CESSNA AIRCRAFT COMPANY 

MODEL 550 BRAVO 

MAINTENANCE MANUAL 

CHAPTER 

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. 

APPROVED BY_.fl!'J~ ......... ~----------- ~Everett W. Pittman, Manager 

Aircraft Certification Office 

Federal Aviation Administration 

Wichita, Kansas 

DATE OF APPROVAL_.-1#.~-'4;.../t;""'-~----

4 DECEMBER 1996 

REVISION 12 23 JUNE 2014 
CESSNA AIRCRAFT COMPANY 

MODEL 550 BRAVO 

MAINTENANCE MANUAL 

4 - LIST OF EFFECTIVE PAGES 

CHAPTER-SECTION-SUBJECT 

4-Title 

4-List of Effective Pages 

4-Record of Temporary Revisions 

4-Contents 

PAGE DATE 

4-00-00 Page 1 Jun 25/2007 

4-10-00 

4-11 -00 

Page 1 Jun 23/2014 

Pages 1-2 Jun 23/2014 

\.-. 

APPROVED BY ____ ~~----~~---

r-uet Kline. lviHnan• 

1\irr.raft Cr'!rllfiC;lllun 0 1cr. 

F1!<leral 'J a~un/\d ll~lm tion 

DAT~~~ :;;~~ VA L ~ f '-'- ami_ 

© Cessna Aircraft Company 

4 -LIST OF EFFECTIVE PAGES Page 1 of 1 

Jun 23/2014 
CESSNA AIRCRAFT COMPANY 

MODEL 550 BRAVO 

MAINTENANCE MANUAL 

4- CONTENTS 

AIRWORTHINESS LIMITATIONS ..... . . ... . 0 • 0 • •••• • •• • • • •••••••• • • • •••••••••• • • • 

Scope . . .... . . . . ...... .. . . . . 0 ••• 0 ••••• • •• • • • • ••••• • • •• • ••• • •• • • •••••••••• • • • 

Definition . . . . . . . . .. . . ............. . . .. . .. . ... .. .. . . ........................ . 

INSPECTION TIME LIMITS .... . . . . ......... . . .. . . .. ........... . . ...... . . . . . . . . .. . 

General .... . . ..... 0 •••••••••• • • •••••• •••••••••••• • •••• • • • • • • •••• • • • • ••••••• 

Inspection Schedule ........ . ............................................... . 

REPLACEMENT TIME LIMITS ........... ... . . .. . .. . ........................ . .... . 

General . ... . . . . . . .. . .......... . . ..... . .. . . . .. ..... 0 ••••• • •• ••• • • • • • • • • • • • • • 

Replacement Schedule . ... . .. . . . . . . ... . .. . . . .. ......... . . ........ . ... . . . . .. . 

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© Cessna Aircraft Company 

4 - CONTENTS Page 1 of 1 

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I 

1. Scope 

CESSNA AIRCRAFT COMPANY 

MODEL 550 BRAVO 

MAINTENANCE MANUAL 

AIRWORTHINESS LIMITATIONS 

A. This chapter gives the mandatory replacement times and inspection intervals for components and 

airplane structures that are life-limited. This chapter also gives the details required to monitor them 

through scheduled inspections. This chapter applies to items such as fatigue components and 

structures, which are specified as a part of the certification procedures. 

NOTE: The Airworthiness Limitations section is FAA-approved and gives inspections and 

maintenance procedures that are required by Parts 43.16 and 91.409 of Title 14 of the 

Code of Federal Regulations, unless an alternative program has been FAA-approved. 

2. Definition 

A. This chapter contains the sections that follow: 

(1) Inspection Time Limits (4-10-00) gives the systems and components, that must be examined at 

specified intervals. These intervals show the maximum time permitted between inspections. 

(2) Replacement Time Limits (4-11-00) gives the life-limited components, that are to be replaced at 

a specified time. 

© Cessna Aircraft Company 

4-00-00 Page 1 

Jun 25/2007 
I 

CESSNA AIRCRAFT COMPANY 

MODEL 550 BRAVO 

MAINTENANCE MANUAL 

INSPECTION TIME LIMITS 

1. General 

2. 

A. The inspection time intervals that apply to the systems and components that follow represent the 

maximum inspection intervals which must be adhered to. 

NOTE: The inspection intervals for structural elements defined in this chapter are absolute limits 

which shall not be exceeded. These intervals are calculated based on criteria which will 

detect cracks before they grow to a critical size. By following the continuous inspection 

requirements outlined in Chapter 5, the inspection requirements presented in this chapter 

will be satisfied. In some cases, the corresponding inspection defined in Chapter 5 is at an 

interval which coincides with a phase inspection having a lesser time limit. Performing the 

inspection during the regularly scheduled phase(s) will, in most cases, be more economical 

than completing each item at its maximum inspection interval. 

NOTE: Repairs made to structures, for example, the addition of doublers, may invalidate an 

inspection and/or procedure. Modified inspections may be required for structures which 

have been repaired. 

Inspection Schedule 

A. Air Conditioning (Chapter 21) 

( 1) Vapor Cycle Cooling System Hourmeter Check (Compressor Motors 1134104-1, -5 or 

FWA 1134104-1, -5) - Examine every 300 hours. Refer to Task 21-51-03-212. 

NOTE: Refer to the Enviro Systems Inc. Operating, Servicing and Component Maintenance 

Manual 21 -00-24. 

B. Landing Gear (Chapter 32) 

(1) Nose landing gear fork (Part Number 5542300-2) -Inspect first 10,000 landings and every 1000 

landings thereafter. Task 32-21-01-250 

NOTE: This component also has replacement time limits. Refer to Replacement Time Limits 

for replacement criteria. 

C. Fuselage (Part Number 6510000-1) (Chapter 53) 

(1) Forward pressure bulkhead web-- Inspect every 4450 hours. Task 53-10-00-212 

(2) Forward pressure bulkhead attach angles- Inspect every 6725 hours. Task 53-10-03-250 

(3) Aft pressure bulkhead attach angles- Inspect every 6725 hours. Task 53-10-04-251 

(4) Aft pressure bulkhead web, aft side -- Inspect every 4450 hours. Task 53-10-04-211 

(5) Cabin door frame- Inspect every 5000 hours. Task 53-10-09-211 

(6) Emergency exit door frame -- Inspect every 1456 hours. Task 53-10-09-212 

(7) Windshield, cockpit side window and cabin window frames- Inspect every 5130 hours. Task 

53-1 0-09-213 

(8) Fuselage exterior skin - Inspect every 2523 hours. Task 53-30-00-210 

(9) Cabin lower skin longitudinal splice- Inspect every 5900 hours. Task 53-30-00-251 

© Cessna Aircraft Company 

4-10-00 Page 1 

Jun 23/2014 
I 

CESSNA AIRCRAFT COMPANY 

MODEL 550 BRAVO 

MAINTENANCE MANUAL 

REPLACEMENT TIME LIMITS 

1. General 

2. 

A. The life-limited components that follow must be replaced at the specified time. It is recommended that 

the components be scheduled for replacement during the airplane's inspection interval that aligns with, 

or occurs just before, the specified time limit is expired. Procedures to replace the components are 

given in the applicable chapters in this maintenance manual. 

Replacement Schedule 

A. Air Conditioning (Chapter 21) 

(1) Vapor Cycle Cooling System Compressor Drive Motor Brushes (Compressor Motors 1134104-1, 

-5 or FWA1134104-1 , -5) - Replace every 500 compressor hours. 

NOTE: Refer to the Enviro Systems Inc. Operating, Servicing and Component Maintenance 

Manual 21-00-24. 

