for program scheduling, recording, and accountability  for continuing accomplishment of the program. This  section serves to facilitate administration of the program  by the certificate holder and to direct its accomplishment  by mechanics or repair stations. The operator’s manual  should include instructions to accomplish the maintenance/ inspections tasks. It should also contain a list of the  necessary tools and equipment needed to perform the  maintenance and inspections. The FAA FSDO will provide each operator with computer- generated Operations Specifications when they approve the  program. The definition of maintenance in 14 CFR part 1 includes  inspection. The inspection program required for 14 CFR  part 121 and part 135 air carriers is part of the Continuous  Airworthiness Maintenance Program (CAMP). CAMP is  not required of every part 135 carrier; it depends on aircraft  being operated. It is a complex program that requires an  organization of experienced and knowledgeable aviation  personnel to implement it.  The FAA has developed an Advisory Circular, AC 120-16 (as  revised) Air Carrier Maintenance Programs, which explains  the background as well as the FAA regulatory requirements  for these programs. The AC applies to air carriers subject to  14 CFR parts 119, 121, and 135. For part 135, it applies only  to aircraft type certificated with ten or more passenger seats. Any person wanting to place their aircraft on this type of  program should contact their local FAA FSDO for guidance.  This regulation applies to airplanes having a seating capacity  of 20 or more passengers or a maximum payload capacity  of 6,000 pounds or more when the aircraft is not required  to be operated under 14 CFR parts 121, 129, 135, and 137.  Inspection programs which may be approved for use under  this 14 CFR part include, but are not limited to: 1.  A continuous inspection program which is part of a  current continuous airworthiness program approved  for use by a certificate holder under 14 CFR part 121  or part 135; 2.  Inspection programs currently recommended by  the manufacturer of the airplane, airplane engines,  propellers, appliances, or survival and emergency  equipment; or 3.  An inspection program developed by a certificate  holder under 14 CFR part 125. •  The replacement times for life-limited parts  specified in the aircraft type certificate data  sheets, or other documents approved by the FAA  are complied with; •  Defects disclosed between inspections, or as  a result of inspection, have been corrected in  accordance with 14 CFR part 43; and •  The airplane, including airframe, aircraft  engines, propellers, appliances, and survival and  emergency equipment, and their component parts,  is inspected in accordance with an inspection  program approved by the FAA. These inspections  must include at least the following: ○ Instructions, procedures and standards for  the particular make and model of airplane,  including tests and checks. The instructions  and procedures must set forth in detail the  parts and areas of the airframe, aircraft  engines, propellers, appliances, and survival  and emergency equipment required to be  inspected. ○ A schedule for the performance of the  inspections that must be performed under  the program, expressed in terms of the time  in service, calendar time, number of system  operations, or any combination of these. ○ The person used to perform the inspections  required by 14 CFR part 125, must be  authorized to perform maintenance under  14 CFR part 43. The airplane subject to  part 125 may not be operated unless the  installed engines have been maintained  in accordance with the overhaul periods  recommended by the manufacturer or a  program approved by the FAA; the engine  overhaul periods are specified in the  inspection programs required by 14 CFR  part 125, section 125.247. Title 14 CFR part 125, section 125.247, Inspection  Programs and Maintenance Helicopter Inspections, Piston-Engine and Turbine- Powered  A piston-engine helicopter must be inspected in accordance  with the scope and detail of 14 CFR part 43, Appendix D  for an Annual Inspection. However, there are additional  performance rules for inspections under 14 CFR part 43,  2-67 Continuous Airworthiness Maintenance Program  (CAMP) The airplane subject to this part may not be operated  unless: