Attachment #6-PAR 56 300W First Article Test Plan- Procedure Form 10-24-2017_FINAL.docx

October 24, 2017

First Article Test Plan/Procedure Form

For FAA 20A 300W Par 56

Q20A/PAR-56/C INCANDESCENT LAMP

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, paragraph 4.5 Appendix B of Par-56, 300 watt, Incandescent Lamps Statement of Work.

4.0 Wattage rating test. (Reference 4.5.1 in FAA-E-2408B Dated July 31, 2000) Test set up and procedure:

5.0 Filament Motion and Shorting Test (Reference 4.5.2 in FAA-E-2408B Dated July 31, 2000)

6.0 Life Test. (Reference 4.5.3 in FAA-E-2408B Dated July 31, 2000)

7.0 Photometric Testing (Reference 4.5.4 in FAA-E-2408B Dated July 31, 2000)

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

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 horizontal - 14 left

7,000 horizontal - 14 right

7,000

Maximum Intensity, 48,000

Candela (not to be exceeded in any direction)

Prismatic Prismatic

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.)

13.5R 14R

5U

4U

3.5U

2.5U

1U

1D

2.5D

3.5D

4D

5D

Table 2 for Photometric Test Data for S/N:

8.0 Light Maintenance (Reference 4.5.5 in FAA-E-2408B Dated July 31, 2000)

10. 0 Thermal shock test

11. 0 Cold Water Test (Reference 4.5.6.1 in FAA-E-2408B Dated July 31, 2000): Can be performed in the last test

12.0 Icing Test (Reference 4.5.6.2 in FAA-E-2408B Dated July 31, 2000) Can be performed after cold water test

13.0 High Temperature Test (Reference 4.5.7.1 in FAA-E-2408B Dated July 31, 2000)

14.0 Low Temperature Test (Reference 4.5.7.2 in FAA-E-2408B Dated July 31, 2000)

15.0 Vibration Test (Reference 4.5.8 in FAA-E-2408B Dated July 31, 2000)

16.0 Humidity Test (Reference 4.5.9 in FAA-E-2408B Dated July 31, 2000)

17.0 Low Pressure (Altitude) Test (Reference 4.5.10 in FAA-E-2408B Dated July 31, 2000)

18.0 Salt Fog Test (Reference 4.5.11 in FAA-E-2408B Dated July 31, 2000)

19.0 Rain Test (Reference 4.5.12 in FAA-E-2408B Dated July 31, 2000)

20.0 Two Hour Test (Reference 4.5.13 in FAA-E-2408B Dated July 31, 2000)

21.0 Solar Radiation Test (Reference 4.5.14 in FAA-E-2408B Dated July 31, 2000)

The solar radiation (sunshine) test shall be performed IAW Procedure II, method 505.4, of MIL-STD-810F. An irradiance of 1120 watts per square meter shall be applied to the lamp coating for 630 days. At the end of the test the lamp coating transmittance shall be 95% of the initial transmittance, and the lamp at rated life shall meet the 80% light maintenance requirement. (9.0)

Figure 1 Lamp PAR-56 Bulb, Mogul End Prong.

Figure1 Lamp Design Parameters (Mogul End Prong) Type

9.0 Wattage rating test (paragraph 4.5.1)

Test set up and procedure: (prepare by contractor)

10.0 Filament Motion and Shorting Test (paragraph 4.5.2)

11.0 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

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 horizontal - 14 left

7,000 horizontal - 14 right

7,000

Maximum Intensity, 48,000

Candela (not to be exceeded in any direction)

Prismatic Prismatic

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.)

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:

12.0 Two Hour Test (paragraph 4.5.13)

13.0 Light up (100% production built samples)

14.0

15.0 Test set up and procedure: (prepare by contractor)

16.0

17.0 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.

Prepared for: FAA Logistics Center

Name of Company:

Address:

Phone number:

Prepared By:

Title:

Date: ______________

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