personnel, or cause injury to personnel on deck not
paying attention to what is happening around them.
Pendant Retraction
The retracting cycle of the deck pendant is
normally executed at full speed. The operator, prior to
pulling the retracting lever, must ascertain that no
personnel or equipment are in a position to be struck
during
retraction.
If
for
any
reason
a
sudden
interruption of the retracting cycle occurs, the same
precaution must be taken prior to the resumption of the
retraction cycle.
Wire Supports
Broken or deformed wire supports should be
replaced as soon as practical.
Stanchions
Personnel should stay clear of areas where
stanchions are being raised or lowered, and particularly
when barricades are being raised or lowered. When
stanchion repair is to be effected, the stanchions safety
brace must be installed.
Terminals, Fittings, and Cables
Frequent inspection of all cables, terminals, and
fittings should be maintained. Any indication (no
matter how slight) of failure should be corrected
immediately. Particular attention should be given to
terminals jamming sheaves. Any condition where this
is evident is extremely critical. The unit involved
should not be operated until correction of the condition
is made.
Sheaves and Winches
Generally all sheaves should be free running, have
no indication of turning of the lips, or indication of
jamming by terminals. No slippage of the sheave on
races should be evident, and any fault of this nature
should be corrected. Winches should be checked for
running and positioning. Both sheaves and winches
should be kept clean of debris or foreign matter, and be
regularly lubricated.
BELOW DECKSTHE ARRESTING ENGINE
The greatest safety factor in the operation of the
arresting engine is constant attention to inspection,
maintenance, and overhaul. Preventive maintenance is
particularly necessary. Daily inspection, inspection
after each arrestment, and depending on the unit
involved, inspection and maintenance at regular
intervals nullify many of the conditions that might arise
to endanger operating and flight personnel. Always
keep hands and body clear when engine is operating or
in a condition to become operable.
Weight Selector Settings
The safe arrestment of incoming aircraft can be
directly attributed to proper setting of the aircraft
weight selector. Aircraft weight selector settings should
always be made according to current aircraft recovery
bulletins. Maximum efficiency is obtained from the
arresting engine through proper weight settings. There
is one distinct error in arrestment that can be directly
attributed to improper weight settings or error in the
gross
weight
estimate.
This
error
results
in
TWO-BLOCKING the engine.
TWO-BLOCKING is a condition in which the
weight selector is set too light for the incoming aircraft.
This condition causes the ram to ride forward into the
cylinder until the crosshead bangs into the mouth of the
cylinder. A wooden block assembly, called a ram block,
is positioned at the crosshead end of the ram to act as a
shock absorber by preventing metal-to-metal contact
between the crosshead and the mouth of the cylinder.
BOUNCEBACK is the movement of an arrested
aircraft backward and is caused by the stretch inherent
in the purchase cables. Bounceback is desirable
because the hook is disengaged, allowing rapid deck
clearance for future landings. Pilots are instructed to
allow for bounceback before braking.
Control Valve Failure
Prime
failure,
with
resultant
disastrous
consequences, could be failure of the drive system that
would result in improper opening or closing of the CRO
valve. Cam alignment is equally important, as improper
alignment would result in fluid flow through the CRO
valve at a ratio different from that indicated on the
aircraft weight selector indicator. Thus, while the
operator would have an indication of a proper setting,
actual flow control would be different.
Drive System Hazards
Much of the cable system is contained behind
U-channels to protect personnel during operation. This
cable, with connections, is subject to wear and fatigue
3-61