Lectrogram - Issue 4
Author: Lectromec
Published: 08-01-2004
Lectromec
LECTROGRAM
August
2004 Newsletter
A Resource for your Wire Maintenance Program
When it comes to wiring maintenance, consider the
basic rule in medicine: “First, do no harm.” But where to
find the best guidance to avoid inadvertent maintenance malpractice?
Fortunately, for those in need of a quick reference, the Federal
Aviation Administration (FAA) has produced a single, well-illustrated
document known as the Aircraft Wiring Practices Job Aid 1.0. It
presents essential examples of good, bad and outright dangerous
wiring practices.
Job Aid 1.0 is an outgrowth of the need for better
training in wiring maintenance identified by the Aging Transport
Systems Rulemaking Advisory Committee (ATSRAC). The inspections done
by the members of this government-industry task force showed that
wire ages in service, it can be abused during maintenance, and that
the problems fall into clear categories of improper installation,
aging or traumatic damage. Job Aid 1.0 offers cautionary cases of
what to avoid while illustrating “best practices” for
prudent and proactive wiring maintenance, modification or
modernization.
1. Thou shalt not consider wire as immortal.
At least a half-dozen agents of aging are involved: degraded wire
repairs or splices, heat-damaged or burnt wire, vibration damage or
chafing, cracked insulation, arcing, and delaminated insulation.
2. Thou shalt hold Job Aid 1.0 as the first
guidance before thee. Job Aid 1.0 warns that there are many
texts: “For now, there is no one rule or AC [advisory circular]
that ties everything together.” But Job Aid 1.0 may come
the closest of any of the materials produced to date. Moreover, it
points out conflicting information that can mislead the layman. For
example, one AC says the circuit breaker must protect against any
downstream component failure. But this same AC also says that
breakers are designed such that they DO NOT protect components. Job
Aid 1.0 clarifies the matter: “Breakers are sized to protect
the aircraft wiring as the main design constraint.” Job Aid 1.0
also notes that most circuit breaker (CB) failures are latent in
nature, “So you won’t know they have failed until you
need them.”

3. Thou shalt not take proven wiring routing
practices in vain. The overarching guidance in Job Aid 1.0 is to
eliminate the potential for chafing against structure or other
components. Above all, the doctrine of three applies: wires should
not ride on structure, wires should not ride on other wires, and
wires should not ride on weight-reducing lightening holes cut into
bulkheads, ribs, spars, etc.
4. Thou shalt honor clamping criteria.
Supporting the wiring with proper clamping can minimize the
deleterious effects of vibration and mechanical strain. As a general
rule, support clamps should be spaced at least every 24 inches.
In high vibration areas, or locations where the
wiring must be routed around structural intrusions, the clamping
intervals should be reduced. To minimize strain at the terminal, some
slack should be allowed between the last clamp and the termination of
a wire run.

5. Thou shalt not crimp or crush wire. The
operative rule-of-thumb is that when the wire is properly clamped,
the fitting will be snug enough to prevent the wiring from sliding
freely through the clamp, but not so tightly clamped that the wire
won’t move when a light tug is applied.
6. Thou shalt not adulterate bend radii.
Insulation is put under strain when a wire bent at too sharp a
radius, which can lead to accelerated topcoat flaking and breaches in
the insulation. For a bundle of wires, the minimum bend radius must
not be less than 10 times the outside diameter of the largest wire in
the bundle.
7. Thou shalt not bear false witness to unsafe
wiring. In other words, there are times when the wiring’s
condition cannot be overlooked or ignored and replacement is in
order. Here are some of the conditions in which wire replacement is
in order: it’s chafed or frayed; the insulation has been
penetrated to conductor; the insulation is so brittle that slight
flexing causes it to crack; discoloration shows that the insulation
has been heat-damaged; sections of the wire have been spliced at less
than 10-foot intervals.
8. Thou shalt not splice unless necessary.
Splicing of wire should be kept to a minimum and avoided entirely in
locations subject to high vibrations. In these areas, even well
supported, clamped and semi-tautened wiring may experience
accelerated wear (e.g., chafing).
9. Thou shalt covet true terminals. The
beginnings and endings of wiring are as important as the routing and
support in between. Connectors and terminals in aircraft require
special attention to ensure a safe installation. Electrical system
malfunctions frequently have been traced to poor terminal
connections. For example, loose contacts can produce localized
heating that may ignite nearby combustible materials or inflict heat
damage on the insulation of adjacent wiring.
10. Thou shalt clean as thou goest. If
“cleanliness is next to Godliness” for the human body,
cleanliness of aircraft wiring is essential for safety. Job Aid 1.0
urges a basic standard: keep wiring clean throughout the life of the
aircraft.
Job Aid 1.0 was produced to “preclude accidents
that may result from wire degradation.” In this respect, Job
Aid 1.0 exemplifies a basic precept – the devil is in the
details.
Job Aid 1.0 :
www.academy.jccbi.gov/AIRDL/wiringcourse