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Aviation Regulation Part 91.409.
The Cirrus Design Progressive Inspection Program provides for the
complete inspection of the airplane utilizing a five-phase cyclic
inspection program. A total of eight inspections are accomplished over
the course of 400 flight hours, with an inspection occurring every 50
flight hours. The inspection items to be covered in the Progressive
Inspection are very similar to the Annual Inspection items. The
Progressive Inspection will accomplish a full Inspection of the airplane
at 400 flight hours or at 12 calendar months. The inspection is listed, in
detail, in Chapter 5 of the Aircraft Maintenance Manual.
June 2007
8-8 Information Manual
Section 8 Cirrus Design
Handling, Servicing, Maintenance SR22
Pilot Performed Preventative Maintenance
The holder of a Pilot Certificate issued under FAR Part 61 may
perform certain preventive maintenance described in FAR Part 43,
Appendix A. This maintenance may be performed only on an aircraft
that the pilot owns or operates and which is not used in air carrier
service. The regulation also stipulates that the pilot must also
complete the appropriate logbook entries. The following is a list of the
maintenance that the pilot may perform:
• Note •
The pilot should have the ability and manual procedures for
the work to be accomplished.
The pilot may not accomplish any work involving the removal
or disassembly of primary structure or operating system, or
interfere with an operating system, or affect the primary
structure.
• Remove, install, and repair tires.
• Clean, grease, or replace wheel bearings
• Replace defective safety wire or cotter pins.
• Lubrication not requiring disassembly other than removal of nonstructural
items such as access covers, cowlings, or fairings.
• Caution •
Do not use unapproved lubricants. Unapproved lubricants
may damage control system components, including but not
limited to engine and flight controls. Refer to the Airplane
Maintenance Manual for approved lubricants.
• Replenish hydraulic fluid in the hydraulic and brake reservoirs.
• Refinish the airplane interior or exterior (excluding balanced
control surfaces) with protective coatings.
• Repair interior upholstery and furnishings.
• Replace side windows.
• Replace bulbs, reflectors and lenses of position and landing lights.
• Replace cowling not requiring removal of the propeller.
• Replace, clean or set spark plug gap clearance.
June 2007
Information Manual 8-9
Cirrus Design Section 8
SR22 Handling, Servicing, Maintenance
• Replace any hose connection, except hydraulic connections, with
replacement hoses.
• Clean or replace fuel and oil strainers, as well as replace or clean
filter elements.
• Replace prefabricated fuel lines.
• Replace the battery and check fluid level and specific gravity.
Logbook Entry
After any of the above work is accomplished, appropriate logbook
entries must be made. Logbook entries should contain:
• The date the work was accomplished.
• Description of the work.
• Number of hours on the aircraft.
• The certificate number of pilot performing the work.
• Signature of the individual doing the work.
Logbooks should be complete and up to date. Good records reduce
maintenance cost by giving the mechanic information about what has
or has not been accomplished.
June 2007
8-10 Information Manual
Section 8 Cirrus Design
Handling, Servicing, Maintenance SR22
Ground Handling
Application of External Power
A ground service receptacle, located just aft of the cowl on the left side
of the airplane, permits the use of an external power source for cold
weather starting and maintenance procedures.
• WARNING •
If external power will be used to start engine, keep yourself,
others, and power unit cables well clear of the propeller
rotation plane.
To apply external power to the airplane:
• Caution •
Do not use external power to start the airplane with a ‘dead’
battery or to charge a dead or weak battery in the airplane.
The battery must be removed from the airplane and battery
maintenance performed in accordance with the appropriate
Airplane Maintenance Manual procedures.
1. Ensure that external power source is regulated to 28 VDC.
2. Check BAT and AVIONICS power switches are ‘off.’
3. Plug external power source into the receptacle.
4. Set BAT 1 switch to ON. 28 VDC from the external power unit will
　
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