OP4-B12 OPLITE Series Interior Aircraft Lights User Guide
- June 13, 2024
- Oplite
Table of Contents
OP4-B12 OPLITE Series Interior Aircraft Lights
Product Information
The OPLITE Series Interior Aircraft Lights are non-required safety enhancing
equipment (NORSEE) designed and manufactured by Machine Incorporated dba
OPLITE. These lights are available in various models and colors, including
blue, green, red, and white.
They are suitable for installation on aircraft certified under 14 CFR Part 23
or precursor regulations.
The OPLITE Series 4 & 6 and Gooseneck 4 & 6 meet the design and performance requirements of FAA Policy PS-AIR-21.8-1602 for NORSEE. The manufacturing of the equipment is authorized based on the acceptance of the certification statement provided by Machine Incorporated dba OPLITE.
The authorized part numbers for the OPLITE Series Interior Aircraft Lights are as follows:
| Model | Part Number | Function |
|---|---|---|
| SINGLE COLOR OP4-B12 | 4 LED OPLITE BLUE 12V | Interior Aircraft Light |
| SINGLE COLOR OP4-G12 | 4 LED OPLITE GREEN 12V | Interior Aircraft Light |
| SINGLE COLOR OP4-R12 | 4 LED OPLITE RED 12V | Interior Aircraft Light |
| SINGLE COLOR OP4-W12 | 4 LED OPLITE WHITE 12V | Interior Aircraft Light |
| SINGLE COLOR OP4-B24 | 4 LED OPLITE BLUE 24V | Interior Aircraft Light |
| SINGLE COLOR OP4-G24 | 4 LED OPLITE GREEN 24V | Interior Aircraft Light |
| SINGLE COLOR OP4-R24 | 4 LED OPLITE RED 24V | Interior Aircraft Light |
The installation eligibility of the OPLITE Series Interior Aircraft Lights is subject to the requirements of 14 CFR Part 1.1 and 14 CFR Part 43 Appendix A. The installation must not detrimentally obstruct the pilot’s view of required instrumentation. Please refer to FAA memorandum number PS-AIR-21.8-1602 for detailed guidelines on installation eligibility.
Product Usage Instructions
To install the OPLITE Series Interior Aircraft Lights, follow the steps below:
- Ensure that the aircraft is certified under 14 CFR Part 23 or precursor regulations.
- Verify compliance with the requirements of 14 CFR Part 1.1 and 14 CFR Part 43 Appendix A.
- Select the appropriate OPLITE model and color based on your requirements.
- Refer to the Installation Manual OPLITE 4 and 6 series LED light Installation Instructions, Document Number MIW-II4/6 Revision A for detailed installation steps.
- During installation, make sure that the lights are positioned in a way that does not obstruct the pilot’s view of required instrumentation.
Aircraft Certification Service Compliance & Airworthiness Division
June 29, 2022
Richard Mileika
President
Machine Incorporated dba OPLITE
879 Turnpike Street
Stoughton, MA 02072
Dear Mr. Mileika:
This is in response to your letter dated June 16, 2022 requesting Non Required
Safety Enhancing System (NORSEE) approval of your OPLITE Series Interior
Aircraft Lights. This is based on the data presented in Prodcut Design
Standard OPLITE Series 4 & 6 and Gooseneck 4 & 6, Document Number MID-4/6,
Revision A and Installation Manual OPLITE 4 and 6 series LED light
Installation Instructions, Document Number MIW-II4/6 Revision A.
We acknowledge your statement certifying your OPLITE Series 4 & 6 and
Gooseneck 4 & 6meets the design and performance requirements of FAA Policy PS-
AIR-21.8-1602 for Non Required Safety Enhancing Equipment (NORSEE). Based on
our acceptance of your statement and 14 CFR 21.8(d), we authorize the
manufacturing of your equipment as detailed by the part numbers shown in the
following table:
Model| Part Number| Authorized Function|
Approved Replacement for| FAA Approval Basis and Approved
Design Data| Installation Eligibility:
---|---|---|---|---|---
SINGLE COLOR 4 LED OPLITE BLUE 12V| OP4-B12| Interior Aircraft Light|
Alteration Part| FAA memorandum number PS-AIR-21.8- 1602
Drawing: 4501-00 Rev.: A
Date: 03-12-21 or later FAA-approved revisions
| Provided the requirements of 14 CFR Part 1.1 and 14 CFR Part 43 Appendix A
are met and the installation does not detrimentally obstruct the pilots view
of required instrumentation, equipment may be installed as a minor alteration
on an Aircraft Certified under 14 CFR Part 23 or precursor regulations, as
outlined in FAA memorandum number PS-AIR-21.8-1602.
