Term
| 1. (001) Which character of an Air Force specialty code (AFSC) identifies the skill level? |
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Definition
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2. (001) Which Air Force specialty code (AFSC) identifies the awarded specialty in which an airman is most highly qualified to perform duty? |
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Definition
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3. (001) Which Air Force specialty code (AFSC) identifies the authorized manning document position to which an airman is assigned? |
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Definition
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Term
4. (002) Which tasks require the initials of a certifying official in the last column of a specialty training standard (STS)? |
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Definition
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Term
| 5. (003) As an aircraft fuel systems journeyman, you’ll be expected to |
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Definition
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Term
| 6. (003) As an aircraft fuel systems journeyman, what are your duties regarding hazardous materials? |
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Definition
| Handle, label, and dispose of them according to environmental standards. |
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Term
| 7. (004) What are the three types of wings? |
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Definition
| Operational, air base, and specialized mission wings. |
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Term
| 8. (004) Which group is responsible for operating the primary mission equipment? |
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Definition
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Term
| 9. (004) Which group is concerned with the maintenance of air and space weapon systems? |
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Definition
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Term
10. (005) To whom is the component maintenance squadron commander responsible for the overall squadron management? |
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Definition
| Maintenance group commander. |
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Term
| 11. (005) The technical authority and advisor of maintenance production in a maintenance shop is the |
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Definition
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Term
| 12. (005) Propellers are maintained by personnel assigned to the |
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Definition
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Term
13. (005) Maintenance and repair of gaseous and cryogenic servicing units are performed by the personnel assigned to the |
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Definition
| electro-environmental (E/E) flight. |
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Term
| 14. (006) Responsibility for enforcing sound maintenance practices rests with the |
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Definition
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Term
| 15. (006) Who selects personnel to perform special certification tasks? |
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Definition
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Term
16. (006) Responsibility for reviewing, evaluating, and taking corrective action based on quality assurance (QA) and other inspection reports rests with the |
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Definition
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Term
| 17. (007) Who approves local manufacture requests? |
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Definition
| Maintenance group commander (MXG/CC). |
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Term
| 18. (007) Who ensures there is an orientation program developed for all newly assigned personnel? |
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Definition
| Maintenance group commander (MXG/CC). |
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Term
19. (007) Advising the wing staff on operational capabilities, limitations, and status of resources is a function of the personnel assigned to the |
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Definition
| weapons and tactics flight. |
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Term
| 20. (007) Which flight trains aircrew, prepares the wing for wartime missions, and provides threat assessments? |
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Definition
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Term
| 21. (007) The maintenance schedule usually covers a period of |
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Definition
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Term
22. (008) Which of the following is a dynamic inspection system designed to improve aircraft combat capability? |
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Definition
| Maintenance standardization/evaluation program (MSEP). |
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Term
| 23. (008) The product improvement program is tasked to promote |
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Definition
| deficiency reporting programs. |
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Term
24. (009) Which is an inspection requiring skills, equipment, and facilities beyond your normal duties? |
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Definition
| Programmed depot maintenance (PDM). |
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Term
25. (010) Which basic inspection concept looks for cut tires, foreign object damage (FOD) covers and removal of safety pins? |
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Definition
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Term
| 26. (010) Which inspection concept is applicable to aircraft doing an immediate turnaround? |
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Definition
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Term
| 27. (011) Which inspection augments the basic post flight? |
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Definition
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Term
28. (012) Which inspection consists of checking certain components, areas or systems to ensure no condition exists that could result in failure before the next scheduled inspection? |
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Definition
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Term
| 29. (012) Which inspection concept is performed when the aircraft returns from a long range mission? |
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Definition
| Home station check (HSC). |
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Term
| 30. (013) What type inspection is performed on all newly assigned aircraft? |
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Definition
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Term
31. (013) An aircraft is examined with sufficient thoroughness to determine its mechanical fitness for flight and the completeness of its equipment and supporting documents during a |
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Definition
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Term
32. (013) Which inspection is outlined in the –6 technical order (TO) and differs from other types of inspections in that only one part of the aircraft or item requires the inspection. |
