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Key Reqs Analysis kra Show Simple Rules Show Complex Rules
. . .
1. Functional 2. Performance 3. Systems 4. Architecture 5. Safety
6. Software 7. Hardware 8. Environmental 9. Mechanical 10. Facilities
11. Training 12. Maintenance 13. Support 14. RMA 15. EMI
16. Ergonomics 17. ATC RDP 18. ATC FDP 19. ATC Automation 20. Security
21. Air Defense

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Key Reqs Analysis: Key reqs should be methodically sought by asking each stakeholer what they feel are their key reqs. These reqs are cost and or schedule drivers. They can be found by asking:

1. have we done this before
2. has someone else done this before
3. is a new technology, process, or method needed
4. is a new product needed...

This service looks for and counts all word or phrase instances set in the access field. Selecting a word from the list and submitting the report will provide the related text. Since the user defines these words there is no reason to enable noise word filters. This is a very high level service that relies on human ability to recognize their key req from a single word or phrase.

1. SAT-2 Each system must include the following items:
. . . 3. Systems: Key Reqs Analysis system 1

2. SAT-3 a. Control Unit - one per system.
. . . 3. Systems: Key Reqs Analysis system 1

3. SAT-5 (1) Two optical heads for Type L-849I/V systems.
. . . 3. Systems: Key Reqs Analysis systems 1

4. SAT-6 (2) Seven optical heads for Type L-859I/V systems.
. . . 3. Systems: Key Reqs Analysis systems 1

5. SAT-7 c. Power supply (as required for each system).
. . . 3. Systems: Key Reqs Analysis system 1
. . . 8. Environmental: Key Reqs Analysis Power 1

6. SAT-8 d. Instruction manual - one per system.
. . . 3. Systems: Key Reqs Analysis system 1

7. SAT-10 Cables for connecting between the control unit and optical assemblies or between the optical head and power supply when installed remotely (paragraph 3.5.2) are not included in this specification. However, the instruction manual must provide sufficient information to guide the installer in selecting the proper cables.
. . . 8. Environmental: Key Reqs Analysis power 1

8. SAT-11 3.2 System Description.
. . . 3. Systems: Key Reqs Analysis System 1

9. SAT-12 The REIL system is used to identify the threshold (approach end) of a visual or instrument non-precision runway and provides guidance to pilots during approach for landing. The REIL consists of two uni-directional or omni-directional simultaneous discharge-type flashing lights. A light is located at each side of the runway threshold.
. . . 3. Systems: Key Reqs Analysis system 1

10. SAT-13 The ODALS system uses seven omni-directional discharge-type flashing lights, five of which are installed on an extended runway centerline. The lights flash in sequence and appear as a ball of light traveling toward the runway threshold. This aids the pilot in determining which runway is in use. In addition to the five centerline lights, two lights are installed in a REIL configuration. The two REIL system lights flash simultaneously after the last flash of the centerline lights.
. . . 3. Systems: Key Reqs Analysis system 2

11. SAT-14 3.3 Environmental Requirements.
. . . 8. Environmental: Key Reqs Analysis Environment 1

12. SAT-15 The equipment must be designed for outdoor operation in the following environmental conditions:
. . . 8. Environmental: Key Reqs Analysis environment 1

13. SAT-16 a. Temperature: The equipment must operate at temperatures from (-40 to +131 degrees Fahrenheit (F) (-40 to +55 degrees Celsius (C)).
. . . 8. Environmental: Key Reqs Analysis Temperature 2

14. SAT-18 c. Temperature Shock: The equipment must operate and not be damaged by the sudden application of cold water to the light emitting surface of an optical assembly at its normal operating temperature.
. . . 8. Environmental: Key Reqs Analysis Temperature 3
. . . 15. EMI: Key Reqs Analysis emi 1

15. SAT-19 d. Humidity: The equipment must operate at a relative humidity of up to 100 percent, including conditions of dew or frost.
. . . 8. Environmental: Key Reqs Analysis Humidity 2

16. SAT-29 The effective intensity must be maintained when the equipment is operated within plus or minus 10 percent of the design input voltage or when operated at the design input voltage and subjected to the temperature range per paragraph 3.3a. Light output below the vertical cutoff points must be minimized.
. . . 8. Environmental: Key Reqs Analysis temperature 1

