Special Condition (SC)

Applicable to Large Aeroplanes

Applicable to Large Aeroplane category

on Aeronautical Telecommunication Network (ATN) over SATCOM

Applicable to Large Aeroplanes

Applicable to Large Aeroplanes

Applicable to Large Aeroplanes

Applicable to Large Aeroplanes

Applicable to Large Aeroplanes

Applicable to Large Aeroplane category

Applicable to Large Aeroplanes

SC E-18

Applicable to Large Aeroplanes

CS-E, all amendments

Applicable to A330-700L “Beluga XL”

Applicable to Large Rotorcraft when fitted with a cargo / baggage compartment

Rudder Control Reversal Load Conditions Applicable to Large Aeroplane category

Installation of Li-type storage batteries in sailplanes/powered sailplanes, LSA and VLA

Applicable to A330/A340

Applicable to Boeing 777-9

Applicable to Boeing 777-9

intended for Use in Rotorcraft

Applicable to A330-700L “Beluga XL”

for CS-23 aircraft

Single Point Refuel and Defuel System

Flight Instrument External Probes – Qualification in Icing Conditions

Applicable to Airbus A330 NEO

Applicable to Airbus A330 NEO

Applicable to Boeing 787-10

Applicable to Large Aeroplanes

Special condition applicable to LSA Propulsion Batteries

Applicable Airbus A350

Applicable to Embraer EMB-545

Remote Pilot Station

Maintenance Certifying Staff Data

Interaction of Systems and Structure on helicopters with Fly-by-Wire (FBW) Flight Control System (FCS)

Use of flaperons for lift and roll control - Applicable to Dassault Aviation Falcon 5X

Proposed Special Condition RPAS Flight Control System

RPAS Ancillary elements – Arresting cable system

RPAS Required Communications, Navigation and Surveillance

RPAS Command and Control (C2)

RPAS Human Factors

Applicable to Bombardier DHC-8 400, modified by auxiliary fuel tank system installation

Supplementary requirement to CS-23 901 for clarification of water ingestion and harmonisation with FAR 23.901

Applicable to Large Aeroplane category

RPA Electronic Equipment Fault Detection and Isolation

Ground Control Station Electrical Systems

Applicable to Large Aeroplane category

Certification of Auto-Throttle Function in CS-23 Aircraft

Fan blade loss - effects at aircraft level - Applicable to Airbus A-320 Neo (equipped with CFN LEAP-1A engines)

Equipment, Systems and Installations in Small Remotely Piloted Unmanned Systems (RPAS)

Limited Icing Clearances Applicable to Large Rotorcraft, CS-29 or equivalent.

High Wall Mini-Suite (Applicable to Airbus A380 / Boeing 777)

for limited Icing Clearances Applicable to Large Rotorcraft, CS 29 or equivalent

Use of Magnesium Alloys for Passenger Seat Components (Applicable to Airbus A350-941)

Qualification in Icing Conditions of External Probes (Applicable to Bombardier CSeries)

‘A310 Zero G’ cabin layout modification - Applicable to A310-304 aircraft model

Seats and seat belts for hot air balloon baskets

CS-VLA Aeroplanes to be operated according to IFR

Passenger sleeping compartments (Applicable to Airbus A380)

Soft Go-around Mode (Applicable to Airbus A350-941)

Installation of Cargo Seat Bags for the purpose of transporting passenger luggage - Applicable to Large Aeroplane

Transient over-temperature, over-speed and over-torque limit approval

Normal Load Factor limiting System (Applicable to Airbus A350-941)

Lateral Trim function trough Differential Flap Setting (Applicable to Airbus A350-941)

Supplementary requirements to CS-23 for approval of Object Towing Operation (other than glider and banner towing)

Supplementary requirements to CS-VLA for approval of aerobatics with VLA

Crash Survivability for CFRP Fuselage (Applicable to Airbus A350-941)

Crew Rest Compartments (Applicable to Airbus A350-941)

Cancellation of AFM Engine Management Tables (Applicable to Airbus A350-941)

Approval of Turbofan Engine to use two (2) periods “10 Minutes One Engine Inoperative Take-off Thrust at High Ambient Temperature (10 Minutes OEI TOTHAT)” rating

Stalling and Scheduled Operating Speeds (Applicable to Airbus A350-941)

Flight in Icing Condition (Applicable to Airbus A350-941)

Engine Operation with Selectable OEI Ratings Structures

Engine Operation in Auxiliary Power Unit (APU) Mode

Cargo Fire Containment in an occupied Passenger Cabin (Applicable to Learjet 45)

Installations of placards on the aircraft cabin windows, applicable to the Boeing B737 aircraft

Steep Approach and Landing CRI replacing CS 23.1511

Loss of Oil from Gearboxes Utilising a Pressurised Lubrication System - Applicable to AW 189

Applicable to A380

Engine cowl retention (Applicable to Large Aircraft Transport Category)

Pilot Compartment View CS 25.773(b) (Applicable to Embraer EMB 545/550)

Applicable to A380

Medical Evacuation configuration (Applicable to Large Aeroplane category)

Applicable to all aircraft that require certificates in accordance with Regulation (EC) No 1702/2003 intending to fly into European airspace above FL 285

Applicable to Airbus A350