CESSNA®
MODEL 560XL
MAINTENANCE MANUAL
CHAPTER
4
AIRWORTHINESS
LIMITATIONS
THE AIRWORTHINESS LIMITATIONS SECTION IS FAA APPROVED AND GIVES INSPECTIONS AND
MAINTENANCE THAT ARE REQUIRED BY PARTS 43.16 AND 91.403 OF TITLE 14 OF THE CODE OF FEDERAL
REGULATIONS, UNLESS AN ALTERNATIVE PROGRAM HAS BEEN FAA APPROVED.
REVISION 15
22 APRIL 1998
27 SEPTEMBER 2018
CESSNA®
MODEL 560XL
MAINTENANCE MANUAL
4 - LIST OF EFFECTIVE PAGES
CHAPTER-SECTION-SUBJECT
4-Title
4-List of Effective Pages
4-Record of Temporary Revisions
4-Contents
4-00-00
4-10-00
4-10-01
4-10-02
4-11-00
4-11-02
4-12-00
4-12-MB
4-12-MD
4-12-ME
4-12-MF
4-12-MG
4-12-MH
4-12-MI
4-12-MJ
4-12-MK
4-12-ML
4-12-MM
4-12-MN
4-12-MO
4-12-MP
4-12-MR
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© TEXTRON AVIATION INC.
Page 1 of 1
Sep 27/2018
CESSNA®
MODEL 560XL
MAINTENANCE MANUAL
4 - CONTENTS
AIRWORTHINESS LIMITATIONS . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
Scope. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
Airworthiness Limitations Documents . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
Definitions . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
4-00-00 Page 1
4-00-00 Page 1
4-00-00 Page 1
4-00-00 Page 1
AIRWORTHINESS LIMITATIONS INSPECTION TIME LIMITS . . . . . . . . . . . . . . . . . . . . . . .
Purpose and Use . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
4-10-01 Page 1
4-10-01 Page 1
AIRWORTHINESS LIMITATIONS INSPECTION TIME LIMITS . . . . . . . . . . . . . . . . . . . . . . .
Russian Certified Airplanes . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
Purpose and Use . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
4-10-02 Page 1
4-10-02 Page 1
4-10-02 Page 1
REPLACEMENT TIME LIMITS . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
General . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
4-11-00 Page 1
4-11-00 Page 1
RUSSIAN-CERTIFIED AIRPLANES REPLACEMENT TIME LIMITS . . . . . . . . . . . . . . . . . .
General . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
4-11-02 Page 1
4-11-02 Page 1
AIRWORTHINESS LIMITATIONS INSPECTION DOCUMENTS . . . . . . . . . . . . . . . . . . . . . .
Purpose and Use . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
4-12-00 Page 1
4-12-00 Page 1
AIRWORTHINESS LIMITATIONS INSPECTION DOCUMENT MB . . . . . . . . . . . . . . . . . . . .
Description . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
General Inspection Criteria. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
Task Findings. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
INSPECTION DOCUMENT MB Tasks . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
4-12-MB Page 1
4-12-MB Page 1
4-12-MB Page 1
4-12-MB Page 1
4-12-MB Page 1
AIRWORTHINESS LIMITATIONS INSPECTION DOCUMENT MD. . . . . . . . . . . . . . . . . . . .
Description . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
General Inspection Criteria. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
Task Findings. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
INSPECTION DOCUMENT MD Tasks . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
4-12-MD Page 1
4-12-MD Page 1
4-12-MD Page 1
4-12-MD Page 1
4-12-MD Page 1
AIRWORTHINESS LIMITATIONS INSPECTION DOCUMENT ME . . . . . . . . . . . . . . . . . . . .
Description . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
General Inspection Criteria. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
Task Findings. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
INSPECTION DOCUMENT ME Tasks . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
4-12-ME Page 1
4-12-ME Page 1
4-12-ME Page 1
4-12-ME Page 1
4-12-ME Page 1
AIRWORTHINESS LIMITATIONS INSPECTION DOCUMENT MF . . . . . . . . . . . . . . . . . . . .
Description . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
General Inspection Criteria. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
Task Findings. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
INSPECTION DOCUMENT MF Tasks . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
4-12-MF Page 1
4-12-MF Page 1
4-12-MF Page 1
4-12-MF Page 1
4-12-MF Page 1
AIRWORTHINESS LIMITATIONS INSPECTION DOCUMENT MG. . . . . . . . . . . . . . . . . . . .
Description . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
General Inspection Criteria. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
Task Findings. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
INSPECTION DOCUMENT MG Tasks . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
4-12-MG Page 1
4-12-MG Page 1
4-12-MG Page 1
4-12-MG Page 1
4-12-MG Page 1
AIRWORTHINESS LIMITATIONS INSPECTION DOCUMENT MH. . . . . . . . . . . . . . . . . . . .
Description . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
General Inspection Criteria. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
Task Findings. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
INSPECTION DOCUMENT MH Tasks . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
4-12-MH Page 1
4-12-MH Page 1
4-12-MH Page 1
4-12-MH Page 1
4-12-MH Page 1
AIRWORTHINESS LIMITATIONS INSPECTION DOCUMENT MI. . . . . . . . . . . . . . . . . . . . .
Description . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
General Inspection Criteria. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
Task Findings. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
INSPECTION DOCUMENT MI Tasks . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
4-12-MI Page 1
4-12-MI Page 1
4-12-MI Page 1
4-12-MI Page 1
4-12-MI Page 1
4 - CONTENTS
© TEXTRON AVIATION INC.
Page 1 of 2
Sep 27/2018
CESSNA®
MODEL 560XL
MAINTENANCE MANUAL
AIRWORTHINESS LIMITATIONS INSPECTION DOCUMENT MJ . . . . . . . . . . . . . . . . . . . .
Description . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
General Inspection Criteria. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
Task Findings. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
INSPECTION DOCUMENT MJ Tasks . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
4-12-MJ Page 1
4-12-MJ Page 1
4-12-MJ Page 1
4-12-MJ Page 1
4-12-MJ Page 1
AIRWORTHINESS LIMITATIONS INSPECTION DOCUMENT MK . . . . . . . . . . . . . . . . . . . .
Description . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
General Inspection Criteria. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
Task Findings. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
INSPECTION DOCUMENT MK Tasks . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
4-12-MK Page 1
4-12-MK Page 1
4-12-MK Page 1
4-12-MK Page 1
4-12-MK Page 1
AIRWORTHINESS LIMITATIONS INSPECTION DOCUMENT ML . . . . . . . . . . . . . . . . . . . .
Description . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
General Inspection Criteria. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
Task Findings. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
INSPECTION DOCUMENT ML Tasks. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
4-12-ML Page 1
4-12-ML Page 1
4-12-ML Page 1
4-12-ML Page 1
4-12-ML Page 1
AIRWORTHINESS LIMITATIONS INSPECTION DOCUMENT MM . . . . . . . . . . . . . . . . . . .
Description . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
General Inspection Criteria. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
Task Findings. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
INSPECTION DOCUMENT MM Tasks . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
4-12-MM Page 1
4-12-MM Page 1
4-12-MM Page 1
4-12-MM Page 1
4-12-MM Page 1
AIRWORTHINESS LIMITATIONS INSPECTION DOCUMENT MN. . . . . . . . . . . . . . . . . . . .
Description . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
General Inspection Criteria. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
Task Findings. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
INSPECTION DOCUMENT MN Tasks . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
4-12-MN Page 1
4-12-MN Page 1
4-12-MN Page 1
4-12-MN Page 1
4-12-MN Page 1
AIRWORTHINESS LIMITATIONS INSPECTION DOCUMENT MO. . . . . . . . . . . . . . . . . . . .
Description . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
General Inspection Criteria. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
Task Findings. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
INSPECTION DOCUMENT MO Tasks . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
4-12-MO Page 1
4-12-MO Page 1
4-12-MO Page 1
4-12-MO Page 1
4-12-MO Page 1
AIRWORTHINESS LIMITATIONS INSPECTION DOCUMENT MP . . . . . . . . . . . . . . . . . . . .
Description . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
General Inspection Criteria. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
Task Findings. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
INSPECTION DOCUMENT MP Tasks . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
4-12-MP Page 1
4-12-MP Page 1
4-12-MP Page 1
4-12-MP Page 1
4-12-MP Page 1
AIRWORTHINESS LIMITATIONS INSPECTION DOCUMENT MR. . . . . . . . . . . . . . . . . . . .
Description . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
General Inspection Criteria. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
Task Findings. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
INSPECTION DOCUMENT MR Tasks . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
4-12-MR Page 1
4-12-MR Page 1
4-12-MR Page 1
4-12-MR Page 1
4-12-MR Page 1
4 - CONTENTS
© TEXTRON AVIATION INC.
Page 2 of 2
Sep 27/2018
CESSNA®
MODEL 560XL
MAINTENANCE MANUAL
AIRWORTHINESS LIMITATIONS
1.
Scope
A.
2.
4.
NOTE:
The Airworthiness Limitations section is FAA-approved and specifies the inspections and
maintenance required by Parts 43.16 and 91.403 of Title 14 of the Code of Federal
Regulations, unless an alternative program has been approved by the Federal Aviation
Administration (FAA).
NOTE:
The inspections, intervals, and component time limits detailed in the Airworthiness
Limitations sections of this manual are mandatory and must be adhered to in order to
comply with type certification for the Model 560XL airplane.
Airworthiness Limitations Documents
A.
3.
This chapter gives the mandatory intervals for components and airplane structures that are life-limited
or that require scheduled inspection to maintain the airworthiness of the airplane. This chapter applies
to items such as fatigue components, structures and systems, which are considered a part of the
certification process.
The Airworthiness Limitations chapter of the Model 560XL Maintenance Manual contains the following
sections:
(1) Chapter 4-10-01, AIRWORTHINESS LIMITATIONS INSPECTION TIME LIMITS provides a list
of all airworthiness limitations maintenance tasks for the Model 560XL Airplane.
(a) Chapter 4-10-01, Table 3, System and Structural Component Time limit Tasks, provides a
consolidated list of component time limit tasks duplicated from 4-10-01 to assist operators
in maintenance planning.
(2) Chapter 4-10-02, AIRWORTHINESS LIMITATIONS INSPECTION TIME LIMITS (Russian
Certified Airplanes) provides a list of all airworthiness limitations maintenance tasks for Model
560XL Airplanes certified in Russia.
(a) Chapter 4-10-02, Table 3, Russian System and Structural Component Time Limit Tasks,
provides a consolidated list of component time limit tasks duplicated from 4-10-02 to assist
operators in maintenance planning.
(3) Chapter 4-12-00, AIRWORTHINESS LIMITATIONS INSPECTION DOCUMENTS provides a list
of all Model 560XL airworthiness limitation inspection documents and the associated inspection
intervals.
Definitions
A.
System Maintenance Requirements (Refer to Airworthiness Limitations Inspection Time Limits, Table
1 in this chapter.)
(1) A System Maintenance Requirement is a mandatory system or component inspection specifically
defined to detect latent, safety-related failures.
B.
Structural Limitations Items (Refer to Airworthiness Limitations Inspection Time Limits, Table 2 in this
chapter.)
(1) An Structural Limitation Item is a mandatory structural inspection of critical items defined during
the certification process using a fatigue or damage tolerance assessment.
Limitations
A.
Composite Control Surface Paint Colors
(1) The upper surface of flaps must have a color of paint having a reflectance value of 26 or greater.
For additional information, refer to the Citation Standard Practices Manual, Chapter 20, Exterior
Finish - Cleaning/Painting.
4-00-00
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Sep 27/2018
CESSNA®
MODEL 560XL
MAINTENANCE MANUAL
AIRWORTHINESS LIMITATIONS INSPECTION TIME LIMITS
1.
Purpose and Use
A.
This section includes all airworthiness limitations maintenance tasks for the Model 560XL Airplane.
NOTE:
Refer to Chapter 5-12-00, MSG-3 Inspection Documents and Other Required Tasks for a
complete list of the Model 560XL scheduled inspection requirements.
B.
The intervals specified represent the maximum time allowable between inspections.
C.
The MM task numbers are hyperlinked to task details in this manual. The Zone number(s) are also
hyperlinked to Chapter 6, Airplane Zoning - Description and Operation to assist in planning and
completing the tasks.
D.
System Maintenance Requirements
(1) System inspections and Component Time Limits are given in Table 1 and Table 3. The tasks
and intervals specified are mandatory and cannot be changed, escalated, or deleted without the
concurrence of the responsible Aircraft Certification Office (ACO).
E.
Structural Inspection Time Limits
(1) In accordance with §25.571(a) Inspection Time Limits and Component Time Limits are defined
for the Model 560XL and presented in Table 2 and Table 3.
F.
Corrosion Prevention
(1) The airworthiness limitations recondition and discard intervals assume corrosion is maintained
to Level 1 or better. Level 1 is achieved by maintaining the aircraft according to the MSG-3
maintenance procedures identified in this Model 560XL Maintenance Manual. Refer to Chapter
5-10-00, Maintenance Planning Document, Corrosion Prevention and Control Program (CPCP)
for further details.
G.
For
(1)
(2)
(3)
H.
System Maintenance Requirement Tasks
groups of common tasks, refer to:
Table 1 System Maintenance Requirement Tasks
Table 2 Structural Limitation Item Tasks
Table 3 System and Structural Component Time Limit Tasks
(a) Refer to Table 3 for Component Time Limits Tasks that have been duplicated from Table 1
and Table 2 to assist operators in maintenance planning.
NOTE:
All initial intervals are repeat intervals unless otherwise noted.
NOTE:
Inspections that do not apply to all airplanes will have the effectivity noted in the title of
the Inspection Task.
Table 1. System Maintenance Requirement Tasks
Maintenance
Manual Task #
Task Title
Interval/
Note(s)
Inspection
Document
Zone
Effectivity
Chapter 21 - Air Conditioning
4-10-01
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CESSNA®
MODEL 560XL
MAINTENANCE MANUAL
Table 1. System Maintenance Requirement Tasks (continued)
Maintenance
Manual Task #
21-52-00-2100
Task Title
Vapor Cycle Cooling System
Hour Meter Visual Check
(Airplanes -5001 thru -5374
Incorporating Vapor Cycle Cooling
with 1134104-1 and -5 Compressor
Motors)
Interval/
Note(s)
300 Flight
Hours
Inspection
Document
Zone
Effectivity
311
-5001 thru
-5374 Incorporating Vapor Cycle Cooling System with
1134104-1
and -5
Compressor Motors
N/A
311
-5001 thru
-5374 Incorporating Vapor Cycle Cooling System With
1134104-1
and -5
Compressor Motors
N/A
247
-6001 and
On
4-12-MP
NOTE:
Refer to the Enviro Systems
Inc. Operating, Servicing and
Component Maintenance Manual
21-00-06.
21-52-00-9600
Vapor Cycle Cooling System Drive
Motor Brush Discard (Airplanes
-5001 thru -5374 Incorporating
Vapor Cycle Cooling System With
1134104-1 and -5 Compressor
Motors)
NOTE:
Refer to the Enviro Systems
Inc. Operating, Servicing and
Component Maintenance Manual
21-00-06.
500
Compressor
Hours
Chapter 76 - Engine Controls
Time Limited Dispatch Fault Visual
Check (Airplanes -6001 and On)
NOTE:
The repair of any detected faults
found between inspections may
be deferred until the end of the
interval and the airplane can be
dispatched with faults until the end
of the interval.
76-16-00-7100
NOTE:
TLD faults, inspection intervals and
dispatch limitations are defined by
the PW545C Engine Maintenance
Manual, Airworthiness Limitations
section. The tasks and intervals
specified are mandatory and
cannot be changed, escalated or
deleted without concurrence of the
responsible Aircraft Certification
Office (ACO).
170 Flight
Hours (See
NOTES)
4-10-01
© TEXTRON AVIATION INC.
Page 2
Sep 27/2018
CESSNA®
MODEL 560XL
MAINTENANCE MANUAL
I.
Structural Limitation Item Tasks
NOTE:
All initial intervals are repeat intervals unless otherwise noted.
NOTE:
Inspections that do not apply to all airplanes will have the effectivity noted in the title of
the Inspection Task.
NOTE:
For life-limited parts found in Table 2, replacement parts may have part numbers effective
on later units or spares.
Table 2. Structural Limitation Item Tasks
Maintenance
Manual Task #
Task Title
Interval/
Note(s)
Inspection
Document
Zone
Effectivity (Part
Substitutions May
Apply)
Chapter 32 - Landing Gear
NOTE:
The attaching hardware related to these landing gear installations is to be replaced whenever the associated
components are replaced. The attaching hardware can be used again if a rental component is to be installed
for no more than 100 Landings. The attaching hardware can also be used again if the original gear is to be
installed again. If a replacement gear is installed, all of the attachment hardware must be replaced.
32-10-00-9601
6641640-5 Left Main Landing Gear
Trunnion Subassembly Discard
7600
Landings
N/A
730
-5001 thru
-5037
6641640-39 Left Main Landing Gear
Trunnion Subassembly Discard
7300
Landings
N/A
730
5038 thru
-5150
6641630-5 Left Main Landing Gear
Trunnion Subassembly Discard
6900
Landings
N/A
730
-5151 thru
-5339
6641630-27 Left Main Landing Gear
Trunnion Subassembly Discard
33,300
Landings
N/A
730
-5340 thru
-6068
6641630-39 Left Main Landing Gear
Trunnion Subassembly Discard
33,300
Landings
N/A
730
-6069 thru
-6093
6641630-41 Left Main Landing Gear
Trunnion Subassembly Discard
33,300
Landings
N/A
730
-6094 and
On
6641640-6 Right Main Landing Gear
Trunnion Subassembly Discard
7600
Landings
N/A
720
-5001 thru
-5337
6641640-40 Right Main Landing Gear
Trunnion Subassembly Discard
7300
Landings
N/A
720
-5038 thru
-5150
6641630-6 Right Main Landing Gear
Trunnion Subassembly Discard
6900
Landings
N/A
720
-5151 thru
-5339
6641630-28 Right Main Landing Gear
Trunnion Subassembly Discard
33,300
Landings
N/A
720
-5340 thru
-6068
6641630-40 Right Main Landing Gear
Trunnion Subassembly Discard
33,300
Landings
N/A
720
-6069 thru
-6093
6641630- 42 Right Main Landing Gear
Trunnion Subassembly Discard
33,300
Landings
N/A
720
-6094 and
On
4-10-01
© TEXTRON AVIATION INC.
