AMMETER.
The ammeters are mounted in the instrument panel. Each instrument measures the output of the respective alternator into the entire electrical system including the battery charging demand.
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EXTERNAL POWER.
EXTERNAL POWER RECEPTACLE.
The external power receptacle is located on the right side of the nose section. When using external power
for operation of any of the airplane's equipment, the master switch must be ON. To start the engine with
external power proceed as follows: — CAUTION —
EXTERNAL POWER IS SUPPLIED DIRECTLY TO THE ELECTRICAL BUS. TURN OFF ALL ELECTRICAL EQUIPMENT BEFORE APPLYING OR REMOVING EXTERNAL POWER.
1.
Turn aircraft MASTER SWITCH and all electrical equipment OFF.
2.
Connect the RED lead of PEP (Piper External Power) kit jumper cable to the POSITIVE (+) terminal of external 12 volt battery and the BLACK lead goes to the NEGATIVE (-) terminal.
3.
Insert the plug of the jumper cable into the socket located on the aircraft fuselage.
4.
Leave MASTER SWITCH OFF and proceed with engine starting technique as follows:
A. Start engines with the standard technique but after starting both engines reduce power on the left engine to the lowest possible RPM to reduce sparking. and shut down the right engine.
5.
Turn all electrical equipment OFF and remove the jumper cable plug from the aircraft.
6.
Turn the aircraft MASTER SWITCH to the ON position and check the alternator ammeter for an indication of output. Do not attempt any flight if there is no indication of alternator output.
— Note —
For all normal operations using the external power jumper cables, the master switch should be OFF, but it is possible to use the ship 's battery in parallel by turning the master switch ON. This will give longer cranking capabilities, but will not increase the amperage.
— CAUTION —
EXERCISE CARE IF THE AIRPLANE’S BATTERY HAS BEEN, OR IS SUSPECTED OF BEING, DEPLETED. THE EXTERNAL POWER SUPPLY CAN BE REDUCED TO THE LEVEL OF THE AIRPLANE’S BATTERY. TEST THIS BY TURNING THE MASTER SWITCH ON MOMENTARILY WHILE THE STARTER IS ENGAGED. IF CRANKING SPEED INCREASES, THE AIRPLANE’S BATTERY IS AT A HIGHER LEVEL THAN THE EXTERNAL POWER SUPPLY. IF THE BATTERY HAS BEEN DEPLETED BY EXCESSIVE CRANKING IT MUST BE RECHARGED BEFORE THE SECOND ENGINE IS STARTED. ALL THE ALTERNATOR CURRENT WILL GO TO THE LOW BATTERY UNTIL IT RECEIVES SUFFICIENT CHARGE, AND IT MAY NOT START THE OTHER ENGINE IMMEDIATELY.
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CHAPTER
25
EQUIPMENT / FURNISHINGS
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CHAPTER 25 - EQUIPMENT / FURNISHINGS
TABLE OF CONTENTS / EFFECTIVITY
CHAPTER/ SECTION SUBJECT GRID NO. EFFECTIVITY
25-10-00 FLIGHT COMPARTMENT 1K13 1R0202
Description Seat Back Lock and Release - Rigging Instr. 1K13 1K13 1R0202
Lumbar Seats Description Removal of Lumbar Bladder Installation of Lumbar Bladder 1K13 1K13 1K14 1K14 1R0202
25-60-00 EMERGENCY 1K17 1R0202
Emergency Locator Transmitter (ELT) Description Pilot’s Remote Switch 1K17 1K17 1K17 1R0202 1R0202 1R0202
Artex ELT 110 Battery Removal and Installation Testing the Artex ELT 110 1K17 1K18 1K19 1R0202 1R0202 1R0202
25-Cont./Effec. Page 25-3 Revised: February 28, 2002
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25-Cont./Effec. Page 25-4 Revised: February 28, 2002
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FLIGHT COMPARTMENT
DESCRIPTION
The Seminole has the capacity of seating up to 4 (passengers and crew) in a forward facing seat arrangement. Information on seat installations and other options are included in this chapter.
Two fully adjustable forward facing seats are installed for the pilot and co-pilot. They adjust vertically, recline, and adjust fore and aft with a storage pocket on the back of each seat. Two forward facing reclining seats are installed for the passengers. A worktable attaches to either the pilot or co-pilots seat back. It is stored along the left side in the baggage area and secured with a strap.
SEAT BACK LOCK AND RELEASE - RIGGING INSTRUCTIONS (Refer to Figure 25-1.)
1.
Loosen screws and ascertain that clamps are in a relaxed condition. (Push-pull cable is able to move within the clamps.)
2.
Place a straightedge along the lower surface of bushing of the seat back release.
3. 中国航空网 www.aero.cn 航空翻译 www.aviation.cn 本文链接地址：西门诺尔飞机维护手册 simenole PA-44-180 AMM 1(61)