B. Landing Gear (Chapter 32). 

(1) Main Landing Gear 

NOTE: Attached hardware, which includes the bolts, bearings, bushings, trunnion pins, 

and trunnion/link pins, related to the installation of the components below must be 

replaced when the related component is replaced. Refer to Chapter 32 for more 

information. 

(a) Left Trunnion (Part Number 6541460-1 , 6594022-1) - Replace every 41 ,600 landings 

(b) Right Trunnion (Part Number6541460-2, 6594022-2)- Replace every 41 ,600 landings 

(c) Left Trailing Link Assembly (Part Number 6541435-1 , -9, -11, -201, -203, -205)- Replace 

every 41,600 landings 

(d) Right Trailing Link Assembly (Part Number6541435-2, -8,-10,-200, -204, -206)- Replace 

every 41,600 landings 

(e) Oleo Assembly (Part Number 6541420-1 , -4, -7, -8, -200)- Replace every 41,600 landings, 

except the items that follow: 

1 Upper Cap (Part Number 6541421-1 , -2, -4) - Replace every 10,400 landings 

£ Outer Bearing Assembly (Part Number 6541425-2, -6, -13, -15) - Replace every 

27,600 landings 

(f) Left Side Brace Actuator (Part Number 9912465-5, -7) - Replace every 41,600 landings 

(g) Right Side Brace Actuator (Part Number 9912465-6, -8) - Replace every 41 ,600 landings 

(2) Nose Landing Gear Assembly (Part Number 6642000-45, -49, -53, -55, -63, -64, -65, -66, -73, 

-74) -Replace every 23,900 landings, except the items that follow: 

NOTE: Attached hardware, which includes the bolts, bearings, bushings, and axle 

components, related to the installation of the components above must be replaced 

when the related component is replaced. Refer to Chapter 32 for more information. 

(a) Fork and Piston Assembly (Part Number 6642000-3, -209)- Replace every 13,800 landings 

(b) Actuator (Part Number 9912485-2, -3, -4, -5) - Replace every 23,900 landings 

C. Fuselage (Chapter 53). 

(1 ) Left Trunnion Support Fitting (Part Number 6613056-3, -5)- Replace every 12,200 landings 

(2) Right Trunnion Support Fitting (Part Number 6613056-4, -6)- Replace every 12,200 landings 

(3) Actuator Support Fitting (Part Number 6511105-1 , -200) - Replace every 23,900 landings 

D. Wings (Chapter 57). 

(1) Left Aft Trunnion Attach Fitting (Part Number 6522465-1)- Replace every 41 ,600 landings 

(2) Right Aft Trunnion Attach Fitting (Part Number 6522465-2) - Replace every 41,600 landings 

(3) Left Forward Trunnion Attach Fitting (Part Number 6522460-5)- Replace every 41 ,600 landings 

(4) Right Forward Trunnion Attach Fitting (Part Number 6522460-6) -Replace every 41 ,600 landings 

(5) Left Side Brace Fitting (Part Number 6521435-1) - Replace every 41 ,600 landings 

© Cessna Aircraft Company 

4-11-00 Page 1 

Jun 23/2014 
CESSNA AIRCRAFT COMPANY 

MODEL 550 BRAVO 

MAINTENANCE MANUAL 

(6) Right Side Brace Fitting (Part Number 6521 435-2) - Replace every 41 ,600 landings 

© Cessna Aircraft Company 

4-11-00 Page 2 

Jun 23/2014 
CESSNA AIRCRAFT COMPANY 

MODEL 550/551 

MAINTENANCE MANUAL 

CHAPTER 

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. 

APPROVED BY ~4~ LAWRENCE A. HERRON, MANAGER 

AIRCRAFT CERTIFICATION OFFICE 

FEDERAL AVIATION ADMINISTRATION 

WICHITA, KANSAS 

DATE OF APPROVAL DEC. //) Jqqz 

11 DECEMBER 1992 

REVISION 10 23 JUNE 2014 
CESSNA AIRCRAFT COMPANY 

MODEL 550/551 

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 

4-11-00 

1\.largml·!l Klnw. .:m~o 

/\1n~a rt Cl"!rh fi <'...-11ion Of 1c r 

Fml0r<1l f\111atiun Ad111ir tra ~on 

V·hduta, Kansas 

DATE OF APPROVAL 

PAGE 

Page 1 

Page 1 

Pages 1-4 

DATE 

Jan 9/2007 

Jun 23/2014 

Jun 23/2014 

© Cessna Aircraft Company 

4- LIST OF EFFECTIVE PAGES Page 1 of 1 

Jun 23/2014 
CESSNA AIRCRAFT COMPANY 

MODEL 550/551 

MAINTENANCE MANUAL 

4 - CONTENTS 

AIRWORTHINESS LIMITATIONS . . . . ........ . . ... . .... . . ....... . ....... . . ...... . . 

Scope .. . . . .. .......... . . . . . . . ................... . .... . .................... . 

Definition . ............................... . . . . ............... . . .. . . ......... . 

INSPECTION TIME LIMITS ............ . . . . . ........................ . ............ . 

General ......... . . ... ....... ................ ........... ............... .... . 

Inspection Schedule .............. ..... ........................ ... .......... . 

REPLACEMENT TIME LIMITS ..... ................. .......... ................. .. . 

General .... .. . . ... ........ . . .............. .......... .. . ............ . . ..... . 

Replacement Schedule ... .......... . ....................... .. .............. . 

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4-CONTENTS P~e1cl1 

Jun 23/2014 
1. Scope 

CESSNA AIRCRAFT COMPANY 

MODEL 550/551 

MAINTENANCE MANUAL 

AIRWORTHINESS LIMITATIONS 

A. This chapter gives the mandatory replacement times and inspection intervals for life limited 

components and airplane structures, or those that require scheduled inspections. This chapter is 

related to items such as fatigue components and structures, which are thought of as a part of the 

certification process. 

NOTE: The Airworthiness Limitations section is FAA Approved and supplies inspection and 

maintenance required under Parts 43.16 and 91.409 of Part 14 of the Code of Federal 

Regulations, unless an alternative program has been FAA approved. 

2. Definition 

A. This chapter contains sections as shown below. 

(1) Inspection Time Limits (4-10-00) give a list of the systems and components that must be 

examined at specified intervals. The intervals given show the maximum time approved between 

the inspections. 

(2) Replacement Time Limits (4-11-00) give a list ofthe life limited components that must be replaced 

at a specified time. 

© Cessna Aircraft Company 

4-00-00 Page 1 

Jan 9/2007 
I 

CESSNA AIRCRAFT COMPANY 

MODEL 550/551 

MAINTENANCE MANUAL 

INSPECTION TIME LIMITS 

1. General 

2. 

A. The inspection time intervals applying to the following systems and components represent the 

maximum inspection intervals which must be adhered to. 

Inspection Schedule 

A. Air Conditioning (Chapter 21) 

(1) Vapor Cycle Cooling System Hourmeter Check (Compressor Motors 1134104-1, -5 or 

FWA1134104-1 , -5)- Examine every 300 hours. Refer to Task 21-51 -03-212. 

NOTE: Refer to the Enviro Systems Inc. Operating, Servicing and Component Maintenance 

Manual 21-00-24. 

B. Landing Gear (Chapter 32). 

(1) Brake assembly Goodrich P/N 2-1528-6 with stator disks part number 133-893-2, that are 

impression stamped "-" OR "A". 

