Source: https://www.federalregister.gov/documents/2014/07/25/2014-17578/special-conditions-airbus-model-a350-900-airplanes-lateral-trim-function-through-differential-flap
Timestamp: 2018-04-20 20:44:57
Document Index: 383612899

Matched Legal Cases: ['art 25', '§\u200921', 'art 34', 'art 36', '§\u2009611', '§\u200925', '§\u200925', '§\u200925', '§\u200925', '§\u200925']

Federal Register :: Special Conditions: Airbus Model A350-900 Airplanes; Lateral-Trim Function Through Differential Flap Setting
Special Conditions: Airbus Model A350-900 Airplanes; Lateral-Trim Function Through Differential Flap Setting
A Rule by the Federal Aviation Administration on 07/25/2014
79 FR 43236
43236-43237 (2 pages)
Docket No. FAA-2013-0911
Special Conditions No. 25-539-SC
2014-17578
FAA-2013-0911
Lateral-Trim Function Through Differential Flap Setting
https://www.federalregister.gov/d/2014-17578 https://www.federalregister.gov/d/2014-17578
These special conditions are issued for Airbus Model A350-900 airplanes. These airplanes will have a novel or unusual design feature associated with a lateral-trim function that deploys flaps asymmetrically for airplane lateral-trim control. This function replaces the traditional method of providing airplane lateral trim over a small range through flap and aileron mechanical rigging. The applicable airworthiness regulations do not contain adequate or appropriate safety standards for this design feature. These special conditions contain the additional safety standards that the Administrator considers necessary to establish a level of safety equivalent to that established by the existing airworthiness standards.
Effective Date: August 25, 2014.
Robert C. Jones, FAA, Propulsion and Mechanical Systems, ANM-112, Transport Airplane Directorate, Aircraft Certification Service, 1601 Lind Avenue SW., Renton, Washington 98057-3356; telephone (425) 227-1234; facsimile (425) 227-1320.
On conventional airplanes, small, lateral, airplane asymmetries typically have been addressed through flap and aileron rigging (e.g., using shims). On Model A350-900 airplanes, an order for asymmetric flap deployment will be computed by the primary flight-control system as a function of the aileron position. The current airworthiness standards do not contain adequate safety standards for asymmetric use of the flaps for Airbus Model A350-900 airplanes. Special conditions are needed to account for the aspects of a function used to command an intended flap asymmetry. The lateral-trim function is intended to be performed once during climb and once during cruise to compensate for airplane small lateral asymmetries.
The lateral-trim function is not a trim-control system in the conventional sense as it has no pilot interface and is not governed by Title 14, Code of Federal Regulations (14 CFR) 25.677. Some fly-by-wire airplanes have no pilot-operated lateral trim at all. The lateral-trim function is simply an additional fly-by-wire flight-control function that nulls small roll asymmetries in certain flight phases with small, asymmetric flap deployments. Although the function operates under normal conditions within the small range of the traditional rigging, failure cases may result in a significant out-of-range asymmetric flap condition. An asymmetry threshold protects the system against excessive flap asymmetry.
If the Administrator finds that the applicable airworthiness regulations (i.e., 14 CFR part 25) do not contain adequate or appropriate safety standards for the Model A350-900 airplane because of a novel or unusual design feature, special conditions are prescribed under § 21.16.
In addition to the applicable airworthiness regulations and special conditions, the Model A350-900 airplane must comply with the fuel-vent and exhaust-emission requirements of 14 CFR part 34, and the noise-certification requirements of 14 CFR part 36. The FAA must issue a finding of regulatory adequacy under § 611 of Public Law 92-574, the “Noise Control Act of 1972.”
The Airbus Model A350-900 airplane incorporates the following novel or unusual design features: The asymmetric use of flaps to address lateral trim, which is not adequately addressed by § 25.701.Start Printed Page 43237
Section 25.701(a) requires that, unless the airplane has safe-flight characteristics with the flaps or slats retracted on one side and extended on the other, flap and slat surfaces must be synchronized by either a mechanical interconnection or any equivalent means that has the same integrity. Synchronization is interpreted to mean that flap movement is symmetrical throughout the full range of flap motion. Because the lateral-trim function intentionally creates asymmetric flap motions, the flap-system installation of the Model A350-900 airplane does not meet the requirement of § 25.701(a) and (d).
Notice of proposed special conditions no. 25-13-22-SC for Airbus Model A350-900 airplanes was published in the Federal Register on January 8, 2014 (79 FR 1339). No comments were received, and the special conditions are adopted as proposed.
This action affects only certain novel or unusual design features on the Airbus Model A350-900 airplanes. It is not a rule of general applicability.
Accordingly, pursuant to the authority delegated to me by the Administrator, the following special conditions are issued as part of the type-certification basis for Airbus Model A350-900 airplanes:
Current airworthiness standards, specifically § 25.701, do not contain adequate safety standards for this airplane design. In lieu of the requirements of § 25.701(a) and (d) for the lateral-trim function, the following special condition are issued:
1. Airbus must demonstrate that an unsafe condition is not created by using the flaps asymmetrically.
2. The degree of acceptable asymmetry must be defined and justified for all flight phases with respect to:
a. Section 25.701(b) and (c), with the worst-case asymmetric flap configurations, and
b. Providing equivalent protection against excess asymmetry in the same manner as § 25.701 provides to systems that are synchronized, or use another equivalent means to prevent asymmetry.
3. This lateral-trim function is a flight-control system and therefore must be shown to comply with both general system requirements as well as general flight-control requirements. Therefore, the function must be demonstrated not to have significant latent failures, where practicable.
[FR Doc. 2014-17578 Filed 7-24-14; 8:45 am]