Federal Aviation Administration July 19, 2018 – Federal Register Recent Federal Regulation Documents

Special Conditions: Cranfield Aerospace Limited, Textron Aviation Inc. Model 525-Series Airplanes; Tamarack Load Alleviation System and Cranfield Winglets-Interaction of Systems and Structures
Document Number: 2018-15354
Type: Rule
Date: 2018-07-19
Agency: Federal Aviation Administration, Department of Transportation
These amended special conditions are issued for the Textron Aviation Inc. Model 525-series airplanes. These airplanesas modified by Cranfield Aerospace Limitedwill have a novel or unusual design feature associated with the installation of a Tamarack Active Technology Load Alleviation System and Cranfield Winglets. The applicable airworthiness regulations do not contain adequate or appropriate safety standards for this design feature. These amended special conditions contain the additional safety standards the Administrator considers necessary to establish a level of safety equivalent to that established by the existing airworthiness standards, change the Type Certificate holder, and remove the special flight permit requirement.
Settlement Policy for Commercial Pilots in Drug and Alcohol Testing Cases
Document Number: 2018-15352
Type: Rule
Date: 2018-07-19
Agency: Federal Aviation Administration, Department of Transportation
The FAA is adopting a procedure for prompt settlement agreements between the FAA and commercial pilots who have: Received a verified positive result for a Department of Transportation (DOT)- required drug test; received a DOT-required alcohol test result of .04 or above alcohol concentration; refused to submit to a DOT-required drug or alcohol test in violation of FAA regulations; or acted or attempted to act as a crewmember of an aircraft in commercial operations in violation of specified FAA regulations under this policy that proscribe the use, being under the influence or affects, or while have proscribed levels of alcohol or drugs. The settlement agreement procedures in this notification are generally available to pilots who, but for the disqualifying DOT drug or alcohol test result, refusal to submit to a DOT test, or violation of the specified alcohol- and drug- related FAA regulations prohibiting acting or attempting to act as a crewmember, would be qualified for a pilot certificate and who are first-time violators of these drug or alcohol provisions.
Airworthiness Directives; Bell Helicopter Textron Canada Limited Helicopters
Document Number: 2018-15305
Type: Proposed Rule
Date: 2018-07-19
Agency: Federal Aviation Administration, Department of Transportation
We propose to adopt a new airworthiness directive (AD) for Bell Helicopter Textron Canada Limited (Bell) Model 429 helicopters. This proposed AD would revise the life limit for the nose landing gear (NLG) assembly. This proposed AD is prompted by revised airworthiness limitations determined by Bell. The actions of this proposed AD are intended to prevent an unsafe condition on these helicopters.
Airworthiness Directives; Leonardo S.p.A. Helicopters
Document Number: 2018-15304
Type: Proposed Rule
Date: 2018-07-19
Agency: Federal Aviation Administration, Department of Transportation
We propose to adopt a new airworthiness directive (AD) for Leonardo S.p.A. (Leonardo) Model AB139 and AW139 helicopters. This proposed AD would require replacing screws installed on the left and right main landing gear (MLG) shock absorber assembly. This proposed AD is prompted by a report that some screws may have been manufactured without meeting specifications. The actions of this proposed AD are intended to correct an unsafe condition on these helicopters.
Airworthiness Directives; Airbus Helicopters
Document Number: 2018-15303
Type: Rule
Date: 2018-07-19
Agency: Federal Aviation Administration, Department of Transportation
We are adopting a new airworthiness directive (AD) for Airbus Helicopters Model AS350B, AS350B1, AS350B2, AS350B3, AS350BA, AS355E, AS355F, AS355F1, AS355F2, AS355N, and AS355NP helicopters. This AD requires inspecting the tail rotor (TR) pitch rod. This AD is prompted by a report of several cases of damaged TR pitch rod ball joints. The actions of this AD are intended to correct an unsafe condition on these helicopters.
Airworthiness Directives; Pratt & Whitney Division (PW) Turbofan Engines
Document Number: 2018-15291
Type: Proposed Rule
Date: 2018-07-19
Agency: Federal Aviation Administration, Department of Transportation
We propose to adopt a new airworthiness directive (AD) for all Pratt & Whitney Division (PW) PW4074D, PW4077D, PW4084D, PW4090, and PW4090-3 turbofan engines with a low pressure compressor (LPC) fan hub, part number (P/N) 51B821 or P/N 52B521, installed. This proposed AD was prompted by updated low cycle fatigue analysis techniques that indicate certain LPC fan hubs could crack prior to their published life limit. This proposed AD would require repetitive eddy current inspections (ECIs) and fluorescent penetrant inspections (FPIs) for cracks in certain LPC fan hubs and removal of hubs from service that fail inspection. We are proposing this AD to address the unsafe condition on these products.
Airworthiness Directives; ATR-GIE Avions de Transport Régional Airplanes
Document Number: 2018-14809
Type: Rule
Date: 2018-07-19
Agency: Federal Aviation Administration, Department of Transportation
We are adopting a new airworthiness directive (AD) for all ATR-GIE Avions de Transport R[eacute]gional Model ATR72 airplanes. This AD was prompted by a determination that more restrictive maintenance instructions and airworthiness limitations are necessary. This AD requires revising the maintenance or inspection program, as applicable, to incorporate new or revised maintenance instructions and airworthiness limitations. We are issuing this AD to address the unsafe condition on these products.
Airworthiness Directives; Airbus Airplanes
Document Number: 2018-14687
Type: Rule
Date: 2018-07-19
Agency: Federal Aviation Administration, Department of Transportation
We are adopting a new airworthiness directive (AD) for certain Airbus Model A318 series airplanes; Model A319 series airplanes; Model A320-211, -212, -214, -216, -231, -232, and -233 airplanes; and Model A321-111, -112, -131, -211, -212, -213, -231, and -232 airplanes. This AD was prompted by reports of early cracking on certain holes of the crossbeam splicing at certain fuselage frames. This AD requires repetitive inspections for cracking of the fastener holes in certain fuselage frames, and depending on airplane configuration, provides an optional terminating action to the repetitive inspections. We are issuing this AD to address the unsafe condition on these products.