This FAA approved owner/operator program can  be revised at a future date by the FAA, if they  find that revisions are necessary for the continued  adequacy of the program. The owner/operator can  petition the FAA within 30 days of notification  to reconsider the notice to make changes. This is a program developed by the manufacturer for their  product. It is contained in the “Instructions for Continued  Airworthiness” required under 14 CFR part 23, section 23.1529  and part 25, section 25.1529. It is in the form of a manual, or  manuals as appropriate, for the quantity of data to be provided  and including, but not limited to, the following content: The Airworthiness Limitations section must contain a  legible statement in a prominent location that reads: “The  Airworthiness Limitations section is FAA-approved and  specifies maintenance required under 14 CFR part 43,  sections 43.16 and part 91, section 91.403, unless an  alternative program has been FAA-approved.” Any operator who wishes to adopt a manufacturers’  inspection program should first contact their local FAA Flight  Standards District Office, for further guidance. Any person operating an airplane or helicopter in controlled  airspace under instrument flight rules (IFR) must have had,  within the preceding 24 calendar months, each static pressure  system, each altimeter instrument, and each automatic  pressure altitude reporting system tested and inspected and  found to comply with 14 CFR part 43, Appendix E. Those  test and inspections must be conducted by appropriately rated  persons under 14 CFR. Any person using an air traffic control (ATC) transponder  must have had, within the preceding 24 calendar months, that  transponder tested and inspected and found to comply with  14 CFR part 43, Appendix F, and part 91, section 91.411.  Additionally, following any installation or maintenance on  an ATC transponder where data correspondence error could  be introduced, the integrated system must be tested and  inspected and found to comply with 14 CFR part part 43,  Appendix E, and part 91, section 91.411 by an appropriately  person under 14 CFR. This AC combined and updated several ACs on the subject  of ELTs and receivers for airborne service.  Under the operating rules of 14 CFR part 91, most small U.S.  registered civil airplanes equipped to carry more than one  2-62 Emergency Locator Transmitter (ELT) Operational  and Maintenance Practices in Accordance With  Advisory Circular (AC) 91-44  Air Traffic Control (ATC) Transponder Inspections Altimeter and Static System Inspections in Accordance  with 4 CFR Part 91, Section 91.411 Manufacturer’s Inspection Program 1.  Each mandatory replacement time, structural  inspection interval, and related structural inspection  procedures required for type certification or  approved under 14 CFR part 23 or part 25. 2.  Each mandatory replacement time, inspection  interval, related inspection procedure, and all  critical design configuration control limitations  approved under 14 CFR part 23 or part 25, for  the fuel tank system. •  A description of the airplane and its systems and  installations, including its engines, propellers, and  appliances. •  Basic information describing how the airplane  components and systems are controlled and operated,  including any special procedures and limitations that  apply. •  Servicing information that covers servicing points,  capacities of tanks, reservoirs, types of fluids to be  used, pressures applicable to the various systems,  lubrication points, lubricants to be used, equipment  required for servicing, tow instructions, mooring,  jacking, and leveling information. •  Maintenance instructions with scheduling information  for the airplane and each component that provides  the recommended periods at which they should be  cleaned, inspected, adjusted, tested, and lubricated,  and the degree of inspection and work recommended  at these periods. •  The recommended overhaul periods and necessary  cross references to the airworthiness limitations  section of the manual. •  The inspection program that details the frequency and  extent of the inspections necessary to provide for the  continued airworthiness of the airplane. •  Diagrams of structural access plates and information  needed to gain access for inspections when access  plates are not provided. •  Details for the application of special inspection  techniques, including radiographic and ultrasonic  testing where such processes are specified. •  A list of special tools needed. •  An Airworthiness Limitations section that is  segregated and clearly distinguishable from the rest  of the document. This section must set forth—