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Definition
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Term
| 33. (014) During an inspection, when are all write ups found and documented? |
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Definition
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Term
34. (014) During an inspection, when does the performance of operational checks and functional check flights begin? |
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Definition
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Term
35. (015) When you clear a discrepancy in the AF technical order (AFTO) 781’s, what will be placed over the symbol? |
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Definition
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Term
36. (016) Prior to performing maintenance, you review the AF technical order (AFTO) 781’s, to ensure |
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Definition
| there are no potential safety hazards. |
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Term
37. (016) On the AF technical order (AFTO) Form 781H, after refueling the aircraft, the person who performs or supervises the operation puts their name in block 14 using what format? |
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Definition
| Minimum signature (first initial and last name). |
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Term
38. (017) What part of the AF technical order (AFTO) Form 244 provides a means to document a quality control review of the form? |
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Definition
| Part IV, SUPERVISORY REVIEW. |
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Term
39. (017) Which section of AF technical order (AFTO) Form 244 is used to document delayed discrepancies and overdue time changes? |
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Definition
| Part V, INDUSTRIAL/SUPPORT EQUIPMENT RECORD. |
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Term
| 40. (017) In which AF technical order (AFTO) Form 95 block do you enter the manufacturer’s name? |
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Definition
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Term
41. (017) Part two of AF technical order (AFTO) Form 350 is used by the processing center for what purpose? |
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Definition
| Control the item/ensure timely maintenance. |
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Term
| 42. (018) The basic ingredient of all accidents is based on |
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Definition
| the law of cause and effect. |
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Term
| 43. (018) What percentage of all accidents is due to natural causes, such as lightning, storms, or floods? |
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Definition
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Term
| 44. (019) Many accidents can be prevented by simply |
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Definition
| keeping your work area clean and orderly. |
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Term
| 45. (019) All of these are examples of internal distracters except |
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Definition
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Term
| 46. (020) The main purpose of ground mishap reporting is to |
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Definition
| identify the circumstances or causes so that future accidents can be prevented. |
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Term
47. (020) An accident has resulted in the hospitalization of three or more personnel. What kind of mishap would this be classified as? |
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Definition
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Term
48. (020) An accident on the flightline has resulted in the death of a civilian worker. What kind of mishap would this be considered as? |
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Definition
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Term
| 49. (020) Which of these results would categorize an accident as a class C mishap? |
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Definition
| One or more days away from work. |
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Term
| 50. (021) What materials are used to make personnel static discharge plates? |
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Definition
| Copper, zinc, or zinc-coated metal. |
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Term
| 51. (021) The purpose of bonding is to eliminate |
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Definition
| differential in electrical charges between a component and the aircraft. |
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Term
| 52. (021) The correct sequence for bonding is to first attach the cable to the |
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Definition
| equipment then to the aircraft. |
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Term
| 53. (021) Why must you first attach a grounding cable to the earth ground and then the equipment or aircraft? |
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Definition
| You are allowing yourself to be grounded first. |
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Term
| 54. (021) Why shouldn’t you wear gloves when touching the personnel static discharge plate? |
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Definition
| Gloves are insulators and prevent the release of static electricity from your body. |
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Term
| 55. (022) The minimum safe distance from the front of an intake of an operating jet engine is |
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Definition
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Term
56. (022) What should you use to prevent other maintainers of inadvertent operation of devices such as landing gear and flight control surfaces? |
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Definition
| Warning tags AFTO Form 1492. |
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Term
| 57. (022) What type of communication may be used during ground refueling operations? |
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Definition
| The aircraft intercommunication system. |
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Term
| 58. (022) As a fuel systems journeyman, what are your responsibilities concerning ground locks? |
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Definition
| Ensure the ground crew has installed them before you begin work. |
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Term
| 59. (023) Two major contributors of foreign object damage (FOD) are poor |
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Definition
| work habits and housekeeping. |
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Term
| 60. (023) The three general classes of foreign object damage (FOD) are |
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Definition
| metal, stone, and miscellaneous. |
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Term
| 61. (024) Volatility is the rate at which a fuel |
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Definition
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Term
| 62. (024) What is the first thing you should do if your clothes become soaked with fuel or chemicals? |
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Definition
| Leave the area and remove your clothes. |
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Term
