Forty-three elements, twenty-four of them knowledge — the second-widest knowledge-to-skill gap in Airframe. Four station elements.
1. S1 is regulated work with a legal trigger
Almost nothing else in the Airframe curriculum is a named, scheduled, regulation-mandated test. The static system leak check is.
K19 cites parts 43 and 91 directly: part 91 requires the test at an interval for certain
operations, and part 43 appendix
E prescribes the method and the
tolerance.
That makes it unusual and worth recognizing as such. It is not a technique you choose to apply when something seems wrong. It has:
- a legal trigger — an interval, and certain maintenance;
- a prescribed method — you may not substitute your own;
- a pass criterion — a stated leak rate over a stated time;
- a required record entry.
That is the whole chain GEN-I builds, arriving in one task. Learn it as an example of regulated work rather than as a plumbing check.
2. R5 — the test that destroys three instruments at once
The pitot-static system feeds the altimeter, the airspeed indicator and the vertical speed indicator. They share the plumbing.
Applying pressure or vacuum in the wrong place, in the wrong direction, or too fast damages all three simultaneously, and the damage is not visible. An over-pressured airspeed indicator has a stretched diaphragm; it still moves, and it now reads wrong.
The rules that follow:
- Never blow into a pitot or static line. Moisture and pressure both, and the pressure is uncontrolled.
- Apply and release slowly, and never exceed the instruments' ranges.
- Get the sense right: pressure to the pitot, vacuum to the static. Reversing them over-ranges instruments in the direction they cannot take.
- Isolate instruments the manual says to isolate before testing.
Three instruments, one mistake, no outward sign. That is why it is a risk element.
3. R4 — a dropped gyro is destroyed and still works
Handling of mechanical gyros or instruments containing mechanical gyros.
A gyroscopic instrument contains a rotor spinning in precision bearings. Dropping it — or knocking it, or setting it down hard — brinells the bearings.
And the instrument still spins. It runs, it indicates, it looks serviceable. It has a shortened life and degraded accuracy, and there is no test at the ramp that will tell you.
So gyros are handled as though they are fragile, always, and transported in their packaging. This is the same discipline as GEN-A Concepts §1's electrostatic handling: you will never receive feedback telling you it mattered, because the failure arrives later and somewhere else.
R1 is the related one: pressurized air and water in cleaning. Blowing out an instrument
panel with an air line drives water and debris into instruments and connectors.
4. Vacuum systems are a plumbing problem
K9, S10, S11. Candidates look for the fault in the gyro; most gyro failures are supply
failures.
The chain is: pump → filter → regulator → instruments → discharge. Anything that reduces airflow reduces gyro speed, and a slow gyro is an inaccurate gyro long before it is an obviously failed one.
The commonest cause is a clogged filter (S10), and the second commonest is a leak. Setting
the vacuum (S11) without checking the filter first sets the regulator to compensate for a
restriction, which masks the fault and shortens the pump's life.
Check the filter before adjusting the regulator. Always.
5. Range markings connect three subjects
K12, S3, S5 — and GEN-I S12, determine the conformity of instrument range markings
and placarding.
GEN-I decides what the markings should be, from the TCDS. This unit puts them on the glass and checks them. The two halves sit in different sections of the ACS and are one task.
Range markings are airworthiness data, not decoration. The green arc, the yellow arc, the red line — each is a limitation from the type design, and an instrument marked wrongly gives a pilot a limitation that does not apply to their aircraft.
A mark on the glass can also slip. S5 exists because a marking that has rotated relative to
the dial is worse than no marking: it looks authoritative and it is wrong. A slippage mark
across the glass and the case makes that visible, which is the same idea as
GEN-D Concepts §4's witness mark.
6. Six knowledge elements you will not meet
K13 electronic displays, K15 built-in test equipment, K16 EFIS, K17 EICAS, K18 head-up
displays.
No skill element touches any of them. Same pattern as welding in AF-A Concepts §1 and wood and fabric in AF-B Concepts §1: the ACS asks you to know technologies the certificate does not require you to work on.
Read them for what a mechanic actually needs: what the box does, what it is sensitive to, and
how to isolate a fault to it rather than through it. K15 — built-in test equipment — is the
practical one, because BITE is how you will interrogate a modern system, and its fault codes are
GEN-A Concepts §6's binary arriving in the real world.
7. What consumes this unit
| This unit | Is consumed by |
|---|---|
| Range markings | Arrives from GEN-I; feeds GEN-C limits |
| ESD handling | Arrives from GEN-A Concepts §1 |
| Bonding | AF-K Concepts §5, AF-I §2 |
| Pitot-static integrity | AF-L — heated pitot systems |
| Engine instrument principles | PP-D |
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