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components with stated hourly operating limitations is normally accomplished during the calendar inspection falling nearest the hourly limitation.
In some instances, a flight hour limitation is established to limit the number of hours that may be flown during the calendar interval.
Aircraft operating under the flight hour system are inspected when a specified number of flight hours are accumulated. Components with stated hourly operating limitations are normally replaced during the inspection that falls nearest the hourly limitation.
Basic Inspection Techniques/Practices
Before starting an inspection, be certain all plates, access doors, fairings, and cowling have been opened or removed and the structure cleaned. When opening inspection plates and cowling and before cleaning the area, take note of any oil or other evidence of fluid leakage.
Preparation
In order to conduct a thorough inspection, a great deal of paperwork and/or reference information must be accessed and studied before actually proceeding to the aircraft to conduct the inspection. The aircraft logbooks must be reviewed to provide background information and a maintenance history of the particular aircraft. The appropriate checklist or checklists must be utilized to ensure that no items will be forgotten or overlooked during the inspection. Also, many addi-tional publications must be available, either in hard copy or in electronic format to assist in the inspections. These additional publications may include information provided by the aircraft and engine manufacturers, appliance manufacturers, parts venders, and the Federal Aviation Administration (FAA).
Inspections are visual examinations and manual checks to determine the condition of an aircraft or component. An aircraft inspection can range from a casual walk-around to a detailed inspection involving complete disassembly and the use of complex inspection aids.An inspection system consists of several processes, including reports made by mechanics or the pilot or crew flying an aircraft and regularly scheduled inspec-tions of an aircraft. An inspection system is designed to maintain an aircraft in the best possible condition. Thorough and repeated inspections must be considered the backbone of a good maintenance program. Irregu-lar and haphazard inspection will invariably result in gradual and certain deterioration of an aircraft. The time spent in repairing an abused aircraft often totals far more than any time saved in hurrying through routine inspections and maintenance.
It has been proven that regularly scheduled inspections and preventive maintenance assure airworthiness. Operating failures and malfunctions of equipment are appreciably reduced if excessive wear or minor defects are detected and corrected early. The importance of inspections and the proper use of records concerning these inspections cannot be overemphasized.Airframe and engine inspections may range from preflight inspections to detailed inspections. The time intervals for the inspection periods vary with the models of aircraft involved and the types of operations being conducted. The airframe and engine manufacturer’s instructions should be consulted when establishing inspection intervals.
Aircraft may be inspected using flight hours as a basis for scheduling, or on a calendar inspection system. Under the calendar inspection system, the appropriate inspection is performed on the expiration of a speci-fied number of calendar weeks. The calendar inspec-tion system is an efficient system from a maintenance management standpoint. Scheduled replacement
of
Aircraft Logs
“Aircraft logs,” as used in this handbook, is an inclu-sive term which applies to the aircraft logbook and all supplemental records concerned with the aircraft. They may come in a variety of formats. For a small aircraft, the log may indeed be a small 5" × 8" logbook. For larger aircraft, the logbooks are often larger, in the form of a three-ring binder. Aircraft that have been in service for a long time are likely to have several logbooks. The aircraft logbook is the record in which all data con-cerning the aircraft is recorded. Information gathered in this log is used to determine the aircraft condition, date of inspections, time on airframe, engines and propellers. It reflects a history of all significant events occurring to the aircraft, its components, and acces-sories, and provides a place for indicating compliance with FAA airworthiness directives or manufactur-ers’ service bulletins. The more comprehensive the logbook, the easier it is to understand the aircraft’s maintenance history.
When the inspections are completed, appropriate entries must be made in the aircraft logbook certifying that the aircraft is in an airworthy condition and may be returned to service. When making logbook entries, exercise special care to ensure that the entry can be clearly understood by anyone having a need to read it in the future. Also, if making a hand-written entry, use good penmanship and write legibly. To some degree, the organization, comprehensiveness, and appearance of the aircraft logbooks have an impact on the value of the aircraft. High quality logbooks can mean a higher value for the aircraft.
