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C I R R U S A I R P L A N E M A I N T E N A N C E M A N U A L M O D E L S R 2 2
EFFECTIVITY:
PROGRESSIVE INSPECTION PROGRAM
1. DESCRIPTION
The Cirrus Design Progressive Inspection Program is designed to meet Federal Aviation Requirements Parts 43.15 and 91.409. This program was developed to maximize integrity and safety for aircraft with annual expected usage rates in excess of 400 hours. Airplanes operating less than 400 hour annual usage may also utilize this program, if desired.
The Progressive Inspection Program provides for the complete inspection of a specific aircraft utilizing a five-phase cyclical inspection program.
An inspection is accomplished every 50 hours of time in service (+/-10 hours). At the completion of the 400 hour phase inspection, the program will accomplish a full Inspection of the aircraft, constituting an Annual Inspection. If 400 hours are not flown within 12 calendar months from program start, all remaining Phase Inspections must be completed to retain the aircraft within the parameters of the program, and within the guidelines of 14 CFR 91.409.
A. Eligibility
Cirrus Design SR22 airplanes with serial numbers 0002 and subsequent are eligible for the Progres-sive Inspection Program. Eligible airplanes must meet one of the following conditions:
• The airplane must have less than 50 hours total time in service, calendar time remaining within the Annual Inspection period, and comply with all applicable Airworthiness Directives, Special Inspec-tion Requirements, and Mandatory Service Bulletins before initiating the Progressive Inspection Program.
• Airplanes with more than 50 hours time in service must complete an Annual Inspection and com-ply with all applicable Airworthiness Directives, Special Inspection Requirements, and Mandatory Service Bulletins before initiating the Progressive Inspection Program.
B. Initiating the Progressive Inspection Program
To initiate the Progressive Inspection Program, the owner or operator must:
• United States: Submit a letter of request and a copy of the Progressive Inspection Program for approval to the Flight Standards District Office having jurisdiction over the area in which the appli-cant is located. A certified mechanic holding an Inspection Authorization or an appropriately certi-fied Repair Station will be required to supervise or conduct the Progressive Inspection. Approval must be obtained before initiating this program.
• International: Submit the appropriate applications and a copy of the Progressive Inspection Pro-gram for approval to the government agency having jurisdiction over the area in which the appli-cant is located.
• Make an entry in the airplane maintenance records stating that airplane has been placed on the Progressive Inspection Program in accordance with 14 CFR 91.409 (d), noting the airplane total time in service and date.
Note: A sample Letter of Request is provided on the following pages. Contact Cirrus Design Customer Service Department to obtain hardcopy at 218.788.3000 or visit our website at cirrusdesign.com to download a pdf version. (See Figure 05-211)
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EFFECTIVITY:
C. Conducting the Progressive Inspection Program
• Pre-Inspection:
(a) Review airplane inspection records and maintenance history.(b) Determine which Phase Inspection is due.(c) Note any discrepancies indicated by owner or operator.(d) Determine and comply with any FAA Airworthiness Directives. Ensure required compli-
ance will not become due prior to the next scheduled inspection and contrary to the instructions contained within the directive.
(e) Inspect airplane records to determine hourly and calendar replacement times for compo-nents and expendable filters.
• Complete the applicable Phase Inspection:
The Progressive Inspection Program provides a checklist for each Phase Inspection and is used in conjunction with the Cirrus Design Airplane Maintenance Manual, Illustrated Parts Catalog, and all other applicable manufactures and vendor maintenance, service manuals, and bulletins. Each Phase Inspection outlines Routine and Detailed maintenance/inspection tasks. These tasks are numbered in sequence and must be performed in sequence. Each Phase Inspection form must be completed in full.
(f) Each Phase Inspection begins with the Airplane Operational and Functional Check (Refer to 05-30). This check allows for the operational check of essential airplane systems. Any defects found during the operational check should be noted and addressed before return-ing the airplane to service.
(g) Perform the specified Routine and Detailed Inspections. Complete each Phase Inspection form in full.1 Routine Inspections are regular procedures generally consisting of a Visual or Oper-
ational Inspection of the airplane, component, or system.2 Detailed Inspections are comprehensive examinations or Functional Inspections of
the airplane, component, or system. Disassembly is required as necessary to gain access for the inspection of assemblies and related sub-assemblies.
(h) Each Phase Inspection ends with a Airplane Operational and Functional Check and a Post Run-Up Inspection. These inspections allow for the operational check of essential airplane systems, leak checks, and status verification of Airworthiness Directives, Service Bulle-tins, and airplane documents.
(i) In the airplane maintenance records:1 Enter date of inspection and airplane total time.2 Enter type of inspection accomplished.
Note: Inspection must be completed by a certified mechanic holding an Inspector Authorized (IA) or a Certified Repair Station.
3 Enter the signature, certificate number, and kind of certificate held by the mainte-nance Facility/Inspector.
4 Enter the following or similarly worded statement:“I certify that in accordance with a Progressive Inspection Program a Routine Inspection of (identify whether airplane or components) and a Detailed Inspection of (identify components) were performed and the (airplane or components) are (approved/disapproved) for return to service”.
If disapproved, the entry will further state “a list of discrepancies and un-airworthy items dated (date) has been provided to the owner/operator”.
C I R R U S A I R P L A N E M A I N T E N A N C E M A N U A L M O D E L S R 2 2
EFFECTIVITY:
5 Enter the hours when next inspection will be due.Example:
“Next Phase Inspection due at 526.25 time in service”.
(j) At the conclusion of the Phase-II 400 Hour Inspection repeat the program starting with the Phase-I 50 Hour Inspection.
D. Canceling the Progressive Inspection Program
• The owner or operator must notify the local Flight Standards District Office in writing before discon-tinuing the Progressive Inspection Program.
