Examine the seat recline control and attaching hardware to make sure the hardware and lock are not damaged and are correctly installed. Refer to the Model 172 Wiring Diagram Manual, Chapter 20, Soldering - Maintenance Practices. Most components given in Chapter 5 are examined as shown elsewhere in this chapter and repaired, overhauled, or replaced as necessary. Operation 1 gives a list of item s , which has all 50-hour interval inspection items and those 100- or 200-hour interval inspection items contained in the fuselage area. General Inspection Criteria I A.
These general inspections are used to find apparent conditions which can need more maintenance. Refer to the latest revision of McCauley Service Bulletin 240. These tasks are printed in the individual chapters of this manual. These tasks are printed in the individual chapters of this manual. These general inspections are used to find apparent conditions which can need more maintenance. This threenumber sequence is specified in Airplane Zoning - Description and Operation.
Remove the Rear Passenger Intercom Jacks Refer to Figure 201. Ensure that padded block 1 inch X 4 inch X 4 inch with 0. Refer to Chapter 78, Exhaust system - Maintenance Practices. It is important to keep a high level of cleanliness. Check travel if cable tension requires adjustment or if stops are damaged.
Clean fuel inlet screen, check and clean injection nozzles and screens if evidence of contamination is found , and lubricate air throttle shaft. Refer to Chapter 12, Battery - Servicing. Check cables for tension, routing, fraying, corrosion, and turnbuckle safety. Additional information which becomes available may be provided by temporary revision. This includes the alternator, batteries, and relays. Check for abrasions, chafing, security, proper routing and support and for evidence of deterioration. If required, adjust the idle rpm and fuel mixture.
Wash engine and check for security of accessories. Inspection items are given in the order of the zone in which the inspection is to be completed. Inspection items are given in the order of the zone in which the inspection is to be completed. Airplanes operated in extremely humid areas tropics , or in unusually cold, damp climates, etc. Disassemble, flush, and clean screen and bowl. Operation 5 gives a list of item s , which are completed every 400 hours or 1 year, whichever occurs first. Figure 801, Figure 802, etc.
If you need a hard copy, push the print button!! Complete a check for the proper travel, security of attachment, and for evidence of wear. These general inspections are used to find apparent conditions which can need more maintenance. This section provides a general overview of inspection requirements. It also includes landings that are short of the prepared surface, or landings which involve the damage of tires or skids on a runway to the extent that the safety of the airplane is in question. The operator's inspection intervals must not deviate from the inspection time limits shown in this manual except as given below: 1 Each inspection interval can be exceeded by 10 hours if time-controlled , or by 30 days if datecontrolled , or can be performed early at any time prior to the regular interval as provided below: a Inthe event of late compliance of any operation scheduled, the next operation in sequence retains a due point from the time the late operation was originally scheduled. Operation 13 Every 50 hours or four months, whichever occurs first. You can Print any or all pages.
If damage is found, complete a functional check of the glideslope system. These tasks are printed in the individual chapters of this manual. Check that the following documents are up-to-date and in accordance with current Federal Aviation Regulations. During each of the specified inspection tasks in this section, more general inspections of the adjacent areas must be done while access is available. Lower Airplane Refer to Figure 201. There are no airworthiness limitations associated with this airplane.
Examine for chips, scratches, or other damage that lets corrosion get to the steel spring. Complete a fuel quantity calibration check. These adjuncts to the text are used to highlight or emphasize important points. Check strut for evidence of leakage and proper extension. Operation 15 Every 2000 hours. Carefully attach tail stand to tail tie-down ring. Operation 18 Every 6 years.
Refer to Chapter 78, Exhaust system - Maintenance Practices. Do a preflight inspection after these inspections are completed to make sure all the required items are correctly serviced. Do disassembly or assembly of the servo at an electrostatic-safe area. These general inspections are used to find apparent conditions which can need more maintenance. This section will give instructions for the inspection of the pitch, pitch trim, and roll servos. Refer to Chapter 73, Fuel Injection Systems - Maintenance Practices. Examine the seat recline control and attaching hardware to make sure the hardware and lock are not damaged and are correctly installed.