2.6 Type Certificate Data Sheets (TCDS), STCs, ACs & Maintenance Manuals
Key Takeaways
- Type Certificate Data Sheets (TCDS) and Aircraft Specifications are FAA-approved technical design baselines that define airspeed limits, weight/CG envelopes, approved engine/propeller combinations, datum location, leveling means, and control surface deflections.
- Supplemental Type Certificates (STCs) grant FAA approval for major design modifications to a type-certificated product, serving as approved data for major alterations.
- Advisory Circulars (ACs), such as AC 43.13-1B and AC 43.13-2B, provide acceptable methods, techniques, and practices for maintenance and minor repairs when manufacturer data is absent.
- Instructions for Continued Airworthiness (ICA) are manufacturer-developed, FAA-approved maintenance instructions required by 14 CFR § 21.50 for all newly type-certificated aircraft and STC alterations.
- The Air Transport Association (ATA) Spec 100 / iSpec 2200 numbering system standardizes maintenance manual chapter organization across the entire aviation industry.
2.6 Type Certificate Data Sheets (TCDS), STCs, ACs & Maintenance Manuals
Every aircraft operating in civil aviation is built and maintained against a rigid hierarchy of technical publications. A practicing aviation mechanic must be skilled in navigating and interpreting Type Certificate Data Sheets (TCDS), Supplemental Type Certificates (STCs), Advisory Circulars (ACs), Manufacturer Maintenance Manuals, and the ATA 100 / iSpec 2200 numbering system.
1. Type Certificate Data Sheets (TCDS) and Aircraft Specifications
When a manufacturer designs a new aircraft, engine, or propeller, the FAA evaluates the design against airworthiness standards (e.g., 14 CFR Part 23, 25, 27, 33, or 35). Upon successful certification, the FAA issues a Type Certificate (TC) and publishes the Type Certificate Data Sheet (TCDS) under 14 CFR Part 21.
KEY CONTENTS OF A TCDS / AIRCRAFT SPEC
┌────────────────────────────────────────────────────────────────────────┐
│ 1. MODEL DESIGNATIONS & CERTIFICATION BASIS (e.g., Part 23 / CAR 3) │
├────────────────────────────────────────────────────────────────────────┤
│ 2. ENGINE & PROPELLER COMBINATIONS (Approved models, ratings, limits) │
├────────────────────────────────────────────────────────────────────────┤
│ 3. AIRSPEED LIMITATIONS (Vne, Vno, Va, Vfe in KIAS/KCAS) │
├────────────────────────────────────────────────────────────────────────┤
│ 4. CENTER OF GRAVITY (CG) RANGE & DATUM LOCATION │
│ - Forward and aft CG limits, leveling means, empty weight CG limits │
├────────────────────────────────────────────────────────────────────────┤
│ 5. FUEL & OIL CAPACITIES │
│ - Total capacity, usable fuel, unusable fuel weight and arm │
├────────────────────────────────────────────────────────────────────────┤
│ 6. CONTROL SURFACE DEFLECTIONS (Travel limits in degrees ± tolerance) │
├────────────────────────────────────────────────────────────────────────┤
│ 7. MANDATORY PLACARDS & MINIMUM CREW REQUIREMENTS │
└────────────────────────────────────────────────────────────────────────┘
TCDS vs. Aircraft Specifications
- Aircraft Specifications: Documents issued prior to 1958 under the Civil Aeronautics Administration (CAA) for aircraft certificated under the Civil Air Regulations (CARs, such as CAR 3). Aircraft Specifications contain essentially the same technical data as modern TCDS.
- Type Certificate Data Sheets (TCDS): Documents issued by the modern FAA for aircraft certificated under Title 14 CFR.
Exam Fact: The TCDS is the ultimate authority for control surface travel limits, approved propeller diameter ranges, leveling means, and datum location. If there is a discrepancy between an aftermarket maintenance guide and the TCDS, the TCDS governs.
2. Supplemental Type Certificates (STCs)
Under 14 CFR Part 21 Subpart E, any person who alters a product by introducing a major change in type design that is not great enough to require a new application for a type certificate must apply for a Supplemental Type Certificate (STC).
- An STC represents FAA-approved data for that specific modification (e.g., installing a more powerful engine, adding winglets, converting to a glass cockpit avionics suite, or installing a cargo door).
- Permission to Use: Under 14 CFR § 21.120, an installer must have written permission from the STC holder to use the STC on a specific aircraft.
- Instructions for Continued Airworthiness (ICA): Under 14 CFR § 21.50(b), the holder of an STC must furnish at least one complete set of ICAs to the aircraft owner. These ICAs become part of the aircraft's permanent maintenance program.
3. FAA Advisory Circulars (ACs)
The FAA issues Advisory Circulars (ACs) under 14 CFR to provide guidance and acceptable methods in various aviation subjects. The numeric subject system corresponds to the FAR parts (e.g., AC 20 is General; AC 39 is Airworthiness Directives; AC 43 is Maintenance; AC 65 is Certification).
