LANDING GEAR
Nose Wheel Cold Tire Pressure
51 ± 3 PSI on 6.50 x 8, 8 – Ply Rated Tire
35 ± 3 PSI on 22 x 8.0-8, 6 – Ply Rated Tire
Main Wheel Cold Tire Pressure
40 ± 3 PSI on 8.5x10, 8 – Ply Rated Tire
27 ± 3 PSI on 29x11.00-10, 10 – Ply Rated Tire
Nose Gear Shock Strut
Keep lled with MIL-H-5606 hydraulic uid per lling instructions placard.
Maintain 45 PSI air pressure in shock strut. (Use only clean, dry compressed
air or nitrogen when servicing.)
Brakes
Service the brake uid reservoir with MIL-H-5606 hydraulic uid within the
placarded limits posted on the reservoir. Maintain the uid level between the
MIN and MAX markings.
OXYGEN
Aviator’s Breathing Oxygen: MIL-O-27210
Maximum Cylinder Pressure (temperature stabilized after lling):
1850 PSI at
70°F (21.1°C)
Relling Procedure
1. Ensure the Oxygen Cockpit Controller and Display (OCCD) is OFF.
2. Turn the Master Switch OFF.
3. Remove the aft bulkhead panel in the tailcone.
4. Access the ller port and pressure gauge and remove the cap using a
back-up wrench to ensure that the tank tting doesn’t rotate.
5. Briey open the oxygen supply valve on the oxygen ll cart to purge the
ller line. Flow for approximately 10 seconds at a low ow.
6. Connect the oxygen supply line to the ll port and tighten the nut using a
back-up wrench to ensure that the tank tting doesn’t rotate.
CAUTION: Ensure the oxygen supply line and the ller port are clear of
dirt, grease, and oils that may create a re hazard during relling. Check
threads and ensure the ller port tting threads are not damaged.
NOTE: The standard and optional sizes of tires may not be intermixed.
For example, when the optional large main tires are installed on the
airplane the optional large nose tire must also be installed.
CAUTION: The bottle is equipped with a burst disk that may rupture
and prevent the oxygen bottle from holding pressure. If the bottle does not
maintain pressure when lled, perform maintenance in accordance with the
KODIAK 100 Airplane Maintenance Manual.
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