Power Off Landing (3.15) - Arrow PA-28R-201 Pilot's Operating Handbook And Faa Approved Airplane Flight Manual

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I
SECTION 3
EMERGENCY PROCEDURES
PIPER AlRCRAFf CORPORATION
IJA-28R-201, ARROW
3.sc
ENGINE POWER LOSS
IN
FLIGHT (3.13) (continued)
Electric fuel pump ............................................................................. ON
Mixture ......................................................................................... RICH
(
Alternate Air ................................................................................. OPEN
Engine Gauges .................................................... CHECK for indication
of cause of power loss
If no fuel flow/pressure is indicated. check tank selector position
to
be
sure it is on a tank containing fuel.
When power is restored:
Alternate Air .............................................................................. CLOSE
Electric Fuel Pump .......................................................................... OFF
If power is not restored, prepare for power off landing.
Trim for 79 KIAS.
3.Sd
POWER OFF LANDING (3.15)
Trim for 79 KIAS.
Locate suitable field.
Establish spiral pattern.
1000 ft. above field at downwind position for normal landing
('
approach.
When field can be easily reached. slow
to
72 KIAS for shortest landing.
Gear Down Emergency Landing (3.1sa)
Touchdowns should be normally be made at the lowest possible
airspeed wilh full flaps.
When committed to landing:
Landing Gear Selector ................................................................ DOWN
Flaps ................................................................................ AS DESIRED
Throttle ...................................................................................... CLOSE
Mixture ........................................................................ IDLE CUT-OFF
Ignition ............................................................................................ OFF
BATT MASTR Switch .................................................................... OFF
ALTR Switch ................................................................................... OFF
Fuel Selector .................................................................................... OFF
Seat Belts and Harness ................................................................ TIGHT
NOTE
(
If battery master switch is OFF. the landing gear
cannot be retracted.
REPORT: VB-136S
3·4
ISSUED: SEPTEMBER
15,1988
REVISED: MARCH 10, 1989

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