SINGLE COLOR
4 LED OPLITE GREEN 12V
| OP4-G12| Interior Aircraft Light| Alteration Part| FAA memorandum number PS- AIR-21.8- 1602
Drawing: 4501-00 Rev.: A
Date: 03-12-21 or later FAA-approved revisions
| Provided the requirements of 14 CFR Part 1.1 and 14 CFR Part 43 Appendix A
are met and the installation does not detrimentally obstruct the pilots view
of required instrumentation, equipment may be installed as a minor alteration
on an Aircraft Certified under 14 CFR Part 23 or precursor regulations, as
outlined in FAA memorandum number PS-AIR-21.8-1602.
Model| Part Number| Authorized Function|
Approved Replacement for| FAA Approval Basis and Approved
Design Data| Installation Eligibility:
---|---|---|---|---|---
SINGLE COLOR
4 LED OPLITE RED 12V
| OP4-R12| Interior Aircraft Light| Alteration Part| FAA memorandum number PS- AIR-21.8- 1602
Drawing: 4501-00 Rev.: A
Date: 03-12-21 or later FAA-approved revisions
| Provided the requirements of 14 CFR Part 1.1 and 14 CFR Part 43 Appendix A
are met and the installation does not detrimentally obstruct the pilots view
of required instrumentation, equipment may be installed as a minor alteration
on an Aircraft Certified under 14 CFR Part 23 or precursor regulations, as
outlined in FAA memorandum number PS-AIR-21.8-1602.
SINGLE COLOR
4 LED OPLITE WHITE 12V
| OP4-W12| Interior Aircraft Light| Alteration Part| FAA memorandum number PS- AIR-21.8- 1602
Drawing: 4501-00 Rev.: A
Date: 03-12-21 or later FAA-approved revisions
| Provided the requirements of 14 CFR Part 1.1 and 14 CFR Part 43 Appendix A
are met and the installation does not detrimentally obstruct the pilots view
of required instrumentation, equipment may be installed as a minor alteration
on an Aircraft Certified under 14 CFR Part 23 or precursor regulations, as
outlined in FAA memorandum number PS-AIR-21.8-1602.
SINGLE COLOR
4 LED OPLITE BLUE 24V
| OP4-B24| Interior Aircraft Light| Alteration Part| FAA memorandum number PS- AIR-21.8- 1602
Drawing: 4501-00 Rev.: A
Date: 03-12-21 or later FAA-approved revisions
| Provided the requirements of 14 CFR Part 1.1 and 14 CFR Part 43 Appendix A
are met and the installation does not detrimentally obstruct the pilots view
of required instrumentation, equipment may be installed as a minor alteration
on an Aircraft Certified under 14 CFR Part 23 or precursor regulations, as
outlined in FAA memorandum number PS-AIR-21.8-1602.
SINGLE COLOR
4 LED OPLITE GREEN 24V
| OP4-G24| Interior Aircraft Light| Alteration Part| FAA memorandum number PS- AIR-21.8- 1602
Drawing: 4501-00 Rev.: A
Date: 03-12-21 or later FAA-approved revisions
| Provided the requirements of 14 CFR Part 1.1 and 14 CFR Part 43 Appendix A
are met and the installation does not detrimentally obstruct the pilots view
of required instrumentation, equipment may be installed as a minor alteration
on an Aircraft Certified under 14 CFR Part 23 or precursor regulations, as
outlined in FAA memorandum number PS-AIR-21.8-1602.
SINGLE COLOR
4 LED OPLITE RED 24V
| OP4-R24| Interior Aircraft Light| Alteration Part| FAA memorandum number PS- AIR-21.8- 1602
Drawing: 4501-00 Rev.: A
Date: 03-12-21 or later FAA-approved revisions
| Provided the requirements of 14 CFR Part 1.1 and 14 CFR Part 43 Appendix A
are met and the installation does not detrimentally obstruct the pilots view
of required instrumentation, equipment may be installed as a minor alteration
on an Aircraft Certified under 14 CFR Part 23 or precursor regulations, as
outlined in FAA memorandum number PS-AIR-21.8-1602.
Model| Part Number| Authorized Function|
Approved Replacement for| FAA Approval Basis and Approved
Design Data| Installation Eligibility:
---|---|---|---|---|---
SINGLE COLOR
4 LED OPLITE WHITE 24V
| OP4-W24| Interior Aircraft Light| Alteration Part| FAA memorandum number PS- AIR-21.8- 1602
Drawing: 4501-00 Rev.: A
Date: 03-12-21 or later FAA-approved revisions
| Provided the requirements of 14 CFR Part 1.1 and 14 CFR Part 43 Appendix A
are met and the installation does not detrimentally obstruct the pilots view
of required instrumentation, equipment may be installed as a minor alteration
on an Aircraft Certified under 14 CFR Part 23 or precursor regulations, as
outlined in FAA memorandum number PS-AIR-21.8-1602.