(a) Airplanes without thrust reversers or not using thrust reversers -- Inspect by 224 landings 

and every 200 landings until replacement life is reached (7 49 landings). Task 32-42-01-21 0 

(b) Airplanes equipped with and using thrust reversers-- Inspect at 425 landings and replace 

at replacement life (749 landings). Task 32-42-01-210 

(2) Nose Landing Gear Fork (Part Number 5542300-1 , -3) - Airplanes -0002 thru -0626 except 

Airplanes -0491 and -0492- Inspect 5000 landings and every 1000 landings thereafter. Task 

32-21-01-250 

(3) Nose Landing Gear Fork (Part Number 5542300-1, -3) Airplanes -0491 and -0492 -Inspect 3400 

landings and every 1000 landings thereafter. Task 32-21-01-250 

(4) Nose Landing Gear Fork Airplanes -0627 and On (Part Number 5542300-2) - Inspect 10,000 

landings and every 1000 landings thereafter. Task 32-21-01-250 

NOTE: These components also have replacement time limits. Refer to Chapter 4-11-00, 

Replacement Time Limits, for replacement criteria. 

© Cessna Aircraft Company 

4-1 0-00 Page 1 

Jun 23/2014 
I 

CESSNA AIRCRAFT COMPANY 

MODEL 550/551 

MAINTENANCE MANUAL 

REPLACEMENT TIME LIMITS 

1. General 

2. 

A. The life-limited components that follow must be replaced at the specified time. It is recommended that 

the components be scheduled for replacement during the airplane's inspection interval that aligns with, 

or occurs just before, the specified time limit is expired. Procedures to replace the components are 

given in the applicable chapters in this maintenance manual. 

NOTE: The landing gear assemblies include the components that follow, which have given life limits. 

The airplane effectivities of the landing gear assemblies and their components are as the airplane 

was made. Any components that were replaced during normal maintenance or by a service 

bulletin are not given. Examine the individual airplane records for the part numbers of the 

replacement parts. If you can not find the part numbers of the individual components currently 

installed, you must use the lowest replacement life of the like component. 

Replacement Schedule 

A. Air Conditioning (Chapter 21) 

(1) Vapor Cycle Cooling System Compressor Drive Motor Brushes (Compressor Motors 11341 04-1 , 

-5 or FWA 1134104-1, -5) - Replace every 500 compressor hours. 

NOTE: Refer to the Enviro Systems Inc. Operating, Servicing and Component Maintenance 

Manual 21-00-24. 

B. Landing Gear (Chapter 32). 

(1) Brake assembly Goodrich Part Number 2-1528-6 with stator disks Part Number 133-893-2, that 

are impression stamped"-" OR "A". -Replace every 749 landings. 

(2) Nose Landing Gear (Airplanes -0002 thru -0626 except Airplanes -0491 and -0492) 

NOTE: The attaching hardware (bolts, bearings, bushings, and axle components associated 

with the installation of the components below) is to be replaced whenever the 

associated component is replaced. Refer to Chapter 32, Nose Landing Gear and 

Doors - Removal/Installation, for more information. 

(a) Nose Landing Gear Assembly (Part Number 5542000-9, -205) and the attaching hardware 

- Replace every 22,500 landings except for the following items: 

1 Fork (Part Number 5542300-1 , -3)- Replace every 12,500 landings. 

~ Piston Weld Assembly (Part Number 5542105-2, -3)- Replace every 12,500 landings. 

(b) Actuator (Part Number 9912063-11, -13)- Replace every 32,600 landings. 

(c) Actuator (Part Number 9912120-1 , -2, -3, -4) - Replace every 23,900 landings. 

(3) Nose Landing Gear (Airplanes -0491 and -0492) 

NOTE: The attaching hardware (bolts, bearings, bushings, and axle components associated 

with the installation of the components below) is to be replaced whenever the 

associated component is replaced. Refer to Chapter 32, Nose Landing Gear and 

Doors - Removal/Installation, for more information. 

(a) Nose Landing Gear Assembly (Part Number 5542000-9, -205) and the attaching hardware 

-Replace every 15,500 landings except for the following items: 

1 Fork (Part Number 5542300-1, -3) - Replace every 8600 landings. 

~ Piston Weld Assembly (Part Number 5542105-3)- Replace every 8600 landings. 

(b) Actuator (Part Number 9912063-11, -13)- Replace every 21,200 landings. 

(c) Actuator (Part Number 9912120-1 , -2, -3, -4)- Replace every 16,400 landings. 

© Cessna Aircraft Company 

4-11-00 Page 1 

Jun 23/2014 
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I 

CESSNA AIRCRAFT COMPANY 

MODEL 550/551 

MAINTENANCE MANUAL 

(4) Nose Landing Gear (Airplanes -0627 thru -0800) 

NOTE: The attaching hardware (bolts, bearings, bushings, and axle components associated 

with the installation of the components below) is to be replaced whenever the 

associated component is replaced. Refer to Chapter 32, Nose Landing Gear and 

Doors - Removal/Installation, for more information. 

(a) Nose Landing Gear Assembly (Part Number 6642000-5, -11 , -15, -19, -24, -27, -29, -35, 

-45, -49, -53, -55, -66) and Attaching Hardware - Replace every 23,900 landings except 

for the following items: 

1 Fork (Part Number 5542300-2)- Replace every 13,800 landings. 

~ Piston Weld Assembly (Part Number 6642100-1 , -2, -3) - Replace every 13,800 

landings. 

(b) Actuator (Part Number 9912063-11 , -13)- Replace every 36,600 landings. 

(c) Actuator (Part Number 9912120-1, -2, -3, -4) - Replace every 23,900 landings. 

(5) Main Landing Gear (Airplanes -0002 thru -0626 except Airplanes -0491 and -0492) 

NOTE: The attaching hardware (bolts, bearings, bushings, trunnion pins, and trunnion/link 

pin associated with the installation of the components below) is to be replaced 

whenever the associated component is replaced. Refer to Chapter 32, Main Gear 

and Doors - Removal/Installation, for more information. 

(a) Left Main Landing Gear Assembly and the attaching hardware (Part Number 6541000-3, 

-11 , -27, -33, -37)- Replace every 28,600 landings except for the following items: 

1 Outer Cylinder (Part Number 5541109-1, -5 or 5541320-203)- Replace every 16,100 

landings. 

~ Torque Link Assembly, Lower (Part Number 5541304-11 )- Replace every 41 ,600 

landings. 

(b) Right Main Landing Gear Assembly and the attaching hardware (Part Number 6541000-4, 

-12, -28, -34, -38)- Replace every 28,600 landings except for the following items: 

1 Outer Cylinder (Part Number 5541109-2, -6 or 5541320-202) - Replace every 16,100 

landings. 

2 Torque Link Assembly, Lower (Part Number 5541304-6) - Replace every 41 ,600 

landings. 

(c) Left Actuator Assembly (Part Number 9912053-13, -17, -19) - Replace every 37,500 

landings. 

(d) Right Actuator Assembly (Part Number 9912053-14, -18, -20) - Replace every 37,500 

landings. 

(6) Main Landing Gear (Airplanes -0491 and -0492) 

NOTE: The attaching hardware (bolts, bearings, bushings, trunnion pins, and trunnion/link 

pin associated with the installation of the components below) is to be replaced 

whenever the associated component is replaced. Refer to Chapter 32, Main Gear 

and Doors- Removal/Installation, for more information. 

(a) Left Main Landing Gear Assembly (Part Number 6541 000-37) and the attaching hardware 

-Replace every 16,800 landings except for the following items: 

1 Torque Link Assembly, Lower (Part Number 5541304-11)- Replace every 24,500 

landings. 

(b) Right Main Landing Gear Assembly (Part Number 6541 000-38) and the attaching hardware 

-Replace every 16,800 landings except for the following items: 

1 Torque Link Assembly, Lower (Part Number 5541304-6) - Replace every 24,500 

landings. 