Page 3
Sep 27/2018
CESSNA®
MODEL 560XL
MAINTENANCE MANUAL
Table 2. Structural Limitation Item Tasks (continued)
Maintenance
Manual Task #
32-10-00-9602
Interval/
Note(s)
Inspection
Document
Zone
Effectivity (Part
Substitutions May
Apply)
6641640-7 Left Main Landing Gear
Trailing Link Assembly Discard
6400
Landings
N/A
730
-5001 thru
-5002
6641640-15 Left Main Landing Gear
Trailing Link Assembly Discard
6400
Landings
N/A
730
-5009 thru
-5014
6641648-1 Left Main Landing Gear
Trailing Link Assembly Discard
6400
Landings
N/A
730
-5003 thru
-5008 and
-5015 thru
-5037
6641648-7 Left Main Landing Gear
Trailing Link Assembly Discard
6400
Landings
N/A
730
-5038 thru
-5150
6641648-9 Left Main Landing Gear
Trailing Link Assembly Discard
40,300
Landings
N/A
730
-5151 thru
-5223
6641648-15 Left Main Landing Gear
Trailing Link Assembly Discard
40,300
Landings
N/A
730
-5224 thru
-5673
6641530-1 Left Main Landing Gear
Trailing Link Assembly Discard
33,300
Landings
N/A
730
-5674 thru
-6237
6641530-3 Left Main Landing Gear
Trailing Link Assembly Discard
33,300
Landings
N/A
730
-6238 and
On
DDA06877-1 Left Main Landing Gear
Trailing Link Assembly Discard
33,300
Landings
N/A
730
-6238 thru
-6243
6641640-8 Right Main Landing Gear
Trailing Link Assembly Discard
6400
Landings
N/A
720
-5001 thru
-5002
6641640-16 Right Main Landing Gear
Trailing Link Assembly Discard
6400
Landings
N/A
720
-5009 thru
-5014
6641648-2 Right Main Landing Gear
Trailing Link Assembly Discard
6400
Landings
N/A
720
-5003 thru
-5006 and
-5015 thru
-5037
6641648-8 Right Main Landing Gear
Trailing Link Assembly Discard
6400
Landings
N/A
720
-5038 thru
-5150
6641648-10 Right Main Landing Gear
Trailing Link Assembly Discard
40,300
Landings
N/A
720
-5151 thru
-5223
6641648-14 Right Main Landing Gear
Trailing Link Assembly Discard
40,300
Landings
N/A
720
-5224 thru
-5673
6641530-2 Right Main Landing Gear
Trailing Link Assembly Discard
33,300
Landings
N/A
720
-5674 thru
-6237
6641530-4 Right Main Landing Gear
Trailing Link Assembly Discard
33,300
Landings
N/A
720
-6238 and
On
DDA06877-2 Right Main Landing Gear
Trailing Link Assembly Discard
33,300
Landings
N/A
720
-6238 thru
-6243
Task Title
4-10-01
© TEXTRON AVIATION INC.
Page 4
Sep 27/2018
CESSNA®
MODEL 560XL
MAINTENANCE MANUAL
Table 2. Structural Limitation Item Tasks (continued)
Maintenance
Manual Task #
32-10-00-9603
32-10-00-9604
32-10-00-9605
Task Title
Interval/
Note(s)
Inspection
Document
Zone
Effectivity (Part
Substitutions May
Apply)
6641618-8 Main Landing Gear Trailing
Link Spacer Discard
6200
Landings
N/A
720, 730
-5001 thru
-5002
6641618-9 Main Landing Gear Trailing
Link Spacer Discard
6200
Landings
N/A
720, 730
-5003 thru
-5037
6641618-12 Main Landing Gear
Trailing Link Spacer Discard
6200
Landings
N/A
720, 730
-5038 thru
-5150
6641533-1 Main Landing Gear Trailing
Link Spacer Discard
33,300
Landings
N/A
720, 730
-5674 thru
-6068
6641533-2 Main Landing Gear Trailing
Link Spacer Discard
33,300
Landings
N/A
720, 730
-6069 and
On
6641615-3 (Except Upper Cap) Main
Landing Gear Oleo Assembly Discard
38,000
Landings
N/A
720, 730
-5001,
-5003 thru
-5206
6641615-4 (Except Upper Cap) Main
Landing Gear Oleo Assembly Discard
38,000
Landings
N/A
720, 730
-5207 thru
-5294
Upper Cap 6641616-3 Main Landing
Gear Oleo Assembly Discard
4600
Landings
N/A
720, 730
-5001,
-5003 thru
-5294
6641615-5 (Except Upper Cap) Main
Landing Gear Oleo Assembly Discard
38,000
Landings
N/A
720, 730
-6069 and
On
6641615-6 (Except Upper Cap) Main
Landing Gear Oleo Assembly Discard
38,000
Landings
N/A
720, 730
-5320 thru
-6068
6641615-7 (Except Upper Cap) Main
Landing Gear Oleo Assembly Discard
38,000
Landings
N/A
720, 730
-6069 and
On
Upper Cap 6641616-4 Main Landing
Gear Oleo Assembly Discard
14,900
Landings
N/A
720, 730
-5295 thru
-6068
Upper Cap 6641616-5 Main Landing
Gear Oleo Assembly Discard
14,900
Landings
N/A
720, 730
-6069 and
On
9912537-1 Left Main Landing Gear
Actuator Assembly Discard
70,200
Landings
N/A
730
-5001 thru
-5037
9912537-3 Left Main Landing Gear
Actuator Assembly Discard
70,200
Landings
N/A
730
-5038 thru
-6081
9912537-5 Left Main Landing Gear
Actuator Assembly Discard
70,200
Landings
N/A
730
-6082 and
On
9912537-2 Right Main Landing Gear
Actuator Assembly Discard
70,200
Landings
N/A
720
-5001 thru
-5037
9912537-4 Right Main Landing Gear
Actuator Assembly Discard
70,200
Landings
N/A
720
-5038 thru
-6081
9912537-6 Right Main Landing Gear
Actuator Assembly Discard
70,200
Landings
N/A
720
-6082 and
On
4-10-01
© TEXTRON AVIATION INC.
Page 5
Sep 27/2018
CESSNA®
MODEL 560XL
MAINTENANCE MANUAL
Table 2. Structural Limitation Item Tasks (continued)
Maintenance
Manual Task #
32-20-00-9600
Interval/
Note(s)
Inspection
Document
Zone
Effectivity (Part
Substitutions May
Apply)
6642610-3 Nose Landing Gear
Assembly Discard
33,300
Landings
N/A
710
-5001 thru
-5017
6642614-1 Nose Landing Gear
Assembly Discard
33,300
Landings
N/A
710
-5018 thru
-5500
6642625-1 Nose Landing Gear
Assembly Discard
33,300
Landings
N/A
710
-5501 thru
-5675
6642625-5 Nose Landing Gear
Assembly Discard
33,300
Landings
N/A
710
-5676 thru
-5716
6642625-6 Nose Landing Gear
Assembly Discard
33,300
Landings
N/A
710
-5717 thru
-5763
6642625-8 Nose Landing Gear
Assembly Discard
33,300
Landings
N/A
710
-5764 thru
-6068
6642625-10 Nose Landing Gear
Assembly Discard
33,300
Landings
N/A
710
-6069 thru
-6075
6642625-12 Nose Landing Gear
Assembly Discard
33,300
Landings
N/A
710
-6076 thru
-6081
6642625-14 Nose Landing Gear
Assembly Discard
33,300
Landings
N/A
710
-6082 thru
-6187
6642625-214 Nose Landing Gear
Assembly Discard
33,300
Landings
N/A
710
-5501 thru
-6261
6642635-1 Nose Landing Gear
Assembly Discard
33,300
Landings
N/A
710
-6188 thru
-6261
6642635-2 Nose Landing Gear
Assembly Discard
33,300
Landings
N/A
710
-6188 thru
-6261
6642635-4 Nose Landing Gear
Assembly Discard
33,300
Landings
N/A
710
-6262 and
On
6642635-5 Nose Landing Gear
Assembly Discard
33,300
Landings
N/A
710
-6262 and
On
6642635-201 Nose Landing Gear
Assembly Discard
33,300
Landings
N/A
710
-6262 and
On
6642635-202 Nose Landing Gear
Assembly Discard
33,300
Landings
N/A
710
-6262 and
On
Task Title
4-10-01
© TEXTRON AVIATION INC.
Page 6
Sep 27/2018
CESSNA®
MODEL 560XL
MAINTENANCE MANUAL
Table 2. Structural Limitation Item Tasks (continued)
Maintenance
Manual Task #
32-20-00-9601
Interval/
Note(s)
Inspection
Document
Zone
Effectivity (Part
Substitutions May
Apply)
9912491-2 Nose Landing Gear
Actuator Discard
33,300
Landings
N/A
710
-5002 thru
-5017
9912491-3 Nose Landing Gear
Actuator Discard
33,300
Landings
N/A
710
-5018 thru
-5343
9912491-4 Nose Landing Gear
Actuator Discard
33,300
Landings
N/A
710
-5344 thru
-5537
9912491-5 Nose Landing Gear
Actuator Discard
33,300
Landings
N/A
710
-5001, and
-5338 thru
-6081
9912491-6 Nose Landing Gear
Actuator Discard
33,300
Landings
N/A
710
-6082 and
On
Task Title
Chapter 52 - Doors
52-10-00-2200
Cabin Door Assembly Detailed
Inspection
15,000
Flight
Hours
4-12-ME
810, 811
-5001 and
On
52-20-00-2200
Emergency Exit Door Assembly
Detailed Inspection
15,000
Flight
Hours
4-12-ME
820, 821
-5001 and
On
Chapter 53 - Fuselage
NOTE:
The attaching hardware related to these landing gear installations is to be replaced whenever the associated
components are replaced. The attaching hardware can be used again if a rental component is to be installed
for no more than 100 Landings. The attaching hardware can also be used again if the original gear is to be
installed again. If a replacement gear is installed, all of the attachment hardware must be replaced.
53-00-00-9600
53-00-00-9601
6613020-1 Left Nose Landing Gear
Trunnion Support Assembly Discard
25,500
Landings
N/A
710
-5002 thru
-5085
6613020-55 Left Nose Landing Gear
Trunnion Support Assembly Discard
25,500
Landings
N/A
710
-5086 thru
-6068
6613020-63 Left Nose Landing Gear
Trunnion Support Assembly Discard
25,500
Landings
N/A
710
-6069 and
On
6613020-2 Right Nose Landing Gear
Trunnion Support Assembly Discard
25,500
Landings
N/A
710
-5002 thru
-5085
6613020-56 Right Nose Landing Gear
Trunnion Support Assembly Discard
25,500
Landings
N/A
710
-5086 thru
-6068
6613020-64 Right Nose Landing Gear
Trunnion Support Assembly Discard
25,500
Landings
N/A
710
-6069 and
On
6211191-2 Nose Landing Gear
Actuator Fitting Assembly Discard
25,500
Landings
N/A
710
-5001 thru
-5264
6211191-3 Nose Landing Gear
Actuator Fitting Assembly Discard
25,500
Landings
N/A
710
-5265 and
On
4-10-01
© TEXTRON AVIATION INC.
Page 7
Sep 27/2018
CESSNA®
MODEL 560XL
MAINTENANCE MANUAL
Table 2. Structural Limitation Item Tasks (continued)
Maintenance
Manual Task #
Task Title
Interval/
Note(s)
Inspection
Document
Zone
Effectivity (Part
Substitutions May
Apply)
6000
Flight
Hours
or 120
Months,
Whichever
Comes
First, Then
Every
2400
Hours
or 120
Months,
Whichever
Comes
First
Thereafter
4-12-MD
141, 142,
241, 242
-5001 and
On
4-12-ME
171, 172,
261, 262
-5001 and
On
4-12-MJ
213, 214,
243, 244,
253, 254,
263, 264,
323, 324
-5001 and
On
-5001 and
On
53-10-11-2501
Forward Pressure Bulkhead (Eddy
Current) Special Detailed Inspection
53-10-11-2502
Aft Pressure Bulkhead General Visual
Inspection
15,000
Flight
Hours
53-30-01-2100
Upper Fuselage Skin from Right
Stringer 13 to Left Stringer 13 General
Visual Inspection
13,000
Flight
Hours
53-30-01-2101
Lower Fuselage Skin from Right
Stringer 13 to Left Stringer 13 General
Visual Inspection
15,000
Flight
Hours
4-12-ME
143, 144,
151, 152,
161, 162,
171, 172,
213, 214,
223, 224,
321, 322
53-30-01-2501
Upper Fuselage Skin Splice at BL
0.00 (Eddy Current) Special Detailed
Inspection
15,000
Flight
Hours
4-12-ME
241, 242,
251, 252,
261, 262
-5001 and
On
53-30-01-2502
Lower Fuselage Skin Splices at
Stringers 13R and 13L (Eddy Current)
Special Detailed Inspection
15,000
Flight
Hours
4-12-ME
151, 152,
161, 162,
171, 172
-5001 and
On
Chapter 54 - Nacelles/Pylons
4-10-01
© TEXTRON AVIATION INC.
Page 8
Sep 27/2018
CESSNA®
MODEL 560XL
MAINTENANCE MANUAL
Table 2. Structural Limitation Item Tasks (continued)
Maintenance
Manual Task #
Interval/
Note(s)
Inspection
Document
Zone
Effectivity (Part
Substitutions May
Apply)
3000
Flight
Hours,
Then
Every
1500
Flight
Hours
Thereafter
4-12-MB
311, 312,
411, 412
-5001 thru
-5060
13,000
Flight
Hours
4-12-MJ
311, 312,
411, 412
-5001 thru
-5060
Vertical Stabilizer Rear Spar Cap
at WL 146 (Eddy Current) Special
Detailed Inspection (Airplanes -5001
thru -5020)
6500
Flight
Hours,
Then
Every
3000
Flight
Hours
Thereafter
4-12-MG
321, 322,
340
-5001 thru
-5020
Vertical Stabilizer Rear Spar Nested
Angle at WL 146 (Eddy Current)
Special Detailed Inspection (Airplanes
-5001 thru -5020)
11,000
Flight
Hours,
Then
Every
6000
Flight
Hours
Thereafter
4-12-MH
321, 322,
340
-5001 thru
-5020
Vertical Stabilizer Rear Spar Strap at
WL 146.00 (Eddy Current) Special
Detailed Inspection (Airplanes -5001
thru -5020)
5000
Flight
Hours,
Then
Every
2500
Flight
Hours
Thereafter
4-12-MI
321, 322,
340
-5001 thru
-5020
Task Title
54-50-10-2100
Aft Engine Beam General Visual
Inspection (Airplanes -5001 thru
-5060)
54-50-10-2500
Forward Engine Beam Upper Angles,
Horizontal Cap Flange at BL 30.5
thru BL 42.0 (Eddy Current) Special
Detailed Inspection (Airplanes -5001
thru -5060)
Chapter 55 - Stabilizers
55-30-00-2500
55-30-00-2501
55-30-00-2502
4-10-01
© TEXTRON AVIATION INC.
Page 9
Sep 27/2018
CESSNA®
MODEL 560XL
MAINTENANCE MANUAL
Table 2. Structural Limitation Item Tasks (continued)
Maintenance
Manual Task #
55-30-00-2503
55-30-00-2504
Task Title
Interval/
Note(s)
Inspection
Document
Zone
Effectivity (Part
Substitutions May
Apply)
Vertical Stabilizer Forward Spar Strap
at WL 150 (Eddy Current) Special
Detailed Inspection (Airplanes -5001
thru -5020)
11,500
Flight
Hours,
Then
Every
9000
Flight
Hours
Thereafter
4-12-MK
321, 322,
340
-5001 thru
-5020
Vertical Stabilizer Forward Spar Strap
at WL 188.00 (Eddy Current) Special
Detailed Inspection (Airplanes -5001
thru -5020)
10,000
Flight
Hours,
Then
Every
5000
Flight
Hours
Thereafter
4-12-MR
340
-5001 thru
-5020
Lower Wing Main Spar Lower Skin
Splice at WS 22.50 (Eddy Current and
Ultrasonic) Special Detailed Inspection
7500
Flight
Hours,
Then
Every
1400
Flight
Hours
Thereafter
4-12-MF
515, 516
-5001 and
On
Lower Wing Main Spar Skin Splice
Flange at WS 11.50 (Eddy Current and
Ultrasonic) Special Detailed Inspection
11,500
Flight
Hours,
Then
Every
3300
Flight
Hours
Thereafter
4-12-ML
515, 615
-5001 and
On
Lower Wing Main Spar at WS 114.57
(Eddy Current) Special Detailed
Inspection
11,000
Flight
Hours,
Then
Every
4200
Flight
Hours
Thereafter
4-12-MM
523, 524,
623, 624
-5001 and
On
Chapter 57 - Wings
57-10-00-2500
57-10-00-2501
57-10-00-2502
4-10-01
© TEXTRON AVIATION INC.
Page 10
Sep 27/2018
CESSNA®
MODEL 560XL
MAINTENANCE MANUAL
Table 2. Structural Limitation Item Tasks (continued)
Maintenance
Manual Task #
57-10-00-2503
57-10-00-2504
Task Title
Interval/
Note(s)
Inspection
Document
Zone
Effectivity (Part
Substitutions May
Apply)
Lower Wing Main Spar at WS 131.07
(Eddy Current) Special Detailed
Inspection
9000
Flight
Hours,
Then
Every
3400
Flight
Hours
Thereafter
4-12-MN
523, 524,
623, 624
-5001 and
On
Lower Wing Main Spar at WS 149.57
(Eddy Current) Special Detailed
Inspection
12,500
Flight
Hours,
Then
Every
6100
Flight
Hours
Thereafter
4-12-MO
523, 524,
623, 624
-5001 and
On
NOTE:
The attaching hardware related to these landing gear installations is to be replaced whenever the associated
components are replaced. The attaching hardware can be used again if a rental component is to be installed
for no more than 100 Landings. The attaching hardware can also be used again if the original gear is to be
installed again. If a replacement gear is installed, all of the attachment hardware must be replaced.
