-1 Automatic Thrust Limiter System (Viper Engines Only)

Automatic Thrust Limiter System (Viper Engines Only)

Fuel Flow Indicators

1. 
   Associated RPM and JPT/ITT indicators are operative,
   
2. 
   All fuel quantity indicators are operative, and
   
3. 
   A fuel monitoring procedure is established and used.
   

1. 
   Confirm associated RPM and ITT indicators operate normally,
   
2. 
   Confirm all fuel quantity indicators are operative, and
   
3. 
   During flight, monitor engine gauges to ensure that both engines are operating normally,
   
4. 
   Fuel consumption will be monitored to ensure that abnormal fuel imbalances do not occur.
   
5. 
   Fuel flow may be available on the Fuel Management page in the FMS.
   

Ignition Systems

1. 
   Aircraft is not operated in visible moisture or from contaminated runways, and
   
2. 
   Aircraft is not operated in known or forecast icing conditions.
   

1. 
   Prior to each flight, confirm that only one igniter is inoperative on only one engine.
   

• 
  With battery power only on, select Ignition “ON”, and
  
• 
  Then listen to each engine for two distinct “snaps”. If only one distinct “snap” is noticed only one igniter is working on that engine.
  

2. 
   Ensure that the aircraft is not operated in visible moisture or from wet or contaminated runways, and
   
3. 
   Aircraft is not operated in known or forecast icing conditions.
   
4. 
   Plan flights to avoid any of the above mentioned conditions.
   

Engine Indications

Power Loss Indicator Systems (Viper Engine Only)

Above 92% Light Systems (Viper Engine Only)

1. 
   Ensure climb power does not exceed AFM Limitations.
   
2. 
   Non-Flying Pilot will monitor and adjust climb power as needed.
   
3. 
   3. Captain will brief procedure to be used before each departure.
   

Thrust Reversing System (Series 700 and 800, If Installed, and 750, 800XP, 850XP and 900XP)

1. 
   No damage to the thrust reverser system exists which would adversely affect operation of the airplane, and
   
2. 
   A procedure is established and used to ensure that the associated thrust reverser(s) is disabled and pinned in the stowed (forward thrust) position.
   

1. 
   Confirm that the associated (M) procedure for disabling thrust reverser(s) in the stowed position is accomplished, and
   
2. 
   Confirm that no apparent damage to the thrust reverser system exists which would adversely affect operation of the airplane, and
   
3. 
   Plan flight to ensure that safe landings can be made at the airports to be used with the thrust reverser(s) inoperative (INOP).
   

Care should be exercised when advancing single reverse thrust to avoid controllability effects.

Thrust Reverser Indicating Annunciators

1. 
   Confirm that the associated (M) procedure for disabling thrust reverser(s) in the stowed position is accomplished, and
   
2. 
   Plan flight to ensure that safe landings can be made at the airports to be used with the thrust reverser(s) inoperative.
   

Close attention should be paid to the appropriate brake cooling times as set forth in the Normal Procedures section of the Flight Manual.

Starter Power Available Annunciator (TFE-731 Engines Only)

Starter Select Light (Viper Engines Only)

Starter Operating Annunciators (TFE-731 Engines Only)

1. 
   Procedures are established and used to assure that start power and EXT PWR switches are disengaged when engine reaches self-sustaining speed, and
   
2. 
   Procedures are established and used to assure that associated generator(s) is (are) on line after each start.
   

1. 
   Start power and EXT PWR switches are disengaged when engine reaches self-sustaining speed, and
   

2. 
   Generator is verified to be on line. (Reference After Start checklist.)