(c) Left Actuator Assembly (Part Number 9912053-13, -17, -19) - Replace every 22,000 

landings. 

(d) Right Actuator Assembly (Part Number 9912053-14, -18, -20) - Replace every 22,000 

landings. 

© Cessna Aircraft Company 

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MODEL 550/551 

MAINTENANCE MANUAL 

(7) Main Landing Gear (Airplanes -0627 thru -0800) 

NOTE: The attaching hardware (bolts, bearings, bushings, trunnion pins, and trunnion/link 

pin associated with the installation of the components below) is to be replaced 

whenever the associated component is replaced. Refer to Chapter 32, Main Gear 

and Doors - RemovaVInstallation, for more information. 

(a) Left Main Landing Gear Assembly (Part Number 6541001-3, -7, -13, -21) and the attaching 

hardware - Replace every 25,800 landings except for the following items: 

1 Torque Link Bolt (Part Number 5541220-2)- Replace every 21,500 landings. 

(b) Right Main Landing Gear Assembly (Part Number 6541001-4, -8, -14, -22) and the 

attaching hardware - Replace every 25,800 landings except for the following items: 1 Torque Link Bolt (Part Number 5541220-2) - Replace every 21 ,500 landings. 

(c) Left Actuator Assembly (Part Number 9912053-21, -23) -Replace every 41 ,500 landings. 

(d) Right Actuator Assembly (Part Number 9912053-22, -24)- Replace every 41 ,500 landings. 

C. Fuselage (Chapter 53). 

(1) Airplanes -0002 thru -0626 except Airplanes -0491 and -0492 

(a) Nose Landing Gear Actuator Fitting (Part Number 5511169-1) - Replace every 13,800 

landings. 

(b) Nose Landing Gear Actuator Fitting (Part Number 6511105-1, -200- Replace every 23,900 

landings. 

(c) Left Nose Landing Gear Trunnion Support (Part Number 5513056-5, -7, 6390037-13) -

Replace every 22,500 landings. 

(d) Right Nose Landing Gear Trunnion Support (Part Number 5513056-6, -8, 6390037-14)-

Replace every 22,500 landings. 

(2) Airplanes -0491 and -0492 

(a) Nose Landing Gear Actuator Fitting (Part Number 5511169-1) - Replace every 9500 

landings. 

(b) Nose Landing Gear Actuator Fitting (Part Number6511105-1 , -200) - Replace every 16,400 

landings. 

(c) Left Nose Landing Gear Trunnion Support (Part Number 5513056-5, -7, 6390037-13)-

Replace every 15,500 landings. 

(d) Right Nose Landing Gear Trunnion Support (Part Number 5513056-6, -8, 6390037-14)-

Replace every 15,500 landings. 

(3) Airplanes -0627 thru -0800 

(a) Nose Landing Gear Actuator Fitting (Part Number 6511105-1 , -200)- Replace every 23,900 

landings. 

(b) Left Nose Landing Gear Trunnion Support (Part Number 6613056-3) - Replace every 

12,200 landings. 

(c) Right Nose Landing Gear Trunnion Support (Part Number 6613056-4) - Replace every 

12,200 landings. 

D. Wing (Chapter 57). 

(1) Airplanes -0002 thru -0626 except Airplanes -0491 and -0492 

(a) Main Landing Gear Forward Left Trunnion Fitting Assembly (Part Number 5522700-1. -5) 

- Replace every 25,800 landings. 

(b) Main Landing Gear Forward Right Trunnion Fitting Assembly (Part Number 5522700-2, -6) 

- Replace every 25,800 landings. 

(c) Main Landing Gear Aft Left Trunnion Fitting Assembly (Part Number 552271 0-1 , -7, -11) -

Replace every 18,300 landings. 

(d) Main Landing Gear Aft Right Trunnion Fitting Assembly (Part Number 5522710-2, -8, -12) 

- Replace every 18,300 landings. 

(e) Main Landing Gear Left Side Brace Support Fitting (Part Number 5522720-1 , -7, -15, -17, 

-21 , -25) - Replace every 30,000 landings. 

(f) Main Landing Gear Right Side Brace Support Fitting (Part Number 5522720-2, -8, -14, -16, 

-22, -26) - Replace every 30,000 landings. 

© Cessna Aircraft Company 

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Jun 23/2014 
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MODEL 550/551 

MAINTENANCE MANUAL 

(2) Airplanes -0491 and -0492 

(a) Main Landing Gear Forward Left Trunnion Fitting Assembly (Part Number 5522700-5) -

Replace every 15,200 landings. 

(b) Main Landing Gear Forward Right Trunnion Fitting Assembly (Part Number 5522700-6) -

Replace every 15,200 landings. 

(c) Main Landing Gear Aft Left Trunnion Fitting Assembly (Part Number 5522710-11) - Replace 

every 10,800 landings. 

(d) Main Landing Gear Aft Right Trunnion Fitting Assembly (Part Number 5522710-12) -

Replace every 10,800 landings. 

(e) Main Landing Gear Left Side Brace Support Fitting (Part Number 5522720-25)- Replace 

every 17,700 landings. 

(f) Main Landing Gear. Right Side Brace Support Fitting (Part Number 5522720-26) -Replace 

every 17,700 landings. 

(3) Airplanes -0627 thru -0800 

(a) Main Landing Gear Forward Left Trunnion Fitting Assembly (Part Number 5522700-9) -

Replace every 25,800 landings. 

(b) Main Landing Gear Forward Right Trunnion Fitting Assembly (Part Number 5522700-1 0) 

- Replace every 25,800 landings. 

(c) Main Landing Gear Aft Left Trunnion Fitting Assembly (Part Number 5522710-11) - Replace 

every 18,300 landings. 

(d) Main Landing Gear Aft Right Trunnion Fitting Assembly (Part Number 5522710-12) -

Replace every 18,300 landings. 

(e) Main Landing Gear Left Side Brace Support Fitting (Part Number 5522720-29) - Replace 

every 25,800 landings. 

(f) Main Landing Gear Right Side Brace Support Fitting (Part Number 5522720-30) - Replace 

every 25,800 landings. 

© Cessna Aircraft Company 

4-11-00 Page 4 

Jun 23/2014 
CESSNA AIRCRAFT COMPANY 

MODEL 560 

MAINTENANCE MANUAL 

CHAPTER 

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. 

APPROVED 

~ANAGER, 

BY 

AIRCRAFT 

~ 

CERTIFICATION OFFICE 

WICHITA, KANSAS 

CENTRAL REGION 

DATE OF APPROVAL _../~~f-/.:.,~'/'-o:JB~l:J~--

7 DECEMBER 1988 

REVISION 22 23 JUNE 2014 
CESSNA AIRCRAFT COMPANY 

MODEL 560 

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 

4-11-00 

4-11-02 

PAGE 

Page 1 

Pages 1-2 

Page 1 

Pages 1-6 

Pages 1-6 

APP~~~~~t~:, /,ircm ft C:orO

,~~~ fi Galiou Olfl -; 

Fedcr81 NJ1ab on l\dlllllll$lra Uon 

DATE 

Apr 23/2012 

Jun 23/2014 

Sep 23/2004 

Jun 23/2014 

Jun 23/2014 

DA T~ ~~ ~;;~~~ AL ~5 ~,_.__ ~twj_ 

© Cessna Aircraft Company 

4 - LIST OF EFFECTIVE PAGES Page 1 of 1 

Jun 23/2014 
CESSNA AIRCRAFT COMPANY 

MODEL 560 

MAINTENANCE MANUAL 

4- CONTENTS 

AIRWORTHINESS LIMITATIONS ................................................ . 

