MIL-DTL-5096G
b. When an aircraft is removed from extended storage.
c. After ixed light surfaces have been replaced or removed for repairs and reinstalled.
d. After replacement or removal and reinstallation of engine main fuel control (single engine aircraft).
e. After movable light surfaces have been replaced or removed for repairs and reinstalled.
f. After light control cables, rods or actuators have been rerouted, rerigged, readjusted or
replaced. A single aileron actuator change does not normally constitute a requirement for
a functional check light.
g. On Fly-By-Wire aircraft, an FCF shall be performed at the discretion of the Logistics Group
Commander when work has been performed on the light control computers.
h. After a major structural modiication or repair is accomplished.
i. After extensive maintenance or repair is accomplished of such a scope that a test light is
determined to be necessary by the Logistics Group Commander.
j. After a propeller or propeller governor has been replaced and/or adjusted and reinstalled
(single engine aircraft).
k. After adjustments or changes have been made to the photo system requiring a light to insure
operational capability (although this is normally an "In Flight Check," certain weapon systems
may need an FCF to assure all photo systems are working correctly).
l. After three or more engines, on a four engine aircraft, two or more engines on a three engine
aircraft, or one engine on a two engine or less aircraft are replaced by new or completely
overhauled engines resulting from a single maintenance action.
3.2.2.3.4 Chapter 2, Section IV - Historical Documents (see Figure 6). This section shall contain a
listing of speciic weapon system components that require preparation of any of the historical documents
(AFTO Forms) prescribed by the 00-20-series technical orders. The listing shall be by work unit code,
nomenclature of components and form required.
3.2.2.4 Chapter 3, Replacement Schedule (see Figure 7). As speciied by the acquiring activity (see 6.2m.),
this chapter shall include those items and components that must be removed and changed for new or
overhauled like items at the expiration of a speciied number of lying hours, expiration of a number of
cycles, or an interval of calendar time. It shall include only those items that are readily identiiable for
record purposes and that fall in the following categories:
a. Items whose failure due to location or function within a system could compromise light safety
beyond reasonable limits and acceptable risk.
b. Items whose failure due to location or function within a system would cause an operational or
support mission to abort.
c. Items whose cost is high and whose failure might cause damage beyond economical repair.
d. Items whose physical characteristics are subject to deterioration from calendar time, lying
hours, cycles, operation, or usage.
e. Life sustaining items such as oxygen regulators, pressurization components, egress, or jettison
system components.
3.2.2.5 Chapter 4, Repair Restrictions. These restrictions do not apply to normal preventative maintenance
actions such as cleaning, reseating, etc.
NOTE: A part number shall be preceded by the Federal Supply Class (FSC).
3.2.2.5.1 Chapter 4, Section I - Base Level Restrictions (see Figure 8). This section shall contain a
listing of items by work unit code, noun, FSC and part number for which base level (organizational and
intermediate) repair restrictions are established. A description of repair restrictions shall be provided. Items
listed shall be limited to recoverable type items. Items which are Source, Maintenance and Recoverability
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