12.2 Reading Type Data: Serial-Number-Specific Lookups & Interpreting Notes
Key Takeaways
- Type certificate data sheets and Aircraft Specifications are organized by model, with serial number ranges and numbered Notes that make the eligible configuration serial-number specific.
- Weight and balance data on a data sheet, including the weight and arm of unusable fuel and undrainable oil, is read from the model section that covers the specific serial number.
- When an aircraft's empty weight center of gravity falls within the empty weight CG range published on the data sheet, computation of critical forward and aft CG positions is unnecessary.
- Required equipment is identified in the data sheet's equipment section and Notes, and an item listed as required must be installed for the aircraft to conform to type design.
- Where the data sheet does not carry an item such as the marking and placard list, the approved flight manual for that model supplies it, and 14 CFR 91.9 makes those markings and placards mandatory.
12.2 Reading Type Data: Serial-Number-Specific Lookups & Interpreting Notes
[!NOTE] The IAR test supplies the data; it grades the lookup. The Computer Testing Supplement for Inspection Authorization provides excerpts of data sheets, specifications, ADs, and charts. Nothing in this section needs to be memorized aircraft by aircraft. What must be automatic is the method: identify the model section, confirm the serial number falls in range, apply the Notes, and read the right line.
Section 4.2 established what a TCDS and an Aircraft Specification are. This section is about working them.
How a Data Sheet Is Organized
Every FAA data sheet follows the same skeleton, and knowing it turns a five-minute hunt into a fifteen-second lookup:
HEADER Sheet number, revision number and date, TC holder, models covered
|
v
MODEL SECTION Repeated once per model (e.g., "I - Model J3C-40", "II - Model J3C-50")
| Within each model section, in a consistent order:
| Engine
| Fuel
| Engine Limits
| Propeller and Propeller Limits (diameter max/min, static rpm)
| Airspeed Limits
| C.G. Range
| Empty Weight C.G. Range
| Maximum Weight
| Number of Seats (with arms)
| Maximum Baggage (with arm)
| Fuel Capacity (with arm)
| Oil Capacity (with arm)
| Control Surface Movements
| Serial Nos. eligible
v
DATA PERTINENT TO ALL MODELS Datum, leveling means, certification basis,
production basis, equipment
|
v
NOTES Numbered notes that modify, restrict, or extend the data above
Two structural facts drive most lookup errors. First, the model section is authoritative for that model and does not carry over to the next model — engine limits for a J3C-50 tell you nothing about a J3C-65. Second, the Notes are not commentary; they are part of the approved data and frequently narrow eligibility by serial number.
Serial Number Eligibility
Each model section ends with the serial numbers eligible under it, and Notes commonly carve out subsets. A worked example from Aircraft Specification A-691 (Piper J-3 series) shows the pattern: the base model carries a CG range of (+10.6) to (+22.7), and Note 3 lists specific serial numbers that are eligible only with a restricted CG range of (+10.6) to (+21.5) as a landplane, with different limits on floats.
For the IA this is the whole ballgame:
- Read the data plate, not the paperwork, for the serial number.
- Find the model section that lists that serial number.
- Read every Note referenced in that section, and scan the Notes for any that name serial numbers.
- Apply the most restrictive applicable value.
Skipping step 3 produces confidently wrong answers, because the base data looks complete on its own.
Extracting Weight and Balance Items
Data sheets carry the constants that a weight and balance revision depends on, and the exam asks for them directly:
| Item on the Data Sheet | What It Gives You | Where It Is Used |
|---|---|---|
| Datum | The reference plane for all arms | Every moment calculation (Section 6.1) |
| Leveling means | How to level the aircraft for weighing | Weighing procedure |
| Empty Weight C.G. Range | The range within which adverse checks are unnecessary | Section 6.1 and 6.2 |
| C.G. Range | Forward and aft flight limits, often varying with weight | Adverse loading checks |
| Maximum Weight | Certificated gross weight, sometimes by category | Loading and alteration limits |
| Number of Seats (with arms) | Seat count and station | Adverse loading checks |
| Maximum Baggage (with arm) | Compartment limit and station | Adverse loading checks and placards |
| Fuel Capacity (with arm) | Total capacity, usable/unusable split, fuel arm | Empty weight, minimum fuel |
| Oil Capacity (with arm) | Oil quantity and station | CAR 3 vs Part 23 oil accounting |
Unusable fuel and undrainable oil deserve special mention because they are the most commonly asked lookup. Empty weight includes unusable fuel (Section 6.1), so the data sheet's weight and arm of unusable fuel are inputs to the empty weight and empty weight moment. A question asking for "the location for weight and balance purposes of any unusable fuel" on a specific serial number is asking you to find the right model section, check the Notes for a serial-number-specific value, and read the arm.
