AircraftNoiseCertificationLevel

AircraftNoiseCertificationLevel

Term

AircraftNoiseCertificationLevel

Business term

Aircraft Noise Certification Level

Definition

The classification of an Aircraft based on the ICAO noise certification standard it complies with.

Allowed values

It is only the chapter number, i.e. "2", "12", that are used in this attribute.

Allowed values are: "2" - "13"

Comments

Also known as Aircraft Chapter, ref. ICAO Annex 16 V1 

The following levels are defined:

"2"

Subsonic jet aeroplanes - Application for type certificate submitted before 6 October 1977

"3"

Subsonic jet aeroplanes - application for type certificate submitted on or after 6 October 1977 and before 1 January 2006

Propeller-driven aeroplanes over 5700 kg - application for type certificate submitted on or after 1 January 1985 and before 17 November 1988

Propeller-driven aeroplanes over 8616 kg - application for type certificate submitted on or after 6 October 1977 and before 1 January 2006

"4"

Subsonic jet aeroplanes -application for type certificate submitted on or after 1 January 2006
Propeller-Driven aeroplanes over 8618 kg - application Certificate submitted on or after 1 January 2006

"5"

Propeller-Driven aeroplanes over 5700 kg - application Certificate submitted before 1 January 1985

"6"

Propeller-Driven aeroplanes not exceeding 8616 kg - application Certificate submitted before 17 November 1988

"7"

Propeller-Driven Short Take Off and Landing (STOL) Aeroplanes

"8"

Helicopters

"9"

Installed auxiliary power unites (APU) and associated aircraft/systems during ground operations

"10"

Propeller driven aeroplanes not exceeding 8616 kg - application for type certificate or derived version submitted on or after 17 November 1988.

"11"

Helicopters not exceeding 3175 kg maximum certificated take off mass.

"12"

Supersonic aeroplanes

"13"

Tilt rotor aircraft

 

Status

Approved

XML type

string(2)

AIRM equivalent

CodeNoiseCertificationType

AIDM equivalent