TM 1-1520-265-23
INDEX-Continued
Subject
Paragraph
Page
Number
Number
F
Ferrous Bolts and Pins Contained within the Airframe and Landing
Gear System (MT) ................................................................................................................. 4.36
4-81
Description ...................................................................................................................... 4.36.1
4-81
Ferrous Bolts Contained within the Flight Control System (MT).................................................... 6.23
6-44
Description ...................................................................................................................... 6.23.1
6-44
Ferrous Connecting Links, Rod Ends, Clevises, Levers, and Attaching
Parts (MT).............................................................................................................................. 6.15
6-29
Backup Method................................................................................................................ 6.15.4
6-31
Defects............................................................................................................................ 6.15.2
6-29
Description ...................................................................................................................... 6.15.1
6-29
Primary Method ............................................................................................................... 6.15.3
6-29
System Securing ............................................................................................................. 6.15.5
6-31
Ferrous Flight Control System Push-Pull Rods (MT) .................................................................... 6.10
6-18
Backup Method................................................................................................................ 6.10.4
6-20
Defects............................................................................................................................ 6.10.2
6-18
Description ...................................................................................................................... 6.10.1
6-18
Primary Method ............................................................................................................... 6.10.3
6-18
System Securing ............................................................................................................. 6.10.5
6-20
Ferrous Rotor System Bolts and Pins (MT)..................................................................................... 2.3
2-6
Backup Method.................................................................................................................. 2.3.4
2-7
Defects.............................................................................................................................. 2.3.2
2-6
Description ........................................................................................................................ 2.3.1
2-6
Primary Method ................................................................................................................. 2.3.3
2-6
System Securing ............................................................................................................... 2.3.5
2-7
Fluid in Honeycomb Core Panels and Structures (RT).................................................................... 4.4
4-10
Backup Method.................................................................................................................. 4.4.4
4-13
Defects.............................................................................................................................. 4.4.2
4-10
Description ........................................................................................................................ 4.4.1
4-10
Primary Method ................................................................................................................. 4.4.3
4-10
System Securing ............................................................................................................... 4.4.5
4-13
Forward Bellcrank (MT)................................................................................................................ 6.19
6-37
Backup Method................................................................................................................ 6.19.4
6-39
Defects............................................................................................................................ 6.19.2
6-37
Description ...................................................................................................................... 6.19.1
6-37
Primary Method ............................................................................................................... 6.19.3
6-37
System Securing ............................................................................................................. 6.19.5
6-39
Forward Support Tube (ET).......................................................................................................... 5.10
5-19
Backup Method................................................................................................................ 5.10.4
5-20
Defects............................................................................................................................ 5.10.2
5-19
Description ...................................................................................................................... 5.10.1
5-19
Primary Method ............................................................................................................... 5.10.3
5-19
System Securing ............................................................................................................. 5.10.5
5-20
Index 5