Checklists
Always use a checklist when performing an inspection. The checklist may be of your own design, one provided by the manufacturer of the equipment being inspected, or one obtained from some other source. The checklist should include the following:
1. Fuselage and hull group.
a. Fabric and skin—for deterioration,
distortion, other evidence of failure, and
defective or insecure attachment of fittings.
b. Systems and components—for proper
installation, apparent defects, and satisfactory
operation.
c. Envelope gas bags, ballast tanks, and related
parts—for condition.2. Cabin and cockpit group.
a. Generally—for cleanliness and loose
equipment that should be secured.
b. Seats and safety belts—for condition and
security.
c. Windows and windshields—for deterioration
and breakage.
d. Instruments—for condition, mounting,
marking, and (where practicable) for proper
operation.
e. Flight and engine controls—for proper
installation and operation.
f. Batteries—for proper installation and charge.
g. All systems—for proper installation, general
condition, apparent defects, and security of
attachment.
3. Engine and nacelle group.
a. Engine section—for visual evidence of
excessive oil, fuel, or hydraulic leaks, and
sources of such leaks.
b. Studs and nuts—for proper torquing and
obvious defects.
c. Internal engine—for cylinder compression
and for metal particles or foreign matter on
screens and sump drain plugs. If cylinder
compression is weak, check for improper
internal condition and improper internal
tolerances.
d. Engine mount—for cracks, looseness of
mounting, and looseness of engine to mount.
e. Flexible vibration dampeners—for condition
and deterioration.
f. Engine controls—for defects, proper travel,
and proper safetying.
g. Lines, hoses, and clamps—for leaks,
condition, and looseness.
h. Exhaust stacks—for cracks, defects, and
proper attachment.
i. Accessories—for apparent defects in security
of mounting.
j. All systems—for proper installation, general
condition defects, and secure attachment.
k. Cowling—for cracks and defects.
l. Ground runup and functional check—check
all powerplant controls and systems for
correct response, all instruments for proper
operation and indication.
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c. Anti-icing devices—for proper operation and obvious defects.
d. Control mechanisms—for proper operation, secure mounting, and travel. 8. Communication and navigation group.
a. Radio and electronic equipment—for proper installation and secure mounting.
b. Wiring and conduits—for proper routing, secure mounting, and obvious defects.
c. Bonding and shielding—for proper installation and condition.
d. Antennas —for condition, secure mounting, and proper operation. 9. Miscellaneous.
a. Emergency and first aid equipment—for general condition and proper stowage.
b. Parachutes, life rafts, flares, and so forth—inspect in accordance with the manufacturer’s recommendations.
c. Autopilot system—for general condition, security of attachment, and proper operation.
Publications
Aeronautical publications are the sources of informa-tion for guiding aviation mechanics in the operation and maintenance of aircraft and related equipment. The proper use of these publications will greatly aid in the efficient operation and maintenance of all air-craft. These include manufacturers’ service bulletins, manuals, and catalogs; FAA regulations; airworthiness directives; advisory circulars; and aircraft, engine and propeller specifications.
Manufacturers’ Service Bulletins/Instructions Service bulletins or service instructions are two of sev-eral types of publications issued by airframe, engine, and component manufacturers.
The bulletins may include: (1) purpose for issuing the publication, (2) name of the applicable airframe, engine, or component, (3) detailed instructions for service, adjustment, modification or inspection, and source of parts, if required and (4) estimated number of manhours required to accomplish the job.Maintenance Manual
The manufacturer’s aircraft maintenance manual contains complete instructions for maintenance of all systems and components installed in the aircraft. It contains information for the mechanic who normally
4. Landing gear group.
a. All units —for condition and security of attachment.
b. Shock absorbing devices—for proper oleo fluid level.
c. Linkage, trusses, and members—for undue or excessive wear, fatigue, and distortion.
d. Retracting and locking mechanism—for proper operation.
e. Hydraulic lines—for leakage.
f. Electrical system—for chafing and proper operation of switches.
g. Wheels—for cracks, defects, and condition of bearings.
h. Tires —for wear and cuts.
i. Brakes —for proper adjustment.
j. Floats and skis —for security of attachment and obvious defects. 5. Wing and center section.
a. All components—for condition and security.
b. Fabric and skin—for deterioration, distortion, other evidence of failure, and security of attachment.
c. Internal structure (spars, ribs compression members)—for cracks, bends, and security.
d. Movable surfaces —for damage or obvious defects, unsatisfactory fabric or skin attachment and proper travel.
