FAA Advisory Circular 43.13-1B

Acceptable Methods, Techniques, and Practices

Aircraft Inspection and Repair

AC 43.13-1B | 7. Aircraft Hardware, Control Cables, and Turnbuckles | 11. Hardware Identification Tables | 7-209. Bolts

Previous
Next
9/8/98
TABLE 7-11. (CONTINUED)
Screw MS, AN, or
Description
NAS Number
NAS6100-6103
Screw, hex head,
tri-wing recess, full thr.,
titanium
NAS6500-6506
Screw, 100° oval hd.,
tri-wing recess, full thr.,
cres.
NAS6900-6904
Screw, panhead,
tri-wing recess, full thr.,
cres.
TABLE 7-12. TABLE OF BOLTS.
Bolt Number
AN3-20
Description
Bolt, machine
AC 43.13-1B
TABLE 7-12. (CONTINUED)
Bolt Number
AN148551-149350
Description
Bolt, socket head,
6-hole drilled, .190-.625
AN101001-101900
Bolt, hex, steel, head
AN101901-102800
Bolt, hex.,
drilled shank, steel
AN102801-103700
Bolt. Drilled hex. Head,
(one hole), steel
AN103701-104600
Bolt, drilled hex. Head,
steel, (six holes)
AN21-36
Bolt, clevis
AN104601-105500
Bolt, hex. Head, corro-
sion-resistant steel
AN42-49
AN73-81
AN173-186
AN774
AN775
Bolt, eye
Bolt, machine, drilled
Bolt, aircraft
Close tolerance
Bolt, flared tube
Bolt, universal fitting
AN105501-106400
AN106401-107300
AN107301-108200
MS9033-9039
MS9060-9066
Bolt, hex. Head,
drilled shank,
corrosion-resistant
steel
Bolt, hex., drilled head,
(one holes),
corrosion-resistant
steel
Bolt, hex., drilled head,
(six holes),
corrosion-resistant
steel
Bolt, machine 12pt.
Head, 130,000 psi min.
T.S.
Bolt, machine 12pt.
Double hex. 130,000
psi min. T.S. ext.
washer head, drilled
Par 7-196
Page 7-57
Public domain content provided by US Federal Aviation Administration. Navigation features courtesy of Land Sea Sky Space LLC