14.1 14 CFR Part 43 Appendix D: Scope of 100-Hour & Annual Inspections
Key Takeaways
- 14 CFR Part 43 Appendix D establishes the mandatory minimum scope and detail for both 100-hour and Annual inspections, requiring systematic examination across 9 major aircraft groups using a checklist.
- While 100-hour and Annual inspections share an identical technical scope under Appendix D, an Annual inspection requires an A&P mechanic holding an Inspection Authorization (IA), whereas a 100-hour inspection may be approved by any certificated A&P mechanic.
- Under 14 CFR §91.409(b), the 100-hour inspection limitation may be exceeded by up to 10 hours strictly to ferry the aircraft to an inspection location, but those excess hours are deducted from the next 100-hour cycle; Annual inspections have no 10-hour allowance.
- When unairworthy discrepancies are discovered during an Annual or 100-hour inspection, the technician does not impound the aircraft or revoke its airworthiness certificate; instead, they must provide a signed, dated list of discrepancies to the owner/operator per 14 CFR §43.11.
- Progressive inspection programs (14 CFR §91.409(d)) allow operators to divide the annual inspection scope into scheduled increments across a 12-calendar-month cycle, subject to FAA FSDO approval.
14.1 14 CFR Part 43 Appendix D: Scope of 100-Hour & Annual Inspections
FAA Airframe Subject Matter Focus: Aviation maintenance technicians must master the regulatory scope, technical depth, and administrative execution of aircraft inspection programs. Under Title 14 of the Code of Federal Regulations (14 CFR) Part 43, Appendix D defines the minimum inspection standards required to determine whether an aircraft is in an airworthy condition. Technicians must understand the legal boundaries separating 100-hour, Annual, and Progressive inspection programs, the exact privileges and limitations of certificated A&P mechanics versus holders of an Inspection Authorization (IA), and the mandatory procedures for handling unairworthy discrepancy findings.
1. 14 CFR Part 43 Appendix D: Scope & Checklist Architecture
Under 14 CFR §43.15(c), each person performing a 100-hour or Annual inspection must perform the inspection in such a manner as to determine whether the aircraft concerned meets all applicable airworthiness requirements. Furthermore, the technician must use a checklist while performing the inspection. This checklist may be of the mechanic's own design, one provided by the aircraft manufacturer, or one obtained from another commercial source, provided it includes the complete scope and detail of the items listed in 14 CFR Part 43, Appendix D.
PART 43 APPENDIX D INSPECTION ARCHITECTURE
┌─────────────────────────────────────────────────────────────┐
│ 14 CFR Part 43 Appendix D Minimum Scope │
└──────────────────────────────┬──────────────────────────────┘
│
┌──────────────────────────────┼──────────────────────────────┐
│ │ │
┌────────┴────────┐ ┌────────┴────────┐ ┌────────┴────────┐
│ Fuselage & Hull │ │ Cabin & Cockpit │ │ Engine Nacelle │
│ Group (Skin, │ │ Group (Cables, │ │ & Propeller │
│ Rivets, Frames) │ │ Flaps, Avionics)│ │ (Mounts, Leaks) │
└────────┬────────┘ └────────┬────────┘ └────────┬────────┘
│ │ │
┌────────┴────────┐ ┌────────┴────────┐ ┌────────┴────────┐
│ Landing Gear │ │ Wing & Center │ │ Empennage Group │
│ Group (Struts, │ │ Section Group │ │ (Stabs, Rudder, │
│ Brakes, Tires) │ │ (Spars, Tanks) │ │ Elevator, Trim) │
└────────┬────────┘ └────────┬────────┘ └────────┬────────┘
│ │ │
┌────────┴────────┐ ┌────────┴────────┐ ┌────────┴────────┐
│ Radio & Avionics│ │ Miscellaneous & │ │ Operational Run │
│ Group (Antennas,│ │ Emergency Equip │ │ & Functional │
│ Static Lines) │ │ (ELT, Flares) │ │ Systems Check │
└─────────────────┘ └─────────────────┘ └─────────────────┘
The 9 Major Inspection Groups of Appendix D
Appendix D organizes the complete aircraft into nine distinct technical zones, each requiring systematic visual and mechanical verification:
| Inspection Group | Key Inspection Scope & Specific Failure Modes |
|---|---|
