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Question 1 of 29
1. Question
Refer to Figure 1. Determine which portion of the AD is applicable for Model )-690 series engine, serial No. 5863-40 with 283 hours time in service.
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Question 2 of 29
2. Question
A Cessna 180 aircraft has a McCauley propeller Model No. 2A34C50/90A. The propeller is severely damaged in a ground accident, and this model propeller is not available for replacement. Which of the following should be used to find an approved alternate replacement?
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Question 3 of 29
3. Question
Which of the following is used to monitor the mechanical integrity of the turbines, as well as to check engine operating conditions of a turbine engine?
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Question 4 of 29
4. Question
On a reciprocating engine aircraft using a shrouded exhaust muffler system as a source for cabin heat, the exhaust system should be
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Question 5 of 29
5. Question
(1) Airworthiness Directives are Federal Aviation Regulations and must be complied with unless specific exemption is granted.
(2) Airworthiness Directives of an emergency nature may require immediate compliance upon receipt.
Regarding the above statements,
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Question 6 of 29
6. Question
Which of the following contains a minimum checklist for 100-hour inspections of engines?
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Question 7 of 29
7. Question
When must an Airworthiness Directive (AD) be complied with after it becomes effective?
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Question 8 of 29
8. Question
Which of the following contains a table that lists the engines to which a given propeller is adaptable?
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Question 9 of 29
9. Question
Which of the following component inspections is to be accomplished on a 100-hour inspection?
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Question 10 of 29
10. Question
You are performing a 100-hour inspection on an R985-22 aircraft engine. What does the “985” indicate?
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Question 11 of 29
11. Question
Where would one find type design information for an R1830-92 engine certificated under the Civil Air Regulations (CAR) and installed on a DC-3?
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Question 12 of 29
12. Question
Straightening nitrided crankshafts is
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Question 13 of 29
13. Question
The breaking loose of small pieces of metal from coated surfaces, usually caused by defective plating or excessive loads, is called
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Question 14 of 29
14. Question
Each powerplant installed on an airplane with a Standard Airworthiness Certificate must have been
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Question 15 of 29
15. Question
A severe condition of chafing or fretting in which a transfer of metal from one part to another occurs is called
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Question 16 of 29
16. Question
Indentations on bearing races caused by high static loads are known as
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Question 17 of 29
17. Question
When inspecting an aircraft reciprocating engine what document is used to determine if the proper magnetos are installed?
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Question 18 of 29
18. Question
Which of the following can inspect and approve an engine major repair for return to service?
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Question 19 of 29
19. Question
What publication is used for guidance to determine whether a powerplant repair is major or minor?
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Question 20 of 29
20. Question
The airworthiness standards for the issue of type certificates for small airplanes with nine or less passenger seats in the normal, utility, and acrobatic categories may be found in the
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Question 21 of 29
21. Question
Which of the following contains approved data for performing a major repair to an aircraft engine?
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Question 22 of 29
22. Question
What maintenance records is/are required following a major repair of an aircraft engine?
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Question 23 of 29
23. Question
A ground incident that results in propeller sudden stoppage would require a crankshaft runout inspection. What publication would be used to obtain crankshaft runout tolerance?
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Question 24 of 29
24. Question
Select the Airworthiness Directive applicability statement which applies to an IVO-355 engine, serial number T8164 with 2,100 hours total time and 300 hours since rebuiliding.
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Question 25 of 29
25. Question
What publication contains the mandatory replacement time for parts of a turbine engine?
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Question 26 of 29
26. Question
How is the flow range of the fuel discharge nozzles installed in a fuel injected reciprocating engine indicated?
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Question 27 of 29
27. Question
What section in the instructions for continued airworthiness is FAA approved?
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Question 28 of 29
28. Question
Which of the following conditions is usually not acceptable to any extent in turbine blades?
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Question 29 of 29
29. Question
(1) Serviceability limits for turbine blades are much more stringent that are those for turbine nozzle vanes.
(2) A limited number of small nicks and dents can usually be permitted in any area of a turbine blade.
Regarding the above statements,
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