e. Control mechanism—for freedom of movement, alignment, and security.
f. Control cables—for proper tension, fraying, wear and proper routing through fairleads and pulleys. 6. Empennage group.
a. Fixed surfaces—for damage or obvious defects, loose fasteners, and security of attachment.
b. Movable control surfaces—for damage or obvious defects, loose fasteners, loose fabric, or skin distortion.
c. Fabric or skin—for abrasion, tears, cuts or defects, distortion, and deterioration. 7. Propeller group.
a. Propeller assembly—for cracks, nicks, bends, and oil leakage.
b. Bolts —for proper torquing and safetying.
works on components, assemblies, and systems while they are installed in the aircraft, but not for the over-haul mechanic. A typical aircraft maintenance manual contains:
• A description of the systems (i.e., electrical, hydraulic, fuel, control)
• Lubrication instructions setting forth the frequency and the lubricants and fluids which are to be used in the various systems,
• Pressures and electrical loads applicable to the various systems,
• Tolerances and adjustments necessary to proper functioning of the airplane,
• Methods of leveling, raising, and towing,
• Methods of balancing control surfaces,
• Identification of primary and secondary structures,• Frequency and extent of inspections necessary to the proper operation of the airplane,
• Special repair methods applicable to the airplane,• Special inspection techniques requiring x-ray, ultrasonic, or magnetic particle inspection, and • A list of special tools.
Overhaul Manual
The manufacturer’s overhaul manual contains brief descriptive information and detailed step by step instructions covering work normally performed on a unit that has been removed from the aircraft. Simple, inexpensive items, such as switches and relays on which overhaul is uneconomical, are not covered in the overhaul manual.
Structural Repair Manual
This manual contains the manufacturer’s information and specific instructions for repairing primary and sec-ondary structures. Typical skin, frame, rib, and stringer repairs are covered in this manual. Also included are material and fastener substitutions and special repair techniques.
Illustrated Parts Catalog
This catalog presents component breakdowns of struc-ture and equipment in disassembly sequence. Also included are exploded views or cutaway illustrations for all parts and equipment manufactured by the aircraft manufacturer.Code of Federal Regulations (CFRs)
The CFRs were established by law to provide for the safe and orderly conduct of flight operations and to prescribe airmen privileges and limitations. A knowl-edge of the CFRs is necessary during the performance of maintenance, since all work done on aircraft must comply with CFR provisions.
Airworthiness Directives
A primary safety function of the FAA is to require correction of unsafe conditions found in an aircraft, aircraft engine, propeller, or appliance when such con-ditions exist and are likely to exist or develop in other products of the same design. The unsafe condition may exist because of a design defect, maintenance, or other causes. Title 14 of the Code of Federal Regulations (14 CFR) part 39, Airworthiness Directives, defines the authority and responsibility of the Administra-tor for requiring the necessary corrective action. The Airworthiness Directives (ADs) are published to notify aircraft owners and other interested persons of unsafe conditions and to prescribe the conditions under which the product may continue to be operated. Airworthiness Directives are Federal Aviation Regu-lations and must be complied with unless specific exemption is granted.
Airworthiness Directives may be divided into two categories: (1) those of an emergency nature requiring immediate compliance upon receipt and (2) those of a less urgent nature requiring compliance within a rela-tively longer period of time. Also, ADs may be a one-time compliance item or a recurring item that requires future inspection on an hourly basis (accrued flight time since last compliance) or a calendar time basis.
The contents of ADs include the aircraft, engine, pro-peller, or appliance model and serial numbers affected. Also included are the compliance time or period, a description of the difficulty experienced, and the nec-essary corrective action.
Type Certificate Data Sheets
The type certificate data sheet (TCDS) describes the type design and sets forth the limitations prescribed by the applicable CFR part. It also includes any other limitations and information found necessary for type certification of a particular model aircraft.
Type certificate data sheets are numbered in the upper right-hand corner of each page. This number is the same as the type certificate number. The name of the type certificate holder, together with all of the approved
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models, appears immediately below the type certificate number. The issue date completes this group. This information is contained within a bordered text box to set it off.
The data sheet is separated into one or more sections. Each section is identified by a Roman numeral followed by the model designation of the aircraft to which the section pertains. The category or categories in which the aircraft can be certificated are shown in parenthe-ses following the model number. Also included is the approval date shown on the type certificate.