17. SAT-97 The color of light emitted by the optical head assemblies must be equivalent to that produced by an unfiltered xenon gas discharge lamp (approximately 4,000-8,000 degrees Kelvin).
. . . 15. EMI: Key Reqs Analysis emi 1

18. SAT-100 a. The discharge-type flashing light systems must be capable of for continuous operation.
. . . 1. Functional: Key Reqs Analysis capable 1
. . . 3. Systems: Key Reqs Analysis systems 1

19. SAT-102 c. All systems must have provisions for remote control per paragraph 3.5.4.2
. . . 3. Systems: Key Reqs Analysis systems 1

20. SAT-104 e. The power input to the optical assembly may be interrupted during intensity step changes.
. . . 8. Environmental: Key Reqs Analysis power 1

21. SAT-105 f. The system design must prohibit the occurrence of flashes other than per paragraphs 3.4.2 and 3.4.3.
. . . 3. Systems: Key Reqs Analysis system 1

22. SAT-107 a. The optical assembly consists of an optical head and a power supply.
. . . 8. Environmental: Key Reqs Analysis power 1

23. SAT-108 b. The Type L-849 optical head must be attached to the power supply enclosure.
. . . 8. Environmental: Key Reqs Analysis power 1
. . . 9. Mechanical: Key Reqs Analysis enclosure 1

24. SAT-109 c. Type L-859 optical heads must be capable of being attached to the power supply enclosure or installed remotely up to 150 feet (45 m) from the power supply.
. . . 1. Functional: Key Reqs Analysis capable 1
. . . 8. Environmental: Key Reqs Analysis power 2
. . . 9. Mechanical: Key Reqs Analysis enclosure 1

25. SAT-110 d. Brackets must be provided for mounting the optical head directly to the power supply enclosure or onto a single vertical 2-inch Electrical Metallic Tubing (EMT) conduit for remote locations.
. . . 7. Hardware: Key Reqs Analysis Electrical 1
. . . 8. Environmental: Key Reqs Analysis power 1
. . . 9. Mechanical: Key Reqs Analysis enclosure 1

26. SAT-113 g. Frangible mounting hardware per FAA Drawing C-6046 (or equivalent) must be provided for Type L-849 optical assemblies and for Type L-859 optical heads mounted on 2-inch EMT conduit.
. . . 7. Hardware: Key Reqs Analysis hardware 1

27. SAT-116 3.5.2.2 Power Supply.
. . . 8. Environmental: Key Reqs Analysis Power 1

28. SAT-117 The power supply provides power and triggering pulses to the optical head.
. . . 8. Environmental: Key Reqs Analysis power 2

29. SAT-118 a. A power supply may power more than one optical head assembly.
. . . 8. Environmental: Key Reqs Analysis power 2

30. SAT-119 b. The power supply must be designed to operate safely and reliably with the voltages and amperages required and with safety features consistent with those required for the control unit.
. . . 5. Safety: Key Reqs Analysis safe 2
. . . 8. Environmental: Key Reqs Analysis power 1

31. SAT-120 c. The power supply must be housed in a National Electrical Manufacturers Association (NEMA) type 4 (or equal) enclosure with a hinged access door and provision for padlocking.
. . . 7. Hardware: Key Reqs Analysis Electrical 1
. . . 8. Environmental: Key Reqs Analysis power 1
. . . 9. Mechanical: Key Reqs Analysis enclosure 1

32. SAT-121 d. Frangible points per FAA Drawing C-6046 (or equivalent) and associated hardware must be provided to mount the power supply enclosure on its foundation
. . . 7. Hardware: Key Reqs Analysis hardware 1
. . . 8. Environmental: Key Reqs Analysis power 1
. . . 9. Mechanical: Key Reqs Analysis enclosure 1

33. SAT-129 The control unit powers and controls the individual optical assemblies.
. . . 8. Environmental: Key Reqs Analysis power 1

34. SAT-130 NOTE: At the manufacturer's option, the control unit may be integrated into a power supply enclosure; however, the following requirements must still be met with regard to any power supply/control unit.
. . . 8. Environmental: Key Reqs Analysis power 2
. . . 9. Mechanical: Key Reqs Analysis enclosure 1

35. SAT-132 b. The control unit must be housed in a NEMA type 4 enclosure (or equal) with a hinged door and have provisions for padlocking.
. . . 9. Mechanical: Key Reqs Analysis enclosure 1