SINGLE COLOR
6 LED OPLITE BLUE 12V
| OP6-B12| Interior Aircraft Light| Alteration Part| FAA memorandum number PS- AIR-21.8- 1602
Drawing: 6501-00 Rev.: A
Date: 03-12-21 or later FAA-approved revisions
| Provided the requirements of 14 CFR Part 1.1 and 14 CFR Part 43 Appendix A
are met and the installation does not detrimentally obstruct the pilots view
of required instrumentation, equipment may be installed as a minor alteration
on an Aircraft Certified under 14 CFR Part 23 or precursor regulations, as
outlined in FAA memorandum number PS-AIR-21.8-1602.
SINGLE COLOR
6 LED OPLITE GREEN 12V
| OP6-G12| Interior Aircraft Light| Alteration Part| FAA memorandum number PS- AIR-21.8- 1602
Drawing: 6501-00 Rev.: A
Date: 03-12-21 or later FAA-approved revisions
| Provided the requirements of 14 CFR Part 1.1 and 14 CFR Part 43 Appendix A
are met and the installation does not detrimentally obstruct the pilots view
of required instrumentation, equipment may be installed as a minor alteration
on an Aircraft Certified under 14 CFR Part 23 or precursor regulations, as
outlined in FAA memorandum number PS-AIR-21.8-1602.
SINGLE COLOR
6 LED OPLITE RED 12V
| OP6-R12| Interior Aircraft Light| Alteration Part| FAA memorandum number PS- AIR-21.8- 1602
Drawing: 6501-00 Rev.: A
Date: 03-12-21 or later FAA-approved revisions
| Provided the requirements of 14 CFR Part 1.1 and 14 CFR Part 43 Appendix A
are met and the installation does not detrimentally obstruct the pilots view
of required instrumentation, equipment may be installed as a minor alteration
on an Aircraft Certified under 14 CFR Part 23 or precursor regulations, as
outlined in FAA memorandum number PS-AIR-21.8-1602.
SINGLE COLOR
6 LED OPLITE WHITE 12V
| OP6-W12| Interior Aircraft Light| Alteration Part| FAA memorandum number PS- AIR-21.8- 1602
Drawing: 6501-00 Rev.: A
Date: 03-12-21 or later FAA-approved revisions
| Provided the requirements of 14 CFR Part 1.1 and 14 CFR Part 43 Appendix A
are met and the installation does not detrimentally obstruct the pilots view
of required instrumentation, equipment may be installed as a minor alteration
on an Aircraft Certified under 14 CFR Part 23 or precursor regulations, as
outlined in FAA memorandum number PS-AIR-21.8-1602.
Model| Part Number| Authorized Function|
Approved Replacement for| FAA Approval Basis and Approved
Design Data| Installation Eligibility:
---|---|---|---|---|---
SINGLE COLOR
6 LED OPLITE BLUE 24V
| OP6-B24| Interior Aircraft Light| Alteration Part| FAA memorandum number PS- AIR-21.8- 1602
Drawing: 6501-00 Rev.: A
Date: 03-12-21 or later FAA-approved revisions
| Provided the requirements of 14 CFR Part 1.1 and 14 CFR Part 43 Appendix A
are met and the installation does not detrimentally obstruct the pilots view
of required instrumentation, equipment may be installed as a minor alteration
on an Aircraft Certified under 14 CFR Part 23 or precursor regulations, as
outlined in FAA memorandum number PS-AIR-21.8-1602.
SINGLE COLOR
6 LED OPLITE GREEN 24V
| OP6-G24| Interior Aircraft Light| Alteration Part| FAA memorandum number PS- AIR-21.8- 1602
Drawing: 6501-00 Rev.: A
Date: 03-12-21 or later FAA-approved revisions
| Provided the requirements of 14 CFR Part 1.1 and 14 CFR Part 43 Appendix A
are met and the installation does not detrimentally obstruct the pilots view
of required instrumentation, equipment may be installed as a minor alteration
on an Aircraft Certified under 14 CFR Part 23 or precursor regulations, as
outlined in FAA memorandum number PS-AIR-21.8-1602.
