BELL HELICOPTER 430 Maintenance Manual page 17

TC APPROVED
4-1. AIRWORTHINESS LIMITATIONS
SCHEDULE
WARNING
A L L R E P A I R
PROCEDURES PUBLISHED BY BELL
HELICOPTER TEXTRON, INCLUDING
COMPONENT RETIREMENT LIFE, ARE
BASED SOLELY ON THE USE OF BELL
APPROVED PARTS AND PROCESSES.
IF PARTS OR PROCESSES DEVELOPED
OR APPROVED BY PARTIES OTHER
THAN BELL HELICOPTER ARE USED,
T H E N T H E D A T A P U B L I S H E D O R
O T H E R W I S E S U P P L I E D B Y B E L L
HELICOPTER ARE NOT APPLICABLE.
THE USER IS WARNED TO NOT RELY
O N B E L L H E L I C O P T E R D A T A F O R
P A R T S A N D
APPROVED BY BELL HELICOPTER. ALL
A P P L I C A B L E I N S P E C T I O N S A N D
REPAIR METHODS MUST BE OBTAINED
FROM THE SUPPLIER OF THE PARTS
OR PROCESSES NOT APPROVED BY
BELL HELICOPTER. BELL HELICOPTER
IS NOT RESPONSIBLE FOR PARTS OR
PRO CE S SE S OT H ER T HAN T HO SE
WHICH IT HAS ITSELF DEVELOPED OR
APPROVED.
WARNING
C O N T I N U E D U S E O F A N Y T I M E /
C A L E N D A R / R I N
COMPONENT PAST ITS STATED LIMITS
I S N O T P E R M I T T E D A S I T C O U L D
S E R I O U S L Y
AIRWORTHINESS OF THE HELICOPTER.
THE COMPONENT MUST BE REMOVED
FROM THE HELICOPTER NOT LATER
THAN THE END OF THE LIFE LIMIT. IT
M U S T E I T H E R
UNSERVICEABLE OR MARKED IN A
CONSPICUOUS MANNER TO PREVENT
ECCN EAR99
AIRWORTHINESS LIMITATIONS SCHEDULE
A N D O V E R H A U L
P R O C E S S E S N O T
L I F E L I M I T E D
A F F E C T T H E
B E M A D E
CONTINUED USE, EVEN INADVERTENT
USE.
W H E N A R E P L A C E M E N T P A R T I S
INSTALLED, THE PART NAME, PART
N U M B E R, S E R I A L N U M B E R, A N D
C U R RE N T O P E R A T I N G H O U R S , I F
APPLICABLE, MUST BE RECORDED IN
THE HISTORICAL SERVICE RECORD
FOR THE ASSEMBLY OR HELICOPTER.
The requirements stated in Chapter 5 are to
be complied with and the appropriate
maintenance actions are to be performed.
The airworthiness life or inspection interval
for any part number contained in this
schedule applies to all the successive dash
numbers for that component unless it is
otherwise specified.
The mandatory Airworthiness Limitation Schedule
(Table 4-1) summarizes the mandatory maximum life,
in hours, years, or by Retirement Index Number (RIN)
of components with a limited airworthiness life. Parts
that are not on the schedule have an unlimited
airworthiness life. The Inspection Limitations Schedule
(Table 4-2) summarizes the mandatory inspection
interval in hours.
Refer to the engine manufacturer's publications for the
airworthiness limitations
components.
WARNING
S O M E P A R T S A R E I N S T A L L E D A S
O R I G I N A L E Q U I P M E N T O N B O T H
M I L I T A R Y A N D
H E L I C O P T E R S A N D M A Y H A V E A
LOWER AIRWORTHINESS LIFE AND/OR
OVERHAUL SCHEDULE WHEN USED
O N A M I L I T A R Y H E L I C O P T E R. I N
A D D I T I O N ,
SURROUNDING THEIR USE MAY CALL
1 NOV 2012 Rev. 19
BHT-430-MM-2
NOTE
NOTE
of the power plant
C O M M E R C I A L
C I R C U M S T A N C E S
4-00-00
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