summary/shortened power point presentation about airworthiness. reference: PCAR part 5

1. Part 5
Airworthiness

2. REPORTING OF FAILURES,
MALFUNCTIONS, AND
DEFECTS

3. • Shutdown during flight
because of malfunction
in one or more engine
• A propeller feathering
system to control over
speed during flight
• Fuel-dumping
• An unintended landing
gear extension or
retraction, or opening or
closing of landing gear
doors during flight

4. • Brake system components that result in loss of
brake
• Aircraft structure that requires major repair
• Aircraft components or systems malfunctions that
result in taking emergency actions during flight
• Interruption to a flight route, unscheduled stops,
change or diversion from a route, caused by
known or suspected technical

5. • Any abnormal vibration or buffeting
• Failures to airspeed or altitude instrument during
a given operation of the aircraft.
• The number of engines removed prematurely
because of malfunction listed by make and
model and the aircraft type in which it was
installed or the number of propeller featherings in
flight, listed by type of propeller and engine and
aircraft on which it was installed

6. Here are the things needed to
include specifically in the report:
 Aircraft serial number
 Product model

7. APPROVAL OF
MATERIALS, PARTS,
PROCESSES, AND
APPLIANCES

8. REPLACEMENT AND MODIFICATION PARTS

9. An application for a Parts
Manufacturer Approval is
made to the Authority and
must include the following:
The identity of the
product
The name and address
of the manufacturing
facilities at which these
parts are to be
manufactured.
The design of the part

10. Test reports and
computations show the
design of the part meets the
airworthiness requirements.
Examination of the design
meets the airworthiness
requirements.

11. Each applicant for a Parts Manufacturer Approval
must make all inspections and tests necessary to
determine:
• Compliance with the applicable airworthiness
requirements
• That materials conform to the specifications in
the design
• That the part conforms to the drawings in the
design
• That the fabrication processes, construction, and
assembly conform to those specified in the
design.

12. Each holder of a Parts Manufacturer Approval shall
establish and maintain a fabrication inspection
system that ensures that each completed part
conforms to its design data and is safe for
installation on applicable type certificated
products. The system shall include the following:

13. • Materials subject to
damage and
deterioration
• Processes affecting the
quality and safety
• Parts in process must be
inspected for conformity
• Current design drawings
must be readily available
• Major changes to the
basic design
• Rejected materials and
components must be
segregated and identified
• Inspection records must
be maintained

14. APPROVAL OF
MATERIALS, PARTS,
PROCESSES, AND
APPLIANCES

15. It may be approved—
-Under a Parts Manufacturer Approval
-Under a Technical Standard Order issued by the
Federal Aviation Administration of the United States
of America.
-In conjunction with type certification procedures
for a product or in any other manner approved by
the Authority.

16. DAMAGE
TO
AIRCRAFT

17. A. When the aircraft
has sustained damage
that requires major
repair or replacement
of the affected
component, the CAAP
shall judge whether
the damage is of a
nature such that the
aircraft is no longer
airworthy as defined
by the appropriate
airworthiness
requirements.

18. B. If the damage is sustained or ascertained when the
aircraft is in the territory of another Contracting State,
the authorities of that Contracting State shall be
entitled to prevent the aircraft from resuming its flight
on the condition that they shall advise the CAAP
immediately, communicating to all details necessary
to formulate the judgment referred to in (A).

19. C. When CAAP considers that the damage
sustained is of a nature such that the aircraft is still
airworthy, the aircraft shall be allowed to resume its
flight.

20. APPROVAL OF MATERIALS, PARTS, PROCESSES,
AND APPLIANCES

21. It may be approved:
 Under a Parts Manufacturer Approval
 Under a Technical Standard Order issued by the
Federal Aviation Administration of the United
States of America.
 In conjunction with type certification procedures
for a product or in any other manner approved
by the Authority.

22. AIRCRAFT
MAINTENANCE
AND
INSPECTION

23. PERSONS AUTHORIZED
TO PERFORM
MAINTENANCE

24. A pilot licensed by the Authority
A person working under the supervision of a
aviation maintenance technician
A licensed aviation maintenance technician
An AMO