57-10-00-9600
57-10-00-9601
6622123-1 Left Main Landing Gear
Forward Trunnion Fitting Discard
23,800
Landings
N/A
730
-5001 thru
-6068
6622123-5 Left Main Landing Gear
Forward Trunnion Fitting Discard
23,800
Landings
N/A
730
-6069 and
On
6622123-2 Right Main Landing Gear
Forward Trunnion Fitting Discard
23,800
Landings
N/A
720
-5001 thru
-6068
6622123-6 Right Main Landing Gear
Forward Trunnion Fitting Discard
23,800
Landings
N/A
720
-6069 and
On
6622124-1 Left Main Landing Gear Aft
Trunnion Fitting Discard
23,800
Landings
N/A
730
-5001 thru
-6068
6622124-5 Left Main Landing Gear Aft
Trunnion Fitting Discard
23,800
Landings
N/A
730
-6069 and
On
6622124-2 Right Main Landing Gear
Aft Trunnion Fitting Discard
23,800
Landings
N/A
720
-5001 thru
-6068
6622124-6 Right Main Landing Gear
Aft Trunnion Fitting Discard
23,800
Landings
N/A
720
-6069 and
On
4-10-01
© TEXTRON AVIATION INC.
Page 11
Sep 27/2018
CESSNA®
MODEL 560XL
MAINTENANCE MANUAL
Table 2. Structural Limitation Item Tasks (continued)
Maintenance
Manual Task #
57-10-00-9602
57-50-04-9600
J.
Interval/
Note(s)
Inspection
Document
Zone
Effectivity (Part
Substitutions May
Apply)
6621125-1 Left Main Landing Gear
Actuator Fitting Discard
23,800
Landings
N/A
730
-5001 thru
-5022
6621125-5 Left Main Landing Gear
Actuator Fitting Discard
23,800
Landings
N/A
730
-5023 thru
-6068
6621125-9 Left Main Landing Gear
Actuator Fitting Discard
23,800
Landings
N/A
730
-6069 and
On
6621125-2 Right Main Landing Gear
Actuator Fitting Discard
23,800
Landings
N/A
720
-5001 thru
-5022
6621125-6 Right Main Landing Gear
Actuator Fitting Discard
23,800
Landings
N/A
720
-5023 thru
-6068
6621125-10 Right Main Landing Gear
Actuator Fitting Discard
23,800
Landings
N/A
720
-6069 and
On
S3049-5F8 Inboard and Outboard
Flap Rollers Discard
5000
Landings
N/A
500, 600
-5001 and
On
Task Title
System and Structural Component Time Limit Tasks
NOTE:
All initial intervals are repeat intervals unless otherwise noted.
NOTE:
For life-limited parts found in Table 3, replacement parts may have part numbers effective
on later units or spares.
Table 3. System and Structural Component Time Limit Tasks
Maintenance
Manual Task #
Task Title
Interval/
Note(s)
Inspection
Document
Zone
Effectivity (Part
Substitutions May
Apply)
311
-5001 thru
-5374 Incorporating Vapor Cycle Cooling With
1134104-1
and -5
Compressor Motors
Chapter 21 - Air Conditioning
21-52-00-9600
Vapor Cycle Cooling System Drive
Motor Brush Discard (Airplanes -5001
thru -5374 Incorporating Vapor Cycle
Cooling System With 1134104-1 and
-5 Compressor Motors)
NOTE:
Refer to the Enviro Systems Inc.
Operating, Servicing and Component
Maintenance Manual 21-00-06.
500 Compressor
Hours
N/A
Chapter 32 - Landing Gear
4-10-01
© TEXTRON AVIATION INC.
Page 12
Sep 27/2018
CESSNA®
MODEL 560XL
MAINTENANCE MANUAL
Table 3. System and Structural Component Time Limit Tasks (continued)
Maintenance
Manual Task #
Task Title
Interval/
Note(s)
Inspection
Document
Zone
Effectivity (Part
Substitutions May
Apply)
NOTE:
The attaching hardware related to these landing gear installations is to be replaced whenever the associated
components are replaced. The attaching hardware can be used again if a rental component is to be installed
for no more than 100 Landings. The attaching hardware can also be used again if the original gear is to be
installed again. If a replacement gear is installed, all of the attachment hardware must be replaced.
32-10-00-9601
6641640-5 Left Main Landing Gear
Trunnion Subassembly Discard
7600
Landings
N/A
730
-5001 thru
-5037
6641640-39 Left Main Landing Gear
Trunnion Subassembly Discard
7300
Landings
N/A
730
5038 thru
-5150
6641630-5 Left Main Landing Gear
Trunnion Subassembly Discard
6900
Landings
N/A
730
-5151 thru
-5339
6641630-27 Left Main Landing Gear
Trunnion Subassembly Discard
33,300
Landings
N/A
730
-5340 thru
-6068
6641630-39 Left Main Landing Gear
Trunnion Subassembly Discard
33,300
Landings
N/A
730
-6069 thru
-6093
6641630-41 Left Main Landing Gear
Trunnion Subassembly Discard
33,300
Landings
N/A
730
-6094 and
On
6641640-6 Right Main Landing Gear
Trunnion Subassembly Discard
7600
Landings
N/A
720
-5001 thru
-5337
6641640-40 Right Main Landing Gear
Trunnion Subassembly Discard
7300
Landings
N/A
720
-5038 thru
-5150
6641630-6 Right Main Landing Gear
Trunnion Subassembly Discard
6900
Landings
N/A
720
-5151 thru
-5339
6641630-28 Right Main Landing Gear
Trunnion Subassembly Discard
33,300
Landings
N/A
720
-5340 thru
-6068
6641630-40 Right Main Landing Gear
Trunnion Subassembly Discard
33,300
Landings
N/A
720
-6069 thru
-6093
6641630- 42 Right Main Landing Gear
Trunnion Subassembly Discard
33,300
Landings
N/A
720
-6094 and
On
4-10-01
© TEXTRON AVIATION INC.
Page 13
Sep 27/2018
CESSNA®
MODEL 560XL
MAINTENANCE MANUAL
Table 3. System and Structural Component Time Limit Tasks (continued)
Maintenance
Manual Task #
32-10-00-9602
Interval/
Note(s)
Inspection
Document
Zone
Effectivity (Part
Substitutions May
Apply)
6641640-7 Left Main Landing Gear
Trailing Link Assembly Discard
6400
Landings
N/A
730
-5001 thru
-5002
6641640-15 Left Main Landing Gear
Trailing Link Assembly Discard
6400
Landings
N/A
730
-5009 thru
-5014
6641648-1 Left Main Landing Gear
Trailing Link Assembly Discard
6400
Landings
N/A
730
-5003 thru
-5008 and
-5015 thru
-5037
6641648-7 Left Main Landing Gear
Trailing Link Assembly Discard
6400
Landings
N/A
730
-5038 thru
-5150
6641648-9 Left Main Landing Gear
Trailing Link Assembly Discard
40,300
Landings
N/A
730
-5151 thru
-5223
6641648-15 Left Main Landing Gear
Trailing Link Assembly Discard
40,300
Landings
N/A
730
-5224 thru
-5673
6641530-1 Left Main Landing Gear
Trailing Link Assembly Discard
33,300
Landings
N/A
730
-5674 thru
-6237
6641530-3 Left Main Landing Gear
Trailing Link Assembly Discard
33,300
Landings
N/A
730
-6238 and
On
DDA06877-1 Left Main Landing Gear
Trailing Link Assembly Discard
33,300
Landings
N/A
730
-6238 thru
-6243
6641640-8 Right Main Landing Gear
Trailing Link Assembly Discard
6400
Landings
N/A
720
-5001 thru
-5002
6641640-16 Right Main Landing Gear
Trailing Link Assembly Discard
6400
Landings
N/A
720
-5009 thru
-5014
6641648-2 Right Main Landing Gear
Trailing Link Assembly Discard
6400
Landings
N/A
720
-5003 thru
-5006 and
-5015 thru
-5037
6641648-8 Right Main Landing Gear
Trailing Link Assembly Discard
6400
Landings
N/A
720
-5038 thru
-5150
6641648-10 Right Main Landing Gear
Trailing Link Assembly Discard
40,300
Landings
N/A
720
-5151 thru
-5223
6641648-14 Right Main Landing Gear
Trailing Link Assembly Discard
40,300
Landings
N/A
720
-5224 thru
-5673
6641530-2 Right Main Landing Gear
Trailing Link Assembly Discard
33,300
Landings
N/A
720
-5674 thru
-6237
6641530-4 Right Main Landing Gear
Trailing Link Assembly Discard
33,300
Landings
N/A
720
-6238 and
On
DDA06877-2 Right Main Landing Gear
Trailing Link Assembly Discard
33,300
Landings
N/A
720
-6238 thru
-6243
Task Title
4-10-01
© TEXTRON AVIATION INC.
Page 14
Sep 27/2018
CESSNA®
MODEL 560XL
MAINTENANCE MANUAL
Table 3. System and Structural Component Time Limit Tasks (continued)
Maintenance
Manual Task #
32-10-00-9603
32-10-00-9604
32-10-00-9605
Task Title
Interval/
Note(s)
Inspection
Document
Zone
Effectivity (Part
Substitutions May
Apply)
6641618-8 Main Landing Gear Trailing
Link Spacer Discard
6200
Landings
N/A
720, 730
-5001 thru
-5002
6641618-9 Main Landing Gear Trailing
Link Spacer Discard
6200
Landings
N/A
720, 730
-5003 thru
-5037
6641618-12 Main Landing Gear
Trailing Link Spacer Discard
6200
Landings
N/A
720, 730
-5038 thru
-5150
6641533-1 Main Landing Gear Trailing
Link Spacer Discard
33,300
Landings
N/A
720, 730
-5674 thru
-6068
6641533-2 Main Landing Gear Trailing
Link Spacer Discard
33,300
Landings
N/A
720, 730
-6069 and
On
6641615-3 (Except Upper Cap) Main
Landing Gear Oleo Assembly Discard
38,000
Landings
N/A
720, 730
-5001,
-5003 thru
-5206
6641615-4 (Except Upper Cap) Main
Landing Gear Oleo Assembly Discard
38,000
Landings
N/A
720, 730
-5207 thru
-5294
Upper Cap 6641616-3 Main Landing
Gear Oleo Assembly Discard
4600
Landings
N/A
720, 730
-5001,
-5003 thru
-5294
6641615-5 (Except Upper Cap) Main
Landing Gear Oleo Assembly Discard
38,000
Landings
N/A
720, 730
-6069 and
On
6641615-6 (Except Upper Cap) Main
Landing Gear Oleo Assembly Discard
38,000
Landings
N/A
720, 730
-5320 thru
-6068
6641615-7 (Except Upper Cap) Main
Landing Gear Oleo Assembly Discard
38,000
Landings
N/A
720, 730
-6069 and
On
Upper Cap 6641616-4 Main Landing
Gear Oleo Assembly Discard
14,900
Landings
N/A
720, 730
-5295 thru
-6068
Upper Cap 6641616-5 Main Landing
Gear Oleo Assembly Discard
14,900
Landings
N/A
720, 730
-6069 and
On
9912537-1 Left Main Landing Gear
Actuator Assembly Discard
70,200
Landings
N/A
730
-5001 thru
-5037
9912537-3 Left Main Landing Gear
Actuator Assembly Discard
70,200
Landings
N/A
730
-5038 thru
-6081
9912537-5 Left Main Landing Gear
Actuator Assembly Discard
70,200
Landings
N/A
730
-6082 and
On
9912537-2 Right Main Landing Gear
Actuator Assembly Discard
70,200
Landings
N/A
720
-5001 thru
-5037
9912537-4 Right Main Landing Gear
Actuator Assembly Discard
70,200
Landings
N/A
720
-5038 thru
-6081
9912537-6 Right Main Landing Gear
Actuator Assembly Discard
70,200
Landings
N/A
720
-6082 and
On
4-10-01
© TEXTRON AVIATION INC.
Page 15
Sep 27/2018
CESSNA®
MODEL 560XL
MAINTENANCE MANUAL
Table 3. System and Structural Component Time Limit Tasks (continued)
Maintenance
Manual Task #
32-20-00-9600
Interval/
Note(s)
Inspection
Document
Zone
Effectivity (Part
Substitutions May
Apply)
6642610-3 Nose Landing Gear
Assembly Discard
33,300
Landings
N/A
710
-5001 thru
-5017
6642614-1 Nose Landing Gear
Assembly Discard
33,300
Landings
N/A
710
-5018 thru
-5500
6642625-1 Nose Landing Gear
Assembly Discard
33,300
Landings
N/A
710
-5501 thru
-5675
6642625-5 Nose Landing Gear
Assembly Discard
33,300
Landings
N/A
710
-5676 thru
-5716
6642625-6 Nose Landing Gear
Assembly Discard
33,300
Landings
N/A
710
-5717 thru
-5763
6642625-8 Nose Landing Gear
Assembly Discard
33,300
Landings
N/A
710
-5764 thru
-6068
6642625-10 Nose Landing Gear
Assembly Discard
33,300
Landings
N/A
710
-6069 thru
-6075
6642625-12 Nose Landing Gear
Assembly Discard
33,300
Landings
N/A
710
-6076 thru
-6081
6642625-14 Nose Landing Gear
Assembly Discard
33,300
Landings
N/A
710
-6082 thru
-6187
6642625-214 Nose Landing Gear
Assembly Discard
33,300
Landings
N/A
710
-5501 thru
-6261
6642635-1 Nose Landing Gear
Assembly Discard
33,300
Landings
N/A
710
-6188 thru
-6261
6642635-2 Nose Landing Gear
Assembly Discard
33,300
Landings
N/A
710
-6188 thru
-6261
6642635-4 Nose Landing Gear
Assembly Discard
33,300
Landings
N/A
710
-6262 and
On
6642635-5 Nose Landing Gear
Assembly Discard
33,300
Landings
N/A
710
-6262 and
On
6642635-201 Nose Landing Gear
Assembly Discard
33,300
Landings
N/A
710
-6262 and
On
6642635-202 Nose Landing Gear
Assembly Discard
33,300
Landings
N/A
710
-6262 and
On
Task Title
4-10-01
© TEXTRON AVIATION INC.
Page 16
Sep 27/2018
CESSNA®
MODEL 560XL
MAINTENANCE MANUAL
Table 3. System and Structural Component Time Limit Tasks (continued)
Maintenance
Manual Task #
32-20-00-9601
Interval/
Note(s)
Inspection
Document
Zone
Effectivity (Part
Substitutions May
Apply)
9912491-2 Nose Landing Gear
Actuator Discard
33,300
Landings
N/A
710
-5002 thru
-5017
9912491-3 Nose Landing Gear
Actuator Discard
33,300
Landings
N/A
710
-5018 thru
-5343
9912491-4 Nose Landing Gear
Actuator Discard
33,300
Landings
N/A
710
-5344 thru
-5537
9912491-5 Nose Landing Gear
Actuator Discard
33,300
Landings
N/A
710
-5001, and
-5338 thru
-6081
9912491-6 Nose Landing Gear
Actuator Discard
33,300
Landings
N/A
710
-6082 and
On
Task Title
Chapter 53 - Fuselage
NOTE:
The attaching hardware related to these landing gear installations is to be replaced whenever the associated
components are replaced. The attaching hardware can be used again if a rental component is to be installed
for no more than 100 Landings. The attaching hardware can also be used again if the original gear is to be
installed again. If a replacement gear is installed, all of the attachment hardware must be replaced.
53-00-00-9600
53-00-00-9601
6613020-1 Left Nose Landing Gear
Trunnion Support Assembly Discard
25,500
Landings
N/A
710
-5002 thru
-5085
6613020-55 Left Nose Landing Gear
Trunnion Support Assembly Discard
25,500
Landings
N/A
710
-5086 thru
-6068
6613020-63 Left Nose Landing Gear
Trunnion Support Assembly Discard
25,500
Landings
N/A
710
-6069 and
On
6613020-2 Right Nose Landing Gear
Trunnion Support Assembly Discard
25,500
Landings
N/A
710
-5002 thru
-5085
6613020-56 Right Nose Landing Gear
Trunnion Support Assembly Discard
25,500
Landings
N/A
710
-5086 thru
-6068
6613020-64 Right Nose Landing Gear
Trunnion Support Assembly Discard
25,500
Landings
N/A
710
-6069 and
On
6211191-2 Nose Landing Gear
Actuator Fitting Assembly Discard
25,500
Landings
N/A
710
-5001 thru
-5264
6211191-3 Nose Landing Gear
Actuator Fitting Assembly Discard
25,500
Landings
N/A
710
-5265 and
On
Chapter 57 - Wings
NOTE:
The attaching hardware related to these landing gear installations is to be replaced whenever the associated
components are replaced. The attaching hardware can be used again if a rental component is to be installed
for no more than 100 Landings. The attaching hardware can also be used again if the original gear is to be
installed again. If a replacement gear is installed, all of the attachment hardware must be replaced.
4-10-01
© TEXTRON AVIATION INC.
