Maintenance Practices 201 [*]
[*] AIRPLANES WITHOUT EFIS
Adjustment/Test 501 [*] Operational Test 504 System Test 513
[*] AIRPLANES WITHOUT EFIS
34-CONTENTS
BEJ Page 24 Mar 15/96
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
737-300/400/500MAINTENANCE MANUAL
CHAPTER 34 - NAVIGATION
TABLE OF CONTENTS_________________
Chapter
Section
Subject Subject Page_______ _______ ____ Effectivity___________
FLIGHT MANAGEMENT COMPUTER SYSTEM 34-62-01
Description and Operation 1 CONFIG 1 [*]
General 1
Computation - Guidance 46
Computation - Navigation 39
Computation - Performance 36
Computer - Flight Management 22
Failure Detection and Alerts 54
Interface - EFIS 30
Messages - FMCS 56
Navigation Aid and Tuning 45
Management
Operation FMCS 63
Overview - FMCS 9
System Interface 10
Unit - Control Display 16
Unit - Fuel Summation 34
[*] AIRPLANES WITH EFIS AND A SINGLE FMC
Description and Operation 1 CONFIG 2 [*]
General 1
Computation - Guidance 49
Computation - Navigation 42
Computation - Performance 38
Computer - Flight Management 27
Failure Detection and Alerts 56
Interface - EFIS 32
Messages - FMCS 58
Navigation Aid and Tuning 47
Management
Operation FMCS 67
Overview - FMCS 9
System Interface 10
Unit - Control Display 20
Unit - Fuel Summation 38
[*] AIRPLANES WITH DUAL FMC
Trouble Shooting 101 [*]
[*] AIRPLANES WITH EFIS
Maintenance Practices 201 [*]
[*] AIRPLANES WITH EFIS
34-CONTENTS
BEJ Page 25 Mar 15/96
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
737-300/400/500MAINTENANCE MANUAL
CHAPTER 34 - NAVIGATION
TABLE OF CONTENTS
_________________
Chapter Section Subject_______ Subject ____ Effectivity
_______ Page ___________
Adjustment/Test 501 [*] Operational Test 504 System Test 515
[*] AIRPLANES WITH EFIS
RELAY - FMCS TRANSFER 34-62-51 Removal/Installation 401 [*] [*] AIRPLANES WITH DUAL FMC
UNIT - FMCS COMPUTER 34-62-21 Removal/Installation 401 ALL
UNIT - FMCS CONTROL DISPLAY 34-62-11 Maintenance Practices 201 ALL Servicing 301 ALL Removal/Installation 401 ALL
34-CONTENTS
BEJ Page 26 Mar 15/96
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
1.
2.
3.
A
737-300/400/500MAINTENANCE MANUAL
PITOT-STATIC SYSTEM - DESCRIPTION AND OPERATION
_______________________________________________
General
_______
A. The pitot-static system provides dynamic (pitot) and ambient (static) air pressures to connected airplane equipment and instruments. These pressures are used to determine airplane altitude, airspeed, mach number and vertical speed.
B. The pitot-static system consists of four combined pitot-static probes, two alternate flush static ports, two static source selector valves and connecting tubing. The pitot-static lines are self draining. Where this is impractical, drain traps are provided.
C. Heater circuits are provided for anti-icing of the pitot static probes. Refer to Chapter 30, Pitot Static Tubes, Alpha Vane and Temperature Probe Anti-Icing System.
Pitot System (Fig. 2)
____________
A. The airplane pitot system consists of four separate pitot systems: captain's, first officer's, auxiliary No. 1 and auxiliary No. 2. Four combined pitot-static probes are used to sense pitot pressure. Two probes are mounted on each side of the airplane below control cabin window No. 3.
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