Beechcraft C-12C Operator And Technical Reference Manual page 879

Army c-12c aircraft nsn 1510-01-070-3661, army c-12d aircraft nsn 1510-01-087-9129, army c-12t aircraft nsn 1510-01-470-0220
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During approach, propellers should be set
at
1900
RPM
interference (ILS approach), provide better
power response during approach, and
minimize attitude change when advancing
propeller levers for landing.
5. FLAPS (below 199 KIAS) – APPROACH.
6. GEAR (below 181 KIAS) – DN, confirm.
7. LANDING LIGHTS – As required.
8. CONDITION levers – HIGH IDLE.
9. TCAS – Set as required.
8A-41. LANDING.
Performance
data
computations assume the runway is paved, level, and
dry. Additional runway must be allowed when these
conditions are not met. Do not consider headwind
during landing computations; however, if landing must
be downwind, include the tailwind in landing distance
computation. Conduct all landings in accordance with
the appropriate ATM. Perform the following procedure
as the aircraft nears the runway.
1. AP & YD – Disengaged.
2. GEAR DOWN lights – Check/confirm.
3. PROP levers – HIGH RPM.
8A-42. TOUCH AND GO LANDING.
The instructor should select a point on the
runway where all pre-takeoff procedures will have
been completed prior to the pilot's initial application of
power.
In selecting this point, prime consideration
shall be given to the required accelerate-stop distance
pre-computed on a current Takeoff and Landing Data
(TOLD) card.
The nose wheel should be on the
runway and rolling straight before the power is
advanced. After the pilot applies power to within 5% of
the takeoff power, the instructor's actions are the same
as during a normal takeoff.
procedure.
1. PROP levers – HIGH RPM.
2. FLAPS – As required.
3. Trim – Set.
4. Power stabilized – Check 27% minimum.
5. Takeoff power – Set.
NOTE
to
prevent
glideslope
charts
for
landing
Use the following
8A-43. GO-AROUND/MISSED APPROACH.
Accomplish the maneuver in accordance with
the appropriate ATM.
1. Power – As required.
2. FLAPS – Retract to APPROACH.
3. GEAR (Positive climb) – UP.
4. FLAPS (105 KIAS) – UP.
5. LANDING/TAXI LIGHTS – OFF.
6. Climb power – Set.
7. YAW DAMP – As required.
8. BRAKE DEICE switch – Off.
8A-44. AFTER LANDING.
Complete the following procedures after the
landing rollout is complete and normal taxi speed is
attained.
1. CONDITION levers – As required.
2. AUTO IGN – Off.
3. ICE & RAIN switches – Off.
4. FLAPS – UP.
5. XPNDR – As required.
6. Radar – As required.
7. Lights – As required.
a. Strobe lights – Off.
b. RECOG – OFF.
c. LANDING/TAXI LIGHTS – As required.
8A-45. ENGINE SHUTDOWN.
To prevent sustained loads on rudder
shock links, the aircraft should be parked
with the nose gear centered.
1. BRAKE DEICE switch – Off.
2. Parking brake – Set.
3. LANDING/TAXI lights – OFF.
4. EFIS POWER – OFF.
5. INVERTERS – OFF.
6. AUTOFEATHER switch – OFF.
7. CABIN AIR/TEMP MODE switch – OFF.
TM 1-1510-218-10
NOTE
8A-19

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