ARROW II
THE AIRPLANE
DESCRIPTION
AIRPLANE AND SYSTEMS
The Cherokee Arrow II is a single-engine, retractable landing gear, aU metal aircraft.
Increased fuselage length has enhanced the comfort in the rear seats. A large cabin door allows
composed entry and exit of the spacious interior. Four individual seats aUow individual comfort
for extended cross-country flights. Sound proofing has been built into the aircraft to reduce
fatigue and pem1it restful conversation. Simplicity of operation was designed into the aircraft to
allow the aircraft to operate in VFR or IFR conditions with unhurried en route planning.
AIRFRAME
Aluminum alloy construction has been used throughout for the primary structure except
for the steel tube engine mount, steel landing gear struts and isolated areas. Fiberglass and
thermoplastic are used extensively for wing tip, engine cowling and non-structure components.
The airframe has been designed to a positive limit load factor of 3.8/'
The fuselage is a conventional semi-monocoque structure. External stringers on the bottom
of the fuselage extend the length of the cabin area, and are used to maximize cabin room. On
the right side of the aircraft are a large cabin door and a large baggage compartment door.
Maintenance has been reduced to a minimum with advanced fuselage design
The
wing
is of conventional design incorporating a laminar flow NACA
65
2
-415
airfoil
section. This allows for locating the main spar 40% aft of the leading edge, an arrangement
which benefits the structure
in
two ways.
1.
It provides unobstructed cabin space for the rear passengers.
2.
It allows for a lighter wing structure to improve the useful load of the aircraft.
The wing also incorporates a rear spar and front stub spar. The main spar carries the
bending loads and the rear and stub spars carry torsional loads. The main spars are bolted into a
spar carry through at both sides of the fuselage. The rear and stub spars are bolted to
attachments at each side of the fuselage.
The
ailerons
are of modern metal construction incorporating a balance weight on the
outboard end of each aileron, and are controlled
by
a right or left rotation of the control wheel.
The flaps are also of metal construction. When the flaps are in the retracted position, the
right flap acts as a step. The flap control is located between the front seats.
The
empennage
consists of a vertical stabilizer, a rudder and a horizontal stabilator. The
empennage construction is of a modem lightweight design.
AIRPLANE AND SYSTEMS
REVISED: December
5,
1975
2-1
N16422 POH
Содержание Cherokee Arrow II
Страница 34: ...ARROW II OVERRIDE LATCH 2 4 Throttle Quadrant Console AIRPLANE AND SYSTEMS REVISED August 30 1973 N16422 POH...
Страница 37: ...AIRPLANE AND SYSTEMS ISSUED Novemoer 15 1971 Main Wheel Assembly ARROWil BRAKE HOUSING 2 7 N16422 POH...
Страница 47: ...AIRPLANE AND SYSTEMS ISSUED November 1s 1971 Static System ARROW IT 2 17 _ I N16422 POH...
Страница 52: ...ARROW II 2 22 THIS PAGE INTENTIONALLY LEFT BLANK AIRPLANE AND SYSTEMS ISSUED November 15 1971 N16422 POH...
Страница 100: ...ARROW TIDS PAGE INTENTIONALLY LEFT BLANK REPORT VB 334 PAGE S 30 MODEL PA 28R 200 l UED October 14 1971 N16422 POH...
Страница 112: ...ARROW II 6 8 THIS PAGE INTENTIONALLY LEFT BLANK OPERATING INSTRUCTIONS ISSUED November 15 1971 N16422 POH...
Страница 113: ...THJS PAGE INTENTIONALLY LEFT BLANK OPERATING INSTRUCTIONS ISSUED February 4 1972 ARROW 11 6 9 N16422 POH...
Страница 114: ...ARROWD 6 10 Tms PAGE INTENTIONALLY LEFT BLANK OPERATING INSTRUCTIONS ISSUED February 4 1972 N16422 POH...
Страница 138: ...ARROW II 9 10 THIS PAGE INTENTIONALLY LEFT BLANK a I l j I HANDLING AND SERVICING ISSUED November 15 1971 u J N16422 POH...