BELL HELICOPTER 205A-1, Руководство по обслуживанию

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BHT-205A1-MM-1
5-00-00
Page 4
Rev. 7 8 JUL 2013 Export Classification C, ECCN EAR99
3. Make sure the scheduled inspections, the special
inspections, and the required tests for all of the
installed kits are complied with.
4. Make sure all parts and components for which
Historical Service Records are required have
documented traceability to their original installation in
the helicopter.
WARNING
A L L P A R T S R E M O V E D , D U E T O
REACHING THEIR LIMITS OR AS A
RESULT OF AN ACCIDENT/INCIDENT
I N S P E C T I O N A N D D E E M E D
U N A I R W O R T H Y, S H A L L B E
PERMANENTLY MARKED AS SCRAP OR
PHYSICALLY DESTROYED TO THE
EXTENT THAT THERE IS NO CHANCE
OF REPAIR OR INSTALLATION ON ANY
HELICOPTER OR COMPONENT.
5. Make sure all limited life parts that have
completed their published operating limits are
replaced.
6. Make sure all of the components that have
completed their published overhaul periods are
overhauled.
7. Make sure all of the maintenance that is done on
the helicopter is done by an approved maintenance
organization.
The maintenance organization/person doing the
maintenance is responsible for the quality of the
maintenance done.
The owner/operator may choose to ask the
maintenance organization/person doing the
maintenance to perform the tasks listed by prior
arrangement through a separate formal agreement.
5-3. CRASH DAMAGE
Because of the many possible combinations that can
result from crash damage, it is not possible to include
the specific repair tasks in this category. The
helicopter mechanic must make an analysis of the
crash damage for each situation. Do the repair in
accordance with the degree of damage to the specific
part and the applicable repair procedures in this
manual. Call Product Support Engineering with your
analysis of the crash damage.
5-4. TYPES OF INSPECTIONS
1. The maintenance procedures may include
scheduled inspections, special inspections, conditional
inspections, component interim inspections, and
component overhaul inspections.
a. Scheduled inspections must occur at specified
operating intervals. The intervals may be in operating
time (hours), cycles, torque events (RIN), calendar
(days, months, years) or other assigned units. This
makes sure that the helicopter is airworthy.
b. Special inspections are of a temporary nature
or of a special interval that is not consistent with the
scheduled inspections.
c. Conditional inspections do not occur at a
specified time. A conditional inspection is the result of
known or suspected unusual event, known or
suspected malfunctions, or defects.
d. An interim inspection occurs between
overhauls.
e. The component overhaul schedule gives the
elapsed operating time at which a component must be
removed, disassembled, examined for condition, and
overhauled, in accordance with data approved by Bell
Helicopter Textron.
2. Airworthiness limitations — Replace components
in accordance with Airworthiness Limitations Schedule
(Chapter 4).
3. Lubrication and servicing requirements are in
addition to those stated in this chapter (Chapter 12).
4. For corrosion control refer to the Corrosion
Control Guide, CSSD-PSE-87-001 and the
BHT-ALL-SPM.
5. For the T53 Series engines, refer to the Lycoming
Maintenance and Overhaul Manual for the scheduled
inspection, special inspection, conditional inspection,
and component overhaul schedule.