ARROWD
change power settings unnecessarily, as this may hasten complete power loss.
Depending on the circumstances, it may be advisable to make an off airport landing while
power is still available, particularly if other indications of actual oil pressure loss, such as sudden
increase in temperatures, or oil smoke, are apparent, and an airport is not close.
If engine stoppage occurs, proceed to POWER OFF LANDING.
LOSS OF FUEL
PRESSURE
I.
Electric Boost Pump - On.
2.
Mixture Control Forward.
3.
Fuel Selector - Check on full tank.
If problem is not an empty fuel tank, land as soon as practicable and have the fuel system
checked.
IDGH OIL TEMPERATURE
An abnonnally high oil temperature indication may be caused by a low oil level, an
obstruction in the oil cooler, damaged or improper baffle seals, a defective gauge, or other
causes. Land as soon as practicable at an appropriate airport, and have the cause investigated.
A steady, rapid rise in oil temperature is a sign of trouble. Land at the nearest airport and
let a mechanic investigate the problem. Watch the oil pressure gauge for an accompanying loss
of pressure.
ALTERNATOR FAILURE
Loss of alternator output is detected through a zero reading on the ammeter. Before
executing the following procedure, insure that the reading is zero and not merely low by
actuating an electrically powered device, such as the landing light. If no increase in the ammeter
reading is noted, alternator failure can be assumed.
1.
Reduce electrical load.
2.
Alternator Circuit Breakers - Check.
3.
":Alt" Switch - Off (for 1 second), then On.
If the ammeter continues to indicate no output, or alternator will not stay reset, tum off
"Alt" switch, maintain minimum electrical load, and land as soon as practical. All electrical
power is being supplied by the battery.
4-8
NOTE
If the battery is fully discharged, the gear will have to be lowered
using the "EMERGENCY LANDING GEAR EXTENSION"
procedure, and the position lights will of course not be operating.
EMERGENCY PROCEDURES
REVISED: December S, 1975
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...