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i. Vertical Stabilizer Deice Boot- - - - - - - - - - - - - - - CONDITION
j. Right Horizontal Stabilizer, Elevator,
and Trim Tab - - - - - - - - - - - - - - - - - - - - - - - - - - CONDITION
(Make sure trim tab position matches indicator.)
k. Rudder and Trim Tab - - - - - - - - - - - - - - - - - - - - - - SECURE
(Make sure trim tab position matches indicator.)
l. Static Wicks (Rudder, Both Elevators, and Tailcone)- - CHECK
(10 installed. 1 may be missing from either elevator
and 1 may be missing from Rudder or Tailcone. No
more than 2 total missing on entire airplane)
m. Left Horizontal Stabilizer, Elevator, and
Trim Tab - - - - - - - - - - - - - - - - - - - - - - - - - - - - - CONDITION
(Make sure trim tab position matches indicator.)
n. Left Horizontal Stabilizer Deice Boot - - - - - - - - - CONDITION
o. Rudder Gust Lock - - - - - - - - - - - - - - - - - - - - - DISENGAGE
9. Left Engine/Nacelle - - - - - - - - - - - - - - - - - - - - - - - - - - - CHECK
a. Pylon Precooler Exhaust- - - - - - - - - - - - - - - - - - - - - CLEAR
b. Engine Exhaust and Bypass Duct - CONDITION and CLEAR
c. Oil Level - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - CHECK
d. Filler Cap and Access Door- - - - - - - - - - - - - - - - - - SECURE
e. Engine Fluid Drains - - - - - - - - - - - - - - - - - - - - - - - - CLEAR
f. Generator Cooling Air Exhaust - - - - - - - - - - - - - - - - CLEAR
g. Engine Anti-Ice Exhaust - - - - - - - - - - - - - - - - - - - - - CLEAR
h. Generator Cooling Air Inlet - - - - - - - - - - - - - - - - - - - CLEAR
i. EngineT2 Probe- - - - - - - - - - - - - - - - - - - - - - - - CONDITION
j. Engine Air Inlet - - - - - - - - - - - - - - - - - - - - - - - - - - - CLEAR
k. Engine Fan Duct and Fan - - - - - - - - - - - - - - - - - - - - CHECK
(for bent blades, nicks and blockage of fan stators)
l. Pylon Precooler Inlet - - - - - - - - - - - - - - - - - - - - - - - CLEAR
m. Oil Filter Differential Pressure Indicator - - - NOT EXTENDED
10. Aft Compartment - - - - - - - - - - - - - - - - - - - - - - - - - - - - - CHECK
a. Fire Bottle Pressure Gauge- - - - - - - - - - -CHECK per placard
b. Junction Box Circuit Breakers - - - - - - - - - - - - - - - - - - - - - IN
c. Equipment and Junction Box Access Doors - - - - - - SECURE
d. Aft Compartment Baggage - - - - - - - - - - - - - - - - - - SECURE
e. Aft Compartment Light - - - - - - - - - - - - - - - - - - - - - - - - -OFF
f. Aft Compartment Access Door - - - - -SECURE and LOCKED
(Continued Next Page)
6 AA 510CLNP-06
Configuration
MODEL 510 NORMAL PROCEDURES
EXTERIOR INSPECTION (Continued)
11. Left Wing- - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - CHECK
a. Flap, Speed Brakes, Aileron, and Trim Tab - - - - -CONDITION
(Make sure flap position and trim tab matches indicators)
b. Static Wicks - - - - - - - -CHECK (3 installed. 1 may be missing.
No more than 2 total missing on entire airplane)
c. Fuel Tank Vent - - - - - - - - - - - - - - - - - - - - - - - - - - - - CLEAR
d. Fuel Filler Cap - - - - - - - - - - - - - - - - - - - - - - - - - - - SECURE
e. Wing Deice Boot- - - - - - - - - - - - - - - - - - - - - - - -CONDITION
f. Vortex Generators (8 per wing) - - - - - - - - - - - - -CONDITION
g. Stall Strip - - - - - - - - - - - - - - - - - - - - - - - - - - - - -CONDITION
h. Main Gear Door, Wheel, Tire, and Strut - - - - - - - -CONDITION
i. Fuel Quick Drains (4) - - - - - - - - - - DRAIN and CHECK FOR
CONTAMINATION
12. Fuselage Left Side - - - - - - - - - - - - - - - - - - - - - - - - - - - - CHECK
a. Wing Inspection Light - - - - - - - - - - - - - - - - - - - -CONDITION
b. Landing Light - - - - - - - - - - - - - - - - - - - - - - - - - -CONDITION
c. Cabin Door Seal - - - - - - - - - - -CHECK for RIPS and TEARS
COCKPIT PREPARATION
1. BATTERY DISCONNECT Switch- - - - - - - NORM/COVER DOWN
2. INTERIOR DISCONNECT Switch - - - - - - - - - - - - - - - - - -NORM
3. Circuit Breakers - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - IN
4. STBY INST Switch - - - - - - - - - - - - - - - BATT TEST (5 seconds);
GREEN LIGHT ON
5. STBY INST Switch - - - - - - - - - - STBY INST; AMBER LIGHT ON
6. If Ground Power Unit is connected (for battery power only, skip to
Step 7):
a. BATT Switch - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - ON
b. AVN PWR Switch - - - - - - - - - - - - - - - - - - - - - - - - - - - - - ON
c. BATTERY VOLTAGE - - - - - - - - - - - - - - - - - - - -CHECK 28V
d. COCKPIT/CABIN FAN Knobs - - - - - - - - - - - - -AS DESIRED
e. AIR COND Switch - - - - - - - - - - - - - - - - - - - - -AS DESIRED
7. Cockpit Switches and Controls - - - - - - - - - - - - - - - - - - - - - -SET
　
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