ARROW II
!I ,. •
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Two micro-switches in the throttle quadrant activate a warning horn and a red "Warning
Gear Up" light under the following conditions:
1.
Gear up and power reduced below approximately 14 inches of manifold pressure.
2.
On aircraft equipped with the backup gear extender. if the system has extended the
landing gear and the gear selector is UP. except at full throttle.
3.
Gear selector switch "UP" while on the ground .
.
On aircraft NOT equipped with the backup gear extender an additional switch is installed
which activates the warning horn and light whenever the flaps are extended beyond the approach
position (I 00) and the gear are not down and locked.
The nose gear is steerable through a 60-degree arc through use of the rudder pedals. As the
nose gear retracts. the steering linkage disengages to reduce rudder pedal loads in night. T�e nose
wheel is equipped with a hydraulic shimmy dampener to reduce nose wheel shimmy.
The oleo strots are of the air-oil type, with normal extension being 2.7.5 inches for the nose
gear and 2.0 inches for the main gear under normal static load (empty weignt of airplane plus full
fuel and oil).
The standard brake system includes toe brakes on t
.
�e left set of rudder pedals and a hand
brake located below and near the center of the instrument paneL
:
1.pe brakes on the right rudoer
pedal are optional. The toe brakes and the harid brake have jndividaul orake cylinders. but all
cylinders use a common reservoir. The parking brake is incorpora�ed in jhe lever brake and is
operated by pulling back on the lever and depressing the kriob attacned to the top of the handle.To
release the parking brake, pull back on the brake lever; then allow the handle to swing forward.
A single disc. single puck brake is mounted on the main g�ars. A brake di
'
sc is mounted on the
inboard side of the wheels and the brake housing which incorporates the pucks is mounted to the
inboard side of the wheel axle.
1-6
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...