MS14168A(AS)
RIM DATA (IN INCHES)
WIDTH BETWEEN
FLANGE WIDTH
LEDGE DIAMETER
LEDGE WIDTH
FLANGE HEIGHT
HEEL RADIUS
FLANGE RADIUS
FLANGE EDGE
The tire covered by this MS specification sheet shall be suitable for use and provide reasonable service life during all normal operations at takeoff and landing speeds indicated herein on all types of runways and on aircraft carriers.
Test inflation pressure: Test tire 1 shall be inflated to give a rated deflection at rated load. Test tires 2, 3, and 4 shall be inflated to 400 pounds per square inch (psi) adjusted for flywheel curvature.
Test tire 1 shall complete sequences 1 through 8 as defined below without failure or visible deterioration other than normal expected tread wear. The tire shall then be used for test K for information only with the results included in the qualification test report.
SEQUENCE |
NUMBER OF CYCLES |
TEST |
TEST DESCRIPTION OPERATION |
1 |
48 |
A |
TAXI - TAKEOFF |
2 |
2 |
B |
TAXI - HIGH SPEED TAKEOFF |
3 |
48 |
C |
LANDING - TAXI |
4 |
2 |
D |
HIGH SPEED LANDING - TAXI |
5 |
1 |
E |
REJECTED TAKEOFF |
6 |
24 |
F |
INBOARD CAMBER TAXI |
7 |
24 |
G |
OUTBOARD CAMBER TAXI |
8 |
4 |
H |
LONG TAXI |
Test tire 2 shall complete sequences 1 through 3 as defined herein without failure or visible deterioration other than normal expected tread wear. The tire shall then be used for test K for information only with the results included in the qualification test report.
2
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