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
Chicago ACO Branch 2300 East Devon Avenue Des Plaines, IL 60018
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
Authorized
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
Approved Replacement for
Alteration Part
Alteration Part
FAA Approval Basis and Approved Design Data
FAA memorandum number PS-AIR-21.81602 Drawing: 4501-00 Rev.: A Date: 03-12-21 or later FAA-approved revisions
FAA memorandum number PS-AIR-21.81602 Drawing: 4501-00 Rev.: A Date: 03-12-21 or later FAA-approved revisions
Installation Eligibility:
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.
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
Authorized
Number Function
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
2
Approved Replacement for
Alteration Part
Alteration Part
Alteration Part
Alteration Part
Alteration Part
FAA Approval Basis and Approved Design Data
FAA memorandum number PS-AIR-21.81602 Drawing: 4501-00 Rev.: A Date: 03-12-21 or later FAA-approved revisions
FAA memorandum number PS-AIR-21.81602 Drawing: 4501-00 Rev.: A Date: 03-12-21 or later FAA-approved revisions
FAA memorandum number PS-AIR-21.81602 Drawing: 4501-00 Rev.: A Date: 03-12-21 or later FAA-approved revisions
FAA memorandum number PS-AIR-21.81602 Drawing: 4501-00 Rev.: A Date: 03-12-21 or later FAA-approved revisions
FAA memorandum number PS-AIR-21.81602 Drawing: 4501-00 Rev.: A Date: 03-12-21 or later FAA-approved revisions
Installation Eligibility:
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.
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.
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.
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.
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
Authorized
Number Function
SINGLE COLOR OP4-W24 4 LED OPLITE WHITE 24V
Interior Aircraft Light
SINGLE COLOR OP6-B12 6 LED OPLITE BLUE 12V
Interior Aircraft Light
SINGLE COLOR OP6-G12 6 LED OPLITE GREEN 12V
Interior Aircraft Light
SINGLE COLOR OP6-R12 6 LED OPLITE RED 12V
Interior Aircraft Light
SINGLE COLOR OP6-W12 6 LED OPLITE WHITE 12V
Interior Aircraft Light
3
Approved Replacement for
Alteration Part
Alteration Part
Alteration Part
Alteration Part
Alteration Part
FAA Approval Basis and Approved Design Data
FAA memorandum number PS-AIR-21.81602 Drawing: 4501-00 Rev.: A Date: 03-12-21 or later FAA-approved revisions
FAA memorandum number PS-AIR-21.81602 Drawing: 6501-00 Rev.: A Date: 03-12-21 or later FAA-approved revisions
FAA memorandum number PS-AIR-21.81602 Drawing: 6501-00 Rev.: A Date: 03-12-21 or later FAA-approved revisions
FAA memorandum number PS-AIR-21.81602 Drawing: 6501-00 Rev.: A Date: 03-12-21 or later FAA-approved revisions
FAA memorandum number PS-AIR-21.81602 Drawing: 6501-00 Rev.: A Date: 03-12-21 or later FAA-approved revisions
Installation Eligibility:
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.
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.
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.
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.
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.
4
Model
Part
Authorized
Number Function
SINGLE COLOR OP6-B24 6 LED OPLITE BLUE 24V
Interior Aircraft Light
SINGLE COLOR OP6-G24 6 LED OPLITE GREEN 24V
Interior Aircraft Light
SINGLE COLOR OP6-R24 6 LED OPLITE RED 24V
Interior Aircraft Light
SINGLE COLOR OP6-W24 6 LED OPLITE WHITE 24V
Interior Aircraft Light
DUAL COLOR 6 LED OPLITE WHITE/BLUE 12V
OP6W/B12
Interior Aircraft Light
Approved Replacement for
Alteration Part
Alteration Part
Alteration Part
Alteration Part
Alteration Part
FAA Approval Basis and Approved Design Data
FAA memorandum number PS-AIR-21.81602 Drawing: 6501-00 Rev.: A Date: 03-12-21 or later FAA-approved revisions
FAA memorandum number PS-AIR-21.81602 Drawing: 6501-00 Rev.: A Date: 03-12-21 or later FAA-approved revisions
FAA memorandum number PS-AIR-21.81602 Drawing: 6501-00 Rev.: A Date: 03-12-21 or later FAA-approved revisions
FAA memorandum number PS-AIR-21.81602 Drawing: 6501-00 Rev.: A Date: 03-12-21 or later FAA-approved revisions
FAA memorandum number PS-AIR-21.81602 Drawing: 6501-00 Rev.: A Date: 03-12-21 or later FAA-approved revisions
Installation Eligibility:
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.
