MG 16 Certification guidance for rotorcraft Night
Vision Imaging System (NVIS) aircraft lighting systems
ED
Decision 2018/015/R
This AMC
provides further guidance and acceptable means of compliance to supplement FAA
AC 27-1B Change 7 MG 16, which is the EASA acceptable means of compliance, as
provided for in AMC 27 General. However, some aspects of the FAA AC are deemed
by EASA to be at variance with EASA’s interpretation or its regulatory system.
EASA’s interpretation of these aspects is described below. Paragraphs of FAA
AC 27-1B Change 7 MG 16 that are not amended below are considered to be EASA
acceptable means of compliance.
[...]
d. References (use the current versions of the following references).
(1) Regulatory (CS-27).
|
27.1 |
27.1322 |
27.1501 |
|
27.21 |
27.1351 |
27.1523 |
|
27.141(c) |
27.1357 |
27.1525 |
|
27.603(c) |
27.1367 |
27.1529 |
|
27.771 |
27.1381 |
27.1541 |
|
27.773 |
27.1383 |
27.1543 |
|
27.777 |
27.1385 |
27.1545 |
|
27.785 |
27.1387 |
27.1549 |
|
27.807(b)(3) |
27.1389 |
27.1553 |
|
27.853 |
27.1391 |
27.1555 |
|
27.1301 |
27.1393 |
27.1557 |
|
27.1303 |
27.1395 |
27.1561 |
|
27.1305 |
27.1397 |
27.1581 |
|
27.1307 |
27.1399 |
27.1583 |
|
27.1309 |
27.1401 |
27.1585 |
|
27.1321 |
|
|
(2) Other references
|
Document |
Title |
|
FAA AC 25-11B |
Electronic Flight Displays |
|
FAA AC 20-74 |
Aircraft Position and Anticollision Light Measurements |
|
FAA AC 20-88A |
Guidelines on the Marking of Aircraft Powerplant Instruments (Displays) |
|
FAA AC 20-152 |
RTCA, Inc., Document RTCA/DO-254, Design Assurance Guidance for Airborne Electronic Hardware |
|
RTCA DO-268 |
Concept of Operations, Night Vision Imaging System for Civil Operators |
|
RTCA DO-275 |
Minimum Operational Performance Standards for Integrated Night Vision Imaging System Equipment |
|
SAE ARP 4754A |
Certification considerations for highly-integrated or complex aircraft systems |
|
SAE ARP 4761 |
Guidelines and Methods for Conducting the Safety Assessment Process on Civil Airborne Systems and Equipment |
|
Document |
Title |
|
SAE ARP 5825A |
Design Requirements and Test Procedures for Dual Mode Exterior Lights |
|
ETSO-C4c |
Bank and Pitch Instruments |
|
ETSO-C8e |
Vertical Velocity Instrument (Rate-of-Climb) |
|
ETSO-C87a |
Airborne Low-Range Radio Altimeter |
|
ETSO-C164 |
Night Vision Goggles (NVG) |
[...]
e. Background.
[...]
(7) Night
vision goggles (NVGs) enhance a pilot’s night vision by amplifying certain
energy frequencies. The NVGs for civil use are based on performance criteria
in ETSO-C164 and RTCA Document DO-275. These NVGs are known as ‘Class B NVGs’
because they have filters applied to the objective lenses that block energy
below the wavelength of 665 nanometres (nm). The Class B objective lens filter
allows more use of colour in the cockpit, with truer reds and ambers. The ETSO
specifies Class B NVGs for civil use. Because NVGs will amplify energy that is
not within the range of the filter, it is important that the NVIS lighting
system keeps those incompatible frequencies out of the cockpit. However, there
are NVGs in civil use that do not conform to the ETSO-C164 standard because
they have Class A filters on their objective lenses. Class A filters block
energy below the wavelength of 625 nm. As a result, Class A NVGs amplify more
wavelengths of visible light, so they require special care in the use of
colour in the cockpit. Applicants are advised that Class A NVGs are deemed to
be not acceptable for certification by EASA.
[...]
(9) Point
21.A.91 of Annex I to Regulation (EU) No 748/2012 contains the criteria for
the classification of changes to a type certificate. For NVIS-approved
rotorcraft, experience has shown that some changes, which are classified as
being minor according to the AMC to 21.A.91 for unaided flight, may have an
appreciable effect on the cockpit/cabin lighting characteristics, and thus on
crew vision through the NVGs. Therefore, the classification of design changes
of NVIS-approved rotorcraft should take into account the effects on
cockpit/cabin lighting characteristics and the NVIS.
[...]
f. Procedures.
[...]
(6) Required
equipment, instrument arrangement and visibility.
(i) In
addition to the instruments and equipment required for flight at night, the
following additional instruments and equipment will typically be necessary for
NVG operations (to be defined for each rotorcraft). The applicable operational
regulations that specify aircraft equipment required for night and NVG
operations should be reviewed.
(A) NVIS
lighting.
(B) A helmet with suitable NVG mount for each pilot and crew member required to use NVGs.
(C) NVGs for
each pilot and crew members required to use NVGs.
(D) Point
SPA.NVIS.110(b) of Annex V (Part-SPA) to Regulation (EU) 965/2012 on air
operations, and the associated AMC and GM, requires a radio altimeter with an
analogue representation. It is recommended that an applicant carries out a
careful evaluation of the radio altimeter human-machine interface (including
the presentation of height and the possibility of selecting the DH) to
establish that it is able to provide the crew with the necessary information.
(E) A
slip/skid indicator.
(F) A
gyroscopic attitude indicator.
(G) A
gyroscopic direction indicator or its equivalent.
(H) A
vertical speed indicator or its equivalent.
(I) Communications
and navigation equipment necessary for the successful completion of an
inadvertent IMC procedure in the intended area of operations.
(J) Any other aircraft or personal equipment required for the operation (e.g. curtains, NVG stowage, extra batteries for NVGs).
[Amdt No: 27/6]
EASA provides guidance for rotorcraft Night Vision Imaging System (NVIS) aircraft lighting, supplementing FAA standards with EASA interpretations. Civil NVIS should use Class B NVGs. Design changes must consider cockpit lighting effects on NVIS. Specific equipment, including radio altimeters and attitude indicators, are needed for NVG operations.
* Summary by Aviation.Bot - Always consult the original document for the most accurate information.
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