Scope .. .... .................. ..... ........................................ . 

Definition ............................ .. .... . .............. ...... ........... . 

INSPECTION TIME LIMITS ....... .......... .................. ........... ........ . 

General ......................... . . ... . ... ........ ........................ . . 

Inspection Schedule ........................................................ . 

560-0597 AIRPLANE INSPECTION TIME LIMITS ................................. . 

General ............................................................. ...... . 

Inspection Schedule ............ ........... ................................. . 

REPLACEMENT TIME LIMITS ................................................... . 

General .... ........... ... ............. .. .................. ..... . .......... . 

Replacement Schedule ............ . ... ..................................... . 

UC35A AIRPLANE REPLACEMENT TIME LIMITS ............. .............. ...... . 

General .... ......... ..... ......... ...... . ... ............. ............. .... . 

Replacement Schedule ......... ..... .. .. ............. .............. ........ . 

4-00-00 Page 1 

4-00-00 Page 1 

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4-1 0-00 Page 1 

4-1 0-00 Page 1 

4-10-00 Page 1 

4-10-01 Page 1 

4-10-01 Page 1 

4-10-01 Page 1 

4-11-00 Page 1 

4-11-00 Page 1 

4-11-00 Page 1 

4-11-00 Page 1 

4-11-00 Page 1 

4-11-00 Page 1 

©Cessna Aircraft Company 

4 - CONTENTS Page 1 of 1 

Jun 23/2014 
I 

I 

1. Scope 

CESSNA AIRCRAFT COMPANY 

MODEL 560 

MAINTENANCE MANUAL 

AIRWORTHINESS LIMITATIONS 

A. This chapter outlines the mandatory replacement times and inspection intervals for components 

and airplane structures considered to be life-limited, or to require monitoring through scheduled 

inspections. This chapter applies to items such as fatigue components and structures which are 

considered a part of the certification process. 

B. The Airworthiness Limitations section is FAA-approved and gives inspections and maintenance 

procedures that are required by Parts 43.16 and 91.409 of Title 14 of the Code of Federal Regulations, 

unless an alternative program has been FAA-approved. 

2. Definition 

A. This chapter contains the below sections outlined: 

(1) Inspection Time Limits (4-10-00) section describes and lists systems and components which are 

required to be inspected at specified intervals. The intervals specified represent the maximum 

time allowable between inspections. 

(2) Inspection Time Limits (4-10-01) section describes and lists additional systems and components 

which are required to be inspected at specified intervals for the Model 560-0597 airplane. The 

intervals specified represent the maximum time allowable between inspections. 

(3) Replacement Time Limits (4-11-00) section describes and lists life-limited components which 

are to be replaced at a specific time. 

(4) Section 4-11-02 describes and lists life-limited components for the Model 560 UC35A airplanes 

having a gross ramp weight of 16,850 pounds. 

© Cessna Aircraft Company 

4-00-00 Page 1 

Apr 23/2012 
I 

CESSNA AIRCRAFT COMPANY 

MODEL 560 

MAINTENANCE MANUAL 

INSPECTION TIME LIMITS 

1. General 

2. 

A. The inspection time intervals applying to the following systems and components show the maximum 

inspection intervals which must be obeyed. 

NOTE: The inspection intervals for structural elements defined in this chapter are absolute limits 

which must not be exceeded. They are calculated based on criteria which will detect cracks 

before they grow to a critical size. By following the continuous inspection requirements 

outlined in Chapter 5, the inspection requirements presented in this chapter will be satisfied. 

In some cases, the corresponding inspection defined in Chapter 5 is at an interval which 

coincides with a phase inspection having a lesser time limit. Performing the inspection 

during the regularly scheduled phase(s) will, in most cases, be more economical than 

completing each item at its maximum inspection interval. 

NOTE: Repairs that are made to structures, for example, the addition of doublers, may invalidate 

an inspection and/or procedure. Modified inspections may be required for structures which 

have been repaired. 

Inspection Schedule 

A. Air Conditioning (Chapter 21) 

(1) Vapor Cycle Cooling System Hourmeter Check (Compressor Motors 1134104-1, -5 or 

FWA1134104-1 , -5 only)- Examine every 300 hours. Refer to Task 21-52-00-212. 

NOTE: Refer to the Enviro Systems Inc. Operating, Servicing and Component Maintenance 

Manual 21-00-24 for Airplanes -0001 thru -0462 equipped with an Enviro Systems 

R-134a system or Enviro Systems Inc. Operating, Servicing and Component 

Maintenance Manual 21-00-07 for Airplanes -0463 thru -0815. 

B. Ice and Rain Protection (Chapter 30). 

(1) Wing Anti-Ice Crossfeed Valve (Part Number 9912403-2) Operational Check Airplanes -0539 

and On- Do the check every 150 hours. Task 30-14-00-710 

C. Landing Gear (Chapter 32). 

(1) Nose Gear Fork (Part Number 6642000-3, -209) - Do every 10,000 landings and every 1000 

landings thereafter. Task 32-21-01-250 

D. Fuselage (Part Number 6510002-1 for Airplanes 560-0001 thru 560-0538) and (Part Number 

6510500-1 for Airplanes 560-0539 and On) (Chapter 53). 

(1) Forward Side of Forward Pressure Bulkhead Web -- Do the inspection every 4450 hours. Task 

53-10-00-213. 

(2) Forward Pressure Bulkhead Attach Angles - Do the inspection every 6725 hours. Task 53-1 0-

00-251 

(3) Aft Side of Aft Pressure Bulkhead Web- Do the inspection every 4450 hours. Task 53-10-04-211 

(4) Aft Pressure Bulkhead Attach Angles-- Do the inspection every 6725 hours. Task 53-10-00-252 

(5) Cabin Door Frame Inspection for Airplanes -0001 thru -0045 -- Do the inspection every 5000 

hours. Task 53-1 0-09-290 

(6) Cabin Door Frame Inspection for airplanes -0046 and On - Do the inspection every 5000 hours. 

Task 53-10-10-210 

(7) Emergency Exit Door Frame- Do the inspection every 1456 hours. Task 53-10-09-212 

(8) Windshield, Cockpit Side Window and Cabin Window Frames- Do the inspection every 5130 

hours. Task 53-30-00-211 

(9) Fuselage Exterior Skin-- Do the inspection every 2523 hours. Task 53-30-00-210 

(1 0) Cabin Lower Skin Longitudinal Splice- Do the inspection every 5900 hours. Task 53-30-00-251 

© Cessna Aircraft Company 

4-10-00 Page1 

Jun 23/2014 
1. General 

CESSNA AIRCRAFT COMPANY 

MODEL 560 

MAINTENANCE MANUAL 

560-0597 AIRPLANE INSPECTION TIME LIMITS 

A. These inspection time intervals must be performed in addition to the inspections required in Inspection 

Time Limits. 

B. The inspection time intervals applying to the following systems and components represent the 

maximum inspection intervals which must be adhered to. 

2. Inspection Schedule 

A. Fuselage (Part Number 6510500-1) (Chapter 53) 

(1) Optical Window Structure Borescope Inspection - Inspect every 3608 hours or 76 calendar 

months, whichever occurs first. Refer to the Model 560-0597 Maintenance Manual Supplement, 

Task 53-90-00-290. 

(2) Optical Window Frame Weld Assembly Inspection- Inspect every 10,007 hours. Refer to the 

Model 560-0597 Maintenance Manual Supplement, Task 53-90-00-250. 

B. Windows (Part Number 6510500-1) (Chapter 56) 

(1) Optical Window - Inspect using optical prism test procedure at the first 2500 hours and then 

every 1300 hours thereafter. Refer to the Model 560-0597 Maintenance Manual Supplement, 

Task 56-90-00-280. 