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.
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.
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.
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.
5
Model
Part Number
Authorized Function
Approved Replacement for
DUAL COLOR 6 LED OPLITE WHITE/GREEN 12V
OP6-W/G12
Interior Aircraft Light
Alteration Part
DUAL COLOR 6 LED OPLITE WHITE/RED 12V
OP6-W/R12
Interior Aircraft Light
Alteration Part
DUAL COLOR 6 LED OPLITE WHITE/BLUE 24V
OP6-W/B24
Interior Aircraft Light
Alteration Part
DUAL COLOR 6 LED OPLITE WHITE/GREEN 24V
OP6-W/G24
Interior Aircraft Light
Alteration Part
DUAL COLOR 6 LED OPLITE WHITE/RED 24V
OP6-W/R24
Interior Aircraft Light
Alteration Part
FAA Approval Basis and Approved Design Data
FAA memorandum number PS-AIR-21.81602 Drawing: 6501-00 Rev.: A Date: 03-12-21 or later FAA-approved revisions
FAA memorandum number PS-AIR-21.81602 Drawing: 6501-00 Rev.: A Date: 03-12-21 or later FAA-approved revisions
FAA memorandum number PS-AIR-21.81602 Drawing: 6501-00 Rev.: A Date: 03-12-21 or later FAA-approved revisions
FAA memorandum number PS-AIR-21.81602 Drawing: 6501-00 Rev.: A Date: 03-12-21 or later FAA-approved revisions
FAA memorandum number PS-AIR-21.81602 Drawing: 6501-00 Rev.: A Date: 03-12-21 or later FAA-approved revisions
Installation Eligibility:
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.
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.
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.
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.
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.
6
Model
Part Number
SINGLE COLOR 4 LED GOOSENECK BLUE 12V
GN4-B12
Authorized Function
Interior Aircraft Light
Approved Replacement for
Alteration Part
SINGLE COLOR 4 LED GOOSENECK GREEN 12V
GN4-G12
Interior Aircraft Light
Alteration Part
SINGLE COLOR 4 LED GOOSENECK WHITE 12V
GN4-W12
Interior Aircraft Light
Alteration Part
SINGLE COLOR 4 LED GOOSENECK BLUE 24V
GN4-B24
Interior Aircraft Light
Alteration Part
SINGLE COLOR 4 LED GOOSENECK GREEN 24V
GN4-G24
Interior Aircraft Light
Alteration Part
FAA Approval Basis and Approved Design Data
FAA memorandum number PS-AIR-21.81602 Drawing: GN4 Rev.: Date: 04-04-16 or later FAA-approved revisions
FAA memorandum number PS-AIR-21.81602 Drawing: GN4 Rev.: Date: 04-04-16 or later FAA-approved revisions
FAA memorandum number PS-AIR-21.81602 Drawing: GN4 Rev.: Date: 04-04-16 or later FAA-approved revisions
FAA memorandum number PS-AIR-21.81602 Drawing: GN4 Rev.: Date: 04-04-16 or later FAA-approved revisions
FAA memorandum number PS-AIR-21.81602 Drawing: GN4 Rev.: Date: 04-04-16 or later FAA-approved revisions
Installation Eligibility:
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
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
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
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
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
7
Model
Part Number
SINGLE COLOR 4 LED GOOSENECK RED 24V
GN4-R24
Authorized Function
Interior Aircraft Light
Approved Replacement for
Alteration Part
SINGLE COLOR 4 LED GOOSENECK WHITE 24V
GN4-W24
Interior Aircraft Light
Alteration Part
SINGLE COLOR 6 LED GOOSENECK BLUE 12V
GN6-B12
Interior Aircraft Light
Alteration Part
SINGLE COLOR 6 LED GOOSENECK GREEN 12V
GN6-G12
Interior Aircraft Light
Alteration Part
SINGLE COLOR 6 LED GOOSENECK RED 12V
GN6-R12
Interior Aircraft Light
Alteration Part
FAA Approval Basis and Approved Design Data
FAA memorandum number PS-AIR-21.81602 Drawing: GN4 Rev.: Date: 04-04-16 or later FAA-approved revisions
FAA memorandum number PS-AIR-21.81602 Drawing: GN4 Rev.: Date: 04-04-16 or later FAA-approved revisions
FAA memorandum number PS-AIR-21.81602 Drawing: GN6 Rev.: Date: 04-20-16 or later FAA-approved revisions
FAA memorandum number PS-AIR-21.81602 Drawing: GN6 Rev.: Date: 04-20-16 or later FAA-approved revisions
FAA memorandum number PS-AIR-21.81602 Drawing: GN6 Rev.: Date: 04-20-16 or later FAA-approved revisions
Installation Eligibility:
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