| 1. Fuselage and Hull Group | • Structure, skin, stringers, formers, bulkheads, and pressure domes for corrosion, distortion, cracks, loose or missing rivets, and debonding.<br>• Systems and components installed within the fuselage, including hydraulic lines, electrical harnesses, and fuel tubing.<br>• Hull and floats (for seaplanes/amphibians) for integrity, water leakage, bilge pump operation, and corrosion.<br>• Drain holes, scuppers, and weep paths for unobstructed drainage. |
| 2. Cabin and Cockpit Group | • Cleanliness and loose equipment that could foul flight controls.<br>• Seats, seat tracks, positive locking pins, and safety belts/shoulder harnesses (TSO-C22/C114 tags, webbing fraying, inertial reels).<br>• Flight and engine controls for proper travel, free movement, correct stops, safetying, and friction adjustments.<br>• Instruments, glass condition, markings, range markings (red radial lines, green arcs), and pitot-static plumbing.<br>• Cabin heating, ventilation, and combustion heater safety shutoffs (carbon monoxide leakage risk).<br>• Doors, emergency exits, latching mechanisms, and environmental seals. |
| 3. Engine and Nacelle Group | • Engine mounts, vibration isolators (Lord mounts), and firewalls for cracking, distortion, and grounding bonding.<br>• Nacelle cowlings, baffles, and cooling cylinder fins for cracks and proper seal contact.<br>• Engine case, cylinders, accessories, and lines for fuel, oil, or hydraulic fluid leaks.<br>• Induction systems, air filters (carb heat/alternate air doors), and turbocharger clamps.<br>• Exhaust stacks, manifolds, mufflers, and internal heat exchanger shrouds for cracks, thinning, or CO leaks. |
| 4. Landing Gear Group | • Shock struts (oleo struts) for proper fluid/nitrogen extension height, scoring, and seal leakage.<br>• Retraction and locking mechanisms, linkage wear, uplocks, downlocks, and overcenter travel.<br>• Hydraulic cylinders, flexible brake hoses, valves, and mechanical linkages.<br>• Wheels, bearings (greasing and race spalling), brake discs, lining wear limits, tires (tread depth, cuts, uneven wear, dry rot).<br>• Gear doors, hinges, linkage rigging, and landing gear position microswitches. |
| 5. Wing and Center Section | • Primary structural members: main spars, auxiliary spars, drag/anti-drag wire rigging, ribs, and compression struts.<br>• Exterior skin (metallic or composite) for distortion, wrinkles (indicating structural overload), corrosion, or delamination.<br>• Movable surfaces: ailerons, flaps, slats, spoilers, and tab hinges for hinge-pin wear, free travel, balance, and bonding.<br>• Wing attachment fittings and critical spar carry-through bolts for torque witness marks and corrosion.<br>• Integral and bladder fuel tanks, vent lines, sumps, caps, and fuel selector valves. |
| 6. Empennage Group | • Fixed surfaces: vertical fin and horizontal stabilizer attachment fittings and alignment.<br>• Movable surfaces: rudder, elevator, and trim/servo tabs for play, binding, static mass balance, and travel limits.<br>• Fabric or metallic skin covering for deterioration, cracking, and rib-stitch integrity.<br>• Internal control horns, bellcranks, push-pull rods, pulleys, and trim-tab screw actuators. |
| 7. Propeller Group | • Propeller blades for nicks, gouges, cracks, erosion, and proper track (within 1/16 inch on typical GA props).<br>• Hub assembly, pitch-change mechanism, spinner, and backplate for cracking, grease/oil leakage, and safety wiring.<br>• Propeller mounting bolts for correct torque and cotter pinning. |
| 8. Radio & Instrument Group | • Antennas, blade fairings, mounting doublers, and coax connectors for secure attachment and low bonding resistance.<br>• Avionics racks, shock mounts, tray bonding straps, and harness routing.<br>• Pitot tube, static ports, and alternate static selector valves for obstruction and heater operation. |
| 9. Miscellaneous Items | • Emergency Locator Transmitter (ELT) installation, antenna security, and inspection per 14 CFR §91.207.<br>• First aid kits, survival equipment, fire extinguishers (gauge pressure and hydrostatic test dates).<br>• Required warning placards, compass correction cards, and FAA-approved Flight Manual (AFM/POH) on board. |
2. Regulatory Comparison: 100-Hour vs. Annual Inspections
A central concept tested extensively on FAA mechanic examinations is the precise regulatory distinction between the 100-Hour Inspection and the Annual Inspection under 14 CFR §91.409 and Part 43.