• After discontinuance, the first Annual Inspection will be due within 12 calendar months after com-pletion of the Phase-II 400 Hour Inspection. The 100 Hour inspection will be due within 100 hours of the Phase-II 400 Hour Inspection.
E. Airplanes Away From Normal Base Of Operation
If airplane is away from base of operation where inspections are normally conducted, a certified tech-nician holding an Inspection Authorization or appropriately certified Repair Station may perform inspection.
The inspection will be completed in appropriate sequence and in accordance with procedures and forms of technician who would normally perform the inspection. Electronic transmittal is acceptable means of communicating procedures and forms from normal base of operation to technician perform-ing inspection.
2. INSPECTION GROUPS AND CRITERIA
Note: Supplemental Type Certified and/or other field installed equipment is not applicable to the Cirrus Design Progressive Inspection Program. Applicable items are required to be inspected in accordance with the manufacturer’s approved Instructions For Continued Air-worthiness.
All references to “5-20” under the Chap-Sect column are to be understood as reference to Visual Inspection criteria defined under Inspection Groups and Criteria in Chapter 5, “Scheduled Maintenance Checks”. (Refer to 05-20)
A. Inspection Intervals (See Figure 05-212)
• Phase I Inspection is accomplished after 50 hours of operation. Phase I Inspection is a Routine Inspection of the Engine, Landing Gear, and Ice Protection Groups, and a Detailed Inspection of the Avionics Group.
• Phase II Inspection is accomplished after 100, 200, 300, and 400 hours of operation. Phase II Inspection is a Routine Inspection of the Landing Gear Group and a Detailed Inspection of the Engine and Propeller Groups.
• Phase III Inspection is accomplished after 150 hours of operation. Phase III Inspection is a Routine Inspection of the Engine, Ice Protection, and Air Conditioning Groups and a Detailed Inspection of the Landing Gear Group.
• Phase IV Inspection is accomplished after 250 hours of operation. Phase IV Inspection is a Rou-tine Inspection of the Engine, Landing Gear, Ice Protection, and Avionics Groups and a Detailed Inspection of the Airframe Exterior and CAPS Groups.
• Phase V Inspection is accomplished after 350 hours of operation. Phase V Inspection is a Routine Inspection of the Engine and Landing Gear Groups and a Detailed Inspection of the Ice Protection, Air Conditioning, and Flight Controls and Below Floor Groups.
• At the conclusion of the Phase II, 400 Hour Inspection, repeat the program starting with the Phase I, 50 Hour Inspection.
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EFFECTIVITY:
Figure 05-211Sample Letter of Request
Cirrus Design Progressive Inspection ProgramLetter of Request
Submitted To: Federal Aviation Administration
Flight Standards District Office Date: _________________________
City, State, Zip: _________________________________________________________________________
Contact Name: _______________________ Phone:__________________ Fax: ________________________________________________________________________________________________________
In accordance with FAR 91.409 (d), the undersigned desire to use and request acceptance of the CirrusDesign Progressive Inspection Program for use as an Approved Aircraft Inspection Program. The subjectfacility has appropriate housing, equipment, and technical information for the necessary disassembly andproper inspection of the aircraft.______________________________________________________________________________________
Certificated Mechanic with Inspection Authorization:
Name: ___________________________________________ Certificate No.: ________________________
Certificated Airframe Repair Station:
Name: ___________________________________________ Certificate No.: ______________________________________________________________________________________________________________
The aircraft qualifies to begin the Progressive Inspection Program because:
___ it is a new aircraft with less than 50 hours time in service.
Date of Original Airworthiness Certificate ______________________________________________
Total Time in Service to Date ______________________________________________
___ an Annual Inspection was completed less than 50 hours ago.
Date of Annual ______________________________________________
Total Time in Service at Annual ______________________________________________
Total Time in Service to Date ____________________________________________________________________________________________________________________________________
Aircraft Registration Number: _________________________ Aircraft Model: _____________________
Aircraft Serial Number: ______________________________ Engine Model: _____________________
Engine Serial Number: ______________________________ Propeller Model: ____________________
Propeller Serial Number: __________________________________________________________________________________________________________________
Registered Owners Name: ________________________________________________________________
City, State, Zip: _________________________________________________________________________
Contact Name: _______________________ Phone: ________________ Fax: ______________________________________________________________________________________________________
Operator Name: ________________________________________________________________________
City, State, Zip: _________________________________________________________________________
Contact Name: _______________________ Phone: ________________ Fax: ______________________________________________________________________________________________________
Service Facility Name: ___________________________________________________________________
City, State, Zip: _________________________________________________________________________
Contact Name: _______________________ Phone: ________________ Fax: ______________________________________________________________________________________________________
Signatures:
___________________________ __________________________ __________________________
Registered Owner Operator Service Facility
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EFFECTIVITY:
Figure 05-212Progressive Phase Inspection Intervals
Hour Phase I Phase II Phase III Phase IV Phase V Complete
50 X
100 X
150 X
200 X
250 X
300 X
350 X
400 X
450 X
500 X
550 X
600 X
650 X
700 X
750 X
800 X
850 X
900 X
950 X
1000 X
1050 X
1100 X
1150 X
1200 X
1250 X
1300 X
1350 X
1400 X
1450 X
1500 X
1550 X
1600 X
1650 X
1700 X
1750 X
1800 X
1850 X
1900 X
1950 X
2000 X
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EFFECTIVITY:
Phase I - 50 Hour InspectionProgressive Inspection Report
MakeCirrus Design
ModelSR22
Serial Number Registration Number
Owner Date
Inspector Name Operating Time
Phase Inspection Criteria Reference Date Initl
1. Perform Pre-Inspection. Page 11, Pre-Inspection Inspection Crite-ria
2. Perform Airplane Operational and Functional Check.
(Refer to 05-30)
3. Perform Routine Inspection - Engine Group. Page 12, Engine Group Routine Inspec-tion Criteria
4. Perform Routine Inspection - Landing Gear Group. Page 13, Landing Gear Group Routine Inspection Criteria
5. Perform Routine Inspection - Ice Protection. Page 14, Ice Protection Group Routine Inspection Criteria
6. Perform Detailed Inspection - Avionics Group. Page 21, Avionics Group Detailed Inspec-tion Criteria
7. Perform Airplane Operational and Functional Check.
(Refer to 05-30)
8. Perform Post Run-Up Inspection. Page 33, Post Run-Up Inspection Inspec-tion Criteria
Signature of Mechanic or Inspector Not required per 14 CFR § 43.11.
