-1 Windscreen (Panel “A”) (Series 1 Through 700)

Windscreen (Panel “A”) (Series 1 Through 700)

1. 
   Visibility through the affected windscreen(s) is acceptable to the crew,
   
2. 
   Airplane is not operated in known or forecast icing conditions,
   
3. 
   Associated SCREEN HEAT Control (CTL) circuit breaker is pulled and collared, and
   
4. 
   AFM limitations are observed.
   

1. 
   Locate affected SCREEN HEAT CTL circuit breaker.
   
2. 
   Pull and collar circuit breaker.
   
3. 
   Place INOP placard adjacent to affected switch.
   

1. 
   Confirm that delamination does not affect visibility.
   
2. 
   Plan flight to avoid flight in known or forecast icing conditions.
   
3. 
   Review AFM low altitude airspeed limitations for windscreen heat inoperative.
   

Windscreens “A” or “B” (Series 750, 800, 800XP, 850XP and 900XP)

1. 
   Visibility through the affected windscreen is acceptable to the crew, and vision is not impaired on the remaining windscreens,
   
2. 
   Airplane is not operated in known or forecast icing conditions,
   
3. 
   Associated SCREEN HEAT CTL circuit breaker is pulled and collared, and
   
4. 
   AFM limitations are observed.
   

1. 
   Locate affected SCREEN HEAT CTL circuit breaker.
   
2. 
   Pull and collar circuit breaker.
   
3. 
   Place INOP placard adjacent to affected switch.
   

1. 
   Confirm that delamination does not affect visibility.
   
2. 
   Plan flight to avoid flight in known or forecast icing conditions.
   
3. 
   Review AFM low altitude airspeed limitations for windscreen heat inoperative.
   

22-1

Engine Synchronizer System (Series 1 Through 800A With TFE-731 Engines Only)

1. 
   System is selected “OFF”,
   
2. 
   Automatic Performance Reserve (APR) system is not armed, and
   
3. 
   AFM limitations are observed.
   

1. 
   Prior to flight, review Aircraft AFM procedures with APR inoperative.
   
2. 
   Observe limitations with APR inoperative.
   
3. 
   Select engine synchronization (synch) OFF and do not use.
   
4. 
   Install ‘INOP’ placard adjacent to engine synch switch.
   

Top Temperature Control System (Viper Engine Only)

1. 
   Associated switch remains OFF,
   
2. 
   Associated circuit breakers are pulled and collared, and
   
3. 
   Associated JPT indicator is operative.
   

1. 
   Select associated system OFF.
   
2. 
   Confirm normal operation of associated JPT indication.
   

23-1

APR Computer System (Series 1 Through 800A With TFE-731 Engines Only)

1. 
   AFM performance limitations are observed,
   
2. 
   APR system is selected OFF, and
   
3. 
   Procedures for monitoring engine limitations are established and used.
   

1. 
   Prior to flight, review AFM procedures with APR inoperative.
   
2. 
   Observe limitations with APR inoperative.
   
3. 
   Select APR OFF and do not use.
   
4. 
   Install Inoperative (‘INOP’) placard adjacent to APR switch.