Pilot’s Manual
PM-126A 7-5
The pedestal is typically equipped with a single flight management
system (FMS), a trim control panel, a weather radar control panel and
an engine/fuel control panel. Optional equipment in the pedestal may
include a second (dual) FMS, a high frequency comm control head, a
SELCAL control panel, an Auxiliary Power Unit (APU) control panel,
an Emergency Locator Transmitter (ELT) switch, and a 12-vdc cigarette
lighter.
An inflatable harness type oxygen mask with an integral microphone is
stored on the outboard side of each crew seat. Smoke goggles are stored
in the left and right lower sidewall storage compartments. Hand-held
fire extinguishers are installed on the crew seats directly behind the
pilot’s and copilot’s legs. Life vests are stowed inside plastic holders
which are mounted to cabinets located directly behind each crew seat.
A magnetic compass is installed on the windshield center post near the
top of the windshield. The headliner houses a dome light, air outlets,
an assist handle and an access for a plumb bob location for leveling the
aircraft. An optional sunvisor may also be attached to the headliner. No
switches, instruments or placards are located overhead. Circuit breaker
panels are located on the pilot and copilot upper sidewall panels. A
flexible map light is attached to the upper sidewall above the circuit
breaker panel on each side. Cabin and spot light control switches are located
adjacent to the copilot’s circuit breaker panel. Flashlights are installed
on the cabinet behind each crew seat. Air outlets are installed in
the cockpit sidewall panels and lower forward cockpit side panels.
Storage compartments are built into the lower sidewall panels for
charts and Jeppesen manuals. Drink holders are attached to the forward
side of the storage compartments. Additional manual storage is
provided in the left storage cabinet located behind the pilot’s seat.
CREW SEATS
The crew seats (Figure 7-2) are comprised of three basic structures: the
seat base, the seat bottom and the seat back. The seat base is attached to
and travels on the seat tracks. The seat bottom is located above the seat
base and provides controls for forward/aft movement, seat height
adjustment and seat back reclining adjustment. The seat back contains
the lumbar adjustment control, adjustable armrests and an adjustable
headrest.
The crew seats are constructed of lightweight alloys covered with foam
padding and sheepskin and are equipped with a five point restraint
system. The lap belts and negative-G strap are mounted to the seat
bottom. The rotary buckle is attached to the outboard lap belt. The manual
lock/unlock handle for the shoulder harness belts is located on the
inboard side of the seat back frame.
Pilot’s Manual
7-6 PM-126A
Seat height adjustment is accomplished by pulling up on the vertical
adjustment control lever located under the forward edge of the seat
bottom near the outboard side of the seat. When the lever is pulled, the
mechanism is unlocked and the seat will move downward under the
occupant’s weight. To raise the seat, remove occupant weight from the
seat while pulling up on the lever. Gas cylinders will cause the seat to
automatically raise up. Release the lever at the desired height to lock
the seat into place.
Forward and aft adjustment of the seat is accomplished by pulling up
on the fore/aft adjustment control lever located under the forward
edge of the seat bottom near the inboard side of the seat. The seat can
be moved by holding the control lever up, and at the same time, sliding
the seat forward or aft on the seat tracks. When the desired position is
obtained, the control lever can be released to lock the seat to the seat
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