Certificate Number
C I R R U S A I R P L A N E M A I N T E N A N C E M A N U A L M O D E L S R 2 2
EFFECTIVITY:
Phase II - 100, 200, 300, 400 Hour InspectionProgressive Inspection Report
MakeCirrus Design
ModelSR22
Serial Number Registration Number
Owner Date
Inspector Name Operating Time
Phase Inspection Criteria Reference Date Initl
1. Perform Pre-Inspection. Page 11, Pre-Inspection Inspection Crite-ria
2. Perform Airplane Operational and Functional Check.
(Refer to 05-30)
3. Perform Routine Inspection - Landing Gear Group. Page 13, Landing Gear Group Routine Inspection Criteria
4. Perform Detailed Inspection - Engine Group. Page 17, Engine Group Detailed Inspec-tion Criteria
5. Perform Detailed Inspection - Propeller Group. Page 20, Propeller Group Detailed Inspection Criteria
6. Perform Airplane Operational and Functional Check.
(Refer to 05-30)
7. Perform Post Run-Up Inspection. Page 33, Post Run-Up Inspection Inspec-tion Criteria
Signature of Mechanic or Inspector Not required per 14 CFR § 43.11.
Certificate Number
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EFFECTIVITY:
Phase III - 150 Hour InspectionProgressive Inspection Report
MakeCirrus Design
ModelSR22
Serial Number Registration Number
Owner Date
Inspector Name Operating Time
Phase Inspection Criteria Reference Date Initl
1. Perform Pre-Inspection. Page 11, Pre-Inspection Inspection Crite-ria
2. Perform Airplane Operational and Functional Check.
(Refer to 05-30)
3. Perform Routine Inspection - Engine Group. Page 12, Engine Group Routine Inspec-tion Criteria
4. Perform Routine Inspection - Ice Protection Group. Page 14, Ice Protection Group Routine Inspection Criteria
5. Perform Detailed Inspection - Landing Gear Group. Page 22, Landing Gear Group Detailed Inspection Criteria
6. Perform Routine Inspection - Air Conditioning Group
Page 16, Air Conditioning Group Routine Inspection Criteria
7. Perform Airplane Operational and Functional Check.
(Refer to 05-30)
8. Perform Post Run-Up Inspection. Page 33, Post Run-Up Inspection Inspec-tion Criteria
Signature of Mechanic or Inspector Not required per 14 CFR § 43.11.
Certificate Number
C I R R U S A I R P L A N E M A I N T E N A N C E M A N U A L M O D E L S R 2 2
EFFECTIVITY:
Phase IV - 250 Hour InspectionProgressive Inspection Report
MakeCirrus Design
ModelSR22
Serial Number Registration Number
Owner Date
Inspector Name Operating Time
Phase Inspection Criteria Reference Date Initl
1. Perform Pre-Inspection. Page 11, Pre-Inspection Inspection Crite-ria
2. Perform Airplane Operational and Functional Check.
(Refer to 05-30)
3. Perform Routine Inspection - Engine Group. Page 12, Engine Group Routine Inspec-tion Criteria
4. Perform Routine Inspection - Landing Gear Group. Page 13, Landing Gear Group Routine Inspection Criteria
5. Perform Routine Inspection - Ice Protection Group. Page 14, Ice Protection Group Routine Inspection Criteria
6. Perform Routine Inspection - Avionics Group. Page 15, Avionics Group Routine Inspec-tion Criteria
7. Perform Detailed Inspection - Airframe Exterior Group.
Page 24, Airframe Exterior Group Detailed Inspection Criteria
8. Perform Detailed Inspection - CAPS Group. Page 26, CAPS Group Detailed Inspec-tion Criteria
9. Perform Airplane Operational and Functional Check.
(Refer to 05-30)
10. Perform Post Run-Up Inspection. Page 33, Post Run-Up Inspection Inspec-tion Criteria
Signature of Mechanic or Inspector Not required per 14 CFR § 43.11.
Certificate Number
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EFFECTIVITY:
Phase V - 350 Hour InspectionProgressive Inspection Report
MakeCirrus Design
ModelSR22
Serial Number Registration Number
Owner Date
Inspector Name Operating Time
Phase Inspection Criteria Reference Date Initl
1. Perform Pre-Inspection. Page 11, Pre-Inspection Inspection Crite-ria
2. Perform Airplane Operational and Functional Check.
(Refer to 05-30)
3. Perform Routine Inspection - Engine Group. Page 12, Engine Group Routine Inspec-tion Criteria
4. Perform Routine Inspection - Landing Gear Group. Page 13, Landing Gear Group Routine Inspection Criteria
5. Perform Detailed Inspection - Flight Controls and Below Floor Group.
Page 27, Flight Controls and Below Floor Group Detailed Inspection Criteria
6. Perform Detailed Inspection - Ice Protection Group. Page 30, Ice Protection Group Detailed Inspection Criteria
7. Perform Detailed Inspection - Air Conditioning Group
Page 32, Air Conditioning Group Detailed Inspection Criteria
8. Perform Airplane Operational and Functional Check.
(Refer to 05-30)
9. Perform Post Run-Up Inspection. Page 33, Post Run-Up Inspection Inspec-tion Criteria
Signature of Mechanic or Inspector Not required per 14 CFR § 43.11.