36. SAT-133 c. Terminal blocks with a suitable voltage rating must be located near the side or bottom of the enclosure for termination of external power and control wires feeding into the control unit. The terminal blocks must accommodate No. 8 through No. 20 American Wire Gauge (AWG) wires with an insulation rating up to 600V.
. . . 8. Environmental: Key Reqs Analysis power 1
. . . 9. Mechanical: Key Reqs Analysis enclosure 1

37. SAT-134 d. Mounting lugs or bolts must be provided on the back of the enclosure to allow vertical mounting.
. . . 9. Mechanical: Key Reqs Analysis enclosure 1

38. SAT-135 e. If the control unit is not integrated with the power supply, frangible points per FAA Drawing C-6046 (or equivalent) and associated hardware must be provided to mount the control enclosure on its foundation.
. . . 7. Hardware: Key Reqs Analysis hardware 1
. . . 8. Environmental: Key Reqs Analysis power 1
. . . 9. Mechanical: Key Reqs Analysis enclosure 1

39. SAT-136 f. A service entrance power disconnect switch must be furnished when utilizing either a voltage or constant current power source.
. . . 8. Environmental: Key Reqs Analysis power 2

40. SAT-137 g. If the disconnect switch is mounted external to the control unit enclosure, it must be weatherproof and have provisions for locking.
. . . 9. Mechanical: Key Reqs Analysis enclosure 1

41. SAT-138 h. A ground terminal must be provided on the outside of the control unit enclosure.
. . . 9. Mechanical: Key Reqs Analysis enclosure 1

42. SAT-140 The manufacturer may optionally offer elapsed time meters in either L-849 or L-859 power supply assemblies.
. . . 8. Environmental: Key Reqs Analysis power 1

43. SAT-144 An optional adapter may be provided to allow the discharge-type lighting system to be powered by an airport series lighting circuit (that may or may not have other types of lighting on the same circuit) which is energized by a constant current regulator as described in AC 150/5345-10, Specification for Constant Current Regulators Regulator Monitor. When the runway edge lights are on, the discharge-type lighting equipment must be on.
. . . 3. Systems: Key Reqs Analysis system 1
. . . 8. Environmental: Key Reqs Analysis power 1

44. SAT-145 a. The circuit adapter must be compatible with series to series isolation transformer per AC 150/5345-47, Specification for Series to Series Isolation Transformers for Airport Lighting Systems. The input to the isolation transformer will be either from a 6.6 or 20 ampere series lighting circuit. The output of the transformer must be 6.6A to the series lighting circuit adapter. The manufacturer does not supply the isolation transformer or any associated cabling.
. . . 3. Systems: Key Reqs Analysis Systems 1

45. SAT-146 b. The discharge-type lighting system must operate and be compatible with all approved constant current regulators. A series circuit adapter must provide ON/OFF control of Type L-849I, Styles A,B,C, and D single intensity equipment depending on the current level in the runway lighting circuit. For Type L-849I Styles E and F and Type-L859 Style F three intensity level equipments, see Table 2 to correlate regulator current steps with discharge-type lighting equipment brightness levels.
. . . 3. Systems: Key Reqs Analysis system 1

46. SAT-147 c. The series circuit adapter circuitry may be incorporated into the control unit or housed in a separate enclosure. Any separate enclosure must pass all the environmental tests in this specification.
. . . 8. Environmental: Key Reqs Analysis environment 1
. . . 9. Mechanical: Key Reqs Analysis enclosure 2

47. SAT-220 3.5.4 System Control.
. . . 3. Systems: Key Reqs Analysis System 1

48. SAT-222 All discharge-type lighting systems must have a local control capability located in the control unit for maintenance purposes. For equipment Styles A, B, C, and D, a three position switch must be per Table 3.
. . . 1. Functional: Key Reqs Analysis capability 1
. . . 3. Systems: Key Reqs Analysis systems 1
. . . 12. Maintenance: Key Reqs Analysis maintenance 1

