AFI 11-2C-130v3 - BITS

50 AFI11-2C-130V3 23 APRIL 2012
Indicator
Hydraulic Suction Boost
Pumps
Auxiliary Hydraulic
Pump
Auxiliary Hydraulic
Pressure Indicator
Rudder Boost Pressure
Indicators
Table 4.8. Landing Gear.
2 2 2
1 1 1
1 1 1 Direct reading gauge in cargo compartment
may be inoperative
2 2 1
Item/System Installed Required
A B Remarks/Limitations/Exceptions
Landing Gear System 1 1 1* *Shall be repaired at next repair capable
facility.
Landing Gear Position
Indicators
Landing Gear Warning
Light
Table 4.9. Brake/Anti Skid Systems.
In the event of an actual or suspected
landing gear malfunction, the gear will not be
moved from the down and locked position. If
landing gear has been tied down IAW
Flight Manual emergency procedures, no
further flights are authorized until repair is
made or inspected by authorized
maintenance personnel.
Flight (including enroute stops) with
landing gear doors removed may be
accomplished to a destination with repair
capability.
3 3 0* *Shall be repaired at next repair capable
facility. Gear will not be moved from the
down and locked position.
1 1 0* *Shall be repaired at next repair capable
facility. Gear will not be moved from the
down and locked position.
Item/System Installed Required
A B Remarks/Limitations/Exceptions
Wheel Brakes 4 4 4
Parking Brake 1 1 1
Anti-Skid 1 1 0* *Shall be repaired at next repair capable
facility.
Maximum effort landings with antiskid inoperative
are not authorized. A local training flight may
continue if the antiskid fails provided the system is
turned off. Multiple landings or formation landings
will not be accomplished.