Piper ARCHER III Pilot Operating Handbook page 366

SECTION 9
SUPPLEMENT 23
SECTION 3 - EMERGENCY PROCEDURES (continued)
Cross Check Monitor
Indication: Yellow Crosscheck Attitude Annunciator on PFD.
Establish aircraft in straight and level unaccelerated flight.
Aircraft Attitude ........................................................Crosscheck aircraft attitude
Total Loss of Engine Instruments
Indication: Indicator needle removed from dial and digital readout
replaced with white dashes.
DAU Circuit Breaker ..............................................................PULL and RESET
If engine data is still invalid:
The following engine messages will be displayed on the
MFD if an exceedance is detected:
• Check Oil Temp
• Check Oil Press
• Check RPM
• Check EGT
If failure occurs during takeoff:
Mixture ......................................................................................Maintain full rich
Throttle ................................................................................................Full power
Return to airport for landing.
If failure occurs during climb or landing:
Mixture ......................................................................................Maintain full rich
Throttle................................................................................................As required
Land as soon as practical.
If failure occurs after setting cruise power and mixture:
Power ................................................................................Maintain power setting
Land as soon as practical.
If failure occurs prior to or during descent:
Mixture ....................................................................................................Full rich
Throttle ......................................................................Set for 500 feet per minute
REPORT: VB-1611
9-164, 12 of 36
NOTE
REVISED: April 11, 2008
PA-28-181, ARCHER III
with standby attitude gyro
descent at 122 KIAS
ISSUED: JULY 12, 1995