49. SAT-223 Table 3. Single Intensity Switch Functions
. . . 1. Functional: Key Reqs Analysis Function 1

50. SAT-225 Switch Function
. . . 1. Functional: Key Reqs Analysis Function 1

51. SAT-227 System controlled by remote control (ON/OFF/Intensity)
. . . 3. Systems: Key Reqs Analysis System 1

52. SAT-229 System ON
. . . 3. Systems: Key Reqs Analysis System 1

53. SAT-231 System OFF
. . . 3. Systems: Key Reqs Analysis System 1

54. SAT-233 For equipment Styles E and F, the switch must be a five position rotary switch with mechanical detents, labeled as follows to perform the indicated functions per Table 4.
. . . 1. Functional: Key Reqs Analysis function 1
. . . 9. Mechanical: Key Reqs Analysis mechanical 1

55. SAT-234 Table 4. Three Intensity Switch Functions
. . . 1. Functional: Key Reqs Analysis Function 1

56. SAT-236 Switch Function
. . . 1. Functional: Key Reqs Analysis Function 1

57. SAT-238 System controlled by remote control (ON/OFF/Intensity)
. . . 3. Systems: Key Reqs Analysis System 1

58. SAT-240 Power and control circuits de-energized
. . . 8. Environmental: Key Reqs Analysis Power 1

59. SAT-242 System operating at LOW intensity flash
. . . 3. Systems: Key Reqs Analysis System 1

60. SAT-244 System operating at MEDIUM intensity flash
. . . 3. Systems: Key Reqs Analysis System 1

61. SAT-246 System operating at HIGH intensity flash
. . . 3. Systems: Key Reqs Analysis System 1

62. SAT-249 a. The Control Unit for Types L-849V and L-859V must have provisions for remote control by a switch or by a radio receiver/decoder unit. The operating voltage for the remote control system must not exceed 120 volts AC or plus 48 volts DC and is applied only when the local control is in the REMOTE position.
. . . 3. Systems: Key Reqs Analysis system 1

63. SAT-250 b. For single intensity discharge-type lighting systems (Styles A, B, C, and D), ON/OFF control is provided via 3 terminals (120 volts AC or plus 48 volts DC, ON, and Neutral).
. . . 3. Systems: Key Reqs Analysis systems 1

64. SAT-251 c. For three intensity discharge-type lighting systems (Styles E and F), five terminals must be provided for control, as follows:
. . . 3. Systems: Key Reqs Analysis systems 1

65. SAT-259 b. For single-step style systems, the remote switch will close a circuit between the 120-volt or plus 48 volt DC source and an "on" terminal; the system will turn on when this terminal receives the 120-volt AC or plus 48 volt DC potential.
. . . 3. Systems: Key Reqs Analysis systems 2

66. SAT-260 c. For multiple-step systems, the 120-volt AC or plus 48 volts DC potential (terminal (4)) is provided only when the local control switch is in the "remote" position.
. . . 3. Systems: Key Reqs Analysis systems 1

67. SAT-261 d. The remote switching network will return the 120-volt AC or plus 48 volts DC potential to terminal (1), (2), or (3), and the system will turn on to the selected intensity.
. . . 3. Systems: Key Reqs Analysis system 1

68. SAT-262 e. If more than one intensity terminal is energized, the system shall operate at the highest intensity selected.
. . . 3. Systems: Key Reqs Analysis system 1

69. SAT-264 The circuit design and construction must be in accordance with highest standards, with emphasis on reliability and long life. The brightness control circuit must be designed such that it will revert to the lowest brightness setting in the event of failure.
. . . 14. RMA: Key Reqs Analysis reliability 1

70. SAT-265 3.5.6 Electrical Protection.
. . . 7. Hardware: Key Reqs Analysis Electrical 1

71. SAT-266 The system must be protected against electrical transients found in the airport environment as described below.
. . . 3. Systems: Key Reqs Analysis system 1
. . . 7. Hardware: Key Reqs Analysis electrical 1
. . . 8. Environmental: Key Reqs Analysis environment 1

72. SAT-268 To protect against input power line surges, the system must withstand without operational interruption or damage a 50-millisecond pulse with a peak value of 500 volts superimposed on the input power lines.
. . . 3. Systems: Key Reqs Analysis system 1
. . . 8. Environmental: Key Reqs Analysis power 2

73. SAT-270 When installed in an operational environment per the manufacturer's instructions, the system must withstand repeated applications of a 5,000 volt potential between the equipment case (electrical ground) and any control or power conductor for 10 milliseconds.
. . . 3. Systems: Key Reqs Analysis system 1
. . . 7. Hardware: Key Reqs Analysis electrical 1
. . . 8. Environmental: Key Reqs Analysis environment 2