SINGLE COLOR
6 LED OPLITE RED 24V
| OP6-R24| Interior Aircraft Light| Alteration Part| FAA memorandum number PS- AIR-21.8- 1602
Drawing: 6501-00 Rev.: A
Date: 03-12-21 or later FAA-approved revisions
| Provided the requirements of 14 CFR Part 1.1 and 14 CFR Part 43 Appendix A
are met and the installation does not detrimentally obstruct the pilots view
of required instrumentation, equipment may be installed as a minor alteration
on an Aircraft Certified under 14 CFR Part 23 or precursor regulations, as
outlined in FAA memorandum number PS-AIR-21.8-1602.
SINGLE COLOR
6 LED OPLITE WHITE 24V
| OP6-W24| Interior Aircraft Light| Alteration Part| FAA memorandum number PS- AIR-21.8- 1602
Drawing: 6501-00 Rev.: A
Date: 03-12-21 or later FAA-approved revisions
| Provided the requirements of 14 CFR Part 1.1 and 14 CFR Part 43 Appendix A
are met and the installation does not detrimentally obstruct the pilots view
of required instrumentation, equipment may be installed as a minor alteration
on an Aircraft Certified under 14 CFR Part 23 or precursor regulations, as
outlined in FAA memorandum number PS-AIR-21.8-1602.
DUAL COLOR 6 LED OPLITE WHITE/BLUE 12V| OP6- W/B12| Interior Aircraft
Light| Alteration Part| FAA memorandum number PS-AIR-21.8- 1602
Drawing: 6501-00 Rev.: A
Date: 03-12-21 or later FAA-approved revisions
| Provided the requirements of 14 CFR Part 1.1 and 14 CFR Part 43 Appendix A
are met and the installation does not detrimentally obstruct the pilots view
of required instrumentation, equipment may be installed as a minor alteration
on an Aircraft Certified under 14 CFR Part 23 or precursor regulations, as
outlined in FAA memorandum number PS-AIR-21.8-1602.
Model| Part Number| Authorized Function|
Approved Replacement for| FAA Approval Basis and Approved
Design Data| Installation Eligibility:
---|---|---|---|---|---
DUAL COLOR 6 LED OPLITE WHITE/GREEN 12V| OP6-W/G12| Interior Aircraft Light|
Alteration Part| FAA memorandum number PS-AIR-21.8- 1602
Drawing: 6501-00 Rev.: A
Date: 03-12-21 or later FAA-approved revisions
| Provided the requirements of 14 CFR Part 1.1 and 14 CFR Part 43 Appendix A
are met and the installation does not detrimentally obstruct the pilots view
of required instrumentation, equipment may be installed as a minor alteration
on an Aircraft Certified under 14 CFR Part 23 or precursor regulations, as
outlined in FAA memorandum number PS-AIR-21.8-1602.
DUAL COLOR 6 LED OPLITE WHITE/RED 12V| OP6-W/R12| Interior Aircraft Light|
Alteration Part| FAA memorandum number PS-AIR-21.8- 1602
Drawing: 6501-00 Rev.: A
Date: 03-12-21 or later FAA-approved revisions
| Provided the requirements of 14 CFR Part 1.1 and 14 CFR Part 43 Appendix A
are met and the installation does not detrimentally obstruct the pilots view
of required instrumentation, equipment may be installed as a minor alteration
on an Aircraft Certified under 14 CFR Part 23 or precursor regulations, as
outlined in FAA memorandum number PS-AIR-21.8-1602.
DUAL COLOR 6 LED OPLITE WHITE/BLUE 24V| OP6-W/B24| Interior Aircraft Light|
Alteration Part| FAA memorandum number PS-AIR-21.8- 1602
Drawing: 6501-00 Rev.: A
Date: 03-12-21 or later FAA-approved revisions
| Provided the requirements of 14 CFR Part 1.1 and 14 CFR Part 43 Appendix A
are met and the installation does not detrimentally obstruct the pilots view
of required instrumentation, equipment may be installed as a minor alteration
on an Aircraft Certified under 14 CFR Part 23 or precursor regulations, as
outlined in FAA memorandum number PS-AIR-21.8-1602.
DUAL COLOR 6 LED OPLITE WHITE/GREEN 24V| OP6-W/G24| Interior Aircraft Light|
Alteration Part| FAA memorandum number PS-AIR-21.8- 1602
Drawing: 6501-00 Rev.: A
Date: 03-12-21 or later FAA-approved revisions
| Provided the requirements of 14 CFR Part 1.1 and 14 CFR Part 43 Appendix A
are met and the installation does not detrimentally obstruct the pilots view
of required instrumentation, equipment may be installed as a minor alteration
on an Aircraft Certified under 14 CFR Part 23 or precursor regulations, as
outlined in FAA memorandum number PS-AIR-21.8-1602.