| 63. (024) One of the most common signs of excessive fuel vapor inhalation is |
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Definition
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Term
64. (025) What type of fuel spill involves an area greater than two feet, but is ten foot or less in any direction, or less than 50 square feet, and is not of a continuing nature? |
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Definition
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Term
| 65. (025) What action must be taken regarding a class I fuel spill on the flightline? |
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Definition
| Monitor the spill until the aircraft is moved. |
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Term
| 66. (026) At what percentage of oxygen is the atmosphere level considered to be oxygen deficient? |
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Definition
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Term
| 67. (026) What are the three hazards associated with compressed air? |
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Definition
| Air pressure, flying, particles and noise. |
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Term
| 68. (026) Which of the following would not be on a compressed air safety checklist? |
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Definition
| Use air in well ventilated area. |
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Term
| 69. (027) Respirator training must be documented on an |
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Definition
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Term
| 70. (027) Individually issued respirators should be cleaned and sanitized |
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Definition
| at the end of the each day in which they were used. |
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Term
| 71. (027) Respirators stored for emergency or rescue use must be inspected at least |
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Definition
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Term
| 72. (028) Which footwear items are authorized for wear inside a fuel cell? |
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Definition
| Static resistant or neoprene booties. |
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Term
| 73. (028) When you’re applying solvents to an aircraft structure, you may wear |
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Definition
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Term
| 74. (029) You must wear safety goggles when you’re |
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Definition
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Term
75. (029) What should you do to a self-contained emergency eyewash station before you begin any fuel systems maintenance? |
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Definition
| Ensure the unit is filled with fresh water. |
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Term
| 76. (030) What type of index technical order (TO) is most frequently used? |
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Definition
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Term
| 77. (030) Which is not listed by the index technical order (TO)? |
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Definition
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Term
| 78. (030) Which is a complete listing of technical order’s (TO) for a specific weapons system? |
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Definition
| List of applicable publications (LOAP). |
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Term
| 79. (031) A job guide is an example of |
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Definition
| an operations and maintenance (O&M) manual. |
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Term
80. (032) What type of time compliance technical order (TCTO) is issued for conditions that could have a negative effect on aircraft operational efficiency? |
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Definition
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Term
81. (032) Which time compliance technical order (TCTO) requires compliance within a specified time limit of one to ten days? |
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Definition
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Term
| 82. (034) What type of technical order (TO) is mainly a work simplification device? |
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Definition
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Term
| 83. (034) Which abbreviated technical order (TO) is meant to be followed step by step? |
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Definition
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Term
| 84. (035) What does the first number of a technical order (TO) designate? |
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Definition
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Term
| 85. (035) Technical order (TO) 1B–52G–4–4–1 is an example of what kind of TO? |
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Definition
| Illustrated parts breakdown (IPB). |
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Term
86. (037) A work stoppage caused by a technical order (TO) deficiency is considered to be a basis for what kind of TO improvement report? |
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Definition
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Term
| 87. (037) How are emergency technical order (TO) improvement reports submitted? |
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Definition
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Term
| 88. (038) The Air Force supply system is different from civilian supply systems because it |
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Definition
| requires more flexibility. |
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Term
| 89. (038) The Air Force supply system |
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Definition
| is managed on a functional basis. |
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Term
90. (039) Which system allows logistics personnel, customers, and commanders to track every item in the supply system through standardized procedures? |
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Definition
| Standard Base Supply System (SBSS). |
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Term
91. (040) The responsibility of a person to make good any loss, destruction, or damage of government property caused by misuse or negligence is known as what kind of liability? |
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Definition
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Term
| 92. (040) Concerning command responsibility for Air Force property, commanders are |
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Definition
| not exempt from pecuniary liability within their command. |
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Term
| 93. (040) Commanders must ensure that records of supply transactions are |
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Definition
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Term
| 94. (040) The term “custodian” as applied to the Air Force supply system refers to a |
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Definition
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Term
| 95. (040) What methods are used to relieve personnel of property responsibility? |
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Definition
| Turn-in and property transfer. |