74. SAT-274 3.5.6.4 Radiated and Conducted Emissions.
. . . 15. EMI: Key Reqs Analysis Emi 1

75. SAT-275 a. The discharge light system must cause minimal conducted emissions (power lines/interface cables) and radiated RF emissions that may cause harmful interference to FAA or other airport equipment located on or near the airport (see paragraph 4.2.7 for measurements).
. . . 3. Systems: Key Reqs Analysis system 1
. . . 8. Environmental: Key Reqs Analysis power 1
. . . 15. EMI: Key Reqs Analysis emi 2

76. SAT-277 c. A discharge lighting system must employ sound engineering practices to minimize the risk of harmful interference. Since the equipment is operated in an environment where radiated RF and conducted emissions are a concern, both the conducted and radiated limits must be tested.
. . . 3. Systems: Key Reqs Analysis system 1
. . . 8. Environmental: Key Reqs Analysis environment 1
. . . 15. EMI: Key Reqs Analysis emi 1

77. SAT-278 3.5.6.5 Electromagnetic Interference (EMI).
. . . 15. EMI: Key Reqs Analysis EMI 1

78. SAT-279 EMI sensitive components, such as timers or controllers, must be adequately shielded or otherwise protected.
. . . 15. EMI: Key Reqs Analysis EMI 1

79. SAT-281 a. Interlock switches must be used in the control unit and power supplies so that opening the enclosure will:
. . . 8. Environmental: Key Reqs Analysis power 1
. . . 9. Mechanical: Key Reqs Analysis enclosure 1

80. SAT-282 (1) Disconnect the input power.
. . . 8. Environmental: Key Reqs Analysis power 1

81. SAT-283 (2) Safely discharge all voltages over 150 volts to 50 volts within 30 seconds. This discharge must occur, even if components that normally draw current from the high voltage power supply are removed.
. . . 5. Safety: Key Reqs Analysis Safe 1
. . . 8. Environmental: Key Reqs Analysis power 1

82. SAT-284 (3) Means must be provided to defeat the interlock with the door open for maintenance purposes.
. . . 12. Maintenance: Key Reqs Analysis maintenance 1

83. SAT-285 b. The system design must include bleeder resistors to discharge the high voltage (>150V) power supply to 50 volts within 5 minutes after input power is disconnected. This feature must serve as a back-up to the interlock activated bleeder circuit.
. . . 3. Systems: Key Reqs Analysis system 1
. . . 8. Environmental: Key Reqs Analysis power 2

84. SAT-286 c. If an interlock is not provided on an optical assembly, a warning label must be attached advising the maintainer not to open the optical assembly until the system power has been disconnected and the high voltage power supply is safely discharged.
. . . 3. Systems: Key Reqs Analysis system 1
. . . 5. Safety: Key Reqs Analysis safe 1
. . . 8. Environmental: Key Reqs Analysis power 2

85. SAT-288 a. All materials and parts used in the discharge lighting system must be suitable for the intended purpose and adequately protected against corrosion.
. . . 3. Systems: Key Reqs Analysis system 1

86. SAT-289 b. All assembly hardware, including screws, bolts, nuts, washers, and latches must be 18-8 stainless steel.
. . . 7. Hardware: Key Reqs Analysis hardware 1

87. SAT-295 a. Gasket material used must withstand temperatures from -40 to +131 degrees F (-40 to +55 degrees C).
. . . 8. Environmental: Key Reqs Analysis temperature 1

88. SAT-304 d. Nonferrous enclosures will not require painting if the exterior material color matches aviation orange; otherwise the exterior surfaces must receive the 3 coats of paint.
. . . 9. Mechanical: Key Reqs Analysis enclosure 1

89. SAT-308 b. Each electrical component or part thereof must be identified by a reference designation marked adjacent to the physical location of the part of the equipment and readily visible to maintenance personnel.
. . . 7. Hardware: Key Reqs Analysis electrical 1
. . . 12. Maintenance: Key Reqs Analysis maintenance 1

90. SAT-312 3.9 System Nameplates.
. . . 3. Systems: Key Reqs Analysis System 1

91. SAT-313 Identification data must be permanently affixed to each equipment unit (optical head, power supply, control unit, etc.) and must contain at least the following information:
. . . 6. Software: Key Reqs Analysis data 1
. . . 8. Environmental: Key Reqs Analysis power 1