100-HOUR VS. ANNUAL INSPECTION
┌─────────────────────────────────────────────────────────────┐
│ Technical Scope: 14 CFR Part 43 App D │
│ (IDENTICAL TECHNICAL CHECKLIST SCOPE) │
└──────────────────────────────┬──────────────────────────────┘
│
┌──────────────────────────┴──────────────────────────┐
│ │
┌────────┴────────────────────────┐ ┌────────────────────┴────────────────────┐
│ 100-HOUR INSPECTION │ │ ANNUAL INSPECTION │
├─────────────────────────────────┤ ├─────────────────────────────────────────┤
│ • Required for aircraft: │ │ • Required for ALL civil aircraft │
│ - Carrying persons for hire │ │ (unless on progressive/AAIP/CAMP) │
│ - Flight instruction for hire │ │ • Interval: Every 12 calendar months │
│ (if aircraft provided) │ │ (expires last day of 12th month) │
│ • Authorized Sign-off: │ │ • Authorized Sign-off: │
│ - Certificated A&P Mechanic │ │ - Certificated Mechanic holding IA │
│ - Certificated Repair Station │ │ - Certificated Repair Station │
│ - Aircraft Manufacturer │ │ - Aircraft Manufacturer │
│ • 10-Hour Ferry Overflight │ │ • NO 10-Hour Overflight Allowance │
│ Allowance Permitted (§91.409b)│ │ (Requires Special Flight Permit) │
└─────────────────────────────────┘ └─────────────────────────────────────────┘
Comprehensive Regulatory Comparison Matrix
| Regulatory Parameter | 100-Hour Inspection | Annual Inspection |
|---|---|---|
| Governing Regulation | 14 CFR §91.409(b) | 14 CFR §91.409(a)(1) |
| Technical Scope | 14 CFR Part 43, Appendix D | 14 CFR Part 43, Appendix D (Identical) |
| Applicability Mandate | Required only for aircraft carrying any person (other than a crewmember) for hire, or provided by any person giving flight instruction for hire. | Required for all civil aircraft operating in the National Airspace System (except progressive/AAIP/CAMP). |
| Calendar Expiration | No calendar expiration; driven purely by tachometer / flight time (every 100.0 hours). | Expires at the end of the 12th calendar month following the month of the last inspection (e.g., done July 12, 2025 $\rightarrow$ expires July 31, 2026). |
| Authorized Approver | • Certificated A&P Mechanic (§65.81/§65.85/§65.87)<br>• Certificated Repair Station (Part 145)<br>• Aircraft Manufacturer | • Certificated Mechanic holding an Inspection Authorization (IA) (§65.95)<br>• Certificated Repair Station (Part 145)<br>• Aircraft Manufacturer |
| Overflight Allowance | Up to 10 hours strictly for the purpose of flying to a place where the inspection can be done (§91.409(b)). | NONE. An expired annual inspection immediately grounds the aircraft. Flying requires a Special Flight Permit (Ferry Permit) under 14 CFR §21.197. |
| Impact on Next Cycle | Excess hours flown (up to 10) must be deducted from the next 100-hour interval. | Not applicable (calendar month rule applies). |
| Cross-Credit Privilege | An Annual Inspection satisfies and resets the 100-hour inspection requirement. | A 100-hour inspection CANNOT substitute for an Annual inspection (unless signed by an IA who endorses it as an Annual). |
The 10-Hour Overflight Calculation Rule
The 10-hour overflight provision under §91.409(b) is frequently tested. The regulation states:
"The 100-hour limitation may be exceeded by not more than 10 hours while en route to reach a place where the inspection can be done. The excess time used to reach a place where the inspection can be done must be included in computing the next 100 hours of time in service."