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Term
| 96. (041) Which element of base supply manages all due-in from maintenance (DIFM) materiel? |
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Definition
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Term
| 97. (041) The repair cycle of a supply asset ends when the item is |
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Definition
| sent back to supply as serviceable or unserviceable. |
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Term
| 98. (042) What activity is the focal point for the resolution of a supply item deficiency? |
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Definition
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Term
99. (043) What monthly supply listing provides a means to monitor and verify that each due-out is still a valid requirement? |
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Definition
| Due-out Validation List (M–30). |
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Term
100. (043) What listing would you check to track the parts that have been ordered to fix repair cycle assets? |
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Definition
| AWP Validation List (D19). |
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Term
1. (201) What type of pumps is used for engine feed in the FWD and AFT reservoir tanks of a fighter aircraft? |
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Definition
| Dual-impeller, electrically driven. |
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Term
| 2. (201) The crossfeed valve on a fighter aircraft is a |
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Definition
| fuel pressure-operated gate valve. |
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Term
3. (201) On a fighter aircraft fuel system, a thermally-actuated valve in the heat exchanger outlet prevents fuel from exceeding |
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Definition
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Term
| 4. (202) To use body tank fuel to feed the engines on a tanker aircraft, the |
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Definition
| air refueling pumps must be operated. |
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Term
| 5. (202) To feed all engines from the center wing tank on a tanker aircraft, the |
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Definition
| tank to manifold valves must be opened. |
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Term
(203) The output pressure and the flow ratings of a centrifugal pump are greater than the amount the system needs in order to |
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Definition
| provide an ample supply of fuel in case of a single pump failure. |
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Term
| 7. (203) When fuel supply is required during negative gravity conditions, |
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Definition
| a dual-impeller centrifugal pump is used. |
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Term
8. (203) What feature prevents foreign objects from holding the bypass valve open in a dual-impeller pump? |
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Definition
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Term
| 9. (203) Which of the following is not an advantage of the quick change electrically drive fuel pump? |
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Definition
| Requires special tools to install. |
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Term
| 10. (204) The arrow stamped on the body of a check valve indicates the |
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Definition
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Term
| 11. (204) The flapper on a flapper-type check valve is opened by |
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Definition
| gravity flow or pump pressure. |
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Term
| 12. (204) What shutoff valve cannot withstand extreme pressures? |
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Definition
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Term
13. (204) What feature prevents excessive pressure from building up in trapped lines or within the body of a sliding gate valve? |
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Definition
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Term
| 14. (204) What type of seal is found between the disc and valve body on a disc-type valve? |
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Definition
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Term
15. (205) The best method for troubleshooting a fighter engine feed system component you suspect of leaking is to |
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Definition
| pressurize the manifold with fuel and look for leaks. |
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Term
16. (205) You are troubleshooting a boost pump problem on a fighter aircraft. To do this properly, your first step is to check for |
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Definition
| a direct pressure reading of the pump. |
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Term
17. (206) On a tanker aircraft, where must fuel be routed in order to feed any engine from any main tank? |
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Definition
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Term
18. (207) You are troubleshooting a malfunction of the crossfeed system on a tanker aircraft when you determine there is no pressure available to route fuel to the crossfeed manifold. The most probable cause of this malfunction is |
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Definition
| a malfunctioning boost pump. |
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Term
| 19. (208) The purpose of the power transfer method on a fighter aircraft is to |
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Definition
| augment fuel transfer and scavenge the tanks. |
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Term
| 20. (208) How many pumps are used in the power transfer system on a fighter aircraft? |
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Definition
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Term
21. (208) On a fighter aircraft, what type of pumps are the scavenge pumps and where are they located? |
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Definition
| Ejector-type; located in the F–2 tank. |
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Term
| 22. (208) On a fighter aircraft, |
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Definition
| the external centerline tank will transfer first. |
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Term
23. (209) You are troubleshooting a problem on a fighter aircraft. You find that none of the external tanks transferred fuel with the select switch in NORM position; however, the external wing tanks did transfer fuel with the select switch in WING FIRST position. The most probable cause of this malfunction is the |
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Definition
| centerline refuel/transfer valve is inoperative. |
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Term
209) You are troubleshooting a problem on a fighter aircraft when you discover that none of the external tanks transfer fuel, regardless of the switch positions. The most probable cause of this malfunction is the |
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Definition
| vent and pressurization valve is inoperative. |
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Term