© Cessna Aircraft Company 

4-10-01 Page 1 

Sep 23/2004 
I 

1. General 

CESSNA AIRCRAFT COMPANY 

MODEL 560 

MAINTENANCE MANUAL 

REPLACEMENT TIME LIMITS 

A. The life-limited components that follow must be replaced at the specified time. It is recommended that 

the components be scheduled for replacement during the airplane's inspection interval that aligns with, 

or occurs just before the specified time limit is expired. Procedures to replace the components are 

given in the applicable chapters in this maintenance manual. 

2. Replacement Schedule 

A. Air Conditioning (Chapter 21) 

(1) Vapor Cycle Air Conditioning System Compressor Drive Motor Brushes (Compressor Motors 

1134104-1, -5 or FWA1134104-1 , -5 only) - Replace every 500 compressor hours. 

NOTE: Refer to the Enviro Systems Inc. Operating, Servicing and Component Maintenance 

Manual 21-00-24 for Airplanes -0001 thru -0462 equipped with an Enviro Systems 

R-134a system or Enviro Systems Inc. Operating, Servicing and Component 

Maintenance Manual 21-00-07 for Airplanes -0463 thru -0815. 

B. Flight Controls (Chapter 27). 

(1) Flaps 

(a) Inboard and Outboard Flap Aft Rollers (Part Number CC50380 or CC59163) - Replace 

every 5000 landings. 

C. Landing Gear (Chapter 32). 

(1) Nose Landing Gear (Airplanes -0001 thru -0259) 

NOTE: Attaching hardware (bolts. bearings, bushings, and axle components associated 

with the installation of the components above} is to be replaced whenever the 

associated component is replaced. Refer to Chapter 32, Nose Landing Gear And 

Doors - Removal/Installation for more information. 

(a) Nose Landing Gear Assembly (Part Number 6642000-10, -14, -18, -25, -26, -28, -34, -44, 

-48, -52, -54, -63, -65) and Attaching Hardware except Fork and Piston Assembly (Part 

Number 6642000-3, -209) -Replace every 23,500 landings. 

(b) Actuator Assembly (Decoto) (Part Number 2-7406-2) - Replace every 23,500 landings. 

(c) Actuator Assembly (Teijin Seiki} (Part Number 1523200-3, -5. -7. -9) - Replace every 

15,000 landings. 

(d) Fork and Piston Assembly (Part Number 6642000-3, -209) - Replace every 13,640 

landings. 

(2) Nose Landing Gear (Airplanes -0260 thru -0538) 

NOTE: Attaching hardware (bolts, bearings, bushings, and axle components associated 

with the installation of the components above} is to be replaced whenever the 

associated component is replaced. Refer to Chapter 32, Nose Landing Gear And 

Doors - Removal/Installation for more information. 

(a) Nose Landing Gear Assembly (Part Number 6642000-26, -28, -34, -44, -48, -52, -54, -63, 

-65) and Attaching Hardware except Fork and Piston Assembly (Part Number 6642000-3, 

-209) - Replace every 23,100 landings. 

(b) Actuator Assembly (Decato) (Part Number 2-7406-2)- Replace every 23,100 landings. 

(c) Actuator Assembly (Teijin Seiki) (Part Number 1523200-5, -7, -9) - Replace every 15,000 

landings. 

(d) Fork and Piston Assembly (Part Number 6642000-3, -209) - Replace every 13,380 

landings. 

© Cessna Aircraft Company 

4-11-00 Page 1 

Jun 23/2014 
CESSNA AIRCRAFT COMPANY 

MODEL 560 

MAINTENANCE MANUAL 

(f) Actuator Assembly, Right (Teijin Seiki) (Part Number 1523100-4, -8) - Replace every 

15,000 landings. 

(g) Torque Link Bolt (Part Number 5541220-2)- Replace every 10,370 landings. 

(7) Main Landing Gear (Airplanes -0260 thru -0538) 

NOTE: Attaching hardware (bolts, bearings, bushings, trunnion pins, and trunnion/link pin 

associated with the installation of the components below) is to be replaced whenever 

the associated component is replaced. Refer to Chapter 32, Main Gear and DoorsRemoval/Installation for more information. 

(a) Main Landing Gear Assembly, Left (Part Number 6641000-15, -27, -35) and Attaching 

Hardware - Replace every 11,425 landings. 

(b) Main Landing Gear Assembly, Right (Part Number 6641000-16, 28, -36) and Attaching 

Hardware- Replace every 11,425 landings. 

(c) Actuator Assembly, Left (Decoto) (Part Number2-7442-3)- Replace every 11,4251andings. 

(d) Actuator Assembly, Right (Decoto) (Part Number 2-7442-4) - Replace every 11 ,425 

landings. 

(e) Actuator Assembly, Left (Teijin Seiki) (Part Number 1523100-7)- Replace every 15,000 

landings. 

(f) Actuator Assembly, Right (Teijin Seiki) (Part Number 1523100-8) - Replace every 15,000 

landings. 

(g) Torque Link Bolt (Part Number 5541220-2) - Replace every 951 0 landings. 

(8) Main Landing Gear (Airplanes -0539 thru -0750 Not Incorporating SB560-32-40) 

NOTE: Attaching hardware (bolts, bearings, bushings, trunnion pins, and trunnion/link pin 

associated with the installation of the components below) is to be replaced whenever 

the associated component is replaced. Refer to Chapter 32, Main Gear and Doors -

RemovaUinstallation for more information. 

(a) Left Trunnion Machining (Part Number 6541561-1 , 6594021-1 ) - Replace every 50,100 

landings. 

(b) Right Trunnion Machining (Part Number 6541561-2, 6594021-2)- Replace every 50,100 

landings. 

(c) Trailing Link Assembly (Airplanes -0539 thru -0580) 

1 Left Trailing Link (Part Number 6541516-1 , -3, -5)- Replace every 9800 landings. f. Right Trailing Link (Part Number6541516-2, -4, -6) - Replace every 9800 landings. 

(d) Trailing Link Assembly (Airplanes -0581 and On) 

1 Left Trailing Link (Part Number 6541516-3, -5)- Replace every 25,000 landings. f. Right Trailing Link (Part Number 6541516-4, -6)- Replace every 25,000 landings. 

(e) Oleo Assembly (Part Number 6541520-2, -3, -4, -5)- Replace every 31,900 landings, 

except for the part that follows: 

1 Outer Bearing Assembly (Part Number 6541425-6, -13, -15)- Replace every 21 ,800 

landings. 

(f) Left Side Brace Actuator (Part Number 9912569-1 , -3) - Replace every 50,1 00 landings. 

(g) Right Side Brace Actuator (Part Number 9912569-2, -4) - Replace every 50,100 landings. 

(9) Main Landing Gear (Airplanes -0539 thru -0750 Incorporating SB560-32-40) 

NOTE: Attaching hardware (bolts, bearings, bushings, trunnion pins, and trunnion/link pin 

associated with the installation of the components below) is to be replaced whenever 

the associated component is replaced. Refer to Chapter 32, Main Gear and Doors -

Removal/Installation for more information. 

(a) Left Trunnion Machining (Part Number 6541561-1 , 6594021-1) - Replace every 42,100 

landings. 

(b) Right Trunnion Machining (Part Number 6541561-2, 6594021-2} - Replace every 42,100 

landings. 

(c) Trailing Link Assembly (Airplanes -0539 thru -0580) 

1 Left Trailing Link (Part Number 6541516-1 , -3, -5)- Replace every 8526 landings. 

© Cessna Aircraft Company 

4-1 1-00 Page 3 

Jun 23/2014 
CESSNA AIRCRAFT COMPANY 

MODEL 560 

MAINTENANCE MANUAL 

(c) Nose Landing Gear Trunnion Support, Right (Part Number 6613056-4, 6) -Replace every 

11 ,233 landings. 