Page 17
Sep 27/2018
CESSNA®
MODEL 560XL
MAINTENANCE MANUAL
Table 3. System and Structural Component Time Limit Tasks (continued)
Maintenance
Manual Task #
57-10-00-9600
57-10-00-9601
57-10-00-9602
57-50-04-9600
Interval/
Note(s)
Inspection
Document
Zone
Effectivity (Part
Substitutions May
Apply)
6622123-1 Left Main Landing Gear
Forward Trunnion Fitting Discard
23,800
Landings
N/A
730
-5001 thru
-6068
6622123-5 Left Main Landing Gear
Forward Trunnion Fitting Discard
23,800
Landings
N/A
730
-6069 and
On
6622123-2 Right Main Landing Gear
Forward Trunnion Fitting Discard
23,800
Landings
N/A
720
-5001 thru
-6068
6622123-6 Right Main Landing Gear
Forward Trunnion Fitting Discard
23,800
Landings
N/A
720
-6069 and
On
6622124-1 Left Main Landing Gear Aft
Trunnion Fitting Discard
23,800
Landings
N/A
730
-5001 thru
-6068
6622124-5 Left Main Landing Gear Aft
Trunnion Fitting Discard
23,800
Landings
N/A
730
-6069 and
On
6622124-2 Right Main Landing Gear
Aft Trunnion Fitting Discard
23,800
Landings
N/A
720
-5001 thru
-6068
6622124-6 Right Main Landing Gear
Aft Trunnion Fitting Discard
23,800
Landings
N/A
720
-6069 and
On
6621125-1 Left Main Landing Gear
Actuator Fitting Discard
23,800
Landings
N/A
730
-5001 thru
-5022
6621125-5 Left Main Landing Gear
Actuator Fitting Discard
23,800
Landings
N/A
730
-5023 thru
-6068
6621125-9 Left Main Landing Gear
Actuator Fitting Discard
23,800
Landings
N/A
730
-6069 and
On
6621125-2 Right Main Landing Gear
Actuator Fitting Discard
23,800
Landings
N/A
720
-5001 thru
-5022
6621125-6 Right Main Landing Gear
Actuator Fitting Discard
23,800
Landings
N/A
720
-5023 thru
-6068
6621125-10 Right Main Landing Gear
Actuator Fitting Discard
23,800
Landings
N/A
720
-6069 and
On
S3049-5F8 Inboard and Outboard
Flap Rollers Discard
5000
Landings
N/A
500, 600
-5001 and
On
Task Title
4-10-01
© TEXTRON AVIATION INC.
Page 18
Sep 27/2018
CESSNA®
MODEL 560XL
MAINTENANCE MANUAL
AIRWORTHINESS LIMITATIONS INSPECTION TIME LIMITS
Russian Certified Airplanes
1.
Purpose and Use
A.
This section includes all airworthiness limitations maintenance tasks for Model 560XL Airplanes
certified in Russia.
NOTE:
Refer to Chapter 5-12-00, MSG-3 Inspection Documents and Other Required Tasks for a
complete list of the Model 560XL scheduled inspection requirements.
B.
The intervals specified represent the maximum time allowable between inspections.
C.
The MM task numbers are hyperlinked to task details in this manual. The Zone number(s) are also
hyperlinked to Chapter 6, Airplane Zoning - Description and Operation to assist in planning and
completing the tasks.
D.
System Maintenance Requirements
(1) System inspections and Component Time Limits are given in Table 1 and Table 3. The tasks
and intervals specified are mandatory and cannot be changed, escalated, or deleted without the
concurrence of the responsible Aircraft Certification Office (ACO).
E.
Structural Inspection Time Limits
(1) In accordance with §25.571(a) Inspection Time Limits and Component Time Limits are defined
for the Model 560XL and presented in Table 2 and Table 3.
F.
Corrosion Prevention
(1) The airworthiness limitations recondition and discard intervals assume corrosion is maintained
to Level 1 or better. Level 1 is achieved by maintaining the aircraft according to the MSG-3
maintenance procedures identified in this Model 560XL Maintenance Manual. Refer to Chapter
5-10-00, Maintenance Planning Document, Corrosion Prevention and Control Program (CPCP)
for further details.
G.
For
(1)
(2)
(3)
H.
System Maintenance Requirement Tasks
groups of common tasks, refer to:
Table 1 Russian System Maintenance Requirement Tasks
Table 2 Russian Structural Limitation Item Tasks
Table 3 System and Structural Component Time Limit Tasks
(a) Refer to Table 3 for Component Time Limits Tasks that have been duplicated from Table 1
and Table 2 to assist operators in maintenance planning.
NOTE:
All initial intervals are repeat intervals unless otherwise noted.
NOTE:
Inspections that do not apply to all airplanes will have the effectivity noted in the title of
the Inspection Task.
Table 1. Russian System Maintenance Requirement Tasks
Maintenance
Manual Task #
Task Title
Interval/
Note(s)
Inspection
Document
Zone
Effectivity
Chapter 21 - Air Conditioning
4-10-02
© TEXTRON AVIATION INC.
Page 1
Sep 27/2018
CESSNA®
MODEL 560XL
MAINTENANCE MANUAL
Table 1. Russian System Maintenance Requirement Tasks (continued)
Maintenance
Manual Task #
21-52-00-2100
Task Title
Vapor Cycle Cooling System
Hour Meter Visual Check
(Airplanes -5001 thru -5374
Incorporating Vapor Cycle Cooling
with 1134104-1 and -5 Compressor
Motors)
Interval/
Note(s)
300 Flight
Hours
Inspection
Document
Zone
Effectivity
311
-5001 thru
-5374 Incorporating Vapor Cycle Cooling System with
1134104-1
and -5
Compressor Motors
N/A
311
-5001 thru
-5374 Incorporating Vapor Cycle Cooling System With
1134104-1
and -5
Compressor Motors
N/A
247
-6001 and
On
4-12-MP
NOTE:
Refer to the Enviro Systems
Inc. Operating, Servicing and
Component Maintenance Manual
21-00-06.
21-52-00-9600
Vapor Cycle Cooling System Drive
Motor Brush Discard (Airplanes
-5001 thru -5374 Incorporating
Vapor Cycle Cooling System With
1134104-1 and -5 Compressor
Motors)
NOTE:
Refer to the Enviro Systems
Inc. Operating, Servicing and
Component Maintenance Manual
21-00-06.
500
Compressor
Hours
Chapter 76 - Engine Controls
Time Limited Dispatch Fault Visual
Check (Airplanes -6001 and On)
NOTE:
The repair of any detected faults
found between inspections may
be deferred until the end of the
interval and the airplane can be
dispatched with faults until the end
of the interval.
76-16-00-7100
NOTE:
TLD faults, inspection intervals and
dispatch limitations are defined by
the PW545C Engine Maintenance
Manual, Airworthiness Limitations
section. The tasks and intervals
specified are mandatory and
cannot be changed, escalated or
deleted without concurrence of the
responsible Aircraft Certification
Office (ACO).
170 Flight
Hours (See
NOTES)
4-10-02
© TEXTRON AVIATION INC.
Page 2
Sep 27/2018
CESSNA®
MODEL 560XL
MAINTENANCE MANUAL
I.
Structural Limitation Item Tasks
NOTE:
All initial intervals are repeat intervals unless otherwise noted.
NOTE:
Inspections that do not apply to all airplanes will have the effectivity noted in the title of
the Inspection Task.
NOTE:
For life-limited parts found in Table 2, replacement parts may have part numbers effective
on later units or spares.
Table 2. Russian Structural Limitation Item Tasks
Maintenance
Manual Task #
Task Title
Interval/
Note(s)
Inspection
Document
Zone
Effectivity (Part
Substitutions May
Apply)
Chapter 32 - Landing Gear
NOTE:
The attaching hardware related to these landing gear installations is to be replaced whenever the associated
components are replaced. The attaching hardware can be used again if a rental component is to be installed
for no more than 100 Landings. The attaching hardware can also be used again if the original gear is to be
installed again. If a replacement gear is installed, all of the attachment hardware must be replaced.
32-10-00-9601
6641640-5 Left Main Landing Gear
Trunnion Subassembly Discard
4500
Landings
N/A
730
-5001 thru
-5037
6641640-39 Left Main Landing Gear
Trunnion Subassembly Discard
4400
Landings
N/A
730
5038 thru
-5150
6641630-5 Left Main Landing Gear
Trunnion Subassembly Discard
4100
Landings
N/A
730
-5151 thru
-5339
6641630-27 Left Main Landing Gear
Trunnion Subassembly Discard
20,000
Landings
N/A
730
-5340 thru
-6068
6641630-39 Left Main Landing Gear
Trunnion Subassembly Discard
20,000
Landings
N/A
730
-6069 thru
-6093
6641630-41 Left Main Landing Gear
Trunnion Subassembly Discard
20,000
Landings
N/A
730
-6094 and
On
6641640-6 Right Main Landing Gear
Trunnion Subassembly Discard
4500
Landings
N/A
720
-5001 thru
-5337
6641640-40 Right Main Landing Gear
Trunnion Subassembly Discard
4400
Landings
N/A
720
-5038 thru
-5150
6641630-6 Right Main Landing Gear
Trunnion Subassembly Discard
4100
Landings
N/A
720
-5151 thru
-5339
6641630-28 Right Main Landing Gear
Trunnion Subassembly Discard
20,000
Landings
N/A
720
-5340 thru
-6068
6641630-40 Right Main Landing Gear
Trunnion Subassembly Discard
20,000
Landings
N/A
720
-6069 thru
-6093
6641630- 42 Right Main Landing Gear
Trunnion Subassembly Discard
20,000
Landings
N/A
720
-6094 and
On
4-10-02
© TEXTRON AVIATION INC.
Page 3
Sep 27/2018
CESSNA®
MODEL 560XL
MAINTENANCE MANUAL
Table 2. Russian Structural Limitation Item Tasks (continued)
Maintenance
Manual Task #
32-10-00-9602
Interval/
Note(s)
Inspection
Document
Zone
Effectivity (Part
Substitutions May
Apply)
6641640-7 Left Main Landing Gear
Trailing Link Assembly Discard
3800
Landings
N/A
730
-5001 thru
-5002
6641640-15 Left Main Landing Gear
Trailing Link Assembly Discard
3800
Landings
N/A
730
-5009 thru
-5014
6641648-1 Left Main Landing Gear
Trailing Link Assembly Discard
3800
Landings
N/A
730
-5003 thru
-5008 and
-5015 thru
-5037
6641648-7 Left Main Landing Gear
Trailing Link Assembly Discard
3800
Landings
N/A
730
-5038 thru
-5150
6641648-9 Left Main Landing Gear
Trailing Link Assembly Discard
24,000
Landings
N/A
730
-5151 thru
-5223
6641648-15 Left Main Landing Gear
Trailing Link Assembly Discard
24,000
Landings
N/A
730
-5224 thru
-5673
6641530-1 Left Main Landing Gear
Trailing Link Assembly Discard
20,000
Landings
N/A
730
-5674 thru
-6237
6641530-3 Left Main Landing Gear
Trailing Link Assembly Discard
20,000
Landings
N/A
730
-6238 and
On
DDA06877-1 Left Main Landing Gear
Trailing Link Assembly Discard
20,000
Landings
N/A
730
-6238 thru
-6243
6641640-8 Right Main Landing Gear
Trailing Link Assembly Discard
3800
Landings
N/A
720
-5001 thru
-5002
6641640-16 Right Main Landing Gear
Trailing Link Assembly Discard
3800
Landings
N/A
720
-5009 thru
-5014
6641648-2 Right Main Landing Gear
Trailing Link Assembly Discard
3800
Landings
N/A
720
-5003 thru
-5006 and
-5015 thru
-5037
6641648-8 Right Main Landing Gear
Trailing Link Assembly Discard
3800
Landings
N/A
720
-5038 thru
-5150
6641648-10 Right Main Landing Gear
Trailing Link Assembly Discard
24,000
Landings
N/A
720
-5151 thru
-5223
6641648-14 Right Main Landing Gear
Trailing Link Assembly Discard
24,000
Landings
N/A
720
-5224 thru
-5673
6641530-2 Right Main Landing Gear
Trailing Link Assembly Discard
20,000
Landings
N/A
720
-5674 thru
-6237
6641530-4 Right Main Landing Gear
Trailing Link Assembly Discard
20,000
Landings
N/A
720
-6238 and
On
DDA06877-2 Right Main Landing Gear
Trailing Link Assembly Discard
20,000
Landings
N/A
720
-6238 thru
-6243
Task Title
4-10-02
© TEXTRON AVIATION INC.
Page 4
Sep 27/2018
CESSNA®
MODEL 560XL
MAINTENANCE MANUAL
Table 2. Russian Structural Limitation Item Tasks (continued)
Maintenance
Manual Task #
32-10-00-9603
32-10-00-9604
32-10-00-9605
Task Title
Interval/
Note(s)
Inspection
Document
Zone
Effectivity (Part
Substitutions May
Apply)
6641618-8 Main Landing Gear Trailing
Link Spacer Discard
3700
Landings
N/A
720, 730
-5001 thru
-5002
6641618-9 Main Landing Gear Trailing
Link Spacer Discard
3700
Landings
N/A
720, 730
-5003 thru
-5037
6641618-12 Main Landing Gear
Trailing Link Spacer Discard
3700
Landings
N/A
720, 730
-5038 thru
-5150
6641533-1 Main Landing Gear Trailing
Link Spacer Discard
20,000
Landings
N/A
720, 730
-5674 thru
-6068
6641533-2 Main Landing Gear Trailing
Link Spacer Discard
20,000
Landings
N/A
720, 730
-6069 and
On
6641615-3 (Except Upper Cap) Main
Landing Gear Oleo Assembly Discard
22,800
Landings
N/A
720, 730
-5001,
-5003 thru
-5206
6641615-4 (Except Upper Cap) Main
Landing Gear Oleo Assembly Discard
22,800
Landings
N/A
720, 730
-5207 thru
-5294
Upper Cap 6641616-3 Main Landing
Gear Oleo Assembly Discard
2800
Landings
N/A
720, 730
-5001,
-5003 thru
-5294
6641615-5 (Except Upper Cap) Main
Landing Gear Oleo Assembly Discard
22,800
Landings
N/A
720, 730
-6069 and
On
6641615-6 (Except Upper Cap) Main
Landing Gear Oleo Assembly Discard
22,800
Landings
N/A
720, 730
-5320 thru
-6068
6641615-7 (Except Upper Cap) Main
Landing Gear Oleo Assembly Discard
22,800
Landings
N/A
720, 730
-6069 and
On
Upper Cap 6641616-4 Main Landing
Gear Oleo Assembly Discard
8900
Landings
N/A
720, 730
-5295 thru
-6068
Upper Cap 6641616-5 Main Landing
Gear Oleo Assembly Discard
8900
Landings
N/A
720, 730
-6069 and
On
9912537-1 Left Main Landing Gear
Actuator Assembly Discard
42,000
Landings
N/A
730
-5001 thru
-5037
9912537-3 Left Main Landing Gear
Actuator Assembly Discard
42,000
Landings
N/A
730
-5038 thru
-6081
9912537-5 Left Main Landing Gear
Actuator Assembly Discard
42,000
Landings
N/A
730
-6082 and
On
9912537-2 Right Main Landing Gear
Actuator Assembly Discard
42,000
Landings
N/A
720
-5001 thru
-5037
9912537-4 Right Main Landing Gear
Actuator Assembly Discard
42,000
Landings
N/A
720
-5038 thru
-6081
9912537-6 Right Main Landing Gear
Actuator Assembly Discard
42,000
Landings
N/A
720
-6082 and
On
4-10-02
© TEXTRON AVIATION INC.
Page 5
Sep 27/2018
CESSNA®
MODEL 560XL
MAINTENANCE MANUAL
Table 2. Russian Structural Limitation Item Tasks (continued)
Maintenance
Manual Task #
32-20-00-9600
Interval/
Note(s)
Inspection
Document
Zone
Effectivity (Part
Substitutions May
Apply)
6642610-3 Nose Landing Gear
Assembly Discard
20,000
Landings
N/A
710
-5001 thru
-5017
6642614-1 Nose Landing Gear
Assembly Discard
20,000
Landings
N/A
710
-5018 thru
-5500
6642625-1 Nose Landing Gear
Assembly Discard
20,000
Landings
N/A
710
-5501 thru
-5675
6642625-5 Nose Landing Gear
Assembly Discard
20,000
Landings
N/A
710
-5676 thru
-5716
6642625-6 Nose Landing Gear
Assembly Discard
20,000
Landings
N/A
710
-5717 thru
-5763
6642625-8 Nose Landing Gear
Assembly Discard
20,000
Landings
N/A
710
-5764 thru
-6068
6642625-10 Nose Landing Gear
Assembly Discard
20,000
Landings
N/A
710
-6069 thru
-6075
6642625-12 Nose Landing Gear
Assembly Discard
20,000
Landings
N/A
710
-6076 thru
-6081
6642625-14 Nose Landing Gear
Assembly Discard
20,000
Landings
N/A
710
-6082 thru
-6187
6642625-214 Nose Landing Gear
Assembly Discard
20,000
Landings
N/A
710
-5501 thru
-6261
6642635-1 Nose Landing Gear
Assembly Discard
20,000
Landings
N/A
710
-6188 thru
-6261
6642635-2 Nose Landing Gear
Assembly Discard
20,000
Landings
N/A
710
-6188 thru
-6261
6642635-4 Nose Landing Gear
Assembly Discard
20,000
Landings
N/A
710
-6262 and
On
6642635-5 Nose Landing Gear
Assembly Discard
20,000
Landings
N/A
710
-6262 and
On
6642635-201 Nose Landing Gear
Assembly Discard
20,000
Landings
N/A
710
-6262 and
On
6642635-202 Nose Landing Gear
Assembly Discard
20,000
Landings
N/A
710
-6262 and
On
Task Title
4-10-02
© TEXTRON AVIATION INC.
Page 6
Sep 27/2018
CESSNA®
MODEL 560XL
MAINTENANCE MANUAL
Table 2. Russian Structural Limitation Item Tasks (continued)
Maintenance
Manual Task #
32-20-00-9601
Interval/
Note(s)
Inspection
Document
Zone
Effectivity (Part
Substitutions May
Apply)
9912491-2 Nose Landing Gear
Actuator Discard
20,000
Landings
N/A
710
-5002 thru
-5017
9912491-3 Nose Landing Gear
Actuator Discard
20,000
Landings
N/A
710
-5018 thru
-5343
9912491-4 Nose Landing Gear
Actuator Discard
20,000
Landings
N/A
710
-5344 thru
-5537
9912491-5 Nose Landing Gear
Actuator Discard
20,000
Landings
N/A
710
-5001, and
-5338 thru
-6081
9912491-6 Nose Landing Gear
Actuator Discard
20,000
Landings
N/A
710
-6082 and
On
Task Title
Chapter 52 - Doors
52-10-00-2200
Cabin Door Assembly Detailed
Inspection
15,000
Flight
Hours
4-12-ME
810, 811
-5001 and
On
52-20-00-2200
Emergency Exit Door Assembly
Detailed Inspection
15,000
Flight
Hours
4-12-ME
820, 821
-5001 and
On
Chapter 53 - Fuselage
NOTE:
The attaching hardware related to these landing gear installations is to be replaced whenever the associated
components are replaced. The attaching hardware can be used again if a rental component is to be installed
for no more than 100 Landings. The attaching hardware can also be used again if the original gear is to be
installed again. If a replacement gear is installed, all of the attachment hardware must be replaced.