| 25. (210) The fuel level control valve on a cargo aircraft is operated |
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Definition
| hydromechanically and controlled by a solenoid. |
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Term
26. (210) While transferring fuel from an auxiliary tank on a cargo aircraft, in order to determine if the auxiliary tank is empty, you would observe the |
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Definition
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Term
27. (211) The cargo aircraft component that is designed to sense fuel pressure and transmit a signal to an indicator on the fuel management panel to allow you to determine the output pressure of a boost pump is the pressure |
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Definition
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Term
28. (211) Which indication shows that a boost pump on a cargo aircraft is putting out sufficient pressure? |
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Definition
| PRESS LOW light extinguishes. |
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Term
29. (212) To prevent the introduction of foreign objects into the fuel transfer system of a cargo aircraft, the jettison mast is equipped with a |
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Definition
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Term
| 30. (212) Which type of fuel valves control the flow of fuel through the jettison system? |
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Definition
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Term
31. (213) What safety feature in the bomber aircraft fuel dump system prevents the accidental dumping of fuel while the aircraft is on the ground? |
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Definition
| The landing gear must be in the airborne position. |
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Term
32. (213) In addition to the dump valve, which valve(s) on a bomber aircraft must be open to allow fuel into the wing transfer lines to be dumped overboard? |
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Definition
| Ballast tank isolation valve only. |
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Term
33. (214) Which would most likely be used to control the automatic pump shutoff, when all fuel is depleted from a fuel tank? |
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Definition
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Term
34. (214) Refueling by using the fuel-level control valves is a much safer operation than filler neck refueling because the valves will |
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Definition
| automatically stop the flow of fuel into a tank prior to overflow. |
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Term
| 35. (214) What principle is used to operate fuel-level control valves? |
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Definition
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Term
| 36. (214) What part of a piston-type fuel-level control valve prevents fuel from entering the tank? |
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Definition
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Term
37. (215) Approximately how much air space is left at the top of the tanks of a cargo aircraft after ground refueling? |
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Definition
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Term
| 38. (215) The single point receptacle in a cargo aircraft refuel system is opened by engaging |
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Definition
| the lever on the refueling nozzle and closed by spring tension. |
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Term
39. (215) To allow fuel to flow from a cargo aircraft single point receptacle to the main wing manifold during ground refueling, the |
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Definition
| refuel isolation valve must be open. |
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Term
40. (216) What component is installed between the refuel manifold and each external tank on a fighter aircraft to permit selective refueling of the externals? |
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Definition
| Manually operated fuel shutoff valve. |
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Term
| 41. (216) When the FWD fuel system on the fighter aircraft is refueled, what tank will fill first? |
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Definition
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Term
| 42. (216) What is the refueling sequence for the AFT fuel system on a fighter aircraft? |
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Definition
| AFT reservoir, A–1 tank, then left wing tank. |
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Term
43. (217) During refueling of a fighter aircraft, fuel was vented overboard and the refueling operation would not stop. The most probable cause of this problem is an inoperative |
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Definition
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Term
44. (218) What light on a bomber aircraft aerial refueling system lets the pilot know if all conditions are satisfied prior to boom and receptacle connection? |
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Definition
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Term
45. (218) The aerial refueling circuitry on a bomber aerial refueling system is energized by the camoperated aerial refuel |
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Definition
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Term
| 46. (218) The reverse aerial refueling shutoff valve is a |
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Definition
| motor-operated butterfly valve. |
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Term
47. (219) What action(s) will generate command output signals from the EMUX and energize the aerial refuel power supply on a bomber aircraft? |
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Definition
Pulling down the PULL REFUEL T-handle and placing the MODE switch in the NORM position. |
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Term
48. (219) Which condition will result in an automatic disconnect of the boom and receptacle during aerial refueling on a bomber aircraft? |
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Definition
| Boom travel limits are exceeded. |
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Term
49. (219) A manual disconnect of the tanker and receiver on a bomber aircraft has been accomplished. What action will reset the UARRSI and signal amplifier, causing the READY/NWS light to illuminate? |
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Definition
| Placing the pilot trigger switch to the first detent. |
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Term
50. (220) You are troubleshooting a malfunction in a bomber aerial refueling system. The fault code for the malfunction is 28–25-AM. What does the letter “A” indicate? |
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Definition
| A fault isolation diagram is provided. |
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Term
51. (220) You are troubleshooting a problem on a bomber aircraft. At a certain point, the fault isolation diagram requests that you enter a PMC. To comply with the request you would enter the code on the |
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Definition
| CITS control and display panel in the aft crew station. |
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Term