Mathematical Example:
- An aircraft's previous 100-hour inspection was completed at 1,250.0 hours total time in service.
- The next 100-hour inspection is legally due at 1,350.0 hours ($1,250.0 + 100.0$).
- At 1,350.0 hours, the aircraft is at an outlying airport without maintenance facilities. The operator flies 6.4 hours to ferry the aircraft to the repair base, arriving at 1,356.4 hours.
- The 100-hour inspection is completed at 1,356.4 hours.
- When is the next 100-hour inspection due?
- The next inspection remains due at 1,450.0 hours, NOT 1,456.4 hours! The 6.4 overflight hours are absorbed by the next cycle.
3. Progressive & Commercial Inspection Programs
For high-utilization aircraft (such as busy flight school fleets or corporate flight departments), taking an aircraft offline for an extended Annual or 100-hour inspection causes significant operational disruption. The FAA provides alternative inspection frameworks under 14 CFR §91.409.
AIRCRAFT INSPECTION PROGRAM TIERS
┌─────────────────────────────────────────────────────────────────────────────┐
│ 1. Standard 100-Hour / Annual (14 CFR §91.409(a), (b)) │
│ • General aviation single/multi-engine piston aircraft │
│ • Complete teardown and inspection once per year / 100 flight hours │
└──────────────────────────────────────┬──────────────────────────────────────┘
│
┌──────────────────────────────────────┴──────────────────────────────────────┐
│ 2. Progressive Inspection Program (14 CFR §91.409(d)) │
│ • Divides annual inspection into staged phases (e.g., 4 phases / 90 days) │
│ • Entire aircraft completely inspected within 12 calendar months │
│ • Requires written FAA FSDO application and approved manual │
└──────────────────────────────────────┬──────────────────────────────────────┘
│
┌──────────────────────────────────────┴──────────────────────────────────────┐
│ 3. Approved Aircraft Inspection Program - AAIP (14 CFR §91.409(e)/(f), §135)│
│ • Large airplanes (>12,500 lbs MTOW), turbojets, multi-engine turbines │
│ • Tailored manufacturer maintenance schedule approved by FAA Principal │
│ Maintenance Inspector (PMI) for Part 135 on-demand operators │
└──────────────────────────────────────┬──────────────────────────────────────┘
│
┌──────────────────────────────────────┴──────────────────────────────────────┐
│ 4. Continuous Airworthiness Maintenance Program - CAMP (14 CFR Part 121/135) │
│ • Scheduled A, B, C, D structural checks, reliability programs, MSG-3 │
│ • Part 121 commercial scheduled airlines and large Part 135 commuter fleets│
└─────────────────────────────────────────────────────────────────────────────┘
Progressive Inspection Program Requirements (§91.409(d))
To adopt a progressive inspection program, the registered owner or operator must submit a written request to the local FAA Flight Standards District Office (FSDO) and meet the following statutory criteria:
- Supervision: The program must be supervised by a certificated mechanic holding an Inspection Authorization (IA), a certificated Part 145 repair station, or the aircraft manufacturer.
