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CAUTION
IT IS DANGEROUS TO APPROACH AN AIRCRAFT WITH ITS ENGINE OPERATING. ONLY GROUND PERSONNEL PROPERLY TRAINED ON PROCEDURES FOR APPROACHING OPERATING AIRCRAFT SHOULD BE ALLOWED TO DISCONNECT EPU SOURCE. PRACTICE THE REMOVAL OF THE POWER CORD BEFORE ATTEMPTING WITH ENGINE OPERATING. NEVER APPROACH THE AIRCRAFT WITHOUT A SIGNAL FROM THE PILOT. ENSURE THE AIRCRAFT IS PARKED OVER AN AREA OF PAVEMENT WHERE THERE IS A SURE FOOTING. PROTECT EYES AND EARS WHEN NEAR THE OPERATING ENGINE.
14.
Select the EPU switch to OFF. EPU light ON
15.
Signal the ground crew to PULL the EPU light OFF EPU cord.
16.
Master Switch (GEN) OFF
17.
Battery Voltage check approx. 12 volts
18.
Master Switch (GEN) ON, check approx. 14 volts
19.
GEN warning light check OFF
5. PERFORMANCE
There is no change in airplane performance associated with EPU operations.
6. WEIGHT AND BALANCE / EQIUPMENT LIST
Refer to Equipment List, Chapter 6.5,
Item Number 24-002 (Aircraft S/N C0001 through C0148 and C0150)
Item Number 24-005 (Aircraft S/N C0149 and C0151 onwards)
CHAPTER 9
SUPPLEMENT 2
WINTERIZATION KIT
1.
GENERAL ................................................................................................................... S2-2
2.
OPERATING LIMITATIONS ....................................................................................... S2-2
3.
EMERGENCY PROCEDURES................................................................................... S2-3
4.
NORMAL PROCEDURES .......................................................................................... S2-3
5.
PERFORMANCE ........................................................................................................ S2-3
6.
WEIGHT AND BALANCE ........................................................................................... S2-3
7.
DESCRIPTION OF THE AIRPLANE AND ITS SYSTEMS ......................................... S2-4
8.
HANDLING, PREVENTIVE AND CORRECTIVE MAINTENANCE............................. S2-4
1. GENERAL
The Winterization Kit consists of cowling inlet and outlet baffles. The inlet baffles are attached to the upper cowling with two winged 1/4-turn fasteners. The outlet baffles are attached to the lower cowling with screws. At take-off outside air temperatures below 14°F/-10°C it is recommended to use both inlet and outlet baffles together. At temperatures between 32°F/0°C and 54.5°F/12.5°C it is not permissible to use both inlet and outlet baffles together. Either the inlet baffles only or the outlet baffles only may be used in this temperature range. At temperatures above 54°F (12.5°C) both inlet baffles and outlet baffles must be removed. These temperature ranges have been established by test to prevent the engine from overheating during a prolonged climb.
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