TOE-IN
TOE-OUT
ANGLE
0°
0° 33'
0° 48'
1° 04'
1° 19'
1° 35'
2° 05'
Max. Allow.
AN960-416L Washers .031 Thick
AN960-416 Washers .062 Thick
CLEANING, INSPECTION AND REPAIR OF MAIN GEAR DOOR ASSEMBLY.
1. Clean the door and retraction rod with a suitable cleaning solvent.
2. Inspect the door for cracks or damage, loose or damaged hinges and brackets.
3. Inspect the door retraction rod and end bearing for damage and corrosion.
4. Repairs to a door may be replacement of hinge, repair of fiberglass and painting.
INSTALLATION OF MAIN GEAR DOOR ASSEMBLY.
1. Install the door by positioning the hinge halves of the door and wing, and inserting the hinge pin. It is
recommended a new pin be used. Bend the end of the pin to secure in place.
2. Install the door retraction rod by positioning the rod at its attachment points at the door and strut
housing. At the door attachment, thin washers are inserted at each side of the rod end bearing and it is secured
with bolt, washer and nut. At the strut housing, place washers between rod end bearing and housing not to
exceed .12 of an inch to obtain proper clearance and secure with bolt. Safety bolt with MS20995C41 wire.
3. Check that the all around clearance between the door and the wing skin is not less than .032 of an inch.
PIPER AIRCRAFT
PA-28RT-201 / 201T
MAINTENANCE MANUAL
CHART 3203. TOE-IN—TOE-OUT CORRECTION CHART
SHIM
WASHERS
WASHERS
UNDER HEAD
AN960-416
AN960-416
AN960-416
AN960-416L
AN960-416
AN960-416
AN960-416 (2)
AN960-416
AN960-416L
AN960-416L
AN960-416 (2)
AN960-416 (3)
AN960-416
AN960-416 (4)
AN960-416
WASHERS
UNDER NUT
AN960-416 (3)
AN960-416 (2)
AN960-416
AN960-416
AN960-416
AN960-416 (2)
AN960-416
2E4
AN 174
BOLT
-14
-14
-14
-14
-14
-15
-15
32-10-11
Page 32-21
December 1, 1978
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