Certificate Number
C I R R U S A I R P L A N E M A I N T E N A N C E M A N U A L M O D E L S R 2 2
EFFECTIVITY:
Pre-InspectionInspection Criteria
Chap-Sect Reference
Initials
1. Review compliance status with current Federal Aviation Regulations. This includes inspection of the following: - Airplane Flight Manual - Aircraft Log Book - Registration Certificate - Weight and Balance Record - FAA Airworthiness Directives - Cirrus Design Service Documents
-
2. Airplane InteriorClean and vacuum.
12-20
3. Airplane ExteriorClean.
12-20
4. Engine and Engine CompartmentRemove engine cowling and clean.
71-1012-20
5. Engine Operational InspectionPerform an Engine Operational Inspection in accordance with the manufac-turer’s approved Instructions For Continued Airworthiness
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EFFECTIVITY:
Engine GroupRoutine Inspection Criteria
Chap-Sect Reference
Initials
1. Engine CowlingVisual Inspection for cracks, distortion, and loose or missing fasteners.
5-20
2. Engine CompartmentVisual Inspection for leaks.
5-20
3. Engine OilDrain and change.
12-10
4. Oil FilterPerform Inspection/Check - Oil Filter Particles.
12-10
5. MagnetosCheck and adjust only if non-conformities were noted during Operational and Functional Check in accordance with the manufacturer's approved service instructions.
6. Spark Plug Cable LeadsVisual Inspection for chafing, corrosion, and deposits.
5-20
7. Induction System FilterVisual Inspection for cleanliness.Replace when filter is more than 50% covered by foreign matter.
71-60
8. Gascolator Fuel Filter and BowlPerform Servicing - Gascolator
28-20
9. Exhaust SystemPerform Inspection/Check for cracks, dents, missing parts, security, and cor-rosion.
78-20
10. Propeller BladesVisual Inspection for nicks, bends, cracks, gouges, erosion, lightning strikes, and condition of tips.
5-20
11. HubVisual Inspection for cracks, corrosion, leaking oil or grease.
5-20
12. De-Ice Propeller BootVisual Inspection for condition and security.
5-20
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EFFECTIVITY:
Landing Gear GroupRoutine Inspection Criteria
Chap-Sect Reference
Initials
1. Remove Main Gear Fairings. 32-10
2. Remove Nose Gear Fairings. 32-20
3. WheelsRemove, Visual Inspection for condition, repack bearings every 100 hours.
32-41
4. WheelsVisual Inspection for cracks, corrosion, and broken bolts.
5-20
5. TiresVisual Inspection for cuts, uneven or excessive wear, and slippage.
5-20
6. TiresInspect for condition, and proper tire pressure.
12-10
7. Main Gear Strut, Attachments, and BoltsVisual Inspection for cracking, splintering, condition, and security.Verify lower strut fairing stand-off securely attached.
32-10
8. Nose Gear AssemblyPerform Inspection/Check - Nose Gear Assembly every 100 hours.
32-20
9. Nose Gear Fork and SpindleInspect fork assembly for cleanliness.Perform Adjustment/Test - Nose Wheel Fork Assembly.
32-20
10. Brake LiningsPerform Inspection/Check - Brake Linings.
32-42
11. Brake AssemblyPerform Inspection/Check - Brake Assembly.Replace O-rings every 100 hours.
32-42
12. Brake DiskVisual Inspection for corrosion, security, and general condition.
5-20
13. Flexible Brake LinesVisual Inspection for leaks, security, and condition.
5-20
14. Brake Fluid ReservoirInspect fluid level, and replenish.
12-10
15. Install Main Gear Fairings. 32-10
16. Install Nose Gear Fairings. 32-20
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EFFECTIVITY:
Ice Protection GroupRoutine Inspection Criteria
Chap-Sect Reference
Initials
1. Blade Feed TubePerform Inspection/Check - Blade Feed Tube Orientation.
30-60
2. Slinger Ring Feed TubePerform Inspection/Check - Slinger Ring Feed Tube Orientation.
30-60
3. Slinger RingPerform Operational Test - Slinger Ring Assembly.
30-60
4. Wing Porous PanelsPerform Operational Test - Wing Porous Panels.
30-10
5. Horizontal Stabilizer Porous PanelsPerform Operational Test - Horizontal Stabilizer Porous Panels.
30-10
6. Ice Protection SystemFill tank with approved de-ice fluid.
12-10
C I R R U S A I R P L A N E M A I N T E N A N C E M A N U A L M O D E L S R 2 2
EFFECTIVITY:
Avionics GroupRoutine Inspection Criteria
Chap-Sect Reference
Initials
1. MagnetometerPerform Functional Test - Magnetometer Calibration (24 month inspection).
34-20
2. AltimeterVisual and Functional Inspection for condition and calibration in accordance with 14 CFR 91.411.Perform Adjustment/Test - Altimeter (24 month inspection).
34-10
14 CFR91.411
3. TransponderVisual and Functional Inspection for condition and calibration in accordance with 14 CFR 91.413 (24 month inspection).
14 CFR 91.413
4. Emergency Locator TransmitterFunctional Inspection in accordance with 14 CFR 91.207.
14 CFR 91.207
5. AntennasVisual Inspection for condition and security.
5-20
6. Outside Air Temperature Gage/Clock Battery (24 month inspection)Replace.
34-10
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EFFECTIVITY:
Air Conditioning GroupRoutine Inspection Criteria
Chap-Sect Reference
Initials
1. Perform Operational Test - Air Conditioning System 21-50
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EFFECTIVITY:
Engine GroupDetailed Inspection Criteria
Chap-Sect Reference
Initials
1. Engine CowlingVisual Inspection for cracks, distortion, and loose or missing fasteners.
5-20
2. Engine OilDrain and change.
12-10
3. Oil ScreenRemove and perform Visual Inspection for metal particulates.
5-20
4. Oil Sump PlugVisual Inspection for condition.
5-20
5. Oil FilterPerform Inspection/Check - Oil Filter Particles.
12-10
6. Oil Lines and FittingsVisual Inspection for leaks, security, chafing, dents, and cracks.
5-20
7. Oil Cooler FinsClean and perform Visual Inspection for cracking, bending, and general con-dition.
5-20
8. BatteryPerform Electrolyte Level Check.
12-10
9. Battery Platform, Terminals, and CablesVisual Inspection for security, corrosion, and general condition.
12-10
10. WiringVisual Inspection for damaged wiring and clamps.
5-20
11. Engine CompressionFunctional Inspection in accordance with the manufacturer’s approved Instructions For Continued Airworthiness.