| 52. (221) The purpose of the tank scavenge system on a cargo aircraft is to |
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Definition
| ensure an uninterrupted flow of fuel to the engines. |
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Term
53. (221) Combined with the ejector pumps, the cargo aircraft components that keep the boost pump inlet submerged with fuel at all times are the |
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Definition
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Term
54. (222) You are preparing to perform an operational check of the tank scavenge system on a cargo aircraft. To do the check properly, ensure the fuel quantity in the outboard main tank is at least |
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Definition
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Term
| 55. (223) Which situation could have a negative effect on the operation of the tank scavenge system? |
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Definition
| Boost pump inlet screens clogged. |
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Term
56. (224) How is the fuel drained from the main wing manifold of a cargo aircraft after a defuel operation? |
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Definition
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Term
| 57. (224) The aerial refueling manifold drain pump on a cargo aircraft is |
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Definition
| a rotary-vane type pump with positive displacement. |
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Term
58. (225) While troubleshooting a problem with the manifold drain system on a cargo aircraft, it seems that the single point receptacle (SPR) manifold does not drain after a refueling operation. You place the GRD REFUEL switch to the DRAIN position and then take a voltage reading at the applicable pins on the cannon plug for the SPR drain shutoff valve. You determine that 115 VAC is present and that the manual override level is in the CLOSED position. In this situation, the malfunctioning component is most likely |
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Definition
| an inoperative shutoff valve. |
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Term
59. (225) When troubleshooting a manifold drain system, the best method you can use to determine whether or not the single point receptacle manifold drain shutoff valve has opened is to |
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Definition
| observe the manual override lever. |
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Term
| 60. (226) On a cargo aircraft, the bellmouth inlet of the vent manifold in a fuel tank is located at the |
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Definition
| inboard end below the upper surface of the wing skin. |
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Term
| 61. (226) On a cargo aircraft vent system, the individual tank vent manifolds terminate |
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Definition
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Term
| 62. (226) Excessive air pressure can be released from the fuel tanks of a cargo aircraft by use of a |
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Definition
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Term
| 63. (227) Which condition could result in the malfunction of a vent float valve? |
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Definition
| Overfilling the fuel tank. |
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Term
64. (228) Which action will initiate the combat pressure schedule of the internal vent and pressurization valve on a fighter aircraft? |
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Definition
| Place the tank inert switch to the TANK INERTING position. |
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Term
65. (228) The external tank vent and pressurization valve on a fighter aircraft will regulate air pressure in psi to the external tanks in a range of |
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Definition
|
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Term
| 66. (229) The internal tank vent and pressurization valve on a fighter aircraft is located in the |
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Definition
|
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Term
67. (230) What would be the most probable cause if all the external tanks on a fighter aircraft failed to transfer? |
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Definition
| Vent and pressurization valve stuck closed. |
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Term
68. (231) The positive signals from the capacitance tank units on the fuel quantity indicating system for a fighter aircraft are routed through |
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Definition
| a control unit, amplifier, to an indicator channel. |
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Term
69. (231) On a fighter aircraft, the TOTAL digital readout displays the total fuel on the aircraft with the fuel quantity select switch in all positions except |
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Definition
|
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Term
70. (232) When the thermistor head on a fuel level sensor for a fighter aircraft is covered with fuel, there will be |
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Definition
| a decrease in temperature and an increase in resistance. |
|
|
Term
71. (232) Which component, when uncovered, will result in the illumination of a FUEL LOW light on the caution light panel of a fighter aircraft? |
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Definition
|
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Term
| 72. (233) Two types of protective devices used in aircraft electrical circuits are the |
|
Definition
| fuse and circuit breaker. |
|
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Term
73. (233) Which electrical circuit component may be considered to be both a protective device and a load device? |
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Definition
|
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Term
| 74. (233) Solenoids are commonly used in aircraft fuel systems to |
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Definition
| manually control a fuel level control valve. |
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Term
75. (233) Which component is designed to provide a way to quickly connect and disconnect wires, thereby simplifying the installation of a shutoff valve? |
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Definition
|
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Term
76. (233) While the pins on a cannon plug are lettered for ease of identification, which letters are not used? |
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Definition
|
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Term
| 77. (234) What is the purpose of a travel limit switch in an aircraft fuel systems electrical circuit? |
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Definition
| Remove power to a shutoff valve after it has opened or closed. |
|
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Term
78. (235) You are using a multimeter to measure voltage in an electrical circuit. During the measurement, the letters “OL” appear on the digital display to indicate that the |
|
Definition
| circuit voltage is higher than the highest range selected. |
|
|
Term
79. (235) While preparing to use a multimeter to test a circuit, you choose to turn the meter on and place it in the auto-range mode. To do this you would |