DUAL COLOR 6 LED OPLITE WHITE/RED 24V| OP6-W/R24| Interior Aircraft Light|
Alteration Part| FAA memorandum number PS-AIR-21.8- 1602
Drawing: 6501-00 Rev.: A
Date: 03-12-21 or later FAA-approved revisions
| Provided the requirements of 14 CFR Part 1.1 and 14 CFR Part 43 Appendix A
are met and the installation does not detrimentally obstruct the pilots view
of required instrumentation, equipment may be installed as a minor alteration
on an Aircraft Certified under 14 CFR Part 23 or precursor regulations, as
outlined in FAA memorandum number PS-AIR-21.8-1602.
Model| Part Number| Authorized Function|
Approved Replacement for| FAA Approval Basis and Approved
Design Data| Installation Eligibility:
---|---|---|---|---|---
SINGLE COLOR 4 LED GOOSENECK BLUE 12V| GN4-B12| Interior Aircraft Light|
Alteration Part| FAA memorandum number PS-AIR-21.8- 1602
Drawing: GN4 Rev.: –
Date: 04-04-16 or later FAA-approved revisions
| Provided the requirements of 14 CFR Part 1.1 and 14 CFR Part 43 Appendix A
are met and the installation does not detrimentally obstruct the pilots view
of required instrumentation, equipment may be installed as a minor alteration
on an Aircraft Certified under 14 CFR Part 23 or precursor regulations, as
outlined in FAA memorandum number PS-AIR-21.8-1602
SINGLE COLOR 4 LED GOOSENECK GREEN 12V| GN4-G12| Interior Aircraft Light|
Alteration Part| FAA memorandum number PS-AIR-21.8- 1602
Drawing: GN4 Rev.: –
Date: 04-04-16 or later FAA-approved revisions
| Provided the requirements of 14 CFR Part 1.1 and 14 CFR Part 43 Appendix A
are met and the installation does not detrimentally obstruct the pilots view
of required instrumentation, equipment may be installed as a minor alteration
on an Aircraft Certified under 14 CFR Part 23 or precursor regulations, as
outlined in FAA memorandum number PS-AIR-21.8-1602
SINGLE COLOR 4 LED GOOSENECK WHITE 12V| GN4-W12| Interior Aircraft Light|
Alteration Part| FAA memorandum number PS-AIR-21.8- 1602
Drawing: GN4 Rev.: –
Date: 04-04-16 or later FAA-approved revisions
| Provided the requirements of 14 CFR Part 1.1 and 14 CFR Part 43 Appendix A
are met and the installation does not detrimentally obstruct the pilots view
of required instrumentation, equipment may be installed as a minor alteration
on an Aircraft Certified under 14 CFR Part 23 or precursor regulations, as
outlined in FAA memorandum number PS-AIR-21.8-1602
SINGLE COLOR 4 LED GOOSENECK BLUE 24V| GN4-B24| Interior Aircraft Light|
Alteration Part| FAA memorandum number PS-AIR-21.8- 1602
Drawing: GN4 Rev.: –
Date: 04-04-16 or later FAA-approved revisions
| Provided the requirements of 14 CFR Part 1.1 and 14 CFR Part 43 Appendix A
are met and the installation does not detrimentally obstruct the pilots view
of required instrumentation, equipment may be installed as a minor alteration
on an Aircraft Certified under 14 CFR Part 23 or precursor regulations, as
outlined in FAA memorandum number PS-AIR-21.8-1602
SINGLE COLOR 4 LED GOOSENECK GREEN 24V| GN4-G24| Interior Aircraft Light|
Alteration Part| FAA memorandum number PS-AIR-21.8- 1602
Drawing: GN4 Rev.: –
Date: 04-04-16 or later FAA-approved revisions
| Provided the requirements of 14 CFR Part 1.1 and 14 CFR Part 43 Appendix A
are met and the installation does not detrimentally obstruct the pilots view
of required instrumentation, equipment may be installed as a minor alteration
on an Aircraft Certified under 14 CFR Part 23 or precursor regulations, as
outlined in FAA memorandum number PS-AIR-21.8-1602
Model| Part Number| Authorized Function|
Approved Replacement for| FAA Approval Basis and Approved
Design Data| Installation Eligibility:
---|---|---|---|---|---
SINGLE COLOR 4 LED GOOSENECK RED 24V| GN4-R24| Interior Aircraft Light|
Alteration Part| FAA memorandum number PS-AIR-21.8- 1602
Drawing: GN4 Rev.: –
Date: 04-04-16 or later FAA-approved revisions
| Provided the requirements of 14 CFR Part 1.1 and 14 CFR Part 43 Appendix A
are met and the installation does not detrimentally obstruct the pilots view
of required instrumentation, equipment may be installed as a minor alteration