The EWCG range shortcut, stated on the data sheet itself in the classic formula: "When empty weight C.G. falls within range given, computation of critical fore and aft C.G. positions is unnecessary." That sentence — printed on the specification, not merely a handbook convention — is the regulatory basis for the adverse-check exemption discussed in Section 6.1. Note the caveat that usually follows it: the range is not valid for non-standard arrangements.
Interpreting the Notes
Notes carry the operational meat. Common Note types and what they do:
| Note Type | Typical Content | Why the IA Cares |
|---|---|---|
| Weight and balance note | Requires a current weight and balance report and equipment list | Establishes the required records |
| Placard note | Lists the exact placards required, with wording | § 91.9 makes them mandatory; missing placards ground the aircraft |
| Serial number note | Restricts limits or eligibility for named serial numbers | Changes the answer for that airplane |
| Equipment note | Identifies required versus optional equipment | Conformity to type design |
| Engine/propeller note | Adds eligible combinations or weight changes for a given installation | Conformity and W&B |
| Fuel note | Approved grades, and any restrictions such as unleaded prohibitions | Airworthiness and placarding |
| Ferry/overweight note | States conditions under which overweight ferry is structurally acceptable | Special flight permit support |
A useful discipline: read the Notes before the model data, not after. Notes reframe what you are about to read, and reading them last means re-reading everything.
When the Data Sheet Does Not Have It
Not everything lives on the data sheet, and knowing where else to look is itself an exam topic.
- Marking and placard lists for many later aircraft are carried in the FAA-approved Airplane Flight Manual rather than in the TCDS Notes. The certification rules require operating limitations to be furnished in the form of placards, markings, and manuals, so on a modern airplane the AFM is the authoritative list. If a data sheet is silent on placards, the approved flight manual — not the maintenance manual and not the sales literature — is the next document.
- Operating limitations for an aircraft whose TCDS does not itemize them are found in the approved flight manual.
- Instructions for Continued Airworthiness, including any Airworthiness Limitations Section, come from the design approval holder under § 21.50(b), not from the data sheet (Chapter 7).
- Required equipment for a kind of operation comes from the Kinds of Operations Equipment List in the AFM and from § 91.205 (Section 7.3), not from the data sheet.
A Repeatable Lookup Procedure
1. Read the data plate: make, model, serial number.
2. Open the correct data sheet and confirm the REVISION DATE in the header box.
3. Locate the model section that lists this serial number.
4. Read every Note that section references, plus any Note naming serial numbers.
5. Read the specific line asked for (engine, arm, capacity, travel, seats).
6. Apply the most restrictive applicable value.
7. Cross-check against the aircraft's records for STCs or 337s that changed it.
Step 7 is the one an inspector adds that a test-taker sometimes forgets: the data sheet describes the aircraft as type certificated. Approved alterations legitimately move the aircraft away from that baseline, and the current approved configuration is the data sheet plus the STCs and Form 337s in the records.
High-Yield Exam Traps
- Serial number governs. Model alone is not enough; Notes routinely restrict specific serial ranges.
- The revision date is in the box on page one, and it is the date of the most recent revision.
- Unusable fuel has both a weight and an arm, and both are on the data sheet.
- "When empty weight C.G. falls within range given, computation of critical fore and aft C.G. positions is unnecessary" — and the range is not valid for non-standard arrangements.
- If the data sheet is silent on placards or operating limitations, go to the approved flight manual, not to the maintenance manual.
- The data sheet is the type-certificated baseline; approved STCs and 337s in the records modify it.
An IA performing an annual inspection cannot find the required marking and placard information in the Type Certificate Data Sheet for a late-model airplane. In which document should the IA look next?
An Aircraft Specification states an Empty Weight C.G. Range and adds the sentence: 'When empty weight C.G. falls within range given, computation of critical fore and aft C.G. positions is unnecessary. Range is not valid for non-standard arrangements.' What does this permit, and what limits it?
When determining the eligible engine models and center of gravity limits for a specific airplane, why is the serial number, rather than the model designation alone, decisive?