53-00-00-9600
53-00-00-9601
6613020-1 Left Nose Landing Gear
Trunnion Support Assembly Discard
15,300
Landings
N/A
710
-5002 thru
-5085
6613020-55 Left Nose Landing Gear
Trunnion Support Assembly Discard
15,300
Landings
N/A
710
-5086 thru
-6068
6613020-63 Left Nose Landing Gear
Trunnion Support Assembly Discard
15,300
Landings
N/A
710
-6069 and
On
6613020-2 Right Nose Landing Gear
Trunnion Support Assembly Discard
15,300
Landings
N/A
710
-5002 thru
-5085
6613020-56 Right Nose Landing Gear
Trunnion Support Assembly Discard
15,300
Landings
N/A
710
-5086 thru
-6068
6613020-64 Right Nose Landing Gear
Trunnion Support Assembly Discard
15,300
Landings
N/A
710
-6069 and
On
6211191-2 Nose Landing Gear
Actuator Fitting Assembly Discard
15,300
Landings
N/A
710
-5001 thru
-5264
6211191-3 Nose Landing Gear
Actuator Fitting Assembly Discard
15,300
Landings
N/A
710
-5265 and
On
4-10-02
© TEXTRON AVIATION INC.
Page 7
Sep 27/2018
CESSNA®
MODEL 560XL
MAINTENANCE MANUAL
Table 2. Russian Structural Limitation Item Tasks (continued)
Maintenance
Manual Task #
Task Title
Interval/
Note(s)
Inspection
Document
Zone
Effectivity (Part
Substitutions May
Apply)
6000
Flight
Hours
or 120
Months,
Whichever
Comes
First, Then
Every
2400
Hours
or 120
Months,
Whichever
Comes
First
Thereafter
4-12-MD
141, 142,
241, 242
-5001 and
On
4-12-ME
171, 172,
261, 262
-5001 and
On
4-12-MJ
213, 214,
243, 244,
253, 254,
263, 264,
323, 324
-5001 and
On
-5001 and
On
53-10-11-2501
Forward Pressure Bulkhead (Eddy
Current) Special Detailed Inspection
53-10-11-2502
Aft Pressure Bulkhead General Visual
Inspection
15,000
Flight
Hours
53-30-01-2100
Upper Fuselage Skin from Right
Stringer 13 to Left Stringer 13 General
Visual Inspection
13,000
Flight
Hours
53-30-01-2101
Lower Fuselage Skin from Right
Stringer 13 to Left Stringer 13 General
Visual Inspection
15,000
Flight
Hours
4-12-ME
143, 144,
151, 152,
161, 162,
171, 172,
213, 214,
223, 224,
321, 322
53-30-01-2501
Upper Fuselage Skin Splice at BL
0.00 (Eddy Current) Special Detailed
Inspection
15,000
Flight
Hours
4-12-ME
241, 242,
251, 252,
261, 262
-5001 and
On
53-30-01-2502
Lower Fuselage Skin Splices at
Stringers 13R and 13L (Eddy Current)
Special Detailed Inspection
15,000
Flight
Hours
4-12-ME
151, 152,
161, 162,
171, 172
-5001 and
On
Chapter 54 - Nacelles/Pylons
4-10-02
© TEXTRON AVIATION INC.
Page 8
Sep 27/2018
CESSNA®
MODEL 560XL
MAINTENANCE MANUAL
Table 2. Russian Structural Limitation Item Tasks (continued)
Maintenance
Manual Task #
Interval/
Note(s)
Inspection
Document
Zone
Effectivity (Part
Substitutions May
Apply)
3000
Flight
Hours,
Then
Every
1500
Flight
Hours
Thereafter
4-12-MB
311, 312,
411, 412
-5001 thru
-5060
13,000
Flight
Hours
4-12-MJ
311, 312,
411, 412
-5001 thru
-5060
Vertical Stabilizer Rear Spar Cap
at WL 146 (Eddy Current) Special
Detailed Inspection (Airplanes -5001
thru -5020)
6500
Flight
Hours,
Then
Every
3000
Flight
Hours
Thereafter
4-12-MG
321, 322,
340
-5001 thru
-5020
Vertical Stabilizer Rear Spar Nested
Angle at WL 146 (Eddy Current)
Special Detailed Inspection (Airplanes
-5001 thru -5020)
11,000
Flight
Hours,
Then
Every
6000
Flight
Hours
Thereafter
4-12-MH
321, 322,
340
-5001 thru
-5020
Vertical Stabilizer Rear Spar Strap at
WL 146.00 (Eddy Current) Special
Detailed Inspection (Airplanes -5001
thru -5020)
5000
Flight
Hours,
Then
Every
2500
Flight
Hours
Thereafter
4-12-MI
321, 322,
340
-5001 thru
-5020
Task Title
54-50-10-2100
Aft Engine Beam General Visual
Inspection (Airplanes -5001 thru
-5060)
54-50-10-2500
Forward Engine Beam Upper Angles,
Horizontal Cap Flange at BL 30.5
thru BL 42.0 (Eddy Current) Special
Detailed Inspection (Airplanes -5001
thru -5060)
Chapter 55 - Stabilizers
55-30-00-2500
55-30-00-2501
55-30-00-2502
4-10-02
© TEXTRON AVIATION INC.
Page 9
Sep 27/2018
CESSNA®
MODEL 560XL
MAINTENANCE MANUAL
Table 2. Russian Structural Limitation Item Tasks (continued)
Maintenance
Manual Task #
55-30-00-2503
55-30-00-2504
Task Title
Interval/
Note(s)
Inspection
Document
Zone
Effectivity (Part
Substitutions May
Apply)
Vertical Stabilizer Forward Spar Strap
at WL 150 (Eddy Current) Special
Detailed Inspection (Airplanes -5001
thru -5020)
11,500
Flight
Hours,
Then
Every
9000
Flight
Hours
Thereafter
4-12-MK
321, 322,
340
-5001 thru
-5020
Vertical Stabilizer Forward Spar Strap
at WL 188.00 (Eddy Current) Special
Detailed Inspection (Airplanes -5001
thru -5020)
10,000
Flight
Hours,
Then
Every
5000
Flight
Hours
Thereafter
4-12-MR
340
-5001 thru
-5020
Lower Wing Main Spar Lower Skin
Splice at WS 22.50 (Eddy Current)
Special Detailed Inspection
7500
Flight
Hours,
Then
Every
1400
Flight
Hours
Thereafter
4-12-MF
515, 516
-5001 and
On
Lower Wing Main Spar Skin Splice
Flange at WS 11.50 (Eddy Current)
Special Detailed Inspection
11,500
Flight
Hours,
Then
Every
3300
Flight
Hours
Thereafter
4-12-ML
515, 615
-5001 and
On
Lower Wing Main Spar at WS
114.57(Eddy Current) Special Detailed
Inspection
11,000
Flight
Hours,
Then
Every
4200
Flight
Hours
Thereafter
4-12-MM
523, 524,
623, 624
-5001 and
On
Chapter 57 - Wings
57-10-00-2500
57-10-00-2501
57-10-00-2502
4-10-02
© TEXTRON AVIATION INC.
Page 10
Sep 27/2018
CESSNA®
MODEL 560XL
MAINTENANCE MANUAL
Table 2. Russian Structural Limitation Item Tasks (continued)
Maintenance
Manual Task #
57-10-00-2503
57-10-00-2504
Task Title
Interval/
Note(s)
Inspection
Document
Zone
Effectivity (Part
Substitutions May
Apply)
Lower Wing Main Spar at WS 131.07
(Eddy Current) Special Detailed
Inspection
9000
Flight
Hours,
Then
Every
3400
Flight
Hours
Thereafter
4-12-MN
523, 524,
623, 624
-5001 and
On
Lower Wing Main Spar at WS 149.57
(Eddy Current) Special Detailed
Inspection
12,500
Flight
Hours,
Then
Every
6100
Flight
Hours
Thereafter
4-12-MO
523, 524,
623, 624
-5001 and
On
NOTE:
The attaching hardware related to these landing gear installations is to be replaced whenever the associated
components are replaced. The attaching hardware can be used again if a rental component is to be installed
for no more than 100 Landings. The attaching hardware can also be used again if the original gear is to be
installed again. If a replacement gear is installed, all of the attachment hardware must be replaced.
57-10-00-9600
57-10-00-9601
6622123-1 Left Main Landing Gear
Forward Trunnion Fitting Discard
14,300
Landings
N/A
730
-5001 thru
-6068
6622123-5 Left Main Landing Gear
Forward Trunnion Fitting Discard
14,300
Landings
N/A
730
-6069 and
On
6622123-2 Right Main Landing Gear
Forward Trunnion Fitting Discard
14,300
Landings
N/A
720
-5001 thru
-6068
6622123-6 Right Main Landing Gear
Forward Trunnion Fitting Discard
14,300
Landings
N/A
720
-6069 and
On
6622124-1 Left Main Landing Gear Aft
Trunnion Fitting Discard
14,300
Landings
N/A
730
-5001 thru
-6068
6622124-5 Left Main Landing Gear Aft
Trunnion Fitting Discard
14,300
Landings
N/A
730
-6069 and
On
6622124-2 Right Main Landing Gear
Aft Trunnion Fitting Discard
14,300
Landings
N/A
720
-5001 thru
-6068
6622124-6 Right Main Landing Gear
Aft Trunnion Fitting Discard
14,300
Landings
N/A
720
-6069 and
On
4-10-02
© TEXTRON AVIATION INC.
Page 11
Sep 27/2018
CESSNA®
MODEL 560XL
MAINTENANCE MANUAL
Table 2. Russian Structural Limitation Item Tasks (continued)
Maintenance
Manual Task #
57-10-00-9602
57-50-04-9600
J.
Interval/
Note(s)
Inspection
Document
Zone
Effectivity (Part
Substitutions May
Apply)
6621125-1 Left Main Landing Gear
Actuator Fitting Discard
14,300
Landings
N/A
730
-5001 thru
-5022
6621125-5 Left Main Landing Gear
Actuator Fitting Discard
14,300
Landings
N/A
730
-5023 thru
-6068
6621125-9 Left Main Landing Gear
Actuator Fitting Discard
14,300
Landings
N/A
730
-6069 and
On
6621125-2 Right Main Landing Gear
Actuator Fitting Discard
14,300
Landings
N/A
720
-5001 thru
-5022
6621125-6 Right Main Landing Gear
Actuator Fitting Discard
14,300
Landings
N/A
720
-5023 thru
-6068
6621125-10 Right Main Landing Gear
Actuator Fitting Discard
14,300
Landings
N/A
720
-6069 and
On
S3049-5F8 Inboard and Outboard
Flap Rollers Discard
5000
Landings
N/A
500, 600
-5001 and
On
Task Title
System and Structural Component Time Limit Tasks
NOTE:
All initial intervals are repeat intervals unless otherwise noted.
NOTE:
For life-limited parts found in Table 3, replacement parts may have part numbers effective
on later units or spares.
Table 3. Russian System and Structural Component Time Limit Tasks
Maintenance
Manual Task #
Task Title
Interval/
Note(s)
Inspection
Document
Zone
Effectivity (Part
Substitutions May
Apply)
311
-5001 thru
-5374 Incorporating Vapor Cycle Cooling With
1134104-1
and -5
Compressor Motors
Chapter 21 - Air Conditioning
21-52-00-9600
Vapor Cycle Cooling System Drive
Motor Brush Discard (Airplanes -5001
thru -5374 Incorporating Vapor Cycle
Cooling System With 1134104-1 and
-5 Compressor Motors)
NOTE:
Refer to the Enviro Systems Inc.
Operating, Servicing and Component
Maintenance Manual 21-00-06.
500 Compressor
Hours
N/A
Chapter 32 - Landing Gear
4-10-02
© TEXTRON AVIATION INC.
Page 12
Sep 27/2018
CESSNA®
MODEL 560XL
MAINTENANCE MANUAL
Table 3. Russian System and Structural Component Time Limit Tasks (continued)
Maintenance
Manual Task #
Task Title
Interval/
Note(s)
Inspection
Document
Zone
Effectivity (Part
Substitutions May
Apply)
NOTE:
The attaching hardware related to these landing gear installations is to be replaced whenever the associated
components are replaced. The attaching hardware can be used again if a rental component is to be installed
for no more than 100 Landings. The attaching hardware can also be used again if the original gear is to be
installed again. If a replacement gear is installed, all of the attachment hardware must be replaced.
32-10-00-9601
6641640-5 Left Main Landing Gear
Trunnion Subassembly Discard
4500
Landings
N/A
730
-5001 thru
-5037
6641640-39 Left Main Landing Gear
Trunnion Subassembly Discard
4400
Landings
N/A
730
5038 thru
-5150
6641630-5 Left Main Landing Gear
Trunnion Subassembly Discard
4100
Landings
N/A
730
-5151 thru
-5339
6641630-27 Left Main Landing Gear
Trunnion Subassembly Discard
20,000
Landings
N/A
730
-5340 thru
-6068
6641630-39 Left Main Landing Gear
Trunnion Subassembly Discard
20,000
Landings
N/A
730
-6069 thru
-6093
6641630-41 Left Main Landing Gear
Trunnion Subassembly Discard
20,000
Landings
N/A
730
-6094 and
On
6641640-6 Right Main Landing Gear
Trunnion Subassembly Discard
4500
Landings
N/A
720
-5001 thru
-5337
6641640-40 Right Main Landing Gear
Trunnion
4400
Landings
N/A
720
-5038 thru
-5350
6641630-6 Right Main Landing Gear
Trunnion Subassembly Discard
4100
Landings
N/A
720
-5151 thru
-5339
6641630-28 Right Main Landing Gear
Trunnion Subassembly Discard
20,000
Landings
N/A
720
-5340 thru
-6068
6641630-40 Right Main Landing Gear
Trunnion Subassembly Discard
20,000
Landings
N/A
720
-6069 thru
-6093
6641630- 42 Right Main Landing Gear
Trunnion Subassembly Discard
20,000
Landings
N/A
720
-6094 and
On
4-10-02
© TEXTRON AVIATION INC.
Page 13
Sep 27/2018
CESSNA®
MODEL 560XL
MAINTENANCE MANUAL
Table 3. Russian System and Structural Component Time Limit Tasks (continued)
Maintenance
Manual Task #
32-10-00-9602
Interval/
Note(s)
Inspection
Document
Zone
Effectivity (Part
Substitutions May
Apply)
6641640-7 Left Main Landing Gear
Trailing Link Assembly Discard
3800
Landings
N/A
730
-5001 thru
-5002
6641640-15 Left Main Landing Gear
Trailing Link Assembly Discard
3800
Landings
N/A
730
-5009 thru
-5014
6641648-1 Left Main Landing Gear
Trailing Link Assembly Discard
3800
Landings
N/A
730
-5003 thru
-5008 and
-5015 thru
-5037
6641648-7 Left Main Landing Gear
Trailing Link Assembly Discard
3800
Landings
N/A
730
-5038 thru
-5150
6641648-9 Left Main Landing Gear
Trailing Link Assembly Discard
24,000
Landings
N/A
730
-5151 thru
-5223
6641648-15 Left Main Landing Gear
Trailing Link Assembly Discard
24,000
Landings
N/A
730
-5224 thru
-5673
6641530-1 Left Main Landing Gear
Trailing Link Assembly Discard
20,000
Landings
N/A
730
-5674 thru
-6237
6641530-3 Left Main Landing Gear
Trailing Link d
20,000
Landings
N/A
730
-6238 and
On
DDA06877-1 Left Main Landing Gear
Trailing Link Assembly Discard
20,000
Landings
N/A
730
-6238 thru
-6243
6641640-8 Right Main Landing Gear
Trailing Link Assembly Discard
3800
Landings
N/A
720
-5001 thru
-5002
6641640-16 Right Main Landing Gear
Trailing Link Assembly Discard
3800
Landings
N/A
720
-5009 thru
-5014
6641648-2 Right Main Landing Gear
Trailing Link Assembly Discard
3800
Landings
N/A
720
-5003 thru
-5006 and
-5015 thru
-5037
6641648-8 Right Main Landing Gear
Trailing Link Assembly Discard
3800
Landings
N/A
720
-5038 thru
-5150
6641648-10 Right Main Landing Gear
Trailing Link Assembly Discard
24,000
Landings
N/A
720
-5151 thru
-5223
6641648-14 Right Main Landing Gear
Trailing Link Assembly Discard
24,000
Landings
N/A
720
-5224 thru
-5673
6641530-2 Right Main Landing Gear
Trailing Link Assembly Discard
20,000
Landings
N/A
720
-5674 thru
-6237
6641530-4 Right Main Landing Gear
Trailing Link Assembly Discard
20,000
Landings
N/A
720
-6238 and
On
DDA06877-2 Right Main Landing Gear
Trailing Link Assembly Discard
20,000
Landings
N/A
720
-6238 thru
-6243
Task Title
4-10-02
© TEXTRON AVIATION INC.
