EASA Module 7 study materials
EASA Module 7 study resources

EASA Module 7 flashcards

EASA Module 7 · Build recall with a focused review session.

33 cards. Read the term and the definition here. The deck at the top of this page is optional.

FOD
Foreign Object Debris - any loose item that can damage aircraft or injure personnel; prevention requires tool control and inspection of intakes, controls and work areas.
Bonding during fuelling
Connecting aircraft, fuel source and earth with bonding leads before fuelling so that static electricity discharges safely instead of producing a spark.
Fire class D
Fire involving combustible metals such as magnesium or titanium; it requires a special dry powder extinguisher, because water or carbon dioxide can make it worse.
Torque wrench calibration
Torque wrenches must be calibrated at intervals stated in the maintenance organisation's procedures, typically every 12 months and after overload or drop.
Lockwire direction
Safety wire is installed so tension pulls the fastener clockwise, in the tightening direction; twisting the wire the wrong way can loosen the fastener.
Helicoil insert
A coiled stainless-steel insert fitted into a drilled and tapped oversize hole to restore a damaged internal thread to its original nominal size.
Micrometer reading
Read the barrel main scale in millimetres, then add the thimble reading multiplied by 0.01 mm; verify the zero setting before measuring.
Torque formula
Torque equals force multiplied by the perpendicular distance from the pivot (T = F × d), expressed in newton metres or pound-feet.
Calibration traceability
A chain of comparisons linking an instrument's calibration to a national or international standard, recorded on a certificate with an expiry date.
Third-angle projection
A drawing convention in which each view is placed on the side of the object from which it is viewed; common on US and some Asian drawings.
ATA 100 chapters
A standard numbering system grouping aircraft systems into chapters, such as 27 for flight controls and 32 for landing gear, used in manuals.
Drawing title block
The area of a drawing giving drawing number, part number, scale, revision, sheet number and approvals; work must follow the latest revision.
Clearance fit
A fit in which the largest permissible shaft is smaller than the smallest permissible hole, so a gap always exists between the assembled parts.
Interference fit
A fit in which the smallest permissible shaft is larger than the largest permissible hole, requiring force or a temperature change to assemble.
Allowance
The intentional difference between the nominal sizes of mating parts; minimum clearance in a clearance fit, or maximum interference in an interference fit.
AWG wire size
American Wire Gauge number indicating conductor cross-section; a smaller number means a thicker wire with greater current-carrying capacity.
Bonding resistance
The electrical resistance between bonded aircraft structure and equipment, typically required to be 2.5 milliohms or less for primary structure.
Megohmmeter test
An insulation resistance test applying a specified DC voltage to a circuit to detect moisture, contamination or damaged insulation; low readings indicate a fault.
EWIS separation
Routing power and signal wires apart to prevent electromagnetic interference; where separation cannot be kept, wires cross at right angles.
Rivet edge distance
The distance from the centre of a rivet hole to the edge of the sheet, normally at least two rivet diameters to prevent tear-out.
AN flare angle
Standard aviation hydraulic flare fittings use a 37-degree flare; SAE 45-degree fittings are not interchangeable with them and must not be mixed.
Turnbuckle safety
A turnbuckle adjusting control cable tension must be secured with lockwire or a locking clip after adjustment to prevent rotation in service.
Bearing preload
An axial or radial load applied during assembly to remove internal clearance; excessive preload causes overheating and premature bearing failure.
Spring rate
The force required to compress or extend a spring by unit length, expressed in newtons per millimetre and used to check springs against specification.
Brazing temperature
Brazing uses a filler metal that melts above 450 degrees Celsius but below the melting point of the parent metal, unlike soldering.
Hydrogen embrittlement
A condition in which hydrogen absorbed during plating, welding or pickling makes high-strength steel brittle; baking after processing reduces the risk.
Welding symbol
A drawing symbol showing weld type, size, length, spacing and finish, placed on a reference line with an arrow pointing to the joint.
CG formula
Centre of gravity equals total moment divided by total weight, where each moment is the item weight multiplied by its arm from the datum.
Weight shift formula
Moving a weight changes the centre of gravity by the amount (weight moved × distance moved) divided by the total aircraft weight.
Datum
A fixed reference point or plane on the aircraft from which all weight and balance arms are measured; arms forward of it are negative.
Dye penetrant inspection
A non-destructive test for surface-breaking defects: penetrant enters cracks, is cleaned from the surface, then drawn out by developer and inspected.
Torque sequence
The order in which fasteners are tightened, usually crisscross or from the centre outward in stages, to distribute clamping load evenly.
Rigging check
Verifying that control surface travel, cable tension and clearances match the maintenance manual throughout the full range of movement.