on an Aircraft Certified under 14 CFR Part 23 or precursor regulations, as
outlined in FAA memorandum number PS-AIR-21.8-1602
SINGLE COLOR 4 LED GOOSENECK WHITE 24V| GN4-W24| Interior Aircraft Light|
Alteration Part| FAA memorandum number PS-AIR-21.8- 1602
Drawing: GN4 Rev.: –
Date: 04-04-16 or later FAA-approved revisions
| Provided the requirements of 14 CFR Part 1.1 and 14 CFR Part 43 Appendix A
are met and the installation does not detrimentally obstruct the pilots view
of required instrumentation, equipment may be installed as a minor alteration
on an Aircraft Certified under 14 CFR Part 23 or precursor regulations, as
outlined in FAA memorandum number PS-AIR-21.8-1602
SINGLE COLOR 6 LED GOOSENECK BLUE 12V| GN6-B12| Interior Aircraft Light|
Alteration Part| FAA memorandum number PS-AIR-21.8- 1602
Drawing: GN6 Rev.: –
Date: 04-20-16 or later FAA-approved revisions
| Provided the requirements of 14 CFR Part 1.1 and 14 CFR Part 43 Appendix A
are met and the installation does not detrimentally obstruct the pilots view
of required instrumentation, equipment may be installed as a minor alteration
on an Aircraft Certified under 14 CFR Part 23 or precursor regulations, as
outlined in FAA memorandum number PS-AIR-21.8-1602
SINGLE COLOR 6 LED GOOSENECK GREEN 12V| GN6-G12| Interior Aircraft Light|
Alteration Part| FAA memorandum number PS-AIR-21.8- 1602
Drawing: GN6 Rev.: –
Date: 04-20-16 or later FAA-approved revisions
| Provided the requirements of 14 CFR Part 1.1 and 14 CFR Part 43 Appendix A
are met and the installation does not detrimentally obstruct the pilots view
of required instrumentation, equipment may be installed as a minor alteration
on an Aircraft Certified under 14 CFR Part 23 or precursor regulations, as
outlined in FAA memorandum number PS-AIR-21.8-1602
SINGLE COLOR 6 LED GOOSENECK RED 12V| GN6-R12| Interior Aircraft Light|
Alteration Part| FAA memorandum number PS-AIR-21.8- 1602
Drawing: GN6 Rev.: –
Date: 04-20-16 or later FAA-approved revisions
| Provided the requirements of 14 CFR Part 1.1 and 14 CFR Part 43 Appendix A
are met and the installation does not detrimentally obstruct the pilots view
of required instrumentation, equipment may be installed as a minor alteration
on an Aircraft Certified under 14 CFR Part 23 or precursor regulations, as
outlined in FAA memorandum number PS-AIR-21.8-1602
Model| Part Number| Authorized Function|
Approved Replacement for| FAA Approval Basis and Approved
Design Data| Installation Eligibility:
---|---|---|---|---|---
SINGLE COLOR 6 LED GOOSENECK WHITE 12V| GN6-W12| Interior Aircraft Light|
Alteration Part| FAA memorandum number PS-AIR-21.8- 1602
Drawing: GN6 Rev.: –
Date: 04-20-16 or later FAA-approved revisions
| Provided the requirements of 14 CFR Part 1.1 and 14 CFR Part 43 Appendix A
are met and the installation does not detrimentally obstruct the pilots view
of required instrumentation, equipment may be installed as a minor alteration
on an Aircraft Certified under 14 CFR Part 23 or precursor regulations, as
outlined in FAA memorandum number PS-AIR-21.8-1602
SINGLE COLOR 6 LED GOOSENECK BLUE 24V| GN6-B24| Interior Aircraft Light|
Alteration Part| FAA memorandum number PS-AIR-21.8- 1602
Drawing: GN6 Rev.: –
Date: 04-20-16 or later FAA-approved revisions
| Provided the requirements of 14 CFR Part 1.1 and 14 CFR Part 43 Appendix A
are met and the installation does not detrimentally obstruct the pilots view
of required instrumentation, equipment may be installed as a minor alteration
on an Aircraft Certified under 14 CFR Part 23 or precursor regulations, as
outlined in FAA memorandum number PS-AIR-21.8-1602
SINGLE COLOR 6 LED GOOSENECK GREEN 24V| GN6-G24| Interior Aircraft Light|
Alteration Part| FAA memorandum number PS-AIR-21.8- 1602
Drawing: GN6 Rev.: –
Date: 04-20-16 or later FAA-approved revisions
| Provided the requirements of 14 CFR Part 1.1 and 14 CFR Part 43 Appendix A
are met and the installation does not detrimentally obstruct the pilots view
of required instrumentation, equipment may be installed as a minor alteration