The data sheet contains information regarding:
1. Model designation of all engines for which the
aircraft manufacturer obtained approval for use with this model aircraft.
2. Minimum fuel grade to be used.
3. Maximum continuous and takeoff ratings of the
approved engines, including manifold pressure (when used), rpm, and horsepower (hp).
4. Name of the manufacturer and model designation for
each propeller for which the aircraft manufacturer obtained approval will be shown together with the propeller limits and any operating restrictions peculiar to the propeller or propeller engine combination.
5. Airspeed limits in both mph and knots.
6. Center of gravity range for the extreme loading
conditions of the aircraft is given in inches from the datum. The range may also be stated in percent of MAC (Mean Aerodynamic Chord) for transport category aircraft.
7. Empty weight center of gravity (CG) range (when
established) will be given as fore and aft limits in inches from the datum. If no range exists, the word “none” will be shown following the heading on the data sheet.
8. Location of the datum.
9. Means provided for leveling the aircraft.
10. All pertinent maximum weights.
11. Number of seats and their moment arms.
12. Oil and fuel capacity.
13. Control surface movements.
14. Required equipment.
15. Additional or special equipment found necessary
for certification.
16. Information concerning required placards.It is not within the scope of this handbook to list all the items that can be shown on the type certificate data sheets. Those items listed above serve only to acquaint aviation mechanics with the type of information gener-ally included on the data sheets. Type certificate data sheets may be many pages in length. Figure 8-1 shows a typical TCDS.
When conducting a required or routine inspection, it is necessary to ensure that the aircraft and all the major items on it are as defined in the type certificate data sheets. This is called a conformity check, and verifies that the aircraft conforms to the specifications of the aircraft as it was originally certified. Sometimes altera-tions are made that are not specified or authorized in the TCDS. When that condition exists, a supplemental type certificate (STC) will be issued. STCs are considered a part of the permanent records of an aircraft, and should be maintained as part of that aircraft’s logs.
Routine/Required Inspections
For the purpose of determining their overall condition, 14 CFR provides for the inspection of all civil aircraft at specific intervals, depending generally upon the type of operations in which they are engaged. The pilot in command of a civil aircraft is responsible for determin-ing whether that aircraft is in condition for safe flight. Therefore, the aircraft must be inspected before each flight. More detailed inspections must be conducted by aviation maintenance technicians at least once each 12 calendar months, while inspection is required for others after each 100 hours of flight. In other instances, an aircraft may be inspected in accordance with a system set up to provide for total inspection of the aircraft over a calendar or flight time period.
To determine the specific inspection requirements and rules for the performance of inspections, refer to the CFR, which prescribes the requirements for the inspection and maintenance of aircraft in various types of operations.
Preflight/Postflight Inspections
Pilots are required to follow a checklist contained within the Pilot’s Operating Handbook (POH) when operating aircraft. The first section of a checklist includes a section entitled Preflight Inspection. The preflight inspection checklist includes a “walk-around” section listing items that the pilot is to visually check for general condition as he or she walks around the airplane. Also, the pilot must ensure that fuel, oil and other items required for flight are at the proper levels
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and not contaminated. Additionally, it is the pilot’s responsibility to review the airworthiness certificate, maintenance records, and other required paperwork to verify that the aircraft is indeed airworthy. After each flight, it is recommended that the pilot or mechanic conduct a postflight inspection to detect any problems that might require repair or servicing before the next flight.
Annual/100-Hour Inspections
Title 14 of the Code of Federal Regulations (14 CFR) part 91 discusses the basic requirements for annual and 100-hour inspections. With some exceptions, all aircraft must have a complete inspection annually. Aircraft that are used for commercial purposes and are likely to be used more frequently than noncommercial aircraft must have this complete inspection every 100 hours. The scope and detail of items to be included in annual and 100-hour inspections is included as appen-dix D of 14 CFR part 43 and shown as Figure 8-2.