Page 14
Sep 27/2018
CESSNA®
MODEL 560XL
MAINTENANCE MANUAL
Table 3. Russian System and Structural Component Time Limit Tasks (continued)
Maintenance
Manual Task #
32-10-00-9603
32-10-00-9604
32-10-00-9605
Task Title
Interval/
Note(s)
Inspection
Document
Zone
Effectivity (Part
Substitutions May
Apply)
6641618-8 Main Landing Gear Trailing
Link Spacer Discard
3700
Landings
N/A
720, 730
-5001 thru
-5002
6641618-9 Main Landing Gear Trailing
Link Spacer Discard
3700
Landings
N/A
720, 730
-5003 thru
-5037
6641618-12 Main Landing Gear
Trailing Link Spacer Discard
3700
Landings
N/A
720, 730
-5038 thru
-5150
6641533-1 Main Landing Gear Trailing
Link Spacer Discard
20,000
Landings
N/A
720, 730
-5674 thru
-6068
6641533-2 Main Landing Gear Trailing
Link Spacer Discard
20,000
Landings
N/A
720, 730
-6069 and
On
6641615-3 (Except Upper Cap) Main
Landing Gear Oleo Assembly Discard
22,800
Landings
N/A
720, 730
-5001,
-5003 thru
-5206
6641615-4 (Except Upper Cap) Main
Landing Gear Oleo Assembly Discard
22,800
Landings
N/A
720, 730
-5207 thru
-5294
Upper Cap 6641616-3 Main Landing
Gear Oleo Assembly Discard
2800
Landings
N/A
720, 730
-5001,
-5003 thru
-5294
6641615-5 (Except Upper Cap) Main
Landing Gear Oleo Assembly Discard
22,800
Landings
N/A
720, 730
-6069 and
On
6641615-6 (Except Upper Cap) Main
Landing Gear Oleo Assembly Discard
22,800
Landings
N/A
720, 730
-5320 thru
-6068
6641615-7 (Except Upper Cap) Main
Landing Gear Oleo Assembly Discard
22,800
Landings
N/A
720, 730
-6069 and
On
Upper Cap 6641616-4 Main Landing
Gear Oleo Assembly Discard
8900
Landings
N/A
720, 730
-5295 thru
-6068
Upper Cap 6641616-5 Main Landing
Gear Oleo Assembly Discard
8900
Landings
N/A
720, 730
-6069 and
On
9912537-1 Left Main Landing Gear
Actuator Assembly Discard
42,000
Landings
N/A
730
-5001 thru
-5037
9912537-3 Left Main Landing Gear
Actuator Assembly Discard
42,000
Landings
N/A
730
-5038 thru
-6081
9912537-5 Left Main Landing Gear
Actuator Assembly Discard
42,000
Landings
N/A
730
-6082 and
On
9912537-2 Right Main Landing Gear
Actuator Assembly Discard
42,000
Landings
N/A
720
-5001 thru
-5037
9912537-4 Right Main Landing Gear
Actuator Assembly Discard
42,000
Landings
N/A
720
-5038 thru
-6081
9912537-6 Right Main Landing Gear
Actuator Assembly Discard
42,000
Landings
N/A
720
-6082 and
On
4-10-02
© TEXTRON AVIATION INC.
Page 15
Sep 27/2018
CESSNA®
MODEL 560XL
MAINTENANCE MANUAL
Table 3. Russian System and Structural Component Time Limit Tasks (continued)
Maintenance
Manual Task #
32-20-00-9600
Interval/
Note(s)
Inspection
Document
Zone
Effectivity (Part
Substitutions May
Apply)
6642610-3 Nose Landing Gear
Assembly Discard
20,000
Landings
N/A
710
-5001 thru
-5017
6642614-1 Nose Landing Gear
Assembly Discard
20,000
Landings
N/A
710
-5018 thru
-5500
6642625-1 Nose Landing Gear
Assembly Discard
20,000
Landings
N/A
710
-5501 thru
-5675
6642625-5 Nose Landing Gear
Assembly Discard
20,000
Landings
N/A
710
-5676 thru
-5716
6642625-6 Nose Landing Gear
Assembly Discard
20,000
Landings
N/A
710
-5717 thru
-5763
6642625-8 Nose Landing Gear
Assembly Discard
20,000
Landings
N/A
710
-5764 thru
-6068
6642625-10 Nose Landing Gear
Assembly Discard
20,000
Landings
N/A
710
-6069 thru
-6075
6642625-12 Nose Landing Gear
Assembly Discard
20,000
Landings
N/A
710
-6076 thru
-6081
6642625-14 Nose Landing Gear
Assembly Discard
20,000
Landings
N/A
710
-6082 thru
-6187
6642625-214 Nose Landing Gear
Assembly Discard
20,000
Landings
N/A
710
-5501 thru
-6261
6642635-1 Nose Landing Gear
Assembly Discard
20,000
Landings
N/A
710
-6188 thru
-6261
6642635-2 Nose Landing Gear
Assembly Discard
20,000
Landings
N/A
710
-6188 thru
-6261
6642635-4 Nose Landing Gear
Assembly Discard
20,000
Landings
N/A
710
-6262 and
On
6642635-5 Nose Landing Gear
Assembly Discard
20,000
Landings
N/A
710
-6262 and
On
6642635-201 Nose Landing Gear
Assembly Discard
20,000
Landings
N/A
710
-6262 and
On
6642635-202 Nose Landing Gear
Assembly Discard
20,000
Landings
N/A
710
-6262 and
On
Task Title
4-10-02
© TEXTRON AVIATION INC.
Page 16
Sep 27/2018
CESSNA®
MODEL 560XL
MAINTENANCE MANUAL
Table 3. Russian System and Structural Component Time Limit Tasks (continued)
Maintenance
Manual Task #
32-20-00-9601
Interval/
Note(s)
Inspection
Document
Zone
Effectivity (Part
Substitutions May
Apply)
9912491-2 Nose Landing Gear
Actuator Discard
20,000
Landings
N/A
710
-5002 thru
-5017
9912491-3 Nose Landing Gear
Actuator Discard
20,000
Landings
N/A
710
-5018 thru
-5343
9912491-4 Nose Landing Gear
Actuator Discard
20,000
Landings
N/A
710
-5344 thru
-5537
9912491-5 Nose Landing Gear
Actuator Discard
20,000
Landings
N/A
710
-5001, and
-5338 thru
-6081
9912491-6 Nose Landing Gear
Actuator Discard
20,000
Landings
N/A
710
-6082 and
On
Task Title
Chapter 53 - Fuselage
NOTE:
The attaching hardware related to these landing gear installations is to be replaced whenever the associated
components are replaced. The attaching hardware can be used again if a rental component is to be installed
for no more than 100 Landings. The attaching hardware can also be used again if the original gear is to be
installed again. If a replacement gear is installed, all of the attachment hardware must be replaced.
53-00-00-9600
53-00-00-9601
6613020-1 Left Nose Landing Gear
Trunnion Support Assembly Discard
15,300
Landings
N/A
710
-5002 thru
-5085
6613020-55 Left Nose Landing Gear
Trunnion Support Assembly Discard
15,300
Landings
N/A
710
-5086 thru
-6068
6613020-63 Left Nose Landing Gear
Trunnion Support Assembly Discard
15,300
Landings
N/A
710
-6069 and
On
6613020-2 Right Nose Landing Gear
Trunnion Support Assembly Discard
15,300
Landings
N/A
710
-5002 thru
-5085
6613020-56 Right Nose Landing Gear
Trunnion Support Assembly Discard
15,300
Landings
N/A
710
-5086 thru
-6068
6613020-64 Right Nose Landing Gear
Trunnion Support Assembly Discard
15,300
Landings
N/A
710
-6069 and
On
6211191-2 Nose Landing Gear
Actuator Fitting Assembly Discard
15,300
Landings
N/A
710
-5001 thru
-5264
6211191-3 Nose Landing Gear
Actuator Fitting Assembly Discard
15,300
Landings
N/A
710
-5265 and
On
Chapter 57 - Wings
NOTE:
The attaching hardware related to these landing gear installations is to be replaced whenever the associated
components are replaced. The attaching hardware can be used again if a rental component is to be installed
for no more than 100 Landings. The attaching hardware can also be used again if the original gear is to be
installed again. If a replacement gear is installed, all of the attachment hardware must be replaced.
4-10-02
© TEXTRON AVIATION INC.
Page 17
Sep 27/2018
CESSNA®
MODEL 560XL
MAINTENANCE MANUAL
Table 3. Russian System and Structural Component Time Limit Tasks (continued)
Maintenance
Manual Task #
57-10-00-9600
57-10-00-9601
57-10-00-9602
57-50-04-9600
Interval/
Note(s)
Inspection
Document
Zone
Effectivity (Part
Substitutions May
Apply)
6622123-1 Left Main Landing Gear
Forward Trunnion Fitting Discard
14,300
Landings
N/A
730
-5001 thru
-6068
6622123-5 Left Main Landing Gear
Forward Trunnion Fitting Discard
14,300
Landings
N/A
730
-6069 and
On
6622123-2 Right Main Landing Gear
Forward Trunnion Fitting Discard
14,300
Landings
N/A
720
-5001 thru
-6068
6622123-6 Right Main Landing Gear
Forward Trunnion Fitting Discard
14,300
Landings
N/A
720
-6069 and
On
6622124-1 Left Main Landing Gear Aft
Trunnion Fitting Discard
14,300
Landings
N/A
730
-5001 thru
-6068
6622124-5 Left Main Landing Gear Aft
Trunnion Fitting Discard
14,300
Landings
N/A
730
-6069 and
On
6622124-2 Right Main Landing Gear
Aft Trunnion Fitting Discard
14,300
Landings
N/A
720
-5001 thru
-6068
6622124-6 Right Main Landing Gear
Aft Trunnion Fitting Discard
14,300
Landings
N/A
720
-6069 and
On
6621125-1 Left Main Landing Gear
Actuator Fitting Discard
14,300
Landings
N/A
730
-5001 thru
-5022
6621125-5 Left Main Landing Gear
Actuator Fitting Discard
14,300
Landings
N/A
730
-5023 thru
-6068
6621125-9 Left Main Landing Gear
Actuator Fitting Discard
14,300
Landings
N/A
730
-6069 and
On
6621125-2 Right Main Landing Gear
Actuator Fitting Discard
14,300
Landings
N/A
720
-5001 thru
-5022
6621125-6 Right Main Landing Gear
Actuator Fitting Discard
14,300
Landings
N/A
720
-5023 thru
-6068
6621125-10 Right Main Landing Gear
Actuator Fitting Discard
14,300
Landings
N/A
720
-6069 and
On
S3049-5F8 Inboard and Outboard
Flap Rollers Discard
5000
Landings
N/A
500, 600
-5001 and
On
Task Title
4-10-02
© TEXTRON AVIATION INC.
Page 18
Sep 27/2018
CESSNA®
MODEL 560XL
MAINTENANCE MANUAL
REPLACEMENT TIME LIMITS
1.
General
A.
The contents of Chapter 4-11-00 REPLACEMENT TIME LIMITS have been moved to Chapter 4-1001. Refer to Table 3, CMR and ALI Component Time Limit Tasks.
4-11-00
© TEXTRON AVIATION INC.
Page 1
Sep 27/2018
CESSNA®
MODEL 560XL
MAINTENANCE MANUAL
RUSSIAN-CERTIFIED AIRPLANES REPLACEMENT TIME LIMITS
1.
General
A.
The contents of Chapter 4-11-02 RUSSIAN-CERTIFIED REPLACEMENT TIME LIMITS have been
moved to Chapter 4-10-02. Refer to Table 3, Russian CMR and ALI Component Time Limit Tasks.
4-11-02
© TEXTRON AVIATION INC.
Page 1
Sep 27/2018
CESSNA®
MODEL 560XL
MAINTENANCE MANUAL
AIRWORTHINESS LIMITATIONS INSPECTION DOCUMENTS
1.
Purpose and Use
A.
This section provides an overview of all Model 560XL airworthiness inspection intervals and
associated Airworthiness Limitations Inspection Documents.
NOTE:
B.
Airworthiness Limitations Inspection Documents are provided to group various tasks with the same
interval, and facilitate completing the tasks at a specified downtime. Airworthiness Limitations
Inspection Documents are numbered as shown below in sequential order, with Inspection Document
4-12-MA the first Airworthiness Limitations Inspection Documents due.
Chapter
Section
Airworthiness Limitations
Inspection Document MA
4-
12
-MA
NOTE:
C.
Airworthiness Limitations Inspection Documents and other required tasks listed in
Chapter 5-12-00, MSG-3 Inspection Documents and Other Required Tasks, Table 1, and
Table 2. provide the basis to set up a maintenance tracking and reporting system for the
Standard Manufacturer’s Recommended Continuous Airworthiness Inspection Program.
The "M" designation preceding the document letter indicates that these are mandatory
inspections, which are required as a condition of certification.
The following Table 1 Airworthiness Limitations Inspection Documents provide links to all Model 560XL
Airworthiness Limitations Inspection Documents and tasks associated to the Standard Manufacturer’s
Recommended Continuous Airworthiness Inspection Program and Custom Continuous Airworthiness
Inspection Program.
NOTE:
All initial intervals are repeat intervals unless otherwise noted.
Table 1. Airworthiness Limitations Inspection Documents
Airworthiness Limitations Inspection Document Intervals
Airworthiness Limitations
Inspection Document
3000 Flight Hours, Then Every 1500 Flight Hours Thereafter
4-12-MB
6000 Flight Hours or 120 Months, Whichever Occurs First, Then Every
2400 Hours or 120 Months, Whichever Occurs First Thereafter
4-12-MD
15,000 Flight Hours
4-12-ME
7500 Flight Hours, Then Every 1400 Flight Hours Thereafter
4-12-MF
6500 Flight Hours, Then Every 3000 Flight Hours Thereafter
4-12-MG
11,000 Flight Hours, Then Every 6000 Flight Hours Thereafter
4-12-MH
5000 Flight Hours, Then Every 2500 Flight Hours Thereafter
4-12-MI
13,000 Flight Hours
4-12-MJ
11,500 Flight Hours, Then Every 9000 Flight Hours Thereafter
4-12-MK
11,500 Flight Hours, Then Every 3300 Flight Hours Thereafter
4-12-ML
11,000 Flight Hours, Then Every 4200 Flight Hours Thereafter
4-12-MM
9000 Flight Hours, Then Every 3400 Flight Hours Thereafter
4-12-MN
4-12-00
© TEXTRON AVIATION INC.
Page 1
Sep 27/2018
CESSNA®
MODEL 560XL
MAINTENANCE MANUAL
Table 1. Airworthiness Limitations Inspection Documents (continued)
Airworthiness Limitations Inspection Document Intervals
Airworthiness Limitations
Inspection Document
12,500 Flight Hours, Then Every 6100 Flight Hours Thereafter
4-12-MO
300 Flight Hours
4-12-MP
10,000 Flight Hours, Then Every 5000 Flight Hours Thereafter
4-12-MR
D.
In addition to Table 1 Airworthiness Limitations Inspection Documents above, operators are
responsible for ensuring all other maintenance tasks listed in Chapter 5-10-00, Maintenance Planning
Document, Standard Manufacturer’s Recommended Continuous Airworthiness Inspection Program
or Custom Continuous Airworthiness Inspection Program, are completed.
4-12-00
© TEXTRON AVIATION INC.
Page 2
Sep 27/2018
CESSNA®
MODEL 560XL
MAINTENANCE MANUAL
AIRWORTHINESS LIMITATIONS INSPECTION DOCUMENT MB
1.
2.
3.
_______________
Airplane Serial Number
_______________
Airplane Registration Number
_______________
Airplane Total Time
_______________
Airplane Total Landings
_______________
Description
A.
Inspection Document 4-12-MB gives a list of Airworthiness Limitations Inspection Tasks to be
completed at 3000 flight hours, then every 1500 flight hours thereafter.
B.
The intervals specified represent the maximum time allowable between inspections.
C.
A task number and hyperlink provides detailed information about each inspection in individual chapters
of this manual.
D.
The right portion of each page provides space for the mechanic's and inspector's initials and remarks.
You can use copies of these pages as a checklist while you complete the tasks.
General Inspection Criteria
A.
As you complete each inspection task, examine the adjacent area while access is available to find
conditions that need more maintenance.
B.
If it is necessary to replace/adjust a component or system during a task, complete any required return
to service procedures for that system before the remaining steps of the task are completed.
C.
Refer to Chapter 5-10-01, MSG-3 Inspection Time Limits for Zone definitions (ENG, AUX, etc.).
Task Findings
A.
Enter the Task Findings into CESCOM/CAMP Systems at http://www.campsystems.com/ or if a
different maintenance tracking system is used, provide them to Cessna, Maintenance Engineering,
Department 753, 2121 South Hoover Road, Wichita, Kansas 67209, Phone: 316-517-9370 , Email:
maintenanceengineering@txtav.com.
NOTE:
4.
Date Completed
An Inspection Document or Inspection Task should only be recorded as completed in
the aircraft log after the findings have been entered into CESCOM/CAMP or sent to
Cessna Maintenance Engineering.
INSPECTION DOCUMENT MB Tasks
A.
Task 54-50-10-2100: Aft Engine Beam General Visual Inspection (Airplanes -5001 thru -5060)
Zone
Task Findings for Task 54-50-10-2100 (Check All That Apply)
Mech
Insp
Aft Engine Beam Task Findings
311,
312,
411,
412
[__]
No Fault Found
[__]
Loose
[__]
Cracks
[__]
Discoloration
[__]
Corrosion
[__]
Delamination
[__]
Debris
[__]
Other
Notes:
4-12-MB
© TEXTRON AVIATION INC.
Page 1
Sep 27/2018
CESSNA®
MODEL 560XL
MAINTENANCE MANUAL
AIRWORTHINESS LIMITATIONS INSPECTION DOCUMENT MD
1.
2.
3.
_______________
Airplane Serial Number
_______________
Airplane Registration Number
_______________
Airplane Total Time
_______________
Airplane Total Landings
_______________
Description
A.
Inspection Document 4-12-MD gives a list of Airworthiness Limitations Inspection Tasks to be
completed at 6000 flight hours or 120 months, whichever occurs first, then every 2400 hours or 120
months, whichever occurs first thereafter.
B.
The intervals specified represent the maximum time allowable between inspections.
C.
A task number and hyperlink provides detailed information about each inspection in individual chapters
of this manual.
D.
The right portion of each page provides space for the mechanic's and inspector's initials and remarks.
You can use copies of these pages as a checklist while you complete the tasks.
General Inspection Criteria
A.
As you complete each inspection task, examine the adjacent area while access is available to find
conditions that need more maintenance.
B.
If it is necessary to replace/adjust a component or system during a task, complete any required return
to service procedures for that system before the remaining steps of the task are completed.
C.
Refer to Chapter 5-10-01, MSG-3 Inspection Time Limits for Zone definitions (ENG, AUX, etc.).
Task Findings
A.
Enter the Task Findings into CESCOM/CAMP Systems at http://www.campsystems.com/ or if a
different maintenance tracking system is used, provide them to Cessna, Maintenance Engineering,
Department 753, 2121 South Hoover Road, Wichita, Kansas 67209, Phone: 316-517-9370 , Email:
maintenanceengineering@txtav.com.