92. SAT-314 a. Name of unit (optical head, power supply, etc.).
. . . 8. Environmental: Key Reqs Analysis power 1

93. SAT-319 An instruction manual must be supplied as part of each system and must contain the following information:
. . . 3. Systems: Key Reqs Analysis system 1

94. SAT-320 a. Safety precautions used while maintaining the equipment.
. . . 5. Safety: Key Reqs Analysis Safety 1

95. SAT-321 b. Theory of circuit and system operation.
. . . 3. Systems: Key Reqs Analysis system 1

96. SAT-324 e. Recommended preventive maintenance.
. . . 12. Maintenance: Key Reqs Analysis maintenance 1

97. SAT-334 The environmental tests specified in the following paragraphs must be conducted on a system (a control unit and at least one optical assembly). Operational tests required during or after environmental tests per the particular test methods must consist of a least one operational cycle per paragraph 4.2.14 with all test components connected together.
. . . 3. Systems: Key Reqs Analysis system 1
. . . 8. Environmental: Key Reqs Analysis environment 2

98. SAT-335 Where tests are conducted on an abbreviated system (a system without a complete complement of optical assemblies), the load imposed by the missing components and their interconnecting cables must be simulated by equivalent circuits.
. . . 3. Systems: Key Reqs Analysis system 2

99. SAT-336 A photometric test as described in this section must be performed before conducting any environmental tests. The same units must be used throughout the tests.
. . . 8. Environmental: Key Reqs Analysis environment 1

100. SAT-340 b. The maximum chamber ambient air temperature must be 131 degrees F (55 degrees C).
. . . 8. Environmental: Key Reqs Analysis temperature 1

101. SAT-341 c. Allow the equipment to temperature stabilize.
. . . 8. Environmental: Key Reqs Analysis temperature 1

102. SAT-342 d. Perform an operational test of the equipment after one hour of altitude and high temperature soak. Failure of the equipment to operate properly will be cause for rejection.
. . . 8. Environmental: Key Reqs Analysis temperature 1

103. SAT-344 4.2.2 Thermal Shock Test
. . . 8. Environmental: Key Reqs Analysis Shock 1

104. SAT-345 The equipment must be installed as in normal use and operated at maximum intensity until the temperatures have stabilized. At a temperature between 32-41 degrees F (0-5 degrees C), water must be applied in droplets, having a diameter range between 0.5 and 4.5 millimeters, to the light face. There must be no cracking of glass, metal, or plastic as a result of this test.
. . . 8. Environmental: Key Reqs Analysis temperature 2

105. SAT-346 4.2.3 Humidity.
. . . 8. Environmental: Key Reqs Analysis Humidity 1

106. SAT-347 The equipment must be tested for humidity tolerance per MIL-STD-810F (1 January 2000), Method 507.4, Humidity.
. . . 8. Environmental: Key Reqs Analysis humidity 2

107. SAT-348 a. The chamber maximum temperature must be 131 degrees F (55 degrees C) maximum for this test.
. . . 8. Environmental: Key Reqs Analysis temperature 1

108. SAT-349 b. Subject the equipment to five cycles (48 hours per cycle) at 95% relative humidity at a maximum temperature per paragraph 4.2.1.4a. See MIL-STD-810F (1 January 2000), Figure 507.4-1 for a graph of humidity cycles. Perform an equipment operational test at hour 24 of the test cycle.
. . . 8. Environmental: Key Reqs Analysis humidity 3

109. SAT-356 (3) The EUT must be at ambient temperature for this test.
. . . 8. Environmental: Key Reqs Analysis temperature 1

110. SAT-358 CAUTION: Perform a preliminary inspection before energizing the equipment to remove any accumulated water and prevent a potential shock hazard to test personnel.
. . . 8. Environmental: Key Reqs Analysis shock 1

111. SAT-363 An optical head mounted to a power supply enclosure and one mounted to a 2-inch EMT conduit must be subjected to a 150-knot wind applied perpendicular to the optical head face. Distress or damage to any part of the assembly must be cause for rejection.
. . . 8. Environmental: Key Reqs Analysis power 1
. . . 9. Mechanical: Key Reqs Analysis enclosure 1