A properly written checklist, such as the one shown earlier in this chapter, will include all the items of appendix D. Although the scope and detail of annual and 100-hour inspections is identical, there are two significant differences. One difference involves persons authorized to conduct them. A certified airframe and powerplant maintenance technician can conduct a 100-hour inspection, whereas an annual inspection must be conducted by a certified airframe and powerplant maintenance technician with inspection authorization (IA). The other difference involves authorized over-flight of the maximum 100 hours before inspection. An aircraft may be flown up to 10 hours beyond the 100-hour limit if necessary to fly to a destination where the inspection is to be conducted.
Progressive Inspections
Because the scope and detail of an annual inspection is very extensive and could keep an aircraft out of service for a considerable length of time, alternative
(a) Each person performing an annual or 100-hour
inspection shall, before that inspection, remove or open all necessary inspection plates, access doors, fairing, and cowling. He shall thoroughly clean the aircraft and aircraft engine. (b) Each person performing an annual or 100-hour
inspection shall inspect (where applicable) the following components of the fuselage and hull group:
(1) Fabric and skin—for deterioration,
distortion, other evidence of failure, and defective or insecure attachment of fittings. (2) Systems and components—for improper
installation, apparent defects, and unsatisfactory operation. (3) Envelope, gas bags, ballast tanks, and
related parts—for poor condition. (c) Each person performing an annual or 100-hour
inspection shall inspect (where applicable) the following components of the cabin and cockpit group:
(1) Generally—for uncleanliness and loose
equipment that might foul the controls. (2) Seats and safety belts—for poor condition
and apparent defects.
Appendix D to Part 43—Scope and Detail of Items (as Applicable to the Particular Aircraft) To Be Included in Annual and 100-Hour Inspections
Figure 8-2. Scope and detail of annual and 100-hour inspections.
(3) Windows and windshields—for
deterioration and breakage.
(4) Instruments—for poor condition,
mounting, marking, and (where practicable) improper operation. (5) Flight and engine controls—for improper
installation and improper operation. (6) Batteries—for improper installation and
improper charge. (7) All systems—for improper installation,
poor general condition, apparent and obvious defects, and insecurity of attachment. (d) Each person performing an annual or 100-hour
inspection shall inspect (where applicable) components of the engine and nacelle group as follows:
(1) Engine section—for visual evidence of
excessive oil, fuel, or hydraulic leaks, and sources of such leaks. (2) Studs and nuts—for improper torquing
and obvious defects.(3) Internal engine—for cylinder compression
and for metal particles or foreign matter on screens and sump drain plugs. If there is
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weak cylinder compression, for improper internal condition and improper internal tolerances.
(4) Engine mount—for cracks, looseness
of mounting, and looseness of engine to mount. (5) Flexible vibration dampeners—for poor
condition and deterioration. (6) Engine controls—for defects, improper
travel, and improper safetying. (7) Lines, hoses, and clamps—for leaks,
improper condition, and looseness. (8) Exhaust stacks—for cracks, defects, and
improper attachment. (9) Accessories—for apparent defects in
security of mounting.
(10) All systems—for improper installation, poor general condition, defects, and insecure attachment.
(11) Cowling—for cracks and defects. (e) Each person performing an annual or 100-hour inspection shall inspect (where applicable) the following components of the landing gear group:
(1) All units —for poor condition and
insecurity of attachment. (2) Shock absorbing devices—for improper
oleo fluid level. (3) Linkages, trusses, and members—for
undue or excessive wear fatigue, and distortion. (4) Retracting and locking mechanism—for
improper operation. (5) Hydraulic lines—for leakage. (6) Electrical system—for chafing and
improper operation of switches. (7) Wheels—for cracks, defects, and
condition of bearings. (8) Tires—for wear and cuts. (9) Brakes—for improper adjustment.
(10) Floats and skis—for insecure attachment and obvious or apparent defects.
Figure 8-2. Scope and detail of annual and 100-hour inspections. (continued)
(f) Each person performing an annual or 100-hour
inspection shall inspect (where applicable) all components of the wing and center section assembly for poor general condition, fabric or skin deterioration, distortion, evidence of failure, and insecurity of attachment.
(g) Each person performing an annual or 100-hour inspection shall inspect (where applicable) all components and systems that make up the com-plete empennage assembly for poor general condition, fabric or skin deterioration, distortion, evidence of failure, insecure attachment, improper component installation, and improper component operation.