(5) Airplanes -0751 and On 

(a) Nose Landing Gear Actuator Fitting (Part Number6511105-1, -200)- Replace every 21 ,958 

landings. 

(b) Nose Landing Gear Trunnion Support, Left (Part Number 6613056-5, -201)- Replace every 

11 ,233 landings. 

(c) Nose Landing Gear Trunnion Support, Right (Part Number 6613056-6, -202) - Replace 

every 11 ,233 landings. 

E. Wings (Chapter 57). 

(1) Airplanes -0001 thru -0259 

(a) Main Landing Gear Trunnion Fitting Assembly, Forward Left (Part Number 6522057-5)-

Replace every 27,460 landings. 

(b) Main Landing Gear Trunnion Fitting Assembly, Forward Right (Part Number 6522057-6)-

Replace every 27,460 landings. 

(c) Main Landing Gear Trunnion Fitting Assembly, Aft (Part Number 552271 0-15) - Replace 

every 27,460 landings. 

(d) Main Landing Gear Side Brace Support Fitting, Left (Part Number 6522047-1, -7) - Replace 

every 28,080 landings. 

(e) Main Landing Gear Side Brace Support Fitting, Right (Part Number 6522047-2, -8) -

Replace every 28,080 landings. 

(2) Airplanes -0260 thru -0538 

(a) Main Landing Gear Trunnion Fitting Assembly, Forward Left (Part Number 6522057-5) -

Replace every 22,900 landings. 

(b) Main Landing Gear Trunnion Fitting Assembly, Forward Right (Part Number 6522057-6)-

Replace every 22,900 landings. 

(c) Main Landing Gear Trunnion Fitting Assembly, Aft (Part Number 5522710-15)- Replace 

every 22,900 landings. 

(d) Main Landing Gear Side Brace Support Fitting, Left (Part Number 6522047-1 , -7)- Replace 

every 24,700 landings. 

(e) Main Landing Gear Side Brace Support Fitting, Right (Part Number 6522047-2, -8) -

Replace every 24,700 landings. 

(3) Airplanes (Airplanes -0539 thru -0750 Not Incorporating SB560-32-40) 

(a) Left Aft Trunnion Attach Fitting (Part Number 6522634-5, -201) -Replace every 23,900 

landings. 

(b) Right Aft Trunnion Attach Fitting (Part Number 6522634-6, -202)- Replace every 23,900 

landings. 

(c) Left Forward Trunnion Attach Fitting (Part Number 6522640-1 , -201)- Replace every 

23,900 landings. 

(d) Right Forward Trunnion Attach Fitting (Part Number 6522640-2, -202) - Replace every 

23,900 landings. 

(e) Left Side Brace Support Fitting (Part Number 6521525-1 , -201)- Replace every 50,100 

landings. 

(f) Right Side Brace Support Fitting (Part Number 6521525-2, -202) - Replace every 50,100 

landings. 

(4) Airplanes (Airplanes -0539 thru -0750 Incorporating SB560-32-40) 

(a) Left Aft Trunnion Attach Fitting (Part Number 6522634-5, -201) - Replace every 23,900 

landings. 

(b) Right Aft Trunnion Attach Fitting (Part Number 6522634-6, -202) -Replace every 23,900 

landings. 

(c) Left Forward Trunnion Attach Fitting (Part Number 6522640-1, -201) - Replace every 

23,900 landings. 

(d) Right Forward Trunnion Attach Fitting (Part Number 6522640-2, -202) - Replace every 

23,900 landings. 

(e) Left Side Brace Support Fitting (Part Number 6521525-1 , -201) - Replace every 42,100 

landings. 

© Cessna Aircraft Company 

4-11-00 Page 5 

Jun 23/2014 

I 

CESSNA AIRCRAFT COMPANY 

MODEL 560 

MAINTENANCE MANUAL 

UC35A AIRPLANE REPLACEMENT TIME LIMITS 

1. General 

2. 

A. The life-limited components that follow must be replaced at the specified time. It is recommended that 

the components be scheduled for replacement during the airplane's inspection interval that aligns with, 

or occurs just before the specified time limit is expired. Procedures to replace the components are 

given in the applicable chapters in this maintenance manual. 

Replacement Schedule 

A. Air Conditioning (Chapter 21 ) 

(1) Vapor Cycle Air Conditioning System Compressor Drive Motor Brushes (Compressor Motors 

1134104-1, -5 or FWA1134104-1 , -5 only)- Replace every 500 compressor hours. 

NOTE: Refer to the Enviro Systems Inc. Operating, Servicing and Component Maintenance 

Manual 21-00-24 for Airplanes -0001 thru -0462 equipped with an Enviro Systems 

R-134a system or Enviro Systems Inc. Operating, Servicing and Component 

Maintenance Manuai21-00-07 for Airplanes -0463 thru -0815. 

B. Flight Controls (Chapter 27). 

(1) Flaps 

(a) Inboard and Outboard Flap Aft Rollers (Part Number CC50380 or CC59163) - Replace 

every 5000 landings. 

C. Landing Gear (Chapter 32). 

(1) Nose Landing Gear. (Airplanes -0001 thru -0259) 

NOTE: Attaching hardware (bolts, bearings, bushings, and axle components associated 

with the installation of the components above) is to be replaced whenever the 

associated component is replaced. Refer to Chapter 32, Nose Landing Gear And 

Doors - Removal/Installation for more information. 

(a) Nose Landing Gear Assembly (Part Number 6642000-10, -14, -18, -25, -26, -28, -34, -44, 

-48, -52, -54, -63, -65) and Attaching Hardware except Fork and Piston Assembly (Part 

Number 6642000-3, -209) - Replace every 23,500 landings. 

(b) Actuator Assembly (Decato) (Part Number 2-7406-2) - Replace every 23,500 landings. 

(c) Actuator Assembly (Teijin Seiki) (Part Number 1523200-3, -5, -7, -9) - Replace every 

15,000 landings. 

(d) Fork and Piston Assembly (Part Number 6642000-3, -209) - Replace every 13,640 

landings. 

(2) Nose Landing Gear (Airplanes -0260 thru -0538) 

NOTE: Attaching hardware (bolts, bearings, bushings, and axle components associated 

with the installation of the components above) is to be replaced whenever the 

associated component is replaced. Refer to Chapter 32, Nose Landing Gear And 

Doors - Removal/Installation for more information. 

(a) Nose Landing Gear Assembly (Part Number 6642000-26, -28, -34, -44, -48, -52, -54, -63, 

-65) and Attaching Hardware except Fork and Piston Assembly (Part Number 6642000-3, 

-209) - Replace every 23,1 00 landings. 

(b) Actuator Assembly (Decato) (Part Number 2-7406-2)- Replace every 23,100 landings. 

(c) Actuator Assembly (Teijin Seiki) (Part Number 1523200-5, -7, -9)- Replace every 15,000 

landings. 

(d) Fork and Piston Assembly (Part Number 6642000-3, -209) - Replace every 13,380 

landings. 

© Cessna Aircraft Company 

4-11 -02 Page 1 

Jun 23/2014 
CESSNA AIRCRAFT COMPANY 

MODEL 560 

MAINTENANCE MANUAL 

(f) Actuator Assembly, Right (Teijin Seiki) (Part Number 1523100-4, -8) - Replace every 

15,000 landings. 

(g) Torque Link Bolt (Part Number 5541220-2)- Replace every 10,370 landings. 

