Damage Limits Aft Fuselage - Condition I; Damage Limits Tail Boom And Landing Gear - Condition I - Bell OH-58A Technical Manual

LOCATION
COMPONENT /
MEMBER
FS
Bulkhead
205.74
205.74
Engine Mount
Support 130.00
130.00
142.33 72.00
COMPONENT /
MEMBER
BS
Tail Boom 31.94-
42.59
31.92
31.87-
164.10
31.87, 42.59,
79.82, 98.29,
116.84, 150.22
174.10-
182.40
174.10-
182.40
174.10-
182.40
Table 4-3 . Dam age Limits Aft Fuselage — Condition I (Cont)
ELEMENT
WL BL
Frame Section
Angles, Clips
Back-Up Structure
8.465L&R
3.50L&R Fitting
12.96L&R Fitting
Table 4-4. Damage Limits Tail Boom and Landing Gear — Condition I
LOCATION
ELEMENT
WL BL
Intercoastals
Attachment Fittings
Skin
Bulkheads
Bulkheads
Fin Supports
Gearbox Mounting Plate
DAMAGE LIMITS
CAP / FLANGE SKIN / WEB
CD' CL' N WL'
(D'=N x CL) (D'=N x WL)
0.40 0.80 10
0.50 1.00 10
No Damage Allowed
No Damage Allowed
No Damage Allowed
DAMAGE LIMITS
CAP / FLANGE SKIN / WEB
CD' CL' N WL'
(D'=N x CL) (D'=N x WL)
No Damage Allowed
No Damage Allowed
Circumference
3.0
No Damage Allowed
0.85 1.70 10
0.17 0.34 10
No Damage Allowed
NOTES /
CAUTIONS
N
NOTES /
CAUTIONS
N
At any No Damage
Allowed BS164.10-
182.40
5