(h) Each person performing an annual or 100-hour inspection shall inspect (where applicable) the following components of the propeller group: (1) Propeller assembly—for cracks, nicks,
binds, and oil leakage. (2) Bolts—for improper torquing and lack of
safetying. (3) Anti-icing devices—for improper
operations and obvious defects. (4) Control mechanisms—for improper
operation, insecure mounting, and restricted travel. (i) Each person performing an annual or 100-hour
inspection shall inspect (where applicable) the following components of the radio group: (1) Radio and electronic equipment—for
improper installation and insecure mounting. (2) Wiring and conduits—for improper
routing, insecure mounting, and obvious defects. (3) Bonding and shielding—for improper
installation and poor condition. (4) Antenna including trailing antenna—for
poor condition, insecure mounting, and improper operation. (j) Each person performing an annual or 100-hour
inspection shall inspect (where applicable) each installed miscellaneous item that is not otherwise covered by this listing for improper installation and improper operation.
Appendix D to Part 43—Scope and Detail of Items (as Applicable to the Particular Aircraft) To Be Included in Annual and 100-Hour Inspections (continued)
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inspection programs designed to minimize down time may be utilized. A progressive inspection program allows an aircraft to be inspected progressively. The scope and detail of an annual inspection is essentially divided into segments or phases (typically four to six). Completion of all the phases completes a cycle that satisfies the requirements of an annual inspection. The advantage of such a program is that any required segment may be completed overnight and thus enable the aircraft to fly daily without missing any revenue earning potential. Progressive inspection programs include routine items such as engine oil changes and detailed items such as flight control cable inspection. Routine items are accomplished each time the aircraft
comes in for a phase inspection and detailed items focus on detailed inspection of specific areas. Detailed inspections are typically done once each cycle. A cycle must be completed within 12 months. If all required phases are not completed within 12 months, the remain-ing phase inspections must be conducted before the end of the 12th month from when the first phase was completed.
Each registered owner or operator of an aircraft desiring to use a progressive inspection program must submit a written request to the FAA Flight Standards District Office (FSDO) having jurisdiction over the area in which the applicant is located. Title 14 of the Code of Federal Regulations (14 CFR) part 91, §91.409(d)
Figure 8-3. 14 CFR §91.409(d) Progressive inspection.
(d) Progressive inspection. Each registered owner or operator of an aircraft desiring to use a progressive inspection program must submit a written request to the FAA Flight Standards district office having jurisdiction over the area in which the applicant is located, and shall provide—(1) A certificated mechanic holding an
inspection authorization, a certificated airframe repair station, or the manufacturer of the aircraft to supervise or conduct the progressive inspection;(2) A current inspection procedures manual
available and readily understandable to pilot and maintenance personnel containing, in detail—
(i) An explanation of the progressive
inspection, including the continuity of inspection responsibility, the making of reports, and the keeping of records and technical reference material; (ii) An inspection schedule, specifying
the intervals in hours or days when routine and detailed inspections will be performed and including instructions for exceeding an inspection interval by not more than 10 hours while en route and for changing an inspection interval because of service experience;
(iii) Sample routine and detailed inspection forms and instructions for their use; and
(iv) Sample reports and records and instructions for their use;
(3) Enough housing and equipment for
necessary disassembly and proper inspection of the aircraft; and (4) Appropriate current technical information
for the aircraft.The frequency and detail of the progressive inspection shall provide for the complete inspection of the aircraft within each 12 calendar months and be consistent with the manufacturer's recommendations, field service experience, and the kind of operation in which the aircraft is engaged. The progressive inspection schedule must ensure that the aircraft, at all times, will be airworthy and will conform to all applicable FAA aircraft specifications, type certificate data sheets, airworthiness directives, and other approved data. If the progressive inspection is discontinued, the owner or operator shall immediately notify the local FAA Flight Standards district office, in writing, of the discontinuance. After the discontinuance, the first annual inspection under §91.409(a)(1) is due within 12 calendar months after the last complete inspection of the aircraft under the progressive inspection. The 100-hour inspection under §91.409(b) is due within 100 hours after that complete inspection. A complete inspection of the aircraft, for the purpose of determining when the annual and 100-hour inspections are due, requires a detailed inspection of the aircraft and all its components in accordance with the progressive inspection. A routine inspection of the aircraft and a detailed inspection of several components is not considered to be a complete inspection.
§91.409 Inspections.。