(7) Main Landing Gear (Airplanes -0260 thru -0538) 

NOTE: Attaching hardware (bolts, bearings, bushings, trunnion pins, and trunnion/link pin 

associated with the installation of the components below) is to be replaced whenever 

the associated component is replaced. Refer to Chapter 32, Main Gear and Doors -

Removal/Installation for more information. 

(a) Main Landing Gear Assembly, Left (Part Number 6641000-15, -27, -35) and Attaching 

Hardware - Replace every 11,425 landings. 

(b) Main Landing Gear Assembly, Right (Part Number 6641000-16, -28, -36) and Attaching 

Hardware - Replace every 11,425 landings. 

(c) Actuator Assembly, Left (Decato) (Part Number2-7442-3)- Replace every 11,425landings. 

(d) Actuator Assembly, Right (Decato) (Part Number 2-7442-4) - Replace every 11,425 

landings. 

(e) Actuator Assembly, Left (Teijin Seiki) (Part Number 1523100-7) - Replace every 15,000 

landings. 

(f) Actuator Assembly, Right (Teijin Seiki) (Part Number 15231 00-8) - Replace every 15,000 

landings. 

(g) Torque Link Bolt (Part Number 5541220-2)- Replace every 9510 landings. 

(8) Main Landing Gear (Airplanes -0539 thru -0750 Not Incorporating SB560-32-40) 

NOTE: Attaching hardware (bolts, bearings, bushings, trunnion pins, and trunnion/link pin 

associated with the installation of the components below) is to be replaced whenever 

the associated component is replaced. Refer to Chapter 32, Main Gear and Doors -

RemovaVInstallation for more information. 

(a) Left Trunnion Machining (Part Number 6541561-1 , 6594021-1) - Replace every 50,100 

landings. 

(b) Right Trunnion Machining (Part Number 6541561-2, 6594021-2)- Replace every 50,100 

landings. 

(c) Trailing Link Assembly (Airplanes -0539 thru -0580) 

1 Left Trailing Link (Part Number 6541516-1)- Replace every 9800 landings. 

~ Right Trailing Link (Part Number 6541516-2) - Replace every 9800 landings. 

(d) Trailing Link Assembly (Airplanes -0581 and On) 

1 Left Trailing Link (Part Number 6541516-3, -5) - Replace every 25,000 landings. 

~ Right Trailing Link (Part Number 6541516-4, -6)- Replace every 25,000 landings. 

(e) Oleo Assembly (Part Number 6541520-2, -3, -4, -5)- Replace every 31 ,900 landings, 

except for the part that follows: 

1 Outer Bearing Assembly (Part Number 6541425-6, -13, -15)- Replace every 21,800 

landings. 

(f) Left Side Brace Actuator (Part Number 9912569-1, -3) - Replace every 50,100 landings. 

(g) Right Side Brace Actuator (Part Number 9912569-2, -4)- Replace every 50,100 landings. 

(9) Main Landing Gear (Airplanes -0539 thru -0750 Incorporating SB560-32-40) 

NOTE: Attaching hardware (bolts, bearings, bushings, trunnion pins, and trunnion/link pin 

associated with the installation of the components below) is to be replaced whenever 

the associated component is replaced. Refer to Chapter 32, Main Gear and Doors -

Removal/Installation for more information. 

(a) Left Trunnion Machining (Part Number 6541561-1, 6594021-1)- Replace every 42,1 00 

landings. 

(b) Right Trunnion Machining (Part Number 6541561-2, 6594021-2) - Replace every 42,100 

landings. 

(c) Trailing Link Assembly (Airplanes -0539 thru -0580) 

1 Left Trailing Link (Part Number 6541516-1, -3, -5) - Replace every 8526 landings. 

© Cessna Aircraft Company 

4-11-02 Page 3 

Jun 23/2014 
CESSNA AIRCRAFT COMPANY 

MODEL 560 

MAINTENANCE MANUAL 

(c) Nose Landing Gear Trunnion Support, Right (Part Number 6613056-4, 6) - Replace every 

11 ,233 landings. 

(5) Airplanes -0751 and On 

(a) Nose Landing Gear Actuator Fitting (Part Number6511105-1 , -200)- Replace every 21 ,958 

landings. 

(b) Nose Landing Gear Trunnion Support, Left (Part Number 6613056-5, -201)- Replace every 

11,233 landings. 

(c) Nose Landing Gear Trunnion Support, Right (Part Number 6613056-6, -202) - Replace 

every 11 ,233 landings. 

E. Wings (Chapter 57). 

(1) Airplanes -0001 thru -0259 

(a) Main Landing Gear Trunnion Fitting Assembly, Forward Left (Part Number 6522057-5) -

Replace every 27,460 landings. 

(b) Main Landing Gear Trunnion Fitting Assembly, Forward Right (Part Number 6522057-6)-

Replace every 27,460 landings. 

(c) Main Landing Gear Trunnion Fitting Assembly, Aft (Part Number 5522710-15)- Replace 

every 27,460 landings. 

(d) Main Landing Gear Side Brace Support Fitting, Left (Part Number 6522047-1 , -7) - Replace 

every 28,080 landings. 

(e) Main Landing Gear Side Brace Support Fitting, Right (Part Number 6522047-2, -8) -

Replace every 28,080 landings. 

(2) Airplanes -0260 thru -0538 

(a) Main Landing Gear Trunnion Fitting Assembly, Forward Left (Part Number 6522057-5) -

Replace every 22,900 landings. 

(b) Main Landing Gear Trunnion Fitting Assembly, Forward Right (Part Number 6522057-6)-

Replace every 22,900 landings. 

(c) Main Landing Gear Trunnion Fitting Assembly, Aft (Part Number 5522710-15) - Replace 

every 22,900 landings. 

(d) Main Landing Gear Side Brace Support Fitting, Left (Part Number 6522047-1 , -7)- Replace 

every 24,700 landings. 

(e) Main Landing Gear Side Brace Support Fitting, Right (Part Number 6522047-2, -8) -

Replace every 24,700 landings. 

(3) Airplanes (Airplanes -0539 thru -0750 Not Incorporating SB560-32-40) 

(a) Left Aft Trunnion Attach Fitting (Part Number 6522634-5, -201) - Replace every 23.900 

landings. 

(b) Right Aft Trunnion Attach Fitting (Part Number 6522634-6, -202) - Replace every 23,900 

landings. 

(c) Left Forward Trunnion Attach Fitting (Part Number 6522640-1 . -201) - Replace every 

23,900 landings. 

(d) Right Forward Trunnion Attach Fitting (Part Number 6522640-2, -202) - Replace every 

23,900 landings. 

(e) Left Side Brace Support Fitting (Part Number 6521525-1, -201)- Replace every 50,100 

landings. 

(f) Right Side Brace Support Fitting (Part Number 6521525-2, -202) - Replace every 50,100 

landings. 

(4) Airplanes (Airplanes -0539 thru -0750 Incorporating SB560-32-40) 

(a) Left Aft Trunnion Attach Fitting (Part Number 6522634-5, -201) - Replace every 23,900 

landings. 

(b) Right Aft Trunnion Attach Fitting (Part Number 6522634-6, -202) - Replace every 23,900 

landings. 

(c) Left Forward Trunnion Attach Fitting (Part Number 6522640-1 , -201) - Replace every 

23,900 landings. 

(d) Right Forward Trunnion Attach Fitting (Part Number 6522640-2, -202) - Replace every 

23,900 landings. 

(e) Left Side Brace Support Fitting (Part Number 6521525-1 , -201)- Replace every 42,100 

landings. 

© Cessna Aircraft Company 

4-11-02 PageS 

Jun 23/2014