SECTION 3
PIPER AIRCRAFT CORPORATION
EMERGENCY PROCEDURES
PA-28R-201, ARROW
3.Sf LOSS OF OIL PRESSURE (3.19)
Land as soon as possible and investigate cause.
Prepare for power off landing.
3.5g LOSS OF FUEL FLOW/PRESSURE (3.21)
Electric Fuel Pump ...................................... ON
Fuel Selector ................................ CHECK on tank
3.Sh HIGH OIL TEMPERATURE (3.23)
Land at nearest airport and investigate the problem.
Prepare for power off landing.
3.51 ELECTRICAL FAILURE (3.25)
ALT annunciator light illuminated:
containing fuel
Ammeter ................................ CHECK to VERI FY
inop. alt.
If ammeter shows zero:
AL TR Switch ......................................... OFF
Reduce electrical loads to minimum:
AL TNTR. FIELD
Circuit Breaker .......................... CHECK and RESET
as required
ALTR Switch .......................................... ON
If power not restored:
ALTR Switch ......................................... OFF
If alternator output cannot be restored, reduce electrical loads and
land as soon as practical. The battery is the only remaining source of
electrical power.
(
(
3.Sj ELECTRICAL OVERLOAD (Alternator over 20
&mps
above known
electrical load) (3.27)
(
BATT MASTR Switch ................................. OFF
REPORT: V8-1365
3-6
ISSUED: SEPTEMBER 15,1988