Design the inspection, perform it, record it

Terms on this page 9

Dotted in the text; open one for its entry, or see the glossary.

Twenty-one elements, and five of the seven skills need the aircraft and its complete records. This is the synthesis unit of Airframe, taught last, and it is the closest the certificate comes to assessing what an A&P actually does.


1. Two elements are higher-order than anything else in Airframe

S5 Provide a checklist for conducting a 100-hour inspection
S6 Determine if any additional inspections are required during a particular 100-hour inspection (i.e., 300-hour filter replacement)

S5 is producing the instrument, not following one. Most of the certificate asks you to execute a procedure someone else wrote. This asks you to write it — from part 43 appendix D, which sets the scope, and from the manufacturer's inspection program where one applies.

S6 is scoping. It asks whether anything reaches into this airplane on this day beyond the routine list: an AD now due, a service bulletin the owner has adopted, a life-limited part approaching its limit, a special inspection triggered by an event — a hard landing, a lightning strike, an overspeed.

Then S1 and S2 perform, and S3 records.

Design, perform, record. Teach the unit in that order rather than in ACS order, because that is the order the work happens in and each stage depends on the one before.


2. R1 — both directions are failures

Interpretation of inspection instructions, which can lead to over or under maintenance being performed.

Under-maintenance is the obvious failure: something in scope was not inspected.

Over-maintenance is a failure too, and it is the one nobody warns you about. Disassembly that was not required introduces the errors that reassembly introduces — a fastener not torqued, a seal disturbed, a connector not fully seated, a part damaged coming out. And it is invisible as a defect, because the aircraft is, if anything, more inspected than the rule demands.

A candidate who reads the scope correctly does less work and produces a better result. That is counter-intuitive and worth saying explicitly, because the instinct under uncertainty is to open more up.

The discipline: the scope is defined before the inspection starts, from appendix D and the manufacturer's program, and anything beyond it is a decision with a reason, not a default.


3. It is GEN-I applied to an airplane

K1, K2, K3, K6, K8 all restate GEN-I. S4 restates GEN-I's AD applicability. K9 restates GEN-G.

That repetition is deliberate on the ACS's part and should not become repetition in the teaching. Learn the regulation once, in GEN-I, and apply it here.

What AF-D adds is the airplane and the logbook. A regulation read in isolation is a rule; the same regulation applied to a specific aircraft with a specific history is a judgment, and the judgment is what this unit assesses.

GEN-I Concepts §5 argues that record entries should be made at the end of real work rather than as paperwork exercises. S3 is where that lands: a 100-hour entry made after performing the inspection, tired, with the work behind you — which is exactly the condition R5 and GEN-I's R3 describe.


4. An inspection entry states a conclusion

K2 and S3, and the distinction that catches people.

A maintenance entry says what you did. This work was performed, to this data, and it is approved for return to service for that work.

An inspection entry says what you found. This aircraft was inspected in accordance with this scope, on this date, at this time in service, and was determined to be airworthy — or was found unairworthy, and here is the list of discrepancies provided to the owner.

An inspection entry without a determination is not an inspection entry. It is a note saying you looked at an airplane. GEN-I Procedures Procedures 6 and 7 keep these separate for that reason.


5. Life limits are a different kind of rule

K4, and candidates resist it.

A life-limited part comes off at a number, regardless of condition. Not when it is worn, not when it fails an inspection — at a stated time or cycle count. It may look perfect. It usually does.

The condition-based intuition that governs everything else in maintenance does not apply, and that is the whole point: these are parts whose failure mode is not detectable by inspection, which is why they are managed by time instead.

That puts life-limited parts alongside fire bottle hydrostatic dates (AF-M §2), ELT batteries, and composite resin shelf life (AF-B Concepts §3): time-based airworthiness that no inspection reveals.


6. What consumes this unit

This unit Is consumed by
The regulation Arrives from GEN-I
Inspection technique Arrives from GEN-K
Corrosion identification Arrives from GEN-G
Scope and checklist production PP-C — the engine equivalent
The record entry GEN-I Procedures Procedure 7

This is the last unit of Airframe because it consumes all of them.

License

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