on an Aircraft Certified under 14 CFR Part 23 or precursor regulations, as
outlined in FAA memorandum number PS-AIR-21.8-1602
SINGLE COLOR 6 LED GOOSENECK RED 24V| GN6-R24| Interior Aircraft Light|
Alteration Part| FAA memorandum number PS-AIR-21.8- 1602
Drawing: GN6 Rev.: –
Date: 04-20-16 or later FAA-approved revisions
| Provided the requirements of 14 CFR Part 1.1 and 14 CFR Part 43 Appendix A
are met and the installation does not detrimentally obstruct the pilots view
of required instrumentation, equipment may be installed as a minor alteration
on an Aircraft Certified under 14 CFR Part 23 or precursor regulations, as
outlined in FAA memorandum number PS-AIR-21.8-1602
SINGLE COLOR 6 LED GOOSENECK WHITE 24V| GN6-W24| Interior Aircraft Light|
Alteration Part| FAA memorandum number PS-AIR-21.8- 1602
Drawing: GN6 Rev.: –
Date: 04-20-16 or later FAA-approved revisions
| Provided the requirements of 14 CFR Part 1.1 and 14 CFR Part 43 Appendix A
are met and the installation does not detrimentally obstruct the pilots view
of required instrumentation, equipment may be installed as a minor alteration
on an Aircraft Certified under 14 CFR Part 23 or precursor regulations, as
outlined in FAA memorandum number PS-AIR-21.8-1602
Model| Part Number| Authorized Function|
Approved Replacement for| FAA Approval Basis and Approved
Design Data| Installation Eligibility:
---|---|---|---|---|---
DUAL COLOR 6 LED GOOSENECK WHITE/BLUE 12V| GN6-W/B12| Interior Aircraft Light|
Alteration Part| FAA memorandum number PS-AIR-21.8- 1602
Drawing: GN6 Rev.: –
Date: 04-20-16 or later FAA-approved revisions
| Provided the requirements of 14 CFR Part 1.1 and 14 CFR Part 43 Appendix A
are met and the installation does not detrimentally obstruct the pilots view
of required instrumentation, equipment may be installed as a minor alteration
on an Aircraft Certified under 14 CFR Part 23 or precursor regulations, as
outlined in FAA memorandum number PS-AIR-21.8-1602
DUAL COLOR 6 LED GOOSENECK WHITE/GREEN 12V| GN6-W/G12| Interior Aircraft
Light| Alteration Part| FAA memorandum number PS-AIR-21.8- 1602
Drawing: GN6 Rev.: –
Date: 04-20-16 or later FAA-approved revisions
| Provided the requirements of 14 CFR Part 1.1 and 14 CFR Part 43 Appendix A
are met and the installation does not detrimentally obstruct the pilots view
of required instrumentation, equipment may be installed as a minor alteration
on an Aircraft Certified under 14 CFR Part 23 or precursor regulations, as
outlined in FAA memorandum number PS-AIR-21.8-1602
DUAL COLOR 6 LED GOOSENECK WHITE/RED 12V| GN6-W/R12| Interior Aircraft Light|
Alteration Part| FAA memorandum number PS-AIR-21.8- 1602
Drawing: GN6 Rev.: –
Date: 04-20-16 or later FAA-approved revisions
| Provided the requirements of 14 CFR Part 1.1 and 14 CFR Part 43 Appendix A
are met and the installation does not detrimentally obstruct the pilots view
of required instrumentation, equipment may be installed as a minor alteration
on an Aircraft Certified under 14 CFR Part 23 or precursor regulations, as
outlined in FAA memorandum number PS-AIR-21.8-1602
DUAL COLOR 6 LED GOOSENECK WHITE/BLUE 24V| GN6-W/B24| Interior Aircraft Light|
Alteration Part| FAA memorandum number PS-AIR-21.8- 1602
Drawing: GN6 Rev.: –
Date: 04-20-16 or later FAA-approved revisions
| Provided the requirements of 14 CFR Part 1.1 and 14 CFR Part 43 Appendix A
are met and the installation does not detrimentally obstruct the pilots view
of required instrumentation, equipment may be installed as a minor alteration
on an Aircraft Certified under 14 CFR Part 23 or precursor regulations, as
outlined in FAA memorandum number PS-AIR-21.8-1602
DUAL COLOR 6 LED GOOSENECK WHITE/GREEN 24V| GN6-W/G24| Interior Aircraft
Light| Alteration Part| FAA memorandum number PS-AIR-21.8- 1602
Drawing: GN6 Rev.: –
Date: 04-20-16 or later FAA-approved revisions
| Provided the requirements of 14 CFR Part 1.1 and 14 CFR Part 43 Appendix A
are met and the installation does not detrimentally obstruct the pilots view
of required instrumentation, equipment may be installed as a minor alteration
on an Aircraft Certified under 14 CFR Part 23 or precursor regulations, as
