SECTION 9
SUPPLEMENT 20 PA-28-181, ARCHER III
REPORT: VB-1611 ISSUED: JULY 12, 1995
9-120, 12 of 30 REVISED: FEBRUARY 14, 2006
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
with standby attitude gyro
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:
NOTE
The following engine messages will be displayed on the
MFD if an exceedance is detected:
• Check Oil Temp
• Check Oil Press
• Check CHT
• 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
descent at 122 KIAS
SECTION 9
SUPPLEMENT 20 PA-28-181, ARCHER III
REPORT: VB-1611 ISSUED: JULY 12, 1995
9-120, 12 of 30 REVISED: FEBRUARY 14, 2006
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
with standby attitude gyro
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:
NOTE
The following engine messages will be displayed on the
MFD if an exceedance is detected:
• Check Oil Temp
• Check Oil Press
• Check CHT
• 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
descent at 122 KIAS
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