 thru 6 May 05/2004 14 Jan 05/2002 15 Jan 05/2002 22-CONTENTS 16 Sep 05/2002 1 Jan 05/2002 17 Jan 05/2002 2 Jan 05/20...
日期： 2011-04-23 10:18:55
CHAPTER 21 Air Conditioning CHAPTER 21 Air Conditioning Subject/Page Date COC Subject/Page Date COC EFFECTIVE PAGES 1 thru 10 21-CONTENTS 1 2 3 4 5 6 7 8 9 10 11 12 21-00-00 1 2 3 4 5 6 7 May 05/2004 Jan 05/2002 Jan 05/2002 Jan 05/2002 Jan...
日期： 2011-04-21 08:08:24
1) The mach/speed trim mode is selected as a default mode when neither the automatic nor manual-electric trim is engaged. B. Fault Indication (Fig. 8) (1) Stabilizer trim control system faults are monitored by the SAM. When a fault is dete...
日期： 2011-04-21 08:06:11
757 MAINTENANCE MANUAL Airplane hydraulic systems left, right, and center move the elevators in response to manual or electrical control inputs. Manual inputs are applied to either control column and electrical inputs come via the autopilo...
日期： 2011-04-21 08:04:49
F. Rudder Trim - Test S 865-604 WARNING: KEEP PERSONS AND EQUIPMENT AWAY FROM ALL CONTROL SURFACES WHEN _______ HYDRAULIC POWER IS SUPPLIED. AILERONS, ELEVATORS, RUDDER, FLAPS, SLATS, SPOILERS, AND STABILIZER ARE FULLY POWERED SURFACES. IN...
日期： 2011-04-21 08:02:45
A 757 MAINTENANCE MANUAL CHAPTER 27 - FLIGHT CONTROLS TABLE OF CONTENTS_________________ Chapter Section Subject Subject_______ _______ Page____ Effectivity___________ FLIGHT CONTROLS 27-00-00_______________ Description and Operation 1 ALL...
日期： 2011-04-21 08:01:37
S 755-013 (19) Wait for a minimum of 5 seconds. S 285-014 (20) Verify the DUCT LEAK BITE message shall appear on the EICAS maintenance page. S 865-030 (21) Open the following circuit breakers on the overhead panel P11 and attach DO-NOT CLO...
日期： 2011-04-21 08:00:15
A 757 MAINTENANCE MANUAL CHAPTER 26 - FIRE PROTECTION Subject _______ FIRE PROTECTION - GENERAL _________________________ DETECTION _________ Description and Operation General APU Fire Detection Duct Leak Detection Engine Fire Detection TA...
日期： 2011-04-21 07:59:24
S 024-061 TASK 25-31-01-414-015 3. Install the Forward Galley G1A (Fig. 401)______________________________ A. Consumable Materials (1) A00027 Adhesive - BAC 5010 Type 60, RTV 174 EFFECTIVITY. 25-31-01 ALL 16 Page 403 Jun 20/97 BOEING PROPR...
日期： 2011-04-21 07:57:42
A 757 MAINTENANCE MANUAL CHAPTER 25 - EQUIPMENT/FURNISHINGS TABLE OF CONTENTS _________________ Chapter Section Subject_______ Subject EQUIPMENT/FURNISHINGS 25-00-00 _____________________ Description and Operation General Cleaning/Painting...
日期： 2011-04-20 08:05:13
757 MAINTENANCE MANUAL HYDRAULIC MOTOR GENERATOR SYSTEM- _________________________________ ADJUSTMENT/TEST _______________ 1. General_______ A. This procedure has two tasks. (1) The first task does an operational test of the hydraulic moto...
日期： 2011-04-20 08:03:40
A 757 MAINTENANCE MANUAL CHAPTER 24 - ELECTRICAL POWER TABLE OF CONTENTS_________________ Chapter Section Subject Subject_______ _______ Page____ Effectivity___________ ELECTRICAL POWER - GENERAL 24-00-00__________________________ Descript...
日期： 2011-04-20 07:59:34
S 034-068 WARNING: HOLD THE SERVO WHEN THE BOLTS AND THE WASHERS THAT ATTACH THE _______ SERVO TO THE AIRPLANE ARE REMOVED. THE SERVO ASSEMBLY WEIGHS 17 POUNDS. IF THE SERVO ASSEMBLY FALLS ON A PERSON INJURY CAN OCCUR. (8) Remove the bolts...
日期： 2011-04-20 07:56:34
D633N117 BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details. A 757 MAINTENANCE MANUAL CHAPTER 22 - AUTOFLIGHT TABLE OF CONTENTS _________________ Chapter Section Subject_______ Subject_______ Page AUTOFLIGHT...