12. Spark PlugsInspect, clean, re-gap and rotate in accordance with the manufacturer’s approved Instructions For Continued Airworthiness.
13. Spark Plug Cable LeadsVisual Inspection for chafing, corrosion, and deposits.
5-20
14. Cylinder Cooling FinsVisual Inspection for cracking, bending, and general condition.
5-20
15. Engine Baffling and SealsVisual Inspection for cracks, tears, and rips.
5-20
16. Ignition HarnessInspect for high tension leaks and continuity in accordance with the manufac-turer’s approved Instructions For Continued Airworthiness.
Cyl # 1 3 5 2 4 6
P.S.I.
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EFFECTIVITY:
17. MagnetoFunctional Inspect magneto to engine timing in accordance with the manu-facturer’s approved Instructions For Continued Airworthiness. Internal Inspection every 500 hours.Verify Airworthiness Directive status.Replace or overhaul every 4 years since new or last overhaul.
18. Induction System FilterReplace at 200 hours, or when filter is more than 50% covered by foreign material.
71-60
19. Air Intake DuctsVisual Inspection for general condition.
5-20
20. Alternate Air DoorCheck operation of alternate air flapper valve.
71-60
21. Fuel PumpVisual Inspection for leaks, security, and condition.
5-20
22. Fuel Injection NozzlesVisual Inspect nozzles and manifold valve for fuel stains, security, and proper venting.Every 300 hours and at first 100 Hour Inspection on new, rebuilt, or over-hauled engine, remove and clean fuel injection nozzles in accordance with the manufacturer’s approved Instructions For Continued Airworthiness.
5-20
23. Gascolator Fuel Filter and BowlPerform Servicing - Gascolator
28-20
24. Flexible Fuel LinesVisual Inspection for leaks, security, and condition.
5-20
25. Throttle, Propeller, and Mixture Control CableVisual Inspection for security and condition of cotter pins, castellated nuts, and oversized washers.
5-20
26. Exhaust SystemPerform Inspection/Check for cracks, dents, missing parts, security, and cor-rosion.
78-20
27. Exhaust SystemPerform Inspection/Check for spring compression.
78-20
28. Exhaust Muffler/Heat ExchangerPerform Inspection/Check for condition, security, and leakage.
78-20
29. Cabin Heat DuctsVisual Inspection for soot, distortion, and general condition.
5-20
30. Breather TubeVisual Inspection for obstructions and security.
5-20
31. CrankcaseVisual Inspection for condition, leaks, and loose components.
5-20
Engine GroupDetailed Inspection Criteria (Continued)
Chap-Sect Reference
Initials
C I R R U S A I R P L A N E M A I N T E N A N C E M A N U A L M O D E L S R 2 2
EFFECTIVITY:
32. Engine Mount WeldmentVisual Inspection for weld cracks, corrosion, bending, and distortion.
5-20
33. Engine Mount Weldment and Lower Mount Attach FittingsAt first Annual Inspection, every 500 Hrs, and after engine install, perform Visual Inspection for security. Verify torque.
5-20
34. Engine Mount IsolatorsVisual Inspection for cracking, splitting, and general condition.
5-20
35. Firewall and SealsVisual Inspection for cracks, condition, and security of attachments.
5-20
36. AlternatorsVisual Inspection for security and condition.
5-20
37. Alternator 1Remove, disassemble, inspect, repair and test in accordance with the manu-facturer’s approved Instructions For Continued Airworthiness every 500 hours.
38. Alternator 2Perform Inspection/Check - Alternator 2Refer to Overhaul and Replacement Schedule.
24-30
05-10
39. StarterVisual Inspection for security and condition.
5-20
40. Master Control UnitPerform Inspection/Check - Master Control Unit.
24-30
41. Brake Fluid ReservoirReplenish.
12-10
42. Engine CompartmentVisual Inspection for loose nuts, bolts, screws, and parts.
5-20
43. Fuel Injection SystemFunctional Inspection of Fuel Injection System in accordance with the manu-facturer’s approved Instructions For Continued Airworthiness after engine installation, every 100 hours, or fuel system component replacement.
44. Air Conditioning CompressorAdjustment/Test - Compressor Drive Belt Tensioning
21-50
Engine GroupDetailed Inspection Criteria (Continued)
Chap-Sect Reference
Initials
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EFFECTIVITY:
Propeller GroupDetailed Inspection Criteria
Chap-Sect Reference
Initials
1. SpinnerRemove, clean and perform Visual Inspection for cracks and corrosion.
5-20
2. Spinner Backing PlateVisual Inspection for condition.
5-20
3. BladesVisual Inspection for nicks, bends, cracks, gouges, erosion, lightning strikes, and condition of tips.
5-20
4. BladesInspect blades for radial play or movement of blade tip.
61-10
5. BladesInspect blade tracking.
61-10
6. Propeller Assembly - Serials 0002 & subs w/ Hartzell PropellerLubricate in accordance with the manufacturer’s approved Instructions For Continued Airworthiness.