112. SAT-364 4.2.6 Salt Fog Test.
. . . 8. Environmental: Key Reqs Analysis Salt Fog 1

113. SAT-365 a. A salt fog test must be conducted to determine the discharge lighting equipment resistance to a salt laden atmosphere. Tests must be conducted per MIL-STD-810F (1 January 2000), Method 509.4, Salt Fog, Paragraph 4.5.2, Procedure I.
. . . 8. Environmental: Key Reqs Analysis salt fog 2

114. SAT-366 b. At the conclusion of salt fog testing, inspect the EUT for evidence of corrosion, flaking paint/powder coating, gasket failure, and in enclosed volumes for water damage where condensation may have occurred. Any evidence of the preceding will be cause for rejection.
. . . 8. Environmental: Key Reqs Analysis salt fog 1

115. SAT-368 CAUTION: Energize the EUT only after it has been determined there will be no shock hazard.
. . . 8. Environmental: Key Reqs Analysis shock 1

116. SAT-370 4.2.7 Radiated and Conducted Emissions Tests.
. . . 15. EMI: Key Reqs Analysis Emi 1

117. SAT-372 b. The equipment tested must not exceed the conducted power line emissions per 47 CFR § 15.107b:
. . . 8. Environmental: Key Reqs Analysis power 1
. . . 15. EMI: Key Reqs Analysis emi 1

118. SAT-373 Table 5. Conducted Emission Limits
. . . 15. EMI: Key Reqs Analysis Emi 1

119. SAT-374 Frequency of Emission
. . . 15. EMI: Key Reqs Analysis Emi 1

120. SAT-376 Quasi-peak Emissions
. . . 15. EMI: Key Reqs Analysis Emi 1

121. SAT-379 Average Emissions dB/µV
. . . 15. EMI: Key Reqs Analysis Emi 1

122. SAT-387 c. The equipment tested must not exceed the radiated emission limits per 47 CFR § 15.109b for the following limits at 33 feet (10 meters):
. . . 15. EMI: Key Reqs Analysis emi 1

123. SAT-388 Table 6. Radiated Emission Limits
. . . 15. EMI: Key Reqs Analysis Emi 1

124. SAT-389 Frequency of Emission
. . . 15. EMI: Key Reqs Analysis Emi 1

125. SAT-411 e. For plastic/thermoplastic optical lenses or covers, the photometric performance must be measured after this test.
. . . 2. Performance: Key Reqs Analysis performance 1

126. SAT-417 a. A dielectric test must be made on power and control wiring of the system.
. . . 3. Systems: Key Reqs Analysis system 1
. . . 8. Environmental: Key Reqs Analysis power 1

127. SAT-418 b. The test must be made by applying both positive and negative 5kV pulses, 10 milliseconds minimum, between input power and control wires and ground (equipment case).
. . . 8. Environmental: Key Reqs Analysis power 1

128. SAT-420 d. The equipment must be capable of normal operation after this test.
. . . 1. Functional: Key Reqs Analysis capable 1

129. SAT-427 a. Subject the equipment power line and control line inputs to 3 pulses at 15 second intervals to a standard 1.2/50 microsecond - 8/20 microsecond combination wave of 4,000 volts at 3,000 amps.
. . . 8. Environmental: Key Reqs Analysis power 1

130. SAT-430 d. See also IEEE C62.45, IEEE Recommended Practice on Surge Testing for Equipment Connected to Low-Voltage (1000 V and less) AC Power Circuits for guidance about equipment test methods.
. . . 8. Environmental: Key Reqs Analysis Power 1

131. SAT-432 a. All components that will be part of a particular system must be connected together when undergoing operational tests.
. . . 3. Systems: Key Reqs Analysis system 1

132. SAT-435 d. All operating requirements of the equipment must be checked over the full range of input voltage variations at the control unit power input terminal.
. . . 8. Environmental: Key Reqs Analysis power 1

133. SAT-438 An 80-hour continuous operation test must be performed on the system. All intensities must be checked using the remote control to cycle the system as described below, with a 10 percent tolerance on the time intervals specified.
. . . 3. Systems: Key Reqs Analysis system 2

134. SAT-483 All measuring and test equipment used in the production of discharge lighting equipment classified under paragraph 1.2 must have their accuracy and precision maintained by a calibration program with traceability to ISO-10012 Measurement Management Systems - Requirements for Measurement Processes or current industry accreditation criteria. The manufacturer must show that all production photometric testing equipment correlates to the certifying laboratory's equipment to within plus or minus 5 percent. Photometric testing must be performed in a properly designed photometric range using a calibrated photometer. All photometric measurements must be based on a minimum five flash average.
. . . 3. Systems: Key Reqs Analysis Systems 1

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Key Reqs Analysis: Key reqs should be methodically sought by asking each stakeholer what they feel are their key reqs. These reqs are cost and or schedule drivers. They can be found by asking:

1. have we done this before
2. has someone else done this before
3. is a new technology, process, or method needed
4. is a new product needed...