|
Definition
| place the function selector rotary switch to the AUTO position. |
|
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Term
80. (236) What type of technical manual would you use to troubleshoot an electrical system problem on a modern-type aircraft? |
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Definition
|
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Term
1. (401) What type of fuselage construction uses a fabric or thin metal covering, and may be found on small, lightweight aircraft? |
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Definition
|
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Term
| 2. (401) The primary structural components of an aircraft wing include the spars, ribs, and |
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Definition
|
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Term
| 3. (401) Which assembly includes the aft end of the fuselage of conventionally designed aircraft? |
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Definition
|
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Term
| 4. (402) Which of the following are examples of secondary flight controls? |
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Definition
|
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Term
| 5. (403) Low observable (LO) technology allows modern aircraft to avoid |
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Definition
|
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Term
6. (404) The situation that describes an ideal installation of a bolt on an aircraft component is the grip length of the bolt is |
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Definition
| slightly shorter than the thickness of the materials being joined. |
|
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Term
| 7. (404) The size of a bolt is generally stated in terms of its |
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Definition
| diameter, length, and threads per inch. |
|
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Term
| 8. (404) What type of bolt is used where standard-type bolt is impractical? |
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Definition
|
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Term
| 9. (405) For which aircraft application should a self-locking nut not be installed? |
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Definition
| Connecting sections of a movable joint. |
|
|
Term
| 10. (406) Which type of rivet is used on the top skin surface of an aircraft? |
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Definition
|
|
Term
| 11. (406) Which is a feature of the hi-lok type of fastener? |
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Definition
| It can be installed with hand tools. |
|
|
Term
| 12. (407) What type of tubing is used in high-pressure systems such as the landing gear system? |
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Definition
|
|
Term
| 13. (408) Flexible hose is used in areas of the aircraft |
|
Definition
| which are subject to great amount of vibration. |
|
|
Term
| 14. (408) Which example is not acceptable regarding the installation of a flexible hose assembly? |
|
Definition
| Use oil to aid the installation of a self-sealing hose. |
|
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Term
| 15. (409) What is the first step when removing a V-band type coupling? |
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Definition
|
|
Term
16. (410) What is the maximum number of widely-spaced bolts that may be safety-wired together using the double-twist method? |
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Definition
|
|
Term
17. (410) What minimum diameter safety wire should be installed on bolts having a .050-inch drilled hole? |
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Definition
|
|
Term
| 18. (411) Why is the use of cotter pins on aircraft systems favorable? |
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Definition
| They can be removed and installed quickly. |
|
|
Term
19. (412) During an integral tank inspection, you discover an area at which the protective coating is scarred and the metal is discolored. Pitting has also occurred to a depth of one mil (0.001 inch). What degree of corrosion has taken place? |
|
Definition
|
|
Term
| 20. (413) When installing removable screws and bolts, what portion is coated with sealant? |
|
Definition
| Coat the lower side of the heads of screws and bolts with sealant. |
|
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Term
| 21. (414) What types of hammers are used in fuel systems maintenance? |
|
Definition
| Soft-faced mallets and ball-peen hammers. |
|
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Term
| 22. (414) Which type of wrench should you use to tighten an internal wrenching nut? |
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Definition
|
|
Term
| 23. (415) What should you use to clean tools that are extremely greasy and grimy? |
|
Definition
| Approved cleaning solvent. |
|
|
Term
24. (416) How many foot-pounds of torque are produced by 120 inch-pounds of force on a breakaway-type torque wrench? |
|
Definition
|
|
Term
| 25. (417) What powered tool would you use to remove access door screws? |
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Definition
|
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Term
| 26. (417) Which tool would you use to repair a fuel cell fitting? |
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Definition
|
|
Term
27. (417) Which type of attachment should you use on the fuel cell pneumatic buffer to buff bladder cells and flanges? |
|
Definition
|
|
Term
28. (418) The ratio of output pressure to input pressure of a two-part sealant high-pressure injection gun is |
|
Definition
|
|
Term
| 29. (419) After you are finished using the sealant filleting gun, what must be done? |
|
Definition
| Clean the residual sealant. |
|
|
Term
| 30. (420) The one-part sealant injection gun is used to inject sealant into |
|
Definition
| channels under the wing skin. |
|
|
Term
| 31. (421) What will happen to an air hose if you run it over with heavy equipment? |
|
Definition
|
|
Term
| 32. (422) When using the electric knife to cut foam, which do you not inspect? |
|
Definition
|
|
Term
| 33. (423) When you use the water manometer, you should |
|
Definition
| unplug the negative pressure connection when the fuel tank is given a positive test. |
|
|
Term
| 34. (424) What is the preferred piece of equipment for monitoring fuel tanks? |
|
Definition
| Photo-ionization detector (PID). |
|
|
Term
| 35. (425) The Model T477W bonding meter is designed to measure |
|
Definition
|
|
Term
| 36. (425) You turn on the display on the T477W bonding meter by pressing the |
|
Definition
|
|
Term
| 37. (425) All values displayed on the T477W Bonding meter are in |
|
Definition
|
|
Term
38. (426) What support equipment item is designed to operate pneumatic tools at a maximum air pressure of 200 pounds per square inch (psi)? |
|
Definition
|
|
Term
| 39. (426) Which is a feature of the MC–7 Air compressor? |
|
Definition
| Capable of delivering high volumes of air. |
|
|
Term
| 40. (427) Which is an inspection requirement on the pneumatic vacuum? |
|
Definition
|
|
Term
| 41. (428) Which two buttons must you press to start the HDU–13/M heater? |
|
Definition
|
|
Term
| 42. (428) Which heater is not explosion proof and must be kept outside the repair area? |
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Definition
|
|
Term
43. (429) If you are using a pneumatic powered blower, the maximum pressure on the pressure gauge should be |