7. HubVisual Inspection for cracks, corrosion, leaking oil or grease.
5-20
8. GovernorVisual Inspection for oil leaks.
5-20
9. Slinger Ring AssemblyPerform Operational Check - Slinger Ring Assembly.
30-60
10. De-Ice Propeller BootVisual Inspection for condition and security.
5-20
C I R R U S A I R P L A N E M A I N T E N A N C E M A N U A L M O D E L S R 2 2
EFFECTIVITY:
Avionics GroupDetailed Inspection Criteria
Chap-Sect Reference
Initials
1. Remove Glareshield. 25-10
2. Remove MFD. 31-60
3. Remove Co-Pilots Seat. 25-10
4. Remove RH Bolster Trim. 25-10
5. Remove Center Bolster Trim. 25-10
6. Remove Access Panels CF5 and CB6. 06-00
7. Remove SKYWATCH Cover below co-pilot seat, if installed. 34-40
8. AvionicsVisual Inspection of components, wiring, and for security.
5-20
9. Radio and Electronic EquipmentVisual Inspection for proper installation, clearance, and security.
5-20
10. WiringVisual Inspection for proper clearance, chafing, fraying, and routing.
5-20
11. Bonding and ShieldingVisual Inspection for proper installation and condition.
5-20
12. Antennas Visual Inspection for condition and security.
5-20
13. Install Glareshield. 25-10
14. Install MFD. 31-60
15. Install RH Bolster Trim. 25-10
16. Install Center Bolster Trim. 25-10
17. Install Access Panels CF5 and CB6. 06-00
18. Install SKYWATCH Cover below co-pilot seat, if installed. 34-40
19. Install Co-Pilots Seat. 25-10
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EFFECTIVITY:
Landing Gear GroupDetailed Inspection Criteria
Chap-Sect Reference
Initials
1. Main Wheel FairingsRemove, clean and perform Visual Inspection on fairings and anti-chafe spacers for cracking, rubbing, and general condition.
5-20
2. Nose Wheel FairingsRemove, clean and perform Visual Inspection on fairings for cracking, rub-bing, and general condition.
5-20
3. TiresVisual Inspection for cuts, uneven or excessive wear, and slippage.
5-20
4. TiresInspect for proper tire pressure.
12-10
5. Brake SystemCheck system for proper operation.
5-20
6. Brake LiningsPerform Inspection/Check - Brake Linings.
32-42
7. Brake AssemblyPerform Inspection/Check - Brake Assembly.Replace O-rings every 100 hours.
32-42
8. Brake DiskVisual Inspection for corrosion, security, and general condition.
5-20
9. Brake Lines and HosesVisual inspection for leaks, chafing, security, and condition.
5-20
10. WheelsRemove, Visual Inspection for condition, repack bearings every 100 hours.
32-41
11. WheelsVisual Inspection for cracks, corrosion, and broken bolts.
5-20
12. Polymer Shock Absorbing Pucks, Puck Tray, and Attach BoltsVisual Inspection of pucks for cracking or splitting. Ensure attach bolts are perpendicular to puck tray and puck stack-up is in alignment.
5-20
13. Nose Gear AssemblyPerform Inspection/Check - Nose Gear Assembly every 100 hours.
32-20
14. Nose Gear Fork and SpindleInspect fork assembly for cleanliness.Perform Adjustment/Test - Nose Wheel Fork Assembly.
32-20
15. Main Gear AssemblyVisual Inspection for condition.
5-20
16. Flexible Brake LinesVisual Inspection for leaks, security, and condition.
5-20
17. Parking Brake Valve and Control Cable LinkageVisual Inspection for leaks, security, chafing, and condition.
5-20
C I R R U S A I R P L A N E M A I N T E N A N C E M A N U A L M O D E L S R 2 2
EFFECTIVITY:
18. Brake Master CylindersVisual Inspection for leaks and security.
5-20
19. Main Gear Strut, Attachments, and BoltsVisual Inspection for cracking, splintering, condition, and security.Verify lower strut fairing stand-off securely attached.
32-10
Landing Gear GroupDetailed Inspection Criteria (Continued)
Chap-Sect Reference
Initials
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EFFECTIVITY:
Airframe Exterior GroupDetailed Inspection Criteria
Chap-Sect Reference
Initials
1. SkinVisual Inspection for general condition, deterioration, delamination, distor-tion, cracks, paint condition, and other evidence of failure.
5-20
2. Vertical Stabilizer and Rudder SurfacesVisual Inspection for distortion, and condition.
5-20
3. Wing TipsRemove and Visual Inspection for cracking and general condition.
57-20
4. Wing Leading Edge and Stall StripsVisual Inspection for foreign matter and debris.
5-20
5. WalkwayVisual Inspection for condition.
5-20
6. Fuel Tank VentsVisual Inspection for condition and obstruction.
5-20
7. Fuel CapPerform Functional Test - Fuel Cap Assembly.
28-10
8. Cabin Doors and Strike PlatesVisual Inspection for damage, operation, and security.
5-20
9. Door LatchesCheck operation of door latch mechanism.
5-20
10. Door Latches and HingesLubricate.
12-20
11. Cabin Windows and WindshieldClean and Visual Inspection for cracking, crazing, and general condition.
5-20
12. UpholsteryVisual Inspection for tears and fraying.
5-20
13. Seats, Seat Belts, and HarnessesPerform Inspection/Check - Crew Seats.Perform Inspection/Check - Crew Seat Harness.Perform Inspection/Check - Rear Seat Harness.
25-10
25-1025-10
14. Seat Belt Inertia ReelsVisual Inspection for security of brackets and bolts.
5-20
15. Seat Rails and SlidesVisual Inspection for condition and lubricate.
12-20
16. Fuel SelectorVisual Inspection for operation.
5-20
17. Strobe, Landing, Navigation, Recognition, Cabin, and Instrument LightsVisual Inspection for condition.Perform Operational Inspection.