AC 43.13-1B and AC 43.13-2B
- AC 43.13-1B (Acceptable Methods, Techniques, and Practices — Aircraft Inspection and Repair): The "bible" of standard aviation maintenance practices. Contains acceptable methods for safety wiring, sheet metal riveting, electrical wiring, wood structures, fabric covering, and non-destructive testing (NDT).
- AC 43.13-2B (Acceptable Methods, Techniques, and Practices — Aircraft Alterations): Provides acceptable methods for structural alterations, radio installations, antenna mounting, and tow hitch installations.
- Legal Status: AC 43.13-1B/2B constitutes acceptable data, not approved data. It may be used as approved data for major repairs only when explicitly authorized by the FAA Administrator, an ASI Field Approval, or relevant FAA policy.
4. The ATA Spec 100 / iSpec 2200 Standardization System
The Air Transport Association of America (ATA) developed Specification 100 (now modernized as iSpec 2200) to standardize technical documentation across all manufacturers and aircraft types. Every maintenance manual, illustrated parts catalog, and wiring diagram follows this standardized chapter numbering format.
Comprehensive ATA Chapter Numbering Reference
| Chapter | Title / System Group | Major Subsystems & Components Included |
|---|---|---|
| ATA 05 | Time Limits / Maintenance Checks | Scheduled inspection intervals, life-limited components, overhaul time limits |
| ATA 06 | Dimensions & Areas | Aircraft stations, reference lines, zones, access panels |
| ATA 08 | Leveling & Weighing | Leveling points, jacking procedures, weighing procedures |
| ATA 11 | Placards & Markings | Exterior/interior warning decals, emergency exit markings |
| ATA 12 | Servicing | Routine fluid replenishment (oil, hydraulic fluid, oxygen, tire inflation) |
| ATA 20 | Standard Practices - Airframe | Torque values, safety wiring methods, cleaning procedures |
| ATA 21 | Air Conditioning & Pressurization | Heating, cooling, humidity control, cabin pressurization outflow valves |
| ATA 22 | Auto Flight | Autopilot, yaw damper, flight director, auto-throttle |
| ATA 23 | Communications | VHF/HF transceivers, cockpit voice recorder (CVR), audio panels, SATCOM |
| ATA 24 | Electrical Power | Generators, alternators, inverters, batteries, AC/DC distribution buses |
| ATA 27 | Flight Controls | Ailerons, elevators, rudder, flaps, trim tabs, control cables, rigging |
| ATA 28 | Fuel System | Fuel tanks, boost pumps, fuel quantity indication, valves, crossfeed lines |
| ATA 29 | Hydraulic Power | Hydraulic pumps, reservoirs, accumulators, filters, pressure relief valves |
| ATA 30 | Ice & Rain Protection | Deice boots, heated leading edges, windshield wipers, pitot-heat systems |
| ATA 32 | Landing Gear | Main/nose gear struts, retract actuators, brakes, wheels, tires, steering |
| ATA 34 | Navigation | Pitot-static instruments, VOR, ILS, GPS, weather radar, transponder |
| ATA 35 | Oxygen | Flight crew and passenger oxygen cylinders, masks, regulators |
| ATA 49 | Airborne Auxiliary Power (APU) | APU engine, generator, bleed air system, fire protection |
| ATA 51 | Standard Practices - Structures | Metallic/composite repair procedures, allowable damage limits |
| ATA 52 | Doors | Passenger doors, emergency exits, cargo doors, door warning sensors |
| ATA 53 | Fuselage | Skin panels, bulkheads, stringers, longerons, frame assemblies |
| ATA 55 | Stabilizers | Horizontal stabilizer, vertical fin, elevators, rudder structure |
| ATA 57 | Wings | Spars, ribs, wing skins, trailing/leading edge assemblies |
| ATA 71 | Powerplant - General | Engine cowlings, engine mounts, nacelle structure |
| ATA 72 | Engine (Turbine / Reciprocating) | Compressor, combustion chamber, turbine, pistons, cylinders, crankshaft |
| ATA 73 | Engine Fuel & Control | Fuel control unit (FCU), carburetors, fuel pumps, engine fuel filters |
| ATA 74 | Ignition | Magnetos, ignition exciters, spark plugs, igniter plugs, harnesses |
| ATA 77 | Engine Indicating | Tachometers, EPR, EGT, CHT, torque indicators, oil pressure/temp |
| ATA 79 | Engine Oil | Oil tanks, scavenge pumps, oil coolers, pressure relief valves |
| ATA 80 | Starting | Electric starters, pneumatic starter turbines, starter-generators |
Where can an aviation mechanic find the official FAA-approved control surface travel deflection limits and datum location for a newly certificated aircraft?
What is the primary regulatory standing of FAA Advisory Circular AC 43.13-1B during standard aircraft maintenance operations?
Under the standard ATA Spec 100 / iSpec 2200 indexing system, which chapter number is assigned to Aircraft Flight Controls (ailerons, elevators, rudders, flaps, and rigging)?