Navigate / EASA

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.

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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)

 

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e.       Background.

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(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.

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f.       Procedures.

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(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]