BHT-206L3-MM-1
5-00-00
15 MAY 2015 Rev. 22
Page 89
Export Classification C, ECCN EAR99
SCHEDULED INSPECTIONS
5-28.
100-HOUR INSPECTION
DATA REFERENCE
INSPECTION TASK DESCRIPTION
INITIAL
MECH OTHER
DATE: __________________W.O. _____________________
FACILITY: __________________________________________
HELICOPTER S/N: ___________________________________
REGISTRY NO.: _____________________________________
TOTAL TIME:_______________________________________
SIGNATURE:_______________
_________________________
NOTE
100-hour inspection must be accomplished when
using the 300-hour airframe progressive inspection
program or the 300-hour airframe periodic inspection
program.
Chapter 62
MAIN ROTOR
1.
Torque check pillow block retention hardware 84 to
107 inch-pounds (9.4 to 12 Nm). Examine for misalignment of
anti-slippage marks.
Chapter 53
TAILBOOM
CAUTION
ANY CRACK, CORROSION, OR LOOSE OR
SHEARED RIVET IS CAUSE FOR IMMEDIATE
GROUNDING OF THE HELICOPTER UNTIL THE
PROBLEM IS CORRECTED.
2.
Remove access panel on right side of aft fuselage.
Содержание Bell 206L3
Страница 10: ......
Страница 16: ......
Страница 30: ......
Страница 38: ......
Страница 46: ......
Страница 48: ......
Страница 70: ......
Страница 80: ......
Страница 86: ......
Страница 94: ......
Страница 114: ......
Страница 120: ......
Страница 132: ......
Страница 134: ......
Страница 140: ......
Страница 142: ......
Страница 146: ......
Страница 148: ......
Страница 154: ......
Страница 156: ......
Страница 158: ......
Страница 160: ......
Страница 162: ......
Страница 166: ......
Страница 172: ......
Страница 176: ......
Страница 178: ......
Страница 180: ......
Страница 186: ......
Страница 192: ......
Страница 204: ......
Страница 210: ......
Страница 226: ......
Страница 230: ......