outlined in FAA memorandum number PS-AIR-21.8-1602
Model| Part Number| Authorized Function|
Approved Replacement for| FAA Approval Basis and Approved
Design Data| Installation Eligibility:
---|---|---|---|---|---
DUAL COLOR 6 LED GOOSENECK WHITE/RED 24V| GN6-W/R24| Interior Aircraft Light|
Alteration Part| FAA memorandum number PS-AIR-21.8- 1602
Drawing: GN6 Rev.: –
Date: 04-20-16 or later FAA-approved revisions
| Provided the requirements of 14 CFR Part 1.1 and 14 CFR Part 43 Appendix A
are met and the installation does not detrimentally obstruct the pilots view
of required instrumentation, equipment may be installed as a minor alteration
on an Aircraft Certified under 14 CFR Part 23 or precursor regulations, as
outlined in FAA memorandum number PS-AIR-21.8-1602
SINGLE COLOR 4 LED GOOSENECK RED 12V| GN4-R12| Interior Aircraft Light|
Alteration Part| FAA memorandum number PS-AIR-21.8- 1602
Drawing: GN4 Rev.: –
Date: 04-04-16 or later FAA-approved revisions
| Provided the requirements of 14 CFR Part 1.1 and 14 CFR Part 43 Appendix A are met and the installation does not detrimentally obstruct the pilots view of required instrumentation, equipment may be installed as a minor alteration on an Aircraft Certified under 14 CFR Part 23 or precursor regulations, as outlined in FAA memorandum number PS-AIR-21.8-1602
It is critical for users of the above equipment to understand that NORSEE is
considered secondary or non-essential to the required equipment and that the
FAA has not verified the functionality of this device. It is vital for the
pilot in command to understand its functionality, limitations, and intent to
provide only supplemental, non-contradictory information. It is the pilot’s
responsibility to use basic airmanship to operate the aircraft safely with or
without the aid of NORSEE.
This approval is based on the authorized functions as stated in the above
table. Uses outside of this authorized function have not been reviewed by the
FAA to comply with the requirements of FAA Policy PS-AIR-21.8-1602 and may
require additional evaluation. It should also be noted that NORSEE production
approval does not grant Installation Approval, Parts Manufacturer Approval
(PMA) or Technical Standard Order Authorization (TSOA).
We also accept the statement that your quality system meets the requirements
of FAA Policy PS-AIR-21.8-1602. We authorize production of this NORSEE
equipment at your Machine Incorporated facility located at 879 Turnpike Street
Stoughton, MA. Components of articles produced under this approval must be
permanently and legibly marked with the authorization holder’s name, or
trademark, or symbol, the part number and “14 CFR 21.8(d)” where practiable.
You must allow the FAA to inspect your quality system, facilities, technical
data, any manufactured articles and witness any tests, including any
inspections or test at a supplier facility as necessary to investigate any
service difficulty or possible non-compliance with FAA Policy PS-
AIR-21.8-1602. Any service difficulties with the equipment should be reported
to the Chicago ACO.
You must notify the FAA before making any changes to the location of any of
your manufacturing facilities, company name or ownership. This approval is
transferable to another U.S. manufacturer subject to the transferee complying
with the NORSEE policy PS-AIR-21.8-1602 (or later policy revision) and design
approval holders responsibilities stated in this letter of authorization.
This approval is effective until surrendered, withdrawn or otherwise
terminated by the FAA. If you have any questions, please call Scott Fohrman,
at 847-294-7136, fax
847-294-7834, email
scott.fohrman@faa.gov.
Sincerely,
Roy E Boffo III
Manager, Propulsion and Program Management Branch Chicago Aircraft
Certification Branch
Federal Aviation Adminstration
cc:
AIR-7C3 R/F
Scott Fohrman (file copy)
K:\Common:\NORSEE\Machine Inc\task light Machine INC NORSEE ltr.doc AIR-
7C3:\sf:\x7379:\sf:\11/09/2021
8110.1.b NORSEE Machine INC 20G05
ASTARS N/A
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