NOTE:
4.
Date Completed
An Inspection Document or Inspection Task should only be recorded as completed in
the aircraft log after the findings have been entered into CESCOM/CAMP or sent to
Cessna Maintenance Engineering.
INSPECTION DOCUMENT MD Tasks
A.
Task 53-10-11-2501: Forward Pressure Bulkhead (Eddy Current) Special Detailed Inspection
Zone
Task Findings for Task 53-10-11-2501 (Check All That Apply)
141,
142,
241,
242
Forward Pressure Bulkhead Task Findings
[__]
No Fault Found
[__]
Other
[__]
Corrosion
[__]
Mech
Insp
Cracks
Notes:
4-12-MD
© TEXTRON AVIATION INC.
Page 1
Sep 27/2018
CESSNA®
MODEL 560XL
MAINTENANCE MANUAL
AIRWORTHINESS LIMITATIONS INSPECTION DOCUMENT ME
1.
2.
3.
_______________
Airplane Serial Number
_______________
Airplane Registration Number
_______________
Airplane Total Time
_______________
Airplane Total Landings
_______________
Description
A.
Inspection Document 4-12-ME gives a list of Airworthiness Limitations Inspection Tasks to be
completed every 15,000 flight hours.
B.
The intervals specified represent the maximum time allowable between inspections.
C.
A task number and hyperlink provides detailed information about each inspection in individual chapters
of this manual.
D.
The right portion of each page provides space for the mechanic's and inspector's initials and remarks.
You can use copies of these pages as a checklist while you complete the tasks.
General Inspection Criteria
A.
As you complete each inspection task, examine the adjacent area while access is available to find
conditions that need more maintenance.
B.
If it is necessary to replace/adjust a component or system during a task, complete any required return
to service procedures for that system before the remaining steps of the task are completed.
C.
Refer to Chapter 5-10-01, MSG-3 Inspection Time Limits for Zone definitions (ENG, AUX, etc.).
Task Findings
A.
Enter the Task Findings into CESCOM/CAMP Systems at http://www.campsystems.com/ or if a
different maintenance tracking system is used, provide them to Cessna, Maintenance Engineering,
Department 753, 2121 South Hoover Road, Wichita, Kansas 67209, Phone: 316-517-9370 , Email:
maintenanceengineering@txtav.com.
NOTE:
4.
Date Completed
An Inspection Document or Inspection Task should only be recorded as completed in
the aircraft log after the findings have been entered into CESCOM/CAMP or sent to
Cessna Maintenance Engineering.
INSPECTION DOCUMENT ME Tasks
A.
Task 52-10-00-2200: Cabin Door Assembly Detailed Inspection
Zone
Task Findings for Task 52-10-00-2200 (Check All That Apply)
Mech
Insp
Cabin Door Assembly Task Findings
810,
811
[__]
No Fault Found
[__]
Improper
Installation
[__]
Binding
[__]
Cracks
[__]
Corrosion
[__]
Chafing
[__]
Wear
[__]
Damaged Seal
[__]
Other
Notes:
B.
Task 52-20-00-2200: Emergency Exit Door Assembly Detailed Inspection
4-12-ME
© TEXTRON AVIATION INC.
Page 1
Sep 27/2018
CESSNA®
MODEL 560XL
MAINTENANCE MANUAL
Zone
Task Findings for Task 52-20-00-2200 (Check All That Apply)
Mech
Insp
Mech
Insp
Emergency Exit Door Assembly Task Findings
820,
821
[__]
No Fault Found
[__]
Improper
Installation
[__]
Binding
[__]
Cracks
[__]
Damaged Seal
[__]
Corrosion
[__]
Other
Notes:
C.
Task 53-10-11-2502: Aft Pressure Bulkhead General Visual Inspection
Zone
Task Findings for Task 53-10-11-2502 (Check All That Apply)
171,
172,
261,
262
Aft Pressure Bulkhead Task Findings
[__]
No Fault Found
[__]
Corrosion
[__]
Cracks
[__]
Failed Fasteners
[__]
Debris
[__]
Other
Notes:
D.
Task 53-30-01-2101: Lower Fuselage Skin from Right Stringer 13 to Left Stringer 13 General Visual
Inspection
Zone
Task Findings for Task 53-30-01-2101 (Check All That Apply)
143,
151,
161,
171,
213,
223,
321
Left Lower Skin Task Findings
[__]
No Fault Found
[__]
Corrosion
[__]
Cracks
[__]
Loose/Missing
Fasteners
[__]
Damage
[__]
Other
Mech
Insp
Notes:
144,
152,
162,
172,
214,
224,
322
Right Lower Skin Task Findings
[__]
No Fault Found
[__]
Corrosion
[__]
Cracks
[__]
Loose/Missing
Fasteners
[__]
Damage
[__]
Other
Notes:
E.
Task 53-30-01-2501: Upper Fuselage Skin Splice at BL 0.00 (Eddy Current) Special Detailed
Inspection
Zone
Task Findings for Task 53-30-01-2501 (Check All That Apply)
241,
242,
251,
252,
261,
262
Upper Fuselage Skin Splice at BL 0.0 Task Findings
[__]
No Fault Found
[__]
Other
[__]
Cracks
[__]
Mech
Insp
Corrosion
Notes:
4-12-ME
© TEXTRON AVIATION INC.
Page 2
Sep 27/2018
CESSNA®
MODEL 560XL
MAINTENANCE MANUAL
F.
Task 53-30-01-2502: Lower Fuselage Skin Splices at Stringers 13R and 13L (Eddy Current) Special
Detailed Inspection
Zone
151,
161,
171
Task Findings for Task 53-30-01-2502 (Check All That Apply)
Mech
Insp
Left Lower Fuselage Skin Splices at Stringer 13 Task Findings
[__]
No Fault Found
[__]
Other
[__]
Cracks
[__]
Corrosion
Notes:
152,
162,
172
Right Lower Fuselage Skin Splices at Stringer 13 Task Findings
[__]
No Fault Found
[__]
Other
[__]
Cracks
[__]
Corrosion
Notes:
4-12-ME
© TEXTRON AVIATION INC.
Page 3
Sep 27/2018
CESSNA®
MODEL 560XL
MAINTENANCE MANUAL
AIRWORTHINESS LIMITATIONS INSPECTION DOCUMENT MF
1.
2.
3.
_______________
Airplane Serial Number
_______________
Airplane Registration Number
_______________
Airplane Total Time
_______________
Airplane Total Landings
_______________
Description
A.
Inspection Document 4-12-MF gives a list of Airworthiness Limitations Inspection Tasks to be
completed at 7500 flight hours, then every 1400 flight hours thereafter.
B.
The intervals specified represent the maximum time allowable between inspections.
C.
A task number and hyperlink provides detailed information about each inspection in individual chapters
of this manual.
D.
The right portion of each page provides space for the mechanic's and inspector's initials and remarks.
You can use copies of these pages as a checklist while you complete the tasks.
General Inspection Criteria
A.
As you complete each inspection task, examine the adjacent area while access is available to find
conditions that need more maintenance.
B.
If it is necessary to replace/adjust a component or system during a task, complete any required return
to service procedures for that system before the remaining steps of the task are completed.
C.
Refer to Chapter 5-10-01, MSG-3 Inspection Time Limits for Zone definitions (ENG, AUX, etc.).
Task Findings
A.
Enter the Task Findings into CESCOM/CAMP Systems at http://www.campsystems.com/ or if a
different maintenance tracking system is used, provide them to Cessna, Maintenance Engineering,
Department 753, 2121 South Hoover Road, Wichita, Kansas 67209, Phone: 316-517-9370 , Email:
maintenanceengineering@txtav.com.
NOTE:
4.
Date Completed
An Inspection Document or Inspection Task should only be recorded as completed in
the aircraft log after the findings have been entered into CESCOM/CAMP or sent to
Cessna Maintenance Engineering.
INSPECTION DOCUMENT MF Tasks
A.
Task 57-10-00-2500: Lower Wing Main Spar Lower Skin Splice at WS 22.50 (Eddy Current and
Ultrasonic) Special Detailed Inspection
Zone
Task Findings for Task 57-10-00-2500 (Check All That Apply)
Mech
Insp
Left Lower Wing Main Spar Lower Skin Splice at WS 22.50 Task Findings
515
[__]
No Fault Found
[__]
Other
[__]
Cracks
[__]
Corrosion
Notes:
4-12-MF
© TEXTRON AVIATION INC.
Page 1
Sep 27/2018
CESSNA®
MODEL 560XL
MAINTENANCE MANUAL
Zone
Task Findings for Task 57-10-00-2500 (Check All That Apply)
Mech
Insp
Right Lower Wing Main Spar Lower Skin Splice at WS 22.50 Task Findings
516
[__]
No Fault Found
[__]
Other
[__]
Cracks
[__]
Corrosion
Notes:
4-12-MF
© TEXTRON AVIATION INC.
Page 2
Sep 27/2018
CESSNA®
MODEL 560XL
MAINTENANCE MANUAL
AIRWORTHINESS LIMITATIONS INSPECTION DOCUMENT MG
1.
2.
3.
_______________
Airplane Serial Number
_______________
Airplane Registration Number
_______________
Airplane Total Time
_______________
Airplane Total Landings
_______________
Description
A.
Inspection Document 4-12-MG gives a list of Airworthiness Limitations Inspection Tasks to be
completed at 6500 flight hours, then every 3000 flight hours thereafter.
B.
The intervals specified represent the maximum time allowable between inspections.
C.
A task number and hyperlink provides detailed information about each inspection in individual chapters
of this manual.
D.
The right portion of each page provides space for the mechanic's and inspector's initials and remarks.
You can use copies of these pages as a checklist while you complete the tasks.
General Inspection Criteria
A.
As you complete each inspection task, examine the adjacent area while access is available to find
conditions that need more maintenance.
B.
If it is necessary to replace/adjust a component or system during a task, complete any required return
to service procedures for that system before the remaining steps of the task are completed.
C.
Refer to Chapter 5-10-01, MSG-3 Inspection Time Limits for Zone definitions (ENG, AUX, etc.).
Task Findings
A.
Enter the Task Findings into CESCOM/CAMP Systems at http://www.campsystems.com/ or if a
different maintenance tracking system is used, provide them to Cessna, Maintenance Engineering,
Department 753, 2121 South Hoover Road, Wichita, Kansas 67209, Phone: 316-517-9370 , Email:
maintenanceengineering@txtav.com.
NOTE:
4.
Date Completed
An Inspection Document or Inspection Task should only be recorded as completed in
the aircraft log after the findings have been entered into CESCOM/CAMP or sent to
Cessna Maintenance Engineering.
INSPECTION DOCUMENT MG Tasks
A.
Task 55-30-00-2500: Vertical Stabilizer Rear Spar Cap at WL 146 (Eddy Current) Special Detailed
Inspection (Airplanes -5001 thru -5020)
Zone
Task Findings for Task 55-30-00-2500 (Check All That Apply)
321,
322,
340
Vertical Stabilizer Rear Spar Cap at WL 146 Task Findings
[__]
No Fault Found
[__]
Cracks
[__]
Mech
Insp
Other
Notes:
4-12-MG
© TEXTRON AVIATION INC.
Page 1
Sep 27/2018
CESSNA®
MODEL 560XL
MAINTENANCE MANUAL
AIRWORTHINESS LIMITATIONS INSPECTION DOCUMENT MH
1.
2.
3.
_______________
Airplane Serial Number
_______________
Airplane Registration Number
_______________
Airplane Total Time
_______________
Airplane Total Landings
_______________
Description
A.
Inspection Document 4-12-MH gives a list of Airworthiness Limitations Inspection Tasks to be
completed at 11,000 flight hours, then every 6000 flight hours thereafter.
B.
The intervals specified represent the maximum time allowable between inspections.
C.
A task number and hyperlink provides detailed information about each inspection in individual chapters
of this manual.
D.
The right portion of each page provides space for the mechanic's and inspector's initials and remarks.
You can use copies of these pages as a checklist while you complete the tasks.
General Inspection Criteria
A.
As you complete each inspection task, examine the adjacent area while access is available to find
conditions that need more maintenance.
B.
If it is necessary to replace/adjust a component or system during a task, complete any required return
to service procedures for that system before the remaining steps of the task are completed.
C.
Refer to Chapter 5-10-01, MSG-3 Inspection Time Limits for Zone definitions (ENG, AUX, etc.).
Task Findings
A.
Enter the Task Findings into CESCOM/CAMP Systems at http://www.campsystems.com/ or if a
different maintenance tracking system is used, provide them to Cessna, Maintenance Engineering,
Department 753, 2121 South Hoover Road, Wichita, Kansas 67209, Phone: 316-517-9370 , Email:
maintenanceengineering@txtav.com.
NOTE:
4.
Date Completed
An Inspection Document or Inspection Task should only be recorded as completed in
the aircraft log after the findings have been entered into CESCOM/CAMP or sent to
Cessna Maintenance Engineering.
INSPECTION DOCUMENT MH Tasks
A.
Task 55-30-00-2501: Vertical Stabilizer Rear Spar Nested Angle at WL 146 (Eddy Current) Special
Detailed Inspection (Airplanes -5001 thru -5020)
Zone
Task Findings for Task 55-30-00-2501 (Check All That Apply)
321,
322,
340
Vertical Stabilizer Rear Spar Nested Angle at WL 146.00 Task Findings
[__]
No Fault Found
[__]
Cracks
[__]
Mech
Insp
Other
Notes:
4-12-MH
© TEXTRON AVIATION INC.
Page 1
Sep 27/2018
CESSNA®
MODEL 560XL
MAINTENANCE MANUAL
AIRWORTHINESS LIMITATIONS INSPECTION DOCUMENT MI
1.
2.
3.
_______________
Airplane Serial Number
_______________
Airplane Registration Number
_______________
Airplane Total Time
_______________
Airplane Total Landings
_______________
Description
A.
Inspection Document 4-12-MI gives a list of Airworthiness Limitations Inspection Tasks to be
completed at 5000 flight hours, then every 2500 flight hours thereafter.
B.
The intervals specified represent the maximum time allowable between inspections.
C.
A task number and hyperlink provides detailed information about each inspection in individual chapters
of this manual.
D.
The right portion of each page provides space for the mechanic's and inspector's initials and remarks.
You can use copies of these pages as a checklist while you complete the tasks.
General Inspection Criteria
A.
As you complete each inspection task, examine the adjacent area while access is available to find
conditions that need more maintenance.
B.
If it is necessary to replace/adjust a component or system during a task, complete any required return
to service procedures for that system before the remaining steps of the task are completed.
C.
Refer to Chapter 5-10-01, MSG-3 Inspection Time Limits for Zone definitions (ENG, AUX, etc.).
Task Findings
A.
Enter the Task Findings into CESCOM/CAMP Systems at http://www.campsystems.com/ or if a
different maintenance tracking system is used, provide them to Cessna, Maintenance Engineering,
Department 753, 2121 South Hoover Road, Wichita, Kansas 67209, Phone: 316-517-9370 , Email:
maintenanceengineering@txtav.com.
NOTE:
4.
Date Completed
An Inspection Document or Inspection Task should only be recorded as completed in
the aircraft log after the findings have been entered into CESCOM/CAMP or sent to
Cessna Maintenance Engineering.
INSPECTION DOCUMENT MI Tasks
A.
Task 55-30-00-2502: Vertical Stabilizer Rear Spar Strap at WL 146.00 (Eddy Current) Special Detailed
Inspection (Airplanes -5001 thru -5020)
Zone
Task Findings for Task 55-30-00-2502 (Check All That Apply)
321,
322,
340
Vertical Stabilizer Rear Spar Strap at WL 146 Findings
[__]
No Fault Found
[__]
Cracks
[__]
Mech
Insp
Other
Notes:
4-12-MI
© TEXTRON AVIATION INC.
Page 1
Sep 27/2018
CESSNA®
MODEL 560XL
MAINTENANCE MANUAL
AIRWORTHINESS LIMITATIONS INSPECTION DOCUMENT MJ
1.
2.
3.
_______________
Airplane Serial Number
_______________
Airplane Registration Number
_______________
Airplane Total Time
_______________
Airplane Total Landings
_______________
Description
A.
Inspection Document 4-12-MJ gives a list of Airworthiness Limitations Inspection Tasks to be
completed every 13,000 flight hours.
B.
The intervals specified represent the maximum time allowable between inspections.
C.
A task number and hyperlink provides detailed information about each inspection in individual chapters
of this manual.
D.
The right portion of each page provides space for the mechanic's and inspector's initials and remarks.
You can use copies of these pages as a checklist while you complete the tasks.
General Inspection Criteria
A.
As you complete each inspection task, examine the adjacent area while access is available to find
conditions that need more maintenance.
B.
If it is necessary to replace/adjust a component or system during a task, complete any required return
to service procedures for that system before the remaining steps of the task are completed.
C.
Refer to Chapter 5-10-01, MSG-3 Inspection Time Limits for Zone definitions (ENG, AUX, etc.).
Task Findings
A.
Enter the Task Findings into CESCOM/CAMP Systems at http://www.campsystems.com/ or if a
different maintenance tracking system is used, provide them to Cessna, Maintenance Engineering,
Department 753, 2121 South Hoover Road, Wichita, Kansas 67209, Phone: 316-517-9370 , Email:
maintenanceengineering@txtav.com.
NOTE:
4.
Date Completed
An Inspection Document or Inspection Task should only be recorded as completed in
the aircraft log after the findings have been entered into CESCOM/CAMP or sent to
Cessna Maintenance Engineering.
INSPECTION DOCUMENT MJ Tasks
A.
Task 53-30-01-2100: Upper Fuselage Skin from Right Stringer 13 to Left Stringer 13 General Visual
Inspection
Zone
Task Findings for Task 53-30-01-2100 (Check All That Apply)
213,
243,
253,
263,
323
Left Upper Skin from Right Stringer 13 to Left Stringer 13 Task Findings
[__]
No Fault Found
[__]
Corrosion
[__]
Cracks
[__]
Loose/Missing
Fasteners
[__]
Damage
[__]
Other
Mech
Insp
Notes:
4-12-MJ
© TEXTRON AVIATION INC.