This service looks for and counts all word or phrase instances set in the access field. Selecting a word from the list and submitting the report will provide the related text. Since the user defines these words there is no reason to enable noise word filters. This is a very high level service that relies on human ability to recognize their key req from a single word or phrase.

Number Sort

34power 27system 16enclosure 10System 9temperature 9systems
8Emi 7environment 6emi 4Power 4Function 4hardware
4maintenance 3Electrical 3electrical 3capable 2Humidity 2safe
2salt fog 2humidity 2Temperature 2Safe 2EMI 2Systems
2shock 2Shock 1Environment 1function 1Salt Fog 1Safety
1performance 1reliability 1capability 1mechanical 1safety 1data

Alpha Sort

2EMI 8Emi 10System 2Systems 6emi 16enclosure
1mechanical 27system 9systems 1Environment 2Humidity 4Power
1Salt Fog 2Shock 2Temperature 7environment 2humidity 1performance
34power 1reliability 2salt fog 2shock 9temperature 2Safe
1Safety 2safe 1safety 1data 4maintenance 3Electrical
4Function 1capability 3capable 3electrical 1function 4hardware

Accessed Patterns Not Found

response time architecture distributed central hybrid flexible
growth flexibility fail\s*safe fail\s*over recovery? software
vibration facility faclities room training train
maintainability support logistics ils maintainability availability
EMC TEMPEST UL Ergonomics HMI MMI
Machine Interface ATCRBS Beacon Primary Secondary Mode-S
track velocity vector history mosaic flight plan fix
posting conflict alert MSAW minimum safe altitude warning flight plan probe clearance delivery
security secure log\s*on log\s*off log\sin log\s*out
restricted area track pairing ADIZ plot maps? range scale
off\s*set


Metrics

Key Reqs Analysis: Key reqs should be methodically sought by asking each stakeholer what they feel are their key reqs. These reqs are cost and or schedule drivers. They can be found by asking:

1. have we done this before
2. has someone else done this before
3. is a new technology, process, or method needed
4. is a new product needed...

This service looks for and counts all word or phrase instances set in the access field. Selecting a word from the list and submitting the report will provide the related text. Since the user defines these words there is no reason to enable noise word filters. This is a very high level service that relies on human ability to recognize their key req from a single word or phrase.

Lines: 422
Imperatives: 7
Shalls: 7
Wills: 15
IsReq:

Item Count Children % lines % imperative % shall % will % isreq
1. Functional kra

9

2.13

60

12. Maintenance kra

4

0.94

57.14

57.14

26.66

14. RMA kra

1

0.23

14.28

14.28

6.66

15. EMI kra

16

3.79

2. Performance kra

1

0.23

14.28

14.28

6.66

3. Systems kra

48

11.37

5. Safety kra

4

0.94

57.14

57.14

26.66

6. Software kra

1

0.23

14.28

14.28

6.66

7. Hardware kra

10

2.36

66.66

8. Environmental kra

65

15.4

9. Mechanical kra

17

4.02

z Mined Objects

134

31.75

Reading Level

Disabling the noise filter may reduce the reading level. Re-run the report to capture metrics for both instances.

Accessed Unique Words:
Accessed Unique Syllables:
Words with 3+ Syllables:
Polysyllabic Count: 0
Reading Level: Select any rule option: Count Accessed Words or select: Generic Capabilites Analysis service.

Document Shape

The number of children at a particular level translate to a document shape. There are diffrent document shapes and each have implications. The document shapes are: random, rectangle, pyramid, inverted pyramid, trapazoid and diamond.

There are no child counts. Try disabling all services except for: Generic Structure Analysis.

original processing URL http://localhost:4444/~sat/satpro.cgi