|
Definition
|
|
Term
| 44. (429) An equipment item that is not permitted inside the fuel systems repair area is the |
|
Definition
|
|
Term
| 45. (430) Where should you position the fuel cell/tank servicing cart? |
|
Definition
| Inside the fuel system repair area. |
|
|
Term
| 46. (430) When must you station a safety guard at the fuel cell/tank servicing cart? |
|
Definition
| During access door removal and cell/tank purging. |
|
|
Term
47. (431) Which support equipment item is equipped with a 110 volts alternating current (VAC) power receptacle to permit the use of electrical equipment outside the repair area? |
|
Definition
|
|
Term
| 48. (432) Which maintenance stand is not adjustable? |
|
Definition
|
|
Term
| 49. (432) Which maintenance stand can you easily move by yourself? |
|
Definition
|
|
Term
| 50. (432) Maintenance stands used specifically for fuel systems maintenance should be equipped with |
|
Definition
|
|
Term
| 51. (433) In a new facility, emergency personnel showers must |
|
Definition
|
|
Term
| 52. (433) What type scrub sinks is required in existing fuel system facilities? |
|
Definition
|
|
Term
53. (433) Aircraft which are adjacent to an open fuel systems repair area must not be operated under their own power within |
|
Definition
|
|
Term
| 54. (434) What outside agency must be notified prior to opening fuel tanks? |
|
Definition
| Fire Protection Services. |
|
|
Term
| 55. (435) Who is responsible for evaluating industrial ventilation systems? |
|
Definition
| Bioenvironmental Engineering Flight. |
|
|
Term
56. (435) When filling out an AFTO Form 1492, Warning Tag, who is required to sign the signature block? |
|
Definition
| RED X qualified supervisor. |
|
|
Term
57. (436) The minimum safe distance between an aircraft using full powered radar and the fuel system repair area is |
|
Definition
|
|
Term
58. (437) What type of wheels must be installed on rolling support equipment used in the fuel systems repair area? |
|
Definition
|
|
Term
59. (437) When tasked to set up the open repair area, where must you place the powered support equipment? |
|
Definition
| Outside the 50 foot marked area. |
|
|
Term
| 60. (437) An air compressor operating outside the fuel systems repair area |
|
Definition
| does not require grounding or bonding. |
|
|
Term
| 61. (438) Who designates the Alternate Entry Authority for a fuel shop? |
|
Definition
|
|
Term
| 62. (438) Which is the most important role when serving as an attendant? |
|
Definition
| Recognizing symptoms of over exposure. |
|
|
Term
63. (439) Who must be identified on the emergency response plan as being authorized to attempt initial removal of incapacitated entrants? |
|
Definition
| Authorized attendant or runner/equipment monitor. |
|
|
Term
| 64. (440) Which task would be considered a change to the entry permit? |
|
Definition
| The aircraft is moved from one repair location to another. |
|
|
Term
| 65. (441) What must you do when you are draining fuel into a metallic container? |
|
Definition
| Bond container to aircraft. |
|
|
Term
| 66. (442) What is the recommended method of purging an aircraft fuel tank? |
|
Definition
|
|
Term
| 67. (443) When removing fire suppression foam from an aircraft fuel tank, you should |
|
Definition
| wear chemical-resistant gloves. |
|
|
Term
| 68. (443) Foam removed from a fuel tank may be stored in an |
|
Definition
| electro-static-free plastic bag. |
|
|
Term
69. (443) If you were planning to cut small quantities of replacement foam for a fuel tank, you would use |
|
Definition
|
|
Term
| 70. (444) If you are performing the task of depuddling, which do you use to remove the fuel? |
|
Definition
|
|
Term
| 71. (445) The structural components that form the end boundaries of an integral tank are the |
|
Definition
|
|
Term
| 72. (446) The three approved methods for locating a fuel leak exit point on an integral tank are |
|
Definition
| Leak detection powder, pressure test, and gas detection. |
|
|
Term
| 73. (447) You have a Class “D” running leak in an external location. Which step is appropriate? |
|
Definition
| Repair to no leakage or condition 1 or 2. |
|
|
Term
| 74. (447) What factor(s) determine the appropriate condition/action of an integral tank fuel leak? |
|
Definition
| Classification and location. |
|
|
Term
75. (448) What type of illustration (view) of the structure should be drawn to aid in locating a seal plane? |
|
Definition
|
|
Term
76. (448) After you have found the exact leak exit point, what is the next step prior to repairing the fuel leak? |
|
Definition
|
|
Term
77. (449) When should the hollow bolt dye injector method be used to isolate a leak source in an integral tank? |
|
Definition
| When the double cup assembly was unsuccessful. |
|
|
Term
| 78. (450) What are the two parts of curing type sealant? |
|
Definition
|
|
Term
79. (451) Which basic type of access door opens into the fuel tank, providing a tighter seal than other types? |
|
Definition
|
|
Term
80. (452) After the defective sealant has been removed, how far from the ends of the fillet should you abrade to prepare the surface for the new fillet? |
|
Definition
|
|
Term
| 81. (453) A brush coat of sealant should be applied with |
|
Definition
|
|
Term
| 82. (453) A large fillet is defined as any fillet |
|
Definition
| greater than a half inch. |
|
|
Term
83. (454) When injecting using high pressure injection gun, which step will protect the aircraft structure? |
|
Definition
| Appling a temporary repair. |
|
|
Term
84. (455) The initial shelf life of a sealant material has expired. The sealant has been tested and has been found to be serviceable. The shelf life may now be updated |
|
Definition
|
|
Term
| 85. (456) Which tool should you use to remove a repair done with Hardman epoxy? |
|
Definition
| Plastic scraper and needle-nose pliers. |
|
|
Term
| 86. (457) The ply of a self-sealing cell that contains the fuel is the |
|
Definition
|
|
Term
| 87. (458) The fuel cell is plasticized prior to storage in order to |
|
Definition
| prevent cracking and drying. |
|
|
Term
| 88. (459) Never attempt to fold, unfold, or flex a bladder cell if the cell temperature is below |
|
Definition
|
|
Term
89. (459) What is the maximum length of time you should allow a self-sealing fuel cell to remain collapsed? |
|
Definition
|
|
Term
| 90. (460) Which condition will likely result in a fuel cell fitting leak? |
|
Definition
| Hair or lint between an o-ring and its groove. |
|
|
Term
| 91. (460) Vithane cells which have been in storage for a long time in a dry climate will tend to |
|
Definition
|
|
Term
| 92. (461) What is the most important factor in isolating a fuel cell leak? |
|
Definition
| Knowledge of the cavity drain system. |
|
|
Term
| 93. (462) Which discrepancy would likely result in a fast and severe type of fuel cell leak? |
|
Definition
| Loose interconnect fitting. |
|
|
Term
| 94. (463) Which cell repair is best performed at depot or contractor facilities? |
|
Definition
|
|
Term
| 95. (463) Which cell repair is best performed at field level? |
|
Definition
|
|
Term
| 96. (464) The inside patch required to repair a hole in a bladder cell must be cut |
|
Definition
|
|
Term
| 97. (465) The curing temperature for the heating element used in the vulcanizing repair method is |
|
Definition
|
|
Term
98. (466) You have removed a fuel cell and during the inspection have found a defect, what should you do next? |
|
Definition
| Refer to applicable TO for allowable limits. |
|
|
Term
| 99. (467) Which does not subject the exterior of the fuel cell to damage? |
|
Definition
|
|
Term
| 100. (468) Cells up to 1000 gallons can be pressurized up to |
|
Definition
|
|