Page 1
Sep 27/2018
CESSNA®
MODEL 560XL
MAINTENANCE MANUAL
Zone
Task Findings for Task 53-30-01-2100 (Check All That Apply)
214,
244,
254,
264,
324
Right Upper Skin from Right Stringer 13 to Left Stringer 13 Task Findings
[__]
No Fault Found
[__]
Corrosion
[__]
Cracks
[__]
Loose/Missing
Fasteners
[__]
Damage
[__]
Other
Mech
Insp
Notes:
B.
Task 54-50-10-2500: Forward Engine Beam Upper Angles, Horizontal Cap Flange at BL 30.5 thru BL
42.0 (Eddy Current) Special Detailed Inspection (Airplanes -5001 thru -5060)
Zone
Task Findings for Task 54-50-10-2500 (Check All That Apply)
Mech
Insp
Left Forward Engine Beam Task Findings
311,
411
[__]
No Fault Found
[__]
Other
[__]
Cracks
[__]
Corrosion
Right Forward Engine Beam Task Findings
312,
412
[__]
No Fault Found
[__]
Other
[__]
Cracks
[__]
Corrosion
Notes:
4-12-MJ
© TEXTRON AVIATION INC.
Page 2
Sep 27/2018
CESSNA®
MODEL 560XL
MAINTENANCE MANUAL
AIRWORTHINESS LIMITATIONS INSPECTION DOCUMENT MK
1.
2.
3.
_______________
Airplane Serial Number
_______________
Airplane Registration Number
_______________
Airplane Total Time
_______________
Airplane Total Landings
_______________
Description
A.
Inspection Document 4-12-MK gives a list of Airworthiness Limitations Inspection Tasks to be
completed at 11,500 flight hours, then every 9000 flight hours thereafter.
B.
The intervals specified represent the maximum time allowable between inspections.
C.
A task number and hyperlink provides detailed information about each inspection in individual chapters
of this manual.
D.
The right portion of each page provides space for the mechanic's and inspector's initials and remarks.
You can use copies of these pages as a checklist while you complete the tasks.
General Inspection Criteria
A.
As you complete each inspection task, examine the adjacent area while access is available to find
conditions that need more maintenance.
B.
If it is necessary to replace/adjust a component or system during a task, complete any required return
to service procedures for that system before the remaining steps of the task are completed.
C.
Refer to Chapter 5-10-01, MSG-3 Inspection Time Limits for Zone definitions (ENG, AUX, etc.).
Task Findings
A.
Enter the Task Findings into CESCOM/CAMP Systems at http://www.campsystems.com/ or if a
different maintenance tracking system is used, provide them to Cessna, Maintenance Engineering,
Department 753, 2121 South Hoover Road, Wichita, Kansas 67209, Phone: 316-517-9370 , Email:
maintenanceengineering@txtav.com.
NOTE:
4.
Date Completed
An Inspection Document or Inspection Task should only be recorded as completed in
the aircraft log after the findings have been entered into CESCOM/CAMP or sent to
Cessna Maintenance Engineering.
INSPECTION DOCUMENT MK Tasks
A.
Task 55-30-00-2503: Vertical Stabilizer Forward Spar Strap at WL 150 (Eddy Current) Special Detailed
Inspection (Airplanes -5001 thru -5020)
Zone
Task Findings for Task 55-30-00-2503 (Check All That Apply)
321,
322,
340
Vertical Stabilizer Forward Spar Strap at WL 150 Task Findings
[__]
No Fault Found
[__]
Cracks
[__]
Mech
Insp
Other
Notes:
4-12-MK
© TEXTRON AVIATION INC.
Page 1
Sep 27/2018
CESSNA®
MODEL 560XL
MAINTENANCE MANUAL
AIRWORTHINESS LIMITATIONS INSPECTION DOCUMENT ML
1.
2.
3.
_______________
Airplane Serial Number
_______________
Airplane Registration Number
_______________
Airplane Total Time
_______________
Airplane Total Landings
_______________
Description
A.
Inspection Document 4-12-ML gives a list of Airworthiness Limitations Inspection Tasks to be
completed at 11,500 flight hours, then every 3300 flight hours thereafter.
B.
The intervals specified represent the maximum time allowable between inspections.
C.
A task number and hyperlink provides detailed information about each inspection in individual chapters
of this manual.
D.
The right portion of each page provides space for the mechanic's and inspector's initials and remarks.
You can use copies of these pages as a checklist while you complete the tasks.
General Inspection Criteria
A.
As you complete each inspection task, examine the adjacent area while access is available to find
conditions that need more maintenance.
B.
If it is necessary to replace/adjust a component or system during a task, complete any required return
to service procedures for that system before the remaining steps of the task are completed.
C.
Refer to Chapter 5-10-01, MSG-3 Inspection Time Limits for Zone definitions (ENG, AUX, etc.).
Task Findings
A.
Enter the Task Findings into CESCOM/CAMP Systems at http://www.campsystems.com/ or if a
different maintenance tracking system is used, provide them to Cessna, Maintenance Engineering,
Department 753, 2121 South Hoover Road, Wichita, Kansas 67209, Phone: 316-517-9370 , Email:
maintenanceengineering@txtav.com.
NOTE:
4.
Date Completed
An Inspection Document or Inspection Task should only be recorded as completed in
the aircraft log after the findings have been entered into CESCOM/CAMP or sent to
Cessna Maintenance Engineering.
INSPECTION DOCUMENT ML Tasks
A.
Task 57-10-00-2501: Lower Wing Main Spar Skin Splice Flange at WS 11.50 (Eddy Current and
Ultrasonic) Special Detailed Inspection
Zone
Task Findings for Task 57-10-00-2501 (Check All That Apply)
Mech
Insp
Left Lower Wing Main Spar Skin Splice Flange at WS 11.50 Task Findings
515
[__]
No Fault Found
[__]
Other
[__]
Cracks
[__]
Corrosion
Notes:
4-12-ML
© TEXTRON AVIATION INC.
Page 1
Sep 27/2018
CESSNA®
MODEL 560XL
MAINTENANCE MANUAL
Zone
Task Findings for Task 57-10-00-2501 (Check All That Apply)
Mech
Insp
Right Lower Wing Main Spar Skin Splice Flange at WS
11.50 Task Findings
615
[__]
No Fault Found
[__]
Other
[__]
Cracks
[__]
Corrosion
Notes:
4-12-ML
© TEXTRON AVIATION INC.
Page 2
Sep 27/2018
CESSNA®
MODEL 560XL
MAINTENANCE MANUAL
AIRWORTHINESS LIMITATIONS INSPECTION DOCUMENT MM
1.
2.
3.
_______________
Airplane Serial Number
_______________
Airplane Registration Number
_______________
Airplane Total Time
_______________
Airplane Total Landings
_______________
Description
A.
Inspection Document 4-12-MM gives a list of Airworthiness Limitations Inspection Tasks to be
completed at 11,000 flight hours, then every 4200 flight hours thereafter.
B.
The intervals specified represent the maximum time allowable between inspections.
C.
A task number and hyperlink provides detailed information about each inspection in individual chapters
of this manual.
D.
The right portion of each page provides space for the mechanic's and inspector's initials and remarks.
You can use copies of these pages as a checklist while you complete the tasks.
General Inspection Criteria
A.
As you complete each inspection task, examine the adjacent area while access is available to find
conditions that need more maintenance.
B.
If it is necessary to replace/adjust a component or system during a task, complete any required return
to service procedures for that system before the remaining steps of the task are completed.
C.
Refer to Chapter 5-10-01, MSG-3 Inspection Time Limits for Zone definitions (ENG, AUX, etc.).
Task Findings
A.
Enter the Task Findings into CESCOM/CAMP Systems at http://www.campsystems.com/ or if a
different maintenance tracking system is used, provide them to Cessna, Maintenance Engineering,
Department 753, 2121 South Hoover Road, Wichita, Kansas 67209, Phone: 316-517-9370 , Email:
maintenanceengineering@txtav.com.
NOTE:
4.
Date Completed
An Inspection Document or Inspection Task should only be recorded as completed in
the aircraft log after the findings have been entered into CESCOM/CAMP or sent to
Cessna Maintenance Engineering.
INSPECTION DOCUMENT MM Tasks
A.
Task 57-10-00-2502: Lower Wing Main Spar at WS 114.57 (Eddy Current) Special Detailed Inspection
Zone
Task Findings for Task 57-10-00-2502 (Check All That Apply)
Mech
Insp
Left Lower Wing Main Spar at WS 114.57 Task Findings
523,
524
[__]
No Fault Found
[__]
Other
[__]
Cracks
[__]
Corrosion
Notes:
Right Lower Wing Main Spar at WS 114.57 Task Findings
623,
624
[__]
No Fault Found
[__]
Other
[__]
Cracks
[__]
Corrosion
Notes:
4-12-MM
© TEXTRON AVIATION INC.
Page 1
Sep 27/2018
CESSNA®
MODEL 560XL
MAINTENANCE MANUAL
AIRWORTHINESS LIMITATIONS INSPECTION DOCUMENT MN
1.
2.
3.
_______________
Airplane Serial Number
_______________
Airplane Registration Number
_______________
Airplane Total Time
_______________
Airplane Total Landings
_______________
Description
A.
Inspection Document 4-12-MN gives a list of Airworthiness Limitations Inspection Tasks to be
completed at 9000 flight hours, then every 3400 flight hours thereafter.
B.
The intervals specified represent the maximum time allowable between inspections.
C.
A task number and hyperlink provides detailed information about each inspection in individual chapters
of this manual.
D.
The right portion of each page provides space for the mechanic's and inspector's initials and remarks.
You can use copies of these pages as a checklist while you complete the tasks.
General Inspection Criteria
A.
As you complete each inspection task, examine the adjacent area while access is available to find
conditions that need more maintenance.
B.
If it is necessary to replace/adjust a component or system during a task, complete any required return
to service procedures for that system before the remaining steps of the task are completed.
C.
Refer to Chapter 5-10-01, MSG-3 Inspection Time Limits for Zone definitions (ENG, AUX, etc.).
Task Findings
A.
Enter the Task Findings into CESCOM/CAMP Systems at http://www.campsystems.com/ or if a
different maintenance tracking system is used, provide them to Cessna, Maintenance Engineering,
Department 753, 2121 South Hoover Road, Wichita, Kansas 67209, Phone: 316-517-9370 , Email:
maintenanceengineering@txtav.com.
NOTE:
4.
Date Completed
An Inspection Document or Inspection Task should only be recorded as completed in
the aircraft log after the findings have been entered into CESCOM/CAMP or sent to
Cessna Maintenance Engineering.
INSPECTION DOCUMENT MN Tasks
A.
Task 57-10-00-2503: Lower Wing Main Spar at WS 131.07 (Eddy Current) Special Detailed Inspection
Zone
Task Findings for Task 57-10-00-2503 (Check All That Apply)
Mech
Insp
Left Lower Wing Main Spar at WS 131.07 Task Findings
523,
524
[__]
No Fault Found
[__]
Other
[__]
Cracks
[__]
Corrosion
Notes:
Right Lower Wing Main Spar at WS 131.07 Task Findings
623,
624
[__]
No Fault Found
[__]
Other
[__]
Cracks
[__]
Corrosion
Notes:
4-12-MN
© TEXTRON AVIATION INC.
Page 1
Sep 27/2018
CESSNA®
MODEL 560XL
MAINTENANCE MANUAL
AIRWORTHINESS LIMITATIONS INSPECTION DOCUMENT MO
1.
2.
3.
_______________
Airplane Serial Number
_______________
Airplane Registration Number
_______________
Airplane Total Time
_______________
Airplane Total Landings
_______________
Description
A.
Inspection Document 4-12-MO gives a list of Airworthiness Limitations Inspection Tasks to be
completed at 12,500 flight hours, then every 6100 flight hours thereafter.
B.
The intervals specified represent the maximum time allowable between inspections.
C.
A task number and hyperlink provides detailed information about each inspection in individual chapters
of this manual.
D.
The right portion of each page provides space for the mechanic's and inspector's initials and remarks.
You can use copies of these pages as a checklist while you complete the tasks.
General Inspection Criteria
A.
As you complete each inspection task, examine the adjacent area while access is available to find
conditions that need more maintenance.
B.
If it is necessary to replace/adjust a component or system during a task, complete any required return
to service procedures for that system before the remaining steps of the task are completed.
C.
Refer to Chapter 5-10-01, MSG-3 Inspection Time Limits for Zone definitions (ENG, AUX, etc.).
Task Findings
A.
Enter the Task Findings into CESCOM/CAMP Systems at http://www.campsystems.com/ or if a
different maintenance tracking system is used, provide them to Cessna, Maintenance Engineering,
Department 753, 2121 South Hoover Road, Wichita, Kansas 67209, Phone: 316-517-9370 , Email:
maintenanceengineering@txtav.com.
NOTE:
4.
Date Completed
An Inspection Document or Inspection Task should only be recorded as completed in
the aircraft log after the findings have been entered into CESCOM/CAMP or sent to
Cessna Maintenance Engineering.
INSPECTION DOCUMENT MO Tasks
A.
Task 57-10-00-2504: Lower Wing Main Spar at WS 149.57 (Eddy Current) Special Detailed Inspection
Zone
Task Findings for Task 57-10-00-2504 (Check All That Apply)
Mech
Insp
Left Lower Wing Main Spar at WS 149.57 Task Findings
523,
524
[__]
No Fault Found
[__]
Other
[__]
Cracks
[__]
Corrosion
Notes:
Right Lower Wing Main Spar at WS 149.57 Task Findings
623,
624
[__]
No Fault Found
[__]
Other
[__]
Cracks
[__]
Corrosion
Notes:
4-12-MO
© TEXTRON AVIATION INC.
Page 1
Sep 27/2018
CESSNA®
MODEL 560XL
MAINTENANCE MANUAL
AIRWORTHINESS LIMITATIONS INSPECTION DOCUMENT MP
1.
2.
3.
_______________
Airplane Serial Number
_______________
Airplane Registration Number
_______________
Airplane Total Time
_______________
Airplane Total Landings
_______________
Description
A.
Inspection Document 4-12-MP gives a list of Airworthiness Limitations Inspection Tasks to be
completed every 300 flight hours.
B.
The intervals specified represent the maximum time allowable between inspections.
C.
A task number and hyperlink provides detailed information about each inspection in individual chapters
of this manual.
D.
The right portion of each page provides space for the mechanic's and inspector's initials and remarks.
You can use copies of these pages as a checklist while you complete the tasks.
General Inspection Criteria
A.
As you complete each inspection task, examine the adjacent area while access is available to find
conditions that need more maintenance.
B.
If it is necessary to replace/adjust a component or system during a task, complete any required return
to service procedures for that system before the remaining steps of the task are completed.
C.
Refer to Chapter 5-10-01, MSG-3 Inspection Time Limits for Zone definitions (ENG, AUX, etc.).
Task Findings
A.
Enter the Task Findings into CESCOM/CAMP Systems at http://www.campsystems.com/ or if a
different maintenance tracking system is used, provide them to Cessna, Maintenance Engineering,
Department 753, 2121 South Hoover Road, Wichita, Kansas 67209, Phone: 316-517-9370 , Email:
maintenanceengineering@txtav.com.
NOTE:
4.
Date Completed
An Inspection Document or Inspection Task should only be recorded as completed in
the aircraft log after the findings have been entered into CESCOM/CAMP or sent to
Cessna Maintenance Engineering.
INSPECTION DOCUMENT MP Tasks
A.
Task 21-52-00-2100: Vapor Cycle Cooling System Hour Meter Visual Check (Airplanes -5001 thru
-5374 Incorporating Vapor Cycle Cooling System)
Zone
Task Findings for Task 21-52-00-2100 (Check All That Apply)
Mech
Insp
Vapor Cycle Cooling System Hour Meter Visual Check Findings
311
[__]
No Fault Found
[__]
300 Compressor
Hour
Maintenance
Due/Scheduled
[__]
Other
Notes:
4-12-MP
© TEXTRON AVIATION INC.
Page 1
Sep 27/2018
CESSNA®
MODEL 560XL
MAINTENANCE MANUAL
AIRWORTHINESS LIMITATIONS INSPECTION DOCUMENT MR
1.
2.
3.
_______________
Airplane Serial Number
_______________
Airplane Registration Number
_______________
Airplane Total Time
_______________
Airplane Total Landings
_______________
Description
A.
Inspection Document 4-12-MR gives a list of Airworthiness Limitations Inspection Tasks to be
completed at 10,000 flight hours, then every 5000 flight hours thereafter.
B.
The intervals specified represent the maximum time allowable between inspections.
C.
A task number and hyperlink provides detailed information about each inspection in individual chapters
of this manual.
D.
The right portion of each page provides space for the mechanic's and inspector's initials and remarks.
You can use copies of these pages as a checklist while you complete the tasks.
General Inspection Criteria
A.
As you complete each inspection task, examine the adjacent area while access is available to find
conditions that need more maintenance.
B.
If it is necessary to replace/adjust a component or system during a task, complete any required return
to service procedures for that system before the remaining steps of the task are completed.
C.
Refer to Chapter 5-10-01, MSG-3 Inspection Time Limits for Zone definitions (ENG, AUX, etc.).
Task Findings
A.
Enter the Task Findings into CESCOM/CAMP Systems at http://www.campsystems.com/ or if a
different maintenance tracking system is used, provide them to Cessna, Maintenance Engineering,
Department 753, 2121 South Hoover Road, Wichita, Kansas 67209, Phone: 316-517-9370 , Email:
maintenanceengineering@txtav.com.
NOTE:
4.
Date Completed
An Inspection Document or Inspection Task should only be recorded as completed in
the aircraft log after the findings have been entered into CESCOM/CAMP or sent to
Cessna Maintenance Engineering.
INSPECTION DOCUMENT MR Tasks
A.
Task 55-30-00-2504: Vertical Stabilizer Forward Spar Strap at WL 188.00 (Eddy Current) Special
Detailed Inspection (Airplanes -5001 thru -5020)
Zone
340
Task Findings for Task 55-30-00-2504 (Check All That Apply)
Mech
Insp
Vertical Stabilizer Forward Spar Strap at WL 188.00 Task Findings
[__]
No Fault Found
[__]
Cracks
[__]
Other
Notes:
4-12-MR
© TEXTRON AVIATION INC.
Page 1
Sep 27/2018