5-20
18. Knobs, Switches, and LeversVisual Inspection for security, attachment and operation.
5-20
C I R R U S A I R P L A N E M A I N T E N A N C E M A N U A L M O D E L S R 2 2
EFFECTIVITY:
19. Cabin Heater ControlsCheck operation for freedom of movement.
5-20
20. Fresh Air Outlets and Heat OutletsVisual Inspection for condition and obstruction or blockage.
5-20
21. Fuselage Drainage HolesVisual Inspection for obstructions or blockage.
5-20
22. Placards and Instrument MarkingsVisual Inspection for conformity, security, and condition.
11-30
23. Fire ExtinguisherPerform Inspection/Check for condition and weigh.
26-20
24. Circuit BreakersPerform Functional Check - Redundant Circuit Breakers
24-50
25. Cabin Air Control AssemblyPerform Inspection/Check - Cabin Air Control Assembly every 500 hours or 5 years.
21-60
Airframe Exterior GroupDetailed Inspection Criteria (Continued)
Chap-Sect Reference
Initials
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EFFECTIVITY:
CAPS GroupDetailed Inspection Criteria
Chap-Sect Reference
Initials
1. CAPS Exit CoverVisual Inspection of perimeter for cracking or crazing, and placard condition.
5-20
2. CAPS Parachute CompartmentVisual Inspection for security, leaks and general condition.
5-20
3. CAPS Activation Handle Mount and CableVisual Inspection security, chafing, and wear.
5-20
C I R R U S A I R P L A N E M A I N T E N A N C E M A N U A L M O D E L S R 2 2
EFFECTIVITY:
Flight Controls and Below Floor GroupDetailed Inspection Criteria
Chap-Sect Reference
Initials
1. Remove Seats. 25-10
2. Remove Glareshield. 25-10
3. Remove MFD. 31-60
4. Remove Carpet. 25-10
5. Remove Cabin Floor Access Panels. 06-00
6. Remove Kickplates. 25-10
7. Remove RH Mid-Console Trim. 25-10
8. Remove Empennage Access Panels LE1, RE1, RE2, RE3, if installed. 06-00
9. Lower Flaps.
10. Remove LH Aileron. 57-50
11. Remove Wing Access Panels LW1, LW2, LW4, LW5, LW6, LW7, LW8, LW9, LW12, LW13, LW14, LW15, LW16, and RW1, RW2, RW4, RW5, RW6, RW7, RW8, RW9, RW12, RW13, RW14, RW16.
06-00
12. Rudder System RiggingPerform Inspection/Check - Rudder System Rigging
27-20
13. Rudder Bearings, Hinges, Horn, and AttachmentsVisual Inspection for security, condition, and freedom of movement.
5-20
14. Rudder SystemOperational Inspection for travel and freedom of movement.
5-20
15. Horizontal Stabilizer and Elevator SurfacesVisual Inspection for distortion, and condition.Verify integrity and security of inspection hole covers.
5-20
16. Horizontal Stabilizer Access PanelsVisual Inspection for condition and security.
5-20
17. Horizontal Stabilizer to Fuselage BondlineVisual Inspection for cracks.
5-20
18. Elevator System RiggingPerform Inspection/Check - Elevator System Rigging
27-30
19. Elevator Pitch Trim Cartridge - Serials 0002 thru 0754Perform Servicing - Pitch Trim Cartridge Lubrication.
27-30
20. Elevator Bearings, Hinges, Horn, and AttachmentsVisual Inspection for wear, condition, and freedom of movement.
5-20
21. Elevator SystemOperational Check for travel and freedom of movement.
5-20
22. Aft Wing Attach BracketVisual Inspection for corrosion. If corrosion evident, contact Cirrus Design for disposition. Reference 57-40 for access instructions.
5-20
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EFFECTIVITY:
23. Aileron SurfacesVisual Inspection for distortion, and condition.
5-20
24. Aileron System RiggingPerform Inspection/Check - Aileron System Rigging
27-10
25. Aileron Actuation ArmVisual Inspection for safetying, and condition.
5-20
26. Aileron Hinges, Hinge Bolts, Bearings, and AttachmentsVisual Inspection for security, freeplay, and binding.
5-20
27. Aileron SystemOperational Check for travel and freedom of movement.
5-20
28. Flap System RiggingPerform Inspection/Check- Flap System Rigging
27-50
29. Flap Hinges, Hinge Bolts, Bearings, and AttachmentsVisual Inspection for wear, security, freeplay, and binding.
5-20
30. Flap SystemPerform Operational Inspection of Flap System.Visual Inspection for condition of rub strips (if installed).
57-50
31. Fuel LinesVisual Inspection for chafing, obstruction, security, and general condition.
5-20
32. Stall Warning Water TrapDrain and perform Visual Inspection for condition.
5-20
33. Wing Air Ducts, Electrical Leads, Lines, and Attaching PartsVisual Inspection for security, routing, chafing, deterioration, wear, and cor-rect installation.
5-20
34. Pitot Mast and Static LinesVisual Inspection for security, condition, and obstruction.
5-20
35. Control QuadrantService in accordance with AMM.
76-10
36. Instrument PanelVisual Inspection for security of lines and wiring.
5-20
37. Control YokesVisual Inspection for excessive play, security, and proper operation.Verify no excessive freeplay in elevator or aileron input.
5-20
38. Rudder PedalsVisual Inspection for excessive play, security, and proper operation.Verify no excessive freeplay in rudder or aileron input.
5-20
39. Rudder Pedal Torque Tube BracketPerform Inspection/Check - Torque Tube Gap Tolerance.
27-20
Flight Controls and Below Floor GroupDetailed Inspection Criteria (Continued)
Chap-Sect Reference
Initials
C I R R U S A I R P L A N E M A I N T E N A N C E M A N U A L M O D E L S R 2 2
EFFECTIVITY:
40. Cabin Air Ducts, Electrical Leads, and Attaching PartsVisual Inspection for security, routing, chafing, deterioration, wear, and cor-rect installation.
