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and applicable displays.
D. Limitations:
The approved limitations from the Airplane Flight Manual (AFM) are
repeated in this module to provide flight crews with a ready source of
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limitations information directly related to the system being studied.
Additional limitations, not included in the AFM, will also be presented in this
module. Observance of these limitations will increase the service life of the
airplane and prevent equipment damage.
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DIMENSIONS AND AREAS, MAJOR COMPONENT LOCATIONS
2A-06-10: General
1. Aircraft:
The Gulfstream IV is a twin engine, swept wing, long range, high speed aircraft. It
is a pressurized, transport category aircraft, certified to operate at altitudes up to
45,000 feet. Certification of the aircraft is based on Federal Aviation Regulation
(FAR) Part 25.
Two Rolls-Royce Tay 611-8 high bypass ratio turbofan engines, mounted on
pylons located on the aft upper fuselage, power the aircraft. Each engine
produces 13,850 lb of rated takeoff thrust (5 minutes maximum) at sea level on a
standard day.
An AiResearch GTCP36-100(G) Auxiliary Power Unit (APU) provides bleed air for
air conditioning and engine starting, and AC power for the aircraft electrical power
system.
2. Fuselage:
The fuselage is of semimonocoque metal construction, with five distinct sections
spliced together to form a single structure. All areas are pressurized with the
exception of the nose radome and aft equipment (tail) compartment. The fuselage
is divided lengthwise into an above-floor section and a below-floor section. For the
purposes of this manual, the fuselage is divided into six compartments as follows:
A. Nose Compartment:
The unpressurized nose compartment extends forward from the forward
pressure bulkhead. It includes an avionics rack and a fiberglass
honeycomb radome. In addition to its aerodynamic necessity, the radome
serves to cover and protect the weather radar and glideslope antennas.
Conductive strips on the radome provide an electrical bond to the aircraft to
minimize lightning strike damage and prevent static accumulation.
B. Cockpit:
The cockpit extends from the forward pressure bulkhead to the entrance
compartment. It includes a pressurized flight compartment and an
unpressurized nose wheel well.
The cockpit is conventionally arranged and contains two flight crew stations
with individually adjustable seats. The logical arrangement of each station
allows easy access to all aircraft controls and displays. A two-piece,
electrically heated, bird-proof and splinter-proof windshield and two fixed
side windows enclose the cockpit.
See Section 2A-06-40, Flight Crew Station Components, for a description
of the cockpit compartment.
C. Entrance Compartment:
The entrance compartment is located immediately aft of the cockpit
bulkhead. It contains the left and right radio racks and main entrance door.
See Section 2A-52-20, Main Entrance Door, for a description of the main
entrance door.
D. Passenger Cabin:
The passenger cabin is pressurized and air conditioned. Depending on
outfitting and configuration, the passenger cabin may seat up to 19
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passengers.
Cabin outfitting is installed by either a furnishing agency or the airframe
manufacturer according to the owner-operator specifications. The majority
of the configurations, however, provide for a 30 inch cabin aisle, with galley
and lavatory areas located aft of the main cabin area.
The location and number of cabin windows and emergency exits differs
based upon whether or not an optional cargo door is installed. Cabin
windows and emergency exits are discussed briefly in Section 2A-06-30,
Entrances, Exits and External Access Doors, and in greater detail in
Section 2A-52-30, Emergency Exits.
E. Baggage Compartment:
The baggage compartment is located immediately aft of the passenger
cabin and galley area. The aft pressure bulkhead serves as the aft wall of
the baggage compartment. An inward opening, plug-type baggage
compartment door is installed on the left side. It may be opened from either
inside or outside the aircraft. See Section 2A-52-40, Baggage Doors, for a
description of the baggage door.
F. Tail Compartment:
The tail compartment includes all fuselage structure aft of the aft pressure
bulkhead. Within this area are the APU, battery compartment and the
　
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