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
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
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
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
8
Model
Part Number
SINGLE COLOR 6 LED GOOSENECK WHITE 12V
GN6-W12
Authorized Function
Interior Aircraft Light
Approved Replacement for
Alteration Part
SINGLE COLOR 6 LED GOOSENECK BLUE 24V
GN6-B24
Interior Aircraft Light
Alteration Part
SINGLE COLOR 6 LED GOOSENECK GREEN 24V
GN6-G24
Interior Aircraft Light
Alteration Part
SINGLE COLOR 6 LED GOOSENECK RED 24V
GN6-R24
Interior Aircraft Light
Alteration Part
SINGLE COLOR 6 LED GOOSENECK WHITE 24V
GN6-W24
Interior Aircraft Light
Alteration Part
FAA Approval Basis and Approved Design Data
FAA memorandum number PS-AIR-21.81602 Drawing: GN6 Rev.: Date: 04-20-16 or later FAA-approved revisions
FAA memorandum number PS-AIR-21.81602 Drawing: GN6 Rev.: Date: 04-20-16 or later FAA-approved revisions
FAA memorandum number PS-AIR-21.81602 Drawing: GN6 Rev.: Date: 04-20-16 or later FAA-approved revisions
FAA memorandum number PS-AIR-21.81602 Drawing: GN6 Rev.: Date: 04-20-16 or later FAA-approved revisions
FAA memorandum number PS-AIR-21.81602 Drawing: GN6 Rev.: Date: 04-20-16 or later FAA-approved revisions
Installation Eligibility:
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
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
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
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
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
9
Model
Part Number
Authorized Function
Approved Replacement for
DUAL COLOR 6 LED GOOSENECK WHITE/BLUE 12V
GN6-W/B12
Interior Aircraft Light
Alteration Part
DUAL COLOR 6 LED GOOSENECK WHITE/GREEN 12V
GN6-W/G12
Interior Aircraft Light
Alteration Part
DUAL COLOR 6 LED GOOSENECK WHITE/RED 12V
GN6-W/R12
Interior Aircraft Light
Alteration Part
DUAL COLOR 6 LED GOOSENECK WHITE/BLUE 24V
GN6-W/B24
Interior Aircraft Light
Alteration Part
DUAL COLOR 6 LED GOOSENECK WHITE/GREEN 24V
GN6-W/G24
Interior Aircraft Light
Alteration Part
FAA Approval Basis and Approved Design Data
FAA memorandum number PS-AIR-21.81602 Drawing: GN6 Rev.: Date: 04-20-16 or later FAA-approved revisions
FAA memorandum number PS-AIR-21.81602 Drawing: GN6 Rev.: Date: 04-20-16 or later FAA-approved revisions
FAA memorandum number PS-AIR-21.81602 Drawing: GN6 Rev.: Date: 04-20-16 or later FAA-approved revisions
FAA memorandum number PS-AIR-21.81602 Drawing: GN6 Rev.: Date: 04-20-16 or later FAA-approved revisions
FAA memorandum number PS-AIR-21.81602 Drawing: GN6 Rev.: Date: 04-20-16 or later FAA-approved revisions
Installation Eligibility:
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
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
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
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
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
10
Model
Part Number
Authorized Function
Approved Replacement for
DUAL COLOR 6 LED GOOSENECK WHITE/RED 24V
GN6-W/R24
Interior Aircraft Light
Alteration Part
SINGLE COLOR 4 LED GOOSENECK RED 12V
GN4-R12
Interior Aircraft Light
Alteration Part
FAA Approval Basis and Approved Design Data
FAA memorandum number PS-AIR-21.81602 Drawing: GN6 Rev.: Date: 04-20-16 or later FAA-approved revisions
FAA memorandum number PS-AIR-21.81602 Drawing: GN4 Rev.: Date: 04-04-16 or later FAA-approved revisions
Installation Eligibility:
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
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 PSAIR-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-
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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 [email protected].
Sincerely,
Roy E Boffo III Manager, Propulsion and Program Management Branch Chicago Aircraft Certification Branch Federal Aviation Adminstration
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cc: AIR-7C3 R/F Scott Fohrman (file copy)
K:Common:NORSEEMachine Inctask light Machine INC NORSEE ltr.doc AIR-7C3:sf:x7379:sf:11/09/2021 8110.1.b NORSEE Machine INC 20G05 ASTARS N/A
