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TABLE 2,1 - Instrumentation, B-36D Aircraft, IVY
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Reference
Number
Measurement
1
Acceleration
4
Acceleration
2
3
5
6
e
L.
eee gs
ete
a ee tee
ae
Fn215
Component
Lower Right Main Longeron, Fus. Sta. 907, (Bomb Bay)
Lower Left Main Longeron, Fus. Sta. 907, (Bomb Bay
Acceleration
7-239
Wing Tip, Left Wing, Sta. 1340
T0239
Pressure
7-223
Bending Moment
Bending Moment
7-215
7-215
1
1z
13
4
Hending
Bending
Bending
Bending
Moment
Moment
Moment
Moment}
vending Moment
7-215
7-239
7-215
T=215
7-215
7-215
7-215
%.
Nose Wheelwell, Fus. Sta. “12
7-225
7-225
Shear
Torsion
15
Location
Acceleration
Acceleration
7
8
9
10
Galvanometer
{Type (CEC No.)
A:
Rear Spar, Horizontal Stabilizer, Fus. Sta. 1770
Boom on Left Wing, Sta. 1301
Front & Rear Spar Web, Left Wing, Sta. 1062
Upper & Lower Skin, Left Wing, Sta. 1062
Caps, Front & Rear Spar, Left Wing, Sta. 1062
Caps, Front & Rear Spar, Left Wing, Sta. 604
Caps,
Caps,
Caps,
Upper
Front &
Front &
Front &
& Lower
Rear
Rear
Rear
Main
Spar, Left Wing, Sta. 390
Spar, Left Wing, Sta, 110
Spar, Right Wing, Sta. 390
Longerons of Bomb Bay, Fus. Sta. 1040
Caps, Front & Rear Spar, Left Stabilizer Sta. 62