Attachment#8-PAR 56 300W Production Unit Test Plan- Procedure Form 10-24-2017_FINAL.docx
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- 6973GH-18-R-00028
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Attachment#8-PAR 56 300W Production Unit Test Plan- Procedure Form 10-24-2017_FINAL (docx)
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October 24, 2017
Production Unit Test Plan/ Procedure Form.
For FAA 20A 300W Par 56
Q20A/PAR-56/C INCANDESCENT LAMP
| TYPE I, MOGUL END PRONG, 300W |
| NSN: 6240-01-432-3996 |
1.0 Scope
1.1 The specifications covers halogen-cycle PAR-56 aviation service lamps or equivalent used for runway approach lighting systems.
1.2 Reference FAA-E-2408b Dated July 31, 2000.
1.3 This procedure will outline any and all test requirements for production build units.
1.4 A test sample rate of 5pcs or 1% whichever is greater shall be tested per production batch.
2.0 Test Equipment List with calibration date (as need).
List all of the equipment
3.0 Test methods
Testing of the UUT shall be performed IAW FAA-E-2408b Dated July 31, 2000, Appendix B of Par-56, 300 watt, Incandescent Lamp Statement of Work.
4.0 Wattage rating test (paragraph 4.5.1)
Test set up and procedure: (prepare by contractor)
5.0 Filament Motion and Shorting Test (paragraph 4.5.2)
6.0 Photometric Testing (paragraph 4.5.4)
Photometric tests shall be conducted to demonstrate compliance with the intensity and beam dimension requirements of Table I, as applicable. Table 2 is used to fill the photometric required in table 1.
Table I. Lamp Design Parameters (Mogul End Prong, Type I)
Q20A/PAR56/C
Wattage Rating
| 200 |
| ±16 |
| 300 |
| +18 |
| 500 ±30 |
| Rated Amperes |
| (RMS) |
| 6.6 |
| ±0.5% |
| 20 |
| ±0.5% |
| 20 ±0 . 5% |
| Average Life, |
| Hours |
| 1000 |
| 300 |
| +18 |
| Rated Amperes | |
| (RMS) |
| 20 |
| ±0.5% |
| Average Life, | |
| Hours |
Minimum Candela Requirements Within Beam Field Point Location (degrees from mechanical axis)
3.5 up - 13.5 left
7,000
3.5 down - 13.5 left
7,000
3.5 up - 13.5 right
7,000
3.5 down - 13.5 right
7,000
4 up - vertical
16,000
4 down - vertical horizontal - 10 left horizontal - 10 right
16,000 16,000 16,000 horizontal - 14 left
7,000 horizontal - 14 right
7,000
Maximum Intensity, 48,000
Candela (not to be exceeded in any direction)
| Cover Glass |
| Prismatic |
Prismatic Prismatic
| Base |
| All three |
| (3) |
| lamps - Mogul End Prong |
| Burning Position |
| All three |
| (3) |
| lamps - Horizontal to 25° |
Base Down
Sample No: Flash Period: On time-one flash:
Brightness Step:
Style: Input:
Neutral Density Filter: Calibration Factor:
Serial #
NA I
Vertical Position (deg.)
Calculated Effective Intensity Data (candela)
Horizontal Position (deg.)
| 15L |
| 14L |
| 13.5 L |
| 10L |
| 11L |
| 7.5L |
| 5L |
| 0 |
| 5R |
| 7.5R |
| 10R |
| 12R |
13.5 R
14R
5U
4U
3.5U
2.5U
1U
1D
2.5D
3.5D
4D
5D
Table 2: Photometric Test Data for S/N:
7.0 Two Hour Test (paragraph 4.5.13)
8.0 Examination Of Product (paragraph 4.4.1)
9.1 The lamp shall be inspected to determine compliance with the requirements specified herein with respect to materials, workmanship and marking. The lamp shall be inspected to determine that outline dimensions meet the dimensions given in Figure 1 as applicable. Lamp prongs shall be flat any curvature in design shall be cause for rejection. Record Inspection results on data sheet.
List of test
5.0 Filament Motion Test and Shorting of Turn Test
6.0 Photometric Test
7.0 Two Hour Test
8.0 Examination of Product
Prepared for: FAA Logistics Center
Name of Company:
Address:
Phone number:
Prepared By:
Title:
Date: ______________
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