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Piper Dakota - Air Intakes; Cleaning, Inspection and Repair of Cowling; Installation of Cowling; Replacement of Engine Shock Mounts

Piper Dakota
616 pages
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CLEANING, INSPECTION, AND REPAIR OF COWLING
1. Clean cowling with a suitable cleaning solvent and wipe dry with a clean cloth.
2. Inspect cowling for dents, cracks, loose rivets, elongated holes, and damaged or missing fasteners.
3. Repair all defects to prevent further damage.
INSTALLATION OF COWLING (figure 71-3)
1. Place bottom cowl into position and install attaching screws.
2. Install induction air hose at filter housing from bottom of cowling and strut fairing.
3. Connect electrical lead to landing light.
4. Install aft end of top cowl and push front down and in.
5. Hook fasteners, two on each side and two at front of nose area.
6. Install aft portion of strut fairing.
MOUNTS
ENGINE SHOCK MOUNTS (figure 71-2)
REPLACEMENT OF ENGINE SHOCK MOUNTS
l. Remove engine cowling.
2. Relieve engine weight on mounts using a one-half ton hoist attached to engine lifting points.
3. Remove four engine mounting bolts.
4. Carefully raise engine sufficiently to remove shock mounts. Check all lines, wires, and cables for
interference. Disconnect lines and cables where necessary.
5. Check all components for wear, damage, or cracks and install new mounting kit.
6. Lower engine slowly using mounting bolts to keep components aligned.
7. When engine is supported by mount, check mounts for proper seating.
8. Install mounting bolt, nut, and washer. Tighten to a torque of 450 to 500 inch-pounds and safety.
9. Reconnect any lines, wires, or cables that were disconnected and install engine cowling.
AIR INTAKES
CARBURETOR ICE DETECTOR
The carburetor ice detector uses an optical probe in carburetor throat below throttle valve. As ice forms
and blocks the passage of light to probe, the warning is triggered. With carburetor heat applied and ice melted
from the probe sufficiently to allow probe to sense light, the warning light will extinguish. A built-in test
switch activates light momentarily each time system is turned on, indicating system is operational.
71 - 61 - 00
Page - 71-13
Reissued: August 1, 1986
2I4
PIPER AIRCRAFT
PA-28-236
MAINTENANCE MANUAL

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