- Inspection Schedule & Manual: A comprehensive inspection schedule and procedures manual must be maintained, detailing the exact scope of each phase (e.g., Phase 1: Cabin/Cockpit; Phase 2: Engine/Nacelle; Phase 3: Wings/Empennage; Phase 4: Landing Gear).
- 12-Month Completion: The progressive schedule must ensure that the complete aircraft is completely inspected within 12 calendar months, satisfying the full scope of Part 43 Appendix D.
- Discontinuance: An owner may discontinue a progressive program at any time by notifying the FAA FSDO in writing. Upon discontinuance, the aircraft reverts to standard 100-hour/annual intervals, with the first annual inspection due within 12 calendar months from the date the progressive program was formally instituted or the last complete cycle completed.
4. Discrepancy Procedures & Owner Notification (§43.11)
One of the most critical legal concepts governing maintenance inspections is the protocol required when an aircraft is inspected and determined to be unairworthy due to severe structural damage, missing mandatory equipment, or outstanding Airworthiness Directives.
UNAIRWORTHY INSPECTION DISPOSITION
[ IA or A&P Conducts Inspection per 14 CFR Part 43 Appendix D ]
│
┌────────────────┴────────────────┐
▼ ▼
[ Aircraft AIRWORTHY ] [ Aircraft UNAIRWORTHY ]
│ │
│ ├────────────────────────┐
▼ ▼ ▼
Logbook Endorsement: Logbook Endorsement: Provide Signed &
"I certify that this "I certify that this Dated Discrepancy
aircraft has been aircraft has been List Directly to
inspected in accordance inspected in accordance Aircraft Owner
with an (Annual/100-Hr) with an (Annual/100-Hr) (14 CFR §43.11(a)(5))
inspection and was inspection and a list of
determined to be in discrepancies and un-
airworthy condition." airworthy items dated
[date] has been provided
to the owner/operator."
Critical Regulatory Realities Regarding Unairworthy Sign-Offs
- No Impoundment or Grounding Authority: A certificated mechanic or IA has no legal authority to impound an aircraft, seize logbooks, scrape registration decals, or confiscate the Standard Airworthiness Certificate (FAA Form 8130-7). The airworthiness certificate remains with the aircraft.
- Discrepancy List Delivery: Under 14 CFR §43.11(a)(5), the approving technician must deliver a signed and dated list containing all discrepancies and unairworthy items directly to the registered owner or operator.
- Logbook Entry Content: The technician makes an entry in the aircraft maintenance record stating the inspection was conducted and that a discrepancy list was provided to the owner. The specific unairworthy defects do not necessarily have to be transcribed in full into the permanent logbook, but the existence and date of the list must be recorded.
- Correcting Discrepancies: The aircraft owner is under no obligation to have the inspecting mechanic or IA repair the discrepancies. The owner may hire any certificated A&P mechanic to correct the unairworthy items. Once the individual items are repaired and signed off per 14 CFR §43.9, the aircraft is legally returned to service without requiring a new complete Annual inspection, provided the Annual inspection sign-off occurred within the preceding 12 calendar months.
Which of the following maintenance personnel is legally authorized under 14 CFR Part 65 to perform an Annual Inspection on a civil aircraft and approve it for return to service?
An aircraft subject to 100-hour inspections has its inspection completed at 2,400.0 hours. The aircraft is flown 106.0 hours before arriving at an inspection facility, where the next 100-hour inspection is completed at 2,506.0 hours. At what total time in service is the subsequent 100-hour inspection legally due?
During an Annual inspection, an IA discovers severe structural corrosion on the lower wing spar cap that renders the aircraft unairworthy. What action is legally mandated for the IA under 14 CFR §43.11?
Which operating document establishes the minimum checklist scope and technical detail required for conducting both 100-hour and Annual inspections on general aviation aircraft?