BELL HELICOPTER 430 Maintenance Manual page 18

BHT-430-MM-2
FOR OPERATION OF THE MILITARY
H E L I C O P T E R O U T S I D E O F T H E
A P P R O V E D C O M M E R C I A L FL I G H T
ENVELOPE. CONSEQUENTLY, PARTS
THAT HAVE BEEN USED ON MILITARY
HELICOPTERS SHOULD NOT BE USED
ON COMMERCIAL HELICOPTERS.
CAUTION
AIRWORTHINESS LIFE OF SOME KIT
COMPONENTS IS NOT COVERED IN
T H I S S C H E D U L E .
APPLICABLE SERVICE INSTRUCTION
( S I ) O R M A I N T E N A N C E M A N U A L
S U P P L E M E N T
COMPONENT SCHEDULES.
COMPONENT
Pin Assembly
Adapter Assembly
Pitch Horn Assembly
Damper Blade Set
Shear Restraint
Clamp Plate Set
Drive Bushing
Drive Plate Assembly
Bolt
Bolt
4-00-00
Page 6 Rev. 19 1 NOV 2012
R E F E R T O
( M M S ) F O R K I T
Table 4-1. Airworthiness Limitations Schedule
PART NUMBER
MAIN ROTOR
The retirement life given, or the failure to
give a retirement life to a component, does
not constitute a warranty of any kind. The
only warranty applicable to the helicopter or
any component is the warranty included in
the Purchase Agreement for the helicopter
or the component.
The airworthiness lives given to the components and
assemblies are determined by experience, tests, and
the judgment of Bell Helicopter engineers. The lives
cannot be changed without the approval of the
Minister of Transport Canada.
Prior to disposing of unsalvageable helicopter parts
and materials, caution should be exercised to ensure
that the parts and material are disposed of in a manner
that does not allow them to be returned for service.
Refer to FAA Advisory Circular 21-38 for guidance on
the disposal of unsalvageable aircraft parts and
materials.
1
430-010-127-101
430-010-109-101
430-010-115-101
430-310-104-105
430-310-101-105
430-010-105-105
430-010-124-101
430-010-126-101
20-065-08083
MS21250-08083
TC APPROVED
NOTE
AIRWORTHINESS LIFE
10,000
10,000
10,000
10,000
10,000
10,000
5000
10,000
5000
5000
ECCN EAR99