Table 6 Time Limited Inspection Requirements (Continued from previous page)
Task number
Item Name
Task Description
Interval
Data Module Refer-
ence
27-30/333
Elevator control ca-
bles tension
Check for new facto-
ry delivered aircraft
that have not done
the 1200 FH or
12 Months Inspection
package
Within the next 300
FH
12-B-27-30-00-00A-
903A-A
27-30/334
Elevator control ca-
bles tension
Check after replace-
ment of any elevator
control system cables
(autopilot, stick push-
er and elevator)
At the next scheduled
inspection, but not
later than 300 FH
12-B-27-30-00-00A-
903A-A
27-50/495
Flap actuators (black
anodized) (P/N
978.73.20.309)
Backlash check
2,400 FH /
3,200 LDG /
24 Months
12-B-27-50-03-00A-
313A-A
28-10/306
Fuel cross vent and
outward check valve
Operational test
2,400 FH
12-B-28-10-01-00A-
903A-A
30-10/79
Airfoil de-icers
Apply a surface coat-
ing of Age Master
No. 1 in accordance
with the manufactur-
ers instructions CMM
30-10-31 (latest is-
sue)
Note
The deice boot treat-
ment with Age Mas-
ter No 1 can be
performed by the op-
erator IAW the in-
structions given in
the AFM §8 Deicing
Boot Care
6 Months
-
32-10/80
Main and nose wheel
bearings
Lubricate
Tire change or 12
Months whichever
comes first
12-B-12-20-06-00A-
902A-A
32-10/315
Main landing gear
hinge pin and bushes
Inspection/check
2,400 FH / 12 Months 12-B-32-10-00-00A-
313A-A
or
12-B-32-10-00-00A-
313B-A
34-11/82
Pitot and static sys-
tem
Leak check
24 Months
12-B-34-11-00-00A-
903A-A
34-11/343
Static ports plate
height (RVSM air-
craft)
Inspection/check
24 Months
12-B-34-11-12-00A-
313A-A
34-21/84
Standby magnetic
compass (if installed)
Check swing
24 Months
12-B-34-21-00-00A-
903A-A
PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719,
1721-1999
12-B-AM-00-00-00-I
UNCLASSIFIED
Effectivity: All
12-B-05-10-20-00A-281A-A
UNCLASSIFIED
2021-12-04 Page 6