Cessna 206 - Page 35

CESSNA AIRCRAFT
COMPANY
SINGLE ENGINE
STRUCTURAL REPA
IR MANUAL
Table 1. Approved Replacement Fasteners Chart (continued)
REPLACE Inch thickness (or thicker)
WITH
MS20426AD5 (Countersunk)
0.063
NAS1739D5, NAS1739B5,
NAS1739E5
0.050
CR3242-5
MS20426AD5 (Dimpled)
0.071
NAS1739B5, NAS1739E5
NOTE 1: Rework Requi
red. Countersink oversize to accommodate oversize rivet.
NOTE 2: GENERAL NOTE: Do not use blind rivets in any portion of the engine air induction system structure.
Table 2. Approved Fastener Substitutions
Fastener Collar DIAMETER Fastener Collar
REPLACE
WITH
NAS178 NAS179 (Refer to Notes 1,
2, 6, 7)
HL18 HL70, HL82
(Refer to N
otes 1,
4)
NAS1054 NAS179, NA
S528
(Refer to Notes 1,
4)
NAS14XX NAS1080C, NAS1080E,
NAS1080G, NAS1080AG
(Refer to Notes 1,
3, 4)
NAS529 NAS528, NAS179
(Refer to Notes 1,
2, 5)
NAS1146 NAS1080C, NAS1080E,
NAS1080G, NAS1080AG
(Refer to Notes 1,
5)
NAS7034 NAS1080K
(Refer to Notes 1,
6)
NAS464 MIL-S-7742
(Refer t
o Notes 1,
6)
NAS1103
-
NAS1116
MIL-S-7
742
(Refer to Notes 1,
6)
NAS1303-
NAS1316
MIL-S-7742
(Refer to Notes 1,
6)
NAS6203-
NAS6216
MIL-S-7742
(Refer to Notes 1,
6)
NAS6603-
NAS6616
MIL-S-7742
(Refer to Notes 1,
6)
AN173
AN305, MS20305,
MS210
44, MS21045
NAS1054 NAS179,
NAS528
(Refer to Notes 1,
4)
NAS14XX NAS1080C, NAS1080E,
NAS1080G, NAS1080AG
(Refe
r to Notes 1,
3, 4)
NAS52
9
NAS52
8, NAS179
(Refer to Notes 1,
2, 5)
NAS1446 NAS1080C, NAS1080E,
NAS1080G, NAS1080AG
51-40-00 Page 4
© Cessna Aircraft Company Jun 1/2005