EasyManua.ls Logo

Piper PA-24-250 Comanche - Battery Overcharge; Electrical Failures (Generator); Excessive Discharge

Piper PA-24-250 Comanche
120 pages
Print Icon
To Next Page IconTo Next Page
To Next Page IconTo Next Page
To Previous Page IconTo Previous Page
To Previous Page IconTo Previous Page
Loading...
Aircrart
Public31ions
Pipcr
Comanchc
250
(Early
Model)
Section
-
3
Ernergcncy
Procedures
ELECTRICAL FAILURES
(For an Aircraft Equipped With a Generator)
1.)
Excessive Discharge:
**
NOTE
**
The generator produces no charging output when the engine is operated below approximately
1200
rpm. An excessive rate of discharge at normal operating rpm indicates a defective
generator or voltage regulator.
Ammeter
...........................
..
..............................................
Indicates Battery Discharge
.......................
............................
Generator Circuit Breaker
..
Check and Reset as Required
**
NOTE
**
Before attempting to reset any circuit breaker, allow for a two to five minute cooling off
period, and reset only once.
If circuit breaker is reset (closed):
.
.
Electrical Load
................................................................................
Reduce to a Wmmum
If generator output cannot be maintained with electrical load reduced to a minimum: Manually
pull the generator circuit breaker, maintain minimum electrical load, and land as soon as
practical.
**
NOTE
**
The battery is the only remaining source of power.
If the battery is depleted: Land without flaps. (VMP
=
95 mph or
83
kt)
Initiate Manual
Gear Extension procedure @Part
3.
(Page
3-8)
2.)
Battery Overcharge:
**
NOTE
**
A
high rate of charge is normal for the first few minutes of flight. An excessive rate of charge
after several minutes at normal operating rpm indicates a defective battery or voltage regulator.
Ammeter
..................................................................................
Indicates Excessive Charge
.
.
Generator C~rcu~t Breaker
.....................................
...
........................................................
Pull
Electrical Load
........................
..
....................................................
Reduce to a Minimum
Anticipate complete electrical failure. Land as soon as practical.
**
NOTE
**
The battery (whlch may be defective) is the only remaining source of power
If the battery is depleted Land without flaps (VMP
=
95 mph or
83
kt)
Initiate Manual
i
Gear Extension procedure
@
Part
3
(Page
3-8)
Copyright:
1993
Page
3-4

Table of Contents

Related product manuals