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-Put the airplane back to its usual condition
-Installation test.
General Paragraph
The general paragraph is an introduction that gives the purpose and limitations of the task. There may be a general paragraph for the page block, or for each task.
Equipment Paragraph (Not Shown)
The equipment paragraph is a summary of all tools and test equipment to support the task. Each piece of equipment also has its part number.
Consumable Materials Paragraph (Not Shown)
The consumable materials paragraph is a summary of all consumable materials necessary to complete the task. The Boeing Spares Department gives each airline a list of all consumable materials that you need to do all the tasks in the maintenance manual.
References Paragraph
The references paragraph is a list that supplies all references. References may be made to other AMM procedures or other manuals.
Access Paragraph
The access paragraph is a summary of all location zones and access panel information to do the task. See chapter six of the maintenance manual for more information on the zone and access panel numbering systems.
Prepare for Paragraph
The prepare for removal paragraph is for tasks in the R/I, A/T, and I/C page block(s). The paragraph gives all the things you must do before you start the task. This includes any doors, panels, or circuit breakers that you must open.

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01-00-00

 

737-600/700/800/900 TRAINING MANUAL MAINTENANCE DOCUMENTS -- AMM PART 2 - MAINTENANCE TASK STRUCTURE Procedure Paragraph (Not Shown)
The procedure paragraph has the steps to complete the task.
Put the Airplane Back to Usual Condition Paragraph (Not Shown)
The paragraph gives all the things you must do to put the airplane back to its usual condition. This includes any doors, panels, or circuit breakers that you must close.
Installation Test Paragraph (Not Shown)
The paragraph lists all the steps you must do to do a test of the component you just installed.
Training Information Point
Each page has a section that gives the effectivity of the page. It may say ALL or it may give specific airplane identification numbers.
01-00-00

737-600/700/800/900 TRAINING MANUAL

 

737-600/700/800/900 MAINTENANCE MANUAL
GENERAL PARAGRAPH

START POWER UNIT-REMOVAL/INSTALLATION
1.  General
A. This procedure has these tasks:

(1)
A removal of the start power unit.

(2)
An installation of the start power unit.

B.  
The start power unit is installed on the E2-2 electrical shelf. The E2-2

electrical shelf is found in the electrical and electronics compartment (section 43)
C.  The start power unit is referred to as the SPU.
TASK 49-41-71-000-801
REFERENCES PARAGRAPH
2.  Start Power Unit Removal (Fig. 401) A.References

(1)
AMM TASK 20-10-07-000-801 p201, E/E Box Removal

(2)
AMM TASK 20-40-12-000-802 p 201, ESDS Handling for Metal Encased Unit

ACCESS
Removal
PARAGRAPH

B.Access

(1)
Location Zones

(a)
118 Electrical and Electronics Compartment - Right

(b)
 121 Forward Cargo Compartment - Left

(c)
 122 Forward Cargo Compartment - Right

(d)
 211 Flight Compartment - Left

 

(2)
Access Panels

(a)
 117A Electronic Equipment Access Door

(b)
821 Forward Cargo Door

 

C.  
Prepare For The Removal

 

PREPARE FOR

SUBTASK 860-001
PARAGRAPH

(1) Make sure that the APU master switch on the P5 forward overhead panel is
PARAGRAPHS NOT SHOWN
-EQUIPMENT
-CONSUMABLE MATERIALS
-PROCEDURE
-PUT THE AIRPLANE BACK TO USUAL CONDITION
-INSTALLATION TEST

OFF and install a DO-NOT-OPERATE tag.
SUBTASK 860-002

(2) Open these circuit breakers and attach D0-NOT-CLOSE tags:
(a) Circuit breaker panel, P6-4:
1) 6A14 AUX POWER UNIT CONT
2) 6B14 AUX POWER UNIT SCU FAN POWER

SUBTASK 010-001

(3)
Open the electrical equipment access door, 117A

SUBTASK 860-005

(4)
Open these circuit breakers and attach DO-NOT-CLOSE tags:

(a)
 Battery Shield, J9:
1) 9Z99 BATTERY CHARGER

(b)
 Power Distribution Panel Number 1, P91:
1) 91G1 APU START CONV

 

 

EFFECTIVITY
49-41-71
ALL
Page 401 Jun 05/98

01-00-00-004 Rev 1 12/03/1998
MAINTENANCE DOCUMENTS - AMM PART 2 - MAINTENANCE TASK STRUCTURE
01-00-00

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