5-20
41. Cable Attachments, Cables, and PulleysVisual Inspection for security, chafing, wear, and general condition.
5-20
42. Wing Attachment BoltsVisual Inspection for condition, fit, and evidence of distress.
5-20
43. Flap Actuation Motor and Attach BracketVisual inspection for condition and security.
5-20
44. Fuel Lines, Valves, and GagesVisual Inspection for chafing, obstruction, security, and general condition.
5-20
45. Pitot-Static System Water TrapDrain and perform Visual Inspection for condition.
5-20
46. Install MFD. 31-60
47. Install Glareshield. 25-10
48. Install Carpet. 25-10
49. Install Cabin Floor Access Panels. 06-00
50. Install Kickplates. 25-10
51. Install RH Mid-Console Trim. 25-10
52. Install Seats. 25-10
53. Install Empennage Access Panels LE1, RE1, RE2, RE3, if installed. 06-00
54. Raise Flaps.
55. Install LH Aileron. 57-50
56. Install Wing Access Panels LW1, LW2, LW4, LW5, LW6, LW7, LW8, LW9, LW12, LW13, LW14, LW15, LW16, and RW1, RW2, RW4, RW5, RW6, RW7, RW8, RW9, RW12, RW13, RW14, RW16.
06-00
Flight Controls and Below Floor GroupDetailed Inspection Criteria (Continued)
Chap-Sect Reference
Initials
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EFFECTIVITY:
Ice Protection GroupDetailed Inspection Criteria
Chap-Sect Reference
Initials
1. Remove LH passenger seat. 25-10
2. Remove copilot seat. 25-10
3. Serials 0002 thru 2437: Remove wing access panels LW6, LW16, RW6, RW16.
Serials 2438 & subs: Remove wing access panels LW4, LW9, RW4, RW9.
06-00
4. Remove cabin access panels CB6, CF2L, CF2R, and CF3L. 06-00
5. Remove LH rear trim covering de-icing fluid tank. 25-10
6. Remove engine cowling. 71-10
7. Remove propeller spinner. 61-10
8. Ice Protection FilterReplace every 2 years or 1200 hours whichever occurs first.
30-05
9. Ice Protection Fluid Tank, Filter, Metering Pump, Drain Block, and Drain ValveVisual Inspection for security and leaks.
5-20
10. Ice Protection Firewall Forward - Fluid Line, Bulkhead Fittings, Feeder Tube, Brackets, Clamps, and Proportioning Unit Visual Inspection for chafing, leaks, and security.
5-20
11. Ice Protection Proportioning Units and PlumbingVisual Inspection for chafing, leaks, security, and condition.
5-20
12. Blade Feed TubePerform Inspection/Check - Blade Feed Tube Orientation.
30-60
13. Slinger Ring Feed TubePerform Inspection/Check - Slinger Ring Feed Tube Orientation.
30-60
14. Slinger RingPerform Operational Test - Slinger Ring Assembly.
30-60
15. Wing Porous PanelsPerform Operational Test - Wing Porous Panels.
30-10
16. Horizontal Stabilizer Porous PanelsPerform Operational Test - Horizontal Stabilizer Porous Panels.
30-10
17. Ice Protection SystemFill tank with approved de-ice fluid.
12-10
18. Serials 0002 thru 2437: Install wing access panels LW6, LW16, RW6, RW16.
Serials 2438 & subs: Install wing access panels LW4, LW9, RW4, RW9.
06-00
19. Install cabin access panels CB6, CF2L, CF2R, and CF3L. 06-00
20. Install LH rear trim covering de-icing fluid tank. 25-10
21. Install LH passenger seat. 25-10
C I R R U S A I R P L A N E M A I N T E N A N C E M A N U A L M O D E L S R 2 2
EFFECTIVITY:
22. Install copilot seat. 25-10
23. Install engine cowling. 71-10
24. Install propeller spinner. 61-10
Ice Protection GroupDetailed Inspection Criteria (Continued)
Chap-Sect Reference
Initials
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EFFECTIVITY:
Air Conditioning GroupDetailed Inspection Criteria
Chap-Sect Reference
Initials
1. Remove engine cowling. 71-10
2. Remove glareshield. 25-10
3. Remove RH crew seat. 25-10
4. Remove RH sidewall air duct trim. 25-10
5. Remove RH rear cabin side trim. 25-10
6. Remove access panel CF5. 06-00
7. Air Conditioning CompressorPerform Inspection/Check - Compressor
21-50
8. Air Conditioning EvaporatorPerform Inspection/Check - Evaporator
21-50
9. Air Conditioning CondenserPerform Inspection/Check - Condenser
21-50
10. Air Conditioning Lines and HosesVisual Inspection for leaks, security, and condition.
5-20
11. Install access panel CF5. 06-00
12. Install RH rear cabin side trim. 25-10
13. Install RH sidewall air duct trim. 25-10
14. Install RH crew seat. 25-10
15. Install glareshield. 25-10
16. Install engine cowling. 71-10
C I R R U S A I R P L A N E M A I N T E N A N C E M A N U A L M O D E L S R 2 2
EFFECTIVITY:
Post Run-Up InspectionInspection Criteria
Chap-Sect Reference
Initials
1. Engine Operational InspectionPerform an Engine Operational Inspection in accordance with the manufac-turer’s approved Instructions For Continued Airworthiness.
2. Perform a “walk-around” Visual Inspection to detect fluid leaks or other abnor-malities.
05-30
3. Install engine cowling. 71-10
4. Check landing light operation. 33-40
5. Verify Airworthiness Directive compliance. 14 CFR 91.403
6. Review Cirrus Design service letters, bulletins, and instructions as applicable. 14 CFR 91.403
7. Verify airplane documents in proper order: - Airworthiness Certificate - Registration - Operating Handbook - Weight and Balance
14